V-6011 adsd we ad sd ad asd

8/10/2019 V-6011 adsd we ad sd ad asd

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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Input Echo : Step: 1 12:10p Dec 10,2014

PV Elite Vessel Analysis Program: Input Data

Desi gn I nt er nal Pressur e ( f or t est ) 18. 000 bar

Desi gn I nternal Temperature 50 C

Type of Test UG- 99( b)

Test Posi t i on Hor i zont al

Proj ect i on of Nozzl e f r omVessel Top 200. 00 mm

Proj ect i on of Nozzl e f r om Vessel Bott om 200. 00 mm

Mi ni mum Desi gn Met al Temper at ure 0 C

Type of Const r uct i on Wel ded

Speci al Servi ce None

Degree of Radi ography RT 1

Mi scel l aneous Wei ght Per cent 0. 0

Use Hi gher Longi t udi nal St r esses ( Fl ag) Y

Sel ect t f or I nt er nal Pressure ( Fl ag) N

Sel ect t f or Ext er nal Pressur e ( Fl ag) N

Sel ect t f or Axi al St r ess ( Fl ag) N

Sel ect Locat i on f or St i f f . Ri ngs ( Fl ag) N

Consi der Vor t ex Sheddi ng N

Per f orm a Corr oded Pressur e t est N

I s t hi s a Heat Exchanger No

User Def i ned Test Press. ( Used i f > 0) 0. 0000 bar

User def i ned MAWP 18. 843 bar

User def i ned MAPnc 0. 0000 bar

Load Case 1 NP+EW+WI +FW+BW

Load Case 2 NP+EW+EE+FS+BS

Load Case 3 NP+OW+WI +FW+BW

Load Case 4 NP+OW+EQ+FS+BS


2/204


Load Case 5 NP+HW+HI

Load Case 6 NP+HW+HE

Load Case 7 I P+OW+WI +FW+BW

Load Case 8 I P+OW+EQ+FS+BS

Load Case 9 EP+OW+WI +FW+BW

Load Case 10 EP+OW+EQ+FS+BS

Load Case 11 HP+HW+HI

Load Case 12 HP+HW+HE

Load Case 13 I P+WE+EW

Load Case 14 I P+WF+CW

Load Case 15 I P+VO+OW

Load Case 16 I P+VE+EW

Load Case 17 NP+VO+OW

Load Case 18 FS+BS+I P+OW

Load Case 19 FS+BS+EP+OW

Wi nd Desi gn Code User Def i ned

Wi nd Prof i l e Hei ght mm Pressur e kPa

10000. 0000 0. 7500

0. 0000 0. 0000

0. 0000 0. 0000

0. 0000 0. 0000

0. 0000 0. 0000

0. 0000 0. 0000

0. 0000 0. 0000

0. 0000 0. 0000

Dampi ng Factor ( Bet a) f or Wi nd ( Ope) 0. 0100

Dampi ng Factor ( Bet a) f or Wi nd ( Empty) 0. 0000

Dampi ng Fact or ( Beta) f or Wi nd ( Fi l l ed) 0. 0000


3/204


Sei smi c Desi gn Code G Loadi ng

Sei smi c I mpor t ance Factor 1. 000

G Loadi ng Coef f i ci ent Gx 0. 500

G Loadi ng Coef f i ci ent Gz 0. 500

G Loadi ng Coef f i ci ent Gy - 2. 000

Per cent Sei smi c f or Test 0. 000

Desi gn Nozzl e f or M. A. W. P. ( maxi mum) Y

Consi der MAP New and Col d i n Noz. Desi gn N

Consi der Ext ernal Loads f or Nozzl e Des. Y

Use ASME VI I I - 1 Appendi x 1- 9 N

Mat er i al Dat abase Year Cur r ent w/ Addenda or Code Year

Configuration Directives:

Do not use Nozzl e MDMT I nterpretat i on VI I I - 1 01- 37 No

Use Tabl e G i nstead of exact equat i on f or "A" Yes

Shel l Head J oi nt s are Tapered Yes

Comput e "K" i n cor r oded condi t i on No

Use Code Case 2286 No

Use t he MAWP t o comput e t he MDMT Yes

Usi ng Met r i c Mater i al Databases, ASME I I D No

Complete Listing of Vessel Elements and Details:

El ement Fr om Node 10

El ement To Node 20

El ement Type El l i pt i cal

Descr i pt i on Head

Di st ance "FROM" t o "TO" 38. 000 mm


4/204


El ement Out si de Di amet er 610. 00 mm

El ement Thi ckness 5. 0000 mm

I nternal Corr osi on Al l owance 0. 0000 mm

Nomi nal Thi ckness 8. 0000 mm

Ext ernal Cor r osi on Al l owance 0. 0000 mm

Desi gn I nter nal Pressur e 18. 000 bar

Desi gn Temper ature I nternal Pressure 50 C

Desi gn Ext ernal Pressur e 1. 0342 bar

Desi gn Temper ature Ext ernal Pressure 50 C

Ef f ecti ve Di amet er Mul t i pl i er 1. 2

Mat er i al Name SA- 240 316L

Al l owabl e St r ess, Ambi ent 115. 15 MPa

Al l owabl e St r ess, Operat i ng 115. 15 MPa

Al l owabl e St r ess, Hydr otest 155. 14 MPa

Materi al Densi t y 8027. 2 kg/ m

P Number Thi ckness 0. 0000 mm

Yi el d St r ess, Operat i ng 165. 40 MPa

External Pressure Char t Name HA- 4

UNS Number S31603

Product For m Pl at e

Ef f i ci ency, Longi t udi nal Seam 1. 0

Ef f i ci ency, Ci rcumf er ent i al Seam 1. 0

El l i pt i cal Head Factor 2. 0


Det ai l Type Li qui d

Det ai l I D LI QUI D

Di st . f r om" FROM" Node / Of f set di st - 150. 00 mm

Hei ght/ Lengt h of Li qui d 188. 00 mm

Li qui d Densi t y 909. 98 kg/ m


5/204



Detai l Type Nozzl e

Det ai l I D N3

Di st . f r om"FROM" Node / Of f set di st 0. 0000 mm

Nozzl e Di ameter 2. 0 i n.

Nozzl e Schedul e 80S

Nozzl e Cl ass 150

Layout Angl e 90. 0

Bl i nd Fl ange ( Y/ N) N

Wei ght of Nozzl e ( Used i f > 0 ) 51. 995 N

Gr ade of At t ached Fl ange GR 2. 2

Nozzl e Mat l SA- 312 TP316L

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


El ement To Node 30

El ement Type Cyl i nder

Descri pt i on Shel l


El ement Out si de Di amet er 610. 00 mm










Mat er i al Name SA- 240 316L


6/204


Ef f i ci ency, Longi t udi nal Seam 1. 0

Ef f i ci ency, Ci rcumf er ent i al Seam 1. 0


Det ai l Type Li qui d

Det ai l I D LI QUI D


Hei ght/ Lengt h of Li qui d 900. 00 mm

Li qui d Densi t y 910. 00 kg/ m



Det ai l I D N1



Nozzl e Schedul e None

Nozzl e Cl ass 600

Layout Angl e 0. 0




Nozzl e Mat l SA- 182 F316



Det ai l I D N2




Nozzl e Cl ass 150

Layout Angl e 270. 0


7/204








Det ai l I D N4




Nozzl e Cl ass 150








Det ai l I D N5




Nozzl e Cl ass 150







8/204




Det ai l I D N6




Nozzl e Cl ass 150








Det ai l I D K1




Nozzl e Cl ass 150








Detai l I D K2A




9/204



Nozzl e Cl ass 150

Layout Angl e 45. 0







Detai l I D K2B




Nozzl e Cl ass 150

Layout Angl e 45. 0







Detai l I D K3A




Nozzl e Cl ass 150

Layout Angl e 45. 0




10/204






Detai l I D K3B




Nozzl e Cl ass 150

Layout Angl e 45. 0







Detai l I D K4A




Nozzl e Cl ass 150









11/204


Detai l I D K4B




Nozzl e Cl ass 150








Detai l I D K5A




Nozzl e Cl ass 150

Layout Angl e 0. 0







Detai l I D K5B




Nozzl e Cl ass 150


12/204


Layout Angl e 0. 0







Detai l I D HH




Nozzl e Cl ass 150


Bl i nd Fl ange ( Y/ N) Y





Detai l Type Lug

Detai l I D LUG


Number of Lugs 2

Di st . f r omOD t o Lug Cnt r l i ne(dl ug) 128. 00 mm

Hei ght of Gusset Pl ates ( hgp) 306. 00 mm

Force Bear i ng Wi dth ( wf b) 204. 00 mm

Wei ght of Lug 150. 00 N

Lug St art Angl e ( degr ees) 90. 0



13/204


Detai l Type Wei ght

Det ai l I D MI ST ELI MI NATOR


Mi scel l aneous Wei ght 980. 60 N

Of f set f r omEl ement Cent erl i ne 0. 0000 mm

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


El ement To Node 40

El ement Type Fl ange

Descr i pt i on Body Fl ange


Fl ange I nsi de Di ameter ( OD f or Bl i nds) 593. 60 mm










Mat er i al Name SA- 182 F316

Al l owabl e St r ess, Ambi ent 137. 90 MPa

Al l owabl e St r ess, Operat i ng 137. 90 MPa

Al l owabl e St r ess, Hydr otest 186. 17 MPa

Materi al Densi t y 8027. 2 kg/ m

P Number Thi ckness 0. 0000 mm

Yi el d St r ess, Operat i ng 217. 74 MPa

External Pressure Char t Name HA- 2


14/204


UNS Number S31600

Cl ass / Thi ckness / Gr ade : : > 5

Product For m For gi ngs

Per f or m Fl ange St r ess Cal cul at i on ( Y/ N) Y

Wei ght of ANSI B16. 5/ B16. 47 Fl ange 0. 0000 N

Cl ass of ANSI B16. 5/ B16. 47 Fl ange

Gr ade of ANSI B16. 5/ B16. 47 Fl ange

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


El ement To Node 50

El ement Type Fl ange

Descri pt i on Bl i nd


Fl ange I nsi de Di ameter ( OD f or Bl i nds) 812. 80 mm










Mat er i al Name SA- 182 F316

Per f or m Fl ange St r ess Cal cul at i on ( Y/ N) Y

Wei ght of ANSI B16. 5/ B16. 47 Fl ange 0. 0000 N

Cl ass of ANSI B16. 5/ B16. 47 Fl ange

Gr ade of ANSI B16. 5/ B16. 47 Fl ange


15/204


PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2013


16/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Flg Calc [Int P] : A1 (flange) Flng: 3 12:10p Dec 10,2014

Flange Input Data Values Description: A1 (flange) :

Body Flange

Descr i pt i on of Fl ange Geometr y ( Type) I ntegral Wel d Neck

Desi gn Pressure P 18. 00 bar

Desi gn Temperat ure 50 C

I nternal Corr osi on Al l owance ci 0. 0000 mm

Ext ernal Cor r osi on Al l owance ce 0. 0000 mm

Use Corr osi on Al l owance i n Thi ckness Cal cs. No

Fl ange I nsi de Di amet er B 593. 600 mm

Fl ange Out si de Di amet er A 812. 800 mm

Fl ange Thi ckness t 47. 7520 mm

Thi ckness of Hub at Smal l End go 8. 0000 mm

Thi ckness of Hub at Lar ge End g1 34. 9240 mm

Lengt h of Hub h 104. 6480 mm

Fl ange Mater i al SA- 182 F316

Fl ange Mat er i al UNS number S31600

Fl ange Al l owabl e St r ess At Temper at ure Sf o 137. 90 MPa

Fl ange Al l owabl e St r ess At Ambi ent Sf a 137. 90 MPa

Bol t Materi al SA- 193 B7

Bol t Al l owabl e Str ess At Temper ature Sb 172. 38 MPa

Bol t Al l owabl e Str ess At Ambi ent Sa 172. 38 MPa

Di amet er of Bol t Ci r cl e C 749. 300 mm

Nomi nal Bol t Di amet er a 31. 7500 mm

Type of Thr eads TEMA Thread Ser i es

Number of Bol t s 20


17/204


Fl ange Face Out si de Di amet er Fod 692. 150 mm

Fl ange Face I nsi de Di amet er Fi d 593. 600 mm

Fl ange Faci ng Sketch 1, Code Sket ch 1a

Gasket Out si de Di amet er Go 685. 800 mm

Gasket I nsi de Di amet er Gi 628. 650 mm

Gasket Fact or m 0. 0000

Gasket Desi gn Seat i ng St r ess y 0. 00 MPa

Col umn f or Gasket Seat i ng 2, Code Col umn I I

Gasket Thi ckness t g 3. 1750 mm

ANSI Fl ange Cl ass 150

ANSI Fl ange Gr ade GR 2. 2

ASME Code, Section VIII, Division 1, 2013

Hub Small End Required Thickness due to Internal Pressure:

= ( P*( D/ 2+Ca) ) / ( S*E- 0. 6*P) per UG- 27 ( c) ( 1)

= ( 18. 00*( 593. 6000/ 2+0. 0000)) / ( 137. 90*1. 00- 0. 6*18. 00) +Ca

= 3. 9053 mm

Hub Small End Hub MAWP:

= ( S*E*t ) / ( R+0. 6*t ) per UG- 27 ( c) ( 1)

= ( 137. 90 * 1. 00 * 8. 0000 ) / ( 296. 8000 + 0. 6 * 8. 0000 )

= 36. 573 bar

Cor r oded Fl ange I D, Bcor = B+2*Fcor 593. 600 mm

Cor r oded Lar ge Hub, g1Cor = g1- ci 34. 924 mm

Cor r oded Smal l Hub, g0Cor = go- ci 8. 000 mm


18/204


Code R Di mensi on, R = ( C- B) / 2 - g1 42. 926 mm

Gasket Cont act Wi dth, N = ( Go - Gi ) / 2 28. 575 mm

Basi c Gasket Wi dt h, bo = N / 2 14. 287 mm

Ef f ect i ve Gasket Wi dth, b = Cb sqr t ( bo) 9. 525 mm

Gasket React i on Di amet er , G = Go ( Sel f - Energi zi ng) 685. 800 mm

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0. 785 * G * Peq

= 0. 785 * 685. 8000 * 18. 000

= 664941. 500 N

Contact Load on Gasket Surfaces [Hp]:

= 2 * b * Pi * G * m * P

= 2 * 9. 5250 * 3. 1416 * 685. 8000 * 0. 0000 * 18. 00

= 0. 000 N

Hydrostatic End Load at Flange ID [Hd]:

= Pi * Bcor * P / 4

= 3. 1416 * 593. 6000 *18. 0000/ 4

= 498168. 531 N

Pressure Force on Flange Face [Ht]:

= H - Hd

= 664941 - 498168

= 166773. 000 N

Operating Bolt Load [Wm1]:

= max( H + Hp + H' p, 0 )

= max( 664941 + 0 + 0 , 0 )

= 664941. 500 N

Gasket Seating Bolt Load [Wm2]:

= y * b * Pi * G + yPart * bPart * l p


19/204


= 0. 00*9. 5250*3. 141*685. 800+0. 00*0. 0000*0. 00

= 0. 000 N

Required Bolt Area [Am]:

= Maxi mum of Wm1/ Sb, Wm2/ Sa

= Maxi mum of 664941/ 172 , 0/ 172

= 3857. 857 mm

ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:

= 2a + 6t / ( m + 0. 5)

= 2 * 31. 750 + 6 * 47. 752/ ( 0. 00 + 0. 5)

= 636. 524 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * si n( pi / n )

= 749. 300 * si n( 3. 142/ 20 )

= 117. 216 mm

ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:

= max( sqr t ( Bs/ ( 2a + t ) ) , 1 )

= max( sqr t ( 117. 216/ ( 2 * 31. 750 + 47. 752 ) ) , 1 )

= 1. 0265

Bolting Information for TEMA Imperial Thread Series (Non Mandatory):

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

Mi ni mum Act ual Maxi mum

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

Bol t Ar ea, mm 3857. 857 11987. 072

Radi al di st ance bet . hub and bol t s 44. 450 42. 926

Radi al di st ance bet . bol t s and t he edge 31. 750 31. 750

Ci r cumf erent i al spaci ng bet ween bol t s 71. 450 117. 216 636. 524

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


20/204


Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172. 38 * ( 3857. 8567 + 11987. 0723 ) / 2

= 1365518. 75 N

Gasket Load for the Operating Condition [HG]:

= Wm1 - H

= 664941 - 664941

= 0. 00 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= ( C - G ) / 2

= ( 749. 3000 - 685. 8000 ) / 2

= 31. 7500 mm

Distance to Face Pressure Reaction [ht]:

= ( R + g1 + hg ) / 2

= ( 42. 9260 + 34. 9240 + 31. 7500 ) / 2

= 54. 8000 mm

Distance to End Pressure Reaction [hd]:

= R + ( g1 / 2 )

= 42. 9260 + ( 34. 9240/ 2. 0 )

= 60. 3880 mm

Summary of Moments for Internal Pressure:

Loadi ng Force Di st ance Bol t Cor r Moment

End Pr essur e, Md 498169. 60. 3880 1. 0265 30892. N- m

Face Pr essur e, Mt 166773. 54. 8000 1. 0265 9385. N- m

Gasket Load, Mg 0. 31. 7500 1. 0265 0. N- m

Gasket Seat i ng, Mat m 1365519. 31. 7500 1. 0265 44520. N- m


21/204


Tot al Moment f or Operat i on, Mop 40277. N- m

Tot al Moment f or Gasket seat i ng, Mat m 44520. N- m

Note: User choose not to perform Stress Calculations on this ANSI Flange.

Pressure rating of the flange will be used to check code compliance.

Est i mated Fi ni shed Wei ght of Fl ange at gi ven Thk. 127. 6 kgm

Est i mated Unf i ni shed Wei ght of Forgi ng at gi ven Thk 296. 2 kgm



22/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Flg Calc [Int P] : A1 (blind) Flng: 4 12:10p Dec 10,2014

Flange Input Data Values Description: A1 (blind) :

Bl i nd

Descr i pt i on of Fl ange Geometr y ( Type) Bl i nd

Desi gn Pressure P 18. 00 bar

Desi gn Temperat ure 50 C

I nternal Corr osi on Al l owance ci 0. 0000 mm

Ext ernal Cor r osi on Al l owance ce 0. 0000 mm

Use Corr osi on Al l owance i n Thi ckness Cal cs. Yes

Fl ange Out si de Di amet er A 812. 800 mm

Fl ange Thi ckness t 47. 7520 mm

Fl ange Mater i al SA- 182 F316

Fl ange Mat er i al UNS number S31600

Fl ange Al l owabl e St r ess At Temper at ure Sf o 137. 90 MPa

Fl ange Al l owabl e St r ess At Ambi ent Sf a 137. 90 MPa


Bol t Al l owabl e Str ess At Temper ature Sb 172. 38 MPa

Bol t Al l owabl e Str ess At Ambi ent Sa 172. 38 MPa

Di amet er of t he Load React i on, Long Span D 0. 000 mm

Di amet er of t he Load React i on, Shor t Span d 0. 000 mm

Peri met er al ong t he Cent er of t he Bol t s L 2353. 995 mm

Di amet er of Bol t Ci r cl e C 749. 300 mm

Nomi nal Bol t Di amet er a 31. 7500 mm

Type of Thr eads TEMA Thread Ser i es

Number of Bol t s 20


23/204


Fl ange Face Out si de Di amet er Fod 692. 150 mm

Fl ange Face I nsi de Di amet er Fi d 590. 550 mm

Fl ange Faci ng Sketch 1, Code Sket ch 1a

Gasket Out si de Di amet er Go 685. 800 mm

Gasket I nsi de Di amet er Gi 628. 650 mm

Gasket Fact or m 0. 0000

Gasket Desi gn Seat i ng St r ess y 0. 00 MPa

Col umn f or Gasket Seat i ng 2, Code Col umn I I

Gasket Thi ckness t g 3. 1750 mm

ANSI Fl ange Cl ass 150

ANSI Fl ange Gr ade GR 2. 2


Gasket Cont act Wi dth, N = ( Go - Gi ) / 2 28. 575 mm

Basi c Gasket Wi dt h, bo = N / 2 14. 287 mm

Ef f ect i ve Gasket Wi dth, b = Cb sqr t ( bo) 9. 525 mm

Gasket React i on Di amet er , G = Go ( Sel f - Energi zi ng) 685. 800 mm

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0. 785 * G * Peq

= 0. 785 * 685. 8000 * 18. 000

= 664941. 500 N

Contact Load on Gasket Surfaces [Hp]:


24/204


= 2 * b * Pi * G * m * P

= 2 * 9. 5250 * 3. 1416 * 685. 8000 * 0. 0000 * 18. 00

= 0. 000 N

Operating Bolt Load [Wm1]:

= max( H + Hp + H' p, 0 )

= max( 664941 + 0 + 0 , 0 )

= 664941. 500 N

Gasket Seating Bolt Load [Wm2]:

= y * b * Pi * G + yPart * bPart * l p

= 0. 00*9. 5250*3. 141*685. 800+0. 00*0. 0000*0. 00

= 0. 000 N

Required Bolt Area [Am]:

= Maxi mum of Wm1/ Sb, Wm2/ Sa

= Maxi mum of 664941/ 172 , 0/ 172

= 3857. 857 mm

ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:

= 2a + 6t / ( m + 0. 5)

= 2 * 31. 750 + 6 * 47. 752/ ( 0. 00 + 0. 5)

= 636. 524 mm

Actual Circumferential Bolt Spacing [Bs]:

= C * si n( pi / n )

= 749. 300 * si n( 3. 142/ 20 )

= 117. 216 mm

ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:

= max( sqr t ( Bs/ ( 2a + t ) ) , 1 )

= max( sqr t ( 117. 216/ ( 2 * 31. 750 + 47. 752 ) ) , 1 )

= 1. 0265


25/204


Bolting Information for TEMA Imperial Thread Series (Non Mandatory):

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

Mi ni mum Act ual Maxi mum

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

Bol t Ar ea, mm 3857. 857 11987. 072

Radi al di st ance bet . bol t s and t he edge 31. 750 31. 750

Ci r cumf erent i al spaci ng bet ween bol t s 71. 450 117. 216 636. 524

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

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * ( Am + Ab ) / 2

= 172. 38 * ( 3857. 8567 + 11987. 0723 ) / 2

= 1365518. 75 N

Gasket Load for the Operating Condition [HG]:

= Wm1

= 664941. 50 N

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= ( C - G ) / 2

= ( 749. 3000 - 685. 8000 ) / 2

= 31. 7500 mm

Note: User choose not to perform Stress Calculations on this ANSI Flange.

Pressure rating of the flange will be used to check code compliance.

Est i mated Fi ni shed Wei ght of Fl ange at gi ven Thk. 198. 9 kgm

Est i mated Unf i ni shed Wei ght of Forgi ng at gi ven Thk 198. 9 kgm



26/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Internal Pressure Calculations : Step: 5 12:10p Dec 10,2014

Element Thickness, Pressure, Diameter and Allowable Stress :

| | I nt . Pr ess | Nomi nal | Tot al Cor r | El ement | Al l owabl e |

From| To | + Li q. Hd | Thi ckness | Al l owance | Di ameter | St r ess(SE) |

| | bar | mm | mm | mm | MPa |

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

Head| 18. 097 | 8. 0000 | . . . | 610. 00 | 115. 15 |

Shel l | 18. 080 | 8. 0000 | . . . | 610. 00 | 115. 15 |

Body Fl ang| 18. 000 | 8. 0000 | . . . | 593. 60 | 137. 90 |

Bl i nd| 18. 000 | 8. 0000 | . . . | 812. 80 | 137. 90 |

Element Required Thickness and MAWP :

| | Desi gn | M. A. W. P. | M. A. P. | Mi ni mum | Requi r ed |

From| To | Pressur e | Corr oded | New & Col d | Thi ckness | Thi ckness |

| | bar | bar | bar | mm | mm |

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

Head| 18. 0000 | 19. 0593 | 19. 1564 | 5. 00000 | 4. 72737 |

Shel l | 18. 0000 | 30. 4379 | 30. 5182 | 8. 00000 | 4. 75991 |

Body Fl ang| 18. 0000 | 18. 3984 | 18. 9983 | 47. 7520 | No Cal c |

Bl i nd| 18. 0000 | 18. 3984 | 18. 9983 | 47. 7520 | No Cal c |

Mi ni mum 18. 843 18. 998

Internal Pressure Calculation Results :


Elliptical HeadFrom 10 To 20 SA-240 316L at 50 C


27/204


Head

Longitudinal Joint: Full Radiography per UW-11(a) Type 1

Circumferential Joint: Full Radiography per UW-11(a) Type 1

Material UNS Number: S31603

Required Thickness due to Internal Pressure [tr]:

= ( P*Do*K) / ( 2*S*E+2*P*( K- 0. 1) ) per Appendi x 1- 4 ( c)

= ( 18. 097*610. 0000*1. 000) / ( 2*115. 15*1. 00+2*18. 097*( 1. 000- 0. 1) )

= 4. 7274 + 0. 0000 = 4. 7274 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:

Less Operating Hydrostatic Head Pressure of 0.097 bar

= ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c)

= ( 2*115. 15*1. 00*5. 0000) / ( 1. 000*610. 0000- 2*5. 0000*( 1. 00- 0. 1) )

= 19. 156 - 0. 097 = 19. 059 bar

Maximum Allowable Pressure, New and Cold [MAPNC]:

= ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c)

= ( 2*115. 15*1. 00*5. 0000) / ( 1. 000*610. 0000- 2*5. 0000*( 1. 000- 0. 1) )

= 19. 156 bar

Actual stress at given pressure and thickness, corroded [Sact]:

= ( P*( K*Do- 2*t *( K- 0. 1) ) ) / ( 2*E*t )

= ( 18. 097*( 1. 000*610. 0000- 2*5. 0000*( 1. 000- 0. 1) ) ) / ( 2*1. 00*5. 0000)

= 108. 779 MPa

Straight Flange Required Thickness:

= ( P*Ro) / ( S*E+0. 4*P) + ca per Appendi x 1- 1 ( a) ( 1)

= ( 18. 097*305. 0000) / ( 115. 15*1. 00+0. 4*18. 097)+0. 000


28/204


= 4. 764 mm

Straight Flange Maximum Allowable Working Pressure:


= ( S*E*t ) / ( Ro- 0. 4*t ) per Appendi x 1- 1 (a) ( 1)

= ( 115. 15 * 1. 00 * 8. 0000 ) / ( 305. 0000 - 0. 4 * 8. 0000 )

= 30. 518 - 0. 084 = 30. 434 bar

Per cent El ongat i on per UHA- 44 ( 75*t nom/ Rf ) *( 1- Rf / Ro) 5. 715 %

Note: Pl ease Check Requi r ement s of Tabl e UHA- 44 f or El ongat i on l i mi t s.

SA-240 316L, Min Metal Temp without impact per UHA-51: -196 C

Cylindrical ShellFrom 20 To 30 SA-240 316L at 50 C

Shel l

Longitudinal Joint: Full Radiography per UW-11(a) Type 1

Circumferential Joint: Full Radiography per UW-11(a) Type 1



= ( P*Ro) / ( S*E+0. 4*P) per Appendi x 1- 1 ( a) ( 1)

= ( 18. 080*305. 0000) / ( 115. 15*1. 00+0. 4*18. 080)

= 4. 7599 + 0. 0000 = 4. 7599 mm




= (115. 15*1. 00*8. 0000) / ( 305. 0000- 0. 4*8. 0000)


29/204


= 30. 518 - 0. 080 = 30. 438 bar

Maximum Allowable Pressure, New and Cold [MAPNC]:


= (115. 15*1. 00*8. 0000) / ( 305. 0000- 0. 4*8. 0000)

= 30. 518 bar

Actual stress at given pressure and thickness, corroded [Sact]:

= ( P*( Ro- 0. 4*t ) ) / ( E*t )

= ( 18. 080*( ( 305. 0000- 0. 4*8. 0000) ) / ( 1. 00*8. 0000)

= 68. 218 MPa

Per cent El ongat i on per UHA- 44 ( 50*t nom/ Rf ) *( 1- Rf / Ro) 1. 329 %

Note: Pl ease Check Requi r ement s of Tabl e UHA- 44 f or El ongat i on l i mi t s.

SA-240 316L, Min Metal Temp without impact per UHA-51: -196 C

Hydrostatic Test Pressure Results:

Pr essur e per UG99b = 1. 3 * M. A. W. P. * Sa/ S 24. 496 bar

Pressure per UG99b[ 34] = 1. 3 * Desi gn Pres * Sa/ S 23. 400 bar

Pressure per UG99c = 1. 3 * M. A. P. - Head(Hyd) 24. 579 bar

Pr essur e per UG100 = 1. 1 * M. A. W. P. * Sa/ S 20. 727 bar

Pr essur e per PED = 1. 43 * MAWP 26. 945 bar

UG-99(b), Test Pressure Calculation:

= Test Factor * MAWP * St r ess Rat i o

= 1. 3 * 18. 843 * 1. 000

= 24. 496 bar

Horizontal Test performed per: UG-99b


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31/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------External Pressure Calculations : Step: 6 12:10p Dec 10,2014

External Pressure Calculation Results :


Elliptical HeadFrom 10 to 20 Ext. Chart: HA-4 at 50 C

Head

Elastic Modulus from Chart: HA-4 at 50 C : 0.192E+06 MPa

Results for Maximum Allowable External Pressure (MAEP):

Tca OD D/ t Fact or A B

5. 000 610. 00 122. 00 0. 0011384 65. 13

EMAP = B/ ( K0*D/ t ) = 65. 1257/ ( 0. 9000 *122. 0000 ) = 5. 9304 bar

Results for Required Thickness (Tca):

Tca OD D/ t Fact or A B

1. 613 610. 00 378. 29 0. 0003672 35. 22

EMAP = B/ ( K0*D/ t ) = 35. 2184/ ( 0. 9000 *378. 2888 ) = 1. 0343 bar

Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.



= ( P*Do*K) / ( 2*S*E+2*P*( K- 0. 1) ) per Appendi x 1- 4 ( c)

= ( 1. 727*610. 0000*1. 000) / ( 2*115. 15*1. 00+2*1. 727*( 1. 000- 0. 1) )

= 0. 4569 + 0. 0000 = 0. 4569 mm


32/204



= ( ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) ) / 1. 67 per Appendi x 1- 4 ( c)

= ( ( 2*115. 15*1. 00*5. 0000) / ( 1. 000*610. 0000- 2*5. 0000*( 1. 00- 0. 1) ) ) / 1. 67

= 11. 471 bar

Maximum Allowable External Pressure [MAEP]:

= mi n( MAEP, MAWP )

= mi n( 5. 93 , 11. 4709 )

= 5. 930 bar

Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.

Cylindrical ShellFrom 20 to 30 Ext. Chart: HA-4 at 50 C

Shel l

Elastic Modulus from Chart: HA-4 at 50 C : 0.192E+06 MPa

Results for Maximum Allowable External Pressure (MAEP):

Tca OD SLEN D/ t L/ D Fact or A B

8. 000 610. 00 2450. 00 76. 25 4. 0164 0. 0004580 43. 93

EMAP = ( 4*B) / ( 3*( D/ t ) ) = ( 4*43. 9307 ) / ( 3*76. 2500 ) = 7. 6808 bar

Results for Required Thickness (Tca):


3. 545 610. 00 2450. 00 172. 09 4. 0164 0. 0001392 13. 35

EMAP = ( 4*B) / ( 3*( D/ t ) ) = ( 4*13. 3512 ) / ( 3*172. 0930 ) = 1. 0343 bar

Results for Maximum Stiffened Length (Slen):



33/204


8. 000 610. 00 67902. 07 76. 25 50. 0000 0. 0001932 18. 54

EMAP = ( 4*B) / ( 3*( D/ t ) ) = ( 4*18. 5364 ) / ( 3*76. 2500 ) = 3. 2409 bar

External Pressure Calculations

| | Secti on | Out si de | Corr oded | Factor | Factor |

From| To | Lengt h | Di ameter | Thi ckness | A | B |

| | mm | mm | mm | | MPa |

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

10| 20| No Cal c | 610. 000 | 5. 00000 | 0. 0011384 | 65. 1257 |

20| 30| 2450. 00 | 610. 000 | 8. 00000 | 0. 00045798 | 43. 9307 |

30| 40| No Cal c | . . . | 47. 7520 | No Cal c | No Cal c |

40| 50| No Cal c | . . . | 47. 7520 | No Cal c | No Cal c |


| | Ext ernal | Ext ernal | Ext ernal | Ext ernal |

From| To | Act ual T. | Requi r ed T. | Des. Press. | M. A. W. P. |

| | mm | mm | bar | bar |

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

10| 20| 5. 00000 | 1. 61252 | 1. 03420 | 5. 93044 |

20| 30| 8. 00000 | 3. 54460 | 1. 03420 | 7. 68076 |

30| 40| 47. 7520 | No Cal c | 1. 03420 | No Cal c |

40| 50| 47. 7520 | No Cal c | 1. 03420 | No Cal c |

Mi ni mum 5. 930


| | Actual Len. | Al l ow. Len. | Ri ng I nert i a | Ri ng I nert i a |

From| To | Bet . St i f f . | Bet . St i f f . | Requi red | Avai l abl e |

| | mm | mm | mm**4 | mm**4 |


34/204


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

10| 20| No Cal c | No Cal c | No Cal c | No Cal c |

20| 30| 2450. 00 | 67902. 1 | No Cal c | No Cal c |



Elements Suitable for External Pressure.



35/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Element and Detail Weights : Step: 7 12:10p Dec 10,2014

Element and Detail Weights

| | El ement | El ement | Corr oded | Corr oded | Ext r a due |

From| To | Metal Wgt . | I D Vol ume | Metal Wgt . | I D Vol ume | Mi sc % |

| | kgm | m | kgm | m | kgm |

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

10| 20| 33. 0736 | 0. 039026 | 33. 0736 | 0. 039026 | 1. 65368 |

20| 30| 286. 871 | 0. 65467 | 286. 871 | 0. 65467 | 14. 3435 |

30| 40| 127. 648 | 0. 042183 | 127. 648 | 0. 042183 | 6. 38241 |

40| 50| 198. 893 | . . . | 198. 893 | . . . | 9. 94463 |

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

Tot al 646 0. 74 646 0. 74 32

Weight of Details

| | Wei ght of | X Of f set , | Y Of f set , |

From| Type| Det ai l | Dt l . Cent . | Dt l . Cent . | Descri pt i on

| | kgm | mm | mm |

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

10| Li qd| 35. 5072 | . . . | - 75. 0000 | LI QUI D

10| Nozl | 5. 56748 | . . . | - 150. 000 | N3

20| Li qd| 226. 965 | . . . | 450. 000 | LI QUI D

20| Nozl | 8. 73081 | 322. 400 | 1362. 00 | N1

20| Nozl | 7. 18497 | 322. 400 | 2149. 00 | N2

20| Nozl | 7. 18497 | 322. 400 | 2149. 00 | N4

20| Nozl | 7. 18497 | 322. 400 | 1874. 00 | N5

20| Nozl | 7. 18497 | 322. 400 | 120. 000 | N6

20| Nozl | 7. 18497 | 322. 400 | 1851. 00 | K1

20| Nozl | 8. 15833 | 341. 450 | 1572. 00 | K2A

20| Nozl | 8. 15833 | 341. 450 | 1362. 00 | K2B


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20| Nozl | 8. 15833 | 341. 450 | 622. 000 | K3A

20| Nozl | 8. 15833 | 341. 450 | 342. 000 | K3B

20| Nozl | 7. 18497 | 322. 400 | 1637. 00 | K4A

20| Nozl | 7. 18497 | 322. 400 | 557. 000 | K4B

20| Nozl | 8. 15833 | 341. 450 | 837. 000 | K5A

20| Nozl | 8. 15833 | 341. 450 | 342. 000 | K5B

20| Nozl | 19. 8200 | 354. 150 | 1662. 00 | HH

20| Lugs| 32. 1232 | . . . | 1210. 00 | LUG

20| Wght | 100. 000 | . . . | 2100. 00 | MI ST ELI MI NATOR

Total Weight of Each Detail Type

Tot al Wei ght of Li qui d 262. 5

Tot al Wei ght of Nozzl es 133. 4

Tot al Wei ght of Lugs 32. 1

Tot al Wei ght of Wei ghts 100. 0

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

Sumof t he Detai l Wei ght s 528. 0 kgm

Weight Summation

Fabr i cat ed Shop Test Shi ppi ng Erect ed Empty Operat i ng

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

678. 8 844. 3 678. 8 844. 3 678. 8 844. 3

. . . 735. 4 . . . . . . . . . 262. 5

133. 4 . . . 133. 4 . . . . . . . . .

32. 1 . . . 32. 1 . . . . . . . . .

. . . . . . . . . . . . . . . 100. 0

. . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . 133. 4 . . .


37/204


38/204


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Note: The cumulative operating weights no liquid in the column above

are the cumulative operating weights minus the operating liquid

weight minus any weights absent in the empty condition.

Cumulative Vessel Moment

| | Cumul at i ve | Cumul ati ve | Cumul ati ve |

Fr om| To | Empt y Mom. | Oper. Mom. | Hydro. Mom. |

| | N- m | N- m | N- m |

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

10| 20| . . . | . . . | . . . |

20| Lugs| 187. 729 | 187. 729 | 187. 729 |

Lugs| 30| 231. 775 | 231. 775 | 231. 775 |

30| 40| . . . | . . . | . . . |

40| 50| . . . | . . . | . . . |



40/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------

Nozzle Flange MAWP : Step: 8 12:10p Dec 10,2014

Nozzle Flange MAWP Results :

Nozzl e - - - - - Fl ange Rat i ng

Descr i pt i on Oper at i ng Ambi ent Temper at ure Cl ass Gr ade| Gr oup

bar bar C

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

N3 18. 4 19. 0 50 150 GR 2. 2

N1 96. 2 99. 3 50 600 GR 2. 2

N2 18. 4 19. 0 50 150 GR 2. 2

N4 18. 4 19. 0 50 150 GR 2. 2

N5 18. 4 19. 0 50 150 GR 2. 2

N6 18. 4 19. 0 50 150 GR 2. 2

K1 18. 4 19. 0 50 150 GR 2. 2

K2A 18. 4 19. 0 50 150 GR 2. 2

K2B 18. 4 19. 0 50 150 GR 2. 2

K3A 18. 4 19. 0 50 150 GR 2. 2

K3B 18. 4 19. 0 50 150 GR 2. 2

K4A 18. 4 19. 0 50 150 GR 2. 2

K4B 18. 4 19. 0 50 150 GR 2. 2

K5A 18. 4 19. 0 50 150 GR 2. 2

K5B 18. 4 19. 0 50 150 GR 2. 2

HH 18. 4 19. 0 50 150 GR 2. 2

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

Mi ni mum Rat i ng 18. 4 19. 0 bar

Note: ANSI Ratings are per ANSI/ASME B16.5 2009 Metric Edition



41/204


Natural Frequency Calculation : Step: 9 12:10p Dec 10,2014

The Natural Frequencies for the vessel have been computed iteratively

by solving a system of matrices. These matrices describe the mass

and the stiffness of the vessel. This is the generalized eigenvalue/

eigenvector problem and is referenced in some mathematical texts.

The Natural Frequency for the Vessel (Empty.) is 74.6233 Hz.

The Natural Frequency for the Vessel (Ope...) is 70.8811 Hz.



42/204


Wind Load Calculation : Step: 10 12:10p Dec 10,2014

Note: Using the User Defined Wind Profile ...

Wind Vibration Calculations

This evaluation is based on work by Kanti Mahajan and Ed Zorilla

Nomenclature

Cf - Cor r ect i on f act or f or nat ur al f r equency

D - Aver age i nternal di ameter of vessel mm

Df - Dampi ng Factor < 0. 75 Unst abl e, > 0. 95 Stabl e

Dr - Aver age i nt er nal di ameter of t op hal f of vessel mm

f - Nat ur al f r equency of vi br at i on ( Her t z)

f 1 - Natural f r equency of bar e vessel based on a uni t val ue of ( D/ L ) ( 104)

L - Tot al hei ght of st r uct ur e mm

Lc - Tot al l engt h of coni cal sect i on( s) of vessel mm

t b - Uncor r oded pl ate thi ckness at bott omof vessel mm

V30 - Desi gn Wi nd Speed pr ovi ded by user km/ hr

Vc - Cr i t i cal wi nd vel oci t y km/ hr

Vw - Maxi mumwi nd speed at t op of st r uct ure km/ hr

W - Total cor r oded wei ght of st r uct ur e N

Ws - Cor . vessel wei ght excl . wei ght of par t s whi ch do not ef f ect st i f f . N

Z - Maxi mumampl i t ude of vi br at i on at t op of vessel mm

Dl - Logari t hmi c decrement ( t aken as 0. 03 f or Wel ded St r uct ures )

Vp - Vi b. Chance,


43/204


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PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Earthquake Load Calculation : Step: 11 12:10p Dec 10,2014

Earthquake Loading Specified in G's

Hor i zont al Accel er at i on f act or ( GX) 0. 500

Hor i zont al Accel er at i on f act or ( GZ) 0. 500

Ver t i cal Accel erat i on f actor ( GY) - 2. 000

The Natural Frequency for the Vessel (Ope...) is 70.8811 Hz.

Earthquake Load Calculation

| | Eart hquake | Ear t hquake | El ement | El ement |

Fr om| To | Hei ght | Wei ght | Ope Load | Emp Load |

| | mm | N | N | N |

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

10| 20| 19. 0000 | 743. 314 | 525. 602 | 279. 399 |

20| Lugs| 1095. 00 | 3317. 37 | 2345. 73 | 1331. 19 |

Lugs| 30| 1747. 50 | 4095. 71 | 2896. 11 | 1643. 52 |

30| 40| 2476. 20 | 1314. 30 | 929. 353 | 929. 353 |

40| 50| 2576. 28 | 2047. 86 | 1448. 05 | 1448. 05 |



46/204


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48/204


Wind Deflection : Step: 13 12:10p Dec 10,2014



49/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Longitudinal Stress Constants : Step: 14 12:10p Dec 10,2014

Longitudinal Stress Constants

| | Metal Ar ea | Metal Ar ea | New & Col d | Corr oded |

From| To | New & Col d | Corr oded | Sect . Mod. | Sect . Mod. |

| | mm | mm | mm | mm |

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

10| 20| 9503. 34 | 9503. 34 | 1. 426E+06 | 1. 426E+06 |

20| 30| 15129. 9 | 15129. 9 | 2. 248E+06 | 2. 248E+06 |

30| 40| 15129. 9 | 15129. 9 | 2. 248E+06 | 2. 248E+06 |

40| 50| 15129. 9 | 15129. 9 | 2. 248E+06 | 2. 248E+06 |



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51/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Longitudinal Stresses Due to . . . Step: 16 12:10p Dec 10,2014

Longitudinal Stress Report

Note: Longitudinal Operating and Empty Stresses are computed in the

corroded condition. Stresses due to loads in the hydrostatic test

cases have been computed in the new and cold condition.

Longitudinal Stresses Due to . . .

| | Long. St r . | Long. St r . | Long. St r . |

From| To | I nt . Pres. | Ext . Pres. | Hyd. Pres. |

| | MPa | MPa | MPa |

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

10| 20| 53. 6478 | - 3. 18083 | 73. 0084 |

20| 30| 33. 0573 | - 1. 99793 | 44. 9871 |

30| 40| . . . | . . . | . . . |

40| 50| . . . | . . . | . . . |


| | Wght . Str . | Wght . Str . | Wght . Str . | Wght . Str . | Wght . Str . |

Fr om| To | Empty | Operat i ng | Hydr otest | Emp. Mom. | Opr. Mom. |

| | MPa | MPa | MPa | MPa | MPa |

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

10| 20| . . . | . . . | . . . | . . . | . . . |

20| Lugs| 0. 026118 | 0. 049133 | . . . | 0. 083498 | 0. 083498 |

Lugs| 30| - 0. 41169 | - 0. 34585 | . . . | 0. 10309 | 0. 10309 |

30| 40| -0. 22224 | -0. 22224 | . . . | . . . | . . . |

40| 50| -0. 13536 | -0. 13536 | . . . | . . . | . . . |



52/204


| | Wght . Str . | Bend. St r. | Bend. Str . | Bend. Str . | Bend. St r. |

Fr om| To | Hyd. Mom. | Oper . Wi nd | Oper . Equ. | Hyd. Wi nd | Hyd. Equ. |

| | MPa | MPa | MPa | MPa | MPa |

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

10| 20| . . . | . . . | . . . | . . . | . . . |

20| Lugs| . . . | 0. 0017799 | 0. 010668 | . . . | . . . |

Lugs| 30| . . . | 0. 10158 | 1. 55693 | . . . | . . . |

30| 40| . . . | 0. 0055003 | 0. 14509 | . . . | . . . |

40| 50| . . . | 0. 00037110 | 0. 015384 | . . . | . . . |


| | Long. St r . | Long. St r . | Long. St r. | Ear t hQuake |

From| To | Vort ex Ope. | Vort ex Emp. | Vort ex Tst . | Empt y |

| | MPa | MPa | MPa | MPa |

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

10| 20| . . . | . . . | . . . | . . . |

20| Lugs | . . . | . . . | . . . | 0. 0056709 |

Lugs | 30| . . . | . . . | . . . | 1. 55264 |

30| 40| . . . | . . . | . . . | 0. 14509 |

40| 50| . . . | . . . | . . . | 0. 015384 |


| | Long. St r . | Long. St r . |

From| To | Y Forces W | Y ForceS S |

| | MPa | MPa |

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

10| 20| . . . | 0. 15645 |

20| Lugs| . . . | 0. 53682 |


53/204


Lugs| 30| . . . | - 0. 98593 |

30| 40| . . . | - 0. 44448 |

40| 50| . . . | - 0. 27073 |

Long. Stresses due to User Forces and Moments

| | Wi nd For / Mom| Eqk For / Mom| Wnd For / Mom| Eqk For / Mom|

From| To | Corr oded | Corr oded | No Corr . | No Corr . |

| | MPa | MPa | MPa | MPa |

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

10| 20| . . . | . . . | . . . | . . . |

20| Lugs| . . . | . . . | . . . | . . . |

Lugs| 30| . . . | . . . | . . . | . . . |

30| 40| . . . | . . . | . . . | . . . |

40| 50| . . . | . . . | . . . | . . . |



54/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Stress due to Combined Loads : Step: 17 12:10p Dec 10,2014

Stress Combination Load Cases for Vertical Vessels:

Load Case Definition Key

I P = Longi t udi nal St r ess due t o I nt er nal Pressur e

EP = Longi t udi nal St r ess due t o External Pressur e

HP = Longi t udi nal St r ess due to Hydr otest Pressur e

NP = No Pr essur e

EW = Longi t udi nal St r ess due t o Wei ght ( No Li qui d)

OW = Longi t udi nal St r ess due to Wei ght ( Operat i ng)

HW = Longi t udi nal St r ess due t o Wei ght ( Hydr otest )

WI = Bendi ng St r ess due t o Wi nd Moment ( Oper at i ng)

EQ = Bendi ng St r ess due t o Ear t hquake Moment ( Oper at i ng)

EE = Bendi ng St r ess due t o Eart hquake Moment ( Empt y)

HI = Bendi ng St r ess due to Wi nd Moment ( Hydr ot est )

HE = Bendi ng St r ess due t o Ear t hquake Moment ( Hydrot est )

WE = Bendi ng St r ess due to Wi nd Moment ( Empt y) ( no CA)

WF = Bendi ng St r ess due to Wi nd Moment ( Fi l l ed) ( no CA)

CW = Longi t udi nal St r ess due t o Wei ght ( Empt y) ( no CA)

VO = Bendi ng St r ess due t o Vor t ex Sheddi ng Loads ( Ope )

VE = Bendi ng St r ess due t o Vor t ex Sheddi ng Loads ( Emp )

VF = Bendi ng Str ess due to Vor t ex Sheddi ng Loads ( Test No CA. )

FW = Axi al St r ess due t o Ver t i cal For ces f or t he Wi nd Case

FS = Axi al St r ess due to Ver t i cal For ces f or t he Sei smi c Case

BW = Bendi ng Str ess due to Lat . Forces f or t he Wi nd Case, Corr oded

BS = Bendi ng St r ess due t o Lat . For ces f or t he Sei smi c Case, Corr oded

BN = Bendi ng Str ess due t o Lat . Forces f or t he Wi nd Case, UnCor r oded

BU = Bendi ng Str ess due to Lat . Forces f or t he Sei smi c Case, UnCorr oded

General Notes:


55/204


Case types HI and HE are in the Un-Corroded condition.

Case types WE, WF, and CW are in the Un-Corroded condition.

A blank stress and stress ratio indicates that the corresponding

stress comprising those components that did not contribute to that

type of stress.

An asterisk (*) in the final column denotes overstress.

Analysis of Load Case 1 : NP+EW+WI+FW+BW

From Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp.

Node St r ess St r ess St r ess St r ess Rati o Rat i o

10 0. 00 138. 18 0. 00 88. 00 0. 0000 0. 0000

20 0. 11 138. 18 - 0. 06 95. 51 0. 0008 0. 0006

20 138. 18 - 0. 62 95. 51 0. 0065

Analysis of Load Case 2 : NP+EW+EE+FS+BS



10 0. 16 138. 18 88. 00 0. 0011

20 0. 65 138. 18 95. 51 0. 0047

20 0. 26 138. 18 - 3. 05 95. 51 0. 0019 0. 0320

Analysis of Load Case 3 : NP+OW+WI+FW+BW



10 0. 00 138. 18 0. 00 88. 00 0. 0000 0. 0000


56/204


20 0. 13 138. 18 - 0. 04 95. 51 0. 0010 0. 0004

20 138. 18 - 0. 55 95. 51 0. 0058

Analysis of Load Case 4 : NP+OW+EQ+FS+BS



10 0. 16 138. 18 88. 00 0. 0011

20 0. 68 138. 18 95. 51 0. 0049

20 0. 33 138. 18 - 2. 99 95. 51 0. 0024 0. 0313

Analysis of Load Case 5 : NP+HW+HI



10 0. 00 186. 17 0. 00 90. 17 0. 0000 0. 0000

20 0. 00 186. 17 0. 00 97. 87 0. 0000 0. 0000

20 0. 00 186. 17 0. 00 97. 87 0. 0000 0. 0000

Analysis of Load Case 6 : NP+HW+HE



10 0. 00 186. 17 0. 00 90. 17 0. 0000 0. 0000

20 0. 00 186. 17 0. 00 97. 87 0. 0000 0. 0000

20 0. 00 186. 17 0. 00 97. 87 0. 0000 0. 0000

Analysis of Load Case 7 : IP+OW+WI+FW+BW



10 53. 65 138. 18 88. 00 0. 3883

20 33. 19 138. 18 95. 51 0. 2402

20 32. 92 138. 18 95. 51 0. 2382


57/204


58/204


10 73. 01 186. 17 90. 17 0. 3922

20 44. 99 186. 17 97. 87 0. 2417

20 44. 99 186. 17 97. 87 0. 2417

Analysis of Load Case 13 : IP+WE+EW



10 53. 65 138. 18 88. 00 0. 3883

20 33. 17 138. 18 95. 51 0. 2400

20 32. 75 138. 18 95. 51 0. 2370

Analysis of Load Case 14 : IP+WF+CW



10 53. 65 138. 18 88. 00 0. 3883

20 33. 11 138. 18 95. 51 0. 2396

20 32. 71 138. 18 95. 51 0. 2367

Analysis of Load Case 15 : IP+VO+OW



10 53. 65 138. 18 88. 00 0. 3883

20 33. 19 138. 18 95. 51 0. 2402

20 32. 81 138. 18 95. 51 0. 2375

Analysis of Load Case 16 : IP+VE+EW



10 53. 65 138. 18 88. 00 0. 3883

20 33. 17 138. 18 95. 51 0. 2400

20 32. 75 138. 18 95. 51 0. 2370


59/204


Analysis of Load Case 17 : NP+VO+OW



10 0. 00 138. 18 0. 00 88. 00 0. 0000 0. 0000

20 0. 13 138. 18 - 0. 03 95. 51 0. 0010 0. 0004

20 138. 18 - 0. 45 95. 51 0. 0047

Analysis of Load Case 18 : FS+BS+IP+OW



10 53. 80 138. 18 88. 00 0. 3894

20 33. 73 138. 18 95. 51 0. 2441

20 31. 83 138. 18 95. 51 0. 2303

Analysis of Load Case 19 : FS+BS+EP+OW



10 138. 18 - 3. 02 88. 00 0. 0344

20 138. 18 - 1. 50 95. 51 0. 0157

20 138. 18 - 3. 43 95. 51 0. 0359

Absol ut e Maxi mum of t he al l of t he St r ess Rati o' s 0. 3922

Governing Element: Head

Governing Load Case 11 : HP+HW+HI



60/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Center of Gravity Calculation : Step: 18 12:10p Dec 10,2014

Shop/Field Installation Options :

Note : The CG is computed from the first Element From Node

Cent er of Gr avi t y of Li qui d 411. 837 mm

Cent er of Gr avi t y of Nozzl es 1233. 806 mm

Cent er of Gr avi t y of Lugs 1248. 000 mm

Cent er of Gr avi t y of Added Wei ght s ( Oper at i ng) 2138. 000 mm

Center of Gr avi t y of Bare Shel l New and Col d 1819. 337 mm

Cent er of Gr avi t y of Bare Shel l Cor r oded 1819. 337 mm

Vessel CG i n t he Oper at i ng Condi t i on 1459. 695 mm

Vessel CG i n t he Fabr i cat ed ( Shop/ Empt y) Condi t i on 1705. 110 mm

Vessel CG i n t he Test Condi t i on 1812. 662 mm



61/204

PV Elite 2013 Licensee: MSET ENGINEERING SDN BHDFileName : V-6011 ----------------------------------------Sup. Lug Calcs: Ope : Lugs: 2 12:10p Dec 10,2014

Support Lug Calculations: Operating Case

INPUT ECHO OF SUPPORT LUG INPUT

Type of Geomet r y : Gusset s wi t h No Top Pl at e

Number of Support Lugs Nl ug 2

Di st ance f r om Vessel OD t o Lug Cont act Poi nt Dl ug 128. 0000 mm

Lug Support For ce Bear i ng Wi dt h Wf b 204. 0000 mm

Lug Mat er i al SA- 240 316L

Lug Yi el d St r ess 165. 40 MPa

Radi al Wi dth of bot t om Suppor t Lug Pl at e Wpl 254. 0000 mm

Ef f ect i ve Force Bear i ng Length Lpl 200. 0000 mm

Thi ckness of bot t omSupport Lug Pl ate Tpl 20. 0000 mm

Di st ance bet ween Gusset s Dgp 154. 0000 mm

Mean Wi dt h of Gusset Pl at e Wgp 102. 0000 mm

Hei ght of Gusset Pl at e Hgp 306. 0000 mm

Thi ckness of Gusset Pl at e Tgp 14. 0000 mm

Pad Wi dt h al ong Ci r cumf er ence C11P 200. 000 mm

Pad Length al ong Vessel Axi s C22P 380. 000 mm

Pad Thi ckness Tpad 8. 000 mm


Bol t Al l owabl e Str ess at Desi gn Temper at ure 172. 38 MPa

Thread Seri es TEMA Met r i c

Bol t Di amet er 24. 00 mm

Results for Support Lugs: Description: LUG

Overt urni ng Moment at Suppor t Lug 3500. N- m


62/204


Wei ght Load at t he t op of one Lug 17278. N

Force on one Lug, Operating Condition [Flug]:

= ( W/ Nl ug + Ml ug/ ( Rl ug * Nl ug/ 2 ) )

= ( 34555/ 2 + 3500/ ( 433. 00 * 2/ 2 ) )

= 25358. 76 N

Force on one lug in the Empty Condition [Flugemp]:

= ( - Wemp/ Nl ug + Ml ugemp/ ( Rl ug * Nl ug/ 2 ) )

= ( - 7964/ 2 + 3490/ ( 433. 00 * 2/ 2 ) )

= 4076. 54 N

Bottom Support Plate Bending Stress (Point Load) [Spl]:

= ( Fl ugemp/ 2*Dgp/ 2) / ( ( Wpl / 6) *Tpl ) ( Upl i f t Condi t i on)

= ( 4076/ 2*154. 000/ 2) / ( ( 254. 00/ 6) *20. 0000 )

= 9. 27 MPa

Bot t om Pl ate Requi r ed Thi ckness ( Poi nt Load) 5. 7987 mm

Bottom Plate required thickness for Uplift per ADM S 3/4 [trUpl]:

= 0. 72 * sqr t ( Fl ugemp * Dgp / ( ( Wpl - dt ) * Spa ) )

= 0. 72 * sqr t ( 4076. 5 * 154. 00/ ( ( 254. 00 - 27. 18 ) * 110. 267 ) )

= 3. 61 mm

Bearing Area [Ba]:

= Lpl * Wf b

= 200. 000 * 204. 000

= 40800. 00 mm

Bending Stress in bottom Plate (Unif. Load) Per Bednar p.156 [Spl2]:

= Bet a1 * Fl ug/ Ba * Wf b / Tpl per Roar k & Young 5t h Ed.


63/204


= 0. 315 * 25358. 8/ 40800. 000 * 204. 000 / 20. 000

= 20. 35 MPa

Bot t om Pl ate Requi r ed Thi ckness ( Uni f orm Load) 8. 5910 mm

Bottom Plate Required Thickness based on ADM S 3/4 [trAD]:

= 0. 71 * Dgp * ( ( Fl ug / ( Lpl * Wf b ) ) / Spa )

= 0. 71*154. 00*( ( 25358/ ( 200. 00*204. 00) ) / 110. 267)

= 8. 209 mm

Note: If using the AD Code recommendations, the force bearing width (Wfb) must

be greater than or equal to 1/3 of the bottom plate radial width (Wpl)

plus the pad thickness (Padthk), if there is a pad.

Bottom Support Plate Allowable Stress [Spa]:

= 2/ 3 * Yl ug

= 2/ 3 * 165

= 110. 27 MPa

Gusset Plate Axial Stress ( Force / Gusset Plate Area ) [Sgp]:

= ( Fl ug/ 2 ) / ( Wgp * Tgp )

= ( 25358/ 2 ) / ( 102. 000 *14. 0000 )

= 8. 88 MPa

Requi r ed Thi ckness of Gusset s per AI SC 5. 7234 mm

Gusset Plate Allowable Stress [Sga]:

= ( 1- ( Kl r) / ( 2*Cc) ) *Fy / ( 5/ 3+3*( Kl r) / ( 8*Cc)- ( Kl r ) / ( 8*Cc)

= ( 1- ( 87. 43 ) / ( 2 * 151. 74 ) ) * 165/

( 5/ 3+3*( 87. 43 ) / ( 8* 151. 74 )- ( 87. 43 ) / ( 8*151. 74 )

= 74. 21 MPa


64/204


Maximum Compressive Gusset Plate Stress per Bednar [SgpB]:

= Fl ug*( 3*Dl ug- Wpl ) / ( Tgp* Wpl * ( Si n( Al ph_G) ) )

= 25358 *( 3*128. 000 -254. 000 )/ ( 14. 0000 *254. 000 *( Si n(45. 19 )) )

= 7. 25 MPa

Gusset Plate Allowable Compressive Stress [SgaB]:

= 18000/ ( 1+( 1/ 18000) *( Hgp/ Si n(Al ph_G) / ( 0. 289*Tgp) ) )

= 18000/ ( 1+( 1/ 18000) * ( 306. 000/ Si n(45. 19 ) / ( 0. 289*14. 0000 ) ) )

= 76. 08 MPa

Determine the required bolt area due to Uplift [Abr]:

= Fl ugemp / Sabol t

= 4076. 543/ 172. 375

= 23. 65 mm

The Area available in a single bolt : 312.748 mm [OK]

Input Echo, WRC107/537 Item 1, Description: LUG

Di ameter Basi s f or Vessel Vbasi s I D

Cyl i ndr i cal or Spher i cal Vessel Cyl sph Cyl i ndr i cal

I nternal Cor r osi on Al l owance Cas 0. 0000 mm

Vessel Di amet er Dv 594. 000 mm

Vessel Thi ckness Tv 8. 000 mm

Desi gn Temperat ure 50. 00 C

At t achment Type Type Rect angul ar

Par amet er C11 C11 92. 40 mm

Par amet er C22 C22 244. 80 mm


65/204


Thi ckness of Rei nf or ci ng Pad Tpad 8. 000 mm

Pad Par amet er C11P C11p 200. 000 mm

Pad Par amet er C22P C22p 380. 000 mm

Desi gn I nt ernal Pressur e Dp 18. 000 bar

I ncl ude Pressur e Thr ust No

Vessel Cent erl i ne Di r ect i on Cosi ne Vx 0. 000

Vessel Cent erl i ne Di r ect i on Cosi ne Vy 1. 000

Vessel Cent erl i ne Di r ect i on Cosi ne Vz 0. 000

Nozzl e Cent erl i ne Di r ect i on Cosi ne Nx 1. 000

Nozzl e Cent erl i ne Di r ect i on Cosi ne Ny 0. 000

Nozzl e Cent erl i ne Di r ect i on Cosi ne Nz 0. 000

Gl obal Force ( SUS) Fx 0. 0 N

Gl obal Force ( SUS) Fy 17277. 8 N

Gl obal For ce ( SUS) Fz 0. 0 N

Gl obal Moment ( SUS) Mx 0. 0 N- m

Gl obal Moment ( SUS) My 0. 0 N- m

Gl obal Moment ( SUS) Mz 2212. 5 N- m

I nt er nal Pressur e ( SUS) P 18. 00 bar

I ncl ude Pressur e Thr ust No

Gl obal Force ( OCC) Fx 4072. 4 N

Gl obal Force ( OCC) Fy 8080. 9 N

Gl obal Force ( OCC) Fz 0. 0 N

Gl obal Moment ( OCC) Mx 0. 0 N- m

Gl obal Moment ( OCC) My 521. 5 N- m


66/204


Gl obal Moment ( OCC) Mz 1034. 8 N- m

Occasi onal I nt ernal Pressur e ( OCC) Pvar 0. 00 bar

Use I nt eract i ve Cont r ol No

WRC107 Ver si on Ver si on Mar ch 1979

I ncl ude Pressur e St r ess I ndi ces per Di v. 2 No

Comput e Pr essure St r ess per WRC- 368 No

WRC 107 Stress Calculation for SUStained loads:

Radi al Load P 0. 0 N

Ci r cumf erent i al Shear VC 0. 0 N

Longi t udi nal Shear VL 17277. 8 N

Ci r cumf erent i al Moment MC 0. 0 N- m

Longi t udi nal Moment ML - 2212. 5 N- m

Torsi onal Moment MT 0. 0 N- m

Di mensi onl ess Par amet er s used : Gamma = 19. 06

Dimensionless Loads for Cylindrical Shells at Attachment Junction:

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

Curves r ead f or 1979 Beta Fi gure Val ue Locat i on

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

N( PHI ) / ( P/ Rm ) 0. 345 4C 2. 411 ( A, B)

N( PHI ) / ( P/ Rm ) 0. 345 3C 1. 447 ( C, D)

M( PHI ) / ( P ) 0. 222 2C1 0. 050 ( A, B)

M( PHI ) / ( P ) 0. 222 1C 0. 080 ( C, D)

N( PHI ) / ( MC/ ( Rm**2 * Beta) ) 0. 210 3A 0. 749 ( A, B, C, D)

M( PHI ) / ( MC/ ( Rm * Beta) ) 0. 250 1A 0. 084 ( A, B, C, D)


67/204


N( PHI ) / ( ML/ ( Rm**2 * Beta) ) 0. 290 3B 1. 929 ( A, B, C, D)

M( PHI ) / ( ML/ ( Rm * Beta) ) 0. 268 1B 0. 027 ( A, B, C, D)

N( x) / ( P/ Rm ) 0. 287 3C 1. 736 ( A, B)

N( x) / ( P/ Rm ) 0. 287 4C 2. 636 ( C, D)

M( x) / ( P ) 0. 298 1C1 0. 058 ( A, B)

M( x) / ( P ) 0. 298 2C ! 0. 034 ( C, D)

N( x) / ( MC/ ( Rm**2 * Beta) ) 0. 210 4A 1. 214 ( A, B, C, D)

M( x) / ( MC/ ( Rm * Beta) ) 0. 331 2A 0. 035 ( A, B, C, D)

N( x) / ( ML/ ( Rm**2 * Beta) ) 0. 290 4B 0. 789 ( A, B, C, D)

M( x) / ( ML/ ( Rm * Beta) ) 0. 335 2B 0. 035 ( A, B, C, D)

Note - The ! mark next to the figure name denotes curve value exceeded.

St r ess Concent r at i on Factors Kn = 1. 00, Kb = 1. 00

Stresses in the Vessel at the Attachment Junction

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

| St r ess Val ues at

Type of | ( MPa )

- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

St r ess Load| Au Al Bu Bl Cu Cl Du Dl

- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

Ci r c. Memb. P | 0 0 0 0 0 0 0 0

Ci r c. Bend. P | 0 0 0 0 0 0 0 0

Ci r c. Memb. MC | 0 0 0 0 0 0 0 0

Ci r c. Bend. MC | 0 0 0 0 0 0 0 0

Ci r c. Memb. ML | 7 7 - 7 - 7 0 0 0 0

Ci r c. Bend. ML | 17 - 17 - 17 17 0 0 0 0


68/204


|

Tot . Ci r c. St r . | 25. 3 - 9. 4 - 25. 3 9. 4 0. 0 0. 0 0. 0 0. 0

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

Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 5 5 - 5 - 5 0 0 0 0

Long. Bend. ML | 17 - 17 - 17 17 0 0 0 0

|

Tot . Long. St r . | 22. 9 - 12. 7 - 22. 9 12. 7 0. 0 0. 0 0. 0 0. 0

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 - 2 - 2 2 2

Shear MT | 0 0 0 0 0 0 0 0

|

Tot . Shear | 0. 0 0. 0 0. 0 0. 0 - 2. 2 - 2. 2 2. 2 2. 2

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

St r . I nt . | 25. 34 12. 72 25. 34 12. 72 4. 41 4. 41 4. 41 4. 41

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


Dimensionless Loads for Cylindrical Shells at Pad edge:

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

Curves r ead f or 1979 Beta Fi gure Val ue Locat i on

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

N( PHI ) / ( P/ Rm ) 0. 597 4C ! 2. 658 ( A, B)

N( PHI ) / ( P/ Rm ) 0. 597 3C ! 0. 987 ( C, D)

M( PHI ) / ( P ) 0. 423 2C1 0. 009 ( A, B)

M( PHI ) / ( P ) 0. 423 1C ! 0. 062 ( C, D)

N( PHI ) / ( MC/ ( Rm**2 * Beta) ) 0. 411 3A 1. 056 ( A, B, C, D)


69/204


M( PHI ) / ( MC/ ( Rm * Beta) ) 0. 447 1A 0. 062 ( A, B, C, D)

N( PHI ) / ( ML/ ( Rm**2 * Beta) ) 0. 510 3B ! 1. 383 ( A, B, C, D)

M( PHI ) / ( ML/ ( Rm * Beta) ) 0. 478 1B 0. 006 ( A, B, C, D)

N( x) / ( P/ Rm ) 0. 516 3C ! 0. 987 ( A, B)

N( x) / ( P/ Rm ) 0. 516 4C ! 2. 658 ( C, D)

M( x) / ( P ) 0. 530 1C1 ! 0. 014 ( A, B)

M( x) / ( P ) 0. 530 2C ! 0. 032 ( C, D)

N( x) / ( MC/ ( Rm**2 * Beta) ) 0. 411 4A 3. 650 ( A, B, C, D)

M( x) / ( MC/ ( Rm * Beta) ) 0. 544 2A ! 0. 024 ( A, B, C, D)

N( x) / ( ML/ ( Rm**2 * Beta) ) 0. 510 4B ! 0. 860 ( A, B, C, D)

M( x) / ( ML/ ( Rm * Beta) ) 0. 562 2B ! 0. 009 ( A, B, C, D)

Note - The ! mark next to the figure name denotes curve value exceeded.

St r ess Concent r at i on Factors Kn = 1. 00, Kb = 1. 00

Stresses in the Vessel at the Edge of Reinforcing Pad

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


Type of | ( MPa )

- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -


- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

Ci r c. Memb. P | 0 0 0 0 0 0 0 0

Ci r c. Bend. P | 0 0 0 0 0 0 0 0

Ci r c. Memb. MC | 0 0 0 0 0 0 0 0

Ci r c. Bend. MC | 0 0 0 0 0 0 0 0

Ci r c. Memb. ML | 7 7 - 7 - 7 0 0 0 0


70/204


Ci r c. Bend. ML | 8 - 8 - 8 8 0 0 0 0

|

Tot . Ci r c. St r . | 15. 2 - 0. 9 - 15. 2 0. 9 0. 0 0. 0 0. 0 0. 0

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

Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 6 6 - 6 - 6 0 0 0 0

Long. Bend. ML | 11 - 11 - 11 11 0 0 0 0

|

Tot . Long. St r . | 17. 4 - 4. 7 - 17. 4 4. 7 0. 0 0. 0 0. 0 0. 0

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 - 2 - 2 2 2

Shear MT | 0 0 0 0 0 0 0 0

|

Tot . Shear | 0. 0 0. 0 0. 0 0. 0 - 2. 8 - 2. 8 2. 8 2. 8

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

St r . I nt . | 17. 37 4. 73 17. 37 4. 73 5. 68 5. 68 5. 68 5. 68

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

WRC 107 Stress Calculation for OCCasional loads:

Radi al Load P 4072. 4 N

Ci r cumf erent i al Shear VC 0. 0 N

Longi t udi nal Shear VL 8080. 9 N

Ci r cumf erent i al Moment MC - 521. 5 N- m

Longi t udi nal Moment ML - 1034. 8 N- m

Torsi onal Moment MT 0. 0 N- m



71/204


Str ess Concent r at i on Factors Kn = 1. 00, Kb = 1. 00

Stresses in the Vessel at the Attachment Junction

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


Type of | ( MPa )

- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -


- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

Ci r c. Memb. P | - 2 - 2 - 2 - 2 - 1 - 1 - 1 - 1

Ci r c. Bend. P | - 4 4 - 4 4 - 7 7 - 7 7

Ci r c. Memb. MC | 0 0 0 0 0 0 0 0

Ci r c. Bend. MC | 0 0 0 0 13 - 13 - 13 13

Ci r c. Memb. ML | 3 3 - 3 - 3 0 0 0 0

Ci r c. Bend. ML | 8 - 8 - 8 8 0 0 0 0

|

Tot . Ci r c. St r . | 5. 0 - 1. 6 - 18. 7 7. 2 5. 2 - 6. 4 - 22. 8 19. 2

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

Long. Memb. P | - 1 - 1 - 1 - 1 - 2 - 2 - 2 - 2

Long. Bend. P | - 5 5 - 5 5 - 3 3 - 3 3

Long. Memb. MC | 0 0 0 0 1 1 - 1 - 1

Long. Bend. MC | 0 0 0 0 4 - 4 - 4 4

Long. Memb. ML | 2 2 - 2 - 2 0 0 0 0

Long. Bend. ML | 8 - 8 - 8 8 0 0 0 0

|

Tot . Long. St r . | 3. 7 - 1. 8 - 17. 7 10. 1 0. 1 - 2. 0 - 11. 0 4. 1

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

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 - 1 - 1 1 1

Shear MT | 0 0 0 0 0 0 0 0

|


72/204


Tot . Shear | 0. 0 0. 0 0. 0 0. 0 - 1. 0 - 1. 0 1. 0 1. 0

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

St r . I nt . | 5. 04 1. 82 18. 66 10. 08 5. 48 6. 64 22. 87 19. 27

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


Str ess Concent r at i on Factors Kn = 1. 00, Kb = 1. 00

Stresses in the Vessel at the Edge of Reinforcing Pad

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


Type of | ( MPa )

- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -


- - - - - - - - - - - - - - - | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

Ci r c. Memb. P | - 4 - 4 - 4 - 4 - 1 - 1 - 1 - 1

Ci r c. Bend. P | - 3 3 - 3 3 - 23 23 - 23 23

Ci r c. Memb. MC | 0 0 0 0 1 1 - 1 - 1

Ci r c. Bend. MC | 0 0 0 0 22 - 22 - 22 22

Ci r c. Memb. ML | 3 3 - 3 - 3 0 0 0 0

Ci r c. Bend. ML | 3 - 3 - 3 3 0 0 0 0

|

Tot . Ci r c. St r . | - 0. 7 - 1. 6 - 14. 9 - 0. 8 - 1. 7 0. 6 - 48. 9 43. 3

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

Long. Memb. P | - 1 - 1 - 1 - 1 - 4 - 4 - 4 - 4

Long. Bend. P | - 5 5 - 5 5 - 12 12 - 12 12

Long. Memb. MC | 0 0 0 0 4 4 - 4 - 4

Long. Bend. MC | 0 0 0 0 7 - 7 - 7 7

Long. Memb. ML | 2 2 -

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