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Stress Analysis Report

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Stress Analysis Report

Analyzed File: Creation Date: Simulation Author: Summary:

ENSAMBLE 1.iam 28/03/2011, 8:37 A.ROMERO

Autodesk Inventor Version: 2011 SP1 (Build 150282100, 282)

 Project Info (iProperties)
 Summary
Author A.ROMERO

 Project
Part Number Designer Cost Date Created ENSAMBLE 1 A.ROMERO 0,00 € 25/03/2011

 StatusDesign Status WorkInProgress

 Physical
Mass Area Volume 247,858 kg 20193400 mm^2 31547300 mm^3 x=-631,732 mm Center of Gravity y=-1062,65 mm z=1272,96 mm Note: Physical values could be different from Physical values used by FEA reported below.

 Simulation:1
General objective and settings: Design Objective Simulation Type Last Modification Date Detect and Eliminate Rigid Body Modes SeparateStresses Across Contact Surfaces Motion Loads Analysis Single Point Static Analysis 28/03/2011, 8:30 No No No

file://D:\diseño 2011 a.romero\MALACATE BODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

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Advanced settings: Avg. Element Size (fraction of model diameter) Min. Element Size (fraction of avg. size) Grading Factor Max. TurnAngle Create Curved Mesh Elements Use part based measure for Assembly mesh 0,1 0,2 1,5 60 deg Yes Yes

 Material(s)
Name Steel, Mild Mass Density 7,86 g/cm^3 General Yield Strength 207 MPa Ultimate Tensile Strength 345 MPa Young's Modulus 220 GPa Stress Poisson's Ratio 0,275 ul Shear Modulus 86,2745 GPa Expansion Coefficient 0,000012 ul/c Stress Thermal Thermal Conductivity 56 W/( m K )Specific Heat 460 J/( kg c ) AISC HSS - 3x2x1_8 - X AISC HSS - 3x2x1_8 - XX AISC HSS - 3x2x1_8 - XX AISC HSS - 3x2x1_8 - X AISC HSS - 3x2x1_8 - XXX AISC HSS - 3x2x1_8 - XXX AISC HSS - 3x2x1_8 - XXX AISC HSS - 3x2x1_8 - XXX Part Name(s) AISC HSS - 3x2x1_8 - XXXX AISC HSS - 3x2x1_8 - XXXXX AISC HSS - 3x2x1_8 - XXXXX AISC HSS - 3x2x1_8 - XXXX AISC HSS - 3x2x1_8 - XXXXXx AISC HSS - 3x2x1_8 - XXXXXxx AISCHSS - 3x2x1_8 - XXXXXxx AISC HSS - 3x2x1_8 - XXXXXx AISC HSS - 3x2x1_8 - XXXXXxx AISC HSS - 3x2x1_8 - XXXXXxx Name LAMINA HR Mass Density General Yield Strength Ultimate Tensile Strength Young's Modulus Stress Poisson's Ratio Shear Modulus Expansion Coefficient Stress Thermal Thermal Conductivity Specific Heat Part Name(s) PLATINA REFUERZO 7,85 g/cm^3 207 MPa 345 MPa 210 GPa 0,3 ul 80,7692 GPa0,000012 ul/c 56 W/( m K ) 460 J/( kg c )

file://D:\diseño 2011 a.romero\MALACATE BODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

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 Operating conditions
 Pressure:1
Load Type Pressure Magnitude 0.003 MPa  Selected Face(s)

 Gravity
Load Type Gravity Magnitude 9810.000 mm/s^2

file://D:\diseño 2011 a.romero\MALACATEBODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

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 Selected Face(s)

 Pin Constraint:1
Constraint Type Fix Radial Direction Fix Axial Direction Fix Tangential Direction Pin Constraint Yes Yes No

file://D:\diseño 2011 a.romero\MALACATE BODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

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Stress Analysis ReportPágina 5 de 34

 Selected Face(s)

 Fixed Constraint:2
Constraint Type Fixed Constraint

file://D:\diseño 2011 a.romero\MALACATE BODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

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 Selected Face(s)

 Results
  Reaction Force and Moment on Constraints
Reaction Force Magnitude Component (X,Y,Z) 0,339074 N PinConstraint:1 1631,98 N -1631,98 N 0,504632 N 69,6711 N Fixed Constraint:2 323,994 N -154,232 N 276,28 N Constraint Name Reaction Moment Magnitude Component (X,Y,Z) 4,52729 N m 5,66318 N m 0,0102026 N m 3,40223 N m 0,723285 N m 1,22283 N m -0,811231 N m -0,560427 N m

file://D:\diseño 2011 a.romero\MALACATE BODEGA\ENSAMBLE 1 Stress Analysis Report 28_03_2011.html

28/03/2011

Stress Analysis Report...
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