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1 Pulse-Pressure Forming (PPF) of Lightweight Materials P.I.: Richard Davies, (509) 375-6474, [email protected] Presenter: Aashish Rohatgi, (509) 372-6047, [email protected] (Project 60184/Agreement 22422) 2011 DOE Vehicle Technologies Program Review Project ID: LM033 This presentation does not contain proprietary, confidential, or otherwise restricted information

Pulse-Pressure Forming of Lightweight Metals...Pulse-Pressure Forming (PPF) of aluminum and Advanced High Strength Steels (AHSS) has the potential to achieve 25 to 45% weight savings

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1

Pulse-Pressure Forming (PPF)of Lightweight Materials

P.I.: Richard Davies, (509) 375-6474, [email protected]

Presenter: Aashish Rohatgi, (509) 372-6047, [email protected]

(Project 60184/Agreement 22422)

2011 DOE Vehicle Technologies Program Review

Project ID: LM033This presentation does not contain proprietary, confidential, or otherwise restricted information

Project OverviewProject Timeline:

Start – 3Q FY08Finish – 4Q FY1185% complete

Budget:Total project funding:

PNNL: $1450k

FY08 Funding Received:$200k

FY09 Funding Received: $450k

FY10 Funding Received:$500k

FY11 Funding Authorized:$300k

TargetsThe VTP target for weight reduction of the vehicle and its

subsystems is 50%.Pulse-Pressure Forming (PPF) of aluminum and Advanced High Strength Steels (AHSS) has the potential to achieve 25 to 45% weight savings vs. conventional steels

BarriersBarriers to using PPF of aluminum and AHSS in the

lightweighting of vehicles:Lack of understanding of the formability and strain rates that develop during PPF processingLack of validated constitutive relations for lightweight materials during PPF processing Lack of validation of finite element simulation of PPF processing

PartnersOEM and Industry participants:

Sergey Golovashchenko (Ford)John Bradley & James Quinn (General Motors)Ajit Desai & DJ Zhou (Chrysler)US Steel

Relevance to Technology GapsProject Objectives:

Enable broader deployment of automotive lightweighting materials in body-in-white and closure panels through extended formability of aluminum alloys, magnesium alloys, and HSS/AHSS.Enable a broad set of PPF technologies to effectively extend the benefits of high rate sheet metal forming beyond the limitations of electrically conductive metals (aluminum) that are required for electromagnetic forming (EMF) processes.Aluminum and AHSS have limited formability at room temperature and conventional strain rates. High strain rate forming (PPF) can enhance room temperature formability

Extended ductility of most metalsExtend the formability of AHSS at high-rate loadingGenerate greater ductility from lower cost steelsIncrease formability of Al and Mg alloys Utilize single-sided tooling at lower costProvide residual stress (springback) management

PPF of Lightweight Materials will address technology gapsDemonstrate and quantify extended ductility in Al, AHSS and Mg using PPF process and high speed camera systemValidate high-strain-rate constitutive relations for PPF of lightweight materialsCharacterize material microstructure and texture evolution at high-strain-rates

3

4

Approach/Strategy

Task 1 Formability and Fracture CharacterizationDesign, fabricate, and demonstrate the operation of the PPF system. This includes procuring high-speed cameras for real-time image capture to quantify deformation history using existing PNNL DIC systemPerform sheet forming experiments using single-pulse and multi-pulse PPF of Al-5182, DP600, and Mg-AZ31 sheet materialsCharacterize high-rate formability and extended ductility

Task 2 Microstructure and Mechanical Property EvolutionDevelop materials constitutive relations for high-rate formingCharacterize microstructural and texture evolution Characterize post-forming mechanical properties

Task 3 Numerical Simulation of PPF ProcessPPF sheet forming finite element modelingSheet-die interaction during PPF

Project Milestones

Milestones Due Status Issues?Demonstrate successful operation of the PPF apparatus

11/08

Complete experimental characterization of PPF process

9/11

Complete constitutive relations for Al, Mg, and AHSS

3/10

Complete evaluation of post-forming properties of materials subject to PPF

6/11 Focus has been shifted to help develop a high-rate forming limit diagram (FLD)

Complete evaluations of numerical simulations

3/11

5

= Complete

= On Track

= At Risk

= Late

6

Background

10-5 10-4 10-3 10-2 10-1 100 101 102 103 104 105

Plate tectonics

Creep Forming

Superplastic Forming

Conventional Forming

Automotive Crash

Strain Rate (1/sec)

High Rate Forming

Terminal Ballistics

Cosmic Events

Atomic Fission…

Interior Ballistics

THIS PROJECT

7

Introduction

High Rate Forming TechnologiesElectromagnetic Forming (EMF)Electrohydraulic Forming (EHF)Explosive Forming (classical)Laser Shock Forming (LSF)

Project Plan - Subject MaterialsAluminum Alloys

Initial focus on AA5182-O (1 mm and 2 mm)AHSS (and HSS)

Initial focus on DP600 (1 mm and 0.6 mm) [ Provided by US Steel]Magnesium Alloys

Initial focus on AZ31-O (1 mm)

8

Technical ProgressTask 1.1 - Fabrication, Assembly, and Testing of PPF Apparatus

PNNL’s PPF Setup For Free-Forming Dome

Test sheet withspeckle pattern for strain evaluation

Clamping ring

Conical Die

φ=6”

5182-O1 mm7500 V

Free-Forming

hmax~2”“Just” cracked

PNNLTest T-15

5182-O1 mm7500 V

“Petaling” failurehmax>2.5”

Conical DiePNNL

Test T-22

9

Technical ProgressTask 1.1 - Fabrication, Assembly, and Testing of PPF

Top View: Free-Forming

Side View: Cone Die

Close-up of Cameras

Looking Inside Conical Die

Test Sheet

Imaging Setup

• Imaging at ~75000 frames/second (~13 microseconds per frame)

10

Technical Progress (PPF Deformation Evolution)Task 1.2 - Single-pulse PPF

Deformation history obtained at any location on the sheet

High-speed Cameras+

Digital Image Correlation

Duration < 1 ms

11

Technical Progress (Free-Forming of Mg, Al, DP600)Task 1.2 – Single-pulse PPF

Room temperature forming of AZ31B needs experimental re-designs to

prevent failure at tool-radius

5182-O1 mm7500 V

PNNLTest T-15

Formable

ALUMINUM

DP6001 mm9500 V

PNNLTest DP6-3

Formable

DP600

Almost No Formability

AZ31B-O1 mm5500 V

PNNLTest AZ-1

FAILURE AT RADIUS

MAGNESIUM

12

Technical Progress (Mg: Quasi-static vs. PPF) Task 1.2 – Single-pulse PPF

(High-Rate)Pulse-Pressure Forming

AZ31B-O1 mm5500 V

Smallcurvature

AZ31B-O1 mm5500 V

Plane-StrainGeometrySmall

curvature•High-strain-rate may improve Mg formability, somewhat, over quasi-static formability•Requires PPF tooling re-design to verify

Quasi-Static Pressure Forming

AZ31B-O1 mmQuasi-static

6”

Nocurvature

13

Technical Progress (Mechanical Characterization)Task 2.1 – Constitutive Relations

• Tensile behavior quantified at quasi-static and high-strain-rates• Constitutive equations are used to model sheet behavior

during pulse-pressure forming

0

100

200

300

400

500

0 5 10 15 20 25 30 35 40

0.001/s0.01/s0.1/s1000/s2000/s2400/s

Eng

inee

ring

Stre

ss (M

Pa)

Engineering Strain (%)

AZ31B-O, Rolling DirectionTension, Room Temperature

AZ31B

Test data from Prof. K.S. Vecchio, UC San Diego

0

100

200

300

400

500

0 5 10 15 20 25 30 35 40

0.001/s0.01/s0.1/s1000/s2000/s2400/s

Eng

inee

ring

Stre

ss (M

Pa)

Engineering Strain (%)

Al 5182-O, Rolling DirectionTension, Room Temperature

5182-O Al

0

200

400

600

800

1000

0 5 10 15 20 25 30 35 40

0.001/s0.01/s0.1/s1000/s2000/s2400/s

Eng

inee

ring

Stre

ss (M

Pa)

Engineering Strain (%)

DP600, Rolling DirectionTension, Room Temperature

DP600

14

Technical Progress (Mg: Strain-rate Effects)Task 2.1 – Constitutive Relations

• Positive strain-rate sensitivity High-rate forming has potential for forming magnesium

• Limiting factors: Low ductility, texture

AZ31BRolling Direction

0

100

200

300

400

500

0 5 10 15 20 25 30 35 40

0.001/s0.01/s0.1/s1000/s2000/s2400/s

Eng

inee

ring

Stre

ss (M

Pa)

Engineering Strain (%)

AZ31B-O, Rolling DirectionTension, Room Temperature

Test data from Prof. K.S. Vecchio, UC San Diego

AZ31BTransverse Direction

0

100

200

300

400

500

0 5 10 15 20 25 30 35 40

0.001/s0.01/s0.1/s1000/s2000/s2400/s

Eng

inee

ring

Stre

ss (M

Pa)

Engineering Strain (%)

AZ31B-O, Transverse DirectionTension, Room Temperature

Technical ProgressForming Limit Diagram (FLD) for High-Rate Forming

15

• Dome formability limited by the location that crosses the ‘safe’ forming-limit first

• Free-forming has not shown extended ductility in literature

PNNL’s Approach• New specimen design to impose

plane-strain deformation• This will provide lower limit of

formability

PPF Dome-forming• Different locations have

different strain-paths.

Technical Progress (Determination of FLD0)Task 3.1 – Numerical Simulation of Sheet Forming

0

0.1

0.2

0.3

0.4

0.5

0.6

-0.6 -0.1 0.4

Maj

or S

trai

n

Minor Strain

Simulated Strain Paths

Design 1

Design 2

Al 5182-O1 mm

Novel specimen geometries developed to determine plane-strain formability during PPF

Question: What is the minimum formability at high-rates

Model 16”

Model 26”

17

Technical Progress (Determination of FLDo)Task 3.1 – Numerical Simulation of Sheet Forming

True eq. plastic strain

Model 15182-O

1 mm8500 V

PNNLTest T-71

Plane-strain formability during PPF demonstratedNumerical model validated

True eq. plastic strain

Model 2

PNNLTest T-74

PNNLTest T-74

5182-O1 mm

8500 V

18

Technical ProgressFLD at High-Strain-Rates during PPF

•Enhanced formability is observed in Al during PPF:•FREE-FORMING () and CONICAL-DIE()•Strain-rates ~4000/s and up

•DEFORMATION HISTORY QUANTIFIED

PPF high-rate formingvs.

quasi-static forming(Reynold’s data)

All data in engineering units

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

-0.5 -0.4 -0.3 -0.2 -0.1 0 0.1 0.2 0.3 0.4 0.5

Maj

or S

trai

n

Minor Strain

T-30 - 6500V Conical Die

T-64 - 9900V Conical Die

T-74 - 8500V Free-forming

T-74 - 8500V Free-forming

Safe,Conical Die(est. ~1700/s

at apex)

Incipient

Safe, Conical Die

(~740/s)

Safe

Free-form(~3900/s)

Forming Limit Diagram for 5182-O Al

•Strain-rate amplification at non-apex locations,strain-rate in die-interior ~ 5000/s (estimated)

PNNLTest T-74

19

0

0.05

0.1

0.15

0.2

0.25

0.3

0.35

0.4

0.45

0.5

-0.5 -0.4 -0.3 -0.2 -0.1 0 0.1 0.2 0.3 0.4 0.5

Maj

or s

trai

n

Minor strain

Point 1 (Near Edge 1/4)Point2 (1/2)Point3 (2/3 from edge)APEX

5182-O Al1 mm

Technical Progress (Strain-path Changes)Task 3.2 – Numerical Simulation of Sheet-Die Interaction

Strain path changeUpon impact with the die

Impact of sheet with the die may lead to: Strain path changes Strain-rate

increase Compressive stresses Void

suppression Net result: Increased formability Opacity of die makes it extremely

challenging to experimentally determine deformation history and verify model predictions

PNNL’s Conical Die

20

Future Work(Remainder of FY11)

Pulse-Pressure Forming of MagnesiumSpecimen re-design

Quasi-static Dome FormingPlane-strain formability: Quasi-static vs. High-rateConventional pre-forming + pulse-pressure forming (re-strike)

Project PlanTechnology Transition including Industry Partners

Industrial partners: GM, Ford, and Chrysler:Review project progressGuidance on material and process prioritiesResults available for internal process development

PNNL has partnered with OEM and materials suppliers who have active development programs in this topic area. The research plans and results are actively shared with those collaborative partners

21

22

SummaryUnique Capabilities Developed

Time-resolved measurements of full-field deformation during PPFHigh-rate forming behavior quantified for AlSafe plane-strains as high as ~50% at ~3900/s peak strain-rate observed in free-forming of aluminumSafe plane-strains of ~65% at ~2000/s peak strain-rate (apex) measured when aluminum is formed in a conical die

Experimentally-validated Numerical SimulationsNovel PPF specimen geometries designed and validated to determine FLD0Analyzed sheet-die interactions and pulse-pressure profiles

Mechanical CharacterizationQuasi-static and high-strain-rate tensile testing of AZ31B-O, 5182-O Al and DP600 performed Constitutive equation development

Publications1 journal manuscript submitted and several others are in preparation

PresentationsInternational conferences: IDDRG-2010 and Plasticity-2011