第22章 热-应力耦合分析实例.pdf

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22 热-应力耦合分析实例 温度的分布不均会导致部件内部产生热应力,在结构分析中常会遇到需要考虑温度场 对应力分布影响的情况。特别在进行各类燃机的部件,如航空发动机的涡轮盘、叶片等的 强度计算分析时通常要考虑热问题。各类输送管道由于内外温度不同也会产生热应力。另 外材料的性能和其温度是相关的,不同的温度下其性能通常不同,这也会造成部件应力分 布的变化。为此,本章通过实例来讲解如何用 ANSYS6.1 来进行这类问题的分析。 22.1 问题描述 一无限长的截面形状和尺寸如图 22.1 所示的厚壁双层圆管,其内、外层温度分别为 Ti To,材料数据和边界条件如表 22.1 所示,利用 ANSYS 程序来求解圆管沿径向的温度分 布情况,并求解圆管内沿径向和周向的应力情况。 22.1 双层管道的截面图 22.1 材料性能参数表 材料编号 热导率(W/mm. o C) 弹性模量(MPa) 泊松比 热膨胀系数(o C -1 ) 1(),内层 0.0234 2.05E5 0.3 10.3 2 () ,外层 0.152 0.63E5 0.33 20.7 从上面描述的问题可以看出,本实例属于轴对称问题,可以采用轴对称方法来进行分 析。同时本问题为典型的热-应力耦合问题,可以采用间接法顺序耦合分析的一般步骤进 行分析。因为管道为无限长,故建立模型时轴向尺寸可以是任意大于零的值,且将其一边

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  • 22

    ANSYS6.1

    22.1

    22.1 Ti To 22.1 ANSYS

    22.1 22.1 (W/mm. oC) (MPa) (oC-1) 1(), 0.0234 2.05E5 0.3 10.3

    2 () , 0.152 0.63E5 0.33 20.7

  • 22.2

    ANSYS6.1

    22.2.1

    Thermal Stress in Concentric Cylinders-Indirect Method

    1 Utility Menu | File | Change Jobname Change Jobname () 22.2 Enter new jobname ()CH20

    22.2

    2 Utility Menu | File | Change Title Change Title () 20.3 Enter new title ()Thermal Stress in Concentric Cylinders-Indirect Method

    22.3

    3Main Menu | Preference Preference of GUI Filtering () 22.4 Thermal() Thermal

  • ANSYS6.1

    22.4

    22.2.2

    8 PLANE77

    1Main Menu | Preprocessor | Element Type | Add/Edit/DeleteElement Types () Library of Element Types (), 22.5

    22.5 PLANE77

    2 Library of Element Type ()Thermal SolidQuad 8node 77 8 PLANE77 Library of Element Types ()Element Types () 22.6

  • 22.6

    3 PLANE77 22.6

    PLANE77 element type options ( PLANE77) 22.7 K3Axisymmetric

    22.7 4( 22.6)

    22.2.3

    1Main Menu | Preprocessor | Material Props | Material ModelsDefine Material Model Behavior () 22.8

  • 22.8

    2 22.8 Thermal | Conductivity | Isotropic 1 KXX 22.9

    22.9 1

    3 22.9 KXX 0.0234 1 0.0234 1 22.10

    22.10 4 22.10Material | New Model Define Material ID

  • () 22.11 22.10

    22.11 5 23 2 0.152W/mm.oC 22.10Material | Exit

    22.2.4

    1 Main Menu | Preprocessor | Modeling | Create | Rectangle | By Dimensions Create Rectangle by Dimensions () 22.12

    22.12 2 XYX1=5.5X2=10.8Y1=0Y2=1.5

    3 Create Rectangle by Dimensions () 2X1=10.8X2=15.6Y1=0Y2=1.5 22.13

  • 22.13 4Main Menu | Preprocessor | Modeling | Operate | Booleans | Glue | Areas Glue Area () ANSYS

    5Main Menu | Preprocessor | Numbering Ctrls | Compress Numbers Compress Numbers () 22.14

    All

    22.14 6 Utility Menu | PlotCtrls | Numbering Plot

    Numbering Controls () LINE () AREA ()On Utility Menu | Plot | ReplotANSYS 22.15

  • 22.15

    22.2.5

    1 Main Menu | Preprocessor | Meshing | Mesh Attributes | Picked Areas Area Attributes () ANSYS

    A1 Area Attributes () 22.16

    22.16

  • 2Material number ()1 Element type number1 PLANE77 A1

    3 Area Attributes () ANSYSA2 Area Attributes () 22.16Material number ()2 Element type number1 PLANE77

    A2 4Main Menu | Preprocessor | Meshing | Size Cntrls |

    ManualSize | Global | Size Global Element Sizes ()22.17 Element edge length ()0.8

    22.17 5Main Menu | Preprocessor | Meshing | Mesh | Areas | FreeMesh Areas ()

    22.18

    22.18

  • 22.3

    22.3.1

    20 18

    1 Utility Menu | Select | Entities 22.19 NodesBy LocationsX coordinates5.5 X 5.5

    2Main Menu | Solution | Define Loads | Apply | Thermal | Temperature | On Nodes Apply TEMP on Nodes (

    ) Apply TEMP on Nodes () 22.20

    22.20 3 Load TEMP value () 180 Utility Menu | Select

    4 13 X 15.6 20 0 22.19

    Everything

    20

  • 22.3.2

    1Main Menu | Solution | Current LS/STATUS Command ()( 22.21) Solve Current Load Step ()( 22.22)

    2 22.21( 22.22)

    22.21

    22.22 3ANSYS ANSYS Solution is Done ()

    22.3.3

    ANSYS6.1 (POST1) ANSYS6.1

  • 1Main Menu | General Postproc | Plot Results | Nodal Solu 22.23

    22.23 2 Item to be contoured ()DOF

    solutionTemperature TEMP ANSYS6.1 22.24

  • 22.24 3Main Menu | General Postproc | Path Operations |

    Define Path | By Location By Location () 22.25

    22.25 4 Define Path Name ()radial By Location in Global Cartesian () 22.26

  • 20.26 5 Path point number () 1 X Location in Global CS

    ( X) 5.5 6 5 20.26(Path point

    number) 2 X Location in Global CS ( X) 15.6

    7Main Menu | General Postproc | Path Operations | Map onto PathMap Result Items onto Path () 22.27

    22.27

    822.27temp Item to be mapped ()DOF solutionTemperature TEMP

    9 Main Menu |

    General Postproc | Path Operations | Archive Path | Store | Path in array Archive Path in to Array Parameters () 22.28

  • 22.28 10 POIN-only points

    Archive Path Points into Array () 22.29

    22.29

    11path

    12Main Menu | General Postproc | Path Operations Plot Path Item | On Graph Plot of Path Items on Graph () 22.30

    22.30 13TEMP ANSYS6.1

    22.31

  • 22.31 14Main Menu | General Postproc

    | Path Operations Plot Path Item | On Geometry Plot of Path Items on Geometry () 22.32

    22.32 15TEMP

    Scale factor offset ()30 ANSYS6.1 22.33

  • 22.33

    22.4

    22.4.1

    ANSYS

    22.4.1.1 PLANE77

  • PLANE82 1 Main Menu |

    Preference Preference of GUI Filtering ()Sturctrual() Structural Thermal ANSYS6.1

    2Main Menu | Preprocessor | Element Type | Switch Elem Type Swith Elem Type () 22.34

    22.34 3 Change element type ()Thermal to Struc ANSYS6.1 22.35

    22.35 4 5Main Menu | Preprocessor | Element Type |

    Add/Edit/Delete(Element Types)

    PLANE82 element type options ( PLANE82) 22.36

    22.36 6 K3 Axisymmetric

  • Element Types ()

    22.4.1.2

    1Main Menu | Preprocessor | Material Props | Material ModelsDefine Material Model Behavior () 22.37

    22.37 2Material Model Number1 ( 1) Structural | Linear | Elastic | Isotropic 1 EX PRXY EX

    2.05E5PRXY0.3 3 22.37 Structural | Thermal

    Expansion Coef | Isotropic Thermal Expansion Coefficient for Material 1 ( 1) 22.38

    22.38 1

  • 4 Reference temperature () 20 20 ALPX 10.3E-6

    1 5 22.37Material Model Number 2 (2) 24 2

    EX 0.63E5 PRXY 0.33 ALPX 20.7E-6( 20) 22.37

    22.4.2

    1 Utility Menu | Select | Entities( 22.19 )NodesBy LocationsX coordinates5.5

    X 5.5 2Main Menu | Preprocessor | Coupling / Ceqn | Couple DOFs

    Define Coupled DOFs () 22.39Set reference number () 1UX

    22.39 3 12 Y 1.5 2 Y 1.5 Y()

    4 1 Y 0 Main Menu | Solution | Define Loads | Apply | Structural | Displacement | On Nodes 22.40

  • 22.40 5 DOFs to be Constrained ()UY

    ANSYS6.1 22.41

    22.41 6 Utility Menu | Select Everything

    7Main Menu | Solution | Define Loads | Apply | Structural | Temperature | From Therm Analy Apply TEMP from Thermal Analysis () 22.42

  • 22.42

    8 Fname Name of results file () CH20.rth

    22.42 CH20.rthANSYS6.1

    9 Utility Menu | PlotCtrls | Symbols22.43

    22.43 10 Body Load Symbols ()Structural temps

  • ANSYS6.1 22.44(/PBF,TEMP,1)

    22.44

    22.4.3

    1Main Menu | Solution | Current LS/STATUS Command () Solve Current Load Step ()

    2

    3ANSYS Solution is Done ()

    22.4.4

    ANSYS

  • (POST1)

    1 Main Menu | General Postproc | Path Operations | Archive Path | Retrieve | Path from array Retrieve Path from Arrays () 22.45

    22.45 2 Define Path with Name ()pathPOIN-only points ANSYS6.1 22.46

    22.46 3 ( PATH )

    4Main Menu | General Postproc | Path Operations | Define Path | Path Options Path Options () 22.47

  • 22.47 5Main Menu | General Postproc | Path Operations

    | Map onto PathMap Result Items onto Path ()

    22.48 6sx Item to be mapped ()StressXdirection SX X()

    7 6 Z()sz

    8Main Menu | General Postproc | Path Operations Plot Path Item | On Graph Plot of Path Items on Graph () 22.49

  • 22.49 9SXSZ ANSYS

    22.50

    22.50 10Main Menu | General Postproc | Path

    Operations Plot Path Item | On Geometry Plot of Path Items on Geometry () 22.51

    22.51 11SX

  • With nodes ANSYS 22.52

    22.52 12 22.51 SZ ANSYS

    22.53

    22.53

  • ANSYS Toobar

    ANSYS ANSYS6.1

    22.5

    ANSYS GUI(!)

    /TITLE,Thermal Stress in Concentric Cylinders-Indirect Method /COM, Thermal /PREP7 ET,1,PLANE77,,,1 !* MP,KXX,1,0.0234 MP,KXX,2,0.152 !* RECTNG,5.5,10.8,0,1.5 RECTNG,10.8,15.6,0,1.5 !* AGLUE,ALL ! NUMCMP,ALL ASEL,S,AREA,,1 1 AATT,1,1,1 1 1 ASEL,S,AREA,,2 AATT,2,1,1 ASEL,ALL !* ESIZE,1.5 ! AMESH,ALL NSEL,S,LOC,X,5.5 D,ALL,TEMP,180 NSEL,S,LOC,X,15.6

  • D,ALL,TEMP,20 NSEL,ALL FINISH !* /SOLU SOLVE FINISH /POST1 PLNSOL,TEMP, ,0, PATH,RADIAL,2 PPATH,1,,5.5 PPATH,2,,15.6 PDEF,TEMP,TEMP PAGET,PATH,POINTS,RADIAL PLPATH,TEMP PLPAGM,TEMP,30 FINISH !* /COM, Structural /PREP7 ETCHG,TTS KEYOPT,1,3,1 !* MP,EX,1,2.05E5 1 MP,ALPX,1,10.3E-6 MP,NUXY,1,.3 !* MP,EX,2,0.63E5 2 MP,ALPX,2,20.7E-6 MP,NUXY,2,.33 !* NSEL,S,LOC,X,5.5 CP,1,UX,ALL !* NSEL,S,LOC,Y,1.5 CP,2,UY,ALL !* NSEL,S,LOC,Y,0 D,ALL,UY,0

  • NSEL,ALL !* FINISH /SOLU TREF,20 LDREAD,TEMP,,,,,ch20.RTH !* /PBF,TEMP, ,1 SOLVE FINISH !* /POST1 PAPUT,PATH,POINTS PMAP,,MAT PDEF,SX,S,X X PDEF,SZ,S,Z !* PLPATH,SX,SZ PLPAGM,SX,,NODE PLPAGM,SZ,,NODE FINISH