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7/23/2019 Informe Fatiga - 1mm - 5000N
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ProjectFirst Saved Thursday, March 12, 2015
Last Saved Thursday, March 12, 2015
Product Version 15.0 Release
Save Project Before Solution No
Save Project After Solution No
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Contents
Units
Model (C4)
Geometry
Parts Coordinate Systems
Connections
Contacts
Contact Regions
Mesh
Refinement
Fatiga (C5)
Analysis Settings
Loads
Solution (C6)
Solution Information
Fatigue Tool
Results
Material Data
ELECTRODO 6013
ZONA AFECTACION TERMICA
MATERIAL BASE
Units
TABLE 1
Model (C4)
Unit System Metric (mm, kg, N, s, mV, mA) Degrees rad/s Celsius
Angle Degrees
Rotational Velocity rad/s
Temperature Celsius
Geometry
TABLE 2Model (C4) > Geometry
Object Name GeometryState Fully Defined
Definition
SourceD:\ANSYS\Proyecto ANSYS soldadura\proyect_files\dp0\SYS-2\DM\SYS-
2.agdb
Type DesignModeler
Length Unit Meters
Element Control Program Controlled
Display Style Body Color
Bounding Box
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TABLE 3Model (C4) > Geometry > Parts
Length X 7,9982 mm
Length Y 15, mm
Length Z 44, mm
Properties
Volume 4032,3 mm
Mass 3,1654e-002 kg
Scale Factor Value 1,
StatisticsBodies 5
Active Bodies 5
Nodes 51066
Elements 25076
Mesh Metric None
Basic Geometry Options
Parameters Yes
Parameter Key DS
Attributes No
Named Selections No
Material Properties No
Advanced Geometry OptionsUse Associativity Yes
Coordinate Systems No
Reader Mode Saves Updated File No
Use Instances Yes
Smart CAD Update No
Compare Parts On Update No
Attach File Via Temp File Yes
Temporary Directory C:\Users\usuario\AppData\Local\Temp
Analysis Type 3-D
Decompose Disjoint Geometry Yes
Enclosure and Symmetry
Processing Yes
Object Name soldadura2:1 zac:1 zac:2 lamina:1 lamina:2
State Meshed
Graphics Properties
Visible Yes
Transparency 1
Definition
Suppressed No
Stiffness Behavior Flexible
Coordinate System Default Coordinate SystemReference Temperature By Environment
Material
Assignment ELECTRODO 6013 ZONA AFECTACION TERMICA MATERIAL BASE
Nonlinear Effects Yes
Thermal Strain Effects Yes
Bounding Box
Length X 7,9982 mm 6, mm
Length Y 15, mm
Length Z 8, mm 4,0771 mm 16,083 mm
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Properties
Volume 682,73 mm 270, mm 1404,8 mm
Mass 5,3594e-003 kg 2,1195e-003 kg 1,1028e-002 kg
Centroid X -2,2403 mm
Centroid Y 1,6802 mm
Centroid Z 2,6254e-002 mm 4,8907 mm -4,8907 mm 14,192 mm -14,192 mm
Moment of Inertia Ip1 0,11956 kgmm 4,1573e-002 kgmm 0,43128 kgmm
Moment of Inertia Ip2 4,1398e-002 kgmm 8,1912e-003 kgmm 0,25697 kgmmMoment of Inertia Ip3 0,12281 kgmm 4,6099e-002 kgmm 0,23922 kgmm
Statistics
Nodes 17620 6573 6623 10125
Elements 8714 3208 3239 4953 4962
Mesh Metric None
Coordinate Systems
TABLE 4Model (C4) > Coordinate Systems > Coordinate System
Object Name Global Coordinate System
State Fully DefinedDefinition
Type Cartesian
Coordinate System ID 0,
Origin
Origin X 0, mm
Origin Y 0, mm
Origin Z 0, mm
Directional Vectors
X Axis Data [ 1, 0, 0, ]
Y Axis Data [ 0, 1, 0, ]
Z Axis Data [ 0, 0, 1, ]
Connections
TABLE 5Model (C4) > Connections
TABLE 6Model (C4) > Connections > Contacts
Object Name Connections
State Fully Defined
Auto Detection
Generate Automatic Connection On Refresh Yes
Transparency
Enabled Yes
Object Name Contacts
State Fully Defined
Definition
Connection Type Contact
Scope
Scoping Method Geometry Selection
Geometry All Bodies
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TABLE 7Model (C4) > Connections > Contacts > Contact Regions
Auto Detection
Tolerance Type Slider
Tolerance Slider 0,
Tolerance Value 0,11792 mm
Use Range No
Face/Face Yes
Face/Edge No
Edge/Edge NoPriority Include All
Group By Bodies
Search Across Bodies
Object Name Contact Region Contact Region 2 Contact Region 3 Contact Region 4
State Fully Defined
Scope
Scoping Method Geometry Selection
Contact 3 Faces
Target 3 FacesContact Bodies soldadura2:1 zac:1 zac:2
Target Bodies zac:1 zac:2 lamina:1 lamina:2
Definition
Type Bonded
Scope Mode Automatic
Behavior Program Controlled
Trim Contact Program Controlled
Trim Tolerance 0,11792 mm
Suppressed No
Advanced
Formulation Program Controlled
Detection Method Program ControlledPenetration Tolerance Program Controlled
Elastic Slip Tolerance Program Controlled
Normal Stiffness Program Controlled
Update Stiffness Program Controlled
Pinball Region Program Controlled
Geometric Modification
Contact Geometry Correction None
Mesh
TABLE 8Model (C4) > Mesh
Object Name Mesh
State Solved
Defaults
Physics Preference Mechanical
Relevance 0
Sizing
Use Advanced Size Function Off
Relevance Center Coarse
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TABLE 9Model (C4) > Mesh > Mesh Controls
Fatiga (C5)
TABLE 10Model (C4) > Analysis
Element Size Default
Initial Size Seed Active Assembly
Smoothing Medium
Transition Fast
Span Angle Center Coarse
Minimum Edge Length 0,381010 mm
Inflation
Use Automatic Inflation NoneInflation Option Smooth Transition
Transition Ratio 0,272
Maximum Layers 5
Growth Rate 1,2
Inflation Algorithm Pre
View Advanced Options No
Patch Conforming Options
Triangle Surface Mesher Program Controlled
Patch Independent Options
Topology Checking Yes
Advanced
Number of CPUs for Parallel Part Meshing Program ControlledShape Checking Standard Mechanical
Element Midside Nodes Program Controlled
Straight Sided Elements No
Number of Retries Default (4)
Extra Retries For Assembly Yes
Rigid Body Behavior Dimensionally Reduced
Mesh Morphing Disabled
Defeaturing
Pinch Tolerance Please Define
Generate Pinch on Refresh No
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default
Statistics
Nodes 51066
Elements 25076
Mesh Metric None
Object Name Refinement
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 30 Faces
Definition
Suppressed No
Refinement 2
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TABLE 11Model (C4) > Fatiga (C5) > Analysis Settings
TABLE 12
Object Name Fatiga (C5)
State Solved
Definition
Physics Type Structural
Analysis Type Static Structural
Solver Target Mechanical APDL
Options
Environment Temperature 22, CGenerate Input Only No
Object Name Analysis Settings
State Fully Defined
Step Controls
Number Of Steps 1,
Current Step Number 1,
Step End Time 1, s
Auto Time Stepping Program Controlled
Solver ControlsSolver Type Program Controlled
Weak Springs Program Controlled
Large Deflection Off
Inertia Relief Off
Restart Controls
Generate Restart Points Program Controlled
Retain Files After Full Solve No
Nonlinear Controls
Newton-Raphson Option Program Controlled
Force Convergence Program Controlled
Moment Convergence Program Controlled
Displacement Convergence Program ControlledRotation Convergence Program Controlled
Line Search Program Controlled
Stabilization Off
Output Controls
Stress Yes
Strain Yes
Nodal Forces No
Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory D:\ANSYS\Proyecto ANSYS soldadura\proyect_files\dp0\SYS-2\MECH\
Future Analysis None
Scratch Solver Files Directory
Save MAPDL db No
Delete Unneeded Files Yes
Nonlinear Solution No
Solver Units Active System
Solver Unit System nmm
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Model (C4) > Fatiga (C5) > Loads
FIGURE 1Model (C4) > Fatiga (C5) > Force
FIGURE 2Model (C4) > Fatiga (C5) > Displacement
Object Name Force Displacement
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Face
Definition
Type Force DisplacementDefine By Vector Components
Magnitude 5000, N (ramped)
Direction Defined
Suppressed No
Coordinate System Global Coordinate System
X Component Free
Y Component Free
Z Component 0, mm (ramped)
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Solution (C6)
TABLE 13Model (C4) > Fatiga (C5) > Solution
TABLE 14Model (C4) > Fatiga (C5) > Solution (C6) > Solution Information
Object Name Solution (C6)
State Solved
Adaptive Mesh RefinementMax Refinement Loops 1,
Refinement Depth 2,
Information
Status Done
Object Name Solution Information
State Solved
Solution Information
Solution Output Solver Output
Newton-Raphson Residuals 0Update Interval 2,5 s
Display Points All
FE Connection Visibility
Activate Visibility Yes
Display All FE Connectors
Draw Connections Attached To All Nodes
Line Color Connection Type
Visible on Results No
Line Thickness Single
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TABLE 15Model (C4) > Fatiga (C5) > Solution (C6) > Fatigue Tools
FIGURE 3Model (C4) > Fatiga (C5) > Solution (C6) > Fatigue Tool
FIGURE 4Model (C4) > Fatiga (C5) > Solution (C6) > Fatigue Tool
Display Type Lines
Object Name Fatigue Tool
State Solved
Materials
Fatigue Strength Factor (Kf) 1,Loading
Type Zero-Based
Scale Factor 1,
Definition
Display Time End Time
Options
Analysis Type Stress Life
Mean Stress Theory Gerber
Stress Component Equivalent (Von Mises)
Life Units
Units Name cycles
1 cycle is equal to 1, cycles
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TABLE 16Model (C4) > Fatiga (C5) > Solution (C6) > Fatigue Tool > Results
Material Data
Object Name Damage Life
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Design Life 1,e+009 cycles
Type Damage Life
Identifier
Suppressed No
Integration Point Results
Average Across Bodies No
Results
Maximum 4033,1
Maximum Occurs On zac:2
Minimum 2,4795e+005 cycles
Minimum Occurs On zac:2
ELECTRODO 6013
TABLE 17ELECTRODO 6013 > Constants
Density 7,85e-006 kg mm^-3
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TABLE 18ELECTRODO 6013 > Compressive Ultimate Strength
TABLE 19ELECTRODO 6013 > Compressive Yield Strength
TABLE 20ELECTRODO 6013 > Tensile Yield Strength
TABLE 21ELECTRODO 6013 > Tensile Ultimate Strength
TABLE 22ELECTRODO 6013 > Isotropic Secant Coefficient of Thermal Expansion
TABLE 23ELECTRODO 6013 > Alternating Stress Mean Stress
TABLE 24ELECTRODO 6013 > Strain-Life Parameters
TABLE 25ELECTRODO 6013 > Isotropic Elasticity
Coefficient of Thermal Expansion 1,2e-005 C^-1
Specific Heat 4,34e+005 mJ kg^-1 C^-1
Thermal Conductivity 6,05e-002 W mm^-1 C^-1
Resistivity 1,7e-004 ohm mm
Compressive Ultimate Strength MPa50,
Compressive Yield Strength MPa
250,
Tensile Yield Strength MPa
580,
Tensile Ultimate Strength MPa
710,
Reference Temperature C
22,
Alternating Stress MPa Cycles Mean Stress MPa
3999, 10, 0,
2827, 20, 0,
1896, 50, 0,
1413, 100, 0,
1069, 200, 0,
441, 2000, 0,
262, 10000 0,
214, 20000 0,
138, 1,e+005 0,
114, 2,e+005 0,
86,2 1,e+006 0,
StrengthCoefficient MPa
StrengthExponent
DuctilityCoefficient
DuctilityExponent
Cyclic StrengthCoefficient MPa
Cyclic StrainHardening Exponent
904, -7,5e-002 0,607 -0,548 1007, 0,155
Temperature C Young's Modulus MPa Poisson's Ratio Bulk Modulus MPa Shear Modulus MPa
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TABLE 26ELECTRODO 6013 > Isotropic Relative Permeability
21, 0,17939 0,3 0,14949 6,8996e-002
315, 0,13807 0,2691 9,9661e-002 5,4397e-002
538, 0,10647 0,3219 9,9635e-002 4,0272e-002
Relative Permeability
10000
ZONA AFECTACION TERMICA
TABLE 27ZONA AFECTACION TERMICA > Constants
TABLE 28ZONA AFECTACION TERMICA > Compressive Ultimate Strength
TABLE 29ZONA AFECTACION TERMICA > Compressive Yield Strength
TABLE 30ZONA AFECTACION TERMICA > Tensile Yield Strength
TABLE 31ZONA AFECTACION TERMICA > Tensile Ultimate Strength
TABLE 32ZONA AFECTACION TERMICA > Isotropic Secant Coefficient of Thermal Expansion
TABLE 33ZONA AFECTACION TERMICA > Alternating Stress Mean Stress
Density 7,85e-006 kg mm^-3
Coefficient of Thermal Expansion 1,23e-005 C^-1
Specific Heat 4,34e+005 mJ kg^-1 C^-1
Thermal Conductivity 6,05e-002 W mm^-1 C^-1
Resistivity 1,7e-004 ohm mm
Compressive Ultimate Strength MPa
500,
Compressive Yield Strength MPa
250,
Tensile Yield Strength MPa534,
Tensile Ultimate Strength MPa
667,
Reference Temperature C
22,
Alternating Stress MPa Cycles Mean Stress MPa
3999, 10, 0,
2827, 20, 0,
1896, 50, 0,
1413, 100, 0,
1069, 200, 0,
441, 2000, 0,
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TABLE 34
ZONA AFECTACION TERMICA > Strain-Life Parameters
TABLE 35ZONA AFECTACION TERMICA > Isotropic Elasticity
TABLE 36ZONA AFECTACION TERMICA > Isotropic Relative Permeability
262, 10000 0,
214, 20000 0,
138, 1,e+005 0,
114, 2,e+005 0,
86,2 1,e+006 0,
StrengthCoefficient MPa
StrengthExponent
DuctilityCoefficient
DuctilityExponent
Cyclic StrengthCoefficient MPa
Cyclic StrainHardening Exponent
724, -6,6e-002 0,218 -0,492 1490, 0,215
Temperature C Young's Modulus MPa Poisson's Ratio Bulk Modulus MPa Shear Modulus MPa
21, 1,7939e+005 0,3 1,4949e+005 68995
315, 1,3807e+005 0,2691 99660 54396
538, 1,0647e+005 0,3219 99634 40271
Relative Permeability
10000
MATERIAL BASE
TABLE 37MATERIAL BASE > Constants
TABLE 38MATERIAL BASE > Compressive Ultimate Strength
TABLE 39MATERIAL BASE > Compressive Yield Strength
TABLE 40MATERIAL BASE > Tensile Yield Strength
TABLE 41MATERIAL BASE > Tensile Ultimate Strength
Density 7,85e-006 kg mm^-3
Coefficient of Thermal Expansion 1,08e-005 C^-1
Specific Heat 4,34e+005 mJ kg^-1 C^-1
Thermal Conductivity 6,05e-002 W mm^-1 C^-1Resistivity 1,7e-004 ohm mm
Compressive Ultimate Strength MPa
300,
Compressive Yield Strength MPa
250,
Tensile Yield Strength MPa
224,
Tensile Ultimate Strength MPa
414,
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TABLE 42MATERIAL BASE > Isotropic Secant Coefficient of Thermal Expansion
TABLE 43MATERIAL BASE > Alternating Stress Mean Stress
TABLE 44MATERIAL BASE > Strain-Life Parameters
TABLE 45MATERIAL BASE > Isotropic Elasticity
TABLE 46MATERIAL BASE > Isotropic Relative Permeability
Reference Temperature C
22,
Alternating Stress MPa Cycles Mean Stress MPa
3999, 10, 0,
2827, 20, 0,
1896, 50, 0,
1413, 100, 0,
1069, 200, 0,
441, 2000, 0,
262, 10000 0,
214, 20000 0,
138, 1,e+005 0,
114, 2,e+005 0,
86,2 1,e+006 0,
StrengthCoefficient MPa
StrengthExponent
DuctilityCoefficient
DuctilityExponent
Cyclic StrengthCoefficient MPa
Cyclic StrainHardening Exponent
780, 0,258 0,271 -0,451 1097, 0,249
Temperature C Young's Modulus MPa Poisson's Ratio Bulk Modulus MPa Shear Modulus MPa
21, 1,7939e+005 0,3 1,4949e+005 68995
315, 1,3807e+005 0,2691 99660 54396
538, 1,0647e+005 0,3219 99634 40271
Relative Permeability
10000
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