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Code: ASME VIII-1 Year: 2007 Cust: N/A Addenda: 2009 File: PVEfea-4431-6.1 MAWP: 300 psi Desc: Hydraulic Manifold Block MEAWP: 0 psi Dwg: PVEdwg-4431-6.1 Max. Temp.: 250 °F Date: MDMT: -20 °F MDMT Press.: 300 psi Min. Thk. (UG-16b): 0.0625 Corrosion Allowance: 0 in Hydrotest: 390 psi Impact Testing: None Impact Exemption: UHA-51(d) Radiography: None Internal Press.: Yes External Press.: No Vessel Weight: No Weight of Attachments: No Attachment of Internals: No Attachment of Externals: No Cyclic or Dynamic Reactions: No Wind Loading: No Seismic Loading: No Fluid Impact Shock Reactions: No Temperature Gradients: No Differential Thermal Expansion: No Author: Cameron Moore Abnormal Pressures: No Reviewer: Laurence Brundrett, P. Eng. Hydrotest Loads: No Pressure Vessel Engineering Ltd. ASME Calculations - CRN Assistance - Vessel Design - Finite Element Analysis Design Conditions UG-22 Loadings Considered Pressure Vessel Engineering Ltd. 120 Randall Drive, Suite B Waterloo, Ontario, Canada, N2V 1C6 www.pveng.com [email protected] Phone 519-880-9808 Finite Element Analysis Report - VIII-1 Conclusion: The Hydraulic Manifold Block PVEdwg- 4431-6.0 is acceptable for ASME VIII-1 use at 300 psi and 250˚F. December 13, 2011 PVEng

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Page 1: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Code: ASME VIII-1

Year: 2007 Cust: N/A

Addenda: 2009 File: PVEfea-4431-6.1

MAWP: 300 psi Desc: Hydraulic Manifold Block

MEAWP: 0 psi Dwg: PVEdwg-4431-6.1

Max. Temp.: 250 °F Date:

MDMT: -20 °F

MDMT Press.: 300 psi

Min. Thk. (UG-16b): 0.0625

Corrosion Allowance: 0 in

Hydrotest: 390 psi

Impact Testing: None

Impact Exemption: UHA-51(d)

Radiography: None

Internal Press.: Yes

External Press.: No

Vessel Weight: No

Weight of Attachments: No

Attachment of Internals: No

Attachment of Externals: No

Cyclic or Dynamic Reactions: No

Wind Loading: No

Seismic Loading: No

Fluid Impact Shock Reactions: No

Temperature Gradients: No

Differential Thermal Expansion: No Author: Cameron Moore

Abnormal Pressures: No Reviewer: Laurence Brundrett, P. Eng.

Hydrotest Loads: No

Pressure Vessel Engineering Ltd.ASME Calculations - CRN Assistance - Vessel Design - Finite Element Analysis

Design Conditions

UG-22 Loadings Considered

Pressure Vessel Engineering Ltd.

120 Randall Drive, Suite B

Waterloo, Ontario, Canada, N2V 1C6

www.pveng.com

[email protected]

Phone 519-880-9808

Finite Element Analysis Report - VIII-1

Conclusion: The Hydraulic Manifold Block PVEdwg-

4431-6.0 is acceptable for ASME VIII-1 use at 300 psi

and 250˚F.

December 13, 2011

PVEng

Page 2: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Table of Contents 13-Dec-11 Page 2 of 13

Description Page Description Page

Cover 1 Restraints 8

Table of Contents 2 Loads 9

Executive Summary 3 Reaction Forces 10

Stress Limits 4 Displacement 11

Model 5 Stress 12

Mesh 6 Stress 13

Error 7

Rev Date By

0 12-Aug-10 CBM

1 13-Dec-11 CBM

Revision(s)

Description

Release

Update Report Captions

Page 3: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Executive Summary ver 4.00 Page 3 of 13

Goal:

Summary Conclusions:

Analysis Software

Analysis Type

Materials

Model and Mesh

Restraints & Loads

Results

Analysis Conclusion:

Material strength properties used in this report are obtained from ASME IID, Table 1A, and are suitable

for VIII-1 components. The rules of ASME VIII-2 are used to set the stress limits.

The Hydraulic Manifold Block PVEdwg-4433-6 will be used under ASME VIII-1 service. This block

cannot be calculated to ASME VIII-1 code rules due to the complexity of its geometry. The rules of VIII-2

are used with VIII-1 allowed stresses to determine the acceptability.

The Hydraulic Manifold Block PVEdwg-4431-6.1 is acceptable for ASME VIII-1 use at 300 psi and 250˚F.

One pipe is fixed; this prevents translation of the model in all three primary planes. The interior cavities

and attached pipes are pressurized to 300 psi. When calculated theoretically, the actual reaction forces

prove acceptable. The model is in balance and can be used for displacement and stress analysis.

The model has a maximum displacement of 0.0017". The displaced shape of the model is as expected

and the magnitude of the displacement is acceptable. The model has a maximum peak stress of 3,043

psi. All stresses in the model are below the primary general membrane stress limit of 20,000 psi and is

acceptable for ASME VIII-1 use.

The model used in this report represents the full hydraulic manifold block. Pipes are added in to transfer

axial loads to the openings and simulate the effect of a closed loop piping system. A 0.125" second

order tetrahedral mesh has been applied globally to the entire model. This results in an error of under 5%

and is therefore valid. The reported reaction forces match those computed theoretically. The model is in

balance and can be used for displacement analysis.

SolidWorks Simulation 2010 SP4.0

A static linear elastic study is performed using small displacement theory.

Page 4: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Material Stress Limits ver 4.02 ASME VIII-2 Fig 5.1 Page 4 of 13

Material Input Chart:

Temperature [ºF]

Material 1 Material 2 Material 3 Material 4

Material = SA-479 316 SA-312 TP316 SA-403 316

Application = Manifold Block Attached Pipes Pipe Caps

Sm [psi] = 20,000 20,000 20,000

Sy [psi] = 24,600 24,600 24,600

Sya [psi] = 30,000 30,000 30,000

Sta [psi] = 75,000 75,000 75,000

E1 = 1.0 1.0 1.0

E2 = 1.0 1.0 1.0

E [psi] = 27,250,000 27,250,000 27,250,000

v = 0.30 0.30 0.30

Coef =

Pm [psi] = 20,000 20,000 20,000

Pl [psi] = 30,000 30,000 30,000

Pl+Pb [psi] = 30,000 30,000 30,000

Pl+Pb+Q [psi] = 60,000 60,000 60,000

Prop. Sources

Comments

Variable Descriptions: VIII-2 5.13

Sm (basic allowable) Sya (yield strength at ambient temp.)

Sta (tensile strength at ambient temp.) E (modulus of elasticity) - IID Table TM-1

E1 (weld efficiency) v (Poison's ratio) - IID Table PRD

E2 (casting efficiency) Coef (coefficient of thermal expansion)

Stress Limit Equations: VIII-2 Figure 5.1

Pm =

Pm =

Pl =

Pl+Pb =

Pl+Pb =

Pl+Pb+Q =

Pl+Pb+Q+F = Use fatigue curves~~peak stress intensity limit

Comments:(1) Sy material property is not required, more conservative Pl+Pb+Q limits might be computed without it.

(2) The thermal expansion coefficient is only required for studies including thermal stresses

(3) Refer to VIII-2 5.15 Figure 5.1 and following for the Pm, Pl, Q and F stress limits

(4) Refer to VIII-2 5.14 Table 5.6 for the correct application of the calculated stress limits

(5) Use IID tables 5A and 5B for Sm for VIII-2 studies

(6) Use IID tables 1A and 1B for Sm values (S) for VIII-1 studies

(7) Use B31.1 Table A for Sm values for B31.1 studies

(8) Use B31.3 Table A for Sm values for B31.3 studies

(9) 2*Sy Pl+Pb+Q not valid went in creep range.

Max(3*E1*E2*Sm,2*E1*E2*Sy)~~primary + secondary stress intensity (2*Sy only valid for Sya/Sta <=0.7)

ASME II-D 2007 Edition, 2009 Addenda

1.5*E1*E2*Sm~~primary membrane + primary bending stress intensity limit (material only)

E1*E2*Sm~~general primary membrane stress intensity limit (material only)

1.5*E1*E2*Sm~~local membrane stress intensity limit

2*Sm~~general primary membrane stress intensity limit (bolting combine operation +seating)

3*Sm~~primary membrane + primary bending stress intensity limit (bolting combine operation + seating)

Page 5: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Model Page 5 of 13

Assembled Model

Assembled view of (Fig-1) with pipes attached to the block. Refer to PVEdwg-4431-6.1 for dimensional

details.

Exploded Model

Exploded view of the hydraulic manifold block. A complete solid model matching the hydraulic manifold block

geometry is used in the analysis. A fixed pipe is modeled in as a method of restraint. Capped pipes are attached

to each of the openings to transmit axial loads generated in a closed loop system. Stresses in the attached pipes

are not analyzed and are outside the scope of this report.

Fixed Pipe

Fig-1

Fig-2

Page 6: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Mesh Page 6 of 13

Mesh Plot

View of the mesh applied to the model.

A 0.125" size with second order tetrahedral solid elements is been applied.

Mesh Rotated Close-up

A close-up of the mesh rotated to show the opposite side of the model. All components are treated as bonded

connections and are meshed as a single body.

Fig-3

Fig-4

Page 7: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Error Page 7 of 13

Mesh Error Plot

A view of the error plot with the mesh overlaid.

No general areas observe error in excess of 5%. The error plot justifies the mesh selected. The model may be

used for further analysis.

Mesh Error Close-up

A close-up of the manifold line in area.

Note that error in excess of 5% is limited to locations of discontinuity.

Error exceeds 5% at areas of discontinuity

Fig-5

Fig-6

Page 8: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Restraints Page 8 of 13

Fixed Restraint

A fixed restraint is applied to the end face of the "line in" pipe. Applying the restraint to the pipe end allows the

Hydraulic Manifold Block to deform as it would in reality.

Fixed Restraint Close-up

A close-up of (Fig-7). The fixed restraint prevents translation of the model is the X, Y and Z directions.

The model is fully restrained from rigid body motion in all three directions.

Fig-7

Fig-8

Page 9: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Loads Page 9 of 13

Internal Pressure

300 psi is applied to all internal faces of the manifold and attached pipes.

Internal Pressure (Sectioned View)

A sectioned view of (Fig-9).

Fig-9

Fig-10

Page 10: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Reaction Forces ver 4.09 Page 10 of 13

300 P [psi] - Pressure

X Axis: reaction forces on the YZ plane caused by loads in the X direction

3.356 XArea [in2] - Pressurized area on YZ plane

0.0 XForce [lbs] - Added force in the X direction

1006.700 XReaction [lbs] - Reaction force in X direction reported by FEA program

TReactionX [lbs] = XArea*P+XForce ~~ Theoretical X reaction force 3.356*300+0 = 1,007

Y Axis: reaction forces on the XZ plane caused by loads in the Y direction

0.000 YArea [in2] - Pressurized area on XZ plane

0.0 YForce [lbs] - Added force in the Y direction

0.093 YReaction [lbs] - Reaction force in Y direction reported by FEA program

TReactionY [lbs] = YArea*P+YForce ~~ Theoretical Y reaction force 0*300+0 = 0

Z Axis: reaction forces on the XY plane caused by loads in the Z direction

0.000 ZArea [in2] - Pressurized area on XY plane

0.0 ZForce [lbs] - Added force in the Z direction

-0.210 ZReaction [lbs] - Reaction force in Z direction reported by FEA program

TReactionZ [lbs] = ZArea*P+ZForce ~~ Theoretical Z reaction force 0*300+0 = 0

Resultant of reaction forces in X, Y and Z:

TResultant [lbs] =

1,007

Resultant [lbs] =

1,007

Error [%] = 100*(TResultant-Resultant)/Resultant 100*(1007-1007)/1007 = 0.0CheckError = abs(Error)<2 ~~ Error should be less than 2% ABS(0)<2 = Acceptable

SQRT(1006.7^2+0.093^2+-0.21^2) =

View showing Global Reaction Forces from analysis 'X' = 1006.7 lb, 'Y' = 0.1 lb, 'Z' = -0.2 lb

Calculated Reaction Forces = Analysis Reaction Forces within 0%

Model is balanced, results are valid.

sqrt(TReactionX^2+TReactionY^2+TReactionZ^2) ~~ Theoretical resultant

SQRT(1007^2+0^2+0^2) =

sqrt(XReaction^2+YReaction^2+ZReaction^2) ~~ Actual resultant

Reaction Forces Plot

X Area = 3.36 in^2

Fig-11

Page 11: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Displacement Page 11 of 13

Displacement Plot (Rotated)

The manifold block expands radially outward and elongates axially away from the fixed restraint. The direction of

displacement is as expected. The magnitude of displacement is acceptable.

Displacement Plot

A view of the displacement plot with superimposed original geometry, results are magnified 5000 times. The

maximum displacement in the model is 0.00017"

Fig-12

Fig-13

Page 12: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Stress Page 12 of 13

von Mises Stress Plot (Rotated)

The maximum peak stress in the model is 3,034 psi and occurs on the inside corner of the middle port as

shown.

von Mises Stress Plot

A view of the von Mises stress plot. All areas in the model are below the primary general membrane limit of

20,000 psi for SA-479 316 and are acceptable.

Fig-14

Fig-15

Page 13: ASME Calculations - CRN Assistance - Vessel Design ... Calculations - CRN Assistance - Vessel Design ... Finite Element Analysis Report ... The model is in balance and can be used

Stress Page 13 of 13

von Mises Stress Plot (With Mesh)

A view of the von Mises stress plot with the mesh overlaid.

von Mises Stress Plot (Close-up With Mesh)

A close-up of (Fig-16). This shows the von Mises stress with the mesh overlaid at the maximum peak

stress location. The stresses in this region are acceptable and no further analysis is necessary.

Fig-16

Fig-17