Prótese : subistituíção por uma peça artificial. Transtibial: ao nível da tíbia, abaixo do joelho. Coto: parte que sobrou de um membro perdido. Cartucho: encaixe onde é alojado o coto.
Transfemural: o nível do fêmur, acima do joelho.
Perineal: dobra da junção da coxa com os órgãos genitais, virilha. Congênito: natural, que nasceu com o indivíduo. Ostemielite: inflamação da medula óssea.
Distal: parte inferior do coto. Proximal: parte superior do coto.
Tíbia: osso longo posterior ao longo da perna.
Ísquio: osso que sobressai na região do grande glúteo, osso ilíaco, localiza- se na parte lateral da bacia.
“Ficha conforme portaria nº388, de 28 de Julho de 1999”
Ficha conforme portaria nº388, de 28 de Julho de 1999
Ficha individual do paciente
PRÓTESES PARA MEMBROS INFERIORS
Nível: ( ) Desartic. Quadril ( )Transfemural ( )Desartic. Joelho ( )Transtibial ( ) Tornozelo ( ) Antepé
Tipo de Equipamento: ( ) Endoesquelético (modular) / ( ) Exoesquelético (con- vencional)
Encaixe: ( )Cesto Desarticulação Quadril/ ( ) Quadrilateral /( ) Contensão Isquiática ( )PTB ( ) PTS
( ) PTB c/coxal/ ( )PTB p/Chopart/Pirogoff/Syme/( )Palmilha p/Compl. Antepé: ( )Rígida
( )flexível
Material: ( ) Resina Acrílica p/ Laminação ( ) Couro ( ) Propileno ( ) Reforço Aço
Carbono ( ) Outro ___________________________________________________________
Suspensão: ( )Válvula vácuo ( )Cinto Pélvico ( )Cinto Silesiano ( )Correia Supra- condilar ( ) Coxal ( ) KBM
Obs.: Em amputados bilaterais, com níveis de amputações diferentes, marcar E ou D nos parênteses.
Articulações: ( ) Quadril: ( ) Exoesquelética ( ) Endoesquelética: ( ) com Trava ( ) sem Trava
( ) Joelho ( ) Exoesquelética ( ) Monoeixo; ( ) Livre ( ) c/ Trava ( ) c/ Freio
( ) c/ Impulsor
( ) Endoesquelética ( ) Monoeixo ( ) Livre ( ) c/Trava ( ) c/Freio ( ) c/Impulsor
( ) Quatro Barras ( ) Livre ( ) c/ Trava
( ) Tornozelo ( ) Exoesquelética ( ) Endoesquelética
Perna: ( ) Exoesquelética ( ) Endoesquelética: ( ) Aço ( )A- lumínio
( ) Revestimento cosmético
Pé: ( ) SACIH ( ) SACH Geriátrico ( ) p/amputação de Piro- goff
( ) Articulado ( ) Dinâmico
___________________________________________________________________ ________
ANEXO B
“Ficha para medições no processo convencional
APENDICE A
“Relatório com exemplo da análise FEM de uma prótese tibial
Design Analysis OrtoCAD
Summary Analysis Type Linear Static Stress Description OrtoCAD I Created By Edson DEM-UFRN Project created on 2007/06/29-09:50:35. Last updated on 2007/06/29-10:20:28. Checked By
Prof Angelo Roncalli Guerra UFRN
Group Information Group 1
Element Properties
Element Type Linear Brick
Compatibility Not Enforced
Integration Order 2nd Order
Stress Free Reference Temperature 0 °C Use Solid Mesher Connectivity Data No
Material Properties
Material Specified composito1500MPa
Material Model Standard
Material Source Minha_bibli_mat
Material Source File C:\ALGOR12\MATLIBS\Minha_bibli_mat.mlb Date Last Updated 2007/06/29-08:44:45
Material Description None
Mass Density 0 kg/m³
Modulus of Elasticity 1500000000 N/m²
Poisson's Ratio 0.3
Thermal Coefficient of Expansion 0 1/°C Shear Modulus of Elasticity 0 N/m²
Global Information
Load Case Multiplier 1 - Pressure 1.0 Load Case Multiplier 1 - Accel/Gravity 0 Load Case Multiplier 1 - Boundary 0 Load Case Multiplier 1 - Thermal 0
Acceleration Due To Body Force 9.81456 m/s² Gravity/Acceleration X Multiplier 0
Gravity/Acceleration Y Multiplier 0 Gravity/Acceleration Z Multiplier -1 Include Specified Centrifugal Load No Default Nodal Temperature 0 °C Source of Nodal Temperature None
Time step from Heat Transfer Analysis Last Disable Calculation and Output of Strains No Calculate Reaction Forces No
Invoke Banded Solver Yes
Avoid Bandwidth Minimization Yes Stop After Stiffness Calculations No Displacement Data in Output File Yes Stress Data in Output File Yes Equation Numbers Data in Output File Yes Element Input Data in Output File Yes Nodal Input Data in Output File Yes Centrifugal Load Data in Output File Yes
Algor (R) Linear Static Stress Version 12.12-WIN 07-DEC-2001
Copyright (c) 1984-2001 Algor, Inc. All rights reserved. DATE: JUNE 29,2007
TIME: 09:52 AM
INPUT MODEL: tempcvm ALG.DLL VERSION: 1000007 --- Linear Stress
1**** CONTROL INFORMATION
number of node points (NUMNP) = 360 number of element types (NELTYP) = 1 number of load cases (LL) = 1 number of frequencies (NF) = 0 analysis type code (NDYN) = 0 equations per block (KEQB) = 0 bandwidth minimization flag (MINBND) = 0 gravitational constant (GRAV) = 9.8146E+00 1**** NODAL DATA
NODE BOUNDARY CONDITION CODES NODAL POINT COORDINATES NO. DX DY DZ RX RY RZ X Y Z T
--- --- --- --- ---
1 1 1 1 1 1 1 6.018E-03 -2.287E-02 2.200E-01 0.000E+00 2 1 1 1 1 1 1 1.637E-02 -2.222E-02 2.200E-01 0.000E+00 3 1 1 1 1 1 1 -1.862E-03 -2.048E-02 2.200E-01 0.000E+00 4 1 1 1 1 1 1 5.000E-03 -1.900E-02 2.200E-01 0.000E+00 5 1 1 1 1 1 1 1.400E-02 -1.900E-02 2.200E-01 0.000E+00 6 1 1 1 1 1 1 2.628E-02 -1.828E-02 2.200E-01 0.000E+00 7 1 1 1 1 1 1 -8.184E-03 -1.763E-02 2.200E-01 0.000E+00 8 1 1 1 1 1 1 -1.500E-03 -1.650E-02 2.200E-01 0.000E+00 9 1 1 1 1 1 1 2.300E-02 -1.600E-02 2.200E-01 0.000E+00 10 1 1 1 1 1 1 -6.500E-03 -1.400E-02 2.200E-01 0.000E+00
...
358 0 0 0 1 1 1 4.000E-03 4.900E-02 4.000E-01 0.000E+00 359 0 0 0 1 1 1 -1.405E-02 5.186E-02 4.000E-01 0.000E+00 360 0 0 0 1 1 1 4.325E-03 5.299E-02 4.000E-01 0.000E+00
1**** EQUATION NUMBERS N DX DY DZ RX RY RZ 1 0 0 0 2 0 0 0 3 0 0 0 4 0 0 0 5 0 0 0 6 0 0 0 7 0 0 0 8 0 0 0 9 0 0 0 10 0 0 0 . . . 356 958 959 960 357 961 962 963 358 964 965 966 359 967 968 969 360 970 971 972
1**** 8-NODE BRICK ELEMENTS
number of elements = 162 number of materials = 1 Incompatible modes included for non-hybrid bricks 1**** MATERIAL DATA
INDEX E MU WEIGHT ALPHA SHEAR DENSITY MODULUS
--- --- --- --- --- ---
1 1.5000E+09 3.0000E-01 0.0000E+00 0.0000E+00 5.7692E+08 1**** ELEMENT LOAD FACTORS
CASE A CASE B CASE C CASE D --- --- --- ---
PRES 1.000E+00 0.000E+00 0.000E+00 0.000E+00 TEMP 0.000E+00 0.000E+00 0.000E+00 1.000E+00 X-DIR 0.000E+00 0.000E+00 0.000E+00 0.000E+00 Y-DIR 0.000E+00 0.000E+00 0.000E+00 0.000E+00 Z-DIR 0.000E+00 -1.000E+00 0.000E+00 0.000E+00
ELEM. NODE NODE NODE NODE NODE NODE NODE NODE I MAT STRESS
NO. N IND FREE
A B C D E F G H T TEMP --- --- --- --- --- --- --- --- --- - --- --- 1 1 2 5 4 38 37 39 42 2 1 0.0 2 3 1 4 8 40 38 42 44 2 1 0.0 3 2 6 9 5 37 41 45 39 2 1 0.0 4 7 3 8 10 43 40 44 46 2 1 0.0 5 11 7 10 12 47 43 46 48 2 1 0.0 6 6 13 15 9 41 50 51 45 2 1 0.0 7 11 12 16 14 47 48 52 49 2 1 0.0 8 14 16 18 17 49 52 54 53 2 1 0.0 9 13 20 19 15 50 56 55 51 2 1 0.0 10 17 18 21 22 53 54 57 58 2 1 0.0 . . . 156 310 309 313 314 346 345 349 350 2 1 0.0 157 312 316 315 311 348 352 351 347 2 1 0.0 158 314 313 317 318 350 349 353 354 2 1 0.0 159 316 320 319 315 352 356 355 351 2 1 0.0 160 318 317 321 323 354 353 357 359 2 1 0.0 161 320 324 322 319 356 360 358 355 2 1 0.0 162 321 322 324 323 357 358 360 359 2 1 0.0 **** Hard disk file size information for processor:
Available hard disk space on current drive = 23597.738 megabytes 1**** NODAL LOADS (STATIC) OR MASSES (DYNAMIC)
NODE LOAD X-AXIS Y-AXIS Z-AXIS X-AXIS Y-AXIS Z-AXIS
NUMBER CASE FORCE FORCE FORCE MOMENT MOMENT MOMENT 1 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00
2 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 3 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 4 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 5 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 6 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 7 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 8 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 9 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 10 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00
. .
356 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 357 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 358 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 359 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 360 1 0.000E+00 0.000E+00 -1.940E+00 0.000E+00 0.000E+00 0.000E+00 1**** ELEMENT LOAD MULTIPLIERS
load case case A case B case C case D case E --- --- --- --- --- ---
1 1.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 **** Invoking Sparse Solver ...
**** Symbolic Assembling Using the Row-Hits Matrix Profile ... **** Assembled in One Block.
**** Real Sparse Matrix Assembly ...
1**** STIFFNESS MATRIX PARAMETERS
minimum non-zero diagonal element = 4.7716E+06 maximum diagonal element = 9.8521E+07 maximum/minimum = 2.0647E+01 average diagonal element = 3.6125E+07 in the upper off-diagonal matrix:
number of entries in the profile = 40932 number of symbolic nonzero entries= 23814 number of real nonzero entries = 23814 **** Sparse Matrix Assembled in One Block **** Load case 1
**** Sparse Matrix Factorization ... **** Sparse Matrix Solving ... **** End Sparse Matrix Solution
1**** STATIC ANALYSIS
LOAD CASE = 1 Displacements/Rotations(degrees) of nodes
NODE X- Y- Z- X- Y- Z-
4 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 5 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 6 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 7 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 8 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 9 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 10 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
. . .
355 -2.1085E-05 -5.0537E-05 -3.4147E-05 0.0000E+00 0.0000E+00 0.0000E+00 356 -1.9235E-05 -5.1108E-05 -3.1433E-05 0.0000E+00 0.0000E+00 0.0000E+00 357 -1.5285E-05 -5.5958E-05 -3.6094E-05 0.0000E+00 0.0000E+00 0.0000E+00 358 -1.7471E-05 -5.0443E-05 -3.2102E-05 0.0000E+00 0.0000E+00 0.0000E+00 359 -1.6914E-05 -5.6333E-05 -3.3226E-05 0.0000E+00 0.0000E+00 0.0000E+00 360 -1.8262E-05 -5.0072E-05 -2.9726E-05 0.0000E+00 0.0000E+00 0.0000E+00
**** TEMPORARY FILE STORAGE (MEGABYTES) --- UNIT NO. 7 : 0.007 UNIT NO. 8 : 0.012 UNIT NO. 9 : 0.000 UNIT NO. 10 : 0.000 UNIT NO. 11 : 0.017 UNIT NO. 12 : 0.007 UNIT NO. 13 : 0.007 UNIT NO. 14 : 0.003 UNIT NO. 15 : 0.000 UNIT NO. 17 : 0.000 UNIT NO. 51 : 0.020 UNIT NO. 52 : 0.550 UNIT NO. 54 : 0.004 UNIT NO. 55 : 0.091
UNIT NO. 56 : 0.182 UNIT NO. 58 : 0.007
TOTAL : 0.909 Megabytes
Processor Log
Algor (R) Linear Static Stress Version 12.12-WIN 07-DEC-2001
Copyright (c) 1984-2001 Algor, Inc. All rights reserved. Linear Stress
360 1 1 0 0 0 **** Linear stress analysis
**** Memory Dynamically Allocated = 45685 KB Options executed are:
NOMIN DOTS STRAIN SPARSE PRTNEQ TRANS processing ...
**** OPENING TEMPORARY FILES NDYN = 0
DATE: JUNE 29,2007 TIME: 09:52 AM
INPUT MODEL: tempcvm ALG.DLL VERSION: 1000007 **** BEGIN NODAL DATA INPUT 360 NODES
**** END NODAL DATA INPUT **** BEGIN TYPE-5 DATA INPUT 162 ELEMENTS
**** END TYPE-5 DATA INPUT
**** Hard disk file size information for processor:
Available hard disk space on current drive = 23597.738 megabytes
**** BEGIN LOAD INPUT
**** Invoking Sparse Solver ...
**** Symbolic Assembling Using the Row-Hits Matrix Profile ... **** Assembled in One Block.
**** Real Sparse Matrix Assembly ... in the upper off-diagonal matrix:
number of entries in the profile = 40932 number of symbolic nonzero entries= 23814 number of real nonzero entries = 23814 **** Sparse Matrix Assembled in One Block **** Load case 1
**** Sparse Matrix Factorization ... **** Sparse Matrix Solving ... **** End Sparse Matrix Solution
**** BEGIN DISPLACEMENT OUTPUT **** END DISPLACEMENT OUTPUT tempcvm.t7 = 7.602 kilobytes tempcvm.t8 = 12.746 kilobytes tempcvm.t9 = 0.000 kilobytes tempcvm.t10 = 0.000 kilobytes tempcvm.t11 = 17.781 kilobytes tempcvm.t12 = 7.594 kilobytes tempcvm.t13 = 7.602 kilobytes tempcvm.t14 = 3.504 kilobytes tempcvm.t15 = 0.000 kilobytes tempcvm.t17 = 0.000 kilobytes tempcvm.t51 = 20.250 kilobytes tempcvm.t52 = 563.203 kilobytes tempcvm.t54 = 3.820 kilobytes tempcvm.t55 = 93.023 kilobytes tempcvm.t56 = 186.047 kilobytes tempcvm.t58 = 7.594 kilobytes
total temporary disk storage (megabytes) = 0.9090 tempcvm.l = 117.160 kilobytes
tempcvm.do = 16.922 kilobytes **** BEGIN DELETING TEMPORARY FILES Processing completed for model:
[tempcvm]
**** TEMPORARY FILES DELETED **** END OF SUCCESSFUL EXECUTION
Total actual hard disk space used = 1.040 megabytes Sub-total elapsed time = 0.011 minutes
Algor (R) FEA Stress Processor Version 12.08-WIN 07-DEC-2001
Copyright (c) 1989-2001 Algor, Inc. All rights reserved. **** Memory Dynamically Allocated = 45685 KB Percent capacity: .07564 DATE: JUNE 29,2007 TIME: 09:52 AM INPUT...tempcvm Percent capacity: .06642 Percent capacity: .06642
**** BEGIN TYPE-5 STRESS OUTPUT 162 ELEMENTS
Percent capacity: 0.3218 0 elements remaining Percent capacity: .06644
**** Writing stress and strain output files ... 0 load cases remaining
**** Hard disk file size information for postprocessor: tempcvm.son = 111.504 kilobytes
tempcvm.nso = 45.609 kilobytes tempcvm.sto = 45.609 kilobytes
Total MKNSO disk space used = 0.19797 megabytes **** End of successful execution
**** MKNSO elapsed time = 0.005 minutes **** The TOTAL elapsed time = 0.016 minutes
Stress Analysis
Algor (R) FEA Stress Processor Version 12.08-WIN 07-DEC-2001
Copyright (c) 1989-2001 Algor, Inc. All rights reserved.
1**** 8-NODE BRICK ELEMENTS
number of elements = 162 number of materials = 1 number of load types = 4
1**** 8-NODE BRICK ELEMENT STRESSES
ELEM. CASE N SIG-XX SIG-YY SIG-ZZ TAU-XY TAU-Y Z TAU-ZX NO. (MODE)O (SIG-MAX) (SIG-MIN) (SIG-INT)
D E
--- ---- - --- --- --- --- --- ---
1 1 1 -3.831E+05 -3.582E+05 -1.035E+06 2.436E+04 9.244E+04 3.174E+04 -3.303E+05 -1.049E+06 -3.975E+05
1 1 2 -4.890E+05 -4.572E+05 -1.137E+06 -1.567E+04 8.277E+04 1.406E+02 -4.421E+05 -1.147E+06 -4.942E+05
1 1 3 -4.267E+05 -4.961E+05 -8.862E+05 -3.637E+04 2.731E+04 -3.990E+04 -4.064E+05 -8.911E+05 -5.115E+05
1 1 4 -2.859E+05 -3.473E+05 -7.483E+05 1.379E+04 6.958E+04 2.843E+03 -2.822E+05 -7.600E+05 -3.393E+05
1 1 5 -4.882E+04 4.634E+03 -1.245E+06 -2.519E+04 2.635E+03 5.270E+03 1.463E+04 -1.245E+06 -5.879E+04
1 1 6 6.681E+04 1.235E+05 -9.715E+05 3.112E+04 1.493E+05 -1.826E+04 1.529E+05 -9.919E+05 5.785E+04
1 1 7 2.573E+05 1.264E+05 -6.725E+05 2.847E+04 1.273E+05 -6.746E+03 2.637E+05 -6.924E+05 1.399E+05
1 1 8 1.385E+05 4.758E+04 -9.214E+05 -3.561E+04 -1.031E+04 1.046E+04 1.509E+05 -9.216E+05 3.533E+04
2 1 1 -5.110E+05 -4.718E+05 -1.221E+06 7.087E+03 1.913E+03 1.143E+04 -4.706E+05 -1.221E+06 -5.120E+05
2 1 2 -4.530E+05 -4.037E+05 -1.098E+06 1.802E+04 4.904E+04 2.223E+04 -3.938E+05 -1.102E+06 -4.589E+05
. . .
161 1 5 8.969E+04 -2.109E+04 4.997E+04 7.071E+04 -2.458E+04 5.090E+04 1.395E+05 -7.248E+04 5.151E+04
6.884E+04 -6.435E+04 9.449E+03
161 1 7 -3.152E+05 -6.605E+04 -1.300E+05 7.066E+04 6.318E+04 -5.782E+03 -1.586E+04 -3.363E+05 -1.591E+05
161 1 8 -1.527E+05 -1.289E+05 -8.166E+04 1.486E+05 3.786E+04 1.445E+04 2.206E+04 -2.910E+05 -9.429E+04
162 1 1 3.016E+04 4.545E+03 -8.163E+04 1.875E+04 3.088E+04 1.402E+04 4.608E+04 -9.204E+04 -9.617E+02
162 1 2 2.236E+04 1.587E+04 -6.101E+04 -1.941E+04 4.304E+04 -6.863E+03 5.025E+04 -8.031E+04 7.284E+03
162 1 3 5.871E+04 1.120E+04 -1.388E+04 -2.491E+03 1.590E+04 -2.510E+04 6.748E+04 -2.721E+04 1.576E+04
162 1 4 7.491E+04 9.651E+03 -1.182E+04 3.301E+04 -1.366E+04 -1.526E+04 9.230E+04 -1.847E+04 -1.095E+03
162 1 5 -1.941E+05 -6.928E+04 -1.064E+05 -2.428E+04 3.976E+04 6.844E+03 -4.206E+04 -2.010E+05 -1.268E+05
162 1 6 -1.762E+05 3.751E+04 -6.759E+04 1.114E+04 3.512E+04 1.343E+04 4.911E+04 -1.781E+05 -7.732E+04
162 1 7 -6.503E+04 6.328E+04 1.066E+04 3.447E+04 9.252E+03 -1.804E+04 7.231E+04 -7.810E+04 1.471E+04
162 1 8 -7.105E+04 -2.589E+04 -2.171E+03 1.791E+03 -8.261E+03 -3.546E+04 1.453E+04 -8.608E+04 -2.756E+04
1**** End of file
Appendix
Deformação Tibial
Gravura mostrando deformação tibial (valores em metros)
Deformação antes após carregameto de 700N ampliada em 167 vezes
Distribuição de tensão no cartucho
“Relatório com exemplo da FEA de uma prótese Femural”
Design Analysis OrtoCAD I
Summary Analysis Type Linear Static Stress Description OrtoCAD Created By Edson DEM-UFRN Project created on 2007/07/25-14:35:12. Last updated on 2007/07/25-14:47:34. Checked By
Group 1
Element Properties
Element Type Linear Brick
Compatibility Not Enforced
Integration Order 2nd Order
Stress Free Reference Temperature 0 °C Use Solid Mesher Connectivity Data No Material Properties
Material Specified composito1500MPa
Material Model Standard
Material Source Minha_bibli_mat
Material Source File C:\ALGOR12\MATLIBS\Minha_bibli_mat.mlb Date Last Updated 2007/06/29-08:44:45
Material Description None
Mass Density 0 kg/m³
Modulus of Elasticity 1500000000 N/m²
Poisson's Ratio 0.3
Thermal Coefficient of Expansion 0 1/°C Shear Modulus of Elasticity 0 N/m² Global Information
Load Case Multiplier 1 - Pressure 1.0 Load Case Multiplier 1 - Accel/Gravity 0 Load Case Multiplier 1 - Boundary 0 Load Case Multiplier 1 - Thermal 0
Acceleration Due To Body Force 9.81456 m/s² Gravity/Acceleration X Multiplier 0
Gravity/Acceleration Y Multiplier 0 Gravity/Acceleration Z Multiplier -1 Include Specified Centrifugal Load No Default Nodal Temperature 0 °C
Disable Calculation and Output of Strains No
Calculate Reaction Forces No
Invoke Banded Solver Yes
Avoid Bandwidth Minimization Yes
Stop After Stiffness Calculations No
Displacement Data in Output File Yes
Stress Data in Output File Yes
Equation Numbers Data in Output File Yes
Element Input Data in Output File Yes
Nodal Input Data in Output File Yes
Centrifugal Load Data in Output File Yes
Processor Output Processor Summary Algor (R) Linear Static Stress Version 12.12-WIN 07-DEC-2001 Copyright (c) 1984-2001 Algor, Inc. All rights reserved. DATE: JULY 25,2007 TIME: 02:35 PM INPUT MODEL: tempcvm ALG.DLL VERSION: 1000007 ---
Linear Stress 1**** CONTROL INFORMATION number of node points (NUMNP) = 432
number of element types (NELTYP) = 1
number of load cases (LL) = 1
number of frequencies (NF) = 0
analysis type code (NDYN) = 0
equations per block (KEQB) = 0
bandwidth minimization flag (MINBND) = 0 gravitational constant (GRAV) = 9.8146E+00
1 1 1 1 1 1 1 3.750E-02 3.000E-03 5.000E-01 0.000E+00 2 1 1 1 1 1 1 3.000E-02 1.400E-02 5.000E-01 0.000E+00 3 1 1 1 1 1 1 2.150E-02 2.100E-02 5.000E-01 0.000E+00 4 1 1 1 1 1 1 1.300E-02 2.700E-02 5.000E-01 0.000E+00 5 1 1 1 1 1 1 3.000E-03 3.200E-02 5.000E-01 0.000E+00 6 1 1 1 1 1 1 -9.000E-03 3.400E-02 5.000E-01 0.000E+00 7 1 1 1 1 1 1 -2.150E-02 3.100E-02 5.000E-01 0.000E+00 8 1 1 1 1 1 1 -3.300E-02 2.250E-02 5.000E-01 0.000E+00 9 1 1 1 1 1 1 -4.250E-02 1.100E-02 5.000E-01 0.000E+00 10 1 1 1 1 1 1 -4.900E-02 -4.500E-03 5.000E-01 0.000E+00
. . .
427 0 0 0 1 1 1 -3.168E-02 -6.863E-02 7.200E-01 0.000E+00 428 0 0 0 1 1 1 -7.360E-03 -8.148E-02 7.200E-01 0.000E+00 429 0 0 0 1 1 1 2.406E-02 -8.786E-02 7.200E-01 0.000E+00 430 0 0 0 1 1 1 5.328E-02 -7.679E-02 7.200E-01 0.000E+00 431 0 0 0 1 1 1 7.429E-02 -5.127E-02 7.200E-01 0.000E+00 432 0 0 0 1 1 1 8.137E-02 -2.152E-02 7.200E-01 0.000E+00 1**** EQUATION NUMBERS N DX DY DZ RX RY RZ 1 0 0 0 2 0 0 0 3 0 0 0 4 0 0 0 5 0 0 0 6 0 0 0 7 0 0 0 8 0 0 0 9 0 0 0
. . . 425 1165 1166 1167 426 1168 1169 1170 427 1171 1172 1173 428 1174 1175 1176 429 1177 1178 1179 430 1180 1181 1182 431 1183 1184 1185 432 1186 1187 1188 1**** 8-NODE BRICK ELEMENTS
number of elements = 198 number of materials = 1 Incompatible modes included for non-hybrid bricks 1**** MATERIAL DATA
INDEX E MU WEIGHT ALPHA SHEAR DENSITY MODULUS
--- --- --- --- --- ---
1 1.5000E+09 3.0000E-01 0.0000E+00 0.0000E+00 5.7692E+08 1**** ELEMENT LOAD FACTORS
CASE A CASE B CASE C CASE D --- --- --- ---
PRES 1.000E+00 0.000E+00 0.000E+00 0.000E+00 TEMP 0.000E+00 0.000E+00 0.000E+00 1.000E+00 X-DIR 0.000E+00 0.000E+00 0.000E+00 0.000E+00 Y-DIR 0.000E+00 0.000E+00 0.000E+00 0.000E+00 Z-DIR 0.000E+00 -1.000E+00 0.000E+00 0.000E+00 **** ELEMENT CONNECTIVITY DATA
ELEM. NODE NODE NODE NODE NODE NODE NODE NODE I MAT S- TRESS
NO. N IND FREE
A B C D E F G H T TEMP --- --- --- --- --- --- --- --- --- - --- --- 1 217 218 2 1 235 236 20 19 2 1 0.0 2 218 219 3 2 236 237 21 20 2 1 0.0 3 219 220 4 3 237 238 22 21 2 1 0.0 4 220 221 5 4 238 239 23 22 2 1 0.0
. . . 190 406 407 191 190 424 425 209 208 2 1 0.0 191 407 408 192 191 425 426 210 209 2 1 0.0 192 408 409 193 192 426 427 211 210 2 1 0.0 193 409 410 194 193 427 428 212 211 2 1 0.0 194 410 411 195 194 428 429 213 212 2 1 0.0 195 411 412 196 195 429 430 214 213 2 1 0.0 196 412 413 197 196 430 431 215 214 2 1 0.0 197 413 414 198 197 431 432 216 215 2 1 0.0 198 414 397 181 198 432 415 199 216 2 1 0.0 **** Hard disk file size information for processor:
Available hard disk space on current drive = 22838.594 megabytes 1**** NODAL LOADS (STATIC) OR MASSES (DYNAMIC)
NODE LOAD X-AXIS Y-AXIS Z-AXIS X-AXIS Y-AXIS Z-AXIS NUMBER CASE FORCE FORCE FORCE MOMENT MOMENT MOMENT
1 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 2 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 3 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 4 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 5 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 6 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 7 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 8 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 9 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00
. . .
431 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 432 1 0.000E+00 0.000E+00 -1.620E+00 0.000E+00 0.000E+00 0.000E+00 1**** ELEMENT LOAD MULTIPLIERS
load case case A case B case C case D case E --- --- --- --- --- ---
1 1.000E+00 0.000E+00 0.000E+00 0.000E+00 0.000E+00 **** Invoking Sparse Solver ...
**** Symbolic Assembling Using the Row-Hits Matrix Profile ... **** Assembled in One Block.
**** Real Sparse Matrix Assembly ...
1**** STIFFNESS MATRIX PARAMETERS
minimum non-zero diagonal element = 9.8666E+06 maximum diagonal element = 1.2659E+08 maximum/minimum = 1.2830E+01 average diagonal element = 4.5867E+07 in the upper off-diagonal matrix:
number of entries in the profile = 50868 number of symbolic nonzero entries= 29538 number of real nonzero entries = 29538 **** Sparse Matrix Assembled in One Block **** Load case 1
**** Sparse Matrix Factorization ... **** Sparse Matrix Solving ... **** End Sparse Matrix Solution
1**** STATIC ANALYSIS
LOAD CASE = 1 Displacements/Rotations(degrees) of nodes
NODE X- Y- Z- X- Y- Z-
number translation translation translation rotation rotation rotation 1 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
2 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
6 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
7 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
8 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
9 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
10 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
. . .
425 -2.9113E-06 8.0593E-06 -4.0388E-05 0.0000E+00 0.0000E+00 0.0000E+00 426 -1.6996E-05 -3.6801E-06 -4.0253E-05 0.0000E+00 0.0000E+00
0.0000E+00
427 -1.9105E-05 -8.1080E-06 -3.8750E-05 0.0000E+00 0.0000E+00 0.0000E+00
428 -1.2140E-05 2.3086E-06 -3.4662E-05 0.0000E+00 0.0000E+00 0.0000E+00
429 -7.0384E-06 2.5938E-05 -2.9397E-05 0.0000E+00 0.0000E+00 0.0000E+00
430 -1.4035E-05 4.2572E-05 -2.8248E-05 0.0000E+00 0.0000E+00 0.0000E+00
431 -1.7728E-05 4.4217E-05 -3.5006E-05 0.0000E+00 0.0000E+00 0.0000E+00
432 -6.3439E-06 4.0360E-05 -4.8068E-05 0.0000E+00 0.0000E+00 0.0000E+00
1**** TEMPORARY FILE STORAGE (MEGABYTES) --- UNIT NO. 7 : 0.009 UNIT NO. 8 : 0.015 UNIT NO. 9 : 0.000 UNIT NO. 10 : 0.000 UNIT NO. 11 : 0.021 UNIT NO. 12 : 0.009 UNIT NO. 13 : 0.009 UNIT NO. 14 : 0.004 UNIT NO. 15 : 0.000 UNIT NO. 17 : 0.000 UNIT NO. 51 : 0.024
UNIT NO. 56 : 0.225 UNIT NO. 58 : 0.009
TOTAL : 1.116 Megabytes
Stress Analysis
Algor (R) FEA Stress Processor Version 12.08-WIN 07-DEC-2001
Copyright (c) 1989-2001 Algor, Inc. All rights reserved.
DATE: JULY 25,2007 TIME: 02:35 PM INPUT...tempcvm
--- 1**** 8-NODE BRICK ELEMENTS
number of elements = 198 number of materials = 1 number of load types = 4
1**** 8-NODE BRICK ELEMENT STRESSES
ELEM. CASE N SIG-XX SIG-YY SIG-ZZ TAU-XY TAU-Y Z TAU-ZX NO. (MODE)O (SIG-MAX) (SIG-MIN) (SIG-INT)
D E
--- ---- - --- --- --- --- --- ---
1 1 1 -2.777E+05 -2.852E+05 -6.171E+05 -5.452E+03 -1.589E+04 1.050E+05 -2.455E+05 -6.475E+05 -2.870E+05
1 1 2 -2.749E+05 -2.570E+05 -6.220E+05 -1.386E+03 -4.229E+04 5.526E+04 -2.489E+05 -6.351E+05 -2.698E+05
1 1 3 -3.017E+05 -2.900E+05 -7.276E+05 5.762E+03 -4.923E+04 6.991E+04 -2.839E+05 -7.442E+05 -2.911E+05
1 1 4 -2.719E+05 -2.895E+05 -6.512E+05 2.165E+03 -2.059E+04 1.187E+05 -2.375E+05 -6.863E+05 -2.887E+05
1 1 5 1.877E+04 -3.892E+04 -6.231E+05 7.908E+04 -2.431E+04 6.253E+04 7.614E+04 -6.308E+05 -8.853E+04
198 1 1 -4.320E+04 1.536E+04 -1.115E+05 -1.055E+04 -1.040E+04 -9.748E+03 1.778E+04 -1.139E+05 -4.318E+04
198 1 2 4.328E+04 4.502E+04 -8.552E+04 -1.693E+04 -1.030E+04 -1.631E+04 6.120E+04 -8.870E+04 3.028E+04
198 1 3 6.643E+04 1.491E+05 4.640E+04 -4.390E+04 1.554E+04 -2.593E+03 1.700E+05 4.196E+04 5.002E+04
198 1 4 -3.891E+04 1.178E+05 4.545E+02 -4.167E+04 1.690E+04 1.290E+04 1.296E+05 -5.441E+04 4.189E+03
198 1 5 -2.903E+04 -5.808E+04 -8.034E+04 3.070E+04 -1.047E+04 - 1.483E+04
-5.220E+03 -8.483E+04 -7.741E+04
198 1 6 -2.362E+04 -8.837E+04 -1.125E+05 9.285E+03 -8.044E+03 - 1.092E+04
-2.075E+04 -1.156E+05 -8.811E+04
198 1 7 -4.832E+03 7.041E+03 1.551E+04 -1.631E+04 1.576E+04 2.986E+03 2.962E+04 -2.030E+04 8.394E+03
198 1 8 -2.554E+04 3.749E+04 2.915E+04 1.905E+03 1.449E+04 7.121E+03 4.885E+04 -2.645E+04 1.870E+04
1**** End of file
Appendix
Deformação antes após carregameto de 700N ampliada em 22000 vezes