audit-vessel-1.pdf

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Table of Contents

Cover Page 1

Warnings and Errors 2Input Echo 3

XY Coordinate Calculations 7

Internal Pressure Calculations 8

External Pressure Calculations 11

Element and Detail Weights 13

Nozzle Flange MAWP 15

Natural Frequency Calculation 16

Wind/Earthquake Shear, Bending 17

Longitudinal Stress Constants 18

Longitudinal Allowable Stresses 19

Longitudinal Stresses Due to . . 20

Stress due to Combined Loads 22

Center of Gravity Calculation 26Leg Check, (Operating Case) 27

Leg Check, (Filled w/Water) 29

Nozzle Calcs. Noz N4 31

Nozzle Calcs. Noz N3, N2 34

Nozzle Calcs. Noz N5, N6 37

Nozzle Calcs. Noz N1 40

Nozzle Schedule 43

Nozzle Summary 44

Vessel Design Summary 45

Problems/Failures Summary 46


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Cover Page

DESI GN CALCULATI ON

I n Accor dance wi t h ASME Sect i on VI I I Di vi si on 1

ASME Code Ver si on : 2007

Anal ysi s Per f or med by : KEDKEP CONSULTI NG, I NC.

J ob Fi l e : E: \ 200828 AUDI T VESSEL\ AUDI T VESSEL. PVI

Date of Anal ysi s : Sep 15, 2008

PV El i t e 2008, May 2008


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PV Elite 2008 Licensee: KEDKEP CONSULTING, INC.

FileName : Audit Vessel ---------------------------------- Page 2 of 46

Warnings and Errors Step: 0 5:25p Sep 15,2008

Cl ass Fr om To : Basi c El ement Checks. ==========================================================================

Cl ass From To: Check of Addi t i onal El ement Dat a

==========================================================================

There were no geomet r y err or s or warni ngs.

PV Elite 2008 c1993-2008 by COADE Engineering Software


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Input Echo Step: 1 5:25p Sep 15,2008

PV Elite Vessel Analysis Program: Input Data

Desi gn I nt er nal Pressur e ( f or Hydr ot est ) 100. 00 psi g

Desi gn I nternal Temper ature 300 F Type of Hydr ot est UG99- b Not e [ 34] Hydr ot est Posi t i on Ver t i cal Proj ect i on of Nozzl e f r om Vessel Top 0. 0000 i n Pr oj ect i on of Nozzl e f r om Vessel Bot t om 0. 0000 i n Mi ni mum Desi gn Met al Temper at ure - 20 F Type of Const r uct i on Wel ded Speci al Servi ce None Degr ee of Radi ogr aphy RT- 4 Mi scel l aneous Wei ght Per cent 0. Use Hi gher Longi t udi nal St r esses ( Fl ag) Y Sel ect t f or I nt er nal Pr essur e ( Fl ag) N Sel ect t f or Ext er nal Pr essur e ( Fl ag) N

Sel ect t f or Axi al St ress ( Fl ag) N Sel ect Locat i on f or St i f f . Ri ngs ( Fl ag) N Use Hydr otest Al l owabl e Unmodi f i ed Y Consi der Vort ex Sheddi ng N Per f orm a Corr oded Hydr otest N I s t hi s a Heat Exchanger No User Def i ned Hydr o. Press. ( Used i f > 0) 0. 0000 psi g User def i ned MAWP 0. 0000 psi g User def i ned MAPnc 0. 0000 psi g

Load Case 1 NP+EW+WI +FW+BW Load Case 2 NP+EW+EE+FS+BS Load Case 3 NP+OW+WI +FW+BW

Load Case 4 NP+OW+EQ+FS+BS Load Case 5 NP+HW+HI Load Case 6 NP+HW+HE Load Case 7 I P+OW+WI +FW+BW Load Case 8 I P+OW+EQ+FS+BS Load Case 9 EP+OW+WI +FW+BW Load Case 10 EP+OW+EQ+FS+BS Load Case 11 HP+HW+HI Load Case 12 HP+HW+HE Load Case 13 I P+WE+EW Load Case 14 I P+WF+CW Load Case 15 I P+VO+OW Load Case 16 I P+VE+EW

Load Case 17 NP+VO+OW Load Case 18 FS+BS+I P+OW Load Case 19 FS+BS+EP+OW

Wi nd Desi gn Code No Wi nd Loads Desi gn Wi nd Speed 70. 000 mi l e/ hr Exposur e Const ant C I mpor t ance Fact or Roughness Fact or Base El evati on 0. 0000 i n Per cent Wi nd f or Hydr otest 33. Use Wi nd Prof i l e ( Y/ N) N Dampi ng Factor ( Beta) f or Wi nd ( Ope) 0. 0100

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

Sei smi c Desi gn Code No Sei smi c

Desi gn Nozzl e f or Des. Press. + St . Head Y


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Consi der MAP New and Col d i n Noz. Desi gn N Consi der External Loads f or Nozzl e Des. Y Consi der Code Case 2168 f or Nozzl e Des. N

Mat er i al Database Year Curr ent w/ Addenda or Code Year

Complete Listing of Vessel Elements and Details:

El ement Fr om Node 10 El ement To Node 20 El ement Type El l i pt i cal Descr i pt i on Bot t om Head Di st ance "FROM" t o "TO" 1. 5000 i n El ement Outsi de Di ameter 16. 000 i n El ement Thi ckness 0. 2250 i n I nt er nal Cor r osi on Al l owance 0. 0000 i n Nomi nal Thi ckness 0. 2500 i n Ext ernal Cor r osi on Al l owance 0. 0000 i n

Desi gn I nt er nal Pressur e 100. 00 psi g Desi gn Temperatur e I nternal Pressure 300 F Desi gn Ext er nal Pressur e 0. 0000 psi g Desi gn Temperatur e Ext ernal Pressure 200 F Ef f ecti ve Di amet er Mul t i pl i er 1. 2 Mat er i al Name SA- 516 70 Al l owabl e St r ess, Ambi ent 20000. psi Al l owabl e St r ess, Operat i ng 20000. psi Al l owabl e St r ess, Hydr ot est 34200. psi Mat eri al Densi t y 0. 2830 l bm/ i n 3̂ P Number Thi ckness 1. 2500 i n Yi el d St r ess, Oper at i ng 33600. psi UCS- 66 Char t Curve Desi gnat i on B

Ext ernal Pr essur e Char t Name CS- 2 UNS Number K02700 Pr oduct For m Pl at e Ef f i ci ency, Longi t udi nal Seam 0. 85 Ef f i ci ency, Ci r cumf er ent i al Seam 0. 7 El l i pt i cal Head Factor 2.

El ement Fr om Node 10 Det ai l Type Li qui d Detai l I D WATER Di st . f r om "FROM" Node / Of f set di st - 4. 0000 i n Hei ght / Lengt h of Li qui d 5. 5000 i n Densi t y of Li qui d 62. 400 l bm/ f t 3̂

El ement Fr om Node 10 Det ai l Type Nozzl e Detai l I D Noz N4 Di st . f r om "FROM" Node / Of f set di st 0. 0000 i n Nozzl e Di amet er 2. 5 i n. Nozzl e Schedul e None Nozzl e Cl ass 0 Layout Angl e 0. Bl i nd Fl ange ( Y/ N) N Wei ght of Nozzl e ( Used i f > 0 ) 0. 0000 l bf Gr ade of At t ached Fl ange None Nozzl e Mat l SA- 105

El ement Fr om Node 20 El ement To Node 30 El ement Type Cyl i nder Descr i pt i on Shel l Di st ance "FROM" t o "TO" 30. 000 i n


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El ement Outsi de Di ameter 16. 000 i n El ement Thi ckness 0. 2500 i n I nt er nal Cor r osi on Al l owance 0. 0000 i n Nomi nal Thi ckness 0. 2500 i n Ext ernal Cor r osi on Al l owance 0. 0000 i n

Desi gn I nt er nal Pressur e 100. 00 psi g Desi gn Temperatur e I nternal Pressure 300 F Desi gn Ext er nal Pressur e 0. 0000 psi g Desi gn Temperatur e Ext ernal Pressure 200 F Ef f ecti ve Di amet er Mul t i pl i er 1. 2 Mat er i al Name SA- 516 70 Ef f i ci ency, Longi t udi nal Seam 0. 7 Ef f i ci ency, Ci r cumf er ent i al Seam 0. 7

El ement Fr om Node 20 Det ai l Type Li qui d Detai l I D WATER Di st . f r om "FROM" Node / Of f set di st 0. 0000 i n

Hei ght / Lengt h of Li qui d 30. 000 i n Densi t y of Li qui d 62. 400 l bm/ f t 3̂

El ement Fr om Node 20 Det ai l Type Nozzl e Detai l I D Noz N3, N2 Di st . f r om "FROM" Node / Of f set di st 5. 0000 i n Nozzl e Di amet er 3. i n. Nozzl e Schedul e None Nozzl e Cl ass 0 Layout Angl e 270. Bl i nd Fl ange ( Y/ N) N Wei ght of Nozzl e ( Used i f > 0 ) 0. 0000 l bf

Gr ade of At t ached Fl ange None Nozzl e Mat l SA- 105

El ement Fr om Node 20 Det ai l Type Nozzl e Detai l I D Noz N5, N6 Di st . f r om "FROM" Node / Of f set di st 5. 0000 i n Nozzl e Di amet er 2. i n. Nozzl e Schedul e 80 Nozzl e Cl ass 150 Layout Angl e 0. Bl i nd Fl ange ( Y/ N) N Wei ght of Nozzl e ( Used i f > 0 ) 0. 0000 l bf

Gr ade of At t ached Fl ange GR 1. 1 Nozzl e Mat l SA- 106 B

El ement Fr om Node 20 Det ai l Type Leg Det ai l I D LEGS Di st . f r om "FROM" Node / Of f set di st 4. 0000 i n Di ameter at Leg Cent erl i ne 17. 184 i n Leg Or i ent at i on 1 Number of Legs 3 Sect i on I dent i f i er L2X2X0. 2500 Length of Legs 15. 500 i n

El ement Fr om Node 30 El ement To Node 40 El ement Type El l i pt i cal Descr i pt i on Top Head Di st ance "FROM" t o "TO" 1. 5000 i n El ement Outsi de Di ameter 16. 000 i n


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El ement Thi ckness 0. 2250 i n I nt er nal Cor r osi on Al l owance 0. 0000 i n Nomi nal Thi ckness 0. 2500 i n Ext ernal Cor r osi on Al l owance 0. 0000 i n Desi gn I nt er nal Pressur e 100. 00 psi g

Desi gn Temperatur e I nternal Pressure 300 F Desi gn Ext er nal Pressur e 0. 0000 psi g Desi gn Temperatur e Ext ernal Pressure 200 F Ef f ecti ve Di amet er Mul t i pl i er 1. 2 Mat er i al Name SA- 516 70 Ef f i ci ency, Longi t udi nal Seam 0. 85 Ef f i ci ency, Ci r cumf er ent i al Seam 0. 7 El l i pt i cal Head Factor 2.

El ement Fr om Node 30 Det ai l Type Li qui d Detai l I D WATER Di st . f r om "FROM" Node / Of f set di st 0. 0000 i n

Hei ght / Lengt h of Li qui d 5. 5000 i n Densi t y of Li qui d 62. 400 l bm/ f t 3̂

El ement Fr om Node 30 Det ai l Type Nozzl e Detai l I D Noz N1 Di st . f r om "FROM" Node / Of f set di st 0. 0000 i n Nozzl e Di amet er 2. 5 i n. Nozzl e Schedul e None Nozzl e Cl ass 0 Layout Angl e 0. Bl i nd Fl ange ( Y/ N) N Wei ght of Nozzl e ( Used i f > 0 ) 0. 0000 l bf

Gr ade of At t ached Fl ange None Nozzl e Mat l SA- 105



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XY Coordinate Calculations Step: 2 5:25p Sep 15,2008

XY Coordinate Calculations

| | | | | | Fr om| To | X ( Hori z. ) | Y ( Ver t . ) | DX ( Hor i z. ) | DY ( Ver t . ) |

| | i n | i n | i n | i n | Bot t om Hea| 0. 00000 | 1. 50000 | 0. 00000 | 1. 50000 | Shel l | 0. 00000 | 31. 5000 | 0. 00000 | 30. 0000 | Top Head| 0. 00000 | 33. 0000 | 0. 00000 | 1. 50000 |



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Internal Pressure Calculations Step: 3 5:25p Sep 15,2008

Element Thickness, Pressure, Diameter and Allowable Stress :

| | I nt . Pr ess | Nomi nal | Tot al Cor r | El ement | Al l owabl e | Fr om| To | + Li q. Hd | Thi ckness | Al l owance | Di ameter | St r ess( SE) |

| | psi g | i n | i n | i n | psi | Bot t om Hea| 101. 481 | 0. 25000 | 0. 00000 | 16. 0000 | 17000. 0 | Shel l | 101. 282 | 0. 25000 | 0. 00000 | 16. 0000 | 14000. 0 | Top Head| 100. 199 | 0. 25000 | 0. 00000 | 16. 0000 | 17000. 0 |

Element Required Thickness and MAWP :

| | Desi gn | M. A. W. P. | M. A. P. | Act ual | Requi r ed | Fr om| To | Pressure | Cor r oded | New & Col d | Thi ckness | Thi ckness | | | ps i g | psi g | ps i g | i n | i n | Bot t om Hea| 100. 000 | 489. 061 | 490. 542 | 0. 22500 | 0. 062500 | Shel l | 100. 000 | 441. 756 | 443. 038 | 0. 25000 | 0. 062500 | Top Head| 100. 000 | 490. 397 | 490. 542 | 0. 22500 | 0. 062500 |

Mi ni mum 228. 899 285. 000

Not e : The M. A. W. P i s Gover ned by an ANSI Fl ange !

Flange MAWP including Static Pressure: 228.899 = 230.000 - 1.101 psig

Note : The M. A. P. ( NC) i s Governed by a Fl ange !

Internal Pressure Calculation Results :

ASME Code, Section VIII, Division 1, 2007

Elliptical Head From 10 To 20 SA-516 70 , UCS-66 Crv. B at 300 F

Bottom Head

Thickness Due to Internal Pressure [Tr]: = ( P*Do*K) / ( 2*S*E+2*P*( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 101. 481*16. 0000*1. 00) / ( 2*20000. 00*0. 85+2*101. 481*( 1. 00- 0. 1) ) = 0. 0475 + 0. 0000 = 0. 0475 i n

Note: The thickness required was less than the Code Minimum, thereforethe Code Minimum value of 0.0625 in will be used.

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:Less Operating Hydrostatic Head Pressure of 1.481 psig

= ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 2*20000. 00*0. 85*0. 2250) / ( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) = 490. 542 - 1. 481 = 489. 061 psi g

Maximum Allowable Pressure, New and Cold [MAPNC]: = ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 2*20000. 00*0. 85*0. 2250) / ( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) = 490. 542 psi g

Actual stress at given pressure and thickness, corroded [Sact]: = ( P*( K*Do- 2*T*( K- 0. 1) ) ) / ( 2*E*t ) = ( 101. 481*( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) ) / ( 2*0. 85*0. 2250) = 4137. 488 psi

Required Thickness of Straight Flange = 0.048 in

Per cent El ongat i on per UCS- 79 ( 75*t nom/ Rf ) *( 1- Rf / Ro) 7. 003 %

Mi n Met al Temp. w/ o i mpact per UCS- 66 - 20 F


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Mi n Metal Temp. at Rqd t hi ckness ( UCS 66. 1) [ r at 0. 24] - 155 F

Cylindrical Shell From 20 To 30 SA-516 70 , UCS-66 Crv. B at 300 F

Shell

Thickness Due to Internal Pressure [Tr]: = ( P*Ro) / ( S*E+0. 4*P) per Appendi x 1- 1 ( a) ( 1) = ( 101. 282*8. 0000) / ( 20000. 00*0. 70+0. 4*101. 282) = 0. 0577 + 0. 0000 = 0. 0577 i n



= ( S*E*t ) / ( Ro- 0. 4*t ) per Appendi x 1- 1 ( a) ( 1) = ( 20000. 00*0. 70*0. 2500) / ( 8. 0000- 0. 4*0. 2500)

= 443. 038 - 1. 282 = 441. 756 psi g

Maximum Allowable Pressure, New and Cold [MAPNC]: = ( S*E*t ) / ( Ro- 0. 4*t ) per Appendi x 1- 1 ( a) ( 1) = ( 20000. 00*0. 70*0. 2500) / ( 8. 0000- 0. 4*0. 2500) = 443. 038 psi g

Actual stress at given pressure and thickness, corroded [Sact]: = ( P*( Ro- 0. 4*t) ) / ( E*t ) = ( 101. 282*( ( 8. 0000- 0. 4*0. 2500) ) / ( 0. 70*0. 2500) = 4572. 156 psi


Mi n Met al Temp. w/ o i mpact per UCS- 66 - 20 F Mi n Metal Temp. at Rqd t hi ckness ( UCS 66. 1) [ r at 0. 20] - 155 F

Elliptical Head From 30 To 40 SA-516 70 , UCS-66 Crv. B at 300 F

Top Head

Thickness Due to Internal Pressure [Tr]: = ( P*Do*K) / ( 2*S*E+2*P*( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 100. 144*16. 0000*1. 00) / ( 2*20000. 00*0. 85+2*100. 144*( 1. 00- 0. 1) ) = 0. 0469 + 0. 0000 = 0. 0469 i n



= ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 2*20000. 00*0. 85*0. 2250) / ( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) = 490. 542 - 0. 144 = 490. 397 psi g

Maximum Allowable Pressure, New and Cold [MAPNC]: = ( 2*S*E*t ) / ( K*Do- 2*t *( K- 0. 1) ) per Appendi x 1- 4 ( c) = ( 2*20000. 00*0. 85*0. 2250) / ( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) = 490. 542 psi g

Actual stress at given pressure and thickness, corroded [Sact]: = ( P*( K*Do- 2*T*( K- 0. 1) ) ) / ( 2*E*t ) = ( 100. 144*( 1. 00*16. 0000- 2*0. 2250*( 1. 00- 0. 1) ) ) / ( 2*0. 85*0. 2250) = 4083. 013 psi


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Required Thickness of Straight Flange = 0.047 in


Mi n Met al Temp. w/ o i mpact per UCS- 66 - 20 F

Mi n Metal Temp. at Rqd t hi ckness ( UCS 66. 1) [ r at 0. 24] - 155 F

MINIMUM METAL DESIGN TEMPERATURE RESULTS :

Mi ni mum Met al Temp. w/ o i mpact per UCS- 66 - 20. F Mi ni mum Metal Temp. at Requi r ed t hi ckness - 155. F

Note: Heads and Shells Exempted to -20F (-29C) by paragraph UG-20F

Mi ni mum Desi gn Metal Temperatur e ( Ent ered by User ) - 20. F

Hydrostatic Test Pressure Results:

Pr essur e per UG99b = 1. 3 * M. A. W. P. * Sa/ S 297. 568 psi g Pressure per UG99b[34] = 1. 3 * Desi gn Pres * Sa/ S 130. 000 psi g Pressure per UG99c = 1. 3 * M. A. P. - Head(Hyd) 370. 500 psi g Pr essur e per UG100 = 1. 1 * M. A. W. P. * Sa/ S 251. 788 psi g

UG-99(b) Note 34, Test Pressure Calculation: = Test Fact or * Desi gn Pressure * St r ess Rati o = 1. 3 * 100. 000 * 1. 000 = 130. 000 psi g

Vertical Hydrotest performed in accordance with: UG-99b (Note 34)

Stresses on Elements due to Hydrostatic Test Pressure:

From To St r ess Al l owabl e Rat i o Pressur e Bot t om Head 5360. 3 34200. 0 0. 157 131. 47 Shel l 5926. 3 34200. 0 0. 173 131. 28 Top Head 5308. 2 34200. 0 0. 155 130. 19

Elements Suitable for Internal Pressure.



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External Pressure Calculations Step: 4 5:26p Sep 15,2008

External Pressure Calculation Results :

ASME Code, Section VIII, Division 1, 2007

Elliptical Head From 10 to 20 Ext. Chart: CS-2 at 200 F

Bottom Head

Elastic Modulus from Chart: CS-2 at 300 F : 0.29000E+08 psi

Results for Maximum Allowable External Pressure (MAEP): Tca OD D/ t Fact or A B 0. 225 16. 00 71. 11 0. 0019531 14970. 13 EMAP = B/ ( K0*D/ t ) = 14970. 1309/ ( 0. 9000 *71. 1111 ) = 233. 9083 psi g

Cylindrical Shell From 20 to 30 Ext. Chart: CS-2 at 200 F

Shell


Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/ t L/ D Fact or A B 0. 250 16. 00 35. 59 64. 00 2. 2245 0. 0011710 13053. 81 EMAP = ( 4*B) / ( 3*( D/ t ) ) = ( 4*13053. 8066) / ( 3*64. 0000 ) = 271. 9543 psi g

Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/ t L/ D Fact or A B 0. 250 16. 00 0. 90E+32 64. 00 . 5000E+02 0. 0002686 3894. 04 EMAP = ( 4*B) / ( 3*( D/ t ) ) = ( 4*3894. 0430 ) / ( 3*64. 0000 ) = 81. 1259 psi g

Elliptical Head From 30 to 40 Ext. Chart: CS-2 at 200 F

Top Head


Results for Maximum Allowable External Pressure (MAEP): Tca OD D/ t Fact or A B 0. 225 16. 00 71. 11 0. 0019531 14970. 13 EMAP = B/ ( K0*D/ t ) = 14970. 1309/ ( 0. 9000 *71. 1111 ) = 233. 9083 psi g

External Pressure Calculations

| | Sect i on | Out si de | Cor r oded | Fact or | Fact or | Fr om| To | Lengt h | Di ameter | Thi ckness | A | B | | | i n | i n | i n | | psi | 10| 20| No Cal c | 16. 0000 | 0. 22500 | 0. 0019531 | 14970. 1 | 20| 30| 35. 5917 | 16. 0000 | 0. 25000 | 0. 0011710 | 13053. 8 | 30| 40| No Cal c | 16. 0000 | 0. 22500 | 0. 0019531 | 14970. 1 |


| | Ext ernal | Ext er nal | Ext er nal | Ext er nal | From| To | Act ual T. | Requi r ed T. | Des. Pr ess. | M. A. W. P. | | | i n | i n | ps i g | ps i g |

10| 20| 0. 22500 | No Cal c | 0. 00000 | 233. 908 | 20| 30| 0. 25000 | No Cal c | 0. 00000 | 271. 954 | 30| 40| 0. 22500 | No Cal c | 0. 00000 | 233. 908 | Mi ni mum 233. 908



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Element and Detail Weights Step: 5 5:26p Sep 15,2008

Element and Detail Weights

| | El ement | El ement | Corr oded | Corr oded | Ext r a due | Fr om| To | Metal Wgt . | I D Vol ume | Metal Wgt . | I D Vol ume | Mi sc % |

| | l bf | gal | l bf | gal | l bf | 10| 20| 26. 4066 | 3. 36386 | 26. 4066 | 3. 36386 | 0. 00000 | 20| 30| 105. 021 | 24. 5054 | 105. 021 | 24. 5054 | 0. 00000 | 30| 40| 26. 4066 | 3. 36386 | 26. 4066 | 3. 36386 | 0. 00000 | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Total 157 31 157 31 0

Weight of Details

| | Wei ght of | X Of f set , | Y Of f set , | From| Type| Det ai l | Dt l . Cent . | Dt l . Cent . | Descri pt i on | | l bf | i n | i n | 10| Li qd| 29. 2713 | 0. 00000 | - 2. 00000 | WATER

10| Nozl | 0. 14670 | 0. 00000 | 0. 32396 | Noz N4 20| Li qd| 204. 416 | 0. 00000 | 15. 0000 | WATER 20| Nozl | 0. 18667 | 9. 25000 | 5. 00000 | Noz N3, N2 20| Nozl | 7. 91375 | 8. 75000 | 5. 00000 | Noz N5, N6 20| Legs| 12. 3436 | 0. 00000 | - 3. 75000 | LEGS 30| Li qd| 28. 0187 | 0. 00000 | 2. 00000 | WATER 30| Nozl | 0. 14670 | 0. 00000 | 0. 32396 | Noz N1

Total Weight of Each Detail Type

Tot al Wei ght of Li qui d 261. 7 Tot al Wei ght of Nozzl es 8. 4 Tot al Wei ght of Legs 12. 3

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Sum of t he Det ai l Wei ght s 282. 4 l bf

Weight Summary

Fabr i cat ed Wt . - Bare Wei ght W/ O Removabl e I nternal s 178. 6 l bf Shop Test Wt . - Fabr i cat ed Wei ght + Wat er ( Ful l ) 439. 1 l bf Shi ppi ng Wt . - Fab. Wt + Rem. I nt l s. + Shi ppi ng App. 178. 6 l bf Er ect ed Wt . - Fab. Wt + Rem. I nt l s. + I nsul . ( et c) 178. 6 l bf Ope. Wt . no Li q - Fab. Wt + I nt l s. + Detai l s + Wght s. 178. 6 l bf Oper at i ng Wt . - Empty Wt . + Oper at i ng Li qui d ( No CA) 440. 3 l bf Fi el d Test Wt . - Empt y Wei ght + Wat er ( Ful l ) 439. 1 l bf Mass of t he Upper 1/ 3 of t he Vert i cal Vessel 152. 6 l bf

Outside Surface Areas of Elements

| | Sur f ace | Fr om| To | Ar ea | | | i n 2̂ | 10| 20| 354. 871 | 20| 30| 1507. 96 | 30| 40| 354. 871 | - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Tot al 2217. 707 i n 2̂ [ 15. 4 Squar e Feet ]

Element and Detail Weights

| To | Tot al El e. | Tot al . El e. | Tota l . El e. | Tot al Dt l . | Oper. Wgt . | Fr om| To | Empty Wgt . | Oper . Wgt . | Hydr o. Wgt . | Of f set Mom. | No Li qui d | | | l bm | l bm | l bm | i n- l b | l bm | 10| 20| 26. 5533 | 55. 8246 | 54. 6135 | 0. 00000 | 26. 5533 | 20| Legs| 15. 0829 | 42. 3384 | 42. 3384 | 9. 46293 | 15. 0829 |


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Element and Detail Weights Step: 5 5:26p Sep 15,2008

Legs| 30| 98. 0390 | 275. 200 | 275. 200 | 61. 5090 | 98. 0390 | 30| 40| 26. 5533 | 54. 5720 | 54. 6135 | 0. 00000 | 26. 5533 |

Cumulative Vessel Weight

| | Cumul at i ve Ope | Cumul at i ve | Cumul at i ve | Fr om| To | Wgt . No Li qui d | Oper. Wgt . | Hydr o. Wgt . | | | l bm | l bm | l bm | 10| 20| - 26. 5533 | - 55. 8246 | - 54. 6135 | 20| Legs| - 41. 6362 | - 98. 1630 | - 96. 9520 | Legs| 30| 124. 592 | 329. 772 | 329. 813 | 30| 40| 26. 5533 | 54. 5720 | 54. 6135 |

Note: The cumulative operating weights no liquid in the column aboveare the cumulative operating weights minus the operating liquidweight minus any weights absent in the empty condition.

Cumulative Vessel Moment

| | Cumul ati ve | Cumul at i ve | Cumul at i ve | Fr om| To | Empt y Mom. | Oper . Mom. | Hydr o. Mom. | | | i n- l b | i n- l b | i n- l b | 10| 20| 0. 00000 | 0. 00000 | 0. 00000 | 20| Legs| 9. 46293 | 9. 46293 | 9. 46293 | Legs| 30| 61. 5090 | 61. 5090 | 61. 5090 | 30| 40| 0. 00000 | 0. 00000 | 0. 00000 |



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18/47



Wind/Earthquake Shear, Bending Step: 8 5:26p Sep 15,2008

The following table is for the Operating Case.

Wind/Earthquake Shear, Bending

| | Di st ance t o| Cummul at i ve| Eart hquake | Wi nd | Eart hquake | Fr om| To | Suppor t | Wi nd Shear | Shear | Bendi ng | Bendi ng | | | i n | l bf | l bf | i n- l b | i n- l b | 10| 20| 4. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 20| Legs| 2. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | Legs| 30| 13. 0000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 30| 40| 26. 0000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |



19/47



Longitudinal Stress Constants Step: 9 5:26p Sep 15,2008

Longitudinal Stress Constants

| | Metal Ar ea | Metal Ar ea | New & Col d | Cor r oded | Fr om| To | New & Col d | Corr oded | Sect . Mod. | Sect . Mod. |

| | i n 2̂ | i n 2̂ | i n 3 | i n 3 | 10| 20| 11. 1507 | 11. 1507 | 43. 3659 | 43. 3659 | 20| 30| 12. 3700 | 12. 3700 | 47. 9580 | 47. 9580 | 30| 40| 11. 1507 | 11. 1507 | 43. 3659 | 43. 3659 |



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Longitudinal Stresses Due to . . . Step: 11 5:26p Sep 15,2008

Longitudinal Stress Report

Note: Longitudinal Operating and Empty Stresses are computed in thecorroded condition. Stresses due to loads in the hydrostatic test

cases have been computed in the new and cold condition.

Longitudinal Stresses Due to . . .

| | Long. St r . | Long. St r . | Long. Str . | From| To | I nt . Pr es. | Ext . Pr es. | Hyd. Pr es. | | | psi | psi | psi | 10| 20| 1707. 78 | 0. 00000 | 2220. 11 | 20| 30| 1530. 00 | 0. 00000 | 1989. 00 | 30| 40| 1707. 78 | 0. 00000 | 2220. 11 |


| | Wght . St r . | Wght . St r . | Wght . St r . | Wght . St r . | Wght . St r . | Fr om| To | Empty | Oper at i ng | Hydr ot est | Emp. Mom. | Opr. Mom. | | | psi | psi | psi | psi | psi | 10| 20| 2. 38131 | 5. 00638 | 4. 89777 | 0. 00000 | 0. 00000 | 20| Legs| 3. 36590 | 7. 93556 | 7. 83765 | 0. 19732 | 0. 19732 | Legs| 30| - 10. 0721 | - 26. 6589 | - 26. 6623 | 1. 28256 | 1. 28256 | 30| 40| - 2. 38131 | - 4. 89405 | - 4. 89777 | 0. 00000 | 0. 00000 |


| | Wght . St r . | Bend. St r . | Bend. St r . | Bend. St r . | Bend. St r . | Fr om| To | Hyd. Mom. | Oper . Wi nd | Oper . Equ. | Hyd. Wi nd | Hyd. Equ. | | | psi | psi | psi | psi | psi |

10| 20| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 20| Legs| 0. 19732 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | Legs| 30| 1. 28256 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 30| 40| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |


| | Long. St r . | Long. St r . | Long. St r . | Ear t hQuake | Fr om| To | Vor t ex Ope. | Vort ex Emp. | Vort ex Tst . | Empt y | | | psi | psi | psi | psi | 10| 20| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 20| Legs| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | Legs| 30| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |

30| 40| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |


| | Long. St r . | Long. St r . | Fr om| To | Y For ces W | Y For ceS S | | | psi | psi | 10| 20| 0. 00000 | 0. 00000 | 20| Legs| 0. 00000 | 0. 00000 | Legs| 30| 0. 00000 | 0. 00000 | 30| 40| 0. 00000 | 0. 00000 |

Long. Stresses due to User Forces and Moments

| | Wi nd For / Mom| Eqk For / Mom| Wnd For / Mom| Eqk For / Mom| Fr om| To | Cor r oded | Corr oded | No Corr . | No Corr . | | | psi | psi | psi | psi | 10| 20| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 20| Legs| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |


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Longitudinal Stresses Due to . . . Step: 11 5:26p Sep 15,2008

Legs| 30| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 | 30| 40| 0. 00000 | 0. 00000 | 0. 00000 | 0. 00000 |



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Stress due to Combined Loads Step: 12 5:26p Sep 15,2008

Stress Combination Load Cases for Vertical Vessels:

Load Case Definition Key

I P = Longi t udi nal St r ess due t o I nt er nal Pr essur e EP = Longi t udi nal St r ess due t o External Pressur e HP = Longi t udi nal St r ess due to Hydr otest Pressur e NP = No Pr essure EW = Longi t udi nal St r ess due to Wei ght ( No Li qui d) OW = Longi t udi nal St r ess due t o Wei ght ( Operat i ng) HW = Longi t udi nal St r ess due to Wei ght ( Hydr ot est ) WI = Bendi ng St r ess due t o Wi nd Moment ( Operat i ng) EQ = Bendi ng St r ess due t o Ear t hquake Moment ( Operat i ng) EE = Bendi ng St r ess due t o Eart hquake Moment ( Empt y) HI = Bendi ng St r ess due t o Wi nd Moment ( Hydrot est ) HE = Bendi ng St r ess due t o Ear t hquake Moment ( Hydrot est ) WE = Bendi ng St r ess due t o Wi nd Moment ( Empt y) ( no CA)

WF = Bendi ng St r ess due t o Wi nd Moment ( Fi l l ed) ( no CA) CW = Longi t udi nal St r ess due t o Wei ght ( Empty) ( no CA) VO = Bendi ng St r ess due t o Vor t ex Sheddi ng Loads ( Ope ) VE = Bendi ng St r ess due t o Vor t ex Sheddi ng Loads ( Emp ) VF = Bendi ng St r ess due to Vor t ex Sheddi ng Loads ( Test No CA. ) FW = Axi al St r ess due t o Ver t i cal For ces f or t he Wi nd Case FS = Axi al St r ess due t o Ver t i cal For ces f or t he Sei smi c Case BW = Bendi ng St r ess due to Lat . Forces f or t he Wi nd Case, Corr oded BS = Bendi ng St r ess due to Lat . Forces f or t he Sei smi c Case, Cor r oded BN = Bendi ng St r ess due t o Lat . Forces f or t he Wi nd Case, UnCor r oded BU = Bendi ng St r ess due t o Lat . Forces f or t he Sei smi c Case, UnCorr oded

General Notes:

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

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

A blank stress and stress ratio indicates that the correspondingstress comprising those components that did not contribute to thattype of stress.

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

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

Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 2. 38 16800. 00 - 19938. 30 0. 0001 20 3. 56 16800. 00 - 20216. 65 0. 0002 20 16800. 00 - 11. 35 - 20216. 65 0. 0006 30 16800. 00 - 2. 38 - 19938. 30 0. 0001

Analysis of Load Case 2 : NP+EW+EE+FS+BS Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 2. 38 16800. 00 - 19938. 30 0. 0001 20 3. 56 16800. 00 - 20216. 65 0. 0002 20 16800. 00 - 11. 35 - 20216. 65 0. 0006

30 16800. 00 - 2. 38 - 19938. 30 0. 0001

Analysis of Load Case 3 : NP+OW+WI+FW+BW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 5. 01 16800. 00 - 19938. 30 0. 0003


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10 2225. 01 28728. 00 - 24922. 88 0. 0775 20 1997. 03 28728. 00 - 25270. 81 0. 0695 20 2194. 73 28728. 00 - 25270. 81 0. 0764 30 28728. 00 - 4. 90 - 24922. 88 0. 0002

Analysis of Load Case 12 : HP+HW+HE Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 2225. 01 28728. 00 - 24922. 88 0. 0775 20 1997. 03 28728. 00 - 25270. 81 0. 0695 20 2194. 73 28728. 00 - 25270. 81 0. 0764 30 28728. 00 - 4. 90 - 24922. 88 0. 0002

Analysis of Load Case 13 : IP+WE+EW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 1710. 16 16800. 00 - 19938. 30 0. 1018 20 1533. 56 16800. 00 - 20216. 65 0. 0913

20 1698. 99 16800. 00 - 20216. 65 0. 1011 30 16800. 00 - 2. 38 - 19938. 30 0. 0001

Analysis of Load Case 14 : IP+WF+CW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 1712. 78 16800. 00 - 19938. 30 0. 1020 20 1537. 94 16800. 00 - 20216. 65 0. 0915 20 1681. 12 16800. 00 - 20216. 65 0. 1001 30 16800. 00 - 4. 89 - 19938. 30 0. 0002

Analysis of Load Case 15 : IP+VO+OW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp.

Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 1712. 78 16800. 00 - 19938. 30 0. 1020 20 1538. 13 16800. 00 - 20216. 65 0. 0916 20 1682. 40 16800. 00 - 20216. 65 0. 1001 30 16800. 00 - 4. 89 - 19938. 30 0. 0002

Analysis of Load Case 16 : IP+VE+EW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 1710. 16 16800. 00 - 19938. 30 0. 1018 20 1533. 56 16800. 00 - 20216. 65 0. 0913 20 1698. 99 16800. 00 - 20216. 65 0. 1011 30 16800. 00 - 2. 38 - 19938. 30 0. 0001

Analysis of Load Case 17 : NP+VO+OW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 5. 01 16800. 00 - 19938. 30 0. 0003 20 8. 13 16800. 00 - 20216. 65 0. 0005 20 16800. 00 - 27. 94 - 20216. 65 0. 0014 30 16800. 00 - 4. 89 - 19938. 30 0. 0002

Analysis of Load Case 18 : FS+BS+IP+OW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp. Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 1712. 78 16800. 00 - 19938. 30 0. 1020

20 1538. 13 16800. 00 - 20216. 65 0. 0916 20 1682. 40 16800. 00 - 20216. 65 0. 1001 30 16800. 00 - 4. 89 - 19938. 30 0. 0002

Analysis of Load Case 19 : FS+BS+EP+OW Fr om Tensi l e Al l . Tens. Comp. Al l . Comp. Tens. Comp.


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Node St r ess St r ess St r ess St r ess Rat i o Rat i o 10 5. 01 16800. 00 - 19938. 30 0. 0003 20 8. 13 16800. 00 - 20216. 65 0. 0005 20 16800. 00 - 27. 94 - 20216. 65 0. 0014 30 16800. 00 - 4. 89 - 19938. 30 0. 0002

Absol ut e Maxi mum of t he al l of t he St r ess Rat i o' s 0. 1020

Governing Element: Bottom HeadGoverning Load Case 7 : IP+OW+WI+FW+BW



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Center of Gravity Calculation Step: 13 5:26p Sep 15,2008

Shop/Field Installation Options :

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

Cent er of Gr avi t y of Li qui d 16. 3 i n Cent er of Gr avi t y of Nozzl es 6. 8 i n Cent er of Gr avi t y of Legs - 2. 2 i n

Cent er of Gr avi t y of Bare Shel l New and Col d 16. 8 i n Cent er of Gr avi t y of Bar e Shel l Cor r oded 16. 8 i n

Vessel CG i n t he Operat i ng Condi t i on 15. 7 i n Vessel CG i n t he Fabr i cated ( Shop/ Empt y) Condi t i on 15. 0 i n



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Leg Check, (Operating Case) Step: 14 5:26p Sep 15,2008

RESULTS FOR LEGS : Operating Case Description: LEGS

Legs attached to: Shell

Section Properties : Single Angle L2X2X0.2500

USA AISC 1989 Steel Table

Over al l Leg Lengt h 15. 500 i n Ef f ect i ve Leg Lengt h Legl en 15. 500 i n Di st ance Leg Up Si de of Vessel 4. 000 i n Number of Legs Nl eg 3 Cr oss Sect i onal Ar ea f or L2X2X0. 2500 Al eg 0. 938 i n 2̂ Secti on I ner t i a ( st r ong axi s ) 0. 348 i n**4 Sect i on I ner t i a ( weak axi s ) 0. 348 i n**4 Secti on Modul us ( st r ong axi s ) 0. 247 i n (̂ 3) Sect i on Modul us ( weak axi s ) 0. 247 i n (̂ 3)

Radi us of Gyrati on ( st r ong axi s ) 0. 609 i n Radi us of Gyrat i on ( weak axi s ) 0. 609 i n

Leg Orientation - Strong Axis

Over t ur ni ng Moment at t op of Legs 0. 0 i n- l b Tot al Wei ght Load at t op of Legs W 427. 9 l bf Tot al Shear f or ce at t op of Legs 0. 0 l bf Addi t i onal f or ce i n Leg due t o Br aci ng Fadd 0. 0 l bf Occasi onal Load Factor Occf ac 1. 000 Ef f ect i ve Leg End Condi t i on Fact or k 1. 000

Note: The Legs are Not Cross Braced

The Leg Shear Force includes Wind and Seismic Effects

Maximum Shear at top of one Leg [Vleg]: = ( Max( Wi nd, Sei smi c) + Fadd ) * ( I max / I t ot ) = ( 0. 0 + 0. 0 ) * ( 0. 3 / 1. 04 ) = 0. 00 l bf

Axial Compression, Leg futhest from N.A. [Sma] = ( ( W/ Nl eg) +( Ml eg/ ( Nl egm*Rn) ) ) / Al eg) = ( ( 427 / 3 ) + ( 0 / ( 1 * 9. 41 ) ) ) / 0. 938 ) = 152. 07 psi

Axial Compression, Leg closest to N.A. [Sva]

= ( W / Nl eg ) / Al eg = ( 427 / 3 ) / 0. 938 = 152. 07 psi

Comput i ng Pri nci pal Axi s and I ner t i as f or Angl e. Leg l engths and t hi ckness: 2. 0000 2. 0000 0. 25000 Di st ance t o geometr i c cent r oi d: 0. 59200 0. 59200 Ar m about YY: 0. 46700 0. 53300 Ar m about ZZ: 0. 40800 0. 46700 Leg areas: 0. 50000 0. 43750 Geomet r i c i ner t i a component s YY: 0. 11165 0. 23594 Geomet r i c i ner t i a component s ZZ: 0. 24990 0. 97693E- 01 Geomet r i c i ner t i as I y & I z: 0. 34759 0. 34759

Pr oduct of i ner t i a: 0. 20417 Mohr s Radi us: 0. 20417 Aver age I ner t i a: 0. 34759

QFACT = 1. 0000 FBZ = 23. 760 Pr i nci pal Axi s I nert i as ( Z&W) = 0. 14342 0. 55176


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Leg Check, (Filled w/Water) Step: 15 5:26p Sep 15,2008

RESULTS FOR LEGS : HydroTest Case Description: LEGS

Legs attached to: Shell

Section Properties : Single Angle L2X2X0.2500

USA AISC 1989 Steel Table

Over al l Leg Lengt h 15. 500 i n Ef f ect i ve Leg Lengt h Legl en 15. 500 i n Di st ance Leg Up Si de of Vessel 4. 000 i n Number of Legs Nl eg 3 Cr oss Sect i onal Ar ea f or L2X2X0. 2500 Al eg 0. 938 i n 2̂ Secti on I ner t i a ( st r ong axi s ) 0. 348 i n**4 Sect i on I ner t i a ( weak axi s ) 0. 348 i n**4 Secti on Modul us ( st r ong axi s ) 0. 247 i n (̂ 3) Sect i on Modul us ( weak axi s ) 0. 247 i n (̂ 3)

Radi us of Gyrati on ( st r ong axi s ) 0. 609 i n Radi us of Gyrat i on ( weak axi s ) 0. 609 i n

Leg Orientation - Strong Axis

Over t ur ni ng Moment at t op of Legs 0. 0 i n- l b Tot al Wei ght Load at t op of Legs W 426. 8 l bf Tot al Shear f or ce at t op of Legs 0. 0 l bf Addi t i onal f or ce i n Leg due t o Br aci ng Fadd 0. 0 l bf Occasi onal Load Factor Occf ac 1. 000 Ef f ect i ve Leg End Condi t i on Fact or k 1. 000

Note: The Legs are Not Cross Braced

The Leg Shear Force includes Wind and Seismic Effects

Maximum Shear at top of one Leg [Vleg]: = ( Max( Wi nd, Sei smi c) + Fadd ) * ( I max / I t ot ) = ( 0. 0 + 0. 0 ) * ( 0. 3 / 1. 04 ) = 0. 00 l bf

Axial Compression, Leg futhest from N.A. [Sma] = ( ( W/ Nl eg) +( Ml eg/ ( Nl egm*Rn) ) ) / Al eg) = ( ( 426 / 3 ) + ( 0 / ( 1 * 9. 41 ) ) ) / 0. 938 ) = 151. 66 psi

Axial Compression, Leg closest to N.A. [Sva]

= ( W / Nl eg ) / Al eg = ( 426 / 3 ) / 0. 938 = 151. 66 psi

Comput i ng Pri nci pal Axi s and I ner t i as f or Angl e. Leg l engths and t hi ckness: 2. 0000 2. 0000 0. 25000 Di st ance t o geometr i c cent r oi d: 0. 59200 0. 59200 Ar m about YY: 0. 46700 0. 53300 Ar m about ZZ: 0. 40800 0. 46700 Leg areas: 0. 50000 0. 43750 Geomet r i c i ner t i a component s YY: 0. 11165 0. 23594 Geomet r i c i ner t i a component s ZZ: 0. 24990 0. 97693E- 01 Geomet r i c i ner t i as I y & I z: 0. 34759 0. 34759

Pr oduct of i ner t i a: 0. 20417 Mohr s Radi us: 0. 20417 Aver age I ner t i a: 0. 34759

QFACT = 1. 0000 FBZ = 23. 760 Pr i nci pal Axi s I nert i as ( Z&W) = 0. 14342 0. 55176


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Leg Check, (Filled w/Water) Step: 15 5:26p Sep 15,2008

Angl e t o Pri nci pal Axi s = 45. 000 Di st ances t o ext r eme f i ber s CW & CZ = 1. 4142 0. 57700 FOB f r om Eq 5- 5 = 455. 65 Bendi ng al l owabl es Fby & Fbz = 23. 760 23. 760

Shear Cent er Coordi nates Wo & Zo: 0. 63728 0. 0000 Val ues f or El ast i c Fl exur al - Tor si onal Buckl i ng St r ess: E, G, J , R0 (̂ 2) : 29500. 11346. 0. 19542E- 01 1. 1473 AREA, LENGTH, Kw, Kz: 0. 93800 15. 500 1. 0000 1. 0000 H, Few, Fez, Fej : 0. 64600 712. 86 185. 30 206. 04 Fe comput ed f r om C4- 1: 183. 52

I ni t i al ( Kl / r ) max, & ( Kl / r ) equi v = 39. 639 39. 831 Fi nal ( Kl / r ) max, & Cc = 39. 831 127. 18 Fa based on Eq 4- 1 = 19. 230

Act ual Al l owabl e Weak Axi s Bendi ng : 0. 00 23760. 00 psi

St r ong Axi s Bendi ng : 0. 00 23760. 00 psi Axi al Compressi on : 151. 66 19229. 93 psi

UNI TY CHECKS ARE: H1- 1 0. 000 H1- 2 0. 000 H1- 3 0. 008

AI SC Uni t y Check : 0. 008 Shoul d be


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Nozzle Calcs. Noz N4 Nozl: 1 5:26p Sep 15,2008

INPUT VALUES, Nozzle Description: Noz N4 From : 10

Pressur e f or Nozzl e Rei nf orcement Cal cul at i ons P 101. 481 psi g Temperatur e f or I nternal Pressure Temp 300 F

Shel l Mat er i al SA- 516 70 Shel l Al l owabl e St r ess at Temperatur e S 20000. 00 psi Shel l Al l owabl e St r ess At Ambi ent Sa 20000. 00 psi

I nsi de Di amet er of El l i pt i cal Head D 15. 5500 i n Aspect Rat i o of El l i pt i cal Head Ar 2. 00 Head Act ual Thi ckness T 0. 2250 i n Head I nt er nal Corr osi on Al l owance Cas 0. 0000 i n Head Ext ernal Cor r osi on Al l owance Caext 0. 0000 i n

Di st ance f r om Head Cent er l i ne L1 0. 0000 i n

User Ent ered Mi ni mum Desi gn Metal Temper at ure - 20. 00 F

Nozzl e Mat eri al SA- 105 Nozzl e Al l owabl e Str ess at Temper ature Sn 20000. 00 psi Nozzl e Al l owabl e Str ess At Ambi ent Sna 20000. 00 psi

Nozzl e Di amet er Basi s ( f or t r cal c onl y) I nbase OD Layout Angl e 0. 00 deg Nozzl e Di ameter Di a 2. 5000 i n.

Nozzl e Si ze and Thi ckness Basi s I dbn Act ual Act ual Thi ckness of Nozzl e Thk 0. 3000 i n

Nozzl e Corr osi on Al l owance Can 0. 0000 i n J oi nt Ef f i ci ency of Shel l Seam at Nozzl e Es 1. 00 J oi nt Ef f i ci ency of Nozzl e Neck En 1. 00

Nozzl e Out si de Proj ect i on Ho 0. 2500 i n Wel d l eg si ze bet ween Nozzl e and Pad/ Shel l Wo 0. 2500 i n Gr oove wel d dept h bet ween Nozzl e and Vessel Wgnv 0. 2250 i n Nozzl e I nsi de Pr oj ect i on H 0. 0000 i n Wel d l eg si ze, I nsi de Nozzl e t o Shel l Wi 0. 0000 i n ASME Code Wel d Type per UW- 16 C

The Pressure Design option was Design Pressure + static head

Nozzle Sketch

| | | | | | | | ____________/| | | \ | | | \ | | | ____________\ | __ |

Insert Nozzle No Pad, no Inside projection

NOZZLE CALCULATION, Description: Noz N4

ASME Code, Section VIII, Division 1, 2007, UG-37 to UG-45

Act ual Nozzl e Out si de Di ameter Used i n Cal cul at i on 2. 500 i n.


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Wal l Thi ckness per UG45( b) , t r b = Mi n( t r b1, t r b4) = 0. 0625 i n

Fi nal Requi r ed Thi ckness, t r 45 = Max( t r a, tr b) = 0. 0625 i n Avai l abl e Nozzl e Neck Thi ckness = 0. 3000 i n - - > OK

M.A.W.P. Results for this Nozzle (Based on Areas and UG-45) at this Location Appr oxi mate M. A. W. P. f or gi ven geomet r y 470. 109 psi g

Note: The MAWP of this junction was limited by the Areas.

Minimum Design Metal Temperature (Nozzle Neck), Curve: B Mi ni mum Temp. w/ o i mpact per UCS- 66 - 20 F Mi ni mum Temp. at r equi r ed t hi ckness - 155 F

Nozzle MDMT Thickness Calc. per UCS-66 (a)1(b), MIN(tn,t,te), Curve: B Mi ni mum Temp. w/ o i mpact per UCS- 66 - 20 F Mi ni mum Temp. at r equi r ed t hi ckness - 155 F Mi ni mum Temp. w/ o i mpact per UG- 20( f ) - 20 F

Weld Size Calculations, Description: Noz N4

I nt er medi at e Cal c. f or nozzl e/ shel l Wel ds Tmi n 0. 2500 i n

Results Per UW-16.1: Requi r ed Thi ckness Act ual Thi ckness Nozzl e Wel d 0. 1750 = 0. 7 * TMI N 0. 1768 = 0. 7 * Wo i n

The Drop for this Nozzle is : 0.0552 inThe Cut Length for this Nozzle is, Drop + Ho + H + T : 0.5302 in



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Nozzle Calcs. Noz N3, N2 Nozl: 2 5:26p Sep 15,2008

INPUT VALUES, Nozzle Description: Noz N3, N2 From : 20



I nsi de Di amet er of Cyl i ndr i cal Shel l D 15. 5000 i n Shel l Act ual Thi ckness T 0. 2500 i n Shel l I nt er nal Cor r osi on Al l owance Cas 0. 0000 i n Shel l Exter nal Cor r osi on Al l owance Caext 0. 0000 i n

Di st ance f r omBot t om/ Lef t Tangent 6. 5000 i n





Nozzl e Corr osi on Al l owance Can 0. 0000 i n

J oi nt Ef f i ci ency of Shel l Seam at Nozzl e Es 1. 00 J oi nt Ef f i ci ency of Nozzl e Neck En 1. 00



Nozzle Sketch

| | | | | | | | ____________/| | | \ | | | \ | | | ____________\ | __ |


NOZZLE CALCULATION, Description: Noz N3, N2


Act ual Nozzl e Out si de Di ameter Used i n Cal cul at i on 3. 000 i n. Act ual Nozzl e Thi ckness Used i n Cal cul at i on 0. 312 i n.


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Nozzle input data check completed without errors.

Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press] = ( P*R) / ( S*E- 0. 6*P) per UG- 27 ( c) ( 1)

= ( 101. 10*7. 7500) / ( 20000*1. 00- 0. 6*101. 10) = 0. 0393 i n

Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press] = ( P*Ro) / ( S*E+0. 4*P) per Appendi x 1- 1 ( a) ( 1) = ( 101. 10*1. 5000) / ( 20000*1. 00+0. 4*101. 10) = 0. 0076 i n

UG-40, Thickness and Diameter Limit Results : [Int. Press] Ef f ecti ve mat er i al di amet er l i mi t , Dl 4. 7500 i n Ef f ect i ve mat er i al t hi ckness l i mi t , no pad Tl np 0. 6250 i n

Results of Nozzle Reinforcement Area Calculations:

AREA AVAI LABLE, A1 t o A5 Desi gn Exter nal Mapnc Ar ea Requi r ed Ar 0. 093 NA NA i n 2̂ Ar ea i n Shel l A1 0. 500 NA NA i n 2̂ Ar ea i n Nozzl e Wal l A2 0. 152 NA NA i n 2̂ Ar ea i n I nwar d Nozzl e A3 0. 000 NA NA i n 2̂ Ar ea i n Wel ds A4 0. 063 NA NA i n 2̂ Ar ea i n Pad A5 0. 000 NA NA i n 2̂ TOTAL AREA AVAI LABLE Atot 0. 715 NA NA i n 2̂

The Internal Pressure Case Governs the Analysis.

Nozzl e Angl e Used i n Ar ea Cal cul at i ons 90. 00 Degs.

The area available without a pad is Sufficient.

Reinforcement Area Required for Nozzle [Ar]: = ( Dl r *Tr+2*Thk*Tr *( 1- f r 1) ) UG- 37( c) = ( 2. 3750*0. 0393+2*( 0. 3125- 0. 0000) *0. 0393*( 1- 1. 0000) ) = 0. 093 i n 2̂

Areas per UG-37.1 but with DL = Diameter Limit, DLR = Corroded ID:

Area Available in Shell [A1]: = ( DL- Dl r ) *( ES*( T- Cas) - Tr ) - 2*( Thk-Can) *( ES*( T- Cas) - Tr ) *( 1- f r 1) = ( 4. 750- 2. 375) *( 1. 00*( 0. 2500- 0. 000) - 0. 039) - 2*( 0. 312- 0. 000) *( 1. 00*( 0. 2500- 0. 0000) - 0. 0393) *( 1- 1. 0000)

= 0. 500 i n 2̂

Area Available in Nozzle Wall, no Pad [A2np]: = ( 2 * mi n( Tl np, ho) ) * ( Thk - Can - Tr n ) * f r 2 = ( 2 * mi n( 0. 625 , 0. 250 ) ) * ( 0. 3125 - 0. 0000 - 0. 0076 ) * 1. 0000 ) = 0. 152 i n 2̂

Area Available in Welds, no Pad [A4np]: = Wo (̂ 2) * f r 2 + ( Wi - Can/ 0. 707 ) (̂ 2) * f r 2 = 0. 2500̂ ( 2) * 1. 0000 + ( 0. 0000 ) (̂ 2) * 1. 0000 = 0. 062 i n 2̂

UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]

Wal l Thi ckness per UG45( a) , t r a = 0. 0076 i n Wal l Thi ckness per UG16( b) , t r 16b = 0. 0625 i n Wal l Thi ckness per UG45( b) ( 1) , t r b1 = 0. 0393 i n Check UG16(b) Mi n. Thi ckness, t r b1 = Max( t r b1, t r 16b) = 0. 0625 i n Std. Wal l Pi pe per UG45( b) ( 4) , t r b4 = 0. 1890 i n Wal l Thi ckness per UG45( b) , t r b = Mi n( t r b1, t r b4) = 0. 0625 i n


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Fi nal Requi r ed Thi ckness, t r 45 = Max( t r a, t r b) = 0. 0625 i n Avai l abl e Nozzl e Neck Thi ckness = 0. 3125 i n - - > OK

M.A.W.P. Results for this Nozzle (Based on Areas and UG-45) at this Location

Appr oxi mate M. A. W. P. f or gi ven geomet r y 431. 344 psi g




Weld Size Calculations, Description: Noz N3, N2






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INPUT VALUES, Nozzle Description: Noz N5, N6 From : 20



I nsi de Di amet er of Cyl i ndr i cal Shel l D 15. 5000 i n Shel l Act ual Thi ckness T 0. 2500 i n Shel l I nt er nal Cor r osi on Al l owance Cas 0. 0000 i n Shel l Exter nal Cor r osi on Al l owance Caext 0. 0000 i n

Di st ance f r omBot t om/ Lef t Tangent 6. 5000 i n


Nozzl e Mat eri al SA- 106 B Nozzl e Al l owabl e Str ess at Temper ature Sn 17100. 00 psi Nozzl e Al l owabl e Str ess At Ambi ent Sna 17100. 00 psi

Nozzl e Di amet er Basi s ( f or t r cal c onl y) I nbase I D Layout Angl e 0. 00 deg Nozzl e Di ameter Di a 2. 0000 i n.

Nozzl e Si ze and Thi ckness Basi s I dbn Nomi nal Nomi nal Thi ckness of Nozzl e Thknom 80

Nozzl e Fl ange Materi al SA- 105

Nozzl e Fl ange Type Sl i p on



Cl ass of at t ached Fl ange 150 Gr ade of at t ached Fl ange GR 1. 1


Nozzle Sketch

| | | | | | | | ____________/| | | \ | |

| \ | | | ____________\ | __ |


NOZZLE CALCULATION, Description: Noz N5, N6


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Act ual Nozzl e I nsi de Di amet er Used i n Cal cul at i on 1. 939 i n. Act ual Nozzl e Thi ckness Used i n Cal cul at i on 0. 218 i n.

Nozzle input data check completed without errors.

Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press] = ( P*R) / ( S*E- 0. 6*P) per UG- 27 ( c) ( 1) = ( 101. 10*7. 7500) / ( 20000*1. 00- 0. 6*101. 10) = 0. 0393 i n

Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press] = ( P*R) / ( S*E- 0. 6*P) per UG- 27 ( c) ( 1) = ( 101. 10*0. 97) / ( 17100*1. 00- 0. 6*101. 10) = 0. 0058 i n

UG-40, Thickness and Diameter Limit Results : [Int. Press] Ef f ecti ve mat er i al di amet er l i mi t , Dl 3. 8780 i n Ef f ect i ve mat er i al t hi ckness l i mi t , no pad Tl np 0. 5450 i n

Results of Nozzle Reinforcement Area Calculations: AREA AVAI LABLE, A1 t o A5 Desi gn Exter nal Mapnc Ar ea Requi r ed Ar 0. 079 NA NA i n 2̂ Ar ea i n Shel l A1 0. 395 NA NA i n 2̂ Ar ea i n Nozzl e Wal l A2 0. 198 NA NA i n 2̂ Ar ea i n I nwar d Nozzl e A3 0. 000 NA NA i n 2̂ Ar ea i n Wel ds A4 0. 053 NA NA i n 2̂ Ar ea i n Pad A5 0. 000 NA NA i n 2̂ TOTAL AREA AVAI LABLE Atot 0. 646 NA NA i n 2̂

The Internal Pressure Case Governs the Analysis.

Nozzl e Angl e Used i n Ar ea Cal cul at i ons 90. 00 Degs.

The area available without a pad is Sufficient.

Reinforcement Area Required for Nozzle [Ar]: = ( Dl r *Tr+2*Thk*Tr *( 1- f r 1) ) UG- 37( c) = ( 1. 9390*0. 0393+2*( 0. 2180- 0. 0000) *0. 0393*( 1- 0. 8550) ) = 0. 079 i n 2̂

Areas per UG-37.1 but with DL = Diameter Limit, DLR = Corroded ID:

Area Available in Shell [A1]: = ( DL- Dl r ) *( ES*( T- Cas) - Tr ) - 2*( Thk-Can) *( ES*( T- Cas) - Tr ) *( 1- f r 1) = ( 3. 878- 1. 939) *( 1. 00*( 0. 2500- 0. 000) - 0. 039) - 2*( 0. 218- 0. 000) *( 1. 00*( 0. 2500- 0. 0000) - 0. 0393) *( 1- 0. 8550) = 0. 395 i n 2̂

Area Available in Nozzle Wall, no Pad [A2np]: = ( 2 * mi n( Tl np, ho) ) * ( Thk - Can - Tr n ) * f r 2 = ( 2 * mi n( 0. 545 , 6. 000 ) ) * ( 0. 2180 - 0. 0000 - 0. 0058 ) * 0. 8550 ) = 0. 198 i n 2̂

Area Available in Welds, no Pad [A4np]:

= Wo (̂ 2) * f r 2 + ( Wi - Can/ 0. 707 ) (̂ 2) * f r 2 = 0. 2500̂ ( 2) * 0. 8550 + ( 0. 0000 ) (̂ 2) * 0. 8550 = 0. 053 i n 2̂

UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.] Wal l Thi ckness per UG45( a) , t r a = 0. 0058 i n


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Wal l Thi ckness per UG16( b) , t r 16b = 0. 0625 i n Wal l Thi ckness per UG45( b) ( 1) , t r b1 = 0. 0393 i n Check UG16(b) Mi n. Thi ckness, t r b1 = Max( t r b1, t r 16b) = 0. 0625 i n Std. Wal l Pi pe per UG45( b) ( 4) , t r b4 = 0. 1347 i n Wal l Thi ckness per UG45( b) , t r b = Mi n( t r b1, t r b4) = 0. 0625 i n

Fi nal Requi r ed Thi ckness, t r 45 = Max( t r a, tr b) = 0. 0625 i n Avai l abl e Nozzl e Neck Thi ckness = . 875 * 0. 2180 = 0. 1908 i n - - > OK


Note: The MAWP of this junction was limited by the shell (minus static head).



ANSI Flange MDMT including temperature reduction per UCS-66.1: Unadj ust ed MDMT of ANSI B16. 5/ 47 f l anges per UCS- 66( c) - 20 F Fl ange MDMT wi t h Temper ature r educt i on per UCS- 66( b) ( 1) ( b) - 55 F

Where the Temperature Reduction per UCS-66(b)(1)(b) is: St r ess rat i o, P / Ambi ent Rati ng = 101. 10 / 285. 00 = 0. 355

Weld Size Calculations, Description: Noz N5, N6






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INPUT VALUES, Nozzle Description: Noz N1 From : 30



I nsi de Di amet er of El l i pt i cal Head D 15. 5500 i n Aspect Rat i o of El l i pt i cal Head Ar 2. 00 Head Act ual Thi ckness T 0. 2250 i n Head I nt er nal Corr osi on Al l owance Cas 0. 0000 i n Head Ext ernal Cor r osi on Al l owance Caext 0. 0000 i n

Di st ance f r om Head Cent er l i ne L1 0. 0000 i n








Nozzle Sketch

| | | | | | | | ____________/| | | \ | | | \ | | | ____________\ | __ |


NOZZLE CALCULATION, Description: Noz N1


Act ual Nozzl e Out si de Di ameter Used i n Cal cul at i on 2. 500 i n.


42/47


43/47




Wal l Thi ckness per UG45( b) , t r b = Mi n( t r b1, t r b4) = 0. 0625 i n

Fi nal Requi r ed Thi ckness, t r 45 = Max( t r a, tr b) = 0. 0625 i n Avai l abl e Nozzl e Neck Thi ckness = 0. 3000 i n - - > OK





ANSI Flange MDMT including temperature reduction per UCS-66.1: Unadj ust ed MDMT of ANSI B16. 5/ 47 f l anges per UCS- 66( c) - 20 F Fl ange MDMT wi t h Temper ature r educt i on per UCS- 66( b) ( 1) ( b) - 55 F

Where the Temperature Reduction per UCS-66(b)(1)(b) is: St r ess rat i o, P / Ambi ent Rati ng = 100. 00 / 285. 00 = 0. 351

Weld Size Calculations, Description: Noz N1


Results Per UW-16.1:

Requi r ed Thi ckness Act ual Thi ckness Nozzl e Wel d 0. 1750 = 0. 7 * TMI N 0. 1768 = 0. 7 * Wo i n




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Nozzle Schedule Step: 20 5:26p Sep 15,2008

Nozzle Schedule:

Nomi nal Fl ange Noz. Wal l Re- Pad Cut Descr i pt i on Si ze Sch/ Type O/ Di a Thk ODi a Thi ck Lengt h

i n. Cl s i n i n i n i n i n - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Noz N5, N6 2. 000 80 Sl i pOn 2. 375 0. 218 - - 6. 34 Noz N4 2. 500 - None 2. 500 0. 300 - - 0. 53 Noz N1 2. 500 - None 2. 500 0. 300 - - 0. 53 Noz N3, N2 3. 000 - None 3. 000 0. 312 - - 0. 65

Note on the Cut Length Calculation:The Cut Length is the Outside Projection + Inside Projection + Drop +In Plane Shell Thickness. This value does not include weld gaps,nor does it account for shrinkage.

Please Note: In the case of Oblique Nozzles, the Outside Diameter must

be increased. The Re-Pad WIDTH around the nozzle is calculated as follows:Width of Pad = (Pad Outside Dia. (per above) - Nozzle Outside Dia.)/2

Nozzle Material and Weld Fillet Leg Size Details: Shl Gr ve Noz Shl / Pad Pad OD Pad Gr ve I nsi de Nozzl e Mat er i al Wel d Wel d Wel d Wel d Wel d i n i n i n i n i n - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Noz N5, SA- 106 B 0. 250 0. 250 - - - Noz N4 SA- 105 0. 225 0. 250 - - - Noz N1 SA- 105 0. 225 0. 250 - - - Noz N3, SA- 105 0. 250 0. 250 - - -

Note: The Outside projections below do not include the flange thickness.

Nozzle Miscellaneous Data:

El evat i on/ Di st ance Layout Pr oj ecti on I nst al l ed I n Nozzl e Fr om Datum Angl e Outsi de I nsi de Component i n deg. i n i n - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Noz N5, N6 6. 500 0. 00 6. 00 0. 00 Shel l Noz N4 0. 00 0. 25 0. 00 Bot t om Head Noz N1 0. 00 0. 25 0. 00 Top Head Noz N3, N2 6. 500 270. 00 0. 25 0. 00 Shel l



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Nozzle Summary Step: 21 5:26p Sep 15,2008

Nozzle Calculation Summary

Descr i pt i on I nternal Ext MAPNC UG45 [ t r ] Wel d Areas psi g psi g Pat h

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Noz N4 468. 63 . . . . . . OK 0. 062 OK Passed Noz N3, N2 430. 24 . . . . . . OK 0. 062 OK Passed Noz N5, N6 441. 76 . . . . . . OK 0. 062 OK Passed Noz N1 470. 11 . . . . . . OK 0. 062 OK Passed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Mi n. - Nozzl es 430. 24 Noz N3, N2 Mi n. Shel l &Fl gs 228. 90

Comput ed Vessel M. A. W. P. 228. 90 psi g

Note: MAWPs (Internal Case) shown above are at the High Point.

Check the Spatial Relationship between the Nozzles

From Node Nozzl e Descr i pt i on Y Coor di nat e, Layout Angl e, Di a. Li mi t 10 Noz N4 0. 000 0. 000 3. 800 20 Noz N3, N2 6. 500 270. 000 4. 750 20 Noz N5, N6 6. 500 0. 000 3. 878 30 Noz N1 0. 000 0. 000 3. 800

The nozzle spacing is computed by the following:= Sqrt( ll^(2) + lc^(2) ) wherell - Arc length along the inside vessel surface in the long. direction.lc - Arc length along the inside vessel surface in the circ. direction

If any interferences/violations are found, they will be noted below.No interference violations have been detected !



46/47



Vessel Design Summary Step: 22 5:26p Sep 15,2008

Design Code: ASME Code Section VIII Division 1, 2007

Di amet er Spec : 16. 000 i n OD Vessel Desi gn Length, Tangent t o Tangent 33. 00 i n

Di st ance of Bot t om Tangent above Gr ade 0. 00 i n Speci f i ed Dat um Li ne Di st ance 0. 00 i n

Shel l / Head Mat l SA- 516 70 Nozzl e Mat eri al SA- 105 Nozzl e Mat eri al SA- 106 B

I nternal Desi gn Temper atur e 300 F I nt er nal Desi gn Pressur e 100. 00 psi g

External Desi gn Temper at ure 0 F

Maxi mum Al l owabl e Worki ng Pressure 228. 90 psi g

Ext er nal Max. Al l owabl e Worki ng Pressur e 233. 91 psi g Hydr ost at i c Test Pressur e 130. 00 psi g

Requi r ed Mi ni mum Desi gn Met al Temper at ure - 20 F War mest Computed Mi ni mum Desi gn Met al Temperat ur e - 55 F

Wi nd Desi gn Code No Wi nd Loads Eart hquake Desi gn Code No Sei smi c

Element Pressures and MAWP: psig

El ement Desc I nt er nal Exter nal M. A. W. P Cor r . Al l . Bot t om Head 101. 481 0. 000 489. 061 0. 0000

Shel l 101. 282 0. 000 441. 756 0. 0000 Top Head 100. 199 0. 000 490. 397 0. 0000

Li qui d Level : 41. 00 i n Dens. : 62. 400 l bm/ f t 3̂ Sp. Gr . : 1. 000

El ement "To" El ev Length El ement Thk R e q d T h k J oi nt Ef f Type i n i n i n I nt . Ext . Long Ci r c El l i pse 1. 50 1. 500 0. 250 0. 062 No Cal c 0. 85 0. 70 Cyl i nder 31. 50 30. 000 0. 250 0. 062 No Cal c 0. 70 0. 70 El l i pse 33. 00 1. 500 0. 250 0. 062 No Cal c 0. 85 0. 70

Element thicknesses are shown as Nominal if specified, otherwise are Minimum

Note: Wind and Earthquake moments include the effects of user definedforces and moments if any exist in the job and were specifiedto act (compute loads and stresses) during these cases. Alsoincluded are moment effects due to eccentric weights if any arepresent in the input.

Weights: Fabr i cat ed - Bare W/ O Removabl e I nt ernal s 178. 6 l bm Shop Test - Fabr i cat ed + Water ( Ful l ) 439. 1 l bm Shi ppi ng - Fab. + Rem. I nt l s. + Shi ppi ng App. 178. 6 l bm

Er ect ed - Fab. + Rem. I nt l s. + I nsul . ( et c) 178. 6 l bm Empt y - Fab. + I nt l s. + Detai l s + Wght s. 178. 6 l bm Oper at i ng - Empty + Oper at i ng Li qui d ( No CA) 440. 3 l bm Fi el d Test - Empt y Wei ght + Wat er ( Ful l ) 439. 1 l bm



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Problems/Failures Summary Step: 23 5:26p Sep 15,2008

Listed below are the known problem areas for the current design. If one or more of the design flags are turned on, please re-run the analysis.Some of these issues may be resolved when using updated input values.

** Warni ng: An ANSI Fl ange i s l i mi t i ng t he MAWP and thi s may af f ect t he pr essur e used i n t he Nozzl e Rei nf orcement Cal cul at i ons.

Please review all reports carefully!


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