Transcript

© Fraunhofer SCAI © SIDACT GmbH

Robustness analysis – Significant reduction of scatter occurrence

Dominik Borsotto, Robin Strickstrock, Clemens A. Thole

Dominik Borsotto

© Fraunhofer SCAI © SIDACT GmbH

Agenda Background

Methods

Example

Summary

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"The model has been developed by The National Crash Analysis Center (NCAC) of The George Washington University under a contract with the FHWA and NHTSA of the US DOT“ http://www.ncac.gwu.edu/vml/models.html

Background

Simulation FE Model Sim.Result

Crash Test Car Result

Verification

© Fraunhofer SCAI © SIDACT GmbH

"The model has been developed by The National Crash Analysis Center (NCAC) of The George Washington University under a contract with the FHWA and NHTSA of the US DOT“ http://www.ncac.gwu.edu/vml/models.html

Background

Simulation FE Model Sim.Result

Crash Test Car Result

Manufacturing

tolerances

Verification

© Fraunhofer SCAI © SIDACT GmbH

"The model has been developed by The National Crash Analysis Center (NCAC) of The George Washington University under a contract with the FHWA and NHTSA of the US DOT“ http://www.ncac.gwu.edu/vml/models.html

Background

Simulation FE Model Sim.Result

Crash Test Car Result

Manufacturing

tolerances

Verification Emulate m.-

tolerances

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Background

Contact / no contact 90° contact buckling

Element failures friction

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Background

Approach:

• Part based thickness variation representing production tolerances

• Generate series of simulations

• Analyze all simulations at once

Simulation i

Statistics

+ PCA

Fringeplots

Scattermodes

Standard

Postprocessor

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Managing variability can be important

R. Brown, JLR at LS-Dyna conference 2013: “Relating Scatter in Occupant Injury to Airbag Behavior”

Methods

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Wind (environment)

Shake (design)

Variability may have a structure

Methods

R. Brown, JLR at LS-Dyna conference 2013: “Relating Scatter in Occupant Injury to Airbag Behavior”

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X = X + α*Mode 1 + β*Mode 2 +..

• Mode 1 => horizontal scatter

• Mode 2 => vertical scatter

Scatter mode representation

Wind (environment)

Shake (design)

Methods

R. Brown, JLR at LS-Dyna conference 2013: “Relating Scatter in Occupant Injury to Airbag Behavior”

© Fraunhofer SCAI © SIDACT GmbH

Can rank by importance

X = X + α*Mode 1 + β*Mode 2 +..

Principal Component Analysis

Wind (environment)

Shake (design)

Methods

R. Brown, JLR at LS-Dyna conference 2013: “Relating Scatter in Occupant Injury to Airbag Behavior”

© Fraunhofer SCAI © SIDACT GmbH

Example: Chevrolet Silverado

Chevrolet Silverado

"The model has been developed by The National Crash Analysis Center (NCAC) of The George Washington University under a contract with the FHWA and NHTSA of the US DOT“ http://www.ncac.gwu.edu/vml/models.html

Model Chevrolet

Silverado

Year 2007

Number of Parts 679

Finite-Elements

929,131

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Maximum variation of node position in [mm]

Example: Chevrolet Silverado

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Example: Chevrolet Silverado

Firewall mode information? X = X + α*Mode 1 + β*Mode 2 +…

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Example: Chevrolet Silverado

1 dominating mode

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Example: Chevrolet Silverado

2 Cluster

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Example: Chevrolet Silverado

Dominating firewall scatter mode at power-brake

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Example: Chevrolet Silverado

Subtraction of power-brake

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Example: Chevrolet Silverado

Dominating firewall scatter mode at longitudinal rail

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Subtraction of longitudinal rail

Example: Chevrolet Silverado

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Firewall scatter after design adaptations

Example: Chevrolet Silverado

Desig

n a

da

pta

tions

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Summary

• Production tolerances can have a big impact on simulation results

• Easy emulation of thickness variation triggers model instabilities

• PCA based scatter modes reveal instabilities

• More robust design

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Thank you for your attention!

Dominik Borsotto


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