memoria de calculo tanque hidroneumatico

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INSTITUTO MEXICANO DEL PETRÓLEO

MEMÓRIA DE CÁLCULOINTERCONEXIÓN DE LOS PAQUETES DE PERFORACIÓN

NUEVOS CON LOS PAQUETES EXISTENTES DE LOS EQUIPOSDE PERFORACIÓN.

AV-PP-AGR-01H-MC-01

PROY. No. F.31171

ELABORO: DLA FECHA: JULIO 2012 REV. 0 HOJA 1 DE 92

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AV-PP-AGR-01H-MC-01

PROY. No. F.31171

ELABORO: DLA FECHA: JULIO 2012 REV. 0 HOJA 2 DE 92

MEMORIA DE CÁLCULO

TANQUE HIDRONEUMÁTICOCLAVE FA-1100

AV-PP-AGR-01-H-MC-01

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REV FECHA REVISIÓN

INSTITUTO MEXICANO DEL PETRÓLEO SUPERVISIÓN PEMEX

ELABOROInicial!

REVI"OInicial!

APROBOInicial!

APROBO FECHA

0 JULIO 2012PARA

CON"#RUCCIONDLA R"$ O$H






AV-PP-AGR-01H-MC-01

PROY. No. F.31171

ELABORO: DLA FECHA: JULIO 2012 REV. 0 HOJA ! DE 92

Table of Contents

Cover Sheet.................................................................................................................................................................................3

Picture.......................................................................................................................................................................................

Internal Pressure Calculations :...........................................................................................................................

External Pressure Calculations :...........................................................................................................................

Element and Detail Weights :......................................................................................................................................

Nozzle Flange MAWP :........................................................................................................................................................

Natural Freuenc! Calculation :...............................................................................................................................

Wind "oad Calculation :..................................................................................................................................................

Earthua#e "oad Calculation :....................................................................................................................................2

Wind$Earthua#e Shear% &ending :...........................................................................................................................

Wind De'lection :...............................................................................................................................................................

"ongitudinal Stress Constants :...............................................................................................................................2

"ongitudinal Allo(a)le Stresses :.........................................................................................................................

"ongitudinal Stresses Due to * * * :...................................................................................................................2

Stress due to Com)ined "oads :................................................................................................................................

Center o' +ravit! Calculation :...............................................................................................................................3

"eg Chec#% ,-.erating Case/ :....................................................................................................................................3

"eg Chec#% ,Filled ($Water/ :....................................................................................................................................4

Nozzle Calcs* : &-0 12 C-NE3I-N...............................................................................................................................5

Nozzle Calcs* : &-0 41 D5EN.......................................................................................................................................

Nozzle Calcs* : &-0 11 A"IM AI5...............................................................................................................................5

Nozzle Calcs* : &-0 16 A"M A+7A...............................................................................................................................6

Nozzle Calcs* : &-0 48 9* P5ES................................................................................................................................

Nozzle Calcs* : &-0 ;A < NI<E"...............................................................................................................................6

Nozzle Calcs* : &-0 ;& < NI<E"...............................................................................................................................7

Nozzle Calcs* : &-0 8A IN9E5....................................................................................................................................7

Nozzle Calcs* : &-0 8& IN9E5....................................................................................................................................7

Nozzle Calcs* : &-0 44 <* SE+*................................................................................................................................

Nozzle Schedule :...............................................................................................................................................................

Nozzle Summar! :...................................................................................................................................................................85

MDM9 Summar! :........................................................................................................................................................................86

<essel Design Summar! :..................................................................................................................................................87

"i'ting "ugs: ……………………………………………………………………………………………………………...

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DESIGN CALCULATION

In Acco%&anc 'i() A"$E "c(ion VIII Di*i!ion 1

A"$E Co& V%!ion: 2010 E&i(ion+ 2011 a A&&n&a

Anal,!i! P%-o%& /,: In!(i((o $icano & P(%lo I$P4 5 "an Ba%(o

Jo/ Fil: D:6DOCU$EN#"6PROYEC#O F.311 #AN8. HIDRONEU$A#I

Da( o- Anal,!i!: Jn 27+ 2012

PV Eli( 2012+ Jana%, 2012



No(: PV Eli( 9%-o%! all calcla(ion! in(%nall, in I9%ial Uni(!(o %ain co9lian( 'i() () A"$E Co& an& an, /il( in a!!9(ion!

in () A"$E Co& -o%la!. #) c!(oa%, I9%ial &a(a/a! i!!& -o% con!i!(nc,. #) -inali& %!l(! a% %-lc(& (o !)o'

() !%! !( o- !lc(& ni(!.



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Internal Pressure alculations: Ste,: 10:./a un 2 2012

Element Thickness, Pressure, Diameter and Allowable Stress :

= = Int* Press = Nominal = 9otal Corr= Element = Allo(a)le = From= 9o = > "i* ?d = 9hic#ness = Allo(ance = Diameter = Stress,SE/= = = #g'$cm@ = mm = mm = mm = #g'$cm@ =

9APA INFE5= 2*B2 = *** = 4*1;B = B8*BB = 16B6*6 = EN<-"<EN9E= 2*B2 = *** = 4*1;B = B8*B = 1B61* = 9APA S7PE5= 2*BBBB = *** = 4*1;B = B8*BB = 16B6*6 =

Element Required Thickness and MAWP :

= = Design = M*A*W*P* = M*A*P* = Minimum = 5euired = From= 9o = Pressure = Corroded = Ne( Cold = 9hic#ness = 9hic#ness = = = #g'$cm@ = #g'$cm@ = #g'$cm@ = mm = mm = 9APA INFE5= 2*BBBBB = 42*BB;1 = ;2*226 = *;6;BB = ;*8;BB = EN<-"<EN9E= 2*BBBBB = 46*68B4 = 2*21; = *;6;BB = ;*8;BB = 9APA S7PE5= 2*BBBBB = 42*B242 = ;2*226 = *;6;BB = ;*8;BB = Minimum 46*68B 2*21

$A;P: 32.2<0 =>-?c@+ lii(& /,: ENVOLVEN#E.

Internal Pressure alculation Results :

ASME ode, Section !III, Di"ision #, $%#%, $%##a

Elli&tical 'ead (rom #% To $% SA)$*+ WP , -S).. r"/ at .0

#APA INFERIOR

Longitudinal Joint: SeamlessCircumferential Joint: Spot Radiography per UW-11(a,,!" #ype 1

$aterial U%S %um!er: &''')

Re*uired #hic+ness due to nternal ressure .tr/: ,PGDoGHcor/$,6GSGE>6GPG,HcorB*1// .er A..endix 1 ,c/ ,2*BGB8*BBBBGB*/$,6G16B6*6;G1*BB>6G2*BG,B*2B*1// 1*468 > 4*1;B *;B68 mm

Note: The thickness required was less than the Code Minimum, therefore the Code Minimum value of 2.5000 mm per !"#$ will %e used.

$a0 2llo3a!le Wor+ing ressure at gi4en #hic+ness, corroded .$2W/:Less 5perating 6ydrostatic 6ead ressure of ''78 +gf9cm ,6GSGEGt/$,HcorGDo6GtG,HcorB*1// .er A..endix 1 ,c/ ,6G16B6*6;G1*BBG8*4;BB/$,B*GB8*BBBB6G8*4;BBG,B*2B*1// 4*;6; B*B 4*8 #g'$cm@

$a0imum 2llo3a!le ressure, %e3 and Cold .$2%C/: ,6GSGEGt/$,HGDo6GtG,HB*1// .er A..endix 1 ,c/ ,6G16B6*6;G1*BBG*;6;B/$,1*BBBGB8*BBBB6G*;6;BG,1*BBBB*1// ;2*22 #g'$cm@

2ctual stress at gi4en pressure and thic+ness, corroded .Sact/: ,PG,HcorGDo6GtG,HcorB*1///$,6GEGt/ ,2*BG,B*GB8*BBBB6G8*4;BBG,B*B*1///$,6G1*BBG8*4;BB/ 6;*4; #g'$cm@

"(%ai>)( Flan> Ri%& #)ic=n!!: ,PG5o/$,SGE>B*GP/ > c .er A..endix 11 ,a/,1/ ,2*BG6B4*BBBB/$,16B6*6;G1*BB>B*G2*B/>4*1;




*;4; mm

"(%ai>)( Flan> $ai Allo'a/l ;o%=in> P%!!%:Less 5perating 6ydrostatic 6ead ressure of ''78 +gf9cm ,SGEGt/$,5oB*Gt/ .er A..endix 11 ,a/,1/ ,16B6*6; G 1*BB G 8*4;BB /$,6B4*BBBB B* G 8*4;BB /

42*B2 B*B 42*BB; #g'$cm@

Fac(o% + co%%o&& con&i(ion co%: , 6 > , Inside Diameter$, 6 G Inside ?ead De.th //6/$8 , 6 > , 44*4BB$, 6 G *16 //6/$8 B*224

MDMT C"#$%#"&'()* ') &+, )%$#, P(/&'()

o*%n. ()=+ (> .G2G + (% G.222 + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.22 + #9. R&c(ion 10 C

Min Metal 9em.* ($o im.act .er 7CS88 6 C Min Metal 9em.* at 5euired thic#ness ,7CS 88*1/ 4 C

MDMT C"#$%#"&'()* ') &+, H," S&/"'+& F#"),o*%n. ()=+ (> .G2G + (% G.02 + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.G1 + #9. R&c(ion C


1lindrical Shell (rom $% To *% SA)#%. , -S).. r"/ at .0

ENVOLVEN#E

Longitudinal Joint: Spot Radiography per UW-11(!" #ype 1Circumferential Joint: Spot Radiography per UW-11(a,,!" #ype 1


Re*uired #hic+ness due to nternal ressure .tr/: ,PG5o/ $ ,SGE>B*GP/ .er A..endix 11 ,a/,1/ ,2*BG6B4*6BBB/$,16B6*6;GB*2;>B*G2*B/ 1*8B14 > 4*1;B *84 mm

Note: The thickness required was less than the Code Minimum, therefore the Code Minimum value of 2.5000 mm per !"#$ will %e used.

$a0 2llo3a!le Wor+ing ressure at gi4en #hic+ness, corroded .$2W/:Less 5perating 6ydrostatic 6ead ressure of ''78 +gf9cm ,SGEGt/$,5oB*Gt/ .er A..endix 11 ,a/,1/ ,16B6*6;GB*2;G8*4;BB/$,6B4*6BBBB*G8*4;BB/ 46*44 B*B 46*68B #g'$cm@

$a0imum 2llo3a!le ressure, %e3 and Cold .$2%C/: ,SGEGt/$,5oB*Gt/ .er A..endix 11 ,a/,1/ ,16B6*6;GB*2;G*;6;B/$,6B4*6BBBB*G*;6;B/ 2*21 #g'$cm@

2ctual stress at gi4en pressure and thic+ness, corroded .Sact/: ,PG,5oB*Gt//$,EGt/ ,2*BG,,6B4*6BBBB*G8*4;BB//$,B*2;G8*4;BB/ 4BB*442 #g'$cm@

M')'% D,*') M,&"# T,3,/"&%/, R,*%#&*




o*%n. ()=+ (> .G2G + (% <.3G0 + c 3.17G0 + E 0.G"(%!! Ra(io (% E4?(> 5 c4 0.G0 + #9. R&c(ion C


Elli&tical 'ead (rom *% To +% SA)$*+ WP , -S).. r"/ at .0

#APA "UPERIOR

Longitudinal Joint: SeamlessCircumferential Joint: Spot Radiography per UW-11(a,,!" #ype 1


Re*uired #hic+ness due to nternal ressure .tr/: ,PGDoGHcor/$,6GSGE>6GPG,HcorB*1// .er A..endix 1 ,c/ ,2*BBBGB8*BBBBGB*/$,6G16B6*6;G1*BB>6G2*BBBG,B*2B*1// 1*41 > 4*1;B *2 mm

Note: The thickness required was less than the Code Minimum, therefore

the Code Minimum value of 2.5000 mm per !"#$ will %e used.

$a0 2llo3a!le Wor+ing ressure at gi4en #hic+ness, corroded .$2W/: ,6GSGEGt/$,HcorGDo6GtG,HcorB*1// .er A..endix 1 ,c/ ,6G16B6*6;G1*BBG8*4;BB/$,B*GB8*BBBB6G8*4;BBG,B*2B*1// 4*;6; #g'$cm@

$a0imum 2llo3a!le ressure, %e3 and Cold .$2%C/: ,6GSGEGt/$,HGDo6GtG,HB*1// .er A..endix 1 ,c/ ,6G16B6*6;G1*BBG*;6;B/$,1*BBBGB8*BBBB6G*;6;BG,1*BBBB*1// ;2*22 #g'$cm@

2ctual stress at gi4en pressure and thic+ness, corroded .Sact/: ,PG,HcorGDo6GtG,HcorB*1///$,6GEGt/ ,2*BBBG,B*GB8*BBBB6G8*4;BBG,B*B*1///$,6G1*BBG8*4;BB/

64*41 #g'$cm@

"(%ai>)( Flan> Ri%& #)ic=n!!: ,PG5o/$,SGE>B*GP/ > c .er A..endix 11 ,a/,1/ ,2*BBBG6B4*BBBB/$,16B6*6;G1*BB>B*G2*BBB/>4*1; *;66 mm

"(%ai>)( Flan> $ai Allo'a/l ;o%=in> P%!!%: ,SGEGt/$,5oB*Gt/ .er A..endix 11 ,a/,1/ ,16B6*6; G 1*BB G 8*4;BB /$,6B4*BBBB B* G 8*4;BB / 42*B2 #g'$cm@

Fac(o% + co%%o&& con&i(ion co%: , 6 > , Inside Diameter$, 6 G Inside ?ead De.th //6/$8 , 6 > , 44*4BB$, 6 G *16 //6/$8

B*224

MDMT C"#$%#"&'()* ') &+, )%$#, P(/&'()

o*%n. ()=+ (> .G2G + (% G.210 + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.20 + #9. R&c(ion 10 C


MDMT C"#$%#"&'()* ') &+, H," S&/"'+& F#"),

o*%n. ()=+ (> .G2G + (% G.3 + c 3.17G0 + E 1.00




"(%!! Ra(io (% E4?(> 5 c4 0. + #9. R&c(ion C


No(: Ha&! an& ")ll! E9(& (o 520F 52C4 /, 9a%a>%a9) U520F

'1drostatic Test Pressure Results:

Pressure .er 7+) 1*4 G M*A*W*P* G Sa$S 1*42 #g'$cm@ Pressure .er 7+)4J 1*4 G Design Pres G Sa$S 1B*BB #g'$cm@ Pressure .er 7+c 1*4 G M*A*P* ?ead,?!d/ 84*44 #g'$cm@ Pressure .er 7+1BB 1*1 G M*A*W*P* G Sa$S 4;*28 #g'$cm@ Pressure .er PED 1*4 G MAWP 8*146 #g'$cm@

U5/4+ #!( P%!!% Calcla(ion: 9est Factor G MAWP G Stress 5atio 1*4 G 46*68B G 1*BBB 1*42 #g'$cm@

!ertical Test &er2ormed &er: -3)44b

&lease note that No''le, (hell, )ead, *lan+e, etc M-&s are all considered when determinin+ the hdrotest pressure for those test tpes that are %ased on the M-& of the vessel.

Stresses on Elements due to '1drostatic Test Pressure:

From 9o Stress Allo(a)le 5atio Pressure 9APA INFE5I-5 16* 661* B*;2 6*B EN<-"<EN9E 1;84*4 661* B*B8 6*B; 9APA S7PE5I-5 168*6 661* B*;8 1*8

Eln(! "i(a/l -o% In(%nal P%!!%.

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------External Pressure alculations : Ste,: 3 10:./a un 22012

E5ternal Pressure alculation Results :

ASME ode, Section !III, Di"ision #, $%#%, $%##a

Elli&tical 'ead (rom #% to $% E5t/ hart: S)$ at .0

#APA INFERIOR

Ela!(ic $o&l! -%o C)a%(: C"52 a( <G C : 0.20EK07 =>-?c@

R!l(! -o% $ai Allo'a/l E(%nal P%!!% $AEP4: 9ca -D D$t Factor A & 8*4;B B8*BB 84* B*BB6164 1B8*;4 EMAP &$,HBGD$t/ 1B8*;446$,B*BBB G84*4B / 12*B26 #g'$cm@

R!l(! -o% Ri%& #)ic=n!! #ca4: 9ca -D D$t Factor A & B*6 B8*BB 8*B B*BBB182 1*8 EMAP &$,HBGD$t/ 1*88B$,B*BBB G8*B41 / B*1;2 #g'$cm@

Check the requirements of !"//a1#1 usin+ & #.$3 4 6ternal 7esi+n pressure for this head.


Re*uired #hic+ness due to nternal ressure .tr/: ,PGDoGHcor/$,6GSGE>6GPG,HcorB*1// .er A..endix 1 ,c/ ,B*6GB8*BBBBGB*/$,6G16B6*6;G1*BB>6GB*6G,B*2B*1// B*B2; > 4*1;B 4*664; mm

$a0 2llo3a!le Wor+ing ressure at gi4en #hic+ness, corroded .$2W/: ,,6GSGEGt/$,HcorGDo6GtG,HcorB*1///$1*8 .er A..endix 1 ,c/ ,,6G16B6*6;G1*BBG8*4;BB/$,B*GB8*BBBB6G8*4;BBG,B*2B*1///$1*8 64*882 #g'$cm@

$ai Allo'a/l E(%nal P%!!% $AEP: min, MAEP% MAWP / min, 12*1 % 64*88; / 12*B2 #g'$cm@

Thickness requirements per !"//a1#1 +overn the required thickness of this head.

1lindrical Shell (rom $% to *% E5t/ hart: S)$ at .0

ENVOLVEN#E


R!l(! -o% $ai Allo'a/l E(%nal P%!!% $AEP4:

9ca -D S"EN D$t "$D Factor A & 8*4;B B8*B 1121*2 8*BB 6*B26 B*BBB262 21*1 EMAP ,G&/$,4G,D$t// ,G21*1B /$,4G8*BBBB / 18*88 #g'$cm@

R!l(! -o% Ri%& #)ic=n!! #ca4: 9ca -D S"EN D$t "$D Factor A & B*6 B8*B 1121*2 B*2 6*B26 B*BBBB;4B ;*B4 EMAP ,G&/$,4G,D$t// ,G;*B4; /$,4GB*244 / B*1;2 #g'$cm@

R!l(! -o% $ai "(i--n& Ln>() "ln4: 9ca -D S"EN D$t "$D Factor A & 8*4;B B8*B 88;* 8*BB ;B*BBBB B*BBB61 6*42 EMAP ,G&/$,4G,D$t// ,G6*421 /$,4G8*BBBB / ;*26B #g'$cm@




Elli&tical 'ead (rom *% to +% E5t/ hart: S)$ at .0

#APA "UPERIOR


R!l(! -o% $ai Allo'a/l E(%nal P%!!% $AEP4: 9ca -D D$t Factor A & 8*4;B B8*BB 84* B*BB6164 1B8*;4 EMAP &$,HBGD$t/ 1B8*;446$,B*BBB G84*4B / 12*B26 #g'$cm@

R!l(! -o% Ri%& #)ic=n!! #ca4: 9ca -D D$t Factor A & B*6 B8*BB 8*B B*BBB182 1*8 EMAP &$,HBGD$t/ 1*88B$,B*BBB G8*B41 / B*1;2 #g'$cm@

Check the requirements of !"//a1#1 usin+ & #.$3 4 6ternal 7esi+n pressure for this head.


Re*uired #hic+ness due to nternal ressure .tr/: ,PGDoGHcor/$,6GSGE>6GPG,HcorB*1// .er A..endix 1 ,c/ ,B*6GB8*BBBBGB*/$,6G16B6*6;G1*BB>6GB*6G,B*2B*1// B*B2; > 4*1;B 4*664; mm

$a0 2llo3a!le Wor+ing ressure at gi4en #hic+ness, corroded .$2W/: ,,6GSGEGt/$,HcorGDo6GtG,HcorB*1///$1*8 .er A..endix 1 ,c/ ,,6G16B6*6;G1*BBG8*4;BB/$,B*GB8*BBBB6G8*4;BBG,B*2B*1///$1*8 64*882 #g'$cm@

$ai Allo'a/l E(%nal P%!!% $AEP: min, MAEP% MAWP / min, 12*1 % 64*88; / 12*B2 #g'$cm@

Thickness requirements per !"//a1#1 +overn the required thickness of this head.

E5ternal Pressure alculations

= = Section = -utside = Corroded = Factor = Factor = From= 9o = "ength = Diameter = 9hic#ness = A = & = = = cm = mm = mm = = #g'$cm@ = 1B= 6B= No Calc = B8*BBB = 8*4;BBB = B*BB6164 = 1B8*;4 = 6B= 4B= 112*12 = B8*BB = 8*4;BBB = B*BBB2624 = 21*1B = 4B= B= No Calc = B8*BBB = 8*4;BBB = B*BB6164 = 1B8*;4 =


= = External = External = External = External = From= 9o = Actual 9* = 5euired 9*=Des* Press* = M*A*W*P* = = = mm = mm = #g'$cm@ = #g'$cm@ = 1B= 6B= *;6;BB = ;*8;BB = B*1; = 12*B26 = 6B= 4B= *;6;BB = *188;4 = B*1; = 18*88 = 4B= B= *;6;BB = ;*8;BB = B*1; = 12*B26 = Minimum 18*8


= = Actual "en*= Allo(* "en*= 5ing Inertia = 5ing Inertia =




From= 9o = &et* Sti''*= &et* Sti''*= 5euired = Availa)le = = = cm = cm = cmGG = cmGG = 1B= 6B= No Calc = No Calc = No Calc = No Calc = 6B= 4B= 112*12 = 88*; = No Calc = No Calc = 4B= B= No Calc = No Calc = No Calc = No Calc =

Eln(! "i(a/l -o% E(%nal P%!!%.

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Eleent and &etail 4ei56ts : Ste,: . 10:./a un 22012

Element and Detail Wei6hts

= = Element = Element = Corroded = Corroded = Extra due = From= 9o = Metal Wgt* = ID <olume =Metal Wgt* = ID <olume = Misc K = = = #gm = cmL = #gm = cmL = #gm =

1B= 6B= 6B*2;6 = 18;;*B = 14*4B6 = 1661*1 = 2*4;21B = 6B= 4B= 22*24 = 114B* = ;*BB = 11;BB* = 4;*;48B = 4B= B= 6B*28 = 18;61*; = 14*1 = 118*2 = 2*4;B = 9otal 14B 182B8*28 2 1;11*; ;6

Wei6ht o2 Details

= = Weight o' = 3 -''set% = -''set% = From=9!.e= Detail = Dtl* Cent* =Dtl* Cent* = Descri.tion = = #gm = cm = cm = 1B="id= 18*;48 = *** = *** = A+7A 1B=Nozl= 8*618;B = 11*222 = *;68 = &-0 12 C-NE3I-N

1B=Nozl= ;*6 = 11*222 = *;68 = &-0 41 D5EN 1B="egs= 6*1B2 = *** = 14*842 = "E+S 6B="id= 6*8; = *** = 4*4BB = A+7A 6B=Nozl= B* = 61*;BB = 22*BBB = &-0 11 A"IM AI5 6B=Nozl= 8*6B2B = 66*424 = *86BBB = &-0 16 A"M A+7A 6B=Nozl= B* = 61*;BB = 22*BBB = &-0 48 9* P5ES 6B=Nozl= ;*66B = 6B*8; = 21*22B = &-0 ;A < NI<E" 6B=Nozl= ;*66B = 6B*8; = *86BBB = &-0 ;& < NI<E" 6B=Nozl= ;*66B = 6B*8; = 21*22B = &-0 8A IN9E5 6B=Nozl= ;*66B = 6B*8; = *86BBB = &-0 8& IN9E5 4B=Nozl= B* = B*1;2; = B*844 = &-0 44 <* SE+*

Total Wei6ht o2 Each Detail T1&e

9otal Weight o' "iuid 1B*4

9otal Weight o' Nozzles B*6 9otal Weight o' "egs 6* Sum o' the Detail Weights 11*2 #gm

5,'+& S%"&'()

Fa)ricated Sho. 9est Shi..ing Erected Em.t! -.erating 126* 68;* 126* 68;* 126* 68;* *** 18* *** *** *** 1B*4 B*6 *** B*6 *** *** *** 6* *** 6* *** *** *** *** *** *** *** *** ***

*** *** *** *** *** *** *** *** *** *** B*6 *** *** *** *** *** 6* *** 68;* 16*6 68;* 68;* 68;* 4* #gm

Miscellaneous Wei6ht Percent: +%/% 7

Note that the a%ove value for the miscellaneous wei+ht percent has%een applied to the shells8heads8flan+e8tu%esheets8tu%es etc. in thewei+ht calculations for metallic components.




Note: The shippin+ total has %een modified %ecause some items have %een specified as %ein+ installed in the shop.

5,'+& S%"/8

Fa)ricated Wt* &are Weight W$- 5emova)le Internals 68;* #gm

Sho. 9est Wt* Fa)ricated Weight > Water , Full / 16*6 #gm Shi..ing Wt* Fa)* Wt > 5em* Intls*> Shi..ing A..* 68;* #gm Erected Wt* Fa)* Wt > 5em* Intls*> Insul* ,etc/ 68;* #gm -.e* Wt* no "i Fa)* Wt > Intls* > Details > Wghts* 68;* #gm -.erating Wt* Em.t! Wt > -.erating "i* 7ncorroded 4* #gm Field 9est Wt* Em.t! Weight > Water ,Full/ 4;*B #gm Mass o' the 7..er 1$4 o' the <ertical <essel 26*; #gm

%ote: #he ;ield #est 3eight as computed in the corroded condition

8utside Sur2ace Areas o2 Elements

= = Sur'ace = From= 9o = Area = = = cm@ =

1B= 6B= 6;2*6 = 6B= 4B= 16464*1 = 4B= B= 6;8*1 = 9otal 1242*B16 cm@

Element and Detail Wei6hts

= 9o = 9otal Ele*= 9otal* Ele*=9otal* Ele*= 9otal Dtl*= -.er* Wgt* = From= 9o = Em.t! Wgt*= -.er* Wgt*=?!dro* Wgt*= -''set Mom*= No "iuid = = = #gm = #gm = #gm = #g'm* = #gm = 1B="egs= 12*68 = 684*646 = 661*;8 = 8*418 = 12*68 = "egs= 6B= 18*;BB = 6B;*6; = 14*41 = *816 = 18*;BB =

6B= 4B= 1;6*;8; = 6;*416 = 66*61 = ;*8141 = 1;6*;8; = 4B= B= 6*86 = 6*86 = 4*112 = B*BBBB81B = 6*86 =

umulati"e !essel Wei6ht

= = Cumulative -.e = Cumulative = Cumulative = From= 9o = Wgt* No "iuid = -.er* Wgt* = ?!dro* Wgt* = = = #gm = #gm = #gm = 1B="egs= *** = *** = *** = "egs= 6B= 4;*424 = 8*B;8 = 4*B66; = 6B= 4B= 126*642 = 6*2 = 688*448 = 4B= B= 6*86 = 6*86 = 4*112 =

No(: #) cla(i* o9%a(in> 'i>)(! no lii& in () coln a/o*

a% () cla(i* o9%a(in> 'i>)(! in! () o9%a(in> lii& 'i>)( in! an, 'i>)(! a/!n( in () 9(, con&i(ion.

umulati"e !essel Moment

= = Cumulative = Cumulative =Cumulative = From= 9o = Em.t! Mom* = -.er* Mom* =?!dro* Mom*= = = #g'm* = #g'm* = #g'm* = 1B="egs= 8*418 = 8*418 = 8*418 = "egs= 6B= 1*BBB = 1*BBB = 1*BBB = 6B= 4B= ;*86B1 = ;*86B1 = ;*86B1 = 4B= B= B*BBBB81B = B*BBBB81B =B*BBBB81B =




PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------

No77le Flan5e M!4P : Ste,: / 10:./a un 22012

9ole (lan6e MAWP Results :

Nozzle Flange 5ating Descri.tion -.erating Am)ient 9em.erature Class +rade=+rou. #g'$cm@ #g'$cm@ C

&-0 12 C-NE3I-N ;B*B ;6*1 8; 4BB +5 1*1 &-0 41 D5EN ;B*B ;6*1 8; 4BB +5 1*1 &-0 16 A"M A+7A ;B*B ;6*1 8; 4BB +5 1*1 &-0 ;A < NI<E" ;B*B ;6*1 8; 4BB +5 1*1 &-0 ;& < NI<E" ;B*B ;6*1 8; 4BB +5 1*1 &-0 8A IN9E5 ;B*B ;6*1 8; 4BB +5 1*1 &-0 8& IN9E5 ;B*B ;6*1 8; 4BB +5 1*1 Minimum 5ating ;B*B ;6*1 #g'$cm@

No(: AN"I Ra(in>! a% 9% AN"I?A"$E B1<.G 200 $(%ic E&i(ion

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




Natural Fre8uenc9 alculation : Ste,: 10:./a un 22012

#) Na(%al F%nci! -o% () *!!l )a* /n co9(& i(%a(i*l,/, !ol*in> a !,!( o- a(%ic!. #)! a(%ic! &!c%i/ () a!!an& () !(i--n!! o- () *!!l. #)i! i! () >n%ali& i>n*al?i>n*c(o% 9%o/l an& i! %-%nc& in !o a()a(ical ((!.

#he %atural ;re*uency for the <essel (=mpty" is >)7)8 6?

#he %atural ;re*uency for the <essel (5pe" is >1)11 6?

#he %atural ;re*uency for the <essel (;illed" is >>787 6?

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




4ind Load alculation : Ste,: 10:./a un 22012

Me5ican Wind ode: Manual de Diseno de 8bras i"iles de /(/E/:

lease %ote: #he follo3ing e*uations employ the follo3ing units--------------- Lengths (m", @arometric ressure (mm 6g" ;orce (+g"

In&ut Data:

Wind Design Code Mexico 6BB2 Percent Wind 'or ?!drotest 44*B Design Wind S.eed ,#m$hr/ 6B*B Site Elevation a)ove Sea "evel ,m/ 1*1 &ase Elevation ,m/ B*81BBBBB1 Structure Class A 9errain Categor! 9o.ogra.h! Factor 1*1 Dam.ing Factor ,eta/ 6*eBB6 Strouhal Num)er B*6 &arometric ?eight ,mm$Mercur!/ 8B*B Am)ient 9em.erature ,deg C/ 4B*B Drag Coe''icient 1*

om&uted !alues:

<essel <i)ration Freuenc! no 61*81; ?z Correction Factor Hre B*BB Note: 'or d!namic anal!sis ,see )elo(/ Fc 1*BBB

"(a(ic Anal,!i! 9%-o%&:

No(: ;in& 9%!!%! a% (a=n a( !c(ion cn(%oi& -%o %a&.

S"3#, C"#$%#"&'() 4(/ &+, F'/*& :;(&&(< E#,,)&

#a/l 9a%a(%! /a!& on () #%%ain Ca(>o%,:

Parameter 'rom 9a)le *6*4 delta B*1B Parameter 'rom 9a)le *6*4 al.ha ;;*BBB Parameter 'rom 9a)le *6*4 c B*21;

P%!!% Fac(o% /a!& on &i!(anc -%o %a& !i( l*l4 F%: c B*21;

Note: 'or zO 1B m% Frz c 'or 1B O z O delta% Frz c, z $ 1B /al.ha

'or z Delta% Frz c,delta$1B/al.ha

Co%%c(& ;in& "9& VD: <r G Ft G al.ha 6B*BBB G 1*1BB G B*21;

61;*18B m$s

Ba%o(%ic P%!!% Co%%c(ion Fac(o% : B*46 G -mega $ ,64 > 9/ B*46 G 8B*BBB$,64 > 4B*BBB / B*24

Ba!ic ;in& P%!!% -o% ()i! ln( : B*BB2 G + G <D6

B*BB2 G B*24 G 61;*18B6

612*2; #g$m6

A&!(& ;in& P%!!% -o% ()i! ln( 9:





Ca G z 1*BB G 612*2; 4B;*2 #g$m6

D,naic A9li-ica(ion Fac(o% Fa&: , 1 > 6 G H. G Ivzs G srt, &@ > 5@ //$, 1 > G Ivzs /

,1>6G*46GB*4Gsrt,B*2>B*6;8//$,1>GB*4/ 1*66;

;in& -o%c on () -i%!( ln(: . G Aex. G Fad 4B;*2 G B*B2 G 1*66; 6*14 #g

<essel ?eight 'rom Element Sea level +rade Fal.ha Frz 9APA INFE5 1*2 B*82 B*21; B*21; EN<-"<EN9E 6B*68 1*18 B*21; B*21; 9APA S7PE5 6B*2 1*82 B*21; B*21;

<essel ?eight 'rom Element Sea lvl +rade <d z Pz 'orce 9APA INFE5 1*; B*8; 61;*18 612*2 4B;*22 18* EN<-"<EN9E 6B*6 1*1 61;*18 612*2 4B;*22 1BB*2 9APA S7PE5 6B* 1*8 61;*18 612*2 4B;*22 18*8

Wind !ibration alculations

#)i! *ala(ion i! /a!& on 'o%= /, an(i $a)aan an& E& Mo%illa

N(,)$#"&%/, C' Correction 'actor 'or natural 'reuenc! D Average internal diameter o' vessel cm D' Dam.ing Factor O B*; 7nsta)le% B*; Sta)le Dr Average internal diameter o' to. hal' o' vessel cm ' Natural 'reuenc! o' vi)ration ,?ertz/ '1 Natural 'reuenc! o' )are vessel )ased on a unit value o' ,D$"@/,1B/ " 9otal height o' structure cm "c 9otal length o' conical section,s/ o' vessel cm t) 7ncorroded .late thic#ness at )ottom o' vessel mm <4B Design Wind S.eed .rovided )! user #m$hr <c Critical (ind velocit! #m$hr <( Maximum (ind s.eed at to. o' structure #m$hr W 9otal corroded (eight o' structure #g'

Ws Cor* vessel (eight excl* (eight o' .arts (hich do not e''ect sti''* #g' Maximum am.litude o' vi)ration at to. o' vessel mm Dl "ogarithmic decrement , ta#en as B*B4 'or Welded Structures / <. <i)* Chance% O B*46BEB4 ,?igh/Q B*46BEB4 O B*BBEB4 ,Pro)a)le/ P4B (ind .ressure 4B 'eet a)ove the )ase

C)c= o()% Con&i(ion! an& Ba!ic A!!9(ion!: R1 9otal Cone "ength $ 9otal "ength O B*; B*BBB$111*B B*BBB

R6 , D $ "@ / G 1B O 2*B ,English 7nits/ , 1*44$4*8@ / G 1B 1*;2 +eometr! <iolationJ





Co9( () *i/%a(ion 9o!!i/ili(,. I- V9 0.00E503 no c)anc. V9: W $ , " G Dr@/ 41$, 111* G 4*48;@ / B*121;EB6

"inc V9 i! 0.00E503 no -%()% *i/%a(ion anal,!i! i! %i%&

#) Na(%al F%nc, -o% () V!!l O9...4 i! 21.<1G1 H.

Wind ;oad alculation

= = Wind = Wind = Wind = Wind = Element = From= 9o = ?eight = Diameter = Area = Pressure = Wind "oad = = = cm = cm = cm@ = #g'$m@ = #g' = 1B= 6B= 62*82BB = 2*6BB = *2;8 = 4B;*222 = 18*8; = 6B= 4B= 2*18; = 2*82B = B*B = 4B;*222 = 1BB*2; = 4B= B= 1B*;;8 = 2*6BB = 8*221 = 4B;*222 = 18*84B =

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Eart68ua;e Load alculation : Ste,: < 10:./a un 22012

Seismic alculations &er Manual de Diseno &or Sismo $%%<

U*,/ I)3%& V"#%,* Maximum Acceleration o' 9errain ao B*BB Design Coe''icient c B*4;B

Control Period 9a B*1BB sec Control Period 9) B*8BB sec S.ectrum Parameter # 6*BBB S.ectrum Parameter r 1*BBB Dam.ing Factor & 1*68B &ehavior Factor 0 4*BBB -verresistance Factor 5 1*6;B

Calcla(& Con(%ol P%io& #c: 9c 6 sec since 9) O 6

Co9( () Dc(ili(, Fac(o% 8: 1 > ,0 1/ G srt, ,& $ #/ /G ,9e $ 9)/ i' 9e O 9) 1 > ,4*BBB 1/ G srt, ,1*68B$6*BBB / / G ,B*B8$B*8BB / 1*166

D(%in () "9c(%al Accl%a(ion O%&ina( aB4: ao > , & G c ao / G ,9e $ 9a/% since 9e O 9a B*BB > , 1*68B G B*4;B B*BB / G ,B*B8$B*1BB / B*1

S"3#, C"#$%#"&'() 4(/ &+, 4'/*& E#,,)&

Co9( () "a(ion o- () Ea%()a= ;i>)( (i! Hi>)( ;nHn: 11* #g'm*

D(%in () ;i>)( Hi>)( Fac(o% ;)-: B*2; G Wn G ?n $ Wn?n B*2; G 684*64 G 6*42$11*42 B*;61

D(%in () "i!ic Ba! ")a% V: Sum,Earthua#e Weights/ G a,&/ $ , 0 G 5 / 446*6 G B*6$, 1*166 G 1*6;B / *662 #g'

D(%in () La(%al ")a% on () -i%!( Eln( P1: Wh' G < B*;66 G *64B ;1*12 #g'

D(%in () A&&i(ional ")a% Fo%c a( () (o9 o- () V!!l P!: B*1; G Sum, Earthua#e Weights / G a,&/ $ , 0 G 5 / B*1; G 446*66 G B*1$, 1*166 G 1*6;B / 1*22; #g'

#) Na(%al F%nc, -o% () V!!l O9...4 i! 21.<1G1 H.

Earthquake ;oad alculation

= = Earthua#e = Earthua#e = Element = Element = From= 9o = ?eight = Weight = -.e "oad = Em. "oad = = = cm = #g' = #g' = #g' = 1B="egs= 6*4216 = 684*646 = ;1*12 = 48*;1; = "egs= 6B= *22B8B = 6B;*6; = 1*86B; = 1B*4B28 = 6B= 4B= ;;*22BB = 6;*416 = 2*;B6B = 8B*12 = 4B= B= 1B*B = 6*86 = 64*B1 = 66*2B; =



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Eart68ua;e Load alculation : Ste,: < 10:./a un 22012

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




4ind=Eart68ua;e S6ear Bendin5 : Ste,: 10 10:./a un 22012

#he follo3ing ta!le is for the 5perating Case

Wind=Earthquake Shear, endin6

= = Distance to= Cumulative =Earthua#e = Wind = Earthua#e =

From= 9o = Su..ort= Wind Shear = Shear = &ending = &ending = = = cm = #g' = #g' = #g'm* = #g'm* = 1B="egs= 6;*16B8 = *** = *** = *** = *** = "egs= 6B= 14*8B8 = ;*;66 = 1;1*B66 = 6*42 = 6*;64 = 6B= 4B= 6B*222 = 11*1 = 148*B1 = 8*2;4 = 8*24 = 4B= B= 8*8221 = 18*84B = 4*21 = B*B146 = B*1686 =

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




4ind &e>lection : Ste,: 11 10:./a un 22012

Wind De>ection alculations:

#he follo3ing ta!le is for the 5perating Case

Wind De>ection

= = Cumulative = Centroid = Elem* End = Elem* Ang* = From= 9o = Wind Shear = De'lection =De'lection = 5otation = = = #g' = mm = mm = = 1B="egs= *** = 1*142 = 1*142 = B*BB612B6 = "egs= 6B= ;*;66 = 1*148B = 1*14;6 = B*BB61; = 6B= 4B= 11*1 = 1*11 = 1*12 = B*BB61241 = 4B= B= 18*84B = 1*1216 = 1*124 = B*BB61241 =

ritical Wind !elocit1 2or Tower !ibration

= = 1st Crit* = 6nd Crit* = From= 9o = Wind S.eed = Wind S.eed =

= = #m$hr = #m$hr = 1B= 6B= 12*B; = 1121*;4 = 6B= 4B= 12*646 = 1126*B = 4B= B= 12*B; = 1121*;4 =

Allo(a)le de'lection at the 9o(er 9o. ,-.e/, 8*BBBT$1BB't* Criteria/ Allo(a)le de'lection : ;*;2 Actual De'lection : 1*12 mm

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Lon5itudinal Stress onstants : Ste,: 12 10:./a un 22012

;on6itudinal Stress onstants

= = Metal Area = Metal Area =Ne( Cold = Corroded = From= 9o = Ne( Cold = Corroded =Sect* Mod* = Sect* Mod* = = = cm@ = cm@ = mm L = mm L =

1B= 6B= 112*8B = *688 = 1*1E>B8 = 24B2* = 6B= 4B= 112*8B = *2B8 = 1*1;1E>B8 = 2;21* = 4B= B= 112*8B = *688 = 1*1E>B8 = 24B2* =

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Lon5itudinal !llo?a@le Stresses : Ste,: 1 10:./a un 22012

;on6itudinal Allowable Stresses

= = = ?!drotest = = ?!drotest = From= 9o = 9ensile = 9ensile = Com.ressive = Com.ressive = = = #g'$cm@ = #g'$cm@ = #g'$cm@ = #g'$cm@ =

1B="egs= 1668*6 = 66;2*8 = 161*;; = 161*;; = "egs= 6B= 1668*6 = 66;2*8 = 161*;; = 161*;; = 6B= 4B= 1668*6 = 66;2*8 = 161*4 = 161*4 = 4B= B= 1668*6 = 66;2*8 = 161*;; = 161*;; =

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Lon5itudinal Stresses &ue to A A A Ste,: 13 10:./a un 22012

From= 9o = Corroded = Corroded = No Corr* = No Corr* = = = #g'$cm@ = #g'$cm@ = #g'$cm@ = #g'$cm@ = 1B="egs= *** = *** = *** = *** = "egs= 6B= *** = *** = *** = *** = 6B= 4B= *** = *** = *** = *** = 4B= B= *** = *** = *** = *** =

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Stress due to o@ined Loads : Ste,: 1. 10:./a un 22012

Stress ombination ;oad ases 2or !ertical !essels:

;oad ase De?nition @e1

IP "ongitudinal Stress due to Internal Pressure

EP "ongitudinal Stress due to External Pressure ?P "ongitudinal Stress due to ?!drotest Pressure NP No Pressure EW "ongitudinal Stress due to Weight ,No "iuid/ -W "ongitudinal Stress due to Weight ,-.erating/ ?W "ongitudinal Stress due to Weight ,?!drotest/ WI &ending Stress due to Wind Moment ,-.erating/ E0 &ending Stress due to Earthua#e Moment ,-.erating/ EE &ending Stress due to Earthua#e Moment ,Em.t!/ ?I &ending Stress due to Wind Moment ,?!drotest/ ?E &ending Stress due to Earthua#e Moment ,?!drotest/ WE &ending Stress due to Wind Moment ,Em.t!/ ,no CA/ WF &ending Stress due to Wind Moment ,Filled/ ,no CA/ CW "ongitudinal Stress due to Weight ,Em.t!/ ,no CA/ <- &ending Stress due to <ortex Shedding "oads , -.e /

<E &ending Stress due to <ortex Shedding "oads , Em. / <F &ending Stress due to <ortex Shedding "oads , 9est No CA* / FW Axial Stress due to <ertical Forces 'or the Wind Case FS Axial Stress due to <ertical Forces 'or the Seismic Case &W &ending Stress due to "at* Forces 'or the Wind Case% Corroded &S &ending Stress due to "at* Forces 'or the Seismic Case% Corroded &N &ending Stress due to "at* Forces 'or the Wind Case% 7nCorroded &7 &ending Stress due to "at* Forces 'or the Seismic Case% 7nCorroded

G,),/"# N(&,*

Ca! (,9! HI an& HE a% in () Co%%o&& con&i(ion.

Ca! (,9! ;E+ ;F+ an& C; a% in () Un5Co%%o&& con&i(ion.

A /lan= !(%!! an& !(%!! %a(io in&ica(! ()a( () co%%!9on&in>!(%!! co9%i!in> ()o! co9onn(! ()a( &i& no( con(%i/( (o ()a((,9 o- !(%!!.

An a!(%i!= 4 in () -inal coln &no(! o*%!(%!!.

2nalysis of Load Case 1 : %A=WAWA;WA@W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 1668*6 B*21 161*;; B*BBB B*BBB8 1B 4*12 1668*6 *B 161*;; B*BB68 B*BB6 6B 8*6 1668*6 11*6 161*4 B*BB;; B*BB 4B 1668*6 B*42 161*;; B*BBB4

2nalysis of Load Case > : %A=WA==A;SA@S From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 1668*6 B*21 161*;; B*BBB B*BBB8 1B 6*8 1668*6 4*;2 161*;; B*BB66 B*BB6; 6B ;*B6 1668*6 *; 161*4 B*BB1 B*BB8 4B 1668*6 B*4 161*;; B*BBB4

2nalysis of Load Case : %A5WAWA;WA@W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 1668*6 B*21 161*;; B*BBB B*BBB8




1B 6*8 1668*6 * 161*;; B*BB64 B*BB46 6B 8*6 1668*6 11*6 161*4 B*BB;; B*BB 4B 1668*6 B*42 161*;; B*BBB4

2nalysis of Load Case B : %A5WA=A;SA@S From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*

Node Stress Stress Stress Stress 5atio 5atio 1B B*21 1668*6 B*21 161*;; B*BBB B*BBB8 1B 4*B4 1668*6 *8 161*;; B*BB6; B*BB44 6B *4 1668*6 11*4 161*4 B*BB8B B*BB2 4B 1668*6 B*4 161*;; B*BBB4

2nalysis of Load Case : %A6WA6 From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 66;2*8 B*21 161*;; B*BBB B*BBB8 1B B*24 66;2*8 1*4 161*;; B*BBB B*BB16 6B 1*6B 66;2*8 ;*8 161*4 B*BBB; B*BB1 4B 66;2*8 B*42 161*;; B*BBB4

2nalysis of Load Case ) : %A6WA6=

From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 66;2*8 B*21 161*;; B*BBB B*BBB8 1B B*B8 66;2*8 B*; 161*;; B*BBBB B*BBB 6B 66;2*8 4*4 161*4 B*BB62 4B 66;2*8 B*4 161*;; B*BBB4

2nalysis of Load Case 7 : A5WAWA;WA@W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 16;*B4 1668*6 161*;; B*1B6B 6B 16*16 1668*6 161*4 B*1B;4 4B 161*1 1668*6 161*;; B*B

2nalysis of Load Case D : A5WA=A;SA@S From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 16;*4B 1668*6 161*;; B*1B66 6B 16* 1668*6 161*4 B*1B;2 4B 161*6 1668*6 161*;; B*B

2nalysis of Load Case 8 : =A5WAWA;WA@W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 1668*6 4*88 161*;; B*BB68 1B 1668*6 *4; 161*;; B*BB;6 6B 4*28 1668*6 1*1 161*4 B*BB41 B*BB 4B 1668*6 4*6 161*;; B*BB64

2nalysis of Load Case 1' : =A5WA=A;SA@S From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 1668*6 4*88 161*;; B*BB68 1B B*1 1668*6 *81 161*;; B*BBB1 B*BB; 6B *;1 1668*6 1* 161*4 B*BB4 B*B1B 4B 1668*6 4*6 161*;; B*BB64

2nalysis of Load Case 11 : 6A6WA6 From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 81*21 66;2*8 161*;; B*621




1B 81*24 66;2*8 161*;; B*621 6B 86*2; 66;2*8 161*4 B*628 4B 8B*84 66;2*8 161*;; B*6248

2nalysis of Load Case 1> : 6A6WA6= From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*

Node Stress Stress Stress Stress 5atio 5atio 1B 81*21 66;2*8 161*;; B*621 1B 81*B; 66;2*8 161*;; B*6242 6B 81*B6 66;2*8 161*4 B*6242 4B 8B*84 66;2*8 161*;; B*6248

2nalysis of Load Case 1 : AW=A=W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 161*; 1668*6 161*;; B*B 6B 16B*22 1668*6 161*4 B*B28 4B 161*B 1668*6 161*;; B*B

2nalysis of Load Case 1B : AW;ACW

From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 166*6 1668*6 161*;; B*B 1B 161*8 1668*6 161*;; B*B6 6B 16B*2 1668*6 161*4 B*B28 4B 166*B6 1668*6 161*;; B*B;

2nalysis of Load Case 1 : A<5A5W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 161*; 1668*6 161*;; B*B1 6B 16B*22 1668*6 161*4 B*B28 4B 161*B 1668*6 161*;; B*B

2nalysis of Load Case 1) : A<=A=W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 161*; 1668*6 161*;; B*B 6B 16B*22 1668*6 161*4 B*B28 4B 161*B 1668*6 161*;; B*B

2nalysis of Load Case 17 : %A<5A5W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B B*21 1668*6 B*21 161*;; B*BBB B*BBB8 1B 1668*6 B* 161*;; B*BBB 6B 1668*6 4*B 161*4 B*BB61 4B 1668*6 B*4 161*;; B*BBB4

2nalysis of Load Case 1D : ;SA@SAA5W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 164*B2 1668*6 161*;; B*1BB 1B 161*; 1668*6 161*;; B*B1 6B 16B*22 1668*6 161*4 B*B28 4B 161*B 1668*6 161*;; B*B

2nalysis of Load Case 18 : ;SA@SA=A5W From 9ensile All* 9ens* Com.* All* Com.* 9ens* Com.*Node Stress Stress Stress Stress 5atio 5atio 1B 1668*6 4*88 161*;; B*BB68




1B 1668*6 4*2; 161*;; B*BB6 6B 1668*6 ;*B 161*4 B*BB6 4B 1668*6 4*64 161*;; B*BB64

A)solute Maximum o' the all o' the Stress 5atioUs B*628

o*%nin> Eln(: ENVOLVEN#Eo*%nin> Loa& Ca! 11 : HPKH;KHI

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------enter o> +rait9 alculation : Ste,: 1/ 10:./a un 22012

Sho&=(ield Installation 8&tions :

No( : #) C i! co9(& -%o () -i%!( Eln( F%o No&

Center o' +ravit! o' "iuid 4*2 cm Center o' +ravit! o' Nozzles 41*B cm Center o' +ravit! o' "egs 14*8B cm

Center o' +ravit! o' &are Shell Ne( and Cold ;;*21 cm Center o' +ravit! o' &are Shell Corroded ;;*21 cm

<essel C+ in the -.erating Condition 4*2;; cm <essel C+ in the Fa)ricated ,Sho.$Em.t!/ Condition 1*114 cm

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Le5 6ec; (,eratin5 ase) : Ste,: 1 10:./a un 22012

+lo)al Force ,S7S/ F! 11*2 #g' +lo)al Force ,S7S/ Fz B*B #g' +lo)al Moment ,S7S/ Mx B*B #g'm* +lo)al Moment ,S7S/ M! B*B #g'm* +lo)al Moment ,S7S/ Mz 4*; #g'm*

Internal Pressure ,S7S/ P 2*BB #g'$cm@ Include Pressure 9hrust No

+lo)al Force ,-CC/ Fx 61B*8 #g' +lo)al Force ,-CC/ F! 6* #g' +lo)al Force ,-CC/ Fz B*B #g' +lo)al Moment ,-CC/ Mx B*B #g'm* +lo)al Moment ,-CC/ M! B*B #g'm* +lo)al Moment ,-CC/ Mz 24*8 #g'm*

-ccasional Internal Pressure ,-CC/ Pvar B*BB #g'$cm@

7se Interactive Control No

W5C1B <ersion <ersion March 1

Include Pressure Stress Indices .er Div* 6 No Com.ute Pressure Stress .er W5C482 No

WRC 1'7 Stress Calculation for SUStained loads: 5adial "oad P B*B #g' Circum'erential Shear <C B*B #g' "ongitudinal Shear <" 11*2 #g' Circum'erential Moment MC B*B #g'm* "ongitudinal Moment M" 4*; #g'm* 9orsional Moment M9 B*B #g'm*

Dimensionless Parameters used : +amma 16*2

Dimensionless ;oads 2or 1lindrical Shells at Attachment Cunction: Curves read 'or 1 &eta Figure <alue "ocation N,P?I/ $ , P$5m / B*;84 C X 1*;; ,A%&/ N,P?I/ $ , P$5m / B*;84 4C X B*26 ,C%D/ M,P?I/ $ , P / B*4 6C1 B*B4 ,A%&/ M,P?I/ $ , P / B*4 1C X B*B; ,C%D/ N,P?I/ $ , MC$,5mGG6 G &eta/ / B*464 4A X B*;4 ,A%&%C%D/ M,P?I/ $ , MC$,5m G &eta/ / B*B; 1A B*B ,A%&%C%D/ N,P?I/ $ , M"$,5mGG6 G &eta/ / B*; 4& X 1*112 ,A%&%C%D/ M,P?I/ $ , M"$,5m G &eta/ / B*4; 1& B*B12 ,A%&%C%D/

N,x/ $ , P$5m / B*84 4C B*1 ,A%&/ N,x/ $ , P$5m / B*84 C 1*;46 ,C%D/

M,x/ $ , P / B*21 1C1 B*B48 ,A%&/ M,x/ $ , P / B*21 6C X B*B46 ,C%D/ N,x/ $ , MC$,5mGG6 G &eta/ / B*464 A X 1*B28 ,A%&%C%D/ M,x/ $ , MC$,5m G &eta/ / B*;; 6A X B*B4 ,A%&%C%D/ N,x/ $ , M"$,5mGG6 G &eta/ / B*; & X B*;4; ,A%&%C%D/ M,x/ $ , M"$,5m G &eta/ / B*;8; 6& X B*B68 ,A%&%C%D/

No( 5 #) a%= n( (o () -i>% na &no(! c%* *al c&&.

Stress Concentration Factors Hn 1*BB% H) 1*BB




Stresses in the !essel at the Attachment Cunction = Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl

= Circ* Mem)* P = B B B B B B B B Circ* &end* P = B B B B B B B B Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = B B B B B B B B Circ* &end* M" = 1 1 1 1 B B B B = 9ot* Circ* Str*= 6*8 B* 6*8 B* B*B B*B B*B B*B "ong* Mem)* P = B B B B B B B B "ong* &end* P = B B B B B B B B "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B "ong* Mem)* M" = B B B B B B B B

"ong* &end* M" = 1 1 1 1 B B B B = 9ot* "ong* Str*= 6*8 1*1 6*8 1*1 B*B B*B B*B B*B Shear <C = B B B B B B B B Shear <" = B B B B 1 1 1 1 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 1*4 1*4 1*4 1*4 Str* Int* = 6*81 1*1; 6*81 1*1; 6*;4 6*;4 6*;4 6*;4

Dimensionless Parameters used : +amma 41*

Dimensionless ;oads 2or 1lindrical Shells at Pad ed6e:

Curves read 'or 1 &eta Figure <alue "ocation N,P?I/ $ , P$5m / B*16 C X 6*41 ,A%&/ N,P?I/ $ , P$5m / B*16 4C X B*81 ,C%D/ M,P?I/ $ , P / B*8 6C1 B*BB ,A%&/ M,P?I/ $ , P / B*8 1C X B*B81 ,C%D/ N,P?I/ $ , MC$,5mGG6 G &eta/ / B*2B 4A B*26 ,A%&%C%D/ M,P?I/ $ , MC$,5m G &eta/ / B*;61 1A X B*B86 ,A%&%C%D/ N,P?I/ $ , M"$,5mGG6 G &eta/ / B*8B; 4& X 1*6 ,A%&%C%D/ M,P?I/ $ , M"$,5m G &eta/ / B*;84 1& X B*BB ,A%&%C%D/

N,x/ $ , P$5m / B*811 4C X B*81 ,A%&/ N,x/ $ , P$5m / B*811 C X 6*41 ,C%D/ M,x/ $ , P / B*86 1C1 X B*B1 ,A%&/

M,x/ $ , P / B*86 6C X B*B41 ,C%D/ N,x/ $ , MC$,5mGG6 G &eta/ / B*2B A 4*B2B ,A%&%C%D/ M,x/ $ , MC$,5m G &eta/ / B*86 6A X B*B68 ,A%&%C%D/ N,x/ $ , M"$,5mGG6 G &eta/ / B*8B; & X B*B ,A%&%C%D/ M,x/ $ , M"$,5m G &eta/ / B*86 6& X B*B11 ,A%&%C%D/

No( 5 #) a%= n( (o () -i>% na &no(! c%* *al c&&.


Stresses in the !essel at the Ed6e o2 Rein2orcin6 Pad




= Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl = Circ* Mem)* P = B B B B B B B B Circ* &end* P = B B B B B B B B Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = 6 6 6 6 B B B B Circ* &end* M" = 6 6 6 6 B B B B = 9ot* Circ* Str*= ;*; B*; ;*; B*; B*B B*B B*B B*B "ong* Mem)* P = B B B B B B B B "ong* &end* P = B B B B B B B B "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B "ong* Mem)* M" = 6 6 6 6 B B B B "ong* &end* M" = B B B B

= 9ot* "ong* Str*= 8*8 6*6 8*8 6*6 B*B B*B B*B B*B Shear <C = B B B B B B B B Shear <" = B B B B 6 6 6 6 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 4*B 4*B 4*B 4*B Str* Int* = 8*; 6*18 8*; 6*18 ;*4 ;*4 ;*4 ;*4

WRC 1'7 Stress Calculation for 5CCasional loads: 5adial "oad P 61B*8 #g' Circum'erential Shear <C B*B #g'

"ongitudinal Shear <" 6* #g' Circum'erential Moment MC B*B #g'm* "ongitudinal Moment M" 24*8 #g'm* 9orsional Moment M9 B*B #g'm*

Dimensionless Parameters used : +amma 16*2 Stress Concentration Factors Hn 1*BB% H) 1*BB

Stresses in the !essel at the Attachment Cunction = Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl =

Circ* Mem)* P = ; ; ; ; Circ* &end* P = 1 1 1 1 6 6 6 6 Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = 66 66 66 66 B B B B Circ* &end* M" = 4 4 4 4 B B B B = 9ot* Circ* Str*= 4;*B *B 22*4 6*8 4*2 6*B 4*2 6*B "ong* Mem)* P = ; ; ; ; "ong* &end* P = 12 12 12 12 1; 1; 1; 1; "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B




"ong* Mem)* M" = 1 1 1 1 B B B B "ong* &end* M" = ; ; ; ; B B B B = 9ot* "ong* Str*= 42* 1;*8 28*2 4*2 6;* 8*B 6;* 8*B Shear <C = B B B B B B B B Shear <" = B B B B 6 6 6 6 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 6* 6* 6* 6* Str* Int* = 42*6 1;*86 22*41 4*24 4;*;1 6*B 4;*;1 6*B

Dimensionless Parameters used : +amma 41* Stress Concentration Factors Hn 1*BB% H) 1*BB

Stresses in the !essel at the Ed6e o2 Rein2orcin6 Pad = Stress <alues at 9!.e o' = ,#g'$cm@ /

= Stress "oad= Au Al &u &l Cu Cl Du Dl = Circ* Mem)* P = B B B B 1; 1; 1; 1; Circ* &end* P = 66 66 66 66 12 12 12 12 Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = 8B 8B 8B 8B B B B B Circ* &end* M" = 6 6 6 6 B B B B = 9ot* Circ* Str*= 8*2 6*B 1;* 8*; 6B;* 14*2 6B;* 14*2 "ong* Mem)* P = 1; 1; 1; 1; B B B B "ong* &end* P = ;6 ;6 ;6 ;6 "ong* Mem)* MC = B B B B B B B B

"ong* &end* MC = B B B B B B B B "ong* Mem)* M" = ;4 ;4 ;4 ;4 B B B B "ong* &end* M" = 1B; 1B; 1B; 1B; B B B B = 9ot* "ong* Str*= B*6 1;*; 66*1 22*8 14*4 ;8* 14*4 ;8* Shear <C = B B B B B B B B Shear <" = B B B B 8 8 8 8 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 8*4 8*4 8*4 8*4 Str* Int* = B*66 62*; 66*B2 ;*B 6B8*64 1*11 6B8*64 1*11

WR #%B Stress Summations:

!essel Stress Summation at Attachment Cunction 9!.e o' = Stress <alues at Stress Int* = ,#g'$cm@ / = "ocation = Au Al &u &l Cu Cl Du Dl = Circ* Pm ,S7S/ = ; 1B4 ; 1B4 ; 1B4 ; 1B4 Circ* Pm ,-CC/ = B B B B B B B B Circ* Pm,9-9A"/= ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 Circ* Pl ,S7S/ = B B B B B B B B




Circ* Pl ,-CC/ = 14 14 41 41 ; ; ; ; Circ* Pl,9-9A"/= 14* 14* 46*2 46*2 ;* ;* ;* ;* Circ* 0 ,S7S/ = 1 1 1 1 B B B B Circ* 0 ,-CC/ = 66 66 ;8 ;8 6 6 6 6 Circ* 0 ,9-9A"/= 64* 64* ;2*1 ;2*1 6* 6* 6* 6* "ong* Pm ,S7S/ = "ong* Pm ,-CC/ = B B B B B B B B "ong* Pm,9-9A"/= *8 *8 *8 *8 *8 *8 *8 *8 "ong* Pl ,S7S/ = B B B B B B B B "ong* Pl ,-CC/ = 11 11 64 64 "ong* Pl,9-9A"/= 16* 16* 6*6 6*6 * * * * "ong* 0 ,S7S/ = 1 1 1 1 B B B B "ong* 0 ,-CC/ = 6 6 84 84 1; 1; 1; 1; "ong* 0 ,9-9A"/= 6*6 6*6 8;*6 8;*6 18*B 18*B 18*B 18*B Shear Pm ,S7S/ = B B B B B B B B Shear Pm ,-CC/ = B B B B B B B B Shear Pm,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Shear Pl ,S7S/ = B B B B 1 1 1 1 Shear Pl ,-CC/ = B B B B 6 6 6 6

Shear Pl,9-9A"/= B*B B*B B*B B*B *B *B *B *B Shear 0 ,S7S/ = B B B B B B B B Shear 0 ,-CC/ = B B B B B B B B Shear 0 ,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Pm ,S7S/ = ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 Pm ,S7S>-CC/ = ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 ;*4 1B4*4 Pm>Pl ,S7S/ = 8*6 1B*6 *4 1B6*4 ;*4 1B4*4 ;*4 1B4*4 Pm>Pl ,S7S>-CC/= 1B*6 11*6 86*; B*; B*6 2*1 B*6 2*1 Pm>Pl>0 ,9otal/= 146*2 4*; 8*6 162*; 8B* 16*; 8B* 16*;

9!.e o' = Max* S*I* S*I* Allo(a)le = 5esult Stress Int* = #g'$cm@ = = Pm ,S7S/ = 1B4*6; 16B6*6; = Passed Pm ,S7S>-CC/ = 1B4*6; 16*B = Passed Pm>Pl ,S7S/ = 1B*12 12B4*4 = Passed Pm>Pl ,S7S>-CC/= 11*12 618*B; = Passed Pm>Pl>0 ,9-9A"/= 146*2; 48B8*; = Passed


!essel Stress Summation at Rein2orcin6 Pad Ed6e

9!.e o' = Stress <alues at Stress Int* = ,#g'$cm@ / = "ocation = Au Al &u &l Cu Cl Du Dl = Circ* Pm ,S7S/ = 64 6;1 64 6;1 64 6;1 64 6;1 Circ* Pm ,-CC/ = B B B B B B B B Circ* Pm,9-9A"/= 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 Circ* Pl ,S7S/ = 6 6 6 6 B B B B Circ* Pl ,-CC/ = 6B 6B 1B1 1B1 1; 1; 1; 1; Circ* Pl,9-9A"/= 64*B 64*B 1B4*8 1B4*8 1;* 1;* 1;* 1;* Circ* 0 ,S7S/ = 6 6 6 6 B B B B




Circ* 0 ,-CC/ = 12 12 12 12 Circ* 0 ,9-9A"/= ;6* ;6* *8 *8 12* 12* 12* 12* "ong* Pm ,S7S/ = 161 161 161 161 161 161 161 161 "ong* Pm ,-CC/ = B B B B B B B B "ong* Pm,9-9A"/= 161* 161* 161* 161* 161* 161* 161* 161* "ong* Pl ,S7S/ = 6 6 6 6 B B B B "ong* Pl ,-CC/ = 4 4 8 8 B B B B "ong* Pl,9-9A"/= 4*8 4*8 1* 1* B*4 B*4 B*4 B*4 "ong* 0 ,S7S/ = B B B B "ong* 0 ,-CC/ = ;6 ;6 1; 1; "ong* 0 ,9-9A"/= ;*6 ;*6 186*6 186*6 *B *B *B *B Shear Pm ,S7S/ = B B B B B B B B Shear Pm ,-CC/ = B B B B B B B B Shear Pm,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Shear Pl ,S7S/ = B B B B 6 6 6 6 Shear Pl ,-CC/ = B B B B 8 8 8 8 Shear Pl,9-9A"/= B*B B*B B*B B*B *4 *4 *4 *4 Shear 0 ,S7S/ = B B B B B B B B Shear 0 ,-CC/ = B B B B B B B B

Shear 0 ,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Pm ,S7S/ = 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 Pm ,S7S>-CC/ = 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 64*2 6;1*2 Pm>Pl ,S7S/ = 68*4 6;*4 61*4 6*4 64* 6;1* 64* 6;1* Pm>Pl ,S7S>-CC/= 688*2 6*2 1B*6 12*6 662*; 648* 662*; 648* Pm>Pl>0 ,9otal/= 41*1 666* 1;*4 6;*2 ;8* 6;* ;8* 6;*

9!.e o' = Max* S*I* S*I* Allo(a)le = 5esult

Stress Int* = #g'$cm@ = = Pm ,S7S/ = 6;1*21 16B6*6; = Passed Pm ,S7S>-CC/ = 6;1*21 16*B = Passed Pm>Pl ,S7S/ = 6;*44 12B4*4 = Passed Pm>Pl ,S7S>-CC/= 6* 618*B; = Passed Pm>Pl>0 ,9-9A"/= 6;*4 48B8*; = Passed

oltin6 Sie Requirement 2or ;e6 ase&lates :

&ase.late Material SA48 &ase.late Allo(a)le Stress S&A 118*1B #g'$cm@ &ase.late "ength & 14B*B2B mm &ase.late Width D 14B*B2B mm

&ase.late 9hic#ness &9?H 16*BBB mm "eg Dimension Along &ase.late "ength d 84*;BBB mm "eg Dimension Along &ase.late Width ) 84*;BBB mm Dist* 'rom the "eg Edge to &olt ?ole Center z 44*B6BB mm &olt Material SA14 & &olt Allo(a)le Stress S9&A 1;*82 #g'$cm@ Anchor &olt Nominal Diameter &-D 6;*BBB mm Num)er o' Anchor &olts in 9ension .er "eg N& 1 9otal Num)er o' Anchors &olt .er "eg N&9 1 7ltimate 62da! Concrete Strength FCP5IME 61B*61 #g'$cm@

Pla( ()ic=n!! %i%& 1?2Q 13 4 9% D. $o!!




(ince there is onl # %olt, the standard computation for this+eometr is not possi%le. reasona%le %olt si'e should %eselected. &er Me+es, use a # inch 25.9 mm1 %olt.

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012



PV Elite 2012 Licensee: Instituto Mexicano de Petroleo (IMP) - San BartoFileNae : F!-1100 "!N#$E %I&'NE$M!"I !*!L-+' 'EV ------Le5 6ec; (Filled ?=4ater) : Ste,: 1 10:./a un 22012

RES-;TS (8R ;E3S : '1droTest ase Descri&tion: ;E3S

;e6s attached to: TAPA I9(ERI8R

Section Pro&erties : Sin6le An6le ;$/0$/0%/*B0%

US2 2SC 18D8 Steel #a!le

-verall "eg "ength *626 cm E''ective "eg "ength "eglen 6*4B cm Distance "eg 7. Side o' <essel 4;*BB1 cm Num)er o' "egs Nleg 4 Cross Sectional Area 'or "6*;36*;3B*4;B Aleg 11*181 cm@ Section Inertia , strong axis / B*; cmGG Section Inertia , (ea# axis / B*; cmGG Section Modulus , strong axis / 6;*B mm L Section Modulus , (ea# axis / 6;*B mm L 5adius o' +!ration , strong axis / 1*168 mm 5adius o' +!ration , (ea# axis / 1*168 mm

Leg 5rientation - Eiagonal

-verturning Moment at to. o' "egs *1 #g'm* 9otal Weight "oad at to. o' "egs W 421* #g' 9otal Shear 'orce at to. o' "egs *6 #g' Additional 'orce in "eg due to &racing Fadd B*B #g' -ccasional "oad Factor -cc'ac 1*444 E''ective "eg End Condition Factor # 1*6BB

%ote: #he Legs are %ot Cross @raced #he Leg Shear ;orce includes Wind and Seismic =Fects

Pad Width along Circum'erence C11P 1;6*BB mm Pad "ength along <essel Axis C66P 4B*2BB mm Pad 9hic#ness 9.ad *;6; mm

$a0imum Shear at top of one Leg .<leg/: , Max,Wind% Seismic/ > Fadd / G , Imax $ Itot / , *6 > B*B / G , 8*2$*B; / 62*4 #g'

20ial Compression, Leg futhest from %2 .Sma/ ,,W$Nleg/>,Mleg$,NlegmG5n///$Aleg/ ,,421 $ 4 / > , $, 1 G 64*46 ///$ 11*181 / 1*22 #g'$cm@

20ial Compression, Leg closest to %2 .S4a/ , W $ Nleg / $ Aleg , 421 $ 4 / $ 11*181 11*B #g'$cm@

Com.uting Princi.al Axis and Inertias 'or Angle* "eg lengths and thic#ness: 84*;BB 84*;BB *;6;B Distance to geometric centroid: 1*4;; 1*4;; Arm a)out : 1*;6 1*1;2 Arm a)out : 16*4; 1*;6 "eg areas: 8*B2 ;*111 +eometric inertia com.onents : 14*448 6*818 +eometric inertia com.onents : 6*81 11*448 +eometric inertias I! Iz: B*;4 B*;4 Product o' inertia: B*64216E>B8 Mohrs 5adius: 1*;41 Average Inertia: B*;4




0FAC9 1*BBBB F& 1*8B; Princi.al Axis Inertias ,W/ 1*11 8*8 Angle to Princi.al Axis ;*BBB Distances to extreme 'i)ers CW C *B1 1*;6 F-& 'rom E ;; 68*14 &ending allo(a)les F)! F)z 1*8B; 1*8B;

Shear Center Coordinates Wo o: 1*;6 B*BBBB <alues 'or Elastic Flexural9orsional &uc#ling Stress: E% +% V% 5B@: 6;BB* 1148* B*21BEB1 1*416 A5EA% "EN+9?% H(% Hz: 1*4BB 62*;BB 1*6BBB 1*6BBB ?% Fe(% Fez% Fe: B*8;B6 664*22 ;*6; 4B*61 Fe com.uted 'rom C1: 181*;

Initial ,Hl$r/max% ,Hl$r/euiv B*B 6*BB Final ,Hl$r/max% Cc B*B 16*12 Fa )ased on E 1 1*1;22

Actual Allo(a)le Wea# Axis &ending : 1;1*; 6668* #g'$cm@

Strong Axis &ending : 1B6*8 6668* #g'$cm@ Axial Com.ression : 1*22 1;*B #g'$cm@

7NI9 C?ECHS A5E: ?11 B*BBB ?16 B*BBB ?14 B*16

AISC 7nit! Chec# : B*16 Should )e O to 1

WRC 1'7 Stress 2nalysis for Leg to Shell Junction, #est Condition

5ectangular Attachment Parameter C11 2*2B4 mm 5ectangular Attachment Parameter C66 62;*;B mm

In&ut Echo, WR#%B Item #, Descri&tion: ;E3S

Diameter &asis 'or <essel <)asis ID C!lindrical or S.herical <essel C!ls.h C!lindrical Internal Corrosion Allo(ance Cas B*BBBB mm <essel Diameter Dv 428*;B mm <essel 9hic#ness 9v *;6; mm

Design 9em.erature 8;*BB C

Attachment 9!.e 9!.e 5ectangular Parameter C11 C11 2*2B mm Parameter C66 C66 62;*; mm

9hic#ness o' 5ein'orcing Pad 9.ad *;6; mm Pad Parameter C11P C11. 1;6*BB mm

Pad Parameter C66P C66. 4B*2BB mm

Design Internal Pressure D. 2*BBB #g'$cm@ Include Pressure 9hrust No

<essel Centerline Direction Cosine <x B*BBB <essel Centerline Direction Cosine <! 1*BBB <essel Centerline Direction Cosine <z B*BBB Nozzle Centerline Direction Cosine Nx 1*BBB Nozzle Centerline Direction Cosine N! B*BBB Nozzle Centerline Direction Cosine Nz B*BBB

+lo)al Force ,S7S/ Fx B*B #g'




+lo)al Force ,S7S/ F! 16*4 #g' +lo)al Force ,S7S/ Fz B*B #g' +lo)al Moment ,S7S/ Mx B*B #g'm* +lo)al Moment ,S7S/ M! B*B #g'm* +lo)al Moment ,S7S/ Mz 4*2 #g'm*

Internal Pressure ,S7S/ P 2*BB #g'$cm@ Include Pressure 9hrust No

+lo)al Force ,-CC/ Fx 62* #g' +lo)al Force ,-CC/ F! 42*2 #g' +lo)al Force ,-CC/ Fz B*B #g' +lo)al Moment ,-CC/ Mx B*B #g'm* +lo)al Moment ,-CC/ M! B*B #g'm* +lo)al Moment ,-CC/ Mz 11*8 #g'm*

-ccasional Internal Pressure ,-CC/ Pvar B*BB #g'$cm@

7se Interactive Control No

W5C1B <ersion <ersion March 1

Include Pressure Stress Indices .er Div* 6 No Com.ute Pressure Stress .er W5C482 No

WRC 1'7 Stress Calculation for SUStained loads: 5adial "oad P B*B #g' Circum'erential Shear <C B*B #g' "ongitudinal Shear <" 16*4 #g' Circum'erential Moment MC B*B #g'm* "ongitudinal Moment M" 4*2 #g'm* 9orsional Moment M9 B*B #g'm*

Dimensionless Parameters used : +amma 1B*88

Dimensionless ;oads 2or 1lindrical Shells at Attachment Cunction: Curves read 'or 1 &eta Figure <alue "ocation N,P?I/ $ , P$5m / B*;82 C X 1*68 ,A%&/ N,P?I/ $ , P$5m / B*;82 4C X B*8; ,C%D/ M,P?I/ $ , P / B*4;1 6C1 B*B4 ,A%&/ M,P?I/ $ , P / B*4;1 1C X B*B86 ,C%D/ N,P?I/ $ , MC$,5mGG6 G &eta/ / B*46; 4A X B*4 ,A%&%C%D/ M,P?I/ $ , MC$,5m G &eta/ / B*B2 1A B*B2B ,A%&%C%D/ N,P?I/ $ , M"$,5mGG6 G &eta/ / B* 4& X 1*B46 ,A%&%C%D/ M,P?I/ $ , M"$,5m G &eta/ / B*42 1& B*B1 ,A%&%C%D/

N,x/ $ , P$5m / B*8 4C B*24B ,A%&/ N,x/ $ , P$5m / B*8 C 1*4; ,C%D/

M,x/ $ , P / B*2; 1C1 B*BB ,A%&/ M,x/ $ , P / B*2; 6C X B*B4 ,C%D/ N,x/ $ , MC$,5mGG6 G &eta/ / B*46; A X B*2;6 ,A%&%C%D/ M,x/ $ , MC$,5m G &eta/ / B*;;2 6A X B*B48 ,A%&%C%D/ N,x/ $ , M"$,5mGG6 G &eta/ / B* & X B* ,A%&%C%D/ M,x/ $ , M"$,5m G &eta/ / B*;B 6& X B*B4B ,A%&%C%D/

No( 5 #) a%= n( (o () -i>% na &no(! c%* *al c&&.





Stresses in the !essel at the Attachment Cunction = Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl

= Circ* Mem)* P = B B B B B B B B Circ* &end* P = B B B B B B B B Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = B B B B B B B B Circ* &end* M" = 1 1 1 1 B B B B = 9ot* Circ* Str*= 6*6 B*8 6*6 B*8 B*B B*B B*B B*B "ong* Mem)* P = B B B B B B B B "ong* &end* P = B B B B B B B B "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B "ong* Mem)* M" = B B B B B B B B

"ong* &end* M" = 1 1 1 1 B B B B = 9ot* "ong* Str*= 6*4 1*1 6*4 1*1 B*B B*B B*B B*B Shear <C = B B B B B B B B Shear <" = B B B B 1 1 1 1 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 1*6 1*6 1*6 1*6 Str* Int* = 6*68 1*B; 6*68 1*B; 6*4 6*4 6*4 6*4

Dimensionless Parameters used : +amma 6B*21

Dimensionless ;oads 2or 1lindrical Shells at Pad ed6e:

Curves read 'or 1 &eta Figure <alue "ocation N,P?I/ $ , P$5m / B*12 C X 1*B2 ,A%&/ N,P?I/ $ , P$5m / B*12 4C X B*1; ,C%D/ M,P?I/ $ , P / B*;BB 6C1 X B*B11 ,A%&/ M,P?I/ $ , P / B*;BB 1C X B*B;2 ,C%D/ N,P?I/ $ , MC$,5mGG6 G &eta/ / B*2 4A B*82B ,A%&%C%D/ M,P?I/ $ , MC$,5m G &eta/ / B*;6 1A X B*B8 ,A%&%C%D/ N,P?I/ $ , M"$,5mGG6 G &eta/ / B*81B 4& X 1*188 ,A%&%C%D/ M,P?I/ $ , M"$,5m G &eta/ / B*;6 1& X B*B1B ,A%&%C%D/

N,x/ $ , P$5m / B*818 4C X B*1; ,A%&/ N,x/ $ , P$5m / B*818 C X 1*B2 ,C%D/ M,x/ $ , P / B*84 1C1 X B*B6 ,A%&/

M,x/ $ , P / B*84 6C X B*B4B ,C%D/ N,x/ $ , MC$,5mGG6 G &eta/ / B*2 A 6*1 ,A%&%C%D/ M,x/ $ , MC$,5m G &eta/ / B*8;; 6A X B*B6 ,A%&%C%D/ N,x/ $ , M"$,5mGG6 G &eta/ / B*81B & X B*81 ,A%&%C%D/ M,x/ $ , M"$,5m G &eta/ / B*821 6& X B*B12 ,A%&%C%D/

No( 5 #) a%= n( (o () -i>% na &no(! c%* *al c&&.


Stresses in the !essel at the Ed6e o2 Rein2orcin6 Pad




= Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl = Circ* Mem)* P = B B B B B B B B Circ* &end* P = B B B B B B B B Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = 1 1 1 1 B B B B Circ* &end* M" = 6 6 6 6 B B B B = 9ot* Circ* Str*= *B B*8 *B B*8 B*B B*B B*B B*B "ong* Mem)* P = B B B B B B B B "ong* &end* P = B B B B B B B B "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B "ong* Mem)* M" = 1 1 1 1 B B B B "ong* &end* M" = 4 4 4 4 B B B B

= 9ot* "ong* Str*= * 6*B * 6*B B*B B*B B*B B*B Shear <C = B B B B B B B B Shear <" = B B B B 6 6 6 6 Shear M9 = B B B B B B B B = 9ot* Shear= B*B B*B B*B B*B 6*6 6*6 6*6 6*6 Str* Int* = *1 6*B4 *1 6*B4 *42 *42 *42 *42

WRC 1'7 Stress Calculation for 5CCasional loads: 5adial "oad P 62* #g' Circum'erential Shear <C B*B #g'

"ongitudinal Shear <" 42*2 #g' Circum'erential Moment MC B*B #g'm* "ongitudinal Moment M" 11*8 #g'm* 9orsional Moment M9 B*B #g'm*

Dimensionless Parameters used : +amma 1B*88 Stress Concentration Factors Hn 1*BB% H) 1*BB

Stresses in the !essel at the Attachment Cunction = Stress <alues at 9!.e o' = ,#g'$cm@ / = Stress "oad= Au Al &u &l Cu Cl Du Dl =

Circ* Mem)* P = B B B B B B B B Circ* &end* P = 1 1 1 1 6 6 6 6 Circ* Mem)* MC = B B B B B B B B Circ* &end* MC = B B B B B B B B Circ* Mem)* M" = 6 6 6 6 B B B B Circ* &end* M" = B B B B = 9ot* Circ* Str*= 4* B*2 * 6*8 4*; 6* 4*; 6* "ong* Mem)* P = B B B B 1 1 1 1 "ong* &end* P = 1 1 1 1 1 1 1 1 "ong* Mem)* MC = B B B B B B B B "ong* &end* MC = B B B B B B B B




Circ* Pl ,-CC/ = 1 1 4 4 B B B B Circ* Pl,9-9A"/= 6*4 6*4 *6 *6 B*8 B*8 B*8 B*8 Circ* 0 ,S7S/ = 1 1 1 1 B B B B Circ* 0 ,-CC/ = 6 6 8 8 6 6 6 6 Circ* 0 ,9-9A"/= 4*8 4*8 * * 6* 6* 6* 6* "ong* Pm ,S7S/ = 42 42 42 42 42 42 42 42 "ong* Pm ,-CC/ = B B B B B B B B "ong* Pm,9-9A"/= 42* 42* 42* 42* 42* 42* 42* 42* "ong* Pl ,S7S/ = B B B B B B B B "ong* Pl ,-CC/ = 1 1 6 6 1 1 1 1 "ong* Pl,9-9A"/= 1*2 1*2 4*1 4*1 1*B 1*B 1*B 1*B "ong* 0 ,S7S/ = 1 1 1 1 B B B B "ong* 0 ,-CC/ = 4 4 8 8 1 1 1 1 "ong* 0 ,9-9A"/= *2 *2 2*8 2*8 1*8 1*8 1*8 1*8 Shear Pm ,S7S/ = B B B B B B B B Shear Pm ,-CC/ = B B B B B B B B Shear Pm,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Shear Pl ,S7S/ = B B B B 1 1 1 1 Shear Pl ,-CC/ = B B B B B B B B

Shear Pl,9-9A"/= B*B B*B B*B B*B 1*; 1*; 1*; 1*; Shear 0 ,S7S/ = B B B B B B B B Shear 0 ,-CC/ = B B B B B B B B Shear 0 ,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Pm ,S7S/ = * 2;* * 2;* * 2;* * 2;* Pm ,S7S>-CC/ = * 2;* * 2;* * 2;* * 2;* Pm>Pl ,S7S/ = 2*6 28*6 8*8 2*8 *; 2;*; *; 2;*; Pm>Pl ,S7S>-CC/= * 2* 4*6 21*6 8* 2* 8* 2* Pm>Pl>0 ,9otal/= 24*4 2*B 8;*2 22*8 *B 2* *B 2*

9!.e o' = Max* S*I* S*I* Allo(a)le = 5esult Stress Int* = #g'$cm@ = = Pm ,S7S/ = 2;* 16B6*6; = Passed Pm ,S7S>-CC/ = 2;* 16*B = Passed Pm>Pl ,S7S/ = 28*6 12B4*4 = Passed Pm>Pl ,S7S>-CC/= 2*8 618*B; = Passed Pm>Pl>0 ,9-9A"/= 22*8; 48B8*; = Passed


!essel Stress Summation at Rein2orcin6 Pad Ed6e

9!.e o' = Stress <alues at Stress Int* = ,#g'$cm@ / = "ocation = Au Al &u &l Cu Cl Du Dl = Circ* Pm ,S7S/ = 1;2 188 1;2 188 1;2 188 1;2 188 Circ* Pm ,-CC/ = B B B B B B B B Circ* Pm,9-9A"/= 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 Circ* Pl ,S7S/ = 1 1 1 1 B B B B Circ* Pl ,-CC/ = 6 6 2 2 1 1 1 1 Circ* Pl,9-9A"/= 4* 4* *2 *2 1* 1* 1* 1* Circ* 0 ,S7S/ = 6 6 6 6 B B B B




Circ* 0 ,-CC/ = 2 2 11 11 11 11 Circ* 0 ,9-9A"/= *B *B 11*6 11*6 11*B 11*B 11*B 11*B "ong* Pm ,S7S/ = "ong* Pm ,-CC/ = B B B B B B B B "ong* Pm,9-9A"/= *4 *4 *4 *4 *4 *4 *4 *4 "ong* Pl ,S7S/ = 1 1 1 1 B B B B "ong* Pl ,-CC/ = 6 6 ; ; 6 6 6 6 "ong* Pl,9-9A"/= *B *B 8*2 8*2 6* 6* 6* 6* "ong* 0 ,S7S/ = 4 4 4 4 B B B B "ong* 0 ,-CC/ = ; ; 1 1 ; ; ; ; "ong* 0 ,9-9A"/= *B *B 12*6 12*6 ;* ;* ;* ;* Shear Pm ,S7S/ = B B B B B B B B Shear Pm ,-CC/ = B B B B B B B B Shear Pm,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Shear Pl ,S7S/ = B B B B 6 6 6 6 Shear Pl ,-CC/ = B B B B B B B B Shear Pl,9-9A"/= B*B B*B B*B B*B 6* 6* 6* 6* Shear 0 ,S7S/ = B B B B B B B B Shear 0 ,-CC/ = B B B B B B B B

Shear 0 ,9-9A"/= B*B B*B B*B B*B B*B B*B B*B B*B Pm ,S7S/ = 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 Pm ,S7S>-CC/ = 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 1;2*8 188*8 Pm>Pl ,S7S/ = 18B*4 182*4 1;8* 18* 1;2* 188*8 1;2* 188*8 Pm>Pl ,S7S>-CC/= 186*; 1B*; 12*2 1;8*2 1;*4 18;*4 1;*4 18;*4 Pm>Pl>0 ,9otal/= 18*8 184*; 14*8 182*1 18*4 18*4 18*4 18*4

9!.e o' = Max* S*I* S*I* Allo(a)le = 5esult

Stress Int* = #g'$cm@ = = Pm ,S7S/ = 188*; 16B6*6; = Passed Pm ,S7S>-CC/ = 188*; 16*B = Passed Pm>Pl ,S7S/ = 182*6 12B4*4 = Passed Pm>Pl ,S7S>-CC/= 1B*;6 618*B; = Passed Pm>Pl>0 ,9-9A"/= 18*46 48B8*; = Passed

oltin6 Sie Requirement 2or ;e6 ase&lates :

&ase.late Material SA48 &ase.late Allo(a)le Stress S&A 118*1B #g'$cm@ &ase.late "ength & 14B*B2B mm &ase.late Width D 14B*B2B mm

&ase.late 9hic#ness &9?H 16*BBB mm "eg Dimension Along &ase.late "ength d 84*;BBB mm "eg Dimension Along &ase.late Width ) 84*;BBB mm Dist* 'rom the "eg Edge to &olt ?ole Center z 44*B6BB mm &olt Material SA14 & &olt Allo(a)le Stress S9&A 1;*82 #g'$cm@ Anchor &olt Nominal Diameter &-D 6;*BBB mm Num)er o' Anchor &olts in 9ension .er "eg N& 1 9otal Num)er o' Anchors &olt .er "eg N&9 1 7ltimate 62da! Concrete Strength FCP5IME 61B*61 #g'$cm@

Pla( ()ic=n!! %i%& 1?2Q 13 4 9% D. $o!!




(ince there is onl # %olt, the standard computation for this+eometr is not possi%le. reasona%le %olt si'e should %eselected. &er Me+es, use a # inch 25.9 mm1 %olt.

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# 1 NECIN No7l: 11 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 #< 89EI89 (rom : #%

Pressure 'or 5ein'orcement Calculations P 2*BBB #g'$cm@ 9em.erature 'or Internal Pressure 9em. 8; C Design External Pressure Pext B*12 #g'$cm@

9em.erature 'or External Pressure 9em.ex 8; C

Shell Material SA64 WP& Shell Allo(a)le Stress at 9em.erature S 16B6*6; #g'$cm@ Shell Allo(a)le Stress At Am)ient Sa 16B6*6; #g'$cm@

Inside Diameter o' Elli.tical ?ead D 428*; mm As.ect 5atio o' Elli.tical ?ead Ar 6*BB ?ead Finished ,Minimum/ 9hic#ness t *;6;B mm ?ead Internal Corrosion Allo(ance c 4*1;B mm ?ead External Corrosion Allo(ance co B*BBBB mm

Distance 'rom ?ead Centerline "1 11*222B mm

7ser Entered Minimum Design Metal 9em.erature 62*2 C

Type of Element Connected to the Shell : Nozzle

Material SA1B8 & Material 7NS Num)er HB4BB8 Material S.eci'ication$9!.e Smls* .i.e Allo(a)le Stress at 9em.erature Sn 16B6*6; #g'$cm@ Allo(a)le Stress At Am)ient Sna 16B6*6; #g'$cm@

Diameter &asis ,'or tr calc onl!/ ID "a!out Angle 12B*BB deg Diameter 6*BBBB in*

Size and 9hic#ness &asis Nominal Nominal 9hic#ness tn 18B

Flange Material SA1B; Flange 9!.e Weld Nec# Flange

Corrosion Allo(ance can 4*1;B mm Voint E''icienc! o' Shell Seam at Nozzle E1 1*BB Voint E''icienc! o' Nozzle Nec# En 1*BB

-utside Proection ho 2*6B mm Weld leg size )et(een Nozzle and Pad$Shell Wo *;6;B mm +roove (eld de.th )et(een Nozzle and <essel Wgnv *;6;B mm Inside Proection h B*BBBB mm Weld leg size% Inside Element to Shell Wi B*BBBB mm ASME Code Weld 9!.e .er 7W18 None

Class o' attached Flange 4BB +rade o' attached Flange +5 1*1

#) P%!!% D!i>n o9(ion 'a! D!i>n P%!!% K !(a(ic )a&.

No77le S;etc6 (a9 not re,resent actual ?eld t9,e=con>i5uration)

D D D D D D D D =D DD D D





D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

No( : C)c=in> Nol in () $%i&ional &i%c(ion.

Rein2orcement A;-;ATI89, Descri&tion: 8 #< 89EI89

A"$E Co&+ "c(ion VIII+ Di*i!ion 1+ 2010+ 2011a+ U537 (o U5G

Actual Inside Diameter 7sed in Calculation 1*82 in* Actual 9hic#ness 7sed in Calculation B*4 in*

%o??le input data chec+ completed 3ithout errors

Re*d th+ per UG-7(a"of =lliptical 6ead, #r .nt ress/ ,PGDGH/$,6GSGEB*6GP/ A..endix 1,c/ ,2*BBG44*4BBBGB*/$, 6G16B6*6;G1*BBB*6G2*BB/ 1*621 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BBG6*8B/$,16B6G1*BBB*8G2*BB/ B*184 mm

Ri%& Nol ()ic=n!! n&% E(%nal P%!!% 9% U52 : 0.1112

UG-?0 L''&* (4 R,')4(/$,,)& @I)&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 1B;*61 mm Parallel to <essel Wall% o.ening length d ;6*848 mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 14*B8; mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< #= C;N>?;N.

This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.

9ole Cunction Minimum Desi6n Metal Tem&erature MDMTF alculations:

MDMT of the Nozzle Neck to Flange Weld, Curve:

o*%n. ()=+ (> 7.<G + (% 0.1< + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.037 + #9. R&c(ion 7 C

Min Metal 9em.* ($o im.act .er 7CS88 6 C Min Metal 9em.* at 5euired thic#ness ,7CS 88*1/ 1B C

MDMT of Nozzle!Shell"#ead Weld for the Nozzle $%CS!&&$a'($)'', Curve:

o*%n. ()=+ (> 7.<G + (% 0.1< + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.037 + #9. R&c(ion 7 C


+overning MDM9 o' all the su)oints o' this Vunction : 1B C

ANSI F#"), MDMT ')$#%') T,3,/"&%/, /,%$&'() 3,/ UCS-BB.1





7nadusted MDM9 o' ANSI &18*;$ 'langes .er 7CS88,c/ 6 C Flange MDM9 (ith 9em. reduction .er 7CS88,)/,1/,)/ 1B C Flange MDM9 (ith 9em. reduction .er 7CS88,)/,1/,c/ 1B C

;)% () "(%!! R&c(ion Ra(io 9% UC"5<</414/4 i! : Design Pressure$Am)ient 5ating 2*BB$;6*11 B*1;

Note: sin+ the minimum value from %1#1%1 and %1#1c1 a%ove as the calculated no''le flan+e M7MT.

Weld Si?e Calculations, Eescription: @5 1D C5%=H5%

Intermediate Calc* 'or nozzle$shell Welds 9min ;*;868 mm

R,*%#&* P,/ U5-1B.1 5euired 9hic#ness Actual 9hic#ness Nozzle Weld 4*242 B* G tmin* 8*46 B* G Wo mm

NO#E : "=i99in> () nol a((ac)n( 'l& !(%n>() calcla(ion!. P% U;51G/424 () nol! 9(& /, U53<c434a4

!all nol!4 &o no( %i% a 'l& !(%n>() c)c=.

M"6'% A##(";#, P/,**%/, 4(/ &+'* N(==#, "& &+'* L($"&'() Converged Max* Allo(* Pressure in -.erating case 42*BB; #g'$cm@

No(: #) $A;P o- ()i! nc(ion 'a! lii(& /, () 9a%n( ")ll?Ha&.

No( : C)c=in> Nol in () La(i(&inal &i%c(ion.

Rein2orcement A;-;ATI89, Descri&tion: 8 #< 89EI89


Actual Inside Diameter 7sed in Calculation 1*82 in* Actual 9hic#ness 7sed in Calculation B*4 in*


Re*d th+ per UG-7(a"of =lliptical 6ead, #r .nt ress/ ,PGDGH/$,6GSGEB*6GP/ A..endix 1,c/ ,2*BBG44*4BBBGB*/$, 6G16B6*6;G1*BBB*6G2*BB/ 1*621 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BBG6*8B/$,16B6G1*BBB*8G2*BB/ B*184 mm


UG-?0 L''&* (4 R,')4(/$,,)& @I)&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 2*48 mm Parallel to <essel Wall% o.ening length d *12 mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 14*B8; mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< #= C;N>?;N. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.





UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*444 mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *;8 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm

Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*;;B mm

D(%in Nol #)ic=n!! can&i&a( (/: min t)4% max, t)1%t)6/ J min 8*;; % max, ;*8; % ;*8; / J ;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*444 % ;*8;B / ;*8;B mm

A*aila/l Nol Nc= #)ic=n!! 0.7G .73 7.<G 55 O

Weld Si?e Calculations, Eescription: @5 1D C5%=H5%

Intermediate Calc* 'or nozzle$shell Welds 9min ;*;868 mm

R,*%#&* P,/ U5-1B.1 5euired 9hic#ness Actual 9hic#ness Nozzle Weld 4*242 B* G tmin* 8*46 B* G Wo mm

NO#E : "=i99in> () nol a((ac)n( 'l& !(%n>() calcla(ion!. P% U;51G/424 () nol! 9(& /, U53<c434a4 !all nol!4 &o no( %i% a 'l& !(%n>() c)c=.



#) D%o9 -o% ()i! Nol i! : 12.373 #) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : 111.0

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# 1 &'EN No7l: 12 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 *# DRE9 (rom : #%





Distance 'rom ?ead Centerline "1 11*222B mm




Diameter &asis ,'or tr calc onl!/ ID "a!out Angle B*BB deg Diameter 1*;BBB in*

Size and 9hic#ness &asis Nominal Nominal 9hic#ness tn 33S



-utside Proection ho B*;1B mm Weld leg size )et(een Nozzle and Pad$Shell Wo *;6;B mm +roove (eld de.th )et(een Nozzle and <essel Wgnv *;6;B mm Inside Proection h B*BBBB mm Weld leg size% Inside Element to Shell Wi B*BBBB mm ASME Code Weld 9!.e .er 7W18 None









D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

No( : C)c=in> Nol in () $%i&ional &i%c(ion.

Rein2orcement A;-;ATI89, Descri&tion: 8 *# DRE9


Actual Inside Diameter 7sed in Calculation 1*1BB in* Actual 9hic#ness 7sed in Calculation B*BB in*


Re*d th+ per UG-7(a"of =lliptical 6ead, #r .nt ress/ ,PGH1GD//$,6GSGEB*6GP/ .er 7+4,a/,4/ ,2*BBGB*228G44*4BBB/$,6 G16B6*6;G1*BBB*6G2*BB/ 1*18B8 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BBG1*1/$,16B6G1*BBB*8G2*BB/ B*11; mm


UG-?0 L''&* (4 R,')4(/$,,)& @I)&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 4*8B mm Parallel to <essel Wall% o.ening length d 48*266B mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 1;*2;B mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< /# 7AN.

This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.



o*%n. ()=+ (> .0 + (% 0.11G + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.020 + #9. R&c(ion 7 C



o*%n. ()=+ (> .0 + (% 0.11G + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.020 + #9. R&c(ion 7 C









;)% () "(%!! R&c(ion Ra(io 9% UC"5<</414/4 i! : Design Pressure$Am)ient 5ating 2*BB$;6*11 B*1;


Weld Si?e Calculations, Eescription: @5 1 ER=%

Intermediate Calc* 'or nozzle$shell Welds 9min 8*4;BB mm

R,*%#&* P,/ U5-1B.1 5euired 9hic#ness Actual 9hic#ness Nozzle Weld *;B B* G tmin* 8*46 B* G Wo mm

NO#E : "=i99in> () nol a((ac)n( 'l& !(%n>() calcla(ion!. P% U;51G/424 () nol! 9(& /, U53<c434a4

!all nol!4 &o no( %i% a 'l& !(%n>() c)c=.



No( : C)c=in> Nol in () La(i(&inal &i%c(ion.

Rein2orcement A;-;ATI89, Descri&tion: 8 *# DRE9




Re*d th+ per UG-7(a"of =lliptical 6ead, #r .nt ress/ ,PGH1GD//$,6GSGEB*6GP/ .er 7+4,a/,4/ ,2*BBGB*228G44*4BBB/$,6 G16B6*6;G1*BBB*6G2*BB/ 1*18B8 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BBG1*1/$,16B6G1*BBB*8G2*BB/ B*11; mm


UG-?0 L''&* (4 R,')4(/$,,)& @I)&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 82*;2BB mm Parallel to <essel Wall% o.ening length d 4*6BB mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 1;*2;B mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< /# 7AN. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.





UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*62; mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *;8 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm

Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm

D(%in Nol #)ic=n!! can&i&a( (/: min t)4% max, t)1%t)6/ J min 8*4; % max, ;*8; % ;*8; / J ;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*62; % ;*8;B / ;*8;B mm

A*aila/l Nol Nc= #)ic=n!! 0.7G 10.1<0 .0 55 O

Weld Si?e Calculations, Eescription: @5 1 ER=%






#) D%o9 -o% ()i! Nol i! : .<12 #) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : 110.<17

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# 11 !LIM !I' No7l: 1 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 ## A;IM AIR (rom : $% Pressure 'or 5ein'orcement Calculations P 2*BBB #g'$cm@ 9em.erature 'or Internal Pressure 9em. 8; C Design External Pressure Pext B*12 #g'$cm@


Shell Material SA1B8 & Shell Allo(a)le Stress at 9em.erature S 16B6*6; #g'$cm@ Shell Allo(a)le Stress At Am)ient Sa 16B6*6; #g'$cm@

Inside Diameter o' C!lindrical Shell D 42*4; mm Design "ength o' Section " 1121*21 mm Shell Finished ,Minimum/ 9hic#ness t *;6;B mm Shell Internal Corrosion Allo(ance c 4*1;B mm Shell External Corrosion Allo(ance co B*BBBB mm

Distance 'rom &ottom$"e't 9angent 8*;6BB cm



Material SA1B; Material 7NS Num)er HB4;B Material S.eci'ication$9!.e Forgings Allo(a)le Stress at 9em.erature Sn 1B8*1 #g'$cm@ Allo(a)le Stress At Am)ient Sna 1B8*1 #g'$cm@

Diameter &asis ,'or tr calc onl!/ -D "a!out Angle 12B*BB deg Diameter 1*;BB in*

Size and 9hic#ness &asis Actual Actual 9hic#ness tn 2*2BB mm


-utside Proection ho 1*6;B mm Weld leg size )et(een Nozzle and Pad$Shell Wo 8*4;BB mm +roove (eld de.th )et(een Nozzle and <essel Wgnv *;6;B mm Inside Proection h B*BBBB mm Weld leg size% Inside Element to Shell Wi B*BBBB mm ASME Code Weld 9!.e .er 7W18 None



D D D D D D D D =D DD D DD D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()




No77le alcsA : B# 11 !LIM !I' No7l: 1 10:./a un 22012


Weld Si?e Calculations, Eescription: @5 11 2L$ 2R

Intermediate Calc* 'or nozzle$shell Welds 9min ;*1;B mm

R,*%#&* P,/ U5-1B.1 5euired 9hic#ness Actual 9hic#ness Nozzle Weld *BBB; B* G tmin* *2 B* G Wo mm


M"6'% A##(";#, P/,**%/, 4(/ &+'* N(==#, "& &+'* L($"&'() Converged Max* Allo(* Pressure in -.erating case 46*68B #g'$cm@


#) D%o9 -o% ()i! Nol i! : 1.27

#) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : G2.07

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# 12 !LM !+$! No7l: 13 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 #$ A;M A3-A (rom : $%

Pressure 'or 5ein'orcement Calculations P 2*B1 #g'$cm@ 9em.erature 'or Internal Pressure 9em. 8; C Design External Pressure Pext B*12 #g'$cm@




Distance 'rom &ottom$"e't 9angent 1;*6BB cm




Diameter &asis ,'or tr calc onl!/ -D "a!out Angle 12B*BB deg Diameter 6*BBBB in*

Size and 9hic#ness &asis Nominal Nominal 9hic#ness tn 18B



-utside Proection ho 22*BBB mm Weld leg size )et(een Nozzle and Pad$Shell Wo *;6;B mm +roove (eld de.th )et(een Nozzle and <essel Wgnv *;6;B mm Inside Proection h B*BBBB mm Weld leg size% Inside Element to Shell Wi B*BBBB mm ASME Code Weld 9!.e .er 7W18 None








No77le alcsA : B# 12 !LM !+$! No7l: 13 10:./a un 22012

D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

Rein2orcement A;-;ATI89, Descri&tion: 8 #$ A;M A3-A


Actual -utside Diameter 7sed in Calculation 6*4; in* Actual 9hic#ness 7sed in Calculation B*4 in*


Re*d th+ per UG-7(a"of Cylindrical Shell, #r .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BG18*2;BB/$,16B6G1*BBB*8G2*B/ 1*468 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5o/$,SGE>B*GP/ .er A..endix 11 ,a/,1/

,2*BG4B*186;/$,16B6G1*BB>B*G2*B/ B*6B1 mm


UG-?0 L''&* (4 R,')4(/$,,)& @E6&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 2*48 mm Parallel to <essel Wall% o.ening length d *12 mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 14*B8; mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< #2 BM !. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les

that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.

UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*48 mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *;B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*;;B mm

D(%in Nol #)ic=n!! can&i&a( (/: min t)4% max, t)1%t)6/ J min 8*;; % max, ;*8; % ;*8; / J

;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*48 % ;*8;B / ;*8;B mm

A*aila/l Nol Nc= #)ic=n!! 0.7G .73 7.<G 55 O






No77le alcsA : B# / "A P'ES No7l: 1. 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 *. T/ PRES (rom : $%





Distance 'rom &ottom$"e't 9angent 8*;6BB cm




Diameter &asis ,'or tr calc onl!/ -D "a!out Angle 8B*BB deg Diameter 1*;BB in*







I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()




No77le alcsA : B# / "A P'ES No7l: 1. 10:./a un 22012

Rein2orcement A;-;ATI89, Descri&tion: 8 *. T/ PRES


Actual -utside Diameter 7sed in Calculation 1*;B in* Actual 9hic#ness 7sed in Calculation B*4;B in*


Re*d th+ per UG-7(a"of Cylindrical Shell, #r .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/ ,2*BBG18*2;BB/$,16B6G1*BBB*8G2*BB/ 1*41;1 mm

Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5o/$,SGE>B*GP/ .er A..endix 11 ,a/,1/ ,2*BBG66*66;B/$,1B8G1*BB>B*G2*BB/ B*1686 mm

Ri%& Nol ()ic=n!! n&% E(%nal P%!!% 9% U52 : 0.0<7G

UG-?0 L''&* (4 R,')4(/$,,)& @E6&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 88*BBB mm Parallel to <essel Wall% o.ening length d 44*B6BB mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 1*62; mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< /$ T. &A(. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les that are not isolated or do not meet Code spacin+ requirements. To force the computation of areas for small no''les +o to Tools"@Confi+uration and check the %o6 to force the !"/3 area or pp #"#0 computation.

UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**.

Wall 9hic#ness 'or Internal$External .ressures ta 4*4B16 mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm

D(%in Nol #)ic=n!! can&i&a( (/: min t)4% max, t)1%t)6/ J min 8*4; % max, ;*8; % ;*8; / J ;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*4B16 % ;*8;B /

;*8;B mm

A*aila/l Nol Nc= #)ic=n!! .00 55 O



o*%n. ()=+ (> .0 + (% 0.12< + c 3.17G0 + E 1.00"(%!! Ra(io (% E4?(> 5 c4 0.022 + #9. R&c(ion 7 C





No77le alcsA : B# 3.! V NIVEL No7l: 1/ 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 +0A ! 9I!E; (rom : $%





Distance 'rom &ottom$"e't 9angent 2*B2B cm




Diameter &asis ,'or tr calc onl!/ ID "a!out Angle 6B*BB deg Diameter 1*;BBB in*












No77le alcsA : B# 3.! V NIVEL No7l: 1/ 10:./a un 22012

D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

Rein2orcement A;-;ATI89, Descri&tion: 8 +0A ! 9I!E;





Re*d th+ per UG-7(a"of %o??le Wall, #rn .nt ress/ ,PG5/$,SGEB*8GP/ .er 7+6 ,c/,1/

,2*BBG1*1/$,16B6G1*BBB*8G2*BB/ B*11; mm


UG-?0 L''&* (4 R,')4(/$,,)& @E6&,/)"# P/,**%/, Parallel to <essel Wall ,Diameter "imit/ Dl 82*;2BB mm Parallel to <essel Wall% o.ening length d 4*6BB mm Normal to <essel Wall ,9hic#ness "imit/% no .ad 9ln. 1;*2;B mm

Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< 95 N?B. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les


UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*62; mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm

D(%in Nol #)ic=n!! can&i&a( (/: min t)4% max, t)1%t)6/ J min 8*4; % max, ;*8; % ;*8; / J

;*8;B mm








No77le alcsA : B# 3.B V NIVEL No7l: 1 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 +0 ! 9I!E; (rom : $%









Diameter &asis ,'or tr calc onl!/ ID "a!out Angle 6B*BB deg Diameter 1*;BBB in*













D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

Rein2orcement A;-;ATI89, Descri&tion: 8 +0 ! 9I!E;






,2*BG1*1/$,16B6G1*BBB*8G2*B/ B*11;8 mm



Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< 95 N?B. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les


UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*6B8 mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *;B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm


;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*6B8 % ;*8;B / ;*8;B mm
















;)% () "(%!! R&c(ion Ra(io 9% UC"5<</414/4 i! : Design Pressure$Am)ient 5ating 2*B$;6*11 B*1;;


Weld Si?e Calculations, Eescription: @5 B@ < %<=L




M"6'% A##(";#, P/,**%/, 4(/ &+'* N(==#, "& &+'* L($"&'() Converged Max* Allo(* Pressure in -.erating case 46*441 #g'$cm@


#) D%o9 -o% ()i! Nol i! : 1.G01 #) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : .31

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# 3/! IN"E' No7l: 1 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 +.A I9TER (rom : $%





Distance 'rom &ottom$"e't 9angent 2*B2B cm




Diameter &asis ,'or tr calc onl!/ ID "a!out Angle 41;*BB deg Diameter 1*;BBB in*












No77le alcsA : B# 3/! IN"E' No7l: 1 10:./a un 22012

D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

Rein2orcement A;-;ATI89, Descri&tion: 8 +.A I9TER






,2*BBG1*1/$,16B6G1*BBB*8G2*BB/ B*11; mm



Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< 9$ ?NTA. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les


UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*62; mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm


;*8;B mm








No77le alcsA : B# 3/B IN"E' No7l: 1< 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 +. I9TER (rom : $%









Diameter &asis ,'or tr calc onl!/ ID "a!out Angle 41;*BB deg Diameter 1*;BBB in*













D D DDDD

I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()

Rein2orcement A;-;ATI89, Descri&tion: 8 +. I9TER






,2*BG1*1/$,16B6G1*BBB*8G2*B/ B*11;8 mm



Note:

Takin+ a !"/$c1/1a1 e6emption for no''le: ;< 9$ ?NTA. This calculation is valid for no''les that meet all the requirements of para+raph !"/$. &lease check the Code carefull, especiall for no''les


UG-? M')'% N(==#, N,$ T+'$),** R,%'/,,)& @I)&. P/,**. Wall 9hic#ness 'or Internal$External .ressures ta 4*6B8 mm Wall 9hic#ness .er 7+18,)/% tr18) ;*8;B mm Wall 9hic#ness% shell$head% internal .ressure tr)1 *;B1 mm Wall 9hic#ness t)1 max,tr)1% tr18)/ ;*8;B mm Wall 9hic#ness t)6 max,tr)6% tr18)/ ;*8;B mm Wall 9hic#ness .er ta)le 7+; t)4 8*4;B mm


;*8;B mm

$ini ;all #)ic=n!! o- Nol Nc=! (U5G: max, ta% t) / max, 4*6B8 % ;*8;B / ;*8;B mm
















;)% () "(%!! R&c(ion Ra(io 9% UC"5<</414/4 i! : Design Pressure$Am)ient 5ating 2*B$;6*11 B*1;;


Weld Si?e Calculations, Eescription: @5 B)@ %#=R




M"6'% A##(";#, P/,**%/, 4(/ &+'* N(==#, "& &+'* L($"&'() Converged Max* Allo(* Pressure in -.erating case 46*441 #g'$cm@


#) D%o9 -o% ()i! Nol i! : 1.G01 #) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : .31

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le alcsA : B# VA SE+A No7l: 20 10:./a un 22012

I9P-T !A;-ES, 9ole Descri&tion: 8 ** !/ SE3/ (rom : *%





Distance 'rom ?ead Centerline "1 1*;2; mm




Diameter &asis ,'or tr calc onl!/ -D "a!out Angle B*BB deg Diameter 1*;BB in*







I)*,/& N(==#, N( P" )( I)*', 3/(>,$&'()




No77le alcsA : B# VA SE+A No7l: 20 10:./a un 22012


Weld Si?e Calculations, Eescription: @5 < S=G

Intermediate Calc* 'or nozzle$shell Welds 9min ;*1;B mm

R,*%#&* P,/ U5-1B.1 5euired 9hic#ness Actual 9hic#ness Nozzle Weld *BBB; B* G tmin* *2 B* G Wo mm


M"6'% A##(";#, P/,**%/, 4(/ &+'* N(==#, "& &+'* L($"&'() Converged Max* Allo(* Pressure in -.erating case 42*B2 #g'$cm@


#) D%o9 -o% ()i! Nol i! : 0.<7

#) C( Ln>() -o% ()i! Nol i!+ D%o9 K Ho K H K # : G1.7

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le Sc6edule : Ste,: 2< 10:./a un 22012

9ole Schedule:

Nominal Flange Noz* Wall 5ePad Cut Descri.tion Size Sch$9!.e -$Dia 9h# -Dia 9hic# "ength in* Cls in* mm mm mm mm

&-0 41 D5EN 1*;BB 33S WNF 1*BB 1B*18B 11B*8 &-0 ;A < NI<E" 1*;BB 33S WNF 1*BB 1B*18B *4 &-0 ;& < NI<E" 1*;BB 33S WNF 1*BB 1B*18B *4 &-0 8A IN9E5 1*;BB 33S WNF 1*BB 1B*18B *4 &-0 8& IN9E5 1*;BB 33S WNF 1*BB 1B*18B *4&-0 11 A"IM AI5 1*;B None 1*;B 2*2B ;6*B2&-0 48 9* P5ES 1*;B None 1*;B 2*2B ;6*B2&-0 44 <* SE+* 1*;B None 1*;B 2*2B ;1* &-0 12 C-NE3I-N 6*BBB 18B WNF 6*4; 2*42 111*B &-0 16 A"M A+7A 6*BBB 18B WNF 6*4; 2*42 1BB*

!eneral Notes for the a%ove ta%le:

#) C( Ln>() i! () O(!i& P%oc(ion K In!i& P%oc(ion K D%o9 K

In Plan ")ll #)ic=n!!. #)i! *al &o! no( incl& 'l& >a9!+no% &o! i( accon( -o% !)%in=a>.

In () ca! o- O/li Nol!+ () O(!i& Dia(% !(/ inc%a!&. #) R5Pa& ;ID#H a%on& () nol i! calcla(& a! -ollo'!:;i&() o- Pa& Pa& O(!i& Dia. 9% a/o*4 5 Nol O(!i& Dia.4?2

Fo% )/ nol!+ () ()ic=n!! an& &ia(% !)o'n a% ()o! o- () !all% an& ()inn% !c(ion.

9ole Material and Weld (illet ;e6 Sie Details: Shl +rve Noz Shl$Pad Pad -D Pad +rve Inside Nozzle Material Weld Weld Weld Weld Weld mm mm mm mm mm

&-0 41 SA1B8 & *;6; *;6; &-0 ;A SA1B8 & *;6; *;6; &-0 ;& SA1B8 & *;6; *;6; &-0 8A SA1B8 & *;6; *;6; &-0 8& SA1B8 & *;6; *;6; &-0 11 SA1B; *;6; 8*4;B &-0 48 SA1B; *;6; 8*4;B &-0 44 SA1B; *;6; 8*4;B &-0 12 SA1B8 & *;6; *;6; &-0 16 SA1B8 & *;6; *;6;

No(: #) O(!i& 9%oc(ion! /lo' &o no( incl& () -lan> ()ic=n!!.

N(==#, M'*$,##"),(%* D"&"

Elevation$Distance "a!out Proection Installed In Nozzle From Datum Angle -utside Inside Com.onent cm deg* mm mm &-0 41 D5EN B*BB B*; B*BB 9APA INFE5I- &-0 ;A < NI<E" 2*B2 6B*BB 22*B B*BB EN<-"<EN9E &-0 ;& < NI<E" 1;*6B 6B*BB 22*B B*BB EN<-"<EN9E &-0 8A IN9E5 2*B2 41;*BB 22*B B*BB EN<-"<EN9E &-0 8& IN9E5 1;*6B 41;*BB 22*B B*BB EN<-"<EN9E &-0 11 A"IM AI5 8*;6B 12B*BB 1*6 B*BB EN<-"<EN9E &-0 48 9* P5ES 8*;6B 8B*BB 1*6 B*BB EN<-"<EN9E &-0 44 <* SE+* B*BB 1*6 B*BB 9APA S7PE5I- &-0 12 C-NE3I-N 12B*BB 2*4 B*BB 9APA INFE5I-




No77le Sc6edule : Ste,: 2< 10:./a un 22012

&-0 16 A"M A+7A 1;*6B 12B*BB 22*B B*BB EN<-"<EN9E

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




No77le Suar9 : Ste,: 0 10:./a un 22012

9ole alculation Summar1:

Descri.tion MAWP Ext MAPNC 7+; trJ Weld Areas or #g'$cm@ #g'$cm@ Path Stresses

&-0 12 C-NE3I-N 42*B1 *** *** -H ;*8 -H NoCalcGJ &-0 12 C-NE3I-N 42*B1 *** *** -H ;*8 -H NoCalcGJ &-0 41 D5EN 42*B1 *** *** -H ;*8 -H NoCalcGJ &-0 41 D5EN 42*B1 *** *** -H ;*8 -H NoCalcGJ &-0 11 A"IM AI5 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 16 A"M A+7A 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 48 9* P5ES 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 ;A < NI<E" 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 ;& < NI<E" 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 8A IN9E5 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 8& IN9E5 46*68 *** *** -H ;*8 -H NoCalcGJ &-0 44 <* SE+* 42*B2 *** *** -H ;*8 -H NoCalcGJ Min* Nozzles 46*68 &-0 8& IN Min* ShellFlgs 46*68 6B 4B 2*26

Com.uted <essel M*A*W*P* 46*68 #g'$cm@

.I/ - #his 3as a small opening and the areas 3ere not computed or the $2W of this connection could not !e computed !ecause the longitudinal !ending stress 3as greater than the hoop stress

%ote: $2Ws (nternal Case" sho3n a!o4e are at the 6igh oint

Chec+ the Spatial Relationship !et3een the %o??les

From Node Nozzle Descri.tion Coordinate% "a!out Angle% Dia* "imit 1B &-0 12 C-NE3I-N B*BBB 12B*BBB 2*BB 1B &-0 41 D5EN B*BBB B*BBB 82*;2B 6B &-0 11 A"IM AI5 8;*6BB 12B*BBB 88*BB

6B &-0 16 A"M A+7A 1;6*BB 12B*BBB 2*BB 6B &-0 48 9* P5ES 8;*6BB 8B*BBB 88*BB 6B &-0 ;A < NI<E" 2*B2B 6B*BBB 82*;2B 6B &-0 ;& < NI<E" 1;6*BB 6B*BBB 82*;2B 6B &-0 8A IN9E5 2*B2B 41;*BBB 82*;2B 6B &-0 8& IN9E5 1;6*BB 41;*BBB 82*;2B 4B &-0 44 <* SE+* B*BBB B*BBB 88*BB

T+, )(==#, *3"$') '* $(3%&, ;8 &+, 4(##(') "%( ll@ K lc@ 4 ')% ll 5 A%c ln>() alon> () in!i& *!!l !%-ac in () lon>. &i%c(ion. lc 5 A%c ln>() alon> () in!i& *!!l !%-ac in () ci%c. &i%c(ion

f any interferences94iolations are found, they 3ill !e noted !elo3

No in(%-%nc *iola(ion! )a* /n &(c(&

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




M&M" Suar9 : Ste,: 1 10:./a un 22012

Minimum Desi6n Metal Tem&erature Results Summar1 :

Curve &asic 5educed 7+6B,'/ 9hic#ness +ov EG Descri.tion MDM9 MDM9 MDM9 ratio 9h# Notes C C C mm

9APA INFE5I-51BJ & 6 4 6 B*266 *;6; 1*BBB 9APA INFE5I-5 J & 6 4 6 B*2;1 *;6; 1*BBB EN<-"<EN9E 2J & 6 4 6 B*2;B *;6; B*2;B 9APA S7PE5I-51BJ & 6 4 6 B*26B *;6; 1*BBB 9APA S7PE5I-5 J & 6 4 6 B*2 *;6; 1*BBB &-0 12 C-NE3I-1J & 6 1B B*B4 *8; 1*BBB Nozzle Flg J 6 1B B*B4 &-0 41 D5EN 1J & 6 1B B*B6B 2*2B 1*BBB Nozzle Flg J 6 1B B*B6B &-0 11 A"IM AI1J & 6 1B B*B66 2*2B 1*BBB &-0 16 A"M A+71J & 6 1B B*B; *8; 1*BBB Nozzle Flg J 6 1B B*B; &-0 48 9* P5ES1J & 6 1B B*B66 2*2B 1*BBB &-0 ;A < NI<E1J & 6 1B B*B6B 2*2B 1*BBB

Nozzle Flg J 6 1B B*B6B &-0 ;& < NI<E1J & 6 1B B*B6B 2*2B 1*BBB Nozzle Flg J 6 1B B*B6B &-0 8A IN9E5 1J & 6 1B B*B6B 2*2B 1*BBB Nozzle Flg J 6 1B B*B6B &-0 8& IN9E5 1J & 6 1B B*B6B 2*2B 1*BBB Nozzle Flg J 6 1B B*B6B &-0 44 <* SE+*1J & 6 1B B*B66 2*2B 1*BBB

Aequired Minimum 7esi+n Metal Temperature "2D C -armest Computed Minimum 7esi+n Metal Temperature "/3 C

N(&,* 5 #)i! 'a! an i9ac( (!(& a(%ial. 1 5 o*%nin> Nol ;l&.

5 AN"I Flan> $D$# Calc! #)ic=n!! %a(io 9% UC"5<</414c4. G 5 AN"I Flan> $D$# Calc! #)ic=n!! %a(io 9% UC"5<</414/4. < 5 $D$# Calcla(ion! a( () ")ll?Ha& Join(. 7 5 $D$# Calcla(ion! -o% () "(%ai>)( Flan>. 5 C,lin&%?Con?Flan> Jnc(ion $D$#. 5 Calcla(ion! in () "9)%ical Po%(ion o- () Ha&.10 5 Calcla(ion! in () nc=l Po%(ion o- () Ha&.11 5 Calcla(& Bo&, Flan>4 Flan> $D$#.12 5 Calcla(& Fla( Ha& $D$# 9% UC"5<<34

U5/424 'a! no( con!i&%&.UC"5<<>4 'a! no( con!i&%&.UC"5<<i4 'a! no( con!i&%&.

No(!:

I9ac( (!( (9! '% no( n(%& in an& no( con!i&%& in () anal,!i!.UC"5<<i4 a99li! (o i9ac( (!(& a(%ial! no( /, !9ci-ica(ion an&UC"5<<>4 a99li! (o a(%ial! i9ac( (!(& 9% U5.1 n%al No( c4.#) Ba!ic $D$# incl&! () 30F4 P;H# c%&i( i- a99lica/l.PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




M&M" Suar9 : Ste,: 1 10:./a un 22012

Desi6n ode: ASME ode Section !III Di"ision #, $%#%, $%##a

Diameter S.ec : B8*BB mm -D <essel Design "ength% 9angent to 9angent 111* cm

Distance o' &ottom 9angent a)ove +rade B*BB cm S.eci'ied Datum "ine Distance B*BB cm

Shell Material S.eci'ication SA1B8 & ?ead Material S.eci'ication SA64 WP& Nozzle Material S.eci'ication SA1B; Nozzle Material S.eci'ication SA1B8 &

Internal Design 9em.erature 8; C Internal Design Pressure 2*BBB #g'$cm@

External Design 9em.erature 8; C External Design Pressure B*18 #g'$cm@

Maximum Allo(a)le Wor#ing Pressure 46*68B #g'$cm@

External Max* Allo(a)le Wor#ing Pressure 18*8 #g'$cm@ ?!drostatic 9est Pressure 1*42 #g'$cm@

5euired Minimum Design Metal 9em.erature 6 C Warmest Com.uted Minimum Design Metal 9em.erature 4 C

Wind Design Code Mexico 6BB2 Earthua#e Design Code Mexico Sismo

Element Pressures and MAWP: k62=cmG

Element Desc = Design Pres* = External = M*A*W*P = Corrosion = > Stat* head = Pressure = = Allo(ance 9APA INFE5I-5 2*B B*18 42*BB; 4*1;B

EN<-"<EN9E 2*B B*18 46*68B 4*1;B 9APA S7PE5I-5 2*BBB B*18 42*B2 4*1;B

"iuid "evel: 2* cm Dens*: *;;6 #gm$mL S.* +r*: 1*BBB

Element T9oT Elev "ength Element 9h# 5 e d 9 h # Voint E'' 9!.e cm cm mm Int* Ext* "ong Circ Elli.se *8 *8 *; ;* ;* 1*BB B*2; C!linder 1B*1 8*; *; ;* *6 B*2; B*2; Elli.se 111* *8 *; ;* ;* 1*BB B*2;

Eln( ()ic=n!!! a% !)o'n a! Noinal i- !9ci-i&+ o()%'i! a% $ini

9otal Wind Shear on to. o' all "egs 14* #g'

9otal Earthua#e Shear on to. o' all "egs 122* #g' 9otal Wind Moment at to. o' all "egs 6* #g'm* 9otal Earthua#e Moment at to. o' all "egs 4B* #g'm*

Max* Wind Shear on one "eg ,to. )ottom/ 611* #g' Max* Earth* Shear on one "eg ,to. )ottom/ 611* #g' Max* Wind Moment at )ase o' one "eg 6B;* #g'm* Max* Earthua#e Moment at )ase o' one "eg 6B;* #g'm* Max* <ertical "oad ,Wt* > Wind/ on one "eg 646* #g' Max* <ertical "oad ,Wt* > E*/ on one "eg 66* #g'

No(: ;in& an& Ea%()a= on(! incl& () --c(! o- !% &-in&




M&M" Suar9 : Ste,: 1 10:./a un 22012

-o%c! an& on(! i- an, i!( in () o/ an& '% !9ci-i& (o ac( co9( loa&! an& !(%!!!4 &%in> ()! ca!!. Al!o incl&& a% on( --c(! & (o ccn(%ic 'i>)(! i- an, a% 9%!n( in () in9(.

5,'+&* Fa)ricated &are W$- 5emova)le Internals 68;* #gm Sho. 9est Fa)ricated > Water , Full / 16*6 #gm Shi..ing Fa)* > 5em* Intls*> Shi..ing A..* 68;* #gm Erected Fa)* > 5em* Intls*> Insul* ,etc/ 68;* #gm Em.t! Fa)* > Intls* > Details > Wghts* 68;* #gm -.erating Em.t! > -.erating "iuid ,No CA/ 4* #gm Field 9est Em.t! Weight > Water ,Full/ 4;*B #gm

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




M&M" Suar9 : Ste,: 1 10:./a un 22012

In&ut Echo, ;e6 H ;u6 Item #, Descri&tion: 8RECA DE IACE

Design Internal Pressure 2*BB #g'$cm@ Design 9em.erature 'or Attachment 9EMP 8;*BB C <essel -utside Diameter -D B8*BBB mm <essel Wall 9hic#ness 9s *;6;B mm

<essel Corrosion Allo(ance Cas 4*1;B mm <essel Material SA1B8 & <essel Material 7NS Num)er HB4BB8 <essel Allo(a)le Stress at Design S 16B6*6; #g'$cm@ Anal!sis 9!.e: "i'ting "ug

Em.t! Weight o' <essel Wem. 46B*BB #g' -.erating Weight o' <essel ,vertical load / W B*BB #g'

"i'ting "ug Material SA;18 B "i'ting "ug Material 7NS Num)er HB6BB "i'ting "ug ield Stress IE"D 6;14*64 #g'$cm@

"i'ting "ug -rientation to <essel Per.endicular 9otal ?eight o' "i'ting "ug ( B*BBBB mm 9hic#ness o' "i'ting "ug t 16*BBB mm Diameter o' ?ole in "i'ting "ug dh 6;*BBBB mm 5adius o' SemiCircular Arc o' "i'ting "ug r 4B*BBBB mm ?eight o' "ug 'rom )ottom to Center o' ?ole h ;*BBBB mm -''set 'rom <essel -D to Center o' ?ole o'' B*BBBB mm Minimum thic#ness o' Fillet Weld around "ug t( *;6;B mm "ength o' (eld along side o' "i'ting "ug (l B*BBBB mm "ength o' Weld along &ottom o' "i'ting "ug () 16*BBB mm "i't -rientation <ertical Force Along <essel Axis Fax B*BB #g' Force Normal to <essel Fn 18B*BB #g' Force 9angential to <essel Ft B*BB #g' Im.act Factor Im.'ac 6*BB

-ccasional "oad Factor ,AISC A;*6/ -cc'ac 1*BB

Results 2or li2tin6 lu6s, Descri&tion : 8RECA DE IACE

Weld +rou. Inertia a)out the Circum'erential Axis I"C 1;*266 cmGG Weld +rou. Centroid distance in the "ong* Direction "" ;*;6; mm Dist* o' Weld +rou. Centroid 'rom "ug )ottom ""Y& ;*BBB mm Weld +rou. Inertia a)out the "ongitudinal Axis I"" 6*B; cmGG Weld +rou. Centroid Distance in the Circ* Direction "C 8*4;B mm

A99l,in> () I9ac( -ac(o% (o () loa&!: Fn 18B*BB G 6*BB 46B*BB #g'

P%ia%, ")a% "(%!! in () ;l&! & (o ")a% Loa&! "!ll: Srt, FaxZ6>FtZ6>FnZ6 / $ , ,6G(l>()/ G t( / Srt,B Z6>B Z6>46B Z6/ $ , ,6GB*B >16* / G *;6;B / 1*4 #g'$cm@

")a% "(%!! in () ;l&! & (o Bn&in> Loa&! "/l-: ,FnG,h""Y&// G""$I"C > ,FaxGo'' G""$I"C/ > ,FtGo'' G"C$I""/ ,46B G,;*BBB ;*BBB // G ;*;6; $1;*266 > ,B GB*BBB G ;*;6; $1;*266 / > ,B GB*BBB G 8*4;B $6*B; / B*BB #g'$cm@

#otal Shear Stress for Com!ined Loads .St/: Ssll > S)l' 1*4 > B*BBB 1*4 #g'$cm@

2llo3a!le Shear Stress for Com!ined Loads .Sta/:




M&M" Suar9 : Ste,: 1 10:./a un 22012

B* G ield G -cc'ac ,AISC Shear All*/ B* G 6;14 G 1*BB 1BB;*6 #g'$cm@

Shear Stress in Lug a!o4e 6ole .Shs/: Srt, FaxZ6 > FnZ6 > FtZ6 / $ Sha Srt, B Z6 > 46B Z6 > B Z6 / $ *;

1* #g'$cm@

2llo3a!le Shear Stress in Lug a!o4e 6ole .Sas/: B* G ield G -cc'ac B* G 6;14 G 1*BB 1BB;*6 #g'$cm@

in 6ole @earing Stress .!s/: Srt, FaxZ6 > FnZ6 / $ , t G dh / Srt, B Z6 > 46B Z6 / $ , 16*BB G 6;*BBB / 1BB* #g'$cm@

2llo3a!le @earing Stress .!a/: Min, B*; G ield G -cc'ac% B*Gield / AISC &earing All* Min, B*; G 6;14 G 1*BB % 6681* / 122*6 #g'$cm@

Bn&in> !(%!! a( () /a! o- () l> F/!: FtGo'' $ ,(GtZ,6/ $ 8/ > FaxGo'' $ ,(Z,6/Gt $ 8/ B G B*BBB $ ,B*BBB G 16*BB Z,6/ $ 8/ > B G B*BBB $ ,B*BBB Z,6/ G 16*BB $ 8/ B*BB #g'$cm@

#n!il !(%!! a( () /a! o- () l> Fa: Fn $ ,( G t/ 46B $ ,B*BBB G 16*BB / 62*BB #g'$cm@

#o(al Co/in& "(%!! a( () /a! o- () l>: F/! K Fa 2.0 =>-?c@

L> Allo'a/l "(%!! -o% Bn&in> an& #n!ion:

Min, B*88 G ield G -cc'ac% B*;Gield / Min, B*88 G 6;14 G 1*BB % 122* / 18;2* #g'$cm@

No(: C)c= () ")ll "(%!!! !in> ()o& !c) a! ;RC5107.

Summar1 82 Results Stress ,#g'$cm@/ Actual Allo(a)le P$F Primar! Shear Stress o' Weld : 1*4 1BB;*6 -# Shear Stress a)ove ?ole : 1* 1BB;*6 -# Pin ?ole &earing Stress : 1BB* 122*6 -# 9otal Com)ined Stress at the lug )ase : 62*BB 18;2*4 -#

PV E#'&, '* " &/","/ (4 I)&,//"3+ CAD5(/6 7 A)"#8*'* S(#%&'()* I)$. 2012




M&M" Suar9 : Ste,: 1 10:./a un 22012

memoria de calculo tanque hidroneumatico

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