12 - Joe Meyecic - AHSS Tooling Technologies

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w w w . a u t o s t e e l . o r g Die Development for AHSS Case Study Joe Meyecic Diversified Tooling Group

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Die Development for AHSSCase StudyJoe Meyecic

Diversified Tooling Group

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Diversified Tooling Group

Superior 

Cam

Superior Cam has established

itself as a technical leader in the

Prototype Sheet Metal Industry

during the past 30 years. We have

built a reputation as an innovative,

experienced and reliable full service

operation which emphasizes

production intent quality at every

step of the tooling process.

Midland

Design

Midland Design has 40 years of 

experience designing all types of 

vehicle sheet metal stamping dies.

Midland Design is regarded as a

leader in the field of “Solid CAD Die

Design.”

Bespro

Pattern

During the past 45 years Bespro

Pattern has developed an excellentreputation for quality, timing and

competitive prices. We are a

respected leader in the CNC

machining of poly patterns off solid

CAD die design.

American

Tooling

Center 

 American Tooling Center is a modernstate-of-the-art Tool and Die facility.

Our full service operation was

designed and constructed in 1989 as

a world class production die facility

which emphasizes a CAD/CAM/CNC

utilization.

4 companies

1 goal:

Full Service

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Defining the Part

• Fiat 500 Cabrio C-Pillar

• Material Specs:

– 1.2mm gage

– Dual Phase 590 steel

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C-Pillar Concerns

• Dimensional Tolerance

• Edge Fractures

• Splits

• Zinc Pick-up

• Excessive Die Wear

• Excessive Tonnage Requirements

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Product Design Modifications 

Changes driven by FEA results

Past design in red

New design in blue

Nose section

New product design also affected assembly

features resulting in modified weld sequence

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Fractures in Stamping 

• Dual phase steel is susceptible to fracture prior to localized necking 

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Zinc Pick-up on Die Steels

• Dies for dual phase material are prone to excessive zinc flaking from the

material during the forming process.

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Excessive Die Wear 

• Dual phase steel drives heavy wear on side walls in forming dies, requiring 

upgraded die materials and heat treatments / coatings.

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Forming Force Requirements 

• Effect of Material Strength

– Increases in material strength result in increases of forming 

force requirements for typical automotive parts

40

60

80

100

120140

160

153 158 163 168 173

Crank Angle

   F   o   r   m   i   n   g   F   o   r   c   e   (   M   e   t   r   i   c

   t   o   n   s   )

100 

200 

300 

400 

500 

600 

700 

145  155  165  175  185  195 

Crank Angle 

   F  o  r  m

   i  n  g   F  o  r  c  e   (   M  e   t  r   i  c   t  o  n  s   ) DP980 

DP780 

DP600 

Binder tonnage

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C-Pillar “Givens” 

• Have to meet dimensional requirements (nominal)

• Lead time is short (22 weeks including design)

• Little time for physical rework loops

• Restrike operations have minimal effect

• Parts have to run double

– Die investment

– Piece cost

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Goals

• Plan for Advanced High Strength Steel Success

• Reduce / Eliminate Iterations in the press

• Increase Capability of Math-based system and

process

• Drive the iterations into Math

• Meet the short lead time requirements

• Meet the dimensional requirements

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C-Pillar Concerns - Addressed

• Dimensional Tolerance

• Edge Fractures

• Splits

• Zinc Pick-up

• Excessive Die Wear

• Excessive Tonnage

Requirements

Full Cycle SimulationWith Part Compensation

& Minor Product Chgs.

D2 Inserts with Coated

Steels for Heat Treat

High Pressure calculated

For Binder System

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C-Pillar Overall Approach

• Examine the historic process

• Implement every technological advantage

• Intense focus on FEA / Full cycle process

• Implement upgraded machining process

• Implement upgraded tryout process

• Intense focus on Project Management

• Meet the requirements

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Historical Die Development Process

Quality

Binder Development Die DesignDuplicating Mill

Tryout Iterations

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Latest Die Development Process

Accurate!

Full Cycle Simulation 3D Solid Model High Speed NC

Press Validation (include scanning + CMM)

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ATOS SCANNER 

ATOS SCANNER 

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C-Pillar Process

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C-Pillar Process

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C-Pillar Process

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Forming Simulation

•Full Cycle Simulation per 3D Die Process– Analyze every operation in the line

–Morph required die faces to accommodate results

Iterate in math to get to nominal• Commercial Codes

• Proprietary Process and Methods

• Resolve forming issues in math (Virtual)

• Cut dies to morphed shape

• Inspect and compare to nominal

DTG Expertise to Highlight

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Full cycle explained

yes

no

Build / Adjust

Binder Development

Assess Draw Die

Assess Trim Die (with draw results)

Assess Form Die (with trim results)

Analyze Results

Results OK?

start

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Full cycle

• IterationD1 DRAW

D2 TRIM-PIERCE

CAM TRIM

D5 RE-STRIKE

COMPLETE

D3 TRIM-CAM TRIM

CAM PIERCE

Keep iterating & adjusting binder development and

Morphing until final results produce a nominal product.

ok 

D4 FLANGE

CAM-FLANGE

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Kick-off Meeting 

• Use full cycle simulation results

• Changes to cutter path programming 

• Bearing maps

• Clearance for side walls

• Variation in metal clearance

• Different tryout process

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 Tryout process changes

• Blank outline

• Blank location

• Binder tonnage / Ram tonnage

• Binder travel

• Lube

• Metal draw-in map

• Engineered beads per FEA force factor

Engineering = Design = Physical Reality

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Blank Outline & Location

Blank location to punch

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Binder Travel / Tonnage

Die set-up / binder travel

65.0mm ring travel

Punch

Binder Home

Position

Upper Die

Technical DataMaterial Spec: 590 Dual Phase

Material Code: 1182 Chrysler CodeThickness: 1.2 mmBlank holder force: 80 approximate tonsTotal force: 450 approximatetonsRing Travel 65 mm ring

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Metal Draw-in Maps

Blank run-in measured from binder set

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First Panel Results

• First panel through the line within 1.8mm of 

nominal on the checking fixture

• Still had one iteration to morph (3 days)

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Process used for Iteration

• White Light Scan

• Color map inspection reports

• Morph 120% correction factor

• Re-cut

• Re-scan

• Results after morph = OK

Total lead time = 22 weeks, including die design

Part met nominal criteria

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