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    STRESS CALCULATION

    EQUIPMENT : SECONDARY SUPPERHEATER

    QUANTITY : ONE

    CLIENT : SINCHAISRI COMPANY LTD.

    PHANOMTUAN, KANCHANABURI, THAILAND.

    ENGINEERING : ENMAS GB POWER SYSTEMS PROJECTS LIMITED,

    DESIGN & CONSTRUCTION CODE : ASME BOILER & PRESSURE VESSEL CODE,

    SECTION - I, 2007 EDITION

    MANUFACTURER : G.B. ENGINEERING ENTERPRISES PVT. LTD.,

    D - 99 DEVELOPED PLOTS ESTATE

    THUVAKKUDY,

    TRICHY - 620 015, INDIA.

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    STRESS CALCULATIONSheet 01

    GB ENGINEERING Rev. 00

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    02. Index

    Cover Sheet

    Index

    Revision Status - Drawing

    Revision Status - Stress Calculation sheet

    List of Drawings

    List of Standards/CodesDesign Data

    Hydrostatic Test Pressure

    Material Constructions

    Allowable Stress

    Radiographic Examinations

    Heat Treatment

    Calculation of minimum required thickness for tubes

    Calculation of minimum required thickness for inlet header

    Calculation of Max. allowable stress during hydro test for inlet header

    Calculation of minimum required thickness for Nozzles

    Calculation of Max. allowable openig on inlet header

    Compensation check for inlet header

    Calculation of end plate thickness for inlet header

    Calculation of Max. allow. stress during hydro test for header end plate

    Minimum requirements for attachments weld on inlet header

    Calculation of minimum required thickness for inlet header

    Calculation of Max. allowable stress during hydro test for inlet header

    Calculation of minimum required thickness and M/C End

    Calculation of Max. allowable openig on outlet header

    Compensation check for outlet header

    Calculation of end plate thickness for inlet header

    Calculation of Max. allow. stress during hydro test for header end plate

    Minimum requirements for attachments weld on inlet header

    07 41

    08 42 to 44

    04 36

    05 37

    06 38 & 40

    01 29

    02 30

    03 31 To 35

    07 24 & 25

    08 26 To 28

    Secondary Superheater outlet header

    04 20

    05 21

    06 22 & 23

    01 15

    02 16

    03 17 to 19

    Secondary Superheater tubes

    01 13 & 14Secondary Superheater inlet header

    10 10

    11 11

    12 12

    07 7

    08 8

    09 9

    04 4

    05 5

    06 6

    01 1

    02 2

    03 3

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    S.No. Description Sheet No.

    STRESS CALCULATIONSheet 02

    GB ENGINEERING Rev. 00

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    03. STATUS OF CALCULATION DUE TO REVISION IN DRAWING

    S.

    NoRev.

    PREPARED CHECKED APPROVED DOCUMENT NO. DATE

    REV.NO. DESCRIPTION PREPARED CHECKED APPROVED

    SCL/XXX/XXX 02.02.2012

    Checked Approved

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S SERIAL

    No.GBE/XXXX/0XX

    Drawing No.Page Of

    CalculationReason For Revision

    Pages

    AffectedPrepared

    STRESS CALCULATIONSheet 03

    GB ENGINEERING Rev. 00

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    04. REVISION STATUS FOR STRESS CALCULATIONS

    0 1 2 3 4 0 1 2 3 4 0 1 2 3 4

    30

    28

    29

    26

    27

    24

    25

    22

    23

    20

    21

    18 48

    19

    16 46

    17 47

    14 44

    15 45

    12 42

    13 43

    10 40

    11 41

    8 38

    9 39

    6 36

    7 37

    4 345 35

    2 32

    3 33

    No. No. No.

    1 31

    Sheet REV. No. Sheet REV. No. Sheet REV. No.

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S SERIAL

    No.GBE/XXXX/0XX

    STRESS CALCULATIONSheet 04

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    05.LIST OF DRAWINGS PREPARED

    Arrangement of Secondary Superheater

    Secondary superheater inlet and outlet headers

    Secondary superheater coil

    Tube bends for secondary supperheater coil

    3 WAAA0200-1-F-05-06-0045 00

    4 WAAA0200-1-F-05-06-0046 00

    1 WAAA0200-1-F-05-05-0047 00

    2 WAAA0200-1-F-05-07-0006 00

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATER MFR'S SERIAL No. GBE/XXXX/0XX

    S.No. Description Drawing No. Rev.

    STRESS CALCULATIONSheet 05

    GB ENGINEERING Rev. 00

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    06.LIST OF STANDARDS / CODES

    1 ASME Section-I, 2007 Edition

    2 ASME Section II, Part-A, 2007 Edition

    3 ASME Section-II, Part-D, 2007 Edition

    4 ASME B36.10M, 2004

    5 ASME Section - VIII, Division - 1, 2007 Edition

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    STRESS CALCULATIONSheet 06

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    07. DESIGN DATA

    Design & Construction code : ASME Boiler & Pressure Vessel Code,

    Section - I, 2007 Edition

    Fluid Handled : Superheated Steam

    Max. Allowable Working Pressure : bar (a) = kg/cm2

    (a)

    Design Pressure : bar (a) = kg/cm2

    (a)

    Design Temperature : oC [ SA 213 Gr.T22 ]

    : oC [ SA 213 Gr.T11 ]

    : oC [SA 106 Gr. B]

    : oC [SA 335Gr. P11]

    Hydrostatic Test Pressure(PG-99) : bar (a) = kg/cm2 (a)

    Hydrostatic Test Temp.(PG-99) : 21 C ( Not less than 70oF)

    Radiography : (Ref page No. 11)

    Post Weld Heat Treatment : (Ref page No. 12)

    Corrosion allowance : mm

    Notified body : LLOYD'S Register Verificaton Limited

    Volume : 2600 ( Litres )

    128.595 131.130

    1

    85.73 87.420

    535

    480

    385

    501

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    85 86.680

    STRESS CALCULATIONSheet 07

    GB ENGINEERING Rev. 00

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    08 Calculation of Design Pressure As per PG-99

    Maximum Allowable working pressure = kg/cm2

    (a) = bar(a)

    (MAWP)

    Design Pressure = MAWP + Hydrostatic Head

    = 86.68 +

    = kg/cm2

    (a) = bar(a)

    Upper elevation

    Lower Elevation

    Effective Static Head

    Static head per meter

    Static head for 7.4 m5 kg/cm2 0.74

    3 mm 7400

    4 kg/cm2 0.1

    1 mm 19675

    2 mm 12275

    0.74

    87.420 85.73

    S.No. Description units Data

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    86.68 85.00

    STRESS CALCULATIONSheet 08

    GB ENGINEERING Rev. 00

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    09 MATERIAL OF CONSTRUCTION

    01 Tubes = SA 210 Gr.T11

    = SA 213 Gr.T22

    02 Inlet Header

    Header = SA 106 Gr.B

    Pipe = SA 106 Gr.B

    Inspection Stub = SA 106 Gr.B

    End Cover = SA 105

    03 Outlet Header

    Header = SA 335 Gr.P11

    Inspection Stub = SA 182 Gr.F11 CL.1

    End Cover = SA 182 Gr.F11 CL.1

    Pipe = SA 335 Gr.P11

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    STRESS CALCULATIONSheet 09

    GB ENGINEERING Rev. 00

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    10 Allowable stress Values

    As per ASME Section - II, Part-D, 2007 Edition

    1

    2

    3

    4

    5

    6

    7

    8 1881.39 4 1

    1881.39 4 1

    SA 182 Gr.F11 CL.1 21 205000 2090.43 501 75671.75 771.64

    1881.39 4 1

    SA 213 Gr.T22 21 205000 2090.43 501 80223.98 818.06

    1 2

    Outlet Header

    SA 335 Gr.P11 21 205000 2090.43 501 75671.75 771.64

    4 1

    SA 105 21 250000 2549.30 385 110599 1127.8 2294.37

    1 1

    SA 213 Gr.T11 21 205000 2090.43 385 103199.9 1052.35 1881.39

    1

    Inlet Header

    SA 106 Gr.B 21 240000 2447.33 385 98560.39 1005.04 2202.60

    1

    SA 213 Gr.T11 21 205000 2090.43 480 91093.63 928.9 1881.39 4

    TubesSA 213 Gr.T22 21 205000 2090.43 535 57480.48 586.14 1881.39 5A

    P.No.

    Grou

    p

    No.TempoC

    Stress

    kPa

    Stress

    kg/cm2

    TempoC

    Stress

    kPa

    Stress

    kg/cm2

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    S.

    No

    Material

    construction

    Min. yield strength at

    ambient temperature"Y"

    Allowable stress at design

    temperature"S"

    Min. yield

    strength at

    ambient

    temp. (0.9xY)

    kg/cm2

    STRESS CALCULATIONSheet 10

    GB ENGINEERING Rev. 00

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    11 Radiographic Examination of Welds as per PW-11

    Conclusion:

    01.Header outside diameter is 219.1 mm and thickness is 18.26 mm.

    02.Hence Radiographic Test is not required as per table PW 11 as above.

    03 However our Manufacturer practice of Radiographic Test is as follows,

    100% for Header joints

    10% for tube joints

    1Circumferential welds in Pipes,

    tubs and Headers

    Table PW 11,

    (Not Subject to

    furnace Radiant Heat)

    (Steam)

    100% radiography shall be

    done. If, circumferential

    weldsin drum exceed NPS 16

    (DN 400 ) or 41 mm thicknss

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    S.No. Description Code Requirement

    STRESS CALCULATIONSheet 11

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    12 Heat Treatment

    Conditions:

    Material : P-No. 1, Group No. 1, 2, 3(a) (1) Postweld heat treatment is not mandatory for circumferential butt welds in pressure

    parts with a nominal Wall thickness of 3/4 in. ( 19 mm ) or less at the joints.

    for Combination groove and fillet welds attaching connections to a vessel as depicted in

    Fig. 16.1(z), provided all of the following conditions are meet:

    (a) both the tube and vessels are P-No.1, Group No. 1 or 2 material

    (b) The dia. of the finished opening does not exceed that allowed in PG-32.1.2 or 2 in. ( 50mm ), whichever is less

    (c)the nominal thickness of the weld does not exceed 3/8 in. (10 mm)

    (d) the connections are not placed in the vessel such as to form ligaments, the efficiency

    of which would affect the vessel thickness

    (e) a minimum preheat of 200o

    F (95oC) is applied when the thickness of either part exceeds 3/4 in. (19mm)

    (f) for welds attaching nonload-carring studs not exceeding 1/2 in. (13mm) in diameter when

    using an automatic arc stud welding or automatic resistance stud welding process.

    ( c ) For all P-No.1 Group No.1 materials, and for P-No.1 Group No.2 materials having a maximum

    actual carbon Content of 0.30%, the postweld heat treatment requirement of PWT 11.2

    for tubes welded to headers is not Mandatory when all of the following conditions are met:

    1) The tubes do not exceed 2 in. ( 50 mm ) O.D. 3) The header thickness does not exceed 1/2 in. ( 13 mm ).

    2) The header does not exceed NPS 8 (DN 200) 4) A minimum preheat of 200oF ( 95 C ) is applied.

    Conclusions:

    01. Header outside diameter is 219.1 mm and thickness is 18.26 mm.(Groove Cum fillet weld size more than 13mm)

    02. Hence the Postweld heat treatment is required.

    Material : P-No. 4, Group No. 1, 2

    (1) for circumferential butt welds in pressure parts with all the following conditions

    (a) a nominal base metal thickness of 16mm or less at the weld

    (b) a max specified carbon content ( SA material specification carbon content except when further limited by

    1 Secondary Superheater welds Table PW 39

    (11)

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/0XX

    S.No. Description Code

    STRESS CALCULATIONSheet 12

    GB ENGINEERING Rev. 00

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    01 Calculation of tube thickness Under Internal Pressure As Per PG - 27.2.1

    Item

    Drg. No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of tube D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Thinnig allowance ( 10%)

    Max. Allow. Stress value at Design Temp. SMin. Yield Strength at ambient Temperature Y

    e

    Corrosion Allowance C.A

    Minimum required thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro20 Hence Satisfactory

    kPa 79239.75 808.02 kg/cm2

    19 kPa 184500.00 1881.38 kg/cm2

    17 bar (a) 128.595 131.130 kg/cm2(a)

    18

    15 mm 3.05

    16 Hence Satisfactory

    14

    mm 2.83

    12 Thickness factor for expanded tube end

    (PG-27.4,Note:4)mm 0.00

    13 mm 1.00

    10 kPa 57480.48 586.14 kg/cm2

    11 kPa 205000 2090.43 kg/cm2

    08 mm 4.50

    09 mm 4.05

    06 mm 4.50

    07 % 0.00

    04 oC 535

    05 mm 38.10

    02 SA 213 Gr.T22

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Secondary Superheater coils

    WAAA0200-2-F-05-06-0046

    Item No. 01

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/00X

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 13

    GB ENGINEERING Rev. 00

    ]eD005.0t[2

    ])eD005.0t(D[PS hhydro

    eD005.0PS2

    DPt min

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    01 Calculation of tube thickness Under Internal Pressure As Per PG - 27.2.1

    Item

    Drg. No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of tube D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Thinnig allowance ( 10%)

    Max. Allow. Stress value at Design Temp. SMin. Yield Strength at ambient Temperature Y

    e

    Corrosion Allowance C.A

    Minimum required thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro20 Hence Satisfactory

    kPa 110029.44 1121.99 kg/cm2

    19 kPa 184500.00 1881.38 kg/cm2

    17 bar (a) 128.595 131.130 kg/cm2(a)

    18

    15 mm 2.29

    16 Hence Satisfactory

    14

    mm 1.90

    12 Thickness factor for expanded tube end

    (PG-27.4,Note:4)mm 0.00

    13 mm 1.00

    10 kPa 91093.633 928.90 kg/cm

    2

    11 kPa 205000 2090.43 kg/cm2

    08 mm 3.66

    09 mm 3.29

    06 mm 3.66

    07 % 0.00

    04 oC 480

    05 mm 38.10

    02 SA 213 Gr.T11

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Secondary Superheater coils

    WAAA0200-2-F-05-06-0046

    Item No. 02

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/00X

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 14

    GB ENGINEERING Rev. 00

    ]eD005.0t[2

    ])eD005.0t(D[PS hhydro

    eD005.0PS2

    DPt min

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    01 Calculation of Header Thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Header D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min.allow. for structural stability(PG-27.4,Notes:3)CCorrosion Allowance C.A

    Ligaments between openings (PG-52)

    p = Longitudinal Pitch

    d1 = Diameter of Hole - 1 ( Tube hole )

    d2 = Diameter of Hole - 2 ( Tube hole )

    d = Average hole Diameter

    EL

    = Long. Ligament Efficiency

    Least Ligament Efficiency E

    Minimum required thickness

    Minimum required thickness ( E = 1 )

    Greater of ( 19, 21 )

    Required thickness

    t = Minimum thickness available - C.A t

    P id d Mi Thi k R i d Thi k25 H S ti f t

    23 mm 11.31

    24 mm 14.98

    21Minimum thickness as per code (PG-16.3)

    For boiler plate minimum thicknessmm 6.00

    22 mm 11.31

    mm 11.31

    20 mm 9.21

    17 0.808

    19

    mm 28.78

    0.808

    mm 28.78

    mm 28.78

    14

    mm 150.00

    12 mm 0.0013 mm 1.00

    10 kPa 240000 2447.33 kg/cm2

    11 0.40

    8 mm 15.98

    9 kPa 98560.389 1005.04 kg/cm2

    6 mm 18.26

    7 % 12.50

    4 oC 385

    5 mm 219.10

    2 SA 106 Gr.B

    3 bar (a) 85.73 87.420 kg/cm2(a)

    1 Secondary superheater Inlet Header

    WAAA0200-2-F-05-07-0006

    01/01

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 15

    GB ENGINEERING Rev. 00

    p

    dpE L

    CPy2ES2

    DPt min

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    02.Calculation of maximum allowable stress during Hydro test As Per PG - 27.2.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Hydrostatic test Pressure Ph

    Outside Diameter of Header D

    Minimum thickness available t

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min.allow. for structural stability(PG-27.4,Notes:3) C

    Efficiency E

    Stress during Hydrostatic test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    11 kPa 216000.00 2202.60 kg/cm2

    12 Hence Satisfactory

    10

    kPa 92298.95 941.19 kg/cm2

    8 mm 0.00

    9 0.808

    6 kPa 240000 2447.33 kg/cm2

    7 0.40

    4 mm 219.10

    5 mm 18.26

    2 SA 106 Gr.B

    3 bar (a) 128.15 131.130 kg/cm2(a)

    1 Secondary superheater Inlet Header

    MFB-F-10-05-07-0001

    01/01

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 16

    GB ENGINEERING Rev. 00

    )Ct(E2

    ])Ct(y2D[P

    S

    h

    hydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 216000.00 2202.60 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 78958.30 805.15 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 4.8018 mm 8.74

    mm 4.80

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 240000 2447.33 kg/cm2

    11 0.40

    08 mm 9.74

    09 kPa 98560.389 1005.04 kg/cm2

    06 mm 11.13

    07 % 12.50

    04 oC 385

    05 mm 114.30

    02 SA 106 Gr.B

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Inspection stub

    MFB-F-10-05-07-0001

    03

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 17

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 216000.00 2202.60 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 67108.98 684.32 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 7.0718 mm 14.98

    mm 7.07

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 240000 2447.33 kg/cm2

    11 0.40

    08 mm 15.98

    09 kPa 98560.389 1005.04 kg/cm2

    06 mm 18.26

    07 % 12.50

    04 oC 385

    05 mm 168.30

    02 SA 106 Gr.B

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Inlet stub

    MFB-F-10-05-07-0001

    06

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 18

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 216000.00 2202.60 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 120836.09 1232.19 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 7.0718 mm 8.59

    mm 7.07

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 240000 2447.33 kg/cm2

    11 0.40

    08 mm 9.59

    09 kPa 98560.389 1005.04 kg/cm2

    06 mm 9.59

    07 % 0.00

    04 oC 385

    05 mm 168.30

    02 SA 106 Gr.B

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Inlet stub machine end

    MFB-F-10-05-07-0001

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    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 19

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    03 Calculation of maximum allowable opening as per ASME PG-32.1.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Header D

    Minimum Thickness t

    Max. Allow. Stress value at Design Temp. S

    Minimum required thickness

    d = Maximum allowable diameter of

    uncompensated opening ( as per Fig. PG-32 )

    d = 8.08 [ D t ( 1 - K ) ](1/3)

    dn = Diameter of the Opening

    Opening List

    Inlet Stub

    Inspection Stub

    Tube3 28.78 96.56 Hence Compensation is not required

    1 139.76 96.56 Hence Compensation is required

    2 92.04 96.56 Hence Compensation is not required

    S.No Description

    Actual

    Opening

    Allowable

    Opening ( dn < d )

    mm mm

    9

    mm 96.56

    10 mm

    8

    0.57

    6 mm 18.26

    7 kPa 98560.389 1005.04 kg/cm2

    4 oC 385

    5 mm 219.10

    2 SA 106 Gr.B

    3 bar (a) 85.73 87.420 kg/cm2(a)

    1 Secondary superheater Inlet Header

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 20

    GB ENGINEERING Rev. 00

    tS82.1

    DPK

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    Compensation check calculation as per ASME Section - I, PG - 33

    Item

    Drg. No.

    Item No.

    Shell Data:

    Minimum Thickness of Shell t

    Required Thickness of Seamless Shell tr

    Max. allowable stress at design temp. Sv

    Finished Diameter of opening d

    Nozzle DataNozzle OD

    Nominal Thickness of Nozzle tn

    Required Thickness of Seamless Nozzle tnr

    Material Specification

    Max. allowable stress at design temp. Snfr1 = ( Sn / Sv )

    Actual projection of nozzle I.S. of the dished head

    2.5 x t

    2.5 x tn

    Minimum of 2.5 t and 2.5 tn

    Actual projection of nozzle I.S. of the shell

    F = Correction factor

    Compensation available in dished head

    ( d - 2 tn ) ( t - F t r)

    2 t ( t - F t r)

    A1 = max. ( i, ii ) A1

    Compensation available in Nozzle

    2 ( tn - trn ) ( 2.5 t fr1 )

    2 ( tn - trn ) ( 2.5 tn + te ) fr1A2 = min. ( i, ii ) A2

    Compensation available in nozzle from inside projection

    h = Projection of nozzle inside the shell

    A3 = 2 tn fr1 h A3

    Compensation available in reinforcement element

    Outer diameter of the reinforcement element Dp

    Thickness of the reinforcement element te

    Max.allowable stress at Design temp. Sp

    fr3 = Sp / Sv fr3A5 = ( Dp - d - 2 tn ) te fr3 A5

    Total Compensation Area available

    A avail = A1 + A2 + A3 + A5 mm2 1955.97

    0.00

    mm2 0.00

    12

    mm 0.00

    mm 0.00

    kPa 0 0.00 kg/cm2

    10

    mm 0.00

    mm2 0.00

    11

    09

    mm2 1021.65

    mm2 1021.65mm

    2 1021.65

    08

    mm2 934.32

    mm2 330.51

    mm2 934.32

    mm 35.68

    06 mm 0.00

    07 1.00

    05 mm 0.00

    mm 45.65

    mm 45.65

    kPa 98560.389 1005.04 kg/cm2

    04 1.00

    mm 7.07

    SA 106 Gr.B.

    03

    mm 168.30

    mm 18.26

    kPa 98560.389 1005.04 kg/cm2

    mm 139.76

    02

    mm 18.26

    mm 9.21

    01 Inlet Stub

    MFB-F-10-05-07-0001

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    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 21

    GB ENGINEERING Rev. 00

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    06 Calculation of End plate thickness Under Internal Pressure As Per PG - 31.3

    Item

    Drg. No.

    Var. No./Item No.

    Design Pressure P

    Design Temperature

    Corrosion Allowance C.A

    End plate data

    Material Specification

    Inside diameter of the Header d

    Provided Thickness of End Plate t

    Allowable Stress value at design temperature S

    Header data

    Actual thicknes of header ts

    Min. required thickness of seamless header tr

    C = Calculation factor as per Fig [ PG-31 (g-1) ]

    m = tr / ts

    0.33 m

    C = 0.33m with a minimum of 0.2

    Selected 'C' C

    Minimum required thickness of end plate

    Required Thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Minimum weld size

    tw = 2 trmin. not less than 1.25 ts, But need not be Greater than t

    2 tr

    1.25 ts

    tw = Minimum weld Size20 mm 10.00

    17

    18 mm 18.42

    19 mm 22.83

    15 mm 29.00

    16 Hence Satisfactory

    mm 22.73

    14 mm 22.73

    mm 0.20

    12 mm 0.20

    13

    11

    mm 0.50

    mm 0.17

    09 mm 18.26

    10 mm 9.21

    07 mm 30.00

    08 kPa 110598.988 1127.80 kg/cm2

    04 mm 1.00

    05 SA 105

    06 mm 182.58

    02 bar (a) 85.73 87.420 kg/cm2(a)

    03 oC 385

    01 Inlet header end Cover

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 22

    GB ENGINEERING Rev. 00

    SPCdt min

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    06 Calculation of End plate thickness Under Internal Pressure As Per UG - 34

    Item

    Drg. No.

    Var. No./Item No.

    Design Pressure P

    Design Temperature

    Corrosion Allowance C.A

    End plate data

    Material Specification

    Inside diameter of the Header d

    Provided Thickness of End Plate t

    Allowable Stress value at design temperature S

    Header data

    Actual thicknes of header ts

    Min. required thickness of seamless header tr

    C = Calculation factor as per Fig [ UG-34 (b-2) & UW-13.3 (b)]

    m = tr / ts

    0.33 m

    C = 0.33m with a minimum of 0.2

    Selected 'C' C

    Minimum required thickness of end plate

    Required Thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    15 mm 19.00

    16 Hence Satisfactory

    mm 11.46

    14 mm 11.46

    12 mm 0.20

    13

    11

    mm 0.50

    mm 0.17

    mm 0.20

    09 mm 18.26

    10 mm 9.21

    07 mm 20.00

    08 kPa 110598.988 1127.80 kg/cm2

    04 mm 1.00

    05 SA 105

    06 mm 92.04

    02 bar (a) 85.73 87.420 kg/cm2(a)

    03 oC 385

    01 Inlet header end Cap

    MFB-F-10-05-07-0001

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    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 23

    GB ENGINEERING Rev. 00

    SPCdt min

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    07 Calculation of Stress at Hydrostatic Test Pressure (PG -99)

    Item

    Drg. No.

    Var. No./Item No.

    Hydrostatic test Pressure Ph

    End plate data

    Material Specification

    Inside diameter of the Header d

    Minimum Thickness of End Plate t

    Minimum yield strength at Ambient temp. Y

    Selected 'C' C

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99) t

    ( 0.9 x Y ) > Shydro10 Hence Satisfactory

    kg/cm2

    09 kPa 225000 2294.37 kg/cm2

    08

    kPa 95260.97 971.40

    06 kPa 250000 2549.30 kg/cm2

    07 mm 0.20

    04 mm 182.58

    05 mm 30.00

    02 bar (a) 128.60 131.130 kg/cm2(a)

    03 SA 105

    01 Inlet header end cover

    MFB-F-10-05-07-0001

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    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 24

    GB ENGINEERING Rev. 00

    2

    h

    2

    hydrot

    PCdS

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    07 Calculation of Stress at Hydrostatic Test Pressure (PG -99)

    Item

    Drg. No.

    Var. No./Item No.

    Hydrostatic test Pressure Ph

    End plate data

    Material Specification

    Inside diameter of the Header d

    Minimum Thickness of End Plate t

    Minimum yield strength at Ambient temp. Y

    Selected 'C' C

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99) t

    ( 0.9 x Y ) > Shydro10 Hence Satisfactory

    kg/cm2

    09 kPa 225000 2294.37 kg/cm2

    08

    kPa 54468.37 555.42

    06 kPa 250000 2549.30 kg/cm2

    07 mm 0.20

    04 mm 92.04

    05 mm 20.00

    02 bar (a) 128.60 131.130 kg/cm2(a)

    03 SA 105

    01 Inlet header end cap

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 25

    GB ENGINEERING Rev. 00

    2

    h

    2

    hydrot

    PCdS

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or the

    thickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    Minimum groove size

    tw = tn but not less than 1/4"

    Required tw

    Provided tw

    Required tw < Provided tw11 Hence Satisfactory

    08

    09 mm 6.00

    10 mm 6.50

    mm 5.50

    07 Hence Satisfactory

    mm 2.56

    mm 2.56

    05

    06 Sketch (z)

    mm 3.66

    04

    02 mm 18.26

    03 mm 3.66

    01 Inlet header to panal stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 26

    GB ENGINEERING Rev. 00

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or the

    thickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    mm 10.00

    07 Hence Satisfactory

    mm 9.99

    mm 9.99

    05

    06 Sketch (a)

    mm 14.27

    04

    02 mm 18.26

    03 mm 14.27

    01 Inlet header to riser stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 27

    GB ENGINEERING Rev. 00

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or the

    thickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    mm 9.0007 Hence Satisfactory

    mm 7.79

    mm 7.79

    05

    06 Sketch (a)

    mm 11.13

    04

    02 mm 18.26

    03 mm 11.13

    01 Inlet header to inspection stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 28

    GB ENGINEERING Rev. 00

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    01 Calculation of Header Thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Header DNominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min.allow. for structural stability(PG-27.4,Notes:3)C

    Corrosion Allowance C.A

    Ligaments between openings (PG-52)

    p = Longitudinal Pitch

    d1 = Diameter of Hole - 1 ( Tube hole )

    d2 = Diameter of Hole - 2 ( Tube hole )

    d = Average hole Diameter

    EL = Long. Ligament Efficiency

    Least Ligament Efficiency E

    Minimum required thickness

    Minimum required thickness ( E = 1 )

    Greater of ( 19, 21 )

    Required thickness

    t = Minimum thickness available - C.A t

    P id d Mi Thi k R i d Thi k25 H S ti f t

    23 mm 14.36

    24 mm 17.04

    21Minimum thickness as per code (PG-16.3)

    For boiler plate minimum thicknessmm 6.00

    22 mm 14.58

    mm 14.36

    20 mm 11.87

    17 0.819

    19

    mm 27.10

    0.819

    mm 27.10

    mm 27.10

    14

    mm 150.00

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    8 mm 18.04

    9 kPa 75671.753 771.64 kg/cm2

    6 mm 20.62

    7 % 12.50

    4 oC 501

    5 mm 219.10

    2 SA 335 Gr.P11

    3 bar (a) 85.73 87.420 kg/cm2(a)

    1 Outlet Header

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 29

    GB ENGINEERING Rev. 00

    p

    dpE L

    CPy2ES2

    DPt min

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    02.Calculation of maximum allowable stress during Hydro test As Per PG - 27.2.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Hydrostatic test Pressure Ph

    Outside Diameter of Header D

    Minimum thickness available t

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min.allow. for structural stability(PG-27.4,Notes:3) C

    Efficiency E

    Stress during Hydrostatic test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    11 kPa 184500.00 1881.38 kg/cm2

    12 Hence Satisfactory

    10

    kPa 80277.95 818.61 kg/cm2

    8 mm 0.00

    9 0.819

    6 kPa 205000 2090.43 kg/cm2

    7 0.40

    4 mm 219.10

    5 mm 20.62

    2 SA 335 Gr.P11

    3 bar (a) 128.60 131.130 kg/cm2(a)

    1 Outlet Header

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX./038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 30

    GB ENGINEERING Rev. 00

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 184500.00 1881.38 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 35466.53 361.66 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 6.50

    18 mm 19.00

    mm 6.50

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    08 mm 20.00

    09 kPa 75671.753 771.64 kg/cm2

    06 mm 20.00

    07 % 0.00

    04 oC 501

    05 mm 120.00

    02 SA 182 F11 CL.1

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Inspection stub

    MFB-F-10-05-07-0001

    03

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 31

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 184500.00 1881.38 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 45760.17 466.63 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 10.30

    18 mm 24.00

    mm 10.30

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    08 mm 25.00

    09 kPa 75671.753 771.64 kg/cm2

    06 mm 25.00

    07 % 0.00

    04 oC 501

    05 mm 190.00

    02 SA 182 F11 CL.1

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Sec. superheater outlet stub

    MFB-F-10-05-07-0001

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    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 32

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 184500.00 1881.38 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 89039.55 907.95 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 9.12

    18 mm 11.49

    mm 9.12

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    08 mm 12.49

    09 kPa 75671.753 771.64 kg/cm2

    06 mm 12.49

    07 % 0.00

    04 oC 501

    05 mm 168.30

    02 SA 182 F11 CL.1

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Sec. superheater outlet stub

    MFB-F-10-05-07-0001

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    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 33

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 184500.00 1881.38 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 60268.90 614.57 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 4.82

    18 mm 8.74

    mm 4.82

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    08 mm 9.74

    09 kPa 75671.753 771.64 kg/cm2

    06 mm 11.13

    07 % 12.50

    04 oC 501

    05 mm 88.90

    02 SA 335 Gr.P11

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Sec.superheater drain stub

    MFB-F-10-05-07-0001

    07

    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 34

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

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    01 Calculation of pipe thickness Under Internal Pressure As Per PG - 27.2.2

    Item

    Drg. No.

    Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Pipe D

    Nominal Thickness

    Under Tolerance on thickness

    Minimum Thickness available

    Max. Allow. Stress value at Design Temp. S

    Min. Yield Strength at ambient Temperature Y

    Temperature Co-efficient ( PG-27.4, Note-6 ) y

    Min. allow. for structural stability(PG-27.4,Note:3) C

    Corrosion Allowance C.A

    Efficiency (PG - 27.4, Note:1) E

    Minimum required thickness

    Minimum thickness as per code (PG-16.3)

    Required Thickness (Greater of 15 & 16)

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    Stress at Hydrostatic Test Pressure (PG -99)

    Hydrostatic test Pressure

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99)

    ( 0.9 x Y ) > Shydro

    23 kPa 184500.00 1881.38 kg/cm2

    24 Hence Satisfactory

    21

    22 kPa 66893.57 682.13 kg/cm2

    19 Hence Satisfactory

    20 bar (a) 128.60 131.14 kg/cm2(a)

    17 mm 1.81

    18 mm 2.98

    mm 1.81

    16 mm N.A.

    14 1.00

    15

    12 mm 0.00

    13 mm 1.00

    10 kPa 205000 2090.43 kg/cm2

    11 0.40

    08 mm 3.98

    09 kPa 75671.753 771.64 kg/cm2

    06 mm 4.55

    07 % 12.50

    04 oC 501

    05 mm 33.40

    02 SA 335 Gr.P11

    03 bar (a) 85.73 87.420 kg/cm2(a)

    01 Sec.superheater drain stub

    MFB-F-10-05-07-0001

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    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 35

    GB ENGINEERING Rev. 00

    CPy2ES2

    DPtmin

    )Ct(E2

    ])Ct(y2D[PS hhydro

    Sh 36

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    03 Calculation of maximum allowable opening as per ASME PG-32.1.2

    Item

    Drg. No.

    Var. No./Item No.

    Material Specification

    Design Pressure P

    Design Temperature

    Outside Diameter of Header D

    Minimum Thickness t

    Max. Allow. Stress value at Design Temp. S

    Minimum required thickness

    d = Maximum allowable diameter of

    uncompensated opening ( as per Fig. PG-32 )

    d = 8.08 [ D t ( 1 - K ) ](1/3)

    dn = Diameter of the Opening

    Opening List

    Panal Stub

    Inspection Stub

    Tube3 27.1 93.10 Hence Compensation is not required

    1 140 93.10 Hence Compensation is required

    2 80 93.10 Hence Compensation is not required

    S.No Description

    Actual

    Opening

    Allowable

    Opening ( dn < d )

    mm mm

    9

    mm 93.10

    10 mm 93.10

    8

    0.66

    6 mm 20.62

    7 kPa 75671.753 771.64 kg/cm2

    4 oC 501

    5 mm 219.10

    2 SA 335 Gr.P11

    3 bar (a) 85.73 87.420 kg/cm2(a)

    1 Sec. superheater outlet Header

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 36

    GB ENGINEERING Rev. 00

    tS82.1

    DPK

    Sheet 37

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    Compensation check calculation as per ASME Section - I, PG - 33

    Item

    Drg. No.

    Item No.

    Shell Data:

    Minimum Thickness of Shell t

    Required Thickness of Seamless Shell tr

    Max. allowable stress at design temp. Sv

    Finished Diameter of opening d

    Nozzle Data

    Nozzle OD

    Nominal Thickness of Nozzle tn

    Required Thickness of Seamless Nozzle tnr

    Material Specification

    Max. allowable stress at design temp. Snfr1 = ( Sn / Sv )

    Actual projection of nozzle I.S. of the dished head

    2.5 x t

    2.5 x tn

    Minimum of 2.5 t and 2.5 tnActual projection of nozzle I.S. of the shell

    F = Correction factor

    Compensation available in dished head

    ( d - 2 tn ) ( t - F t r)

    2 t ( t - F t r)

    A1 = max. ( i, ii ) A1

    Compensation available in Nozzle

    2 ( tn - trn ) ( 2.5 t fr1 )

    2 ( tn

    - trn

    ) ( 2.5 tn

    + te

    ) fr1

    A2 = min. ( i, ii ) A2

    Compensation available in nozzle from inside projection

    h = Projection of nozzle inside the shell

    A3 = 2 tn fr1 h A3

    Compensation available in reinforcement element

    Outer diameter of the reinforcement element Dp

    Thickness of the reinforcement element te

    Max.allowable stress at Design temp. Spfr3 = Sp / Sv fr3

    A5 = ( Dp - d - 2 tn ) te fr3 A5

    Total Compensation Area available

    A avail = A1 + A2 + A3 + A5 mm2 2303.07

    0.00

    mm2 0.00

    12

    mm 0.00

    mm 0.00

    kPa 0 0.00 kg/cm2

    10

    mm 0.00

    mm2 0.00

    11

    09

    mm2 1515.57

    mm

    2 1837.50

    mm2 1515.57

    08

    mm2 787.50

    mm2 360.85

    mm2 787.50

    mm 51.5506 mm 0.00

    07 1.00

    05 mm 0.00

    mm 51.55

    mm 62.50

    kPa 75671.753 771.64 kg/cm2

    04 1.00

    mm 10.30

    SA 182 F11 CL.1

    03

    mm 190.00

    mm 25.00

    kPa 75671.753 771.64 kg/cm2

    mm 140.00

    02

    mm 20.62

    mm 11.87

    01 Outlet Stub

    MFB-F-10-05-07-0001

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    SERIAL No.#REF!

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 37

    GB ENGINEERING Rev. 00

    Sheet 38

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    06 Calculation of End plate thickness Under Internal Pressure As Per PG - 31.3

    Item

    Drg. No.

    Var. No./Item No.

    Design Pressure P

    Design Temperature

    Corrosion Allowance C.AEnd plate data

    Material Specification

    Inside diameter of the Header d

    Provided Thickness of End Plate t

    Allowable Stress value at design temperature S

    Header data

    Actual thicknes of header ts

    Min. required thickness of seamless header tr

    C = Calculation factor as per Fig [ PG-31 (g-1) ]

    m = tr/ ts

    0.33 m

    C = 0.33m with a minimum of 0.2

    Selected 'C' C

    Minimum required thickness of end plate

    Required Thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    15 mm 34.00

    16 Hence Satisfactory

    REV.NO. DESCRIPTION PREPARED CHECKED APPROVED

    mm 26.77

    14 mm 26.77

    mm 0.20

    12 mm 0.20

    13

    11

    mm 0.50

    mm 0.16

    09 mm 20.62

    10 mm 10.30

    07 mm 35.00

    08 kPa 75671.753 771.64 kg/cm2

    04 mm 1.00

    05 SA 182 F11 CL.1

    06 mm 177.86

    02 bar (a) 85.73 87.420 kg/cm2(a)

    03 oC 501

    01 Outlet header end plate

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 38

    GB ENGINEERING Rev. 00

    S

    PCdt min

    STRESS CALCULATIONSheet 39

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    06 Calculation of End plate thickness Under Internal Pressure As Per UG - 34

    Item

    Drg. No.

    Var. No./Item No.

    Design Pressure P

    Design Temperature

    Corrosion Allowance C.A

    End plate data

    Material Specification

    Inside diameter of the Header d

    Provided Thickness of End Plate t

    Allowable Stress value at design temperature S

    Header data

    Actual thicknes of header ts

    Min. required thickness of seamless header tr

    C = Calculation factor as per Fig [ UG-34 (b-2) & UW-13.3 (b)]

    m = tr / ts

    0.33 m

    C = 0.33m with a minimum of 0.2

    Selected 'C' C

    Minimum required thickness of end plate

    Required Thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    15 mm 19.00

    16 Hence Satisfactory

    mm 12.04

    14 mm 12.04

    12 mm 0.20

    13

    11

    mm 0.50

    mm 0.16

    mm 0.20

    09 mm 20.62

    10 mm 10.30

    07 mm 20.00

    08 kPa 75671.753 771.64 kg/cm2

    04 mm 1.00

    05 SA 182 F11 CL.1

    06 mm 80.00

    02 bar (a) 85.73 87.420 kg/cm2(a)

    03 oC 501

    01 Outlet header end Cap

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 39

    GB ENGINEERING Rev. 00

    SPCdt min

    STRESS CALCULATIONSheet 40

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    06 Calculation of End plate thickness Under Internal Pressure As Per UG - 34

    Item

    Drg. No.

    Var. No./Item No.

    Design Pressure P

    Design Temperature

    Corrosion Allowance C.A

    End plate data

    Material Specification

    Inside diameter of the Header d

    Provided Thickness of End Plate t

    Allowable Stress value at design temperature S

    Header data

    Actual thicknes of header ts

    Min. required thickness of seamless header tr

    C = Calculation factor as per Fig [ UG-34 (b-2) & UW-13.3 (b)]

    m = tr / ts

    0.33 m

    C = 0.33m with a minimum of 0.2

    Selected 'C' C

    Minimum required thickness of end plate

    Required Thickness

    t = Minimum thickness available - C.A t

    Provided Min. Thickness > Required Thickness

    15 mm 19.00

    16 Hence Satisfactory

    mm 10.45

    14 mm 10.45

    12 mm 0.20

    13

    11

    mm 0.50

    mm 0.16

    mm 0.20

    09 mm 20.62

    10 mm 10.30

    07 mm 20.00

    08 kPa 75671.753 771.64 kg/cm2

    04 mm 1.00

    05 SA 182 F11 CL.1

    06 mm 69.42

    02 bar (a) 85.73 87.420 kg/cm2(a)

    03 oC 501

    01 Outlet header drain end Cap

    MFB-F-10-05-07-0001

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    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONSheet 40

    GB ENGINEERING Rev. 00

    SPCdt min

    STRESS CALCULATIONSheet 41

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    07 Calculation of Stress at Hydrostatic Test Pressure (PG -99)

    Item

    Drg. No.

    Var. No./Item No.

    Hydrostatic test Pressure Ph

    End plate data

    Material Specification

    Inside diameter of the Header d

    Minimum Thickness of End Plate t

    Minimum yield strength at Ambient temp. Y

    Selected 'C' C

    Stress during Hydrostatic Test Pressure

    ( 0.9 x Y) 90% of Yield Strength (as per PG-99) t

    ( 0.9 x Y ) > Shydro10 Hence Satisfactory

    kg/cm2

    09 kPa 225000 2294.37 kg/cm2

    08

    kPa 66415.83 677.26

    06 kPa 205000 2090.43 kg/cm2

    07 mm 0.20

    04 mm 177.86

    05 mm 35.00

    02 bar (a) 128.60 131.130 kg/cm2(a)

    03 SA 182 F11 CL.1

    01 Outlet header end plate

    MFB-F-10-05-07-0001

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    Enterprises Pvt.Ltd Equip. SECONDARY SUPPERHEATERMFR'S

    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONGB ENGINEERING Rev. 00

    2

    h

    2

    hydrot

    PCdS

    STRESS CALCULATIONSheet 42

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or thethickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    Minimum groove size

    tw = tn but not less than 1/4"

    Required tw

    Provided tw

    Required tw < Provided tw11 Hence Satisfactory

    08

    09 mm 6.00

    10 mm 6.50

    mm 5.50

    07 Hence Satisfactory

    mm 3.15

    mm 3.15

    05

    06 Sketch (z)

    mm 4.50

    04

    02 mm 20.62

    03 mm 4.50

    01 Inlet header to panal stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONGB ENGINEERING Rev. 00

    STRESS CALCULATIONSheet 43

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or thethickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    mm 17.50

    07 Hence Satisfactory

    mm 9.99

    mm 9.99

    05

    06 Sketch (a)

    mm 14.27

    04

    02 mm 14.27

    03 mm 14.27

    01 outlet header to riser stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/038

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONGB ENGINEERING Rev. 00

    STRESS CALCULATIONSheet 44

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    08 Minimum requirements for attachments weld as per PW - 16

    Item

    Drg. No.

    Var. No./Item No.

    Minimum thickness of Shell t

    Nominal thickness of Stub tn

    Conditions

    tmin = the smaller of 3/4 in. (19 mm) or thethickness of either of the weld parts (t,tn)

    tc = Not less than the smaller of 1/4 in. or 0.7 tmin

    Applicable Sketch from Fig.PW-16.1

    tmin

    0.7 tmin

    Required tc

    Provided tc

    Required tc < Provided tc

    mm 14.00

    07 Hence Satisfactory

    mm 13.30

    mm 13.30

    05

    06 Sketch (a)

    mm 19.00

    04

    02 mm 20.62

    03 mm 20.00

    01 outlet header to inspection stub

    MFB-F-10-05-07-0001

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    SERIAL No.GBE/XXXX/XXX

    S.No. DESCRIPTION Units Data

    STRESS CALCULATIONGB ENGINEERING Rev. 00

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    P = Design Pressure in Kg/cm ds = Inside Diameter of End Plate in mm b = Smaller value of ( 2.5 * ts or 2.5 * tn )

    dn = Inside Diameter of Nozzle in mm ts = Actual Thickness of End Plate in mm bi = Inside Projection of Nozzle

    tn = Actual Thickness of Nozzle in mm es = Equivalent Thickness of End Plate in mm Ci = ts + 76 or Dn/2 , whichever is greater

    en = Equivalent Thickness of Nozzle in mm fs = Allowable Stress of End Plate in kg/cm2 Cw = Fillet Weld area

    fn = Allowable Stress of Nozzle in kg/cm2 E = 1 = 0 [ It is not considered since it is negligible]

    Dn = Opening Diameter in mm

    Minimum Required Thickness for End Plate, es = [ ( dn * ( P * K / fs ) ^ 0.5 ) + 1 ]

    Minimum Thickness Required for Nozzle, en = [ ( P * dn ) / ( 2 * fn * E - P ) ] + 0.762

    Area Removed X = Dn * esArea Available Y = [ 2 * ( tn - en ) * b * ( fn / fs ) ] + [ 2 * tn * bi * ( fn / fs ) ] + [ 2 * ( ts - es ) * Ci ] + CW,

    P Design fn Dn dn tn fs ds ts es en b bi Ci X Y

    k /cm2 Temp.C k /cm

    2 mm mm mm k /cm2 mm mm mm mm mm mm mm mm

    2mm

    2

    01 MFB-F-10-05-07-0001 09 87.42 501 SA 335 GR.P22 771.64 24.3 24.3 3.98 771.64 69.42 20.00 11.18 2.22 9.95 0 96 271.67 1728.46

    Remarks : Area Available ( Y ) > Area Removed ( X ) , Hence, It is satisfactory

    Prepared : D.Gunasekaran Checked : A.Shaheb john

    Sl.

    No.Drawing No.

    Item

    No.

    Material

    specification

    G.B. ENGINEERING ENTERPRISES PRIVATE LIMITED,

    TIRUCHIRAPPALLI.

    PROJECT : M/s. SIAM CRYSTAL RICE COMPANY BOILER MAKER'S No. : GB- XXX Page : 07 of 07

    CALCULATION OF NOZZLE COMPENSATION FOR END PLATE AS PER IBR - 279