DP saçlarda geri yaylanma simülasyonu-Mesut_Kaya_Coskunoz_Session15_20102010

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    Presentation Outline

    INTRODUCING COKUNZ METAL FORM COMPANY

    STAMPING PROBLEMS OF DP STEELS

    SIMULATIVE TESTS

    MODELING AND SIMULATION

    STAMPING EXPERIMENTS

    RESULTS AND COMPARISON

    FUTURE WORK

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    Cokunz Metal Form Company

    Mass Production Tools and Machinery Production

    Tests and Analyses

    MTS Durability Test SystemATOS Digitizer

    Fiat Cross Car Beam

    Fiat Fuel TankFord Control Arm

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    Cokunz R&D Activities

    Optimization with Optistruct Crash Analysis with Radioss

    Forming Simulation with Autoform andHyperformPart Design with Catia

    Fiat Fuel Tank BumperCokunz Design

    Control ArmCokunz Design

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    PUNCH

    DIE

    SHEET

    AFTER

    SPRINGBACK

    REFERENCEGEOMETRY

    FEMSimulation

    VirtualMeasurement

    DieCompansation

    OK

    Production

    DieCompansation

    OK

    Measurement

    FEMSimulation

    No

    Yes

    No

    Yes

    SPRINGBACK COMPANSATION FLOW CHART

    TOOL SETUP

    STAMPED PARTGEOMETRY

    Stamping Problems of DP Steels

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    Simulative Tests-Tensile Test

    Zwick

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    FRICTIONTESTERC

    Friction tester was adapted to MTS Test System and friction tests wereperformed for constant clamping forces.

    0

    0,02

    0,04

    0,06

    0,08

    0,1

    0,12

    0,14

    0,16

    0 10 20 30 40

    mu

    Clamping Press ( Mpa )

    Friction Test

    mu (ConstantClamping Press )

    Simulative Tests-Friction Test

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    Tool Mesh Parameters

    Blank Mesh Parameters

    Adaptivity Level

    Modeling - Meshing Parameters

    Altair 10.0 Training Document

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    Modeling - Simulation Setup

    Operations

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    Modeling - Forming Simulation

    Gas cylinder pressure Binder Force at 0 mmstrok

    Binder force at 35 mmstrok

    150 bar 460.000 N 526.000 N

    Hyperform Auto Process

    Gas Cylinder Pressure - Binder Force ChartTable 1

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    Modeling - Springback

    Symmetry Constraint (dof 1,5,6)

    Dof 2,3

    Dof 3

    Altair 10.0 Training Document

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    Die

    Five parts were produced from each material lot, all parts were digitized withAtos system and comparison were made with the reference geometry.

    DeviationBand

    0.5mm

    1mm

    2mm

    Lot1-150bar %16 %29 %52

    Lot2-150bar %15 %28 %51

    Atos Digitizing System

    Binder

    Punch

    Scanned part

    Stamped parts

    Stamping Experiments

    Comparison of Cad-Data withExperimental ResultsTable 2

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    DeviationBand

    0.5mm

    1mm

    2mm

    Lot1-150bar %56 %84 %96

    Lot2-150bar %54 %79 %92

    Results and Comparision

    Comparison of HyperForm Results

    with Experimental Data

    Springback evaluation

    with Hyperview

    Reference Geometry

    Minus Tolerance Border

    Plus Tolerance Border

    Plus Tolerance

    Band

    Minus Tolerance

    Band

    Table 3 shows evaluation of the accuracies of Hyperform simulations. The results were compared with respect tothe reference part geometry. The experimental and FEM results were positioned one by one according to best fit

    methodology and compared.

    Table 3

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    Future Work

    KINEMATIC HARDENING MODEL

    PRESSURE DEPENDED FRICTION COFFICIENT

    INTEGRATION POINT MORE THAN 5

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    THANK YOU...www.coskunoz.com.tr