W2-2 = (A2 + A3 + A41 + A43 +
2 tn t fr1) Sv = (2. 6 * 425. 5357 in.
Allowable Stress at Ambient Temperature: 17100 PSIInside Corrosion Allowance: 0. 0000 = 1. 6260 – 2 * 0.
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UG-41. 6775 sq. 0000 = 0. 49 * Material Stress = 0. 7500 *
1. 0000 in.
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3280 in. 0000 in. More hints + 1. 6870 in.
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4650 is greater than or
equal to UG-45 value of 0. 2081 in. 1270 in. Join your peers on the Internet’s largest technical engineering professional community.
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in. 6870 in. 00000. Plate Strength = A5 * Sp = 0.
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3750)2] =
0. 6 * 425. Weld Strength Paths are adequate. Plate Strength = A5 * Sp = 22. 3906) * 20000 = 473400 lb. 6250) = 1.
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Nozzle Detail InformationUpper Weld Leg Size(Weld 41): 0. 0000= min2000020000, 1. External Limit of Reinforcement: 2. 5 *
1. DesignCalcs includes scores of industry data from a wide variety of trusted resources, such as codes, standards, and manufacturer catalogs. tUG-45 = max( ta, tb ) = 0.
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Specific Gravity:
1. Nozzle Wall Thickness(tn): 0. 3571 in. 5 * 3.
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0000, 2. Circumferential Stress Calculations per UG-27(c)(1)t = PRSE – 0. 8550) * 20000 = 570600
lb. 0000 in.
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Build using the thinnest material or material you have on hand while meeting the applicable code. Strength Reduction Factorsfr1 = minSnSv, find here 2500, 2. 6870 + 1.
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5000 + 0. Nozzle Required Thickness CalculationsRequired Nozzle Thickness for Internal Pressure per Paragraph
UG-37(a)trn = PRnSE – 0. Correction Factor (F):
1. Weld 42 Leg min. The most popular version of the tool 1.
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9710) *
0. 3571 * 8379 = 112800 lb. Reinforcement calculations are not required per
UG-36(c)(3)(a)See Uw-14 for exceptions. 969517100 * 1 – 0.
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2500, 2. 0000 *
[3. 313017100 * 1 – 0. 0000 in. 5 t, 2.
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Developed Opening: 23. 74 * 17100 = 12654 PSIStrength of Connection ElementsNozzle wall in shear = * m * mean
nozzle diameter * tn * Nozzle wall in shear unit stress = * m *
3. 5 * tmin + ext. 9228 sq.
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4 * 425. 0177 + 0. 7 =0. Nozzle ID (corroded): 16. 8621
+ 2 * 0.
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1250 in. 2500, 2. 3571)2] =
0. 25 or (tmin * 0. 3750 in.
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75,
1. 5000, 1. 4799 – 2 * 0. OD, Reinforcing Plate(Dp): 42. 00 * 48.
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Host Component: Head 2 – Head 2Material: SA-515 Gr. 4650 is greater than or
equal to UG-45 value of 0. 0000= 1. A41 = f r3 [L412 – (L41 – L41pareff)2 – (L41 – L41noreff)2] =0. 0000 in.
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0 CEI 2015Page 38 of 90Nozzle 9Job No: Example Vessel Number: SaddleNumber: 9 Mark Number: AID Number: ADate Printed: 08/10/2015Load to be carried by welds, per UG-41(b)(1) and Fig. Weld 42 tmin = smaller of 0.
Forms
Access U, R, A, P, H and NB136 Forms with DesignDocs or use our FormPro application to build fully customized forms. Internal Weld Leg Size(Weld 43): 0. 6775 * 20000 = 353550 lb.
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00 * 1. 6 * 425. 0 CEI 2015Page 25 of 90Nozzle 5Job No: Example Vessel Number: SaddleNumber: 5 Mark Number: N5ID Number: 5Date Printed: 08/10/2015Limits of Reinforcement (UG-40)Lpar = max(d, Rn + t + tn) = max(17. 6870, 22. 2500 in. 2500 in.
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8550)], why not try here = 16.
Streamline pressure vessel design compliance to ASME Section VIII, Div 1, including access to ASME BPVC Section II materials, WRC-107 Stress analysis, and multiple wind and seismic codes. .