The Drop for this Nozzle is : 1.3275 in

The Cut Length for this Nozzle is, Drop + Ho + H + T : 4.4525 in

PVElite is a registered trademark of COADE, Inc. [2009]

FileName

FileName : : Sample Sample 4.1 4.1 --- --- Page Page 45 45 of of 6262 Nozzle

Nozzle Calcs. Calcs. : : N1 N1 Nozl: Nozl: 3 3 8:15a 8:15a Apr Apr 15,201015,2010

INP

INP UT UT VALUES, VALUES, Nozzle Nozzle Description: Description: N1 N1 From From : : 2020

Pressure

Pressure for for Reinforcement Reinforcement Calculations Calculations P P 150.631 150.631 psigpsig Temperature

Temperature for for Internal Internal Pressure Pressure Temp Temp 120 120 FF Shell

Shell Material Material SA-516 SA-516 7070 Shell

Shell Allowable Allowable Stress Stress at at Temperature Temperature S S 20000.00 20000.00 psipsi Shell

Shell Allowable Allowable Stress Stress At At Ambient Ambient Sa Sa 20000.00 20000.00 psipsi Inside

Inside Diameter Diameter of of Cylindrical Cylindrical Shell Shell D D 59.0000 59.0000 inin Shell

Shell Finished Finished (Minimum) (Minimum) Thickness Thickness t t 0.5000 0.5000 inin Shell

Shell Internal Internal Corrosion Corrosion Allowance Allowance c c 0.1250 0.1250 inin Shell

Shell External External Corrosion Corrosion Allowance Allowance co co 0.0000 0.0000 inin Distance

Distance from from Bottom/Left Bottom/Left Tangent Tangent 115.5000 115.5000 inin User

User Entered Entered Minimum Minimum Design Design Metal Metal Temperature Temperature -20.00 -20.00 FF

Type of Element Connected to the Shell : Nozzle

Material

Material SA-106 SA-106 BB

Material

Material UNS UNS Number Number K03006K03006 Material

Material Specification/Type Specification/Type Smls. Smls. pipepipe Allowable

Allowable Stress Stress at at Temperature Temperature Sn Sn 17100.00 17100.00 psipsi Allowable

Allowable Stress Stress At At Ambient Ambient Sna Sna 17100.00 17100.00 psipsi Diameter

Diameter Basis Basis (for (for tr tr calc calc only) only) ODOD Layout

Layout Angle Angle 0.00 0.00 degdeg

Diameter

Diameter 4.0000 4.0000 in.in.

Size

Size and and Thickness Thickness Basis Basis ActualActual Actual

Actual Thickness Thickness tn tn 0.4650 0.4650 inin Flange

Flange Material Material SA-105SA-105 Flange

Flange Type Type Slip Slip onon

Corrosion

Corrosion Allowance Allowance can can 0.1250 0.1250 inin Joint

Joint Efficiency Efficiency of of Shell Shell Seam Seam at at Nozzle Nozzle E1 E1 1.001.00 Joint

Joint Efficiency Efficiency of of Nozzle Nozzle Neck Neck En En 1.001.00 Outside

Outside Projection Projection ho ho 5.0000 5.0000 inin Weld

Weld leg leg size size between between Nozzle Nozzle and and Pad/Shell Pad/Shell Wo Wo 0.3750 in0.3750 in Groove

Groove weld weld depth depth between between Nozzle Nozzle and and Vessel Vessel Wgnv Wgnv 0.5000 0.5000 inin Inside

Inside Projection Projection h h 0.0000 0.0000 inin Weld

Weld leg leg size, size, Inside Inside Element Element to to Shell Shell Wi Wi 0.0000 0.0000 inin ASME

ASME Code Code Weld Weld Type Type per per UW-16 UW-16 CC Class

Class of of attached attached Flange Flange 150150 Grade

Grade of of attached attached Flange Flange GR GR 1.11.1

The Pressure Design option was Design Pressure + static head.

Nozzle Sketch

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FileName

FileName : : Sample Sample 4.1 4.1 --- --- Page Page 46 46 of of 6262 Nozzle

Nozzle Calcs. Calcs. : : N1 N1 Nozl: Nozl: 3 3 8:15a 8:15a Apr Apr 15,201015,2010 ____________/| | ____________/| | | | \ \ | | || | | \ \ | | || |____________\|__| |____________\|__|

Insert Nozzle No Pad, no Inside projection

Reinforcement CALCULATION, Description: N1 Reinforcement CALCULATION, Description: N1

ASME Code, Section VIII, Division 1, 2007, A-08 UG-37 to UG-45

Actual

Actual Outside Outside Diameter Diameter Used Used in in Calculation Calculation 4.000 4.000 in.in. Actual

Actual Thickness Thickness Used Used in in Calculation Calculation 0.465 0.465 in.in.

Nozzle input data check completed without errors.

Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press] Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1) = (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (150.63*29.6250)/(20000*1.00-0.6*150.63) = (150.63*29.6250)/(20000*1.00-0.6*150.63) = 0.2241 in

= 0.2241 in

Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press] Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]

= (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1) = (P*Ro)/(S*E+0.4*P) per Appendix 1-1 (a)(1) = (150.63*2.0000)/(17100*1.00+0.4*150.63) = (150.63*2.0000)/(17100*1.00+0.4*150.63) = 0.0176 in

= 0.0176 in

UG-40, Limits of Reinforcement : [Int. Press]

Parallel

Parallel to to Vessel Vessel Wall Wall (Diameter (Diameter Limit) Limit) Dl Dl 6.6400 6.6400 inin Parallel

Parallel to to Vessel Vessel Wall Wall d d 3.3200 3.3200 inin Normal

Normal to to Vessel Vessel Wall Wall (Thickness (Thickness Limit), Limit), no no pad pad Tlnp Tlnp 0.8500 0.8500 inin

Weld Strength Reduction Factor [fr1]:

= min( 1, Sn/S ) = min( 1, Sn/S ) = min( 1, 17100.0 /20000.0 ) = min( 1, 17100.0 /20000.0 ) = 0.855 = 0.855

Weld Strength Reduction Factor [fr2]:

= min( 1, Sn/S ) = min( 1, Sn/S ) = min( 1, 17100.0 /20000.0 ) = min( 1, 17100.0 /20000.0 ) = 0.855 = 0.855

Weld Strength Reduction Factor [fr3]:

= min( fr2, fr4 ) = min( fr2, fr4 ) = min( 0.9 , 1.0 ) = min( 0.9 , 1.0 ) = 0.855 = 0.855

Results of Nozzle Reinforcement Area Calculations:

AREA

AREA AVAILABLE, AVAILABLE, A1 A1 to to A5 A5 Design Design External External MapncMapnc Area

Area Required Required Ar Ar 0.766 0.766 NA NA NA NA in²in² Area

Area in in Shell Shell A1 A1 0.486 0.486 NA NA NA NA in²in² Area

Area in in Nozzle Nozzle Wall Wall A2 A2 0.469 0.469 NA NA NA NA in²in² Area

Area in in Inward Inward Nozzle Nozzle A3 A3 0.000 0.000 NA NA NA NA in²in² Area

Area in in Welds Welds A41+A42+A43 A41+A42+A43 0.120 0.120 NA NA NA NA in²in² Area

Area in in Element Element A5 A5 0.000 0.000 NA NA NA NA in²in² TOTAL

TOTAL AREA AREA AVAILABLE AVAILABLE Atot Atot 1.075 1.075 NA NA NA NA in²in²

The Internal Pressure Case Governs the Analysis.

Nozzle

FileName

FileName : : Sample Sample 4.1 4.1 --- --- Page Page 47 47 of of 6262 Nozzle

Nozzle Calcs. Calcs. : : N1 N1 Nozl: Nozl: 3 3 8:15a 8:15a Apr Apr 15,201015,2010

In document Sample4_PVElite (Page 48-51)