middot

D0 SOLENOID UPGRADE PROJECT

Thermal Contraction analysis

for the D0 Solenoid Chimney

O-ZERO ENGINEERING NOTE 3823111 EN-349

September 30 1993

Russ Rucinski ROOflJ Mechanical Group

~

r

This engineering note documents the thermal contraction analysis that was done for the D-Zero solenoid chimney The analysis was done as support of the Design Report of the 2 Tesla Superconducting Solenoid for the Fermilab DO Detector upgrade tI

SUMMARY

The cryogenic LHE and LN2 lines were analyzed for combined pressure thermal movement and dead weight The tubing was stress analyzed per ASME code for Pressure Piping standard ANSI ASME B313 for eight combinations of thermal loading A commercial pipe stress analysis and design system by Algorreg was used for the analysis Stresses calculated were well below allowables Based on the analysis the cryogenic lines will be installed at an offset from the vacuum jacket centerline so that during steady state cold operation the cryogenic lines will be in a proper location

ANALYSIS

The chimney route as of this writing follows the path shown in Figure 1 The majority of the analysis was done almost a year earlier (1192 thru 12192) with a slightly different path The difference in the path is in the longest inclined section At the time of analysis it was thought that the chimney would be straight up the incline and then elbow at 90 degrees into the side of the control dewar The analysis was done for that configuration See Figures 2 and 3 for a sketch showing the route and the locations of the spider support guides for the cryogenic piping The slight difference in the chimney path route will not significantly change the outcome of the analysis and therefore the results from the analysis that was done is still considered valid

The analysis was done using Pipe Plus Pipe Stress Analysis and Design System software version 450 from Algorreg This DOS application was borrowed from the RDlMechanica1 support group A copy of the application and case files used in the analysis can be found on the hard drive of the mM machine in the D-Zero cryo control room The computer is a Gateway 2000 model 4DX-33V with a Fermilab property number 78384 The files ~n hard drive C directory PIPE To run the software run the file named PIPEEXE The software filetl menu will allow access to all case files See table 1 for the cases Cases 12 and 3 are saved under filename tlCASEI23 Cases 4 and 5 are saved as CASE4amp5

2 For each case run the results were from the combined effect of

Dead Weight + Pressure + Thermal contraction + Displacement

Dead Weight considered the pipe itselfplus contents with SG - 10

Pressure was always 150 psig

Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall

TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold

CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable

Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads

Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar

Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction

Case 3 Rather trivial case

3

Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage

Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm

Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5

Case 8 Trivial case not run

Allowable

The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded

The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is

Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi

The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi

4

-

Results

The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs

The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2

TABLE 2 Built in offsets to compensate for thermal movement

Location X Offset ny Offset Z Offset

TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches

HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

r

This engineering note documents the thermal contraction analysis that was done for the D-Zero solenoid chimney The analysis was done as support of the Design Report of the 2 Tesla Superconducting Solenoid for the Fermilab DO Detector upgrade tI

SUMMARY

The cryogenic LHE and LN2 lines were analyzed for combined pressure thermal movement and dead weight The tubing was stress analyzed per ASME code for Pressure Piping standard ANSI ASME B313 for eight combinations of thermal loading A commercial pipe stress analysis and design system by Algorreg was used for the analysis Stresses calculated were well below allowables Based on the analysis the cryogenic lines will be installed at an offset from the vacuum jacket centerline so that during steady state cold operation the cryogenic lines will be in a proper location

ANALYSIS

The chimney route as of this writing follows the path shown in Figure 1 The majority of the analysis was done almost a year earlier (1192 thru 12192) with a slightly different path The difference in the path is in the longest inclined section At the time of analysis it was thought that the chimney would be straight up the incline and then elbow at 90 degrees into the side of the control dewar The analysis was done for that configuration See Figures 2 and 3 for a sketch showing the route and the locations of the spider support guides for the cryogenic piping The slight difference in the chimney path route will not significantly change the outcome of the analysis and therefore the results from the analysis that was done is still considered valid

The analysis was done using Pipe Plus Pipe Stress Analysis and Design System software version 450 from Algorreg This DOS application was borrowed from the RDlMechanica1 support group A copy of the application and case files used in the analysis can be found on the hard drive of the mM machine in the D-Zero cryo control room The computer is a Gateway 2000 model 4DX-33V with a Fermilab property number 78384 The files ~n hard drive C directory PIPE To run the software run the file named PIPEEXE The software filetl menu will allow access to all case files See table 1 for the cases Cases 12 and 3 are saved under filename tlCASEI23 Cases 4 and 5 are saved as CASE4amp5

2 For each case run the results were from the combined effect of

Dead Weight + Pressure + Thermal contraction + Displacement

Dead Weight considered the pipe itselfplus contents with SG - 10

Pressure was always 150 psig

Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall

TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold

CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable

Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads

Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar

Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction

Case 3 Rather trivial case

3

Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage

Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm

Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5

Case 8 Trivial case not run

Allowable

The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded

The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is

Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi

The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi

4

-

Results

The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs

The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2

TABLE 2 Built in offsets to compensate for thermal movement

Location X Offset ny Offset Z Offset

TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches

HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

2 For each case run the results were from the combined effect of

Dead Weight + Pressure + Thermal contraction + Displacement

Dead Weight considered the pipe itselfplus contents with SG - 10

Pressure was always 150 psig

Thermal contraction was based on LN2line cold was at -320 F LHe line cold was at -452 F Pipe materials were 112 amp 34 OD aluminum tubing x 0065 wall

TABLE 1 Thermal combinations considered and the maximum stresses from the analysisThe 8 combinations considered W-warm C-cold

CASES LN2LINE LHeLINE SOlENOID Max StlC~~ 1 W C W 59 ksi HE7 2 W C C 60ksi HE6 3 W W C 34ksi HE3 4 C C C 37 ksi HEOb 5 C C W 35 ksi HE6 6 C W C 27 ksi TL6b 7 C W W 27 ksi TL6b 8 W W W not applicable

Displacement was used at anchor points In cases when the solenoid was cold the LHe anchor HEOa was displaced See appendix for calculation of solenoid displacement In cases 4 amp 5 the support locations along the LHe line were displaced to account for the LN2 piping being displaced by thermal and dead weight loads

Comments about the cases Case 1 Guides were used along the LHe line except at the ends which were anchors The guides were considered fixed in space allowing the piping only to move axially The anchor at HEOa was rigid in all directions The anchor at HE9 was free to move simulating built in flexibility in the coptrol dewar

Case 2 Modeled the same as Case 1 except displacement was added at the HEOa anchor due the solenoid contraction

Case 3 Rather trivial case

3

Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage

Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm

Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5

Case 8 Trivial case not run

Allowable

The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded

The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is

Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi

The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi

4

-

Results

The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs

The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2

TABLE 2 Built in offsets to compensate for thermal movement

Location X Offset ny Offset Z Offset

TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches

HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

3

Case 4 Modeled conservatively by changing the guides along the LHe piping into anchors which were rigid except for allowing rotations of the pipe The anchors were displaced by the amount the LN2 piping at each location was displaced The LN2 piping was modeled with an anchor at each end and guides along the pipe In addition the anchor at HEOa was displaced due to the solenoid shrinkage

Case 5 Modeled the same as case 4 except the anchor at HEOa was not displaced because the solenoid was warm

Cases 6 amp 7 The LN2 piping was modeled with an anchor at each end and guides along the pipe The loading conditions for the LN2 piping for this case is identical to that in cases 4 amp 5 Therefore a separate run was not made The stresses and displacements for the LN2 piping in these cases can be read off the output of cases 4 amp 5

Case 8 Trivial case not run

Allowable

The allowable stress used was derived from ANSI ASME B313-1984 code The allowable stress SE listed in Table A-1 is 80 ksi for 6061-T6 seamless pipe and tube that is welded

The allowable stress for stresses due to displacement strains is calculated from section 30235 Equation (la) of the code This stress is

Sa - f (125 Sc + 025 Sh) 10 ( 12580 + 02580) - 120 ksi

The Algorreg piping analysis package prints out an allowable next to the system stress output that is 200 ksi I do not agree with this value Im not exactly sure how the program calculated this because the allowable of 80 ksi was input by me as material data information My feeling is that there is a mistake in the program such that instead of Sa simplifying out to be 15 Sc (due to Sc - Sh) Sa simplified out to 25 Sc I can easily see how this could happen ifEquation (la) was mistyped Another possibility is tIlaJlam not interpreting the code to its fullest extent It is my judgement that the allowable stress to which the piping program output should be compared to is 120 ksi

4

-

Results

The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs

The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2

TABLE 2 Built in offsets to compensate for thermal movement

Location X Offset ny Offset Z Offset

TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches

HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

4

-

Results

The output from the analysis is attached to this note The output shows that the stresses calculated from any combination of thermal loading are well below the allowable of 120 ksi It is also worth noting that the stresses are well distributed along the tubing runs

The construction of the chimney is such that the LHe and LN2 tubing are built with a warm offset at various locations that enable the tubing to displace to a centered position during cryogenic operation The output from the analysis determined the magnitude and location of these built in warm offsets See Table 2

TABLE 2 Built in offsets to compensate for thermal movement

Location X Offset ny Offset Z Offset

TR6 + 0375 inches ------- ----shyTR7 - 0350 inches ------ + 029 inches

HE6 + 0375 inches ------- ------shyHE7 - 0350 inches ------- + 029 inches

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

5 INTDtACTION POIIII1

bull

i----I33000--+----f

J--~-----+--U77IO_t+_fII_--

C ____l

Figure I-Chimney Routing

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

_cno

1

IGr

~

PA

8C

FE

RM

ILA

B

RD

ocent

tyen6 u

~ 3

82

31

-6

0

EN

GIN

EE

RIN

G

NO

TE

~O-EfIolOD

LHe

~ ~

~l

)

jcO JI

U

-s a ~ ~

~

vA 9 ) -)

l= I G

UR

E

ZL-______________________________________

__________________---------------shy~

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

r-ta-=----- -----

~~

38

2a

III --7 H

-ERMI-LA-----~r-miiCii itbullbullcrrft

iO-

Ti

E

NG

INE

ER

ING

N

OT

E

RD

ccent

JyenI5 8

UIE

CT

~OLe-lOC Co ftIN

E-I

Su

PP

QA

TS

LN-z

PI P

-l u

2gt s

FIG

UR

E

~~---------------------------------

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

) )

)

PIPEPLUS VERSION 450 FERMI NATL ACCELERATOR LAB 010693 1605 D-ZERO SOLENOID UPGRADE CHIMNEY DESIGN

21 (j

~ rn ~ G jQ y 1)

r (

o c -4 1 C -

sect8 8

NoTE T-~ OorPOT wAS oeTAIN~() PRc- To

T~i F~p- ~u

PO~Ts t-lE0Q I-t~ NOT 5-OuJN

y

z~ X

m

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

File Name Project Department Contract Number Description Prepared by Checked by

ANSI code Input unit Output unit Output columns Base temperature F factor E factor

Number of dynamic modes Cut-off frequency Max no of iterations Convergence tolerance Force tolerance

CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Research DivisionD-Zero Mechanical Serial 3823111 Liquid Nitrogen amp Liquid Helium lines Russ Rucinski

ANSI B313 English English 80 70 10 133

0 0 Hz 0 0 0 lb

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

I

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~ D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Frm Point OX DY DZ Radius X Y Z To name (feet) (feet) ( feet) ( inch) (feet) (feet) (feet)

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 00 T TR2 0 0 46373 Short 0000 0000 03 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 05 T TR3 82170 -17687 16338 1370 -0295 06 T TR4 351470 -75657 69884 891875 4298 -0925 12middot T TR5 285434 -61442 -14557 6677 -1437 00 C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04shyC Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -60096 Long 8611 -1847 -09 C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 22 T TR6b 0 0 381782 8579 -1847 53 cPt TR7 is -35 in X and +029 in Z to bring to nom location when col T TR7 -035 0 384682 Long 8550 -1847 85 C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when war T TR7a 415738 544685 -029 12015 2692 85 T TR7b 826876 108937 0 18905 11770 85 T TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 95 F HEOa -353 1913 0 -0294 0159 00 T HEOb -260 0 0 Long -0511 0159 00 T HEl 0 0 203 -0511 0159 01 T HE2 0 0 505166 Long -0511 0159 05 T HE3 177721 -38256 353368 0970 -0159 08 T HE4 353646 -76125 703164 89875 3917 -0794 14 T HE5 287412 -61869 -14658 6312 -1309 02 C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -06 C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -1737 13 T HE6b 0 0 218808 8020 -1t37 31 T HE6c 0 0 218808 8020 -1737 50 T HE6d 0 0 218808 8020 -1737 68 C Pt HE7 is -35 in X and +029 in Z to bring to nom location when cold T HE7 -035 0 242900 Long 7991 -1737 88 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate f C HE7 warm deviation from nominal location 8810603 1668T HE7a 313353 408512 -029 8814906 7341T HE7b 516422 680854 0 8819210 13015T HE7c 516422 680854 0 T HE8 309854 408512 0 Long 21792 16419 88

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

-------- -------- -------- -------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASf

Frm Point DX DY DZ Radius X Y l~

To name (feet) (feet) (feet) (inch) (feet) (feet) (feet)

T HE9 o o 12 21792 16419 98 C C The points below TLn represent the top left LN2 piping

o O(F TL1 -300 0 o -0250 0000 T TL2 0 0 550 -0250 0000 04

T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 01 T TL4 355822 -76593 707489 905625 4308 -0981 13 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -03 CPt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06 CPt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53 CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jOg using pt TL7 and TL7a1 was required to maintain the correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7 a 1 4 160 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 f C Pt TL8 was stopped short by 5 to approximate actual piping relationsh~ T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page

- D-Zero Solenoid Upgrade CHIMNEY DESIGN Fi Ie CASE

Point Data Description

TRl Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) (inchinch) 1 70 150 0000000 2 70 150 0000000 3 70 150 0000000

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

TR2

-------------------------------------------------

101593 1057 PagePipePlus version 450 Fermi Natl Accelerator Lab File CASED-Zero Solenoid Upgrade CHIMNEY DESIGN

Point Data Description

TR2a Guide TR3 TR4 TR5 TR5a Guide TR6 TR6a Guide TR6b Guide TR7 TR7a Line stop

Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lbinch)

X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree Free Y restraint during hanger design

HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 lbcuft Content S G = 10

Material Data Identifier = AL Load Load data identifier = LHE

Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)

1 -452 150 -0003900 2 -452 150 -0003900

lt

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAsr

Point Data Description

3 70 150 0000000 Anchor Rigid in all directions

Initial displacement (inchdegree) Case 1 translational X = 0000 inch Case 1 translational Y = 0000 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0000 inch Case 2 translational Y = 01120 inch Case 2 translational Z = 0000 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0000 inch Case 3 translational Y = 01120 inch Case 3 translational Z = 0000 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degree Case 3 rotational Z = 0 degree

HEOb HE1 HE2 HE3 Guide HE4 Guide HE5 Guide HE6 HE6a Guide HE6b HE6c HE6d Guide HE7 HE7a Guide HE7b Line stop

Guide HE7c Guide HE8 HE9 Anchor Translational stiffness (lbinch)

X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case Case Case Case Case

1 1 1 1 2

translational Z = 0 rotational X = 0 rotational Y = Q rotational Z = 0 translational X = 0

inch degree degree degree

inch Case 2 translational Y = 0 inch Case 21 translational Z = 0 inch

----- -------- -------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point Data Description

Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design

TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions

Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-

TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide

~- TL6c TL7 TL7al TL7a Line stop

Guide TL7b Guide TL8

----- -------- -------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~

Point Data Description

TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch

Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree

Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch

Case 2 translational Y 0 inch Case 2 translational Z 0 inch

Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree

Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree

y Case 3 rotational 0 degree Case 3 rotational Z 0 degree

Free Y restraint during hanger design

-

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE

Case number Combination

1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 HEOa Fx

Fy Fz Mx

0 -1

0 2

0 0 0 0

4 0 --gt J

44

-1 -6 -0

0

0 0 0 0

5 -1

4 46

-

r

HE3

HE4Near

HE5

HE6a

HE6d

HE7a

HE7b

HE7b

HE7c

HE9

My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz

2 1 0 1

-0 -0 -2 -0 -0

0 -0 -1

0 -2

0 1 0

-3 -4

1 -1 -0

1 -1 -0

0 -0

0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

14 2 4

17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

-6 -18

0 0

-2 -2

-13 -3

0 -0 -9 -0

0 -0

0 -0 -3 -4 -6

0 -0 -0

0 -0 -0 -0 -0 -0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

~

17 3 4

18 1

-0 -2 -0

2 4

-0 -1

7 6 0 1 0

-3 -4

1 -1

0 1

-1 -0

0 -0

0 -0 -0 -0

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

----- -------- -------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 1015931057Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point Data Description

Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Case 3 translational X = 0 inch Case 3 translational Y = 0 inch Case 3 translational Z = 0 inch Case 3 rotational X = 0 degree Case 3 rotational Y = 0 degreeCase 3 rotational Z = 0 degreeFree Y restraint during hanger design

TLl Pipe Pipe data identifier = 12Material Data Identifier = AL Load Load data identifier = LN2 Anchor Rigid in all directions

Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 degreeCase 2 translational X = 0 inchCase - translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0 degreeCase 3 translational X = 0 inchCase - translational Y = 0 inch Case - translational Z = 0 inch Case 3 rotational X = 0 degreeCase 3 rotational Y = 0 degreeCase rotational Z = 0 degree-

TL2 TL2a Guide TL3 TL4 TLS TLSa Guide TL6 TL6a Guide TL6b Guide

~- TL6c TL7 TL7al TL7a Line stop

Guide TL7b Guide TL8

----- -------- -------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~

Point Data Description

TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch

Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree

Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch

Case 2 translational Y 0 inch Case 2 translational Z 0 inch

Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree

Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree

y Case 3 rotational 0 degree Case 3 rotational Z 0 degree

Free Y restraint during hanger design

-

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE

Case number Combination

1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 HEOa Fx

Fy Fz Mx

0 -1

0 2

0 0 0 0

4 0 --gt J

44

-1 -6 -0

0

0 0 0 0

5 -1

4 46

-

r

HE3

HE4Near

HE5

HE6a

HE6d

HE7a

HE7b

HE7b

HE7c

HE9

My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz

2 1 0 1

-0 -0 -2 -0 -0

0 -0 -1

0 -2

0 1 0

-3 -4

1 -1 -0

1 -1 -0

0 -0

0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

14 2 4

17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

-6 -18

0 0

-2 -2

-13 -3

0 -0 -9 -0

0 -0

0 -0 -3 -4 -6

0 -0 -0

0 -0 -0 -0 -0 -0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

~

17 3 4

18 1

-0 -2 -0

2 4

-0 -1

7 6 0 1 0

-3 -4

1 -1

0 1

-1 -0

0 -0

0 -0 -0 -0

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

----- -------- -------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~

Point Data Description

TL9 Anchor Translational stiffness (lbinch) X=Free Y=Free Z=Free Rotational stiffness ( lb- i nchdeg ) X=Free YFree Z=Free Initial displacement ( inch degree) Case 1 bull translational X = 0 inch Case 1 translational Y = 0 inch Case 1 bull translational Z = 0 inch

Case 1 rotational X 0 degree Case 1 bull rotational Y 0 degree

Case 1 rotational Z == 0 degree Case 2 translational X = 0 inch

Case 2 translational Y 0 inch Case 2 translational Z 0 inch

Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree

Case 3 translational X 0 inch - Case translational Y 0 inch Case - translational Z = 0 inch Case 3 rotational X 0 degree

y Case 3 rotational 0 degree Case 3 rotational Z 0 degree

Free Y restraint during hanger design

-

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE

Case number Combination

1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 HEOa Fx

Fy Fz Mx

0 -1

0 2

0 0 0 0

4 0 --gt J

44

-1 -6 -0

0

0 0 0 0

5 -1

4 46

-

r

HE3

HE4Near

HE5

HE6a

HE6d

HE7a

HE7b

HE7b

HE7c

HE9

My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz

2 1 0 1

-0 -0 -2 -0 -0

0 -0 -1

0 -2

0 1 0

-3 -4

1 -1 -0

1 -1 -0

0 -0

0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

14 2 4

17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

-6 -18

0 0

-2 -2

-13 -3

0 -0 -9 -0

0 -0

0 -0 -3 -4 -6

0 -0 -0

0 -0 -0 -0 -0 -0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

~

17 3 4

18 1

-0 -2 -0

2 4

-0 -1

7 6 0 1 0

-3 -4

1 -1

0 1

-1 -0

0 -0

0 -0 -0 -0

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File ~ASE

Case number Combination

1 DW + Pres1 + Ther1 + Disp1 2 DW + Pres2 + Ther2 + Disp2 3 DW + Pres3 + Ther3 + Disp3

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 HEOa Fx

Fy Fz Mx

0 -1

0 2

0 0 0 0

4 0 --gt J

44

-1 -6 -0

0

0 0 0 0

5 -1

4 46

-

r

HE3

HE4Near

HE5

HE6a

HE6d

HE7a

HE7b

HE7b

HE7c

HE9

My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz

2 1 0 1

-0 -0 -2 -0 -0

0 -0 -1

0 -2

0 1 0

-3 -4

1 -1 -0

1 -1 -0

0 -0

0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

14 2 4

17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

-6 -18

0 0

-2 -2

-13 -3

0 -0 -9 -0

0 -0

0 -0 -3 -4 -6

0 -0 -0

0 -0 -0 -0 -0 -0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

~

17 3 4

18 1

-0 -2 -0

2 4

-0 -1

7 6 0 1 0

-3 -4

1 -1

0 1

-1 -0

0 -0

0 -0 -0 -0

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page ~D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max M --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TRl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TR5a Fz 0 0 0 0 0 0 TR6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TR7a Fx 1 0 0 0 0 1 TR7b Fx 1 0 0 0 0 1 TR9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 HEOa Fx

Fy Fz Mx

0 -1

0 2

0 0 0 0

4 0 --gt J

44

-1 -6 -0

0

0 0 0 0

5 -1

4 46

-

r

HE3

HE4Near

HE5

HE6a

HE6d

HE7a

HE7b

HE7b

HE7c

HE9

My Mz Fx Fy Fz Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fz Fx Fy Fx Fy Fz Fx Fy Fz Fx Fy Fz Mx My Mz

2 1 0 1

-0 -0 -2 -0 -0

0 -0 -1

0 -2

0 1 0

-3 -4

1 -1 -0

1 -1 -0

0 -0

0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

14 2 4

17 1 0 0 0 2 4 0 0 7 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

-6 -18

0 0

-2 -2

-13 -3

0 -0 -9 -0

0 -0

0 -0 -3 -4 -6

0 -0 -0

0 -0 -0 -0 -0 -0 -0 -0 -0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

~

17 3 4

18 1

-0 -2 -0

2 4

-0 -1

7 6 0 1 0

-3 -4

1 -1

0 1

-1 -0

0 -0

0 -0 -0 -0

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 D-Zero Solenoid Upgrade

Fermi Natl CHIMNEY DESIGN

Accelerator Lab 101593 10S7i=lage File CASE

Support Summary Forceslb or Momentsinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy ------shy -------TLl Fx 1 0 0 0 0 1

Fy 1 0 0 0 0 1 Fz 0 0 0 0 0 0 My 2 0 0 0 0 2 Mz 1 0 0 0 0 1

TLSa Fz 0 0 0 0 0 0 TL6b Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0 TL7a Fx 1 0 0 0 0 1 TL7b Fx 1 0 0 0 0 1 TL9 Fx 0 0 0 0 0 0

Fz 0 0 0 0 0 0

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

Pip~Plus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 12 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~ad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204

0027 0057 0000 0191 -0059 0205TR6Far TR6a -0000 -0000 0000 -0011 -0057 0229 TR6b -0000 -0000 0000 0122 0163 0256

0277TR7Near 0214 -0163 0002 0263 0383 0262 0278TR7Far 0216 -0165 0002 0379

TR7a 0000 -0000 --0000 0142 0173 -0141

TR7b -0000 -0000 -0000 -0169 -0211 0131

0229 -0174 0008 -0281 -0433 0294TR8Near -0282 -0438 -0292~R8 Far 0227 -0173 0009

-0447 -0282rR9 0139 -0117 0009 -0285

HEOa 0000 -0000 0000 0000 0000 0000 0008 0014 0002HEObNear 0006 -0000 0000 0020 0035 0005

HEObFar 0011 -0000 -0004 00040011 -0001 -0007 0022 0036HEl 0006 0002-0002 -0023 0022HE2Near 0013

0013 -0053 0000HE2Far 0009 --0002 -0027

-0056 0016 HE3 -0062 0013 -0012 0027

0039 -00120Ol8 -0017 0060HE4Near -0085 0073 -0560 01260053 0102HE4Far -0253 0071 -0590 0140

HE5 -0249 0061 0126 0217 -0049 0203

HE6Near -0232 0162 0307 0321 01960163 0298 0305HE6Far -0232 01300505 0495

HE6a -0000 -0000 0216

HE6b 0048 -0182 0130 0362 0139 0066 0001-0196 -0164

HE6c -0029 -0224 0045 0420 -0064

HE6d 0001 0000 -0040 -1003 -01150462 -0127 -0945 0472

HE7Near 0242 0295 -0117

0249 0474 -0148 -0715HE7Far 0182 -0443 -01000265 -0000HE7a 0201 0065-0271 -0174-0000 -0000 0000HE7b -0160-0000 -0193 -0307-0201 -0266HE7c

-0106 -0583 0010 -0296 -0273 -0350 HE8Near -0349-0308 -0266-0585 -0016HE8Far -0109

-0259 -0346 -E9 -0159 -0525 -0058 -0322

0000 -0000 0000 00000000 0000ILl

0000 -0025 0006 00250001 0002

0004 -0101TL2 0000 -0000 0000 0044

TL2a 0114 0019 -0274-0004-0005 -0031TL3

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

--

--------- ---------- ---------- ---------- ---------- ---------- ----------

~ipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 13 8-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z

-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 -0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -0171 -0299 -0257

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl IAeee crator Lab 101593 1057 Pag p 14D- Zero S 0 I enoid Upgrade CHIMNEY DESIGN shy~d D ad W ht File CASE12~ y ~ e elg + Pressure 1 + Tht=gtrmal 1 I ~bull ~ + D1SP acement 1

System Stresses (ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000

517 1166 1167 1273 20000TR6b 100 100 001 TR7Near 100 100 001 517 299 517 406 20000

530 340 20000TR7Far 100 100 001 517 233 1590 20000TR7a 100 100 001 517 1435 1439

100 100 001 517 1469 1473 1594 20000~7b 200008Near 100 100 001 517 257 532 367

422 20000lH8Far 100 100 001 517 314 518 20000TR9 100 100 001 517 243 518 350

805 1065 1125 1236 20000HEOa 100 100 002 805 935 1022 1105 20000HEObNear 123 102 002

595 806 683 20000HEObFar 123 102 002 805 806 643 20000HEl 100 100 002 805 507

1490 1576 20000HE2Near 123 102 002 805 1490 002 805 1612 1613 1689 20000HE2Far 123 102

1475 20000805 1392 1393HE3 100 100 002 1945 20000HE4Near 100 100 002 805 1719 1720 1747 20000805 1389 1391HE4Far 100 100 002

20000805 1280 1282 1760HE5 100 100 002 20000

HE6Near 102 002 805 5666 5666 5738 5449 5451 5568 20000HE6Far 123 102 002 805

3339 3690 20000HEba 100 100 002 805 3337

1936 2104 20000HE6b 100 100 002 805 1931

2764 2861 20000HE6c 100 100 002 805 2761

4293 5090 20000HE6d 100 100 002 805 4292

5334 5523 20000HE7Near 123 102 002 805 5334

5857 20000HE7Far 123 102 002 805 5719 5719 2048 20000805 1562 1562HE7a 100 100 002

805 782 815 1087 20000HE7b 100 100 002

200001146 1147 1336HE7c 100 100 002 805 581 807 830 20000

HE8Near 123 102 002 805 20000567 806 8081-8Far 1 23 102 002 805

343 806 453 2000019 100 100 002 805

722 751 829 20000TLl 100 100 001 517

20000TL2 100 100 001 517 364 541 471 1600 20000517 1493 1498TL2a 100 100 001

----------~ ~~ ~~-- --- ---- -shy

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

1 A 1 t L b 101593 1057 Page 150ipePlus version 450 Fermi Nat cce era or a File CASE123 )-Zero Solenoid Upgrade CHIMNEY DESIGN _oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

Point Name

TL3 fL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

System Stresses (ANSI B313) In- Out

Plane Plane Section Stressespsi SIF SIF Modulus Hoop Longitu Principal

100 100 001 517 885 897 100 100 001 517 503 576 100 100 001 517 607 668 100 100 001 517 535 620 100 100 001 517 439 580 100 100 001 517 321 555 100 100 001 517 424 519 100 100 001 517 405 518 100 100 001 517 1497 1497 100 100 001 517 251 517 100 100 001 517 328 517 100 100 001 517 322 519 100 100 001 517 241 532 100 100 001 517 1532 1536 100 100 001 517 1410 1414 100 100 001 517 255 532 100 100

100 100

001 001

517 517

318 518 518

Code

992 610 714 641 546 428 530 512

1604 358 435 429 347

1687 1534

365 425 329

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 200(

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

middot PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 16 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~d Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement 0335 inch at point TL7a1Nea Maximum Y displacement -0585 inch at point HE8Far

Maximum Z displacement 0307 inch at point HE6Near

Maximum X rotation -1003 degree at point HE6d Maximum Y rotation = -0590 degree at point HE5 Maximum Z rotation -- 0447 degree at point TL7

Maximum X force -7 Ib at point HE5 Maximum Y force -- 9 Ib at point HE7b

Maximum - force -4 Ib at point HEOa

Maximum X moment 76 inch-lb at point HE7Far Maximum Y moment = 93 inchlb at point HE6Near i1ax imum Z moment -18 inch-lb at point HE7c

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 5719 psi at point HE7Far Maximum principal stress = 5719 psi at point HE7Far Maximum code stress = 5857 psi at point HE7Far Maximum stress ratio (codeallowable) = 029 at point HE7Far

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

bullPipePlus version 450 Fermi Natl Accelerator Lab 101593 10 57 Page 17 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 OOlS TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0OS7 -0015 0303 -010S 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 -middot0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 -0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131 TRSNear 0229 -0174 0008 -0281 -0 -433 -0294 TRSFar 0227 -0173 0009 -0282 -0-438 -029 TR9 0139 -0117 0009 -0285 -0447 -02Si HEOa 0000 0112 0000 0000 0000 -0000 HEObNear 0006 0112 0000 0058 0008 -0019 HEObFar 0010 0111 -0004 0140 0015 middot0064 HEl 0011 o 10S -0008 0161 0012 -0089 HE2Near 0011 0094 -0024 0213 -0023 -0202 HE2Far 0005 0087 -0028 0228 -0OS5 -0263 HE3 -0083 0018 -0017 0164 -OOSl -0046 HE4Near -0107 0023 -0021 0159 0016 0043 HE4Far -0271 0058 0110 0096 -05S2 0107 HE5 -0267 0066 0135 0093 -0610 0123 HE6Near -0250 0166 0315 0231 -0028 0199 HE6Far -0250 o 16S 0306 0319 0357 0192 HE6a -0000 -0000 0224 0512 0535 0126 HE6b 0057 -0183 0138 0364 -0134 0060 HE6c -0023 -0226 0053 -0199 -0177 -0006 HE6d 0000 0000 -0032 -1010 0404 -0072 HE7Near 0237 0466 -0119 -0957 0462 -0123 HE7Far 0244 0478 -0140 -0729 0287 -0125 HE7a 0201 0265 -0000 0168 -0450 -0105 HE7b -0000 -0000 0000 middot0277 -0185 0066 HE7c -0201 -0266 -0000 -0200 -0316 -0161 HESNear -0105 -0584 -0010 -0302 -0281 -0352 HESFar -0108 -0586 -0016 -0314 -0275 -0351 HE9 -0159 -0524 -0058 -0329 -0267 -03shyTLI 0000 0000 0000 -0000 0000 OO~ Tl2 0001 0002 0000 -0025 0006 0025 TL2a 0000 -0000 0000 0044 0004 -0101 TL3 -0005 -0031 -0004 0114 0019 -0274

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 10=57 Page 18 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA5E123 l~d Dead Weight + Pressure 2 + Thel-mal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---------shy ---------shy ---------shy ---------shy ---------shy ---------shyTL4Near -0012 -0066 -0009 0151 0021 -0336 TL4Far -0019 -0126 -0017 0285 -0107 0308 TL5 -0015 -0109 -0015 0283 -0107 0331 TL5a 0013 -0003 -0006 0230 -0085 0383 TL6Near 0025 0042 -0004 0195 --0066 0377 TL6Far 0026 0047 -0004 0187 -0058 0379 TL6a -0000 --0000 -0004 -0026 -0069 0400 TL6b 0000 -0000 -0004 0183 0210 0427 TL6c 0295 -0257 -0001 0428 0546 0446 TL7 0335 -0288 --0001 0424 0537 0447 TL7al Nea 0335 -0259 -0037 0420 0526 0447 TL7alFar 0333 -0254 -0040 0419 0523 0447 TL7a 0000 -0000 -0000 0277 0314 -0075 TL7b -0000 -0000 -0000 -0061 -0063 0143 TL8Near 0187 -0143 0007 -0166 -0281 -0268 TL8Far 0186 -0142 0008 -0166 -0287 -0267 TL9 0128 -0109 0008 -0171 -0299 -0257

I

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

--------- ----- ----- ------- -------- -------- -------- -------- --------

rJipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 19 )-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 ~oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses (ANSI 8313 ) In- Out

Point Plane Plane Section stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000

-))TR7Far 100 100 001 517 -- 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000 TR7b 100 100 001 517 1469 1473 1594 20000 TR8Near 100 100 001 517 257 532 367 200( TR8Far 100 100 001 517 314 518 422 2000 TR9 100 100 001 517 243 518 350 20000 HEOa 100 100 002 805 1145 2032 2702 20000 HEObNear 123 102 002 805 1498 2251 2858 20000 HEObFar 123 102 002 805 2138 2462 2793 20000 HE1 100 100 002 805 1847 2226 2563 20000 HE2Near 123 102 002 805 1512 1973 2335 20000 HE2Far 123 102 002 805 2120 2121 2229 20000 HE3 100 100 002 805 3468 3468 3582 20000 HE4Near 100 100 002 805 1852 1853 2035 20000 HE4Far 100 100 002 805 1362 1368 1731 20000 HE5 100 100 002 805 1250 1257 1749 20000 HE6Near 123 102 002 805 5880 5881 5951 20000 HE6Far 123 102 002 805 5643 5644 5762 20000 HE6a 100 100 002 805 3471 3473 3827 20000 HE6b 100 100 002 805 2000 2005 2178 20000 HE6c 100 100 002 805 2763 2766 2864 20000 HE6d 100 100 002 805 4315 4316 5113 20000 HE7Near 123 102 002 805 5303 5304 5492 20000 HE7Far 123 102 002 805 5690 5690 5828 20000 HE7a 100 100 002 805 1540 1540 2031 20000 HE7b 100 100 002 805 780 815 1082 20000 HE7c 100 100 002 805 1147 1148 1336 20000 HE8Near 123 102 002 805 581 807 830 20000 HE8Far 123 102 002 805 567 806 808 2001 HE9 100 100 002 805 343 806 454 20G TL1 100 100 001 517 722 751 829 20000 TL2 100 100 001 517 364 541 471 20000 TL2a 100 100 001 517 1493 1498 1600 20000

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

---------

PipePlus version 450 Fermi D-Zero Solenoid Upgrade CHIMNEY --ad Dead Weight + Pressure 2

System

In- Out Point Plane Plane Section Name SIF SIF Modulus --------shy ----shy ----shy ------shyTL3 100 100 001 TL4Near 100 100 001 TL4Far 100 100 001 TL5 100 100 001 TL5a 100 100 001 TL6Near 100 100 001 TL6Far 100 100 001 TL6a 100 100 001 TL6b 100 100 001 TL6c 100 100 001 TL7 100 100 001 TL7alNea 100 100 001 TL7alFa)shyTL7a

100 100

100 100

001 001

TL7b 100 100 001 TL8Near 100 100 001 A8Far 100 100 001

9 100 100 001

Natl Accelerator Lab 101593 1057 DESIGN File + Thermal 2 + Displacement shy

Stresses ( ANSI 8313)

Stressespsi Hoop Longitu Principal Code

------- -------- --------- -------shy517 885 897 992 517 503 576 610 517 607 668 714 517 535 620 641 517 439 580 546 517 321 555 428 517 424 519 530 517 405 518 512 517 1497 1497 1604 517 251 517 358 5 1-7 328 517 435 517 322 519 429 517 241 532 347 517 1532 1536 1687 517 1410 1414 1534 517 255 532 365 517 318 518 425 517 222 518 329

Page 20 CASE123

Allow

20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000 20000

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

middot N tl A celer~tor Lab 101593 1057 Page 21PipePlus version 4 50 Ferm1 a Ca

D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead Weight

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum

Maximum Maximum Maximum Maximum Maximum

+ Pressure 2 + Thermal 2 + Displacement 2

System Maxima

X displacement = 0335 inch at point TL7alNea Y displacement = -0586 inch at point HE8Far Z displacement = 0315 inch at point HE6Near

X rotation -1010 degree at point HE6d Y rotation -0610 degree at point HE5 Z rotation 0447 degree at point TL7

X force -8 lb at point HE3 Y force 12 Ib at point HE4Near Z force -3 lb at point HEOa

X moment 75 inch-lb at point HE7Far Y moment 97 inch-lb at point HE6Near Z moment 64 inch-lb at point HE3

hoop stress 805 psi at point HEOa longitudinal stress 5880 psi at point HE6Near principal stress 5881 psi at point HE6Ncar code stress 5951 psi at point HE6Near stress ratio (codeallowable) 030 at point HE6Near

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 22 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 l1qd Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TR1 0000 0000 0000 -0000 0000 0000 TR2Near 0000 0001 0000 -0021 0005 0016 TR2Far 0000 0001 0000 -0019 0002 0018 TR2a 0000 -0000 0000 0035 0003 -0075 TR3 -0005 -0025 -0004 0106 0016 -0234 TR4Near -0010 -0056 -0008 0146 0017 -0290 TR4Far -0015 -0102 -0017 0305 -0108 0235 TR5 -0011 -0087 -0015 0303 -0108 0249 TR5a 0012 -0002 -0006 0249 -0094 0241 TR6Near 0027 0055 -0000 0196 -0066 0204 TR6Far 0027 0057 0000 0191 -0059 0205 TR6a -0000 -0000 0000 -0011 0057 0229 TR6b -0000 -0000 0000 0122 0163 0256 TR7Near 0214 0163 0002 0263 0383 0277 TR7Far 0216 -0165 0002 0262 0379 0278 TR7a 0000 -0000 -0000 0142 0173 -0141 TR7b -0000 -0000 -0000 -0169 -0211 0131

rJR8 Near R8Far

0229 0227

-0174 -0173

0008 0009

-0281 -0282

-0433 -0438

-0294 -0292

rR9 0139 -0117 0009 -0285 -0447 -0282 HEOa -0000 0112 0000 0000 -0000 -0000 HEObNear --0000 0112 -0000 0053 -0003 -0021 HEOb FashyHE1

--0000 -0000

0111 0109

-0000 -0000

0129 0149

-0014 -0016

-0067 -0091

HE2Near HE2Far HE3 HE4Near HE4Far

-0002 -0003 -0020

0020 -0017

0096 0088 0004 0004 0003

-0000 -0001 -0004 -0004 0007

0202 0226 0145 0112 0045

-0022 -0029 -0029 -0024 -0036

-0202 -0261 -0054

0047 0006

HE5 -0016 0004 0008 0039 -0033 0001 HE6Near -0014 0005 0011 0009 0011 -0007 HE6Far -0014 0005 0010 0008 0027 -0006

HE6a -0000 -0000 0011 0033 0028 -0003 HE6b 0003 -0017 0011 0031 -0007 0002 HE6c -0001 -0015 0011 -0039 -0010 0006 HE6d -0000 -0000 0011 -0009 0019 0010 HE7Near 0014 -0011 0011 0035 0043 0013 HE7Far 0015 -0011 0011 0030 0044 0014

HE7a HE7b HE7c HE8Near HE8Far

~E9

L1 TL2 TL2a TL3

-0000 -0000 -0000

0193 0195 0157 0000 0001 0000

-0005

-0000 -0000 -0000 -0147 -0149 -0130 0000 0002

-0000 -0031

0000 -0000 -0000

0015 0016 0016 0000 0000 0000

-0004

-0005 -0046 -0093 -0101 -0100 -0100 -0000 -0025 0044 0114

0011 -0063 -0132 -0189 -0193 -0198 0000 0006 0004 0019

-0023 0040

-0139 -0318 -0317 -0314 0000 0025

-0101 -0274

~--~~~~~~

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

--------- ---------- ---------- ---------- ----------

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 23 D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123 Load Dead

Point Name

TL4Near TL4Far TL5 TL5a TL6Near TL6Far TL6a TL6b TL6c TL7 TL7alNea TL7alFar TL7a TL7b TL8Near TL8Far TL9

Weight + Pressure 3 + Thermal 3 + Displacement 3

System Deflections Displacementsinch Rotationsdegree

X Y Z X Y Z_-w ___ -- ____------_ _shy-0012 -0066 -0009 0151 0021 -0336 -0019 -0126 -0017 0285 -0107 0308 -0015 -0109 -0015 0283 -0107 0331 0013 -0003 -0006 0230 -0085 0383 0025 0042 -0004 0195 -0066 0377 0026 0047 -0004 0187 -0058 0379

-0000 -0000 -0004 -0026 -0069 0400 0000 -0000 -0004 0183 0210 0427 0295 -0257 -0001 0428 0546 0446 0335 -0288 -0001 0424 0537 0447 0335 -0259 -0037 0420 0526 0447 0333 -0254 -0040 0419 0523 0447 0000 -0000 --0000 0277 0314 -0075

-0000 -0000 -0000 -0061 -0063 0143 0187 -0143 0007 -0166 -0281 -middot0268 0186 -0142 0008 -0166 -0287 -0267 0128 -0109 0008 -middot0171 -0299 -0257

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 24D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE123~d Dead Weight + Pressure gt + Thermal- 3 + Displacement 3

System StresSes ( ANSI 831 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow ----------_ ----- ----~ ------- --------- -------- -------- --------shy---~-----

TRl 100 100 001 517 732 751 839 20000 TR2Near 115 100 001 517 287 534 394 20000 TR2Far 115 100 001 517 276 538 383 20000 TR2a 100 100 001 517 1406 1412 1513 20000 TR3 100 100 001 517 833 850 940 20000 TR4Near 100 100 001 517 475 573 582 20000 TR4Far 100 100 001 517 452 553 559 20000 TR5 100 100 001 517 372 538 478 20000 TR5a 100 100 001 517 637 656 744 20000 TR6Near 100 100 001 517 303 529 410 20000 TR6Far 100 100 001 517 348 518 455 20000 TR6a 100 100 001 517 315 518 422 20000 TR6b 100 100 001 517 1166 1167 1273 20000 TR7Near 100 100 001 517 299 517 406 20000 TR7Far 100 100 001 517 233 530 340 20000 TR7a 100 100 001 517 1435 1439 1590 20000

m7b 100 100 001 517 1469 1473 1594 20000 8Near 100 100 001 517 257 532 367 20000

517 314 518 422 20000TR8Fal 100 100 001 100 517 20000TR9 100 001 243 518 350 100 002 805 1118 1936 2566 20000HEOa 100

2743 20000HEObNear 123 102 002 805 1520 2188 123 102 805 2344 20000HEObFar 002 2007 2697

2131 2483 20000HEl 100 100 002 805 1740 1485 20000HE2Near 1 23 102 002 805 722 1996

1576 1580 1787 20000HE2Far 123 102 002 805 20000HE3 100 100 002 805 3213 3215 3373

100 100 805 944 20000HE4Near 002 920 1058 810 714 20000HE4Far 100 100 002 805 494

20000HE5 100 100 002 805 555 811 798 811 20000HE6Near 123 102 002 805 540 654

20000HE6Far 123 102 002 805 529 805 654 805 20000805 647 872HE6a 100 100 002 805 707 20000HE6b 100 100 002 805 535

100 100 805 805 20000HE6c 002 482 625 805 776 806 916 20000HE6d 100 100 002

20000HE7Near 123 102 002 805 403 805 520 1 ) 102 002 805 395 807 506 20000HE7Far - -

813 878 20000HE7a 100 100 002 805 734 100 100 805 809 20000HE7b 002 619 772

805 1110 1112 1237 20000HE7c 100 100 002 807 507 20000HE8Near 123 102 002 805 394

-8Far 123 102 002 805 401 806 511 20000 805 443 20000bull9 100 100 002 805 334

100 100 517 751 20000TLl 001 722 829 541 471 20000TL2 100 100 001 517 364

20000TL2a 100 100 001 517 1493 1498 1600

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

N tl A eler~tor Lab 101593 1057 Page 25FPipePlus version 450 erml a CC a File CASE123 D-Zero Solenoid Upgrade CHIMNEY DESIGN Load Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Stresses (ANSI 8313) In- Out

Point Plane plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allow

TL3 100 100 001 517 885 897 992 20000 TL4Near 100 100 001 517 503 576 610 20000 TL4Far 100 100 001 517 607 668 714 20000 TL5 100 100 001 517 535 620 641 20000 TL5a 100 100 001 517 439 580 546 20000 TL6Near 100 100 001 517 321 555 428 20000 TL6Far 100 100 001 517 424 519 530 20000 TL6a 100 100 001 517 405 518 512 20000 TL6b 100 100 001 517 1497 1497 1604 20000 TL6c 100 100 001 517 251 517 358 20000 TL7 100 100 001 517 328 517 435 20000 TL7alNea 100 100 001 517 322 519 429 20000 TL7alFar 100 100 001 517 241 532 347 20000 TL7a 100 100 001 517 1532 1536 1687 20000 TL7b 100 100 001 517 1410 1414 1534 20000 TL8Near 100 100 001 517 255 532 365 20000 TL8Far 100 100 001 517 318 518 425 20000 TL9 100 100 001 517 222 518 329 20e

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101593 1057 Page 26 ~ero Solenoid Upgrade CHIMNEY DESIGN File CASE123 I ld Dead Weight + Pressure 3 + Thermal 3 + Displacement 3

System Maxima

Maximum X displacement 0335 inch at point TL7alNea Maximum Y displacement = -0288 inch at point TL7 Maximum Z displacement -0040 inch at point TL7alFar

Maximum X rotation 0428 degree at point TL6c Maximum Y rotation 0546 degree at point TL6c Maximum Z rotation 0447 degree at point TL7

Maximum X force -3 lb at point HE3 Maximum Y force 12 lb at point HE4Near

Maximum Z force 1 lb at point HE3

=Maximum X moment -42 inch-lb at point HEOa Maximum Y moment 7 i nch- lb at point TL6b Maximum Z moment = 62 inch-lb at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3213 psi at point HE3 Maximum principal stress = 3215 psi at point HE3 Maximum code stress = 3373 psi at point HE3 Maximum stress ratio (codeallowable) = 017 at point HE3

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS

F i 1e Name CASE4amp5 Project D-Zero Solenoid Upgrade CHIMNEY DESIGN Department Research DivisionD-Zero Mechanical Contract Number Serial 3823111 Description Liquid Nitrogen amp Liquid Helium lines Prepared by Russ Rucinski Checked by

ANSI code ANSI B313 Input unit English Output unit English Output columns 80 Base temperature 70 F factor 10 E factor 133

Number of dynamic modes 0 Cut-off frequency 0 Hz Max no of iterations 0 Convergence tolerance 0 Force tolerance 0 lb

~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File C~S Frm Point DX DY DZ Radius x Y Z To name ( feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet ~

C Points HEO thru HEn represent the LHe supply line C Pt HEO moves when the solenoid is cold HEOa is attached c to the support cylinder C C Points TRl thru TRnn represent nodal points for the top right LN2 line C The supports are spider type supports LN2 shield to VJ C At the solenoid TRl doesnt move when sol is cold since sol shield C floats on panels supported off vacuum jacket F TRl 0 0 0 0000 0000 0(

o ~T TR2 0 0 46373 Short 0000 0000 C The first support is placed midway between TR2 and TR3 T TR2a 82170 -17687 16338 0685 -0147 OE T TR3 82170 -17687 16338 1370 -0295 OE T TR4 351470 -75657 69884 891875 4298 -0925 1 bull Z T TR5 285434 -61442 -14557 6677 -1437 0( C The second support is placed approx midway between TR5 and TR6 T TR5a 121639 -26184 -60645 7691 -1655 -04 C Point TR6 is moved 0375 in +X to bring it to nominal location when col T TR6 110389 -22955 -600~6 Long 8611 -1847 -oe C Pt TR6a offset in X is compensates for TR6 dev from nom when warm T TR6a -0375 0 381782 8579 -1847 T TR6b 0 0 381782 8579 -1847 C Pt TR7 is -35 in X and +029 in Z to bring to nom location when~ T TR7 -035 0 384682 Long 8550 -1847 8 [ C Pt TR7a offset in X amp Z compensates for TR7 deviation from nom when wa T TR7a 415738 544685 -029 12015 2692 8E T TR7b 826876 108937 0 18905 11770 8 shyT TR8 413438 544685 0 Long 22351 16309 85 T TR9 0 0 12 22351 16309 9 cshy

F HEOa -353 1913 0 -0294 0159 O ( T HEOb -260 0 0 Long -0511 0159 O ( T HEl 0 0 203 -0511 0159 o T HE2 0 0 505166 Long -0511 0159 O T HE3 177721 -38256 353368 0970 -0159 O f T HE4 353646 -76125 703164 89875 3917 -0794 1 T HE5 287412 -61869 -14658 6312 -1309 o ~ C Pt HE6 is +0375 longer in X to bring to nom location when cold T HE6 208721 -5128 -10535 Long 8052 -1737 -0( C Pt HE6a X offset is to compensate for HE6 deviation from nom when warm T HE6a -375 0 240000 8020 -b737 1 T HE6b 0 0 218808 8020 -1~37 3 T HE6c 0 0 218808 8020 -1737 5C T HE6d 0 0 218808 8020 -1737 6f C Pt HE7 is -35 in X and +029 in Z to bring to nom location when colr T HE7 -035 0 242900 Long 7991 -1737 8 C Pt HE7a offset in X is +35 more than nom and Z offset to compensate shyC HE7 warm deviation from nominal location T HE7a 313353 408512 -029 10603 1668 T HE7b 516422 680854 0 14906 7341 8 T HE7c 516422 680854 0 19210 13015 8 T HE8 309854 408512 0 Long 21792 16419 8

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Frm Point DX DY DZ Radius x Y Z To name (feet) ( feet) ( feet) ( inch) ( feet) (feet) (feet)

T HE9 o o 12 21792 16419 98shyC C The points below TLn represent the top left LN2 piping F TL1 -300 0 0 -0250 0000 00lt T TL2 0 0 550 -0250 0000 o 4~ T TL2a 108932 -23449 216594 0658 -0195 06 T TL3 82170 -17687 16338 1343 -0343 07shyT TL4 355822 -76593 707489 905625 4308 -0981 1 3 T TL5 289401 -62296 -14760 6719 -1500 01 T TL5a 121639 -26184 -60645 7733 -1718 -OT C Pt TL6 is moved +375 in X to bring it to nominal when cold T TL6 63751 -15456 -32267 Long 8264 -1847 -06middot C Pt TL6a X offset is to compensate for TL6 dev from nom when warm T TL6a -375 0 34118 8233 -1847 22( T TL6b 0 0 381782 8233 -1847 53t CPt TL6c is -35 in X and +29 in Z to bring to nom location when col T TL6c -035 0 384682 8204 -1847 85 C A jog using pt TL7 and TL7a1 was required to maintain tho correct spaci C of the LN2 lines T TL7 0 0 416 8204 -1847 89 T TL7a1 416 0 0 Long 8551 -1847 89 T TL7a 415738 544685 0 12015 2692 89 T TL7b 826876 108937 0 18906 11770 89 C Pt TL8 was stopped short by 5 to approximate actual piping relationship T TL8 392766 517451 0 Long 22179 16082 89 T TL9 0 0 12 22179 16082 99

~

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

-------- -------------------------------------------------

H

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Point

TRl

TR2 TR2a TR3 TR4 TR5 TR5a TR6 TR6a

Data Description

Pipe Pipe data identifier = 12 Nominal Diameter = 12 Pipe Schedule = Actual Pipe O D = 500 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Aluminum aluminum alloys Density = 00978 Ibcuinch Tempera Modulus Expansion (degF) (psi ) (inchinch) -325 11300000 -000390 -150 11100000 -000240 -50 10900000 -000139 70 10600000 000000 200 10400000 000167 300 10200000 000306 400 9500000 000449 500 8500000 000598 Temperature Allowable stresses

(degF) (psi) -320 8000

Load Load data identifier = LN2 Case Temperature Pressure Expansion

No (degF) (psig ) ( i nch inch) 1 -320 150 -0003857 2 -320 150 -0003857

Anchor Rigid in all directions Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degreeCase 1 rotational Y = 0 degree Case 1 rotational Z = 0 degreeCase 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

Guide

Guide

Guide

-------------------------------------------------

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page File CASf~ D-Zero Solenoid Upgrade CHIMNEY DESIGN

Point Data Description

TR6b Guide TR7 TR7a Line stop

Guide TR7b Guide TR8 TR9 Anchor Translational stiffness (lblinch)

X=FREE Y=FREE Z=FREE Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = 0 inch Case 1 translational Y = 0 inch Case 1 translational Z = 0 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 0 inch Case 2 translational Y = 0 inch Case 2 translational Z = 0 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree Free Y restraint during hanger design

HEOa Pipe Pipe data identifier = 34 Nominal Diameter = 34 Pipe Schedule = Actual Pipe O D = 0750 inch Wall Thickness = 0065 inch Corrosion Allowance = 0 inch Insulation Thickness = 0 inch Insulation Density = 0 Ibcuft Content S G = 10

Material Data Identifier = AL Load Load data identifier = LHE

Case Temperature Pressure Expansion No (degF) (psig ) (inchinch)

1 -452 150 -0003900 2 -452 150 -0003900

Anchor Rigid in all directions Initial displacement (inchdegree)~-shyCase 1 translational X = 00000 inch Case 1 translational Y = 01120 inch Case 1 translational Z = 0000 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = 00 inch Case 2 translational Y = 00 inch Case 2 translational Z = 00 inch Case 2 rotational X = 0 degree Case 2 rotational Y= 0 degree

----- --------

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~

Point Data Description

Case 2 rotational Z = 0 degree HEOb HE1 HE2 HE3 Anchor Translational stiffness (lbinch)

X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0077 inch Case 1 translational Y = -0017 inch Case 1 translational Z = -0004 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0077 inch Case 2 translational Y = -0017 inch Case 2 translational Z = -0004 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

HE4 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0109 inch Case 1 translational Y = -0052 inch Case 1 translational Z = -0008 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0109 inch Case 2 translational Y = -0052 inch Case 2 translational Z = -0008 inch Case 2 rotational X = 0 degree Case 2 rotational Y = 0 degree Case 2 rotational Z = 0 degree

HE5 Anchor Translational stiffness (lbinch) X=Rigid Y=Rigid Z=Rigid Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) Case 1 translational X = -0311 inch Case 1 translational Y = -0052 inch Case 1 translational Z = 0137 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 rotational Z = 0 degree Case 2 translational X = -0311 inch Case 2 translational Y = -0052 inch Case 2 translational Z = 0137 inch

----- -------- -------------------------------------------------

101493 1243 PageFile CAS[

PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN

point Data Description degree

Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0

HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid

Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =

0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0

HE6b HEbc

Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet

2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree

HE7 ~

HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree

----- -------- -------------------------------------------------

------~-- ~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

J

Point Data Description

TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )

translational X 0 inch Case 2 translational Y 0 inch Case )

lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3

rotational Y

rotational Z 0 0

degree degree

Free Y restraint during hanger design

PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Case number Combination

1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot

~

Support Summary Forceslb or Momentslinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1

Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0

TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

----- -------- -------------------------------------------------

101493 1243 PageFile CAS[

PipePlus version 450 Fermi Natl Accelerator Lab ~D-zero Solenoid Upgrade CHIMNEY DESIGN

point Data Description degree

Case 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0

HE6 Translational stiffness (lbinch) AnchorHE6a X=Rigid Y=Rigid Z=Rigid

Rotational stiffness (lb-inchdeg) X=FREE Y=FREE Z=FREE Initial displacement (inchdegree) inch Case 1 translational X = -0096 inchCase 1 translational Y = 0035 inch Case 1 translational Z = 0073 degreeCase 1 rotational X = 0 degreeCase 1 rotational Y = 0 degreeCase 1 rotational Z = 0 -0096 inchCase 2 translational X = 0035 inchCase 2 translational Y =

0073 inchCase 2 translational Z = degreeCase 2 rotational X = 0 degreeCase 2 rotational Y = 0 degreeCase 2 rotational Z = 0

HE6b HEbc

Tra~s~ational stiffness (lbinch) HE6d Anchor X=Rlgld Y=Rigid Z=Rigid R~tational stiffness (lb-inchdeg) X-~R~E Y=FREE Z=FREE Inltlal displacement (inch d )Case 1 t 1 egr ee rans atonal X = 0110 inch Case 1 translatlonal Y = 00~1 inch Case 1 bull t rans 1ational Z = -0 -lS1 inch Case 1 rotational X = 0 degree Case 1 rotational Y = 0 degree Case 1 r 0 t a tlonal Z = 0 degree Case 2 translational X = 0110 inch Case 2 translational Y = 0031 inch Case 2 translational Z = -0181 inch Case 2 bull ro atlonal X = 0 degreet

2 t degreeCaseCase bull ro ational Y = 0 2 rotational Z = 0 degree

HE7 ~

HE7a Anchor Translational stffX=Rigid Y=Rigid ness_(~b(inch) Rotational stiffne~~ (ibR~91dX=FREE Y=FREE ~~ -lnchdeg) Init 1 d Z=FREEla isplacement (Case 1 translational ~n~hdegree) Case 1 translational Y 0052 inch Case 1 translational Z 0060 inch- Case 1 rotational X = 0 -0124 inch Case 1 rotational Y = 0 degree Case 1 rotational Z_= 0 degreedegree

----- -------- -------------------------------------------------

------~-- ~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

J

Point Data Description

TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )

translational X 0 inch Case 2 translational Y 0 inch Case )

lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3

rotational Y

rotational Z 0 0

degree degree

Free Y restraint during hanger design

PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Case number Combination

1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot

~

Support Summary Forceslb or Momentslinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1

Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0

TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

----- -------- -------------------------------------------------

------~-- ~

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

J

Point Data Description

TL9 Anchor Translational stiffness (lbi nch) X=Free Y=Free Z=Free Rotational stiffness (lb-inchdeg) X=Free Y=Free Z=Free Initial displacement (i nch degree) Case 1 translational X 0 inch Case 1 translational Y 0 inch Case 1 translational Z 0 inch Case 1 rotational X 0 degree Case 1 rotational Y 0 degree Case 1 rotational Z 0 degree Case )

translational X 0 inch Case 2 translational Y 0 inch Case )

lt translational Z 0 inch Case 2 rotational X 0 degree Case 2 rotational Y 0 degree Case 2 rotational Z 0 degree Case gt v translational X 0 inch Case gtv translational Y 0 inch Case gtv translational Z 0 inch Case 3 rotational X 0 degree Case gt v Case 3

rotational Y

rotational Z 0 0

degree degree

Free Y restraint during hanger design

PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Case number Combination

1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot

~

Support Summary Forceslb or Momentslinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1

Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0

TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlu8 version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

Case number Combination

1 DW + Pres1 + Therl + Disp1 2 DW + Pres2 + Ther2 + Disp2

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot

~

Support Summary Forceslb or Momentslinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1

Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0

TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~middot

~

Support Summary Forceslb or Momentslinch-lb

Point Global Sustained Expansion Total Name Direction Max Min Max Min Occasion Max Mi --------shy --------shy ------shy ------shy ------shy ------shy --------shy ------shyTL7b Fx 1 0 0 0 0 1

Fv -1 0 0 -0 0 -1 Fz -0 0 0 0 0 0

TL9 Fx 0 0 0 -0 0 0 Fy -0 0 0 -1 0 -0 Fz 0 0 0 -0 0 0 Mx -0 0 0 -0 0 -0 Mz -0 0 0 -0 0 -0

-

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot ~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z

TRl 0000 0000 0000 -0000 -0000 000 TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 001 TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 -0076 -0010 -0003 0085 -0062 -023 TR4Near -0107 -0037 -0005 0126 -0049 -029 TR4Far -0306 -0045 0138 0267 -0208 024 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 023 TR6Far -0374 0146 0156 0267 o A04 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -019

TR7b TR8Near

-0319 middot-0241

-0420 -0807

0000 -0080

-0198 -0666

-0286 -0210

013 -030

TR8Far -0242 -0803 -0088 -0695 -0194 -030

TR9 -0274 -0656 -0132 -0770 -0146 -029

HEOa 0000 0112 0000 0000 0000 -000 HEObNear 0006 0112 0001 0049 0048 -002 HEObFar 0013 0111 -0002 0115 0147 -007

HEl HE2Near HE2Far HE3 HE4Near HE4Far

0015 0025 0022

-0077 -0109 -0309

0109 0098 0091

-0017 -0052 -0064

-0005 -0021 -0027 -0004 -0008 0126

0132 0170 0175 0187 0202 0101

0156 0106

-0033 -0105 -0020 -0216

-010 -022 -029 -036 -032 023

HE5 HE6Near HE6Far HE6a

--03l1 -0358 -0354 -0096

-0052 0088 0097 0035

0137 0170 0155 0073

0097 0095 0123 0201

-0200 0290 0505 0601

025 035 034 o 30(

HE6b HE6c HE6d HE7Near HE7Far HE7a HE7b HE7c HE8Near HE8Far HE9 TLl TL2 TL2a TL3

0046 0081 0110 0187 0184 0052 0264

-0356 -0481 -0479 -0437 0000

-0002 -0048 -0088

-0044 -0062

0031 0201 0205 0060

-0515 -0459 -0609 -0612 -0589 0000 0002 0010

-0013

-0012 -0096 -0181 -0270 -0280 -0124 0067 0026

-0070 -0079 -0121 0000

-0021 -0010 -0007

0163 -0090 -0393 -0327 -0230

0201 0012

-0014 -0095 -0110 -0129 -0000 -0037 0021 0099

0188 0040 0155 0120 0049

-0230 -0011 0084 0192 0207 0222

-0000 -0050 -0102 -0053

025 021 017 014 013

-024 000 026

-009 -009 -009 000 002

-010 -027

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~E Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy ---_ _----shy ---------shy ---------shy ---------shy ---------shy ------shy

TL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c TL7

0368 0411

0010 0002

-0271 -0287

0084 0140

0619 0559

040 040

TL7a1Nea 0396 0029 -0322 0217 0498 039 TL7alFar 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -016 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near TL8Far TL9

-0278 -0277 -0280

-0762 -0760 -0638

-0084 -0092 -0135

-0537 -0564 -0640

-0061 -0045 -0000

-028 -027 -026

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

Fermi Natl Accelerator Lab 101493 1243 PagePipePlus version 450 File CASE-I-Zero Solenoid Upgrade CHIMNEY DESIGN

L-oad Dead Weight -+ Pressure 1 -+ Thermal 1 -+ Displacement 1

System Stresses ( ANSI 8313 ) In- Out

Point Name --------shy

Plane SIF

----shy

Plane SIF

-----shy

Section Modulus ------shy

Stressespsi Hoop Longitu

---------shy ---------shyPrincipal -------shy

Code ~---- -shy

Allot ----_

TRl TR2Near TR2Far TR2a TR3 TR4Near TR4Far TR5 TR5a TR6Near TR6Far TR6a

100 115 115 100 100 100 100 100 100 100 100 100

100 100 100 100 100 100 100 100 100 100 100 100

001 001 001 001 001 001 001 001 001 001 001 001

517 517 517 517 517 517 517 517 517 517 517 517

918 1116 1075 1509

887 4)4 641 659

1124 1793 1752 2005

929 1123 1083 1514

900 577 672 687

1130 1796 1752 2005

1376 1233 1186 1800 1078

611 924 910

1560 1906 1919 2122

200( 200( 200 200 200( 200 200 r

200 200( 200( 200( 200(

TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200 TR7Far 100 100 001 517 1364 1368 1473 200(

T R 7 a TR7b

100 100

100 100

001 001

517 517

1448 1525

1452 1528

2022 1831

200 200

TR8Near 100 100 001 517 994 1001 1237 200 TR8Far 100 100 001 517 957 958 1244 200 TR9 100 100 001 517 274 518 417 200 HEOa 100 100 002 805 2895 3222 3661 200 HEObNear 123 102 002 805 2991 3307 3720 200( HEObFar 123 102 002 805 2244 2600 2926 200( HEl 100 100 002 805 1644 2127 2496 200 HE2Near 123 102 002 805 2867 3141 3396 200( HE2Far 123 102 002 805 3701 3701 3712 2001

HE3 100 100 002 805 2447 2447 2474 200( HE4Near 100 100 002 805 1324 1325 1321 200 HE4Far 100 100 002 805 904 1037 1428 200( HE5 100 100 002 805 951 1072 1575 200 HE6Near 123 102 002 805 3417 3430 3520 200( HE6Far 123 102 002 805 3206 3208 3335 200 1

HE6a 100 100 002 805 2123 2125 2447 200 HE6b 100 100 002 805 1694 1696 1600 200 HE6c 100 100 002 805 1620 1623 1437 200 HE6d 100 100 002 805 1512 1514 2371 200 HE7Near 123 102 002 805 2406 2407 2582 200 HE7Far 123 102 002 805 2550 2550 2701 200 HE7a 100 100 002 805 2071 2071 1816 200 HE7b 100 100 002 805 1619 1619 1956 200 HE7c 100 100 002 805 2002 2002 1723 200

r HE8 Nea r 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 200 HE9 100 100 002 805 336 805 462 200 TLl 100 100 001 517 747 773 1098 200 TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

--------- ----- ----- ------- -------- -------- -------- -------- -----

~ -

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~sE Load Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

I

System Stresses ( ANSI B31 3) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allot

TL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200 TL4Far 100 100 001 517 959 981 1347 200 TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200 TL6Nea( 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200 TL7alFar 100 100 001 517 1194 1199 1297 200

001 517 1495 1498 2092 200TL7a 100 100 TL7b 100 100 001 517 1477 1481 1751 200

981 988 1222 200TL8Near 100 100 001 517 2P-f)001 517 946 947 1236TLSFar 100 100 TL9 100 100 001 517 258 518 393

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page I-)-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

~oad Dead Weight + Pressure 1 + Thermal 1 + Displacement 1

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7a1Far

Maximum X rotation = -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

11 a x imum X force -113 lb at point HE3 Maximum Y force 46 lb at point HE7b Maximum Z force -45 lb at point HE6a

Maximum X moment -39 inch-lb at point HEOa Maximum Y moment 56 inch-lb at point HE6Near Maximum Z moment = -35 inch-lb at point HEObFar

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3701 psi at point HE2Far Maximum principal stress 3701 psi at point HE2Far Maximum code stress 3720 psi at point HEObNear Maximum stress ratio (codeallowable) 019 at point HEObNear

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Name X

Displacementsinch Y Z X

Rotationsdegree Y Z

TRl 0000 0000 0000 -0000 -0000 o OO(

TR2Near -0002 0002 -0016 -0035 -0051 001 TR2Far -0004 0002 -0018 -0038 -0079 o 01~ TR2a -0037 0008 -0007 0007 -0114 -OOT

TR3 --0076 -0010 -0003 0085 -0062 TR4Near -0107 -0037 -0005 0126 -0049 -0 29~

TR4Far -0306 -0045 0138 0267 -0208 0241 TR5 -0308 -0029 0147 0269 -0189 026middot TR5a -0332 0069 0180 0254 0007 o 27( TR6Near -0375 0143 0167 0256 0318 o 23( TR6Far -0374 0146 0156 0267 0404 o 23( TR6a -0000 -0000 0018 0140 0302 021 TR6b 0001 -0000 -0129 -0147 0151 020 TR7Near 0293 0103 -0272 -0028 0430 018 TR7Far 0295 0102 -0278 0008 0397 018 TR7a 0000 -0000 -0000 0310 -0107 -0191

TR7b -0319 -0420 0000 -0198 -0286 o 13~ TR8Near -0241 -0807 -0080 -0666 -0210 -0 ~)( TR8Far -0242 --0803 -0088 -0695 -0194 -0

TR9 -0274 -0656 -0132 -0770 -0146 -029middot HEOa 0000 0000 0000 -0000 0000 -OOO( HEObNear 0006 0000 0000 -0013 0004 -000 HEObFar 0010 0001 -0004 -0037 -0001 -0 01 ~ HEl 0010 0001 -0008 -0042 -0005 -OOli HE2Near 0009 0005 -0024 -0055 -0040 -002 HE2Far 0004 0006 -0027 -0057 -0092 -003 HE3 -0077 -0017 -0004 0060 -0061 -030 HE4Near -0109 -0052 -0008 0106 -0006 -037 HE4Far -0309 -0065 0126 0079 -0212 025 HE5 -0311 -0052 0137 0075 -0196 027 HE6Near -0358 0089 0170 0090 0292 o 35 HE6Far -0354 0098 0155 0121 0506 035 HE6a -0096 0035 0073 0204 0600 030 HE6b 0046 -0045 -0012 0164 0188 02E HE6c 0081 -0063 -0096 -0091 0040 021 HE6d 0110 0031 -0181 -0393 0155 011 HE7Near 0187 0201 -0270 -0327 0120 o 14~

HE7Far 0184 0205 -0280 -0230 0049 013 HE7a 0052 0060 -0124 0201 -0230 -0 24~ HE7b 0264 -0515 0067 0012 -0011 000 HE7c -0356 -0459 0026 -0014 0084 026middot HE8Near -0481 -0609 -0070 -0095 0192 -009 HE8Far -0479 -0612 -0079 -0110 0206 -009 HE9 TLl

-0437 0000

-0589 0000

-0121 0000

-0129 -0000

0222 -0000

-0) o l6(

TL2 -0002 0002 -0021 -0037 -0050 002 TL2a -0048 0010 -0010 0021 -0102 -010 TL3 -0088 -0013 -0007 0099 -0053 -027shy

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASE

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Deflections Point Displacementsinch Rotationsdegree Name X Y Z X Y Z --------shy -----------shy -----_ _-shy _ _-----shy -- _-----shy -----------shy -------shyTL4Near -0119 -0044 -0010 0137 -0045 -033 TL4Far -0319 -0058 0157 0269 -0182 032 TL5 -0321 -0039 0165 0274 -0148 035 1

TL5a -0349 0085 0177 0286 0170 041 TL6Near -0373 0141 0156 0291 0382 041 TL6Far -0370 0146 0144 0302 0476 041 TL6a -0000 -0000 0021 0141 0352 041 TL6b 0001 -0000 -0126 -0070 0165 040 TL6c 0368 0010 -0271 0084 0619 040 TL7 0411 0002 -0287 0140 0559 040 TL7alNea 0396 0029 -0322 0217 0498 039 TL7a1Far 0392 0032 -0326 0233 0481 039 TL7a 0000 -0000 -0000 0424 0047 -0 16 TL7b -0319 -0420 0000 -0091 -0132 015 TL8Near -0278 -0762 -0084 -0537 -0061 -028 TL8Far -0277 -0760 -0092 -0564 -0045 -027

I TL9 -0280 -0638 -0135 -0640 -0000 -026

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

Go

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CAS~4

Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313 ) In- Out

Point Plane Plane Section Stressespsi Name SIF SIF Modulus Hoop Longitu Principal Code Allolr --------- _ _-- - ---- ------- -------- -------- -------- -------- ------TRl 100 100 001 517 918 929 1376 200C TR2Near 115 100 001 517 1116 1123 1233 200C TR2Far 115 100 001 517 1075 1083 1186 200C TR2a 100 100 001 517 1509 1514 1800 200( TR3 100 100 001 517 887 900 1078 200( TR4Near 100 100 001 517 494 577 611 200( TR4Far 100 100 001 517 641 672 924 200C TR5 100 100 001 517 659 687 910 200C TR5a 100 100 001 517 1124 1130 1560 200( TR6Near 100 100 001 517 1793 1796 1906 200( TR6Far 100 100 001 517 1752 1752 1919 200( TR6a 100 100 001 517 2005 2005 2122 200( TR6b 100 100 001 517 1648 1648 2507 200( TR7Near 100 100 001 517 1320 1320 1510 200( TR7Far 100 100 001 517 1364 1368 1473 200( TR7a 100 100 001 517 1448 1452 2022 200( TR7b 100 100 001 517 1525 1528 1831 2P( TR8Near 100 100 001 517 994 1001 1237 2 TR8Far 100 100 001 517 957 958 1244 200C TR9 100 100 001 517 274 518 417 200( HEOa 100 100 002 805 694 994 1193 200lt HEObNear 123 102 002 805 509 937 1071 200( HEObFar 123 102 002 805 843 882 1069 200( HEl 100 100 002 805 830 874 1023 200C HE2Near 123 102 002 805 1383 1388 1485 200C HE2Far 123 102 002 805 1389 1400 1500 200( HE3 100 100 002 805 3584 3586 2869 200( HE4Near 100 100 002 805 1551 1560 1563 200( HE4Far 100 100 002 805 887 1002 1386 200( HE5 100 100 002 805 936 1039 1532 200( HE6Near 123 102 002 805 3413 3423 3511 200( HE6Far 123 102 002 805 3196 3198 3326 200( HE6a 100 100 002 805 2116 2118 2442 200lt HE6b 100 100 002 805 1696 1699 1601 200( HE6c 100 100 002 805 1621 1624 1438 200( HE6d 100 100 002 805 1507 1509 2366 200lt HE7Near 123 102 002 805 2405 2406 2581 200( HE7Far 123 102 002 805 2549 2549 2700 200lt HE7a 100 100 002 805 2070 2070 1815 200C HE7b 100 100 002 805 1619 1619 1956 200( HE7c 100 100 002 805 2002 2002 1723 200( HE8Near 123 102 002 805 717 810 975 200 HE8Far 123 102 002 805 691 805 943 bull (

HE9 100 100 002 805 336 805 462 ~ TL1 100 100 001 517 747 773 1098 200 r

TL2 100 100 001 517 1011 1020 1165 200 TL2a 100 100 001 517 1584 1588 1879 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 1243 Page ~-Zero Solenoid Upgrade CHIMNEY DESIGN File CASEmiddot

_oad Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Stresses ( ANSI 8313) In- Out

Point Plane Plane Section Stressespsi Name --------shy

SIF ----shy

SIF -----shy

Modulus --------shy

Hoop --------

Longitu -------shy

Principal -------shy

Code --------

Allol _ _-shyTL3 100 100 001 517 922 932 1095 200 TL4Near 100 100 001 517 511 580 636 200middot TL4Far 100 100 001 517 959 981 1347 200 r

TL5 100 100 001 517 1017 1035 1372 200 TL5a 100 100 001 517 1569 1578 1845 200shyTL6Near 100 100 001 517 1988 1997 2117 200 TL6Far 100 100 001 517 1934 1934 2167 200 TL6a 100 100 001 517 2303 2303 2441 200 TL6b 100 100 001 517 1833 1833 2743 200 TL6c 100 100 001 517 960 960 1144 200 TL7 100 100 001 517 1247 1247 1428 200 TL7alNea 100 100 001 517 915 1126 1388 200middot TL7alFar 100 100 001 517 1194 1199 1297 200( TL7a 100 100 001 517 1495 1498 2092 200 TL7b 100 100 001 517 1477 1481 1751 200

-TL8Near 100 100 001 517 981 988 1222 200 TL8Far 100 100 001 517 946 947 1236 200 TL9 100 100 001 517 258 518 393 200

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

PipePlus version 450 Fermi Natl Accelerator Lab 101493 12=43 Page D-Zero Solenoid Upgrade CHIMNEY DESIGN File CA~ Load Dead Weight + Pressure 2 + Thermal 2 + Displacement 2

System Maxima

Maximum X displacement -0481 inch at point HE8Near Maximum Y displacement -0807 inch at point TR8Near Maximum Z displacement -0326 inch at point TL7alFar

Maximum X rotation -0770 degree at point TR9 Maximum Y rotation 0619 degree at point TL6c Maximum Z rotation 0414 degree at point TL5a

Maximum X force -110 lb at point HE3 Maximum Y force == 46 lb at point HE7b Maximum Z force == -45 lb at point HE6a

Maximum X moment 32 inch-lb at point HE7Far Maximum Y moment 55 inch-lb at point HE6Near Maximum Z moment == 44 inch-Ib at point HE3

Maximum hoop stress 805 psi at point HEOa Maximum longitudinal stress 3584 psi at point HE3 Maximum principal stress 3586 psi at point HE3 Maximum code stress 3511 psi at point HE6Near Maximum stress ratio (codeallowable) 018 at point HE6Near

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

-------------

I

~

SECTION

IltDJ 016 AI FERMILAB

ENGINEERING NOTE PROJECT SERIAL-CATEGORY

J)cent SO aAJO Ul I e1 3 bull IIItJPGr1f2Ao e )

PAGE

SUBJECT NAME

Rus- RcvlS-rHf~A ceiVT~TtoW AIltJA v-( ~S DATE REVISION DATE

~ENOD -reP-MM MltN~--r DUl2 Q 3

4 OF

c ~ A ~ ( E~

10 80 ~ e - 11 uloJ

eA~E-O

)

IE L He TtJeE

e E itocJ ICD

f

c ~EgtjIlA(-o AT HE 1shy IoJ CASpound

A IJ 1or-1--t ~ f S AN~ a T kGR

A fIO W Ii I-~ STLe-~ ~

o O~ 41 v~ Oo3~ I

eo iVEc i 0r s2~ 26

~~igtb -E

w ~oP7raquo

FQcM I 1 0

r IN L shy

A-lA-l-1S (S

7001 -~-----

505 bull

1+1t FIt-S E(Bow Igtr HEt WILl AJOr 6E E olaquo=p 1b THe

IUPfOR-r C8INOE-Ie 1kl 211 vJj( t WIt- IltSSvMc

M IOWIl(1 BEtWeampN 1l4Cshy 1WO (I)-r H=cent) 11- e IVSE

1$ tANlt~of-EO I bull Iii IS ACH-oJa (4t1) VL I5E

DSttLAltED vJHamp) II-Hz SOLlt-lad~ Cooc-5

~-~---~--~

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220

(

(

PROJECT SERlAl-CATEGORY PAGE IFERMILAB D6~

t)p~ 31)2-3 lIr ~2 i~____________________________________~__________~____~~~~~__________~~__~_4ENGINEERING NOTE ~~ ~n R

rI u~S Ucl tJltS DATE IREVISION DATE

DI~PIC-MN VkIl S0Uiie0tD COOe-S- ook

JIItk ) t) -0 i

eADI~- (A~SCiM- Vfi(tn~-) y) ~ ~I _= 1lt -Cbt qtO _ o oo-4~ ~~ ~ _ ~ 2 1M

r 0(

- I J 254 M

ALO~ 7 p)(

CEtJ~ tJ~ ~e 5011No10 fAove~ 1bVJ~ middotTi-~ Cl-ltAiJE-(

Et-JO _1-1 t tt~F= 6middot~-q3 poundA(4t WAJO) r() S~VI~frS J ~o DU1 a ~IIG lllIt= RIgt j)~ c~~

b -= Cz ~tt) Cgt( (5 oS~ 1M) (oot 3) = a 220