ISO TANK BQ

22PV Elite 2013 Licensee: ORIENTAL MANUFACTURERS (P) LTDFileName : ISO TANK BQ -----------------------------------Vessel Design Summary : Step: 8 4:06p Nov 8,2013

Table of Contents

Cover Sheet2Title Page4Warnings and Errors :6Input Echo :7XY Coordinate Calculations :14Internal Pressure Calculations :15External Pressure Calculations :24Element and Detail Weights :29Center of Gravity Calculation :32MDMT Summary :33Vessel Design Summary :35

DESIGN CALCULATION

In Accordance with ASME Section VIII Division 1

ASME Code Version : 2010 Edition, 2011a Addenda

Analysis Performed by : ORIENTAL MANUFACTURERS (P) LTD

Job File : D:\$@G@R\ISO TANKS, 8.11.13\ISO TANK BQ.PVDB

Date of Analysis : Nov 8,2013

PV Elite 2013, January 2013

2Cover Page

Note: PV Elite performs all calculations internally in Imperial Units to remain compliant with the ASME Code and any built in assumptions in the ASME Code formulas. The customary Imperial database is used for consistency. The finalized results are reflected to show the users set of selected units.

3Title Page

Class From To : Basic Element Checks. ==========================================================================

Class From To: Check of Additional Element Data ==========================================================================

There were no geometry errors or warnings.

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 20134PV Elite 2013 Licensee: ORIENTAL MANUFACTURERS (P) LTDFileName : ISO TANK BQ -----------------------------------Warnings and Errors : Step: 0 4:06p Nov 8,2013

PV Elite Vessel Analysis Program: Input Data

Design Internal Pressure (for test) 5.2000 kgf/cm Design Internal Temperature 170 C Type of Test UG-99(b) Test Position Horizontal Projection of Nozzle from Vessel Top 0.0000 mm Projection of Nozzle from Vessel Bottom 0.0000 mm Minimum Design Metal Temperature 0 C Type of Construction Welded Special Service None Degree of Radiography RT-3 Miscellaneous Weight Percent 0.0 Use Higher Longitudinal Stresses (Flag) Y Select t for Internal Pressure (Flag) N Select t for External Pressure (Flag) N Select t for Axial Stress (Flag) N Select Location for Stiff. Rings (Flag) N Consider Vortex Shedding N Perform a Corroded Pressure test N Is this a Heat Exchanger No User Defined Test Press. (Used if > 0) 0.0000 kgf/cm User defined MAWP 0.0000 kgf/cm User defined MAPnc 0.0000 kgf/cm

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 IP+OW+WI+FW+BW Load Case 8 IP+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 IP+WE+EW Load Case 14 IP+WF+CW Load Case 15 IP+VO+OW Load Case 16 IP+VE+EW Load Case 17 NP+VO+OW Load Case 18 FS+BS+IP+OW Load Case 19 FS+BS+EP+OW

Wind Design Code IS-875 Basic Wind Speed for IS-875 159.00 km/hr Wind Zone Number 3 Base Elevation 1000.0 cm Percent Wind for Test 33.0 Risk Factor 1.0 Terrain Category 1 Equipment Class 1 Topography Factor 1.0 Damping Factor (Beta) for Wind (Ope) 0.0100 Damping Factor (Beta) for Wind (Empty) 0.0000 Damping Factor (Beta) for Wind (Filled) 0.0000

Seismic Design Code IS-1893-SCM Importance Factor for IS-1893 1.000 Soil Factor 1.000 Zone Number 3.000 Percent Seismic for Test 33.000

Design Nozzle for Des. Press. + St. Head Y Consider MAP New and Cold in Noz. Design N Consider External Loads for Nozzle Des. Y Use ASME VIII-1 Appendix 1-9 N

Material Database Year Current w/Addenda or Code Year

Configuration Directives:

Do not use Nozzle MDMT Interpretation VIII-1 01-37 No Use Table G instead of exact equation for "A" Yes Shell Head Joints are Tapered Yes Compute "K" in corroded condition Yes Use Code Case 2286 No Use the MAWP to compute the MDMT Yes Using Metric Material Databases, ASME II D No

Complete Listing of Vessel Elements and Details:

Element From Node 10 Element To Node 20 Element Type Elliptical Description FRONT DISH Distance "FROM" to "TO" 5.0000 cm Inside Diameter 2438.0 mm Element Thickness 10.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 12.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 5.2000 kgf/cm Design Temperature Internal Pressure 170 C Design External Pressure 0.0000 kgf/cm Design Temperature External Pressure 0 C Effective Diameter Multiplier 1.2 Material Name SA-516 70 Allowable Stress, Ambient 1406.1 kgf/cm Allowable Stress, Operating 1406.1 kgf/cm Allowable Stress, Hydrotest 1828.0 kgf/cm Material Density 0.007750 kgm/cm P Number Thickness 31.750 mm Yield Stress, Operating 2332.9 kgf/cm UCS-66 Chart Curve Designation B External Pressure Chart Name CS-2 UNS Number K02700 Product Form Plate Efficiency, Longitudinal Seam 0.85 Efficiency, Circumferential Seam 0.85 Elliptical Head Factor 2.0

Element From Node 10 Detail Type Liquid Detail ID WATER Dist. from "FROM" Node / Offset dist 0.0000 cm Height/Length of Liquid 243.80 cm Liquid Density 999.55 kgm/m

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Element From Node 20 Element To Node 30 Element Type Cylinder Description SHELL-1 Distance "FROM" to "TO" 250.00 cm Inside Diameter 2438.0 mm Element Thickness 10.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 10.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 5.2000 kgf/cm Design Temperature Internal Pressure 170 C Design External Pressure 0.0000 kgf/cm Design Temperature External Pressure 0 C Effective Diameter Multiplier 1.2 Material Name SA-516 70 Efficiency, Longitudinal Seam 0.85 Efficiency, Circumferential Seam 0.85


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Element From Node 30 Element To Node 40 Element Type Cylinder Description SHELL-2 Distance "FROM" to "TO" 224.00 cm Inside Diameter 2438.0 mm Element Thickness 10.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 10.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 5.2000 kgf/cm Design Temperature Internal Pressure 170 C Design External Pressure 0.0000 kgf/cm Design Temperature External Pressure 0 C Effective Diameter Multiplier 1.2 Material Name SA-516 70 Efficiency, Longitudinal Seam 0.85 Efficiency, Circumferential Seam 0.85


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Element From Node 40 Element To Node 50 Element Type Elliptical Description REAR DISH Distance "FROM" to "TO" 5.0000 cm Inside Diameter 2438.0 mm Element Thickness 10.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 12.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 5.2000 kgf/cm Design Temperature Internal Pressure 170 C Design External Pressure 0.0000 kgf/cm Design Temperature External Pressure 0 C Effective Diameter Multiplier 1.2 Material Name SA-516 70 Efficiency, Longitudinal Seam 0.85 Efficiency, Circumferential Seam 0.85 Elliptical Head Factor 2.0


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XY Coordinate Calculations

| | | | | | From| To | X (Horiz.)| Y (Vert.) |DX (Horiz.)| DY (Vert.) | | | cm | cm | cm | cm | -------------------------------------------------------------- FRONT DISH| 5.00000 | ... | 5.00000 | ... | SHELL-1| 255.000 | ... | 250.000 | ... | SHELL-2| 479.000 | ... | 224.000 | ... | REAR DISH| 484.000 | ... | 5.00000 | ... |

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 20139PV Elite 2013 Licensee: ORIENTAL MANUFACTURERS (P) LTDFileName : ISO TANK BQ -----------------------------------XY Coordinate Calculations : Step: 2 4:06p Nov 8,2013

Element Thickness, Pressure, Diameter and Allowable Stress :

| | Int. Press | Nominal | Total Corr| Element | Allowable | From| To | + Liq. Hd | Thickness | Allowance | Diameter | Stress(SE)| | | kgf/cm | mm | mm | mm | kgf/cm | --------------------------------------------------------------------------- FRONT DISH| 5.4440 | 12.000 | 3.0000 | 2438.0 | 1195.2 | SHELL-1| 5.4440 | 10.000 | 3.0000 | 2438.0 | 1195.2 | SHELL-2| 5.4440 | 10.000 | 3.0000 | 2438.0 | 1195.2 | REAR DISH| 5.4440 | 12.000 | 3.0000 | 2438.0 | 1195.2 |

Element Required Thickness and MAWP :

| | Design | M.A.W.P. | M.A.P. | Minimum | Required | From| To | Pressure | Corroded | New & Cold | Thickness | Thickness | | | kgf/cm | kgf/cm | kgf/cm | mm | mm | ---------------------------------------------------------------------------- FRONT DISH| 5.20000 | 6.62106 | 9.79688 | 10.0000 | 8.55035 | SHELL-1| 5.20000 | 6.57915 | 9.75689 | 10.0000 | 8.58123 | SHELL-2| 5.20000 | 6.57915 | 9.75689 | 10.0000 | 8.58123 | REAR DISH| 5.20000 | 6.62106 | 9.79688 | 10.0000 | 8.55035 | Minimum 6.579 9.757

MAWP: 6.579 kgf/cm, limited by: SHELL-2.

Internal Pressure Calculation Results :

ASME Code, Section VIII, Division 1, 2010, 2011a

Elliptical Head From 10 To 20 SA-516 70 , UCS-66 Crv. B at 170 C

FRONT DISH

Longitudinal Joint: Spot Radiography per UW-11(b) Type 1Circumferential Joint: Spot Radiography per UW-11(b) Type 1

Material UNS Number: K02700

Required Thickness due to Internal Pressure [tr]: = (P*D*Kcor)/(2*S*E-0.2*P) Appendix 1-4(c) = (5.444*2444.0000*0.997)/(2*1406.14*0.85-0.2*5.444) = 5.5503 + 3.0000 = 8.5503 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (2*S*E*t)/(Kcor*D+0.2*t) per Appendix 1-4 (c) = (2*1406.14*0.85*7.0000)/(0.997*2444.0000+0.2*7.0000) = 6.865 - 0.244 = 6.621 kgf/cm

Maximum Allowable Pressure, New and Cold [MAPNC]: = (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c) = (2*1406.14*0.85*10.0000)/(1.000*2438.0000+0.2*10.0000) = 9.797 kgf/cm

Actual stress at given pressure and thickness, corroded [Sact]: = (P*(Kcor*D+0.2*t))/(2*E*t) = (5.444*(0.997*2444.0000+0.2*7.0000))/(2*0.85*7.0000) = 1115.071 kgf/cm

Straight Flange Required Thickness: = (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1) = (5.444*1222.0000)/(1406.14*0.85-0.6*5.444)+3.000 = 8.581 mm

Straight Flange Maximum Allowable Working Pressure:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14 * 0.85 * 9.0000 )/(1222.0000 + 0.6 * 9.0000 ) = 8.764 - 0.244 = 8.520 kgf/cm

Factor K, corroded condition [Kcor]: = ( 2 + ( Inside Diameter/( 2 * Inside Head Depth ))2)/6 = ( 2 + ( 2444.000/( 2 * 612.500 ))2)/6 = 0.996739

Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 2.141 %

MDMT Calculations in the Knuckle Portion:

Govrn. thk, tg = 10.000 , tr = 6.957 , c = 3.0000 mm , E* = 0.85Stress Ratio = tr * (E*)/(tg - c) = 0.845 , Temp. Reduction = 9 C

Min Metal Temp. w/o impact per UCS-66, Curve B -29 C Min Metal Temp. at Required thickness (UCS 66.1) -38 C

MDMT Calculations in the Head Straight Flange:


Min Metal Temp. w/o impact per UCS-66, Curve B -23 C Min Metal Temp. at Required thickness (UCS 66.1) -42 C Min Metal Temp. w/o impact per UG-20(f) -29 C

Cylindrical Shell From 20 To 30 SA-516 70 , UCS-66 Crv. B at 170 C

SHELL-1



Required Thickness due to Internal Pressure [tr]: = (P*R)/(S*E-0.6*P) per UG-27 (c)(1) = (5.444*1222.0000)/(1406.14*0.85-0.6*5.444) = 5.5812 + 3.0000 = 8.5812 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14*0.85*7.0000)/(1222.0000+0.6*7.0000) = 6.823 - 0.244 = 6.579 kgf/cm

Maximum Allowable Pressure, New and Cold [MAPNC]: = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14*0.85*10.0000)/(1219.0000+0.6*10.0000) = 9.757 kgf/cm

Actual stress at given pressure and thickness, corroded [Sact]: = (P*(R+0.6*t))/(E*t) = (5.444*(1222.0000+0.6*7.0000))/(0.85*7.0000) = 1121.920 kgf/cm

Percent Elongation per UCS-79 (50*tnom/Rf)*(1-Rf/Ro) 0.408 %

Minimum Design Metal Temperature Results:



Cylindrical Shell From 30 To 40 SA-516 70 , UCS-66 Crv. B at 170 C

SHELL-2



Required Thickness due to Internal Pressure [tr]: = (P*R)/(S*E-0.6*P) per UG-27 (c)(1) = (5.444*1222.0000)/(1406.14*0.85-0.6*5.444) = 5.5812 + 3.0000 = 8.5812 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14*0.85*7.0000)/(1222.0000+0.6*7.0000) = 6.823 - 0.244 = 6.579 kgf/cm

Maximum Allowable Pressure, New and Cold [MAPNC]: = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14*0.85*10.0000)/(1219.0000+0.6*10.0000) = 9.757 kgf/cm

Actual stress at given pressure and thickness, corroded [Sact]: = (P*(R+0.6*t))/(E*t) = (5.444*(1222.0000+0.6*7.0000))/(0.85*7.0000) = 1121.920 kgf/cm

Percent Elongation per UCS-79 (50*tnom/Rf)*(1-Rf/Ro) 0.408 %

Minimum Design Metal Temperature Results:



Elliptical Head From 40 To 50 SA-516 70 , UCS-66 Crv. B at 170 C

REAR DISH



Required Thickness due to Internal Pressure [tr]: = (P*D*Kcor)/(2*S*E-0.2*P) Appendix 1-4(c) = (5.444*2444.0000*0.997)/(2*1406.14*0.85-0.2*5.444) = 5.5503 + 3.0000 = 8.5503 mm

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (2*S*E*t)/(Kcor*D+0.2*t) per Appendix 1-4 (c) = (2*1406.14*0.85*7.0000)/(0.997*2444.0000+0.2*7.0000) = 6.865 - 0.244 = 6.621 kgf/cm

Maximum Allowable Pressure, New and Cold [MAPNC]: = (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c) = (2*1406.14*0.85*10.0000)/(1.000*2438.0000+0.2*10.0000) = 9.797 kgf/cm

Actual stress at given pressure and thickness, corroded [Sact]: = (P*(Kcor*D+0.2*t))/(2*E*t) = (5.444*(0.997*2444.0000+0.2*7.0000))/(2*0.85*7.0000) = 1115.071 kgf/cm

Straight Flange Required Thickness: = (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1) = (5.444*1222.0000)/(1406.14*0.85-0.6*5.444)+3.000 = 8.581 mm

Straight Flange Maximum Allowable Working Pressure:Less Operating Hydrostatic Head Pressure of 0.244 kgf/cm = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (1406.14 * 0.85 * 9.0000 )/(1222.0000 + 0.6 * 9.0000 ) = 8.764 - 0.244 = 8.520 kgf/cm

Factor K, corroded condition [Kcor]: = ( 2 + ( Inside Diameter/( 2 * Inside Head Depth ))2)/6 = ( 2 + ( 2444.000/( 2 * 612.500 ))2)/6 = 0.996739

Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 2.141 %

MDMT Calculations in the Knuckle Portion:



MDMT Calculations in the Head Straight Flange:


Min Metal Temp. w/o impact per UCS-66, Curve B -23 C Min Metal Temp. at Required thickness (UCS 66.1) -42 C Min Metal Temp. w/o impact per UG-20(f) -29 C

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

Hydrostatic Test Pressure Results:

Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 8.553 kgf/cm Pressure per UG99b[34] = 1.3 * Design Pres * Sa/S 6.760 kgf/cm Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 12.440 kgf/cm Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 7.237 kgf/cm Pressure per PED = 1.43 * MAWP 9.408 kgf/cm

UG-99(b), Test Pressure Calculation: = Test Factor * MAWP * Stress Ratio = 1.3 * 6.579 * 1.000 = 8.553 kgf/cm

Horizontal Test performed per: UG-99b

Please note that Nozzle, Shell, Head, Flange, etc MAWPs are all consideredwhen determining the hydrotest pressure for those test types that are basedon the MAWP of the vessel.

Stresses on Elements due to Test Pressure:

From To Stress Allowable Ratio Pressure ---------------------------------------------------------------------- FRONT DISH 1262.6 1828.0 0.691 8.80 SHELL-1 1267.7 1828.0 0.694 8.80 SHELL-2 1267.7 1828.0 0.694 8.80 REAR DISH 1262.6 1828.0 0.691 8.80 ----------------------------------------------------------------------

Elements Suitable for Internal Pressure.

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External Pressure Calculation Results :

ASME Code, Section VIII, Division 1, 2010, 2011a

Elliptical Head From 10 to 20 Ext. Chart: CS-2 at 0 C

FRONT DISH

Elastic Modulus from Chart: CS-2 at 0 C : 0.204E+07 kgf/cm

Results for Maximum Allowable External Pressure (MAEP): Tca OD D/t Factor A B 7.000 2458.00 351.14 0.0003955 403.23 EMAP = B/(K0*D/t) = 403.2276/(0.9000 *351.1429 ) = 1.2759 kgf/cm

Check the requirements of UG-33(a)(1) using P = 1.67 * External Designpressure for this head.


Max. Allowable Working Pressure at given Thickness, corroded [MAWP]: = ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c) = ((2*1406.14*1.00*7.0000)/(0.997*2444.0000+0.2*7.0000))/1.67 = 4.836 kgf/cm

Maximum Allowable External Pressure [MAEP]: = min( MAEP, MAWP ) = min( 1.28 , 4.8362 ) = 1.276 kgf/cm

Cylindrical Shell From 20 to 30 Ext. Chart: CS-2 at 0 C

SHELL-1


Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 7.000 2458.00 5246.33 351.14 2.1344 0.0000935 95.27 EMAP = (4*B)/(3*(D/t)) = (4*95.2706 )/(3*351.1429 ) = 0.3618 kgf/cm

Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B 7.000 2458.00 5246.33 351.14 2.1344 0.0000935 95.27 EMAP = (4*B)/(3*(D/t)) = (4*95.2706 )/(3*351.1429 ) = 0.3618 kgf/cm

Cylindrical Shell From 30 to 40 Ext. Chart: CS-2 at 0 C

SHELL-2


Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 7.000 2458.00 5246.33 351.14 2.1344 0.0000935 95.27 EMAP = (4*B)/(3*(D/t)) = (4*95.2706 )/(3*351.1429 ) = 0.3618 kgf/cm

Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B 7.000 2458.00 5246.33 351.14 2.1344 0.0000935 95.27 EMAP = (4*B)/(3*(D/t)) = (4*95.2706 )/(3*351.1429 ) = 0.3618 kgf/cm

Elliptical Head From 40 to 50 Ext. Chart: CS-2 at 0 C

REAR DISH


Results for Maximum Allowable External Pressure (MAEP): Tca OD D/t Factor A B 7.000 2458.00 351.14 0.0003955 403.23 EMAP = B/(K0*D/t) = 403.2276/(0.9000 *351.1429 ) = 1.2759 kgf/cm

Check the requirements of UG-33(a)(1) using P = 1.67 * External Designpressure for this head.


Max. Allowable Working Pressure at given Thickness, corroded [MAWP]: = ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c) = ((2*1406.14*1.00*7.0000)/(0.997*2444.0000+0.2*7.0000))/1.67 = 4.836 kgf/cm

Maximum Allowable External Pressure [MAEP]: = min( MAEP, MAWP ) = min( 1.28 , 4.8362 ) = 1.276 kgf/cm

External Pressure Calculations

| | Section | Outside | Corroded | Factor | Factor | From| To | Length | Diameter | Thickness | A | B | | | cm | mm | mm | | kgf/cm | --------------------------------------------------------------------------- 10| 20| No Calc | 2458.00 | 7.00000 | 0.00039553 | 403.228 | 20| 30| 524.633 | 2458.00 | 7.00000 | 0.00009 | 95.2706 | 30| 40| 524.633 | 2458.00 | 7.00000 | 0.00009 | 95.2706 | 40| 50| No Calc | 2458.00 | 7.00000 | 0.00039553 | 403.228 |


| | External | External | External | External | From| To | Actual T. | Required T.|Des. Press. | M.A.W.P. | | | mm | mm | kgf/cm | kgf/cm | ---------------------------------------------------------------- 10| 20| 10.0000 | 4.50000 | ... | 1.27592 | 20| 30| 10.0000 | No Calc | ... | 0.36175 | 30| 40| 10.0000 | No Calc | ... | 0.36175 | 40| 50| 10.0000 | 4.50000 | ... | 1.27592 | Minimum 0.362


| | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia | From| To | Bet. Stiff.| Bet. Stiff.| Required | Available | | | cm | cm | cm**4 | cm**4 | ------------------------------------------------------------------- 10| 20| No Calc | No Calc | No Calc | No Calc | 20| 30| 524.633 | No Calc | No Calc | No Calc | 30| 40| 524.633 | No Calc | No Calc | No Calc | 40| 50| No Calc | No Calc | No Calc | No Calc |

Elements Suitable for External Pressure.

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Element and Detail Weights

| | Element | Element | Corroded | Corroded | Extra due | From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % | | | kgm | cm | kgm | cm | kgm | --------------------------------------------------------------------------- 10| 20| 703.946 | 2.130E+06 | 527.960 | 2.145E+06 | ... | 20| 30| 1490.13 | 11.67E+06 | 1044.36 | 11.73E+06 | ... | 30| 40| 1335.15 | 10.46E+06 | 935.747 | 10.51E+06 | ... | 40| 50| 703.946 | 2.130E+06 | 527.960 | 2.145E+06 | ... | --------------------------------------------------------------------------- Total 4233 26388258.00 3036 26527686.00 0

Weight of Details

| | Weight of | X Offset, | Y Offset, | From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description | | kgm | cm | cm | ------------------------------------------------- 10|Liqd| 2129.34 | -20.3167 | ... | WATER 20|Liqd| 11665.5 | 125.000 | ... | WATER 30|Liqd| 10452.3 | 112.000 | ... | WATER 40|Liqd| 2129.34 | 25.3167 | ... | WATER

Total Weight of Each Detail Type

Total Weight of Liquid 26376.4 --------------------------------------------------------------- Sum of the Detail Weights 26376.4 kgm

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating ------------------------------------------------------------------------------ 4233.2 4233.2 4233.2 4233.2 4233.2 4233.2 ... 26376.4 ... ... ... 26376.4 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ------------------------------------------------------------------------------ 4233.2 30609.6 4233.2 4233.2 4233.2 30609.6 kgm

Note: The shipping total has been modified because some items have been specified as being installed in the shop.

Weight Summary

Fabricated Wt. - Bare Weight W/O Removable Internals 4233.2 kgm Shop Test Wt. - Fabricated Weight + Water ( Full ) 30609.6 kgm Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 4233.2 kgm Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 4233.2 kgm Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 4233.2 kgm Operating Wt. - Empty Wt + Operating Liq. Uncorroded 30609.6 kgm Oper. Wt. + CA - Corr Wt. + Operating Liquid 29412.4 kgm Field Test Wt. - Empty Weight + Water (Full) 30609.6 kgm

Note: The Corroded Weight and thickness are used in the Horizontal Vessel Analysis (Ope Case) and Earthquake Load Calculations.

Outside Surface Areas of Elements

| | Surface | From| To | Area | | | cm | ---------------------------- 10| 20| 69572.5 | 20| 30| 193051. | 30| 40| 172974. | 40| 50| 69572.5 | ---------------------------- Total 505169.406 cm

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Shop/Field Installation Options :

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

Center of Gravity of Liquid 242.000 cm

Center of Gravity of Bare Shell New and Cold 242.000 cm Center of Gravity of Bare Shell Corroded 242.000 cm

Vessel CG in the Operating Condition 242.000 cm Vessel CG in the Fabricated (Shop/Empty) Condition 242.000 cm

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 201320PV Elite 2013 Licensee: ORIENTAL MANUFACTURERS (P) LTDFileName : ISO TANK BQ -----------------------------------Center of Gravity Calculation : Step: 6 4:06p Nov 8,2013

Minimum Design Metal Temperature Results Summary :

Curve Basic Reduced UG-20(f) Thickness Gov E* Description MDMT MDMT MDMT ratio Thk Notes C C C mm ---------------------------------------------------------------------------- FRONT DISH [10] B -29 -38 -29 0.845 10.000 0.850 FRONT DISH [7] B -23 -42 -29 0.661 12.000 0.850 SHELL-1 [8] B -29 -37 -29 0.850 10.000 0.850 SHELL-2 [8] B -29 -37 -29 0.850 10.000 0.850 REAR DISH [10] B -29 -38 -29 0.845 10.000 0.850 REAR DISH [7] B -23 -42 -29 0.661 12.000 0.850 ---------------------------------------------------------------------------- Required Minimum Design Metal Temperature 0 C Warmest Computed Minimum Design Metal Temperature -37 C

Notes:[ ! ] - This was an impact tested material.[ 1] - Governing Nozzle Weld.[ 4] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(c).[ 5] - ANSI Flange MDMT Calcs; Thickness ratio per UCS-66(b)(1)(b).[ 6] - MDMT Calculations at the Shell/Head Joint.[ 7] - MDMT Calculations for the Straight Flange.[ 8] - Cylinder/Cone/Flange Junction MDMT.[ 9] - Calculations in the Spherical Portion of the Head.[10] - Calculations in the Knuckle Portion of the Head.[11] - Calculated (Body Flange) Flange MDMT.[12] - Calculated Flat Head MDMT per UCS-66.3[13] - Tubesheet MDMT, shell side, if applicable[14] - Tubesheet MDMT, tube side, if applicable[15] - Nozzle Material[16] - Shell or Head Material

UG-84(b)(2) was not considered.UCS-66(g) was not considered.UCS-66(i) was not considered.

Notes:Impact test temps were not entered in and not considered in the analysis.UCS-66(i) applies to impact tested materials not by specification andUCS-66(g) applies to materials impact tested per UG-84.1 General Note (c).The Basic MDMT includes the (30F) PWHT credit if applicable.

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 201321PV Elite 2013 Licensee: ORIENTAL MANUFACTURERS (P) LTDFileName : ISO TANK BQ -----------------------------------MDMT Summary : Step: 7 4:06p Nov 8,2013

Design Code: ASME Code Section VIII Division 1, 2010, 2011a

Diameter Spec : 2438.000 mm ID Vessel Design Length, Tangent to Tangent 484.00 cm

Specified Datum Line Distance 5.00 cm

Shell Material SA-516 70

Internal Design Temperature 170 C Internal Design Pressure 5.200 kgf/cm

External Design Temperature 0 C

Maximum Allowable Working Pressure 6.579 kgf/cm Hydrostatic Test Pressure 8.553 kgf/cm

Required Minimum Design Metal Temperature 0 C Warmest Computed Minimum Design Metal Temperature -37 C

Wind Design Code IS-875 Earthquake Design Code IS-1893 SCM

Element Pressures and MAWP: kgf/cm

Element Desc | Design Pres. | External | M.A.W.P | Corrosion | + Stat. head | Pressure | | Allowance --------------------------------------------------------------------- FRONT DISH 5.444 0.000 6.621 3.0000 SHELL-1 5.444 0.000 6.579 3.0000 SHELL-2 5.444 0.000 6.579 3.0000 REAR DISH 5.444 0.000 6.621 3.0000

Liquid Level: 243.80 cm Dens.: 999.552 kgm/m Sp. Gr.: 1.000

Element "To" Elev Length Element Thk R e q d T h k Joint Eff Type cm cm mm Int. Ext. Long Circ ----------------------------------------------------------------------- Ellipse 0.0 5.0 12.0 8.6 4.5 0.85 0.85 Cylinder 250.0 250.0 10.0 8.6 No Calc 0.85 0.85 Cylinder 474.0 224.0 10.0 8.6 No Calc 0.85 0.85 Ellipse 479.0 5.0 12.0 8.6 4.5 0.85 0.85

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

Weights: Fabricated - Bare W/O Removable Internals 4233.2 kgm Shop Test - Fabricated + Water ( Full ) 30609.6 kgm Shipping - Fab. + Rem. Intls.+ Shipping App. 4233.2 kgm Erected - Fab. + Rem. Intls.+ Insul. (etc) 4233.2 kgm Empty - Fab. + Intls. + Details + Wghts. 4233.2 kgm Operating - Empty + Operating Liquid (No CA) 30609.6 kgm Field Test - Empty Weight + Water (Full) 30609.6 kgm

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

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