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ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 1
Research and Development in
Forging at ERC/NSM
Dr. Taylan Altan, Professor and Director, [email protected]
Ms. Linda Anastasi, Office Secretary, [email protected]
Center for Precision Forming (CPF)
Engineering Research Center for Net Shape Manufacturing (ERC/NSM)
Columbus, Ohio, USA
Phone: 614-292-9267, Fax: 614-292-7219
www.ercnsm.org & www.cpforming.org
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved.
ERC/NSM Webpage
Slide 2
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved.
Organization Structure
ERC/NSMThe Ohio State University
Dr. Taylan Altan, Professor and Director
Government agenciesDepartment of EnergyDepartment of DefenseNational Science Foundation
Individual companies from countriesU.S.A, Germany, Japan, FranceSpain, New Zealand, Canada
Graduate students
Students pursuing Masters and Ph.D degree at The Ohio state university
Visiting Scholars
Students pursuing Dipl-Ing and Ph.D degree at other universities in Europe
Slide 3
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 4
ERC/NSM Activities
Stamping Hydroforming MachiningForging
Research for Industry and Government
1) Material characterization <flow stress & formability>
2) Tribology < friction,lubrication & wear >
3) Process Modeling (FEA)/Tool and Process Design
4) Short Courses/Training for Industry and Students
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 5
ERC/NSM Activities
Stamping Hydroforming MachiningForging
Research for Industry and Government
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 6
ERC/NSM Activities in Forging
1. Materials Determination of material flow stress data by cylinder compression tests.
2. Tribology (Friction, Tool Wear) Performance evaluation of cold forging lubricants.
Die Failure (Wear/ Fracture) Prediction
3. Process Modeling / Tool and Process Design
• 3D Simulation of Aircraft Structural Components.
• Forging of Internal Combustion Engine Pistons from Aluminum Alloys.
• Multiple Action Cold Forging of Complex Shaped Parts
• Prediction and Reduction of Die Failure in Precision Hot Forging
• Simulation to Compare Surface Quality in Billet Shearing
• Improvement in Tool Life for Cold Header Tooling
• Prevention of Ductile Fracture (Chevron Cracks)
• Stress Analysis and Evaluation of the Bullet Crimping Process
• Three Dimensional Finite Element Simulation of Orbital Forming of Spindle/Bearing Assembly
• Microforming of Medical Devices
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 7
1.Materials/ Compression Test Tooling
Upper plate
Carbide inserts
Load-cell 1
(200 T)
Load-cell 2
(15 T)
Lower plate
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 8
1. Materials/ Deformed billets
Height
reduction =44.5%
Height
reduction =52%Height
reduction =62%Height
reduction =33%
Micrographs of side surface after deformation
0.01 mm
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 9
1. Materials/ Test Results
- Flow stress at different reductions -
Flow Stress Curves-As Received Begin
0
20000
40000
60000
80000
100000
120000
0 0.2 0.4 0.6 0.8 1 1.2Strain
Str
es
s (
psi)
Height reduction=33%
Height reduction=44.5%
Height reduction=52%
Height reduction=67%Reduction=33%
Reduction=44.5%
Reduction=52%Reduction=67%
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 10
1. Materials/ Test Results
- Flow stress Curve -
Flow Stress Curve
0
20000
40000
60000
80000
100000
120000
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7Strain
Str
ess (
psi)
From Experiment
From Equation
K= 117 Ksi, n=0.18 determined by least square fit
18.0117
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 11
Tribology (Friction, Tool Wear)
Performance evaluation of cold forging lubricants by the double
cup extrusion test.
Evaluation of alternative lubricants for replacement of zinc
phosphate coating based lubricants.
Wear and Fracture prediction using FEM simulation.
2. Tribology
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 12
2. Tribology/ Double Cup
Extrusion Tooling
Double cup extrusion tooling with lower punch at
its upper position for billet removal.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 13
Double cup extrusion tooling (sectional view).
2. Tribology/ Double Cup Extrusion
Tooling
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 14
2. Tribology/ Test Results
Initial billet Formed billet
h1
h2
• Ranking the lubricants based on cup height ratio h1/h2
• Surface analysis is done on the cut specimen to investigate galling
• Coefficient of Friction can be determined
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 15
2. Tribology/ Tested Lubricants
Three lubricant candidates for replacement of zinc phosphate
coating based lubricants were tested.
• MEC Homat
• Daido
• Metal Coating International (MCI)
• Zinc Phosphate Coating ( Control lubricant )
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 16
2. Tribology/ Lubricant Performance
Friction factor obtained for different lubricants
0.035
0.075
0.068
0.04
0
0.01
0.02
0.03
0.04
0.05
0.06
0.07
0.08
Mec Homat MCI Phoscoating Daido
Lubricants
Fri
ctio
n fa
cto
r (m
)
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 17
2. Tribology/ Die Failure Prediction
• Die Wear (Abrasive)
• Archard’s Model:
• Behrens’ Model: vdtH(time)
PKW
a
dt(time)H
vPKW
c
ba
Where:
W= Amount of Wear
K= Process Wear Coefficient
P= Normal Pressure
v= Sliding Velocity
H= Hardness of the Die
dt= Time Interval
a, b, c= experimental constants
Current Work being done by:
Adam Groseclose, GRA ([email protected])
Dr. Changhyok Choi, Visiting Scholar ([email protected])
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 18
R
Z
2. Tribology/ Die Failure Prediction (Abrasive Wear)
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 19
2. Tribology/ Die Failure Prediction (Fatigue Fracture)
386MPaFatigue Fracture is predicted,
using Deform 2D, to be in the
same region as experimentally
determined.
The stresses of the region
were found to be tensile, which
would cause a fatigue loading
and eventual fracture.
• Die Fracture (Fatigue)
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 20
• 3D Simulation of Aircraft Structural Components.
• Forging of Internal Combustion Engine Pistons from Aluminum Alloys.
• Multiple Action Cold Forging of Complex Shaped Parts
• Prediction and Reduction of Die Failure in Precision Hot Forging
• Simulation to Compare Surface Quality in Billet Shearing
• Improvement in Tool Life for Cold Header Tooling
• Prevention of Ductile Fracture (Chevron Cracks)
• Stress Analysis and Evaluation of the Bullet Crimping Process
• Three Dimensional Finite Element Simulation of Orbital Forming of
Spindle/Bearing Assembly
• Microforming of Medical Devices
3. Process Modeling and
Development
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 21
Forging sequence for the aircraft wheel.
3. Process Modeling/
Simulation of Aircraft Wheel
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 22
3. Process Modeling/
Simulation of Aircraft Wheel
Software: DEFORM 3D
Part: Aircraft Wheel
Size: Diameter – 560 mm;
Height – 216 mm
Stage: Preforming
Material: AA 2014
Initial Temperature:
• Dies = 700oF
• Billet = 700oF
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 23
Forging sequence for an aircraft fitting.
3. Process Modeling/
Simulation of Aircraft Fitting
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 24
3. Process Modeling/
Simulation of Aircraft Fitting
Software: DEFORM 3D
Part: Aircraft Fitting
Size: 28” x 4” x 4”
Stage: Preforming
Material: Ti – 6Al – 4V
Initial Temperature:
• Dies = 600o F
• Billet = 1750o F
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 25
3. Process Modeling/
Forging of an Automotive Component
Hot forging of an automotive component.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 26
3. Process Modeling/
Simulation of Flashless Forging
Flashless forging of a connecting rod.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 27
3. Process Modeling/ Forging of IC Engine Piston for Racing
Forging of a race-car Al alloy piston.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 28
Cross groove inner race of a constant velocity joint.
3. Process Modeling/ Cold Forging Using Multiple Action Tooling
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 29
3. Process Modeling/ Cold Forging Using Multiple Action Tooling
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 30
3. Process Modeling/
Simulation of Billet Shearing
Billet shearing with element deletion.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 31
3. Process Modeling/
3-D Simulation of Billet Shearing
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 32
3. Process Modeling/
Prediction of Chevron Cracks
Prediction of chevron cracks during forward extrusion.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 33
3. Process Modeling/
Orbital Forming
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 34
3. Process Modeling/
Orbital Forming
Stress contour during orbital forming.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 35
3. Process Modeling/
Micro - Forming
Microforming of cutting blades
(Part thickness = 0.1 mm; flash thickness = 0.01 mm ).
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 36
3. Process Modeling/
Micro - Forming
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 37
3. Process Modeling/ Assembly of Tubular Components by
Mechanical Crimping
Application to bullet crimping with a mechanical tool.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 38
Simulation of bullet pullout test (test of crimp quality).
3. Process Modeling/ Assembly of Tubular Components by
Mechanical Crimping
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 39
3. Process Modeling/ Assembly of Tubular Components by Hydraulic
Crimping
Application to bullet crimping with a rubber tool.
ERC
NSM
© Copyright Engineering Research Center for Net Shape Manufacturing, 2005. All rights reserved. Slide 40
Simulation of bullet pullout test (test of crimp quality).
3. Process Modeling/ Assembly of Tubular Components by Hydraulic
Crimping