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Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Deformation Processing -Drawing

ver. 1

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Overview

• Description• Characteristics• Mechanical Analysis• Thermal Analysis• Tube drawing

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Geometry

DaDb

Fa, σxaFb, σxb

α

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Equipment

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Cold Drawing

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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A. Durer - Wire Drawing Mill (1489)

(copper wire)

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Characteristics• Product sizes:

– 0.0002” (5µm) to several inches (100-150 mm)

• Mostly cold (T < 0.4 Tmelting) – below recrystallization point

• Small diameter (wire):– uses a capstan

• Diameter > 1 inch (25 mm) (rod):– bull blocks on a draw bench– length up to 40 feet (12 m)

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Characteristics

• Fine wire done through several dies

• Speeds– large diameter: 30 feet per minute

(9 m/min)– small diameter: 300 feet per minute

(90 m/min)– fine wires: 5,000 feet per minute

(60 mph – 100 km/h)

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Die Materials• Large diameter

– high carbon steel– high speed steel

• Moderate diameter– tungsten carbide (WC)

• Small diameter– diamond inserts

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Characteristics

• Lubrication– Coatings– Oil

• Die angle (α)– typically small: 4-6o

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Mechanical analysis (round wire / rod)

Reduction in area (RA)

2

2

22

1

−=

−=

b

a

b

ab

DD

DDDRA

⋅=

−=

a

bt D

DRA

ln21

1lnε

DaDb

Fa, σxaFb, σxb

α

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Slab analysis

Assume p, σx are uniform– OK for small α, µ

σx + dσxσx

p

p

µp

µp

DD + dD

dx

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Equilibrium

( ) ( )

0coscos

sincos

4422

=⋅

+⋅

+

−++

αα

πµαα

π

πσπσσ

dxDpdxDp

DdDDd xxx

Expanding

( ) ( )

0coscos

sincos

42

4222

=⋅

+⋅

+

−+++

αα

πµαα

π

πσπσσ

dxDpdxDp

DdDDdDDd xxx

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Equilibrium

( ) ( )[ ]

0coscos

sincos4

224

2

2222

=⋅

+⋅

+−

+++++

αα

πµαα

ππσ

σσσσσσπ

dxDpdxDpD

dDdDdDdDddDDdDD

x

xxxxxx

small small small

Eliminating higher order terms, dividing by D & π, multiplying by 4 and canceling

0coscos

4sincos

42 =+++ αα

µαα

σσ dxpdxpDddD xx

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Equilibrium

dx

dD2tan =α

αtan2dDdx =

Notingdx

D

dD/2 α

0tan2cos

cos4tan2cos

sin42 =+++αα

αµαα

ασσ dDpdDpDddD xx

or

0tan

222 =+++α

µσσ dDppdDDddD xx

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Equilibrium

0tan

122 =⋅

+⋅+⋅+⋅ dDpdDdD xx α

µσσ

Finally

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Maximum shear stress (Tresca) criterion

flowflowx p στσ ==+ 2

B≡α

µtan

p σx

τflow

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Differential form

pBdp

DdD

flow 24 +=

τ

( )BBd

DdD

flowx

x

+−=

142 τσσ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Integrating

( )∫∫ +−=

xb

xa

b

a

BBd

DdD

flowx

xD

D

σ

στσσ

142

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing stress

• where:σxb = back stress (tension)σxa = pulling stress (tension)

B

b

a

flow

xb

B

b

a

flow

xa

DD

DD

BB

22

211

2

+

+=

τσ

τσ

DaDb

σxaσxb

α

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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12

+===nKY

n

flowflowεστ

Strain hardening (cold – below recrystallization

point)• For round parts - Tresca

average flow stress:due to shape of element

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Strain rate effect(hot – above recrystallization point)

• For a round part (derived for extrusion)

– average strain rate due to shape of element– vb = velocity of “b” side– A = area

mflowflow CY εστ &===2

⋅=

a

b

ab

bbAA

DDDv lntan6

33

2 αε&

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Value for p

p = Y – σor

p = 2τflow – σ

maximum at entrance

p σx

τflow

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Effect of back tension

with back tension

without back tension

drawing stress

entry exit

die pressure

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Maximum RA• Solve previous equations with:

α = 6o (typical value)µ = 0.1∴ B = 1σxb = 0For failure: draw stress = material flow {yield} stress

here, say K = 760 MPa, and n = 0.19

12

+===nKY

n

flowflowεστn

xa Kεσσ ==

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Maximum RA

• Yields RA = 0.6– must be solved for each µ, α, σxb

−⋅

+

=

+

B

b

an

n

DD

BB

nKK

2

11

1εε

−⋅

+

=+

2

11

111

119.0

b

aDD

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Energy / unit volume (u)

u = F V / Aa V = σxa

(with no back stress)V= volume

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Rod/Wire Drawing Analysis• Ideal deformation

External work = Work of ideal plastic deformation

for

( ) ( )

ttd

ffd

du

LAuLAt

εσσ

σε

∫==

=

0ntt Kεσ =

==

+=

fftft

nt

d AAYY

nK 0ln

1εεεσ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Rod/Wire Drawing Analysis• Ideal deformation

Drawing force, Fd = σdAf

Drawing power, Pd = Fd Vf

Source: S. Kalpakjian & S. Schmidt, 4th ed. 2003

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing Limit• Ideal deformation of a perfectly

plastic material

1

11 0.63 63%

od

f

o od

f f

o f

o

AY lnA

Y

A Aln eA A

Maximum reduction per passA AA e

ε

ε

σ

σ

σ σ

= ⋅

=

= ⇒ = ⇒ =

−= = − = =

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing Limit• Ideal deformation of a strain

hardening material

ε

σ

n+1

ideal+frictionideal

εσ

dσ dσ1

( 1)

1

1

1

no

df

n

d

o f n

o

A KY lnA n

Kn

Maximum reduction per passA A

eA

ε

ε

εσ

σ εσ σ ε

+

− +

= ⋅ = + == ⇒ = +

−= = −

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Example ProblemAssuming zero redundant work and frictional work to be 20% of the ideal work, derive an expression for the maximum reduction in area per pass for a wire drawing operation for a material with a true-stress strain curve of σ=Kεn

Total work = Ideal work + frictional work + redundant workTotal work = Ideal work + 0.2 x Ideal work = 1.2 x Ideal work

Or, Total work of deformation = 1.2 [u x volume] … (1)

In drawing, external work of deformation = σd x volume … (2)Equating (1) and (2), we get

σd = 1.2u or

12.12.12.1

11

00

11

+===

+

∫∫ nKdKd

n

tntttd

εεεεσσεε

12.1 εσ Yd = where … (3)

=

fAA0

1 lnε

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Example ProblemMax reduction occurs when total drawing stress, σd = Flow stress of material at die exit, Y

+

+

+

−=−

=∴

=⇒+

=⇒+

=

=+

=

=

2.11

0

0

2.11

001

1

11

11

1 passper reduction max

2.11ln

2.111

2.1

2.1

nf

n

ff

nn

nd

eAAA

eAAn

AAn

KnK

KYY

ε

εε

εε

σ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-1Determine power, and plot σx and p

along die length.• Drawing steel rod from φ = 13 mm

to φ = 12 mm @ 1.5 m/s• K = 760 MPa, n = 0.19• µ = 0.1, α = 4o, σxb = 0

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-2• First, we must see if we can do the

process, the limit is

• RA = 1 - (Da/Db)2 = 0.15 = 15%• εt = ln{1/(1-RA)}

= ln {1/(1-0.15)} = 0.16• B = µ/tanα = 0.1 / tan 4o = 1.43

nxa Kεσσ == max

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-3

B

b

a

flow

xb

B

b

a

flow

xa

DD

DD

BB

22

211

2

+

+=

τσ

τσ

12

+==nKY

n

flowετ

nKεσ =max

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-4• So, equating the equations (with no

back stress) yields

−⋅

+

+=

B

b

aDD

BB

n

2

111

11

−⋅

+

+=

×−

43.12min

131

43.143.11

119.011 aD

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-5

• Solving gives Da-min = 8.53 mm, so we can do the process and proceed with the analysis

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-6

35.0013121

43.143.11

2

43.12=+

−+

flow

xaτσ

( ) MPanKY

n

flow 446119.0

16.07601

219.0

=+

⋅=

+==

ετ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Drawing - Ex. 1-7

• σxa = 0.35 x 2τflow

= 0.35 x 446 MPa = 156 MPa• Fdraw = σxa x Area = 156 x π(12/2)2

= 17.6 kN = 3938 lbf• Power = Fdraw x speed = 17.6 kN x 1.5 m/s = 26.4 kW = 35.4 hp

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Dimensionless pressures (divided by 2τflow)

00.10.20.30.40.50.60.70.80.91

1212.212.412.612.813

diameter (mm)

sxp

Drawing - Ex. 1-8

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Limits on analysis

• Larger die angles– more redundant work– σ, p, u will be larger than predicted

DaDbα

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Redundant work

• ∆ = dm/L• dm = (Da + Db) / 2• p = Qr σflow

DaDbα

L (contact length)

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Redundant work factor (Backofen)(frictionless)

Qr =

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Temperature rise

D Do

Do/D ≈ 6 kD

(1-r)Q

DIE

v

kw, ρw, cwrQ

WIRE

l

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Temperatures

θ = θo + θs + θf

θo = ambient (room) temperatureθs = temperature rise in the wire

due to plastic shear energy, us

θf = interface temperature rise due to frictional energy, uf

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Specific energies

u = us + uf

u = σxa

us = 2τflow ε

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Specific energies

From the example above (steel rod):u = σxa = 156 MPaus = 2τflow ε = 446 * 0.16

= 71.4 MPa∴ uf = u - us = 156 – 71.4

= 84.6 MPa

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Shear temperature (θs)• Since the shear strain is uniform

in the wire• and all the shear energy remains

in the rod as heat• Then, we can obtain the shear

temperature in the wire:

ww

ss c

θ =

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Material properties

• For this material:– kw = 60 W/m-K– ρw = 7850 kg/m3

– cw = 500 J/kg-K– αw = 1.53 x 10-5 m2/s

• For a WC die:– kD = 42 W/m-K

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Shear temperature (θs)

Ccu

ww

ss

o2.185007850

1071.4 6

=××

==ρ

θ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Frictional heat (Q)

• v = velocity• (1-r)Q goes into the die

4

2vDuQ fπ

=

Q represents all heat generated by friction

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Die and wire temperatures (θ)• For the die (steady):

• For the wire (moving):

( )DD

lkQr o

Do ln

21

⋅−

+=π

θθ

vl

DlkQr w

wso 207.1 α

πθθθ

++=

ref: Carslaw and Jaeger

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Q calculation

WQ

vDuQ f

143524

5.1012.0106.84

42

6

2

=

⋅⋅⋅×=

=

π

π

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Dimensions• D = 12 mm

– from Do / D ≈ 6– Do = 72 mm in this example

• l = contact length = reduction in radius / sin α= 0.5 mm / sin 4o = 7.17 mm

drlα

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Die temperature

( )DD

lkQr o

Do ln

21

⋅−

+=π

θθ

( )

( )r

r

−⋅+=

⋅⋅⋅⋅−

+=

113591201272ln

00717.042214352120

πθ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Wire temperature

vl

DlkQr ww

so 207.1 απ

θθθ ⋅

⋅++=

r

r

⋅+=

⋅⋅××

⋅⋅⋅

⋅⋅++=

1812.385.12

00717.01053.1

6000717.0012.01435207.12.1820

5

πθ

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Heat flow ratio and Temperature

• Equating the previous equations yields:r = 0.99

• hence θ = 156oC = 429 K

Tmelt = 1500oC = 1723 KSo θ/Tmelt = 0.25, cold (below

recrystallization point

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Temperature in practice

• In practice, r ≈ 1– all heat goes into wire

lvD

cu

cu

www

f

ww

so ⋅

⋅⋅

⋅++=

αρρθθ

219.0

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Tube drawing

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Tube Drawing

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Plane strain / Slab analysis

+=

*

112 *

* B

i

f

flow

xa

tt

BB

τσ

βαµµ

tantan*

−+

≡ mandreldieB

α= semicone angle of dieβ =semicone angle of plug

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Tube Drawing – Special Cases

αµ

tan* ≡B

Fixed mandrel- same friction at both interface(plane – tubeis modeled as aflat section)

Moving mandrel – No friction at interfaceof mandrel and tube(plane and slab)

αµ

tan2* ≡B 2*

tan2 µαµ

−≡B

Moving mandrel with friction towards exit, takes into account motion between mandreland tube (B may be negative) (plane) α

µµtan

* mandreldieB −≡

Fixed mandrel(slab – circular tube)

βαµµ

tantan*

−+

≡ mandreldieB

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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Summary

• Description• Characteristics• Mechanical analysis• Thermal analysis• Tube drawing

Prof. Ramesh Singh, Notes by Dr. Singh/ Dr. Colton

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