d-712 lol

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Available nozzle wall thickness new, t n = 0.875*0.688 = 0.602 in The nozzle neck thickness is adequate. External Pressure, (Corroded & at 450 °F) UG-28(c) L / D o = 16.9932 / 12.75 = 1.3328 D o / t = 12.75 / 0.0506 = 252.0895 From table G: A = 0.000246 From table CS-2: B = 3,317.7143 psi P a = 4*B / (3*(D o / t)) = 4*3,317.71 / (3*(12.75 / 0.0506)) = 17.55 psi Design thickness for external pressure P a = 17.55 psi t a = t + Corrosion = 0.0506 + 0.125 = 0.1756" 50/262

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  • Available nozzle wall thickness new, tn = 0.875*0.688 = 0.602 in

    The nozzle neck thickness is adequate.

    External Pressure, (Corroded & at 450 F) UG-28(c)

    L / Do = 16.9932 / 12.75 = 1.3328Do / t = 12.75 / 0.0506 = 252.0895From table G: A = 0.000246From tableCS-2: B = 3,317.7143 psi

    Pa = 4*B / (3*(Do / t))= 4*3,317.71 / (3*(12.75 / 0.0506))= 17.55 psi

    Design thickness for external pressure Pa = 17.55 psi

    ta = t + Corrosion = 0.0506 + 0.125 = 0.1756"

    50/262

  • VENT (V)

    ASME Section VIII Division 1, 2013 Edition

    Note: round inside edges per UG-76(c)Location and Orientation

    Located on Top Head

    Orientation 0

    End of nozzle to datum line 212"

    Calculated as hillside Yes

    Distance to head center, R 20"

    Passes through a Category A joint NoNozzle

    Description NPS 6 (Thk = 0.375")Access opening No

    Material specification SA-106 B Smls pipe (II-D p. 14, ln. 19)Inside diameter, new 5.875"

    Nominal wall thickness 0.375"

    Corrosion allowance 0.125"

    Opening chord length 7.9106"

    Projection available outside vessel, Lpr 5.4138"Projection available outside vessel to flange face, Lf 8.9138"Local vessel minimum thickness 0.4375"

    Liquid static head included 0 psi

    Longitudinal joint efficiency 1Reinforcing Pad

    Material specification SA-516 70 (II-D p. 22, ln. 6)

    51/262

  • Diameter, Dp 11.4603"

    Thickness, te 0.4375"

    Is split No

    Welds

    Inner Fillet, Leg41 0.5"

    Outer Fillet, Leg42 0.325"

    Nozzle to vessel groove weld 0.375"

    Pad groove weld 0.375"

    ASME B16.5-2009 Flange

    Description NPS 6 Class 150 WN A105

    Bolt Material SA-193 B7 Bolt

  • UCS-66 Material Toughness Requirements Pad

    Governing thickness, tg = 0.4375"

    Exemption temperature from Fig UCS-66 Curve B = -13F

    tr = 150*48.25*0.993145 / (2*20,000*1 - 0.2*150) = 0.1798"Stress ratio = tr*E* / (tn - c) = 0.1798*1 / (0.4375 - 0.125) = 0.5755Reduction in MDMT, TR from Fig UCS-66.1 = 45.1F

    MDMT = max[ MDMT - TR, -55] = max[ -13 - 45.1 , -55] = -55FMaterial is exempt from impact testing at the Design MDMT of -20F.

    53/262

  • Reinforcement Calculations for MAWP

    The thickness requirements of UG-45 govern the MAWP of this nozzle.

    UG-37 Area Calculation Summary (in2) UG-45Summary (in)For P = 169.43 psi @ 450 F

    The opening is adequately reinforcedThe nozzle passes

    UG-45

    Arequired

    Aavailable A1 A2 A3 A5

    Awelds treq tmin

    1.6217 2.7614 0.8572 0.2932 -- 1.3125 0.2985 0.3281 0.3281

    UG-41 Weld Failure Path Analysis Summary (lbf)All failure paths are stronger than the applicable weld loads

    Weld loadW

    Weld loadW1-1

    Path 1-1strength

    Weld loadW2-2

    Path 2-2strength

    Weld loadW3-3

    Path 3-3strength

    16,224.77 38,084 87,302.1 12,393.88 139,858.5 40,755.88 95,839.87

    UW-16 Weld Sizing Summary

    Weld description Required weldsize (in)

    Actual weldsize (in) Status

    Nozzle to pad fillet (Leg41) 0.175 0.35 weld size is adequate

    Pad to shell fillet (Leg42) 0.1562 0.2275 weld size is adequate

    Nozzle to pad groove (Upper) 0.175 0.375 weld size is adequate

    Nozzle to shell groove (Lower) 0.175 0.25 weld size is adequate

    Calculations for internal pressure 169.43 psi @ 450 F

    Parallel Limit of reinforcement per UG-40

    LR = MAX(d, Rn + (tn - Cn) + (t - C))= MAX(7.9106, 3.9553 + (0.375 - 0.125) + (0.4375 - 0.125))= 7.9106 in

    Outer Normal Limit of reinforcement per UG-40

    LH = MIN(2.5*(t - C), 2.5*(tn - Cn) + te)= MIN(2.5*(0.4375 - 0.125), 2.5*(0.375 - 0.125) + 0.4375)= 0.7813 in

    Nozzle required thickness per UG-27(c)(1)

    trn = P*Rn / (Sn*E - 0.6*P)= 169.4262*3.0625 / (17,100*1 - 0.6*169.4262)= 0.0305 in

    54/262