ANALYSIS OF A LIFTING FIXTURE TO HOLD A STEEL …lss.fnal.gov/archive_notes/d0-en/fermilab-d0-en-510.pdf · analysis of a lifting fixture to hold a steel mandrel horizontally from

ANALYSIS OF A LIFTING FIXTURE TO HOLD A STEEL MANDREL HORIZONTALLY FROM ONE END SUPPORT

D-ZERO ENGINEERING NOTE 3823113-EN-51 0

Author Herman Cease PPDETTD-Zero Mech April 7 1999

Approved BY--i-~4-i-~~~ PPDETTD-Zero Project

SUMMARY

A lifting fixture (drawing number 3823 113-MD-372382) that lifts large steel mandrels from one end through the mandrels end support web is described The mandrels are used as a mold to form carbon fiber cylinders The mandrels are held from one end to allow the carbon cylinder to be pulled horizontally off the mandrel Only mandrels as described in drawing s 3823113-MD-358992 and 38231 13-MD-358994 are lifted by the fixture The largest mandrel is 41 inches in diameter 120 inches long and weighs approximately 3000 lbs A detailed procedure for removing the carbon cylinder from the steel mandrel is given in the Appendix

The fixture is to be supported only using Fermilab Forklift 10207 or equivalent The forklift has a nameplate capacity of 12000 lbs 24 inches from the mast at an elevation of 130 inches from the floor The forklift forks must be removed from the truck prior to using the fixture The forklift is to be used to support the mandrels only during the lifting operation and is not to be used to transport the mandrels

Stresses at the lifting fixture are shear stresses on the support brackets due to the overall weight of the mandrel and moment loads due to the cantilever style suppOrt The moment on the forklift due to the overhanging weight of the mandrel is calculated Stresses in the mandrel due to the method of support are also described

ANALYSIS

Expected Size and Weight of the Mandrels

The total weight of a mandrel is based on the weight of the rolled skin that forms the outside barrel and the support webs The journals are stubs welded into the end support webs and do not significantly contribute to the weight of the mandrel The length of mandrels 1 and 2 is approximately 76 inches and of mandrels 3 thru 8 is 110 inches The expected wall thickness for each mandrel is a V2 inch The end support webs are I thick (weight calculations are conservatively based on solid support webs) Mandrels 3 thru 8 also have a I thick center web for additional support The density of steel used is 0284 lbin3

Weights and dimensions of all mandrels are given in Table 1 The total moment on the lifting fixture is calculated as the total mandrel weight multiplied by half the mandrel length

Tab e I 1 MandreIWelglhts andDImenSlOns

SUPPORT TOTAL MONtENTON OUTER MANDREL WALL WEB MANDREL LIFTING

MANDREL DIAMETER LENGTH WEIGHT WEIGHT WEIGHT FIXTURE (in) (in) (Ibs) Jibs) Jibs) (inlbs)

1 15156 76 515 89 604 22952 2 19018 76 645 145 790 30020 3 22864 110 1122 320 1442 79310 4 26738 110 1314 443 1757 96635 5 30602 110 1502 586 2088 114840 6 34464 110 1691 749 2440 134200 7 38326 110 1881 932 2813 154715 8 40292 110 1977 1033 3010 165550

Forklift Capacity

The forklift has a nameplate capacity of 12000 lbs with the load centered 24 inches from the mast at 130 inches of elevation The total moment the Forklift can support is 288000 in lbs Using Table 1 the lowest safety factOr on the load capacity is approximately 4 and the lowest safety factor on the moment capacity is 17

Calculation of Allowable Material Stresses

The maximum allowable stress on any materIal in the lifting system is 033 x Yield Stress according to ASME B3020 - Below-The-Hook lifting devices(2) The fixture brackets are constructed using a mild steel which is assumed to have a yield strength of 30000 psi The welds in the mandrel are also assumed to have a yield strength of 30000 psi The brackets are attached to the base plate using ANSI Grade 5 bolts with a yield strength of 120000 psi(l) The base plate is constructed of Aluminum to reduce the overall weight however it has no significant stresses due to its large size According to the above guidelines the maximum allowable stress for the steei and welds in the fixture is 10000 psi and 40000 psi for the attaching bolts

Stresses on the t1andrel Web Due [0 the Lifting Fixture

The lifting fixture brackets are inserted into the top opening of the end support web see Figures 1 and 2 The mandrel then sticks horizontally out from the lifting fixture and puts a moment on the Jifting fixture The moment creates a pullout force on the end suppOrt web where the lifting fixture brackets attach The pullout force on the support web is equal to the weight of the mandrel times half the length divided by the mandrel diameter The end support web is attached to the JD of the mandrel using Y fillet welds that are 2 inches long every 4 inches around the circumference The shear stress on the weld is the pullout force divided by the area of the weld The pullout force calculated in Table 2 assumes that all of the load is transmitted through only one of the skip welds The shear stress in the weld is then calculated For each case listed the stress in the weld is less than the maximum allowable stress of 10000 psi

T bl 2 Sh a e thear stresses In emandr I b d e we I b IIue to potentla we pu out

MANDREL MANDREL TOTAL PULLOUT STRESS IN OUTER HALF MANDREL FORCE ON WELD

MANDREL DIAMETER LENGTH WEIGHT WEB 2 X 114 I 15156 in 38 in 6041bs 15141bs 3028 psi 2 19018 38 790 1578 3156 3 22864 55 i442 3469 6938 4 26738 55 1757 3614 7228 5 30602 55 2088 3752 7504 6 34464 55 2440 3894 7788 7 38326 55 2813 4037 8074 8 40292 55 3010 4109 8218

Stresses on the Lifting Fixture Bracket

The lifting fixture brackets (dwg s 38231 13-MC-372383 and 3823113-MC-372411) are used to support the mandrel at the end support webs The forces and stresses on the brackets are calculated

Bracket for Mandrels 1 and 2 The maximum shear stress on the bracket due to gravity is the weight of the mandrel divided by the cross sectional area of the bracket The weight of mandrel 2 is 790 Ibs and the cross sectional area of the bracket is 226 inch producing a stress in the bracket of 350 psi

The maximum shear stress on the bracket due to the moment of the mandrel is the web pullout force divided by the cross sectional area of the bracket The pullout force for mandrel 2 is 1578 Ibs and the cross sectional area of the bracket is 15 inch2 producing a stress in the bracket of 1052 psi

Bracket for Mandrels 3 thru 8 The maximum shear stress on the bracket due to gravity is the weight of the mandrel divided by the cross sectional area of the bracket The weight of mandrei 8 IS 30 I 0 Ibs The cross sectional area of the bracket is 684 inch2 producing a stress In the bracket of 440 PSl

The maximum shear stress on the bracket due to the moment of the mandrel is the web pull out force divided by the cross sectional area of the bracket The pullout force for mandrel 8 is 4109 Ibs and the cross sectional area of the bracket is 356 inch 2 producing a stress in the bracket of 1154 psi

All of the above calculated stresses in the brackets used to couple the mandrel to the lifting fixture are less than the maximum allowable stress of 10000 psi

The Stresses in the Lifting Bracket Bolts

Bracket for Mandrels 1 and 2 There are four Grade 5 ANSI 716 inch bolts used to attach the bracket for mandrels 1 and 2 Assuming that only one of the bolts carry load the maximum shear stress in the bolt due to gravity is the weight of the mandrel divided by the cross sectional area of the bolt The weight of mandrel 2 is 790 lbs and the cross sectional area of one bolt is 01063 inch2 producing a stress in the bolt of 7432 psi

Assuming that only one of the bolts carry the load the maximum tensile stress in the bolt is the pull out force divided by the cross sectional area of the bolt The force due to the moment of mandrel 2 is 1578 Ibs and the cross sectional area of one bolt is 01063 inch2 producing a stress in the bolt of 14845 psi

Bracket for Mandrels 3 thru 8 There are eight Grade 5 ANSI 7116 inch bolts used to attach the bracket for mandrels 3 thru 8 Assuming that only one of the bolts carry load the maximum shear stress in the bolt due to gravity is the weight of the mandrel divided by the cross sectional area of the bolt The weight of mandrel 8 is 3010 Ibs and the cross sectional area of one bolt is 01063 inch2 producing a stress in the bolt of 28316 psi

Assuming that only one of the bolts carry the load the maximum tensile stress in the bolt is the pull out force divided by the cross sectional area of the bolt The force due to the moment of mandrel 8 is 4109 lbs and the cross sectional area of one bolt is 01063 inch 2 producing a stress in the bolt of 38654 psi

All of the calculated stresses in the lifting bracket bolts are less than the maximum allowable stress of 40000 psi

Stresses on the Forklift Supports

The forklift supports (dwg s 382113-MB-372481 and 3823113-MC-372384) are used to attach the lifting plate to the forklift The cross sectional area of each support bar is 375 inch2 giving a shear stress due to gravity of 3200 psi at the forklift nameplate load

The force on the support due to the overhanging moment is calculated For mandrels 3 thru 8 the lifting bracket is in line with the forklift support bracket so the pullout force calculated in Table 2 can be used as this force However the position of the lifting bracket for mandrels 1 and 2 is much higher than the forklift support and so the pullout force given in Table 2 needs to be adjusted to compensate for the difference in height The pullout force applied to the forklift support becomes the weight of the mandrel times half the mandrel length divided by the distance from the bottom of the mandrel to the support hook The adjusted force on the support bracket for mandrel 1 is 6750 Ibs and for mandrel 2 is 4363 Ibs The shear stress in support bracket due to the overhanging mandrel moment is the maximum force (6750 lbs for mandrel 1) divided by the cross-sectional area of the bracket (30 in2

) The force applied to the support bracket when lifting mandrel 1 creates a shear stress in the bracket of 225 psi

All of the calculated stresses in the Forklift Supports are less than the maximum allowable stress of 10000 psi

Eight 716 inch ANSI Grade 5 bolts are used to attach the support bar to the lifting plate The bolt shear stress due to gravity when lifting mandrel 8 is 28316 psi assuming that all of the load is carried by one bolt The tensile stress in one bolt due to the overhanging moment when lifting mandrel 1 is 41044 psi Assuming two bolts in the bolt system share the load the stress in one of the two bolts would be 20500 psi which is less than the maximum allowable stress of 40000 psi

Bolt Torques

The 7116 inch ANSI Grade 5 bolts should not be over-torqued because it increases the tensile stress in the bolt

Torque (inlbs) = 15 bolt diam (in) X clamping force (Ibs) Or substituting in stress instead of force

Torque (inlbs) = 15 bolt diam (in) X tensile stress (psi) X bolt cross sectional area (in2)

where 15 is the friction coefficient assumed for steel bolts and sliding surfaces

Using the above formula (3 ) a maximum bolt torque of 180 inchlbs should be used on all bolts This produces and additional 19400 psi of tensile strength on the bolt In the case of one bolt carrying all of the mandrel load the maximum allowable stress in the bolt can be exceeded However if the load is shared over at least two bolts in the bolt system the maximum allowable stress of 40000 psi is not exceeded

CONCLUSION

A lifting fixture is constructed that horizontally lifts large steel mandrels from one end through the mandrels end support web The dropping hazard is minimized using this fixrure The hazard is reduced by securely attaching the lifting fixture to the forklift Also 2x4 lumber is used as anti-rocking sruds across the face of the lifting fixture to prevent the mandrel from swaying as it is being supported Only mandrels as described in drawing s 3823 I 13-MD-358992 and 3823113-MD-358994 are lifted by the fixrure The fixrure is to be supported only with Fennilab Forklift 1 0207 or equivalent The forklift is to be used to support the mandrels only during the lifting operation and is not to be used to transport the mandrels The fixrure is constructed using 30000 psi yield strength steel The brackets are attached using ANSI Grade 5 bolts with a yield strength of 120000 psi(l) The maximum allowable stress on any of the fearures in the lifting system is 033 x Yield Stress The maximum allowable stress for the steel and welds in the fixrure is 10000 psi and 40000 psi for the attaching bolts All stresses in the system are below these values The fixrure is to be inspected prior to each use including identifying any loose or damaged bolts brackets supports or anti- rocking studs

References

1) Marks Standard Handbook For Mechanical Engineers 8th ed

2) ASME B3020 Below-The-Hook Lifting Devices

3) What Every Engineer Should Know About Threaded Fasteners Blake

Appendix - Procedure for removing the carbon fiber cylinder from the mandrels

1) Inspect all fixtures and lifting devices for damage 2) Mount the lifting fixture (3823113-MD-372382)to forklift 10207 or equivalent 3) Position forklift 10207 at one end of the mandrel while the mandrel is still on the

mandrel stand and secure the wheels to prevent the forklift from moving 4) Using the mandrel lifting bar as described in the Engineering Note 3823113 ENshy

500 and a second forklift slightly raise the mandrel out of the mandrel stand The slings used should be around the mandrel journals so as not to damage the surface of the mandrel or carbon cylinder

5) Using forklift 10207 insert the lifting fixture into the web openings at the end of the mandrel

6) Slightly raise the mandrel out of the slings and then loosen the slings from around the mandrel journals Do not completely remove the slings

7) Slide the carbon tube from the mandrel and through the sling 8) Repeat steps 3 thru 5 in reverse to place the mandrel back in the mandrel stand

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~~ Fermilab April 3 1999

W Sam Segler Chair D-Zero ESampH Review Committee

FROM Harry Chair

Carter D-Zero

~tVZ(----Mechanical Safety Review Panel

SUBJECT Review of Mandrel Lifting Fixture for DO CFT

I have completed a review of DO Engineering Note 3823113-ENshy510 for a CFT Mandrel Lifting Fixture which is used in conjunction with a fork lift in order to facilitate removal of the completed carbon fiber tube from the mandrel I conclude that the design is sound and should not constitute a safety hazard to equipment or personnel when fabricated load tested and operated in accordance with the information that was reviewed

I therefore recommend that load testing of the lifting fixture be permitted Upon the successful completion of the load test and the subsequent sign-off on the Engineering Note I further recommend that the fixture be permitted to be placed in service for its intended use

xc Bill Freeman Kurt Krempetz

II

1 Fermilab

To Harry Carter

From Bill Freeman tf~ Date 042799

Re Review of D0 Engineering Note 38231 13-EN-510 for Mandrel Lifting Fixture

The above referenced engineering note is attached for your review Please contact Herman Cease at D0 with any questions or concerns Herman would like to perform the load test next week if possible so we would appreciate a timely review Thanks

wsf

cc Sam Segler wo aU

Herman Cease wo att

Kurt Krempetz wo att

bull Page I

S022TA

BELOW-THE-HOOK LIFTING DEVICE Engineering Note Cover Page

Lifting Device Numbers

FNAL Site No Div Specific No Asset No if applicable if applicable if applicab1e

ASME B3020 Group Group I Structural and Mechanical Lifting Devices (check one) iJB Group II Vacuum Lifting Devices

ffipoundB Group ill Magnets Close Proximity Operated ifB Group IV Magnets Remote Operated

Device Name or Description YlArtJ flE L 11114 F nJll-euro

Device was JII Purchased from a Commercial Lifting Device Manufacturer mfg name

(check all applicable)JB Designed and Bui1t at Fermilab Designed by Fermilab and Built by a Vendor

Assy drawing number 3g~J 1 1 S- 1)- 37 2]81shyifB Provided by a User or Other Laboratory Jfil Other Describe_ ________________

Engineering Note Prepared by ~ 41hi Date 01071 Engineering Note Reviewed by Date OSjr3 99

bull~M~L-Lifting Device Data

Capacity

Fixture Weight

Service normal ifB heavy iiJll severe (refer to B3020 for definitions)

Duty Cycle 8 16 or 24 hour rating (applicable to groups ill and IV)

Inspections Frequency _B e_--= u_= =________ _ ____~=--Fofl f__-= spound _

Rated Load Test by FNAL (if applicable) Date 5-+- 91 Load (fIrIVOU ~ 1- (SO 1amp s a 5i)- fr Avf-fr

111 Check if Load Test was by Vendor and attach the certificate

Satisfactory Load Test Witnessed by ~~ Signature (of Load Test Witness) y~ ~ Notes or Special Information

Fermilab ESampH Manual 5022TA -1 Rev 5 98

SUMMARY

A lifting fixture (drawing number 3823 113-MD-372382) that lifts large steel mandrels from one end through the mandrels end support web is described The mandrels are used as a mold to form carbon fiber cylinders The mandrels are held from one end to allow the carbon cylinder to be pulled horizontally off the mandrel Only mandrels as described in drawing s 3823113-MD-358992 and 38231 13-MD-358994 are lifted by the fixture The largest mandrel is 41 inches in diameter 120 inches long and weighs approximately 3000 lbs A detailed procedure for removing the carbon cylinder from the steel mandrel is given in the Appendix

The fixture is to be supported only using Fermilab Forklift 10207 or equivalent The forklift has a nameplate capacity of 12000 lbs 24 inches from the mast at an elevation of 130 inches from the floor The forklift forks must be removed from the truck prior to using the fixture The forklift is to be used to support the mandrels only during the lifting operation and is not to be used to transport the mandrels

Stresses at the lifting fixture are shear stresses on the support brackets due to the overall weight of the mandrel and moment loads due to the cantilever style suppOrt The moment on the forklift due to the overhanging weight of the mandrel is calculated Stresses in the mandrel due to the method of support are also described

ANALYSIS

Expected Size and Weight of the Mandrels

The total weight of a mandrel is based on the weight of the rolled skin that forms the outside barrel and the support webs The journals are stubs welded into the end support webs and do not significantly contribute to the weight of the mandrel The length of mandrels 1 and 2 is approximately 76 inches and of mandrels 3 thru 8 is 110 inches The expected wall thickness for each mandrel is a V2 inch The end support webs are I thick (weight calculations are conservatively based on solid support webs) Mandrels 3 thru 8 also have a I thick center web for additional support The density of steel used is 0284 lbin3

Weights and dimensions of all mandrels are given in Table 1 The total moment on the lifting fixture is calculated as the total mandrel weight multiplied by half the mandrel length

Tab e I 1 MandreIWelglhts andDImenSlOns

SUPPORT TOTAL MONtENTON OUTER MANDREL WALL WEB MANDREL LIFTING

MANDREL DIAMETER LENGTH WEIGHT WEIGHT WEIGHT FIXTURE (in) (in) (Ibs) Jibs) Jibs) (inlbs)

1 15156 76 515 89 604 22952 2 19018 76 645 145 790 30020 3 22864 110 1122 320 1442 79310 4 26738 110 1314 443 1757 96635 5 30602 110 1502 586 2088 114840 6 34464 110 1691 749 2440 134200 7 38326 110 1881 932 2813 154715 8 40292 110 1977 1033 3010 165550

Forklift Capacity

The forklift has a nameplate capacity of 12000 lbs with the load centered 24 inches from the mast at 130 inches of elevation The total moment the Forklift can support is 288000 in lbs Using Table 1 the lowest safety factOr on the load capacity is approximately 4 and the lowest safety factor on the moment capacity is 17



























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Carter D-Zero






II

1 Fermilab

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wsf

cc Sam Segler wo aU

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S022TA












Capacity

Fixture Weight























Bolt Torques






CONCLUSION


References












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Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight










Bolt Torques






CONCLUSION


References












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1 AL L MACH I NED

DATE

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APPROVED K KREMPETZ

USED ON

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MAT ERIAL


DATE

l OrY REO

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12 3823 113-MB-372481 1 OF 1

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FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight
















I

_ J i -----

TO THE

~ I ~

MANDREL

MOMENT

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U SUPPORT




( MANDREL


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~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








TO THE

~ I ~

MANDREL

MOMENT

I --~

I


U SUPPORT




( MANDREL


r DUE TO I WEIGHT

r~(shy~

J

J



~

I ~ 6--+- - M

IJ F -- II


AS REOO

--~ I

---1

I

U FIGURE 2


)

2 3 4 8

AA

B

9 110

I )7 REF



L--j_---- ---t--t---r--- t-~ ~ ~ -f I I

g oo REF


L__ _ -------~~~-------

-+- i i +

1----lt000----1





NO TES

I I

--~

1 7J REF

5

SEE NOTE l

DO REF

2 ~O REF

I

6

I I I

I J-

t1 ~oo RtF J

- ooREr

lt1gt

bull T

o n[N)1









~~I Pql)oQ

t n 11 -- 11 -- ~~~- lOlXt

~ ~~E~~~


PARTS liST

O rlIIOCl 1211

~ ( -W(Tl

n

IZ1UH

~o-IIIt ~ f--cc---------~






A

B

c C

DD

2 3 4 5 6 7

c

8

A

B

D

2 3 4

~------------------------------------- o oomiddot------------------------------------~

10 00 REr

lt~~r~

pound ~- I

iI 1e7 IIU

~~~

t REf

Iplusmnl


pound

~If--------



NOTES

c DETA I L degA

SCALE 1

SUFfi X 26 7315 )01502


[ middot0 0 297

8

WE - Jl89gl -4

IIIpound-J~aQ9tl-~

trt E -l~89i91 -6

r-J~e9ttl-7

w[-Jegggl - 8



_ I_n

tWd)RE l SHAF 1



PARTS LIST

~ aASC

D 11DC) 1 M coJ[ 1~

PlJIAIII





B

8

5 6 7

4 15 REF

pound r amp

SEE NOTE 1

72 3 4 5 6

c

8

2 3 4 5 6 7 8



tA

OO ------------------------------------------4

8 00 RU

d (~

amp

B

1pound1 ~-$~==t

21 il2 181 REF

I 0 1 _ 002~lo4l1

iImiddot bull R[r

[plusmnJ

r------------------------------------------ 2

pound1


cc


nI 7JC1111

D DETAI L A ScA~


NOT ES

~

k (lAS

O Del ~~

( ~lIIP tl


lt

2 3 4 5 6 7

8

- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








~

I ~ 6--+- - M

IJ F -- II


AS REOO

--~ I

---1

I

U FIGURE 2


)

2 3 4 8

AA

B

9 110

I )7 REF



L--j_---- ---t--t---r--- t-~ ~ ~ -f I I

g oo REF


L__ _ -------~~~-------

-+- i i +

1----lt000----1





NO TES

I I

--~

1 7J REF

5

SEE NOTE l

DO REF

2 ~O REF

I

6

I I I

I J-

t1 ~oo RtF J

- ooREr

lt1gt

bull T

o n[N)1









~~I Pql)oQ

t n 11 -- 11 -- ~~~- lOlXt

~ ~~E~~~


PARTS liST

O rlIIOCl 1211

~ ( -W(Tl

n

IZ1UH

~o-IIIt ~ f--cc---------~






A

B

c C

DD

2 3 4 5 6 7

c

8

A

B

D

2 3 4

~------------------------------------- o oomiddot------------------------------------~

10 00 REr

lt~~r~

pound ~- I

iI 1e7 IIU

~~~

t REf

Iplusmnl


pound

~If--------



NOTES

c DETA I L degA

SCALE 1

SUFfi X 26 7315 )01502


[ middot0 0 297

8

WE - Jl89gl -4

IIIpound-J~aQ9tl-~

trt E -l~89i91 -6

r-J~e9ttl-7

w[-Jegggl - 8



_ I_n

tWd)RE l SHAF 1



PARTS LIST

~ aASC

D 11DC) 1 M coJ[ 1~

PlJIAIII





B

8

5 6 7

4 15 REF

pound r amp

SEE NOTE 1

72 3 4 5 6

c

8

2 3 4 5 6 7 8



tA

OO ------------------------------------------4

8 00 RU

d (~

amp

B

1pound1 ~-$~==t

21 il2 181 REF

I 0 1 _ 002~lo4l1

iImiddot bull R[r

[plusmnJ

r------------------------------------------ 2

pound1


cc


nI 7JC1111

D DETAI L A ScA~


NOT ES

~

k (lAS

O Del ~~

( ~lIIP tl


lt

2 3 4 5 6 7

8

- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








)

2 3 4 8

AA

B

9 110

I )7 REF



L--j_---- ---t--t---r--- t-~ ~ ~ -f I I

g oo REF


L__ _ -------~~~-------

-+- i i +

1----lt000----1





NO TES

I I

--~

1 7J REF

5

SEE NOTE l

DO REF

2 ~O REF

I

6

I I I

I J-

t1 ~oo RtF J

- ooREr

lt1gt

bull T

o n[N)1









~~I Pql)oQ

t n 11 -- 11 -- ~~~- lOlXt

~ ~~E~~~


PARTS liST

O rlIIOCl 1211

~ ( -W(Tl

n

IZ1UH

~o-IIIt ~ f--cc---------~






A

B

c C

DD

2 3 4 5 6 7

c

8

A

B

D

2 3 4

~------------------------------------- o oomiddot------------------------------------~

10 00 REr

lt~~r~

pound ~- I

iI 1e7 IIU

~~~

t REf

Iplusmnl


pound

~If--------



NOTES

c DETA I L degA

SCALE 1

SUFfi X 26 7315 )01502


[ middot0 0 297

8

WE - Jl89gl -4

IIIpound-J~aQ9tl-~

trt E -l~89i91 -6

r-J~e9ttl-7

w[-Jegggl - 8



_ I_n

tWd)RE l SHAF 1



PARTS LIST

~ aASC

D 11DC) 1 M coJ[ 1~

PlJIAIII





B

8

5 6 7

4 15 REF

pound r amp

SEE NOTE 1

72 3 4 5 6

c

8

2 3 4 5 6 7 8



tA

OO ------------------------------------------4

8 00 RU

d (~

amp

B

1pound1 ~-$~==t

21 il2 181 REF

I 0 1 _ 002~lo4l1

iImiddot bull R[r

[plusmnJ

r------------------------------------------ 2

pound1


cc


nI 7JC1111

D DETAI L A ScA~


NOT ES

~

k (lAS

O Del ~~

( ~lIIP tl


lt

2 3 4 5 6 7

8

- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








c

8

A

B

D

2 3 4

~------------------------------------- o oomiddot------------------------------------~

10 00 REr

lt~~r~

pound ~- I

iI 1e7 IIU

~~~

t REf

Iplusmnl


pound

~If--------



NOTES

c DETA I L degA

SCALE 1

SUFfi X 26 7315 )01502


[ middot0 0 297

8

WE - Jl89gl -4

IIIpound-J~aQ9tl-~

trt E -l~89i91 -6

r-J~e9ttl-7

w[-Jegggl - 8



_ I_n

tWd)RE l SHAF 1



PARTS LIST

~ aASC

D 11DC) 1 M coJ[ 1~

PlJIAIII





B

8

5 6 7

4 15 REF

pound r amp

SEE NOTE 1

72 3 4 5 6

c

8

2 3 4 5 6 7 8



tA

OO ------------------------------------------4

8 00 RU

d (~

amp

B

1pound1 ~-$~==t

21 il2 181 REF

I 0 1 _ 002~lo4l1

iImiddot bull R[r

[plusmnJ

r------------------------------------------ 2

pound1


cc


nI 7JC1111

D DETAI L A ScA~


NOT ES

~

k (lAS

O Del ~~

( ~lIIP tl


lt

2 3 4 5 6 7

8

- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








8

2 3 4 5 6 7 8



tA

OO ------------------------------------------4

8 00 RU

d (~

amp

B

1pound1 ~-$~==t

21 il2 181 REF

I 0 1 _ 002~lo4l1

iImiddot bull R[r

[plusmnJ

r------------------------------------------ 2

pound1


cc


nI 7JC1111

D DETAI L A ScA~


NOT ES

~

k (lAS

O Del ~~

( ~lIIP tl


lt

2 3 4 5 6 7

8

- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








- -

--

--

c

A

B

o

L---

I 2 I 3 I 4

1 5 63

~O II

ffj I u


lD0-H~50DI 2X 75 --j r 000

r shy2X 2 47

L

2X 1 00


+-_____ t 500







A

f-


~

-00-1-+ I-shy

~~~~+- 2X

400

I


v l ~IICD ~Attlt

USpoundD OIl bull

110-372382

--1- ---------------1 SQJAR[ 15 1( a 1( IJ7 lebull

ASI 101 CF STEEl




~~2 I~~~ 1----MC-3723831 ~71 T 4T 2 I 3

c

- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








- -

- -

--

c

I I 2 I 3 I 4 DATE

r rr=

7

~ [ A

800 REF 75 REF

Eshy2X 2 375

rl 2X 12



716-14 UNC-2B THRU 2X 1 125

2X 7501 2X 100 tI ~+---I+-_______~


2X 2 25



o

--- shy


~O OER

A

I-- shy



B

I-- shy

IOTY REO

tZU

c


t OJ ~t tmiddot

I IIOtC AU ~ EDen

ICMCUO

I~

H CIASE

Ie ~ETl

I I 21118

14~g I OI~

2 tKI JCJT RAI( ~

JS[o CJIIII


1oID - 372382





~2 1~~231 13-MC-372411 17 7 1 2 1 1 3 T 4

---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








---

I


~--~--~~ ~I~ 2 34 REF

L-_ L

~ 200 200 375~ ~ ~ ---- 1000 REF 2355 l--

T


rAPPROVED



xx xxx ANGLES





1 AL L MACH I NED

DATE

2Z MAX SURFACES

DRAWN D FR IEND

CHECKED H CEASE

APPROVED K KREMPETZ

USED ON

MD - 372382

MAT ERIAL


DATE

l OrY REO

1298

121898

121898

1114199


SCALE



12 3823 113-MB-372481 1 OF 1

~ I

I- shy

4 )



FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight










FROM Harry Chair

Carter D-Zero






II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

S022TA












Capacity

Fixture Weight








II

1 Fermilab

To Harry Carter




wsf

cc Sam Segler wo aU

Herman Cease wo att


bull Page I

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Capacity

Fixture Weight








S022TA












Capacity

Fixture Weight








Documents

ANALYSIS OF A LIFTING FIXTURE TO HOLD A STEEL …lss.fnal.gov/archive_notes/d0-en/fermilab-d0-en-510.pdf · analysis of a lifting fixture to hold a steel mandrel horizontally from