轿车万向传动装置设计与有限元分析【全套含CAD图纸、说明书、三维模型】
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全套含CAD图纸、说明书、三维模型
轿车
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设计
有限元分析
全套
CAD
图纸
说明书
三维
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Solver OutputANSYS Multiphysics *-*| | W E L C O M E T O T H E A N S Y S (R) P R O G R A M | |*-* ANSYS 15.0 LEGAL NOTICES * * Copyright 2014 SAS IP, Inc. All rights reserved. * Unauthorized use, distribution or duplication is * prohibited. * * Ansys is a registered trademark of ANSYS, Inc. or its * subsidiaries in the United States or other countries. * See the ANSYS, Inc. online documentation or the ANSYS, Inc. * documentation CD or online help for the complete Legal * Notice. * * * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION * INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY * PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. * The software products and documentation are furnished by * ANSYS, Inc. or its subsidiaries under a software license * agreement that contains provisions concerning * non-disclosure, copying, length and nature of use, * compliance with exporting laws, warranties, disclaimers, * limitations of liability, and remedies, and other * provisions. The software products and documentation may be * used, disclosed, transferred, or copied only in accordance * with the terms and conditions of that software license * agreement. * * ANSYS, Inc. is a UL registered * ISO 9001:2008 company. * * * This product is subject to U.S. laws governing export and * re-export. * * For U.S. Government users, except as specifically granted * by the ANSYS, Inc. software license agreement, the use, * duplication, or disclosure by the United States Government * is subject to restrictions stated in the ANSYS, Inc. * software license agreement and FAR 12.212 (for non-DOD * licenses). * *Point Releases and Patches installed: ANSYS, Inc. Products 15.0.7 ANSYS Mechanical Products 15.0.7ANSYS Autodyn 15.0.7ANSYS LS-DYNA 15.0.7ANSYS CFX (includes ANSYS CFD-Post) 15.0.7 ANSYS Fluent (includes ANSYS CFD-Post) 15.0.7 ANSYS TurboGrid 15.0.7 ANSYS Polyflow (includes ANSYS CFD-Post) 15.0.7 ANSYS Aqwa 15.0.7 ANSYS ICEM CFD 15.0.7 ANSYS Icepak (includes ANSYS CFD-Post) 15.0.7 Catia, Version 6 15.0.7 ANSYS, Inc. License Manager 15.0.7 * ANSYS COMMAND LINE ARGUMENTS * BATCH MODE REQUESTED (-b) = NOLIST INPUT FILE COPY MODE (-c) = COPY 2 PARALLEL CPUS REQUESTED START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD20100520 VERSION=WINDOWS x64 RELEASE= 15.0.7 Maintenance Release UP20140420CURRENT JOBNAME=file 08:44:47 MAY 03, 2016 CP= 0.781PARAMETER _DS_PROGRESS = 999.0000000 /INPUT FILE= ds.dat LINE= 0DO NOT WRITE ELEMENT RESULTS INTO DATABASE*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 8.74638889 TITLE= unsaved_project-Static Structural (A5) SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_ProjectScratchScr1FA2SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_SOLVERFILES_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2unsaved_project_filesdp0SYSMECHSET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_USERFILES_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2unsaved_project_filesuser_files- Data in consistent NMM units.MPA UNITS SPECIFIED FOR INTERNAL LENGTH = MILLIMETERS (mm) MASS = TONNE (Mg) TIME = SECONDS (sec) TEMPERATURE = CELSIUS (C) TOFFSET = 273.0 FORCE = NEWTON (N) HEAT = MILLIJOULES (mJ)INPUT UNITS ARE ALSO SET TO MPA 1* ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 15.0.7 Maintenance Release *ANSYS Multiphysics 20100520 VERSION=WINDOWS x64 08:44:47 MAY 03, 2016 CP= 0.844unsaved_project-Static Structural (A5) * ANSYS ANALYSIS DEFINITION (PREP7) * Nodes for the whole assembly * Elements for Body 1 Part1 * Send User Defined Coordinate System(s) * Set Reference Temperature * Send Materials * Fixed Supports * Create Remote Point Internal Remote Point * Construct Moment Using RBE3/CERIG Style Contact * ROUTINE COMPLETED * CP = 0.875- Number of total nodes = 2243- Number of contact elements = 42- Number of spring elements = 0- Number of bearing elements = 0- Number of solid elements = 1153- Number of total elements = 1196*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 8.74638889 * SOLUTION * ANSYS SOLUTION ROUTINE *PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSISNEW SOLUTION CONTROL OPTION IS ACTIVATED,THE FOLLOWING COMMANDS ARE RESET TO NEW DEFAULTS: AUTOTS, DELTIM, NSUB, CNVTOL, LNSRCH, PRED, NROPT,TINTP, CUTCONTROL, OPNCONTROL, MONITOR, NEQIT, SSTIF, KBC.CONTACT TIME PREDICTIONS ARE BASED ON ELEMENT KEYOPT(7) SPECIFIED USE PRECONDITIONED CONJUGATE GRADIENT SOLVER CONVERGENCE TOLERANCE = 1.00000E-08 MAXIMUM ITERATION = NumNode*DofPerNode* 1.0000 CONTACT INFORMATION PRINTOUT LEVEL 1NLDIAG: Nonlinear diagnostics CONT option is set to ON. Writing frequency : each ITERATION.DO NOT SAVE ANY RESTART FILES AT ALL* SOLVE FOR LS 1 *SELECT FOR ITEM=NODE COMPONENT= IN RANGE 2243 TO 2243 STEP 1 1 NODES (OF 2243 DEFINED) SELECTED BY NSEL COMMAND.SPECIFIED NODAL LOAD MX FOR SELECTED NODES 1 TO 2243 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI33XSPECIFIED NODAL LOAD MY FOR SELECTED NODES 1 TO 2243 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI33YSPECIFIED NODAL LOAD MZ FOR SELECTED NODES 1 TO 2243 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI33ZALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 2243 STEP 1 2243 NODES (OF 2243 DEFINED) SELECTED BY NSEL COMMAND.PRINTOUT RESUMED BY /GOPUSE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOMFOR AUTOMATIC TIME STEPPING: USE 1 SUBSTEPS AS A MAXIMUM USE 1 SUBSTEPS AS A MINIMUMTIME= 1.0000 ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE FOR ALL APPLICABLE ENTITIESWRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIESWRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIESWRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIESWRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIESWRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIESNONLINEAR STABILIZATION CONTROL:KEY=OFF *GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000 *IF ANSINTER_ ( = 0.00000 ) NE 0 ( = 0.00000 ) THEN *ENDIF* ANSYS SOLVE COMMAND * WARNING * CP = 0.875 TIME= 08:44:47Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. * NOTE * CP = 0.891 TIME= 08:44:47The model data was checked and warning messages were found. Please review output or errors file ( C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_Proj jectScratchScr1FA2file.err ) for these warning messages. * SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS * - GIVE SUGGESTIONS AND RESET THE KEY OPTIONS -ELEMENT TYPE 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLEHYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.1* ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 15.0.7 Maintenance Release *ANSYS Multiphysics 20100520 VERSION=WINDOWS x64 08:44:47 MAY 03, 2016 CP= 0.891unsaved_project-Static Structural (A5) S O L U T I O N O P T I O N S PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE) OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15 EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08 GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC * WARNING * CP = 0.891 TIME= 08:44:47Material number 2 (used by element 1155 ) should normally have at least one MP or one TB type command associated with it. Output of energy by material may not be available. * NOTE * CP = 0.891 TIME= 08:44:47The step data was checked and warning messages were found. Please review output or errors file ( C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_Proj jectScratchScr1FA2file.err ) for these warning messages. * NOTE * CP = 0.891 TIME= 08:44:47The conditions for direct assembly have been met. No .emat or .erot files will be produced. * NOTE * CP = 0.922 TIME= 08:44:47Internal nodes from 2244 to 2244 are created. 1 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. L O A D S T E P O P T I O N S LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1 TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000 NUMBER OF SUBSTEPS. . . . . . . . . . . . . . . 1 STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT DATABASE OUTPUT CONTROLS ITEM FREQUENCY COMPONENT ALL NONE NSOL ALL RSOL ALL STRS ALL EPEL ALL EPPL ALL SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr * NOTE * CP = 0.953 TIME= 08:44:47It is highly recommended to use the auto contact setting option by issuing CNCHECK,AUTO command for this problem in order to achieve better convergence. * NOTE * CP = 0.953 TIME= 08:44:47Force-distributed-surface identified by real constant set 2 and contact element type 2 has been set up. The pilot node 2243 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZPlease verify constraints (including rotational degrees of freedom) on the pilot node by yourself. * NOTE * CP = 1.078 TIME= 08:44:47The PCG solver has automatically set the level of difficulty for this model to 2. The FEA model contains 0 external CE equations and 6 internal CE equations. * PRECISE MASS SUMMARY * TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN Translational mass | Coupled translational/rotational mass 0.84212E-02 0.0000 0.0000 | 0.0000 0.41698E-04 -0.15786E-04 0.0000 0.84212E-02 0.0000 | -0.41698E-04 0.0000 0.56768 0.0000 0.0000 0.84212E-02 | 0.15786E-04 -0.56768 0.0000 - | - | Rotational mass (inertia) | 4.1159 -0.14453E-02 -0.48177E-02 | -0.14453E-02 244.93 0.36744E-03 | -0.48177E-02 0.36744E-03 244.94 TOTAL MASS = 0.84212E-02 The mass principal axes coincide with the global Cartesian axes CENTER OF MASS (X,Y,Z)= 67.411 0.18746E-02 0.49516E-02 TOTAL INERTIA ABOUT CENTER OF MASS 4.1159 -0.38111E-03 -0.20068E-02 -0.38111E-03 206.67 0.36752E-03 -0.20068E-02 0.36752E-03 206.67 The inertia principal axes coincide with the global Cartesian axes * MASS SUMMARY BY ELEMENT TYPE * TYPE MASS 1 0.842123E-02Range of element maximum matrix coefficients in global coordinatesMaximum = 106070851 at element 878. Minimum = 866558.948 at element 839. * ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1153 SOLID187 0.250 0.000217 2 42 CONTA174 0.000 0.000000 3 1 TARGE170 0.000 0.000000Time at end of element matrix formulation CP = 1.234375. Iteration= 10 Ratio= 6.979584E-02 Limit= 1.000000E-08 Wall= 0.0Iteration= 30 Ratio= 9.453129E-04 Limit= 1.000000E-08 Wall= 0.0Iteration= 65 Ratio= 1.749713E-06 Limit= 1.000000E-08 Wall= 0.1PRECONDITIONED SOLVER CP TIME = 0.484PRECONDITIONED SOLVER ELAPSED TIME = 0.342 * ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1153 SOLID187 0.125 0.000108 2 42 CONTA174 0.000 0.000000 3 1 TARGE170 0.000 0.000000 * NODAL LOAD CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1153 SOLID187 0.000 0.000000 2 42 CONTA174 0.000 0.000000 3 1 TARGE170 0.000 0.000000* LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1* TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX* ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384 0.625 MB WRITTEN ON ELEMENT SAVED DATA FILE: file.esav 1.375 MB WRITTEN ON RESULTS FILE: file.rst* Write FE CONNECTORS *WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce * FINISHED SOLVE FOR LS 1 *PARAMETER _DS_PROGRESS DELETED.*GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 8.74666667 *GET _PCGITER FROM ACTI ITEM=SOLU CGIT VALUE= 91.0000000 FINISH SOLUTION PROCESSING* ROUTINE COMPLETED * CP = 1.8441* ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 15.0.7 Maintenance Release *ANSYS Multiphysics 20100520 VERSION=WINDOWS x64 08:44:48 MAY 03, 2016 CP= 1.844unsaved_project-Static Structural (A5) * ANSYS RESULTS INTERPRETATION (POST1) * NOTE * CP = 1.844 TIME= 08:44:48Reading results into the database (SET command) will update the current displacement and force boundary conditions in the database with the values from the results file for that load set. Note that any subsequent solutions will use these values unless action is taken to either SAVE the current values or not overwrite them (/EXIT,NOSAVE). Set Encoding of XML File to:ISO-8859-1Set Output of XML File to: PARM, , , , , , , , , , , , , , , , , , ,DATABASE WRITTEN ON FILE parm.xml EXIT THE ANSYS POST1 DATABASE PROCESSOR* ROUTINE COMPLETED * CP = 1.844PRINTOUT RESUMED BY /GOP*GET _WALLDONE FROM ACTI ITEM=TIME WALL VALUE= 8.74666667 PARAMETER _PREPTIME = 0.000000000 PARAMETER _SOLVTIME = 1.000000000 PARAMETER _POSTTIME = 0.000000000 PARAMETER _TOTALTIM = 1.000000000 EXIT ANSYS WITHOUT SAVING DATABASENUMBER OF WARNING MESSAGES ENCOUNTERED= 2NUMBER OF ERROR MESSAGES ENCOUNTERED= 0+- A N S Y S S T A T I S T I C S -+Release: 15.0.7 Build: UP20140420 Platform: WINDOWS x64 Date Run: 05/03/2016 Time: 08:44Windows Process ID: 5800Processor Model: Intel(R) Core(TM) i5-4210M CPU 2.60GHzCompiler: Intel(R) FORTRAN Compiler Version 12.1.0 (Build: 20120928) Microsoft(R) Visual C/C+ Compiler Version 16.0 (Build: 40219) Intel(R) Math Kernel Library Version 11.0.5 Product Build 20130612Total number of cores available : 4Number of physical cores available : 2Number of cores requested : 2 (Shared Memory Parallel)GPU Acceleration: Not RequestedJob Name: fileWorking Directory: C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_ProjectScratchScr1FA2Total CPU time for main thread : 1.3 secondsTotal CPU time summed for all threads : 1.8 secondsElapsed time spent pre-processing model (/PREP7) : 0.1 secondsElapsed time spent solution - preprocessing : 0.1 secondsElapsed time spent computing solution : 0.5 secondsElapsed time spent solution - postprocessing : 0.0 secondsElapsed time spent post-processing model (/POST1) : 0.0 secondsEquation solver computational rate : 3349.5 MflopsMaximum total memory used : 30.0 MBMaximum total memory allocated : 1088.0 MBMaximum total memory available : 4 GB+- E N D A N S Y S S T A T I S T I C S -+*-*| | ANSYS RUN COMPLETED | |-| | Release 15.0.7 UP20140420 WINDOWS x64 | |-| | Database Requested(-db) 512 MB Scratch Memory Requested 512 MB | Maximum Database Used 2 MB Maximum Scratch Memory Used 28 MB | |-| | CP Time (sec) = 1.844 Time = 08:44:48 | Elapsed Time (sec) = 4.000 Date = 05/03/2016 | |*-*Solver Output?ANSYS Multiphysics? ?*-*?|? |?|? W E L C O M E? T O? T H E? A N S Y S (R)? P R O G R A M? |?|? |?*-*?*?*? ANSYS 15.0 LEGAL NOTICES? *?*?*? *?* Copyright 2014 SAS IP, Inc.? All rights reserved.? *?* Unauthorized use, distribution or duplication is? *?* prohibited.? *?*? *?* Ansys is a registered trademark of ANSYS, Inc. or its? *?* subsidiaries in the United States or other countries.? *?* See the ANSYS, Inc. online documentation or the ANSYS, Inc. *?* documentation CD or online help for the complete Legal? *?* Notice.? *?*? *?*?*? *?* THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION? *?* INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY? *?* PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS.? *?* The software products and documentation are furnished by? *?* ANSYS, Inc. or its subsidiaries under a software license? *?* agreement that contains provisions concerning? *?* non-disclosure, copying, length and nature of use,? *?* compliance with exporting laws, warranties, disclaimers,? *?* limitations of liability, and remedies, and other? *?* provisions.? The software products and documentation may be *?* used, disclosed, transferred, or copied only in accordance? *?* with the terms and conditions of that software license? *?* agreement.? *?*? *?* ANSYS, Inc. is a UL registered? *?* ISO 9001:2008 company.? *?*? *?*?*? *?* This product is subject to U.S. laws governing export and? *?* re-export.? *?*? *?* For U.S. Government users, except as specifically granted? *?* by the ANSYS, Inc. software license agreement, the use,? *?* duplication, or disclosure by the United States Government? *?* is subject to restrictions stated in the ANSYS, Inc.? *?* software license agreement and FAR 12.212 (for non-DOD? *?* licenses).? *?*? *?*?Point Releases and Patches installed:? ? ?ANSYS, Inc. Products 15.0.7 ?ANSYS Mechanical Products 15.0.7?ANSYS Autodyn 15.0.7?ANSYS LS-DYNA 15.0.7?ANSYS CFX (includes ANSYS CFD-Post) 15.0.7? ?ANSYS Fluent (includes ANSYS CFD-Post) 15.0.7? ?ANSYS TurboGrid 15.0.7? ?ANSYS Polyflow (includes ANSYS CFD-Post) 15.0.7 ?ANSYS Aqwa 15.0.7? ?ANSYS ICEM CFD 15.0.7? ?ANSYS Icepak (includes ANSYS CFD-Post) 15.0.7? ?Catia, Version 6 15.0.7 ?ANSYS, Inc. License Manager 15.0.7? ? *? ANSYS COMMAND LINE ARGUMENTS? *? BATCH MODE REQUESTED (-b)? = NOLIST? INPUT FILE COPY MODE (-c)? = COPY? 2 PARALLEL CPUS REQUESTED? START-UP FILE MODE? = NOREAD? STOP FILE MODE? = NOREAD?20100520? VERSION=WINDOWS x64? RELEASE= 15.0.7? Maintenance Release UP20140420?CURRENT JOBNAME=file? 08:44:47? MAY 03, 2016 CP=? 0.781?PARAMETER _DS_PROGRESS =? 999.0000000? ?/INPUT FILE= ds.dat? LINE=? 0?DO NOT WRITE ELEMENT RESULTS INTO DATABASE?*GET? _WALLSTRT? FROM? ACTI? ITEM=TIME WALL? VALUE=? 8.74638889? ?TITLE= ?unsaved_project-Static Structural (A5)? ?SET PARAMETER DIMENSIONS ON? _WB_PROJECTSCRATCH_DIR? TYPE=STRI? DIMENSIONS=? 248? 1? 1?PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_ProjectScratchScr1FA2?SET PARAMETER DIMENSIONS ON? _WB_SOLVERFILES_DIR? TYPE=STRI? DIMENSIONS=? 248? 1? 1?PARAMETER _WB_SOLVERFILES_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2unsaved_project_filesdp0SYSMECH?SET PARAMETER DIMENSIONS ON? _WB_USERFILES_DIR? TYPE=STRI? DIMENSIONS=? 248? 1? 1?PARAMETER _WB_USERFILES_DIR(1) = C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2unsaved_project_filesuser_files?- Data in consistent NMM units.?MPA UNITS SPECIFIED FOR INTERNAL? ? LENGTH? = MILLIMETERS (mm)? MASS? = TONNE (Mg)? TIME? = SECONDS (sec)? TEMPERATURE = CELSIUS (C)? TOFFSET? = 273.0? FORCE? = NEWTON (N)? HEAT? = MILLIJOULES (mJ)?INPUT? UNITS ARE ALSO SET TO MPA 1?* ANSYS - ENGINEERING ANALYSIS SYSTEM? RELEASE 15.0.7? Maintenance Release *?ANSYS Multiphysics? ?20100520? VERSION=WINDOWS x64? 08:44:47? MAY 03, 2016 CP=? 0.844?unsaved_project-Static Structural (A5)? ? * ANSYS ANALYSIS DEFINITION (PREP7) *?* Nodes for the whole assembly *?* Elements for Body 1 Part1 *?* Send User Defined Coordinate System(s) *?* Set Reference Temperature *?* Send Materials *?* Fixed Supports *?* Create Remote Point Internal Remote Point *?* Construct Moment Using RBE3/CERIG Style Contact *?* ROUTINE COMPLETED *? CP =? 0.875?- Number of total nodes = 2243?- Number of contact elements = 42?- Number of spring elements = 0?- Number of bearing elements = 0?- Number of solid elements = 1153?- Number of total elements = 1196?*GET? _WALLBSOL? FROM? ACTI? ITEM=TIME WALL? VALUE=? 8.74638889? ?*?*? SOLUTION? *?*?*? ANSYS SOLUTION ROUTINE? *?PERFORM A STATIC ANALYSIS? THIS WILL BE A NEW ANALYSIS?NEW SOLUTION CONTROL OPTION IS ACTIVATED,?THE FOLLOWING COMMANDS ARE RESET TO NEW DEFAULTS: ?AUTOTS, DELTIM, NSUB, CNVTOL, LNSRCH, PRED, NROPT,?TINTP, CUTCONTROL, OPNCONTROL, MONITOR, NEQIT, SSTIF, KBC.?CONTACT TIME PREDICTIONS ARE BASED ON ELEMENT KEYOPT(7) SPECIFIED ?USE PRECONDITIONED CONJUGATE GRADIENT SOLVER? CONVERGENCE TOLERANCE = 1.00000E-08? MAXIMUM ITERATION? = NumNode*DofPerNode*? 1.0000? ?CONTACT INFORMATION PRINTOUT LEVEL? 1?NLDIAG: Nonlinear diagnostics CONT option is set to ON. ? Writing frequency : each ITERATION.?DO NOT SAVE ANY RESTART FILES AT ALL?*?* SOLVE FOR LS 1 *?SELECT? FOR ITEM=NODE COMPONENT=? ? IN RANGE? 2243 TO? 2243 STEP? 1? 1? NODES (OF? 2243? DEFINED) SELECTED BY? NSEL? COMMAND.?SPECIFIED NODAL LOAD MX? FOR SELECTED NODES? 1 TO? 2243 BY? 1? SET ACCORDING TO TABLE PARAMETER = _LOADVARI33X?SPECIFIED NODAL LOAD MY? FOR SELECTED NODES? 1 TO? 2243 BY? 1? SET ACCORDING TO TABLE PARAMETER = _LOADVARI33Y?SPECIFIED NODAL LOAD MZ? FOR SELECTED NODES? 1 TO? 2243 BY? 1? SET ACCORDING TO TABLE PARAMETER = _LOADVARI33Z?ALL SELECT? FOR ITEM=NODE COMPONENT=? ? IN RANGE? 1 TO? 2243 STEP? 1? 2243? NODES (OF? 2243? DEFINED) SELECTED BY NSEL? COMMAND.?PRINTOUT RESUMED BY /GOP?USE? 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL? DEGREES OF FREEDOM?FOR AUTOMATIC TIME STEPPING:? USE? 1 SUBSTEPS AS A MAXIMUM? USE? 1 SUBSTEPS AS A MINIMUM?TIME=? 1.0000? ?ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.?WRITE ALL? ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE? FOR ALL APPLICABLE ENTITIES?WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL ? FOR ALL APPLICABLE ENTITIES?WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL ? FOR ALL APPLICABLE ENTITIES?WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL ? FOR ALL APPLICABLE ENTITIES?WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL ? FOR ALL APPLICABLE ENTITIES?WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL ? FOR ALL APPLICABLE ENTITIES?NONLINEAR STABILIZATION CONTROL:?KEY=OFF ?*GET? ANSINTER_? FROM? ACTI? ITEM=INT? VALUE=? 0.00000000? ?*IF? ANSINTER_? ( =? 0.00000? )? NE? ? 0? ( =? 0.00000? )? THEN? ?*ENDIF?*? ANSYS SOLVE? COMMAND? *?* WARNING *? CP =? 0.875? TIME= 08:44:47?Element shape checking is currently inactive.? Issue SHPP,ON or? ?SHPP,WARN to reactivate, if desired.? ?* NOTE *? CP =? 0.891? TIME= 08:44:47?The model data was checked and warning messages were found.? ? Please review output or errors file (? ?C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_Proj ?jectScratchScr1FA2file.err ) for these warning messages.? ?* SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *? - GIVE SUGGESTIONS AND RESET THE KEY OPTIONS -?ELEMENT TYPE? 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE?HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.1?* ANSYS - ENGINEERING ANALYSIS SYSTEM? RELEASE 15.0.7? Maintenance Release *?ANSYS Multiphysics? ?20100520? VERSION=WINDOWS x64? 08:44:47? MAY 03, 2016 CP=? 0.891?unsaved_project-Static Structural (A5)? ? S O L U T I O N? O P T I O N S? PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D? ? DEGREES OF FREEDOM. . . . . . UX? UY? UZ? ROTX ROTY ROTZ? ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)? OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . .? 273.15? ? EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG? ? TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08? GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC? ?* WARNING *? CP =? 0.891? TIME= 08:44:47?Material number 2 (used by element 1155 ) should normally have at least ?one MP or one TB type command associated with it.? Output of energy by? ?material may not be available.? ?* NOTE *? CP =? 0.891? TIME= 08:44:47?The step data was checked and warning messages were found.? ? Please review output or errors file (? ?C:UserschanxAppDataLocalTempWB_DESKTOP-VAR389B_chanx_9192_2_Proj ?jectScratchScr1FA2file.err ) for these warning messages.? ?* NOTE *? CP =? 0.891? TIME= 08:44:47?The conditions for direct assembly have been met.? No .emat or .erot? ?files will be produced.? ?* NOTE *? CP =? 0.922? TIME= 08:44:47?Internal nodes from 2244 to 2244 are created.? ?1 internal nodes are used for handling degrees of freedom on pilot? ?nodes of rigid target surfaces.? ? L O A D? S T E P? O P T I O N S? LOAD STEP NUMBER. . . . . . . . . . . . . . . .? 1? TIME AT END OF THE LOAD STEP. . . . . . . . . .? 1.0000? ? NUMBER OF SUBSTEPS. . . . . . . . . . . . . . .? 1? STEP CHANGE BOUNDARY CONDITIONS . . . . . . . .? NO? PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT? DATABASE OUTPUT CONTROLS? ITEM? FREQUENCY? COMPONENT? ALL? NONE? ? NSOL? ALL? ? RSOL? ALL? ? STRS? ALL? ? EPEL? ALL? ? EPPL? ALL? ?SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr? ?* NOTE *? CP =? 0.953? TIME= 08:44:47?It is highly recommended to use the auto contact setting option by? ?issuing CNCHECK,AUTO command for this problem in order to achieve? ?better convergence.? ?* NOTE *? CP =? 0.953? TIME= 08:44:47?Force-distributed-surface identified by real constant set 2 and? ?contact element type 2 has been set up.? The pilot node 2243 is used? ?to apply the force.? Internal MPC will be built.? ?The used degrees of freedom set is? UX? UY? UZ? ROTX ROTY ROTZ?Please verify constraints (including rotational degrees of freedom)? on the pilot node by yourself.? ? ?* NOTE *? CP =? 1.078? TIME= 08:44:47?The PCG solver has automatically set the level of difficulty for this? ?model to 2.? ? ?The FEA model contains 0 external CE equations and 6 internal CE? ?equations.? ? *? PRECISE MASS SUMMARY? *? TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN? Translational mass? |? Coupled translational/rotational mass? 0.84212E-02? 0.0000? 0.0000? |? 0.0000? 0.41698E-04? -0.15786E-04? 0.0000? 0.84212E-02? 0.0000? |? -0.41698E-04? 0.0000? 0.56768? ? 0.0000? 0.0000? 0.84212E-02 |? 0.15786E-04? -0.56768? 0.0000? ? - | -? |? Rotational mass (inertia)? |? 4.1159? -0.14453E-02? -0.48177E-02? |? -0.14453E-02? 244.93? 0.36744E-03? |? -0.48177E-02? 0.36744E-03? 244.94? ? TOTAL MASS = 0.84212E-02? The mass principal axes coincide with the global Cartesian axes? CENTER OF MASS (X,Y,Z)=? 67.411? 0.18746E-02? 0.49516E-02? TOTAL INERTIA ABOUT CENTER OF MASS? 4.1159? -0.38111E-03? -0.20068E-02? -0.38111E-03? 206.67? 0.36752E-03? -0.20068E-02? 0.36752E-03? 206.67? ? The inertia principal axes coincide with the global Cartesian axes? * MASS SUMMARY BY ELEMENT TYPE *? TYPE? MASS? 1? 0.842123E-02?Range of element maximum matrix coefficients in global coordinates?Maximum = 106070851 at element 878.? ?Minimum = 866558.948 at element 839.? ? * ELEMENT MATRIX FORMULATION TIMES? TYPE? NUMBER? ENAME? TOTAL CP? AVE CP? 1? 1153? SOLID187? 0.250? 0.000217? 2? 42? CONTA174? 0.000? 0.000000? 3? 1? TARGE170? 0.000? 0.000000?Time at end of element matrix formulation CP = 1.234375.? ?Iteration=? 10 Ratio=? 6.979584E-02 Limit=? 1.000000E-08 Wall=? 0.0?Iteration=? 30 Ratio=? 9.453129E-04 Limit=? 1.000000E-08 Wall=? 0.0?Iteration=? 65 Ratio=? 1.749713E-06 Limit=? 1.000000E-08 Wall=? 0.1?PRECONDITIONED SOLVER CP TIME? =? 0.484?PRECONDITIONED SOLVER ELAPSED TIME =? 0.342? * ELEMENT RESULT CALCULATION TIMES? TYPE? NUMBER? ENAME? TOTAL CP? AVE CP? 1? 1153? SOLID187? 0.125? 0.000108? 2? 42? CONTA174? 0.000? 0.000000? 3? 1? TARGE170? 0.000? 0.000000? * NODAL LOAD CALCULATION TIMES? TYPE? NUMBER? ENAME? TOTAL CP? AVE CP? 1? 1153? SOLID187? 0.000? 0.000000? 2? 42? CONTA174? 0.000? 0.000000? 3? 1? TARGE170? 0.000? 0.000000?* LOAD STEP? 1? SUBSTEP? 1? COMPLETED.? CUM ITER =? 1?* TIME =? 1.00000? TIME INC =? 1.00000? NEW TRIANG MATRIX?* ANSYS BINARY FILE STATISTICS? BUFFER SIZE USED= 16384? 0.625 MB WRITTEN ON ELEMENT SAVED DATA FILE: file.esav? 1.375 MB WRITTEN ON RESULTS FILE: file.rst?* Write FE CONNECTORS *?WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce? ?*?* FINISHED SOLVE FOR LS 1 *?PARAMETER _DS_PROGRESS? DELETED.?*GET? _WALLASOL? FROM? ACTI? ITEM=TIME WALL? VALUE=? 8.74666667? ?*GET? _PCGI
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