Introduction to Materials Science and Engineering

(1)

Introduction to Materials Science and Engineering

Eun Soo Park

Office: 33-313

Telephone: 880-7221 Email: espark@snu.ac.kr

Office hours: by appointment

2020 Fall

11. 03. 2020

1

(2)

2

• Phase diagrams are useful tools to determine:

-- the number and types of phases present, -- the composition of each phase,

-- and the weight fraction of each phase

given the temperature and composition of the system.

• The microstructure of an alloy depends on

-- its composition, and

-- whether or not cooling rate allows for maintenance of equilibrium.

• In phase diagram, important phase transformations include eutectic, eutectoid, and peritectic.

Summary

Contents for previous class

Chapter 9 Phase Diagrams

(3)

Metatectic reaction: β ↔ L + α Ex. Co-Os, Co-Re, Co-Ru

³

(4)

Syntectic reaction Liquid

¹

+Liquid

²

↔ α

L

¹

+L

²

α

K-Zn, Na-Zn,

K-Pb, Pb-U, Ca-Cd

4

(5)

5

L+α

L+β α +β

200

C, wt% Sn

20 60 80 100

0 300

100

L

α β

T_E

40

(Pb-Sn System)

Hypoeutectic & Hypereutectic

Fig. 11.7, Callister & Rethwisch 9e.[Adapted from Binary Alloy Phase Diagrams, 2nd edition, Vol. 3, T. B.

Massalski (Editor-in-Chief), 1990.

Reprinted by permission of ASM International, Materials Park, OH.]

160 μm eutectic micro-constituent

Fig. 11.13, Callister &

Rethwisch 9e.

hypereutectic: (illustration only)

β β β

β β

β

Adapted from Fig. 11.16, Callister & Rethwisch 9e.

(Illustration only)

(Figs. 11.13 and 11.16 from Metals Handbook, 9th ed., Vol. 9, Metallography and Microstructures, 1985.

Reproduced by permission of ASM International, Materials Park, OH.)

175 μm

α α

α α α

α

hypoeutectic: C₀= 50 wt% Sn

Rethwisch 9e.

T(°C)

61.9 eutectic

eutectic: C₀= 61.9 wt% Sn

(6)

6

• For alloys for which 18.3 wt% Sn < C

₀

< 61.9 wt% Sn

• Result: α phase particles and a eutectic microconstituent

Microstructural Developments in Eutectic Systems

18.3 61.9

S R

97.8 R S

primary α eutectic α

eutectic β

W

_L

= (1- W α) = 0.50 C

_α

= 18.3 wt% Sn C

_L

= 61.9 wt% Sn

S R + S

W

_α

= = 0.50

• Just above T

_E

:

• Just below T

_E

: C

_α

= 18.3 wt% Sn C

_β

= 97.8 wt% Sn

S R + S

W

_α

= = 0.73

W

_β

= 0.27

Rethwisch 9e.

Pb-Sn system

L+ β

200

T(°C)

C, wt% Sn

20 60 80 100

0

300

100

L

α β

L+ α

40

α + β

T_E

L: C₀ wt% Sn

α

L L

α

(7)

α _iron Ferrite

(BCC)

soft & ductile γ iron

austenite (FCC)

Cementite (Fe₃C) hard & brittle

A; eutectic B; eutectoid

B

A

c. Fe-C phase diagram

C concentration 0.008w% 2.14w% 6.7w%

iron steel cast iron

7

(8)

Hypoeutectoid Steel

Proeutect ferriteoid

Pearlite

dark – ferrite light - cementite

8

(9)

Hypereutectoid Steel

Proeutectoid cementite Pearlite

9

(10)

10

Alloying with Other Elements

• T

_eutectoid

changes:

Fig. 11.33, Callister & Rethwisch 9e.

(From Edgar C. Bain, Functions of the Alloying Elements in Steel, 1939. Reproduced by permission of ASM International, Materials Park, OH.)

T Eu te c to id (º C)

wt. % of alloying elements

Ti

Ni

Mo Si

W

Cr Mn

• C

_eutectoid

changes:

Fig. 11.34,Callister & Rethwisch 9e.

(From Edgar C. Bain, Functions of the Alloying Elements in Steel, 1939. Reproduced by permission of ASM International, Materials Park, OH.)

wt. % of alloying elements C eut ec toi d (w t% C )

Ni

Ti

Cr Si

W Mn Mo

(11)

Ternary Eutectic System

(with Solid Solubility)

11

(12)

Ternary Eutectic System

12

(13)

13

Ternary Eutectic System

13

(14)

17

(18)

Ternary Eutectic System

18

(19)

Ternary Eutectic System

T= ternary eutectic temp.

L+ β+γ

L+ α+γ L+ α+β

19

(20)

Ternary Eutectic System

http://www.youtube.com/watch?v=yzhVomAdetM ²⁰

(f) e

₂

> T > E (h) E = T

₂₁

(22)

Vertical section Location of vertical section

THE EUTECTIC EQUILIBRIUM (l = α + β + γ)

22

(23)

THE EUTECTIC EQUILIBRIUM (l = α + β + γ)

23

(24)

THE EUTECTIC EQUILIBRIUM (l = α + β + γ)

(25)

25

THE EUTECTIC EQUILIBRIUM (l = α + β + γ)

(26)

< Quaternary phase Diagrams >

Four components: A, B, C, D

A difficulty of four-dimensional geometry

→ further restriction on the system Most common figure:

“ equilateral tetrahedron “ Assuming isobaric conditions, Four variables: X_A, X_B, X_C and T

4 pure components 6 binary systems 4 ternary systems

A quarternary system

(27)

ISSUES TO ADDRESS...

• Transforming one phase into another takes time.

• How does the rate of transformation depend on time and T ?

• How can we slow down the transformation so that we can engineering non-equilibrium structures?

• Are the mechanical properties of non-equilibrium structures better?

Fe

γ

(Austenite)

Eutectoid transformation

C FCC

Fe₃C

(cementite)

α

(ferrite)

+

(BCC)

Chapter 10. Phase Transformations

: Development of Microstructure and Alteration of Mechanical Properties

Contents for today’s class

27

2 1 0

G G G

∆ = − <

(28)

Microstructure-Properties Relationships

Microstructure Properties

Alloy design &

Processing Performance

“ Phase Transformation ”

“Tailor-made Materials Design”

down to atomic scale

28

(29)

(Ch1) Thermodynamics and Phase Diagrams (Ch2) Diffusion: Kinetics

(Ch3) Crystal Interface and Microstructure

(Ch4) Solidification: Liquid → Solid

(Ch5) Diffusional Transformations in Solid: Solid → Solid (Ch6) Diffusionless Transformations: Solid → Solid

Background to understand

phase

transformation

Representative Phase

transformation

Contents _Phase transformation course

29

(30)

4 Fold Anisotropic Surface Energy/2 Fold Kinetics, Many Seeds

Solidification

: Liquid Solid

Phase Transformations

30

(31)

- casting & welding - single crystal growth - directional solidification - rapid solidification

4.1. Nucleation in Pure Metals

T_m : G_L = G_S

- Undercooling (supercooling) for nucleation: 250 K ~ 1 K

<Types of nucleation>

- Homogeneous nucleation - Heterogeneous nucleation

Solidification

: Liquid Solid

31

(32)

Driving force for solidification

4.1.1. Homogeneous Nucleation

T

m

T G L ∆

V Variation of free energy per unit volume obtained from undercooling (ΔT)

32

(33)

33 33

(34)

4.1.1. Homogeneous Nucleation

L V L

_SL

L V S

V G

G ,

SL SL

S V L

V

S

G G A

V G

G

G = − = − − + γ

∆

₂ ₁

( )

SL V

r

r G r

G π

³

4 π

²

γ

3 4 ∆ +

−

=

∆

: free energies per unit volume

for spherical nuclei (isotropic) of radius : r

Surface Free Energy- destabilizes the nuclei (it takes energy to make an interface)

Volume (Bulk) Free Energy–

stabilizes the nuclei (releases energy)

(35)

**r < r* : unstable**

(lower free E by reduce size)

**r > r* : stable**

(lower free E by increase size)

r*

: critical nucleus size

Why r^* is not defined by ∆G_r= 0?

**r* dG=0**

Unstable equilibrium

SL V

r

r G r

G π

³

4 π

²

γ

3 4 ∆ +

−

=

∆

Calculation of critical radius, r*

embryo nucleus

Gibbs-Thompson Equation

V SL

r G

= ∆

∗

2 γ

SL V

r r G r

G π ³ 4π ² γ

3

4 ∆ +

−

=

∆

2 2

2 3 2

3

) (

1 3

16 )

( 3

* 16

T L

T G G

V m SL V

SL

 ∆



 



= 

= ∆

∆ π γ πγ

Tm

T G = L∆

∆ V

Critical ΔG of nucleation at r*

nuclei < r* shrink; nuclei>r* grow (to reduce energy)

35

(36)

* SL SL m

V V

2 2 T 1

r G L T

γ ^ γ ^

= ∆ =     ∆

² ²

2 3 2

3

) (

1 3

16 )

( 3

* 16

T L

T G G

V m SL V

SL

 ∆



 



= 

= ∆

∆ π γ πγ

36

(37)

Fig. 4.5 The variation of r* and r_max with undercooling ∆T

∆ **T↑ → r* ↓**

→ r

max

↑

The creation of a critical nucleus ~ thermally activated process

of atomic cluster

* SL SL m

V V

2 2 T 1

r G L T

γ ^ γ ^

= ∆ =     ∆

Tm

T G = L∆

∆

∆TN is the critical undercoolingfor homogeneous nucleation.

The number of clusters with r

^*

at ∆T < ∆T

_N

is negligible.

37

(38)

0 500 1000 1500 2000 2500 3000 3500 4000 0

200 400 600 800 1000

Os

W Re

Ta Mo

Nb Ir Ru Hf Rh Zr Pt Fe

Pd Ti Co Ni

Cu Mn Au Ag Ge

Al Sb Te Pb

Cd Bi

Sn

Se In Ga

Hg

Melting temperature > 3000K : Ta, Re, Os, W measured by ESL

Slope : 0.18

JAXA(2007)

JAXA(2005) JAXA(2003)

JAXA(2003)

Δ = 55.9 + 1.83 x 10^-1T Measuring high temperature properties!

Maximum undercooling vs. Melting temperature

38

(39)

39

* Copper Homogeneous nucleation

ΔT = 230 K → r* ~ 10^-7 cm < 4 *

(Diameter of Cu atom)

If nucleus is spherical shape,

V = 4.2 * 10^-21 cm³ ~ 360 atoms (∵one Cu atom 1.16 *10^-23 cm³)

“Typically in case of metal” ΔT * ~ 0.2 T_E / σ_SL ~ 0.4 L r* (critical nucleus for homogeneous nucleation) of metal ~ 200 atoms

But,

if cluster radius

~ (only

4 * atom diameter)

,

“no spherical shape”

(large deviation from spherical shape) →

→ Possible structure for the critical nucleus of Cu : bounded only by {111} and {100} plane

- σ_SL may very with the crystallographic nature of the surface.

- The faces of this crystal are close to their critical size for 2D nucleation at the critical temp for the nucleus as a whole.

(40)

4.1.2. The homogeneous nucleation rate - kinetics

How fast solid nuclei will appear in the liquid at a given undercooling?

C

₀

: atoms/unit volume

C

^*

**: # of clusters with size of C* ( critical size )**

) exp(

* hom

0

kT

C G

C

^∗

= − ∆

clusters / m³

The addition of one more atom to each of these clusters will convert them into stable nuclei.

) exp(

* hom 0

hom

kT

C G f

N

_o

∆

−

=

nuclei / m³∙s f_o ~ 10¹¹ s^-1: frequency ∝ vibration frequency energy

of diffusion in liquid surface area (const.)

C_o ~ typically 10²⁹ atoms/m³

2 2

2 3

) (

1 3

* 16

T L

G T

V m SL

 ∆



 



= 

∆ πγ

- hom

* 3 1

1 cm s when G ~ 78 k

N ≈

⁻

∆ T

Homogeneous Nucleation rate

임계핵 크기의 cluster 수

한 개 원자 추가로 확산시 핵생성

Reasonable nucleation rate ⁴⁰

(41)

kT L A T

V

m SL 2

2 3

3 16 πγ

} =

) exp{ (

₂

0

hom

T

C A f

N

_o

− ∆

≈

A = relatively insensitive to Temp.

Fig. 4.6 The homogeneous nucleation rate as a function of undercooling ∆T. ∆TN is the critical undercooling for homogeneous nucleation.

→

critical value for detectable nucleation

- critical supersaturation ratio - critical driving force

- critical supercooling

How do we define ∆T

_N

?

where

4.1.2. The homogeneous nucleation rate - kinetics

hom 2

~ 1 N T

∆

→ for most metals, ΔT

_N

~0.2 T

_m

(i.e. ~200K)

Changes by orders of magnitude from essentially zero to very high values over a very narrow

temperature range

41

(42)

*

0

exp( * / ) C = C −∆ G kT

Homogeneous Nucleation Rate

hom 0

exp G

^m

exp G *

N C

kT kT

ω ^ ^∆ ^ ^ ^∆ ^

=   −     −  

Concentration of Critical Size Nuclei per unit volume

C₀ : number of atoms

per unit volume in the parent phase

hom

*

N = f C ^f ⁼ ^ω ^exp ( ⁻ ^∆ ^G

_m

^kT )

vibration frequency, area of critical nucleus ω ∝

m :

G activation energy for atomic migration

∆

Homogeneous Nucleation in Solids

If each nucleus can be made supercritical at a rate of f per second,

: f depends on how frequently a critical nucleus can receive an atom from the α matrix.

: This eq. is basically same with eq (4.12) except considering temp. dependence of f.

42

(43)

hom 0

exp G

^m

exp G *

N C

kT kT

ω ^ ^∆ ^ ^ ^∆ ^

=   −     −  

= Q

_d

4.1.2. The homogeneous nucleation rate - kinetics

43

(44)

Under suitable conditions, liquid nickel can be undercooled (or

supercooled) to 250 K below T

_m

(1453

^o

C) and held there indefinitely without any transformation occurring.

Normally undercooling as large as 250 K are not observed.

The nucleation of solid at undercooling of only ~ 1 K is common.

The formation of a nucleus of critical size can be catalyzed by a suitable surface in contact with the liquid. → “Heterogeneous Nucleation”

Which equation should we examine?

) exp(

* hom 0

hom

kT

C G f

N =

_o

− ∆

* ( ) ( )

3 3 2

SL SL m

2 2 2

V V

16 16 T 1

G 3 G 3 L T

πγ ^ πγ ^

∆ = ∆ =     ∆

Why this happens? What is the underlying physics?

Real behavior of nucleation: metal ΔT

_bulk

< ΔT

_{small drop}

Ex) liquid container

or

liquid

Solid thin film (such as oxide)

44

(45)

Introduction to Materials Science and Engineering

Eun Soo Park

Office: 33-313

Telephone: 880-7221 Email: espark@snu.ac.kr

Office hours: by appointment

2020 Fall

11. 05. 2020

1

(46)

2

Ternary Eutectic System

2

(47)

< Quaternary phase Diagrams >

Four components: A, B, C, D

A difficulty of four-dimensional geometry

→ further restriction on the system Most common figure:

“ equilateral tetrahedron “ Assuming isobaric conditions, Four variables: X_A, X_B, X_C and T

4 pure components 6 binary systems 4 ternary systems

A quarternary system

(48)

Microstructure-Properties Relationships

Microstructure Properties

Alloy design &

Processing Performance

“ Phase Transformation ”

“Tailor-made Materials Design”

down to atomic scale

4

(49)

Contents for previous class

5

(Ch1) Thermodynamics and Phase Diagrams (Ch2) Diffusion: Kinetics

(Ch3) Crystal Interface and Microstructure

(Ch4) Solidification: Liquid → Solid

(Ch5) Diffusional Transformations in Solid: Solid → Solid (Ch6) Diffusionless Transformations: Solid → Solid

Background to understand

phase

transformation

Representative Phase

transformation

Contents _Phase transformation course

2 1 0

G G G

∆ = − <

A B

Time

Chapter 10. Phase Transformations

: Development of Microstructure and Alteration of Mechanical Properties

(50)

Liquid Undercooled Liquid Solid

<Thermodynamic>

Solidification:

Liquid Solid

• Interfacial energy ΔT_N T_m

Melting and Crystallization are Thermodynamic Transitions

6

(51)

7 7

(52)

Fig. 4.5 The variation of r* and r_max with undercooling ∆T

∆T↑ → r* ↓

→ rmax↑

The creation of a critical nucleus ~ thermally activated process

of atomic cluster

* SL SL m

V V

2 2 T 1

r G L T

γ ^ γ ^

= ∆ =     ∆

Tm

T G = L∆

∆

∆TN is the critical undercooling for homogeneous nucleation.

The number of clusters with r^* at ∆T < ∆T_Nis negligible. 8

(53)

0 500 1000 1500 2000 2500 3000 3500 4000 0

200 400 600 800 1000

Os

W Re

Ta Mo

Nb Ir Ru Hf Rh Zr Pt Fe

Pd Ti Co Ni

Cu Mn Au Ag Ge

Al Sb Te Pb

Cd Bi

Sn

Se In Ga

Hg

Melting temperature > 3000K : Ta, Re, Os, W measured by ESL

Slope : 0.18

JAXA(2007)

JAXA(2005) JAXA(2003)

JAXA(2003)

Δ = 55.9 + 1.83 x 10^-1T Measuring high temperature properties!

Maximum undercooling vs. Melting temperature

9

(54)

10

* Copper Homogeneous nucleation

ΔT = 230 K → r* ~ 10^-7 cm < 4 *

(Diameter of Cu atom)

If nucleus is spherical shape,

V = 4.2 * 10^-21 cm³ ~ 360 atoms (∵one Cu atom 1.16 *10^-23 cm³)

“Typically in case of metal” ΔT * ~ 0.2 T_E / σ_SL ~ 0.4 L r* (critical nucleus for homogeneous nucleation) of metal ~ 200 atoms

But,

if cluster radius

~ (only

4 * atom diameter)

,

“no spherical shape”

(large deviation from spherical shape) →

→ Possible structure for the critical nucleus of Cu : bounded only by {111} and {100} plane

- σ_SL may very with the crystallographic nature of the surface.

- The faces of this crystal are close to their critical size for 2D nucleation at the critical temp for the nucleus as a whole.

(55)

kT L A T

V

m SL 2

2 3

3 16 πγ

} =

) exp{ (

₂

0

hom

T

C A f

N

_o

− ∆

≈

A = relatively insensitive to Temp.

Fig. 4.6 The homogeneous nucleation rate as a function of undercooling ∆T. ∆TN is the critical undercooling for homogeneous nucleation.

→

critical value for detectable nucleation

- critical supersaturation ratio - critical driving force

- critical supercooling

How do we define ∆T_N?

where

4.1.2. The homogeneous nucleation rate - kinetics

hom 2

~ 1 N T

∆

→ for most metals, ΔT_N~0.2 T_m (i.e. ~200K)

Changes by orders of magnitude from essentially zero to very high values over a very narrow

temperature range

11

(56)

hom 0

exp G

^m

exp G *

N C

kT kT

ω ^ ^∆ ^ ^ ^∆ ^

=   −     −  

= Q_d

4.1.2. The homogeneous nucleation rate - kinetics

12

(57)

Under suitable conditions, liquid nickel can be undercooled (or

supercooled) to 250 K below T

_m

(1453

^o

C) and held there indefinitely without any transformation occurring.

Normally undercooling as large as 250 K are not observed.

The nucleation of solid at undercooling of only ~ 1 K is common.

The formation of a nucleus of critical size can be catalyzed by a suitable surface in contact with the liquid. → “Heterogeneous Nucleation”

Which equation should we examine?

) exp(

* hom 0

hom

kT

C G f

N

_o

∆

−

=

* ( ) ( )

3 3 2

SL SL m

2 2 2

V V

16 16 T 1

G 3 G 3 L T

πγ  πγ 

∆ = ∆ =     ∆

Why this happens? What is the underlying physics?

Real behavior of nucleation: metal ΔT

_bulk

< ΔT

_{small drop}

Ex) liquid container

or

liquid

Solid thin film (such as oxide)

13

(58)

Nucleation becomes easy if ↓ by forming nucleus from mould wall

γ

SL

. From

Fig. 4.7 Heterogeneous nucleation of spherical cap on a flat mould wall.

4.1.3. Heterogeneous nucleation

2 2

2 3

) (

1 3

* 16

T L

G T

V m SL

 ∆



 



= 

∆

πγ

SM SL

ML

γ θ γ

γ = cos +

SL SM

ML

γ γ

γ

θ ( ) /

cos = −

het S v SL SL SM SM SM ML

G V G A γ A γ A γ

∆ = − ∆ + + −

3 2

4 4 ( )

het

3

V SL

G ^ π r G π γ r ^ S θ

∆ = −  ∆ + 

 

where S ( ) θ = (2 cos )(1 cos ) / 4 + θ − θ

²

In terms of the wetting angle (θ ) and the cap radius (r) (Exercies 4.6)

14

(59)

S(θ) has a numerical value ≤ 1 dependent only on θ (the shape of the nucleus)

* *

( )

hom

G

het

S θ G

∆ = ∆

^r ^* ² ^γ_G ^and ^G^* ¹⁶₃ ^πγ_G³² ^S⁽^θ⁾

V SL V

SL ⋅

= ∆

∆ ∆

=

( ) S θ

θ = 10 → S(θ) ~ 10^-4 θ = 30 → S(θ) ~ 0.02 θ = 90 → S(θ) ~ 0.5

15

(60)

S(θ) has a numerical value ≤ 1 dependent only on θ (the shape of the nucleus)

* *

( )

hom

G

het

S θ G

∆ = ∆

Fig. 4.8 The excess free energy of solid clusters for homogeneous and heterogeneous nucleation. Note r* is independent of the nucleation site.

) 3 (

* 16

* 2 ₂

3 θ

πγ

γ S

G G G and

r

V SL V

SL ⋅

= ∆

∆ ∆

=

16

(61)

θ

V

A

V

B

Barrier of Heterogeneous Nucleation

4 ) cos

cos 3

2 ( 3

) 16 3 (

* 16

3 2

3

θ πγ θ θ

πγ − +

∆ ⋅

=

∆ ⋅

=

∆

V SL V

SL

S G G G

θ θ

 − + 

∆ = ∆  

 

3

*

2 3 cos cos

4

*

sub homo

G G

2 3 cos cos

3

4 ( )

A

A B

V S

V V

θ θ θ

− +

= =

+

How about the nucleation at the crevice or at the edge?

* *

( )

hom

G

het

S θ G

∆ = ∆

17

(62)

* homo

3 4 ∆G

homo^*

1 2 ∆G 1

_homo^*

4 ∆G

Nucleation Barrier at the crevice

contact angle = 90 groove angle = 60 What would be the shape of nucleus and the nucleation barrier for the following conditions?

* homo

1 6 ∆G

18

(63)

How do we treat the non-spherical shape?

 

∆ = ∆   +  

* * A

sub homo

A B

G G V

Effect of good and bad wetting on substrate

19

(64)

Although nucleation during solidification usually requires some undercooling, melting invariably occurs at the equilibrium melting temperature even at relatively high rates of heating.

Because, melting can apparently, start at crystal surfaces without appreciable superheating.

Why?

SV LV

SL

γ γ

γ + <

In general, wetting angle = 0 No superheating required!

3.7 The Nucleation of Melting

(commonly)

In the case of gold,

γ

SL

γ

LV

γ

SV

20

(65)

Liquid Undercooled Liquid Solid

<Thermodynamic>

Solidification:

• Interfacial energy ΔT_N

Melting:

• Interfacial energy

SV LV

SL

γ γ

γ + <

No superheating required!

No ΔT_N T_m

vapor

Melting and Crystallization are Thermodynamic Transitions

21

(66)

The Effect of ΔT on ∆G*

het

& ∆G*

hom

?

Fig. 4.9 (a) Variation of ∆G* with undercooling (∆T) for homogeneous and heterogeneous nucleation.

(b) The corresponding nucleation rates assuming the same critical value of ∆G*

-3 1 hom

1 cm

N ≈ s

⁻

Plot ∆G*het & ∆G* hom vs ΔT and N vs ΔT.

* ( ) ( )

3 3 2

SL SL m

2 2 2

V V

16 16 T 1

G 3 G 3 L T

πγ ^ πγ ^

∆ = ∆ =   ∆

) 3 (

* 16 ₂

3 θ

πγ S

G G and

V SL ⋅

= ∆

∆

n₁ atoms in contact with the mold wall

) exp(

* 1

*

kT n G

n ₌ ₋ ^∆

^het

) exp(

* 1

1 kT

C G f

N_het = − ^∆ ^het

22

(67)

입자 성장은 장거리 원자 확산에 의함

성장속도 G의 온도의존성은 확산계수 경우와 동일

.

23

(68)

5.4 Overall Transformation Kinetics – TTT Diagram

The fraction of Transformation as a function of Time and Temperature

Plot the fraction of

transformation (1%, 99%) in T-log t coordinate.

→ f (t,T)

Plot f vs log t.

- isothermal transformation

- f ~ volume fraction of β at any time; 0~1

Fig. 5.23 The percentage transformation versus time for different transformation temperatures.

If isothermal transformation,

24

(69)

Transformation Kinetics

 Avrami proposed that for a three-dimensional nucleation and growth process kinetic law

( ) ^kt

ⁿ

f = 1 − exp −

specimen of

Volume

phase new

of Volume

f : volume fraction transformed

=

 Assumption :

√ reaction produces by nucleation and growth

√ nucleation occurs randomly throughout specimen

√ reaction product grows rapidly until impingement

Johnson-Mehl-Avrami equation

25

(70)

Constant Nucleation Rate Conditions



Nucleation rate ( I ) is constant.



Growth rate (v) is constant.



No compositional change

f

τ t δτ

t-τ

f(t)

specimen of

Volume

during formed

nuclei of

number t

at time measured

during

nucleated particle

one of

Vol. 



 



× 

 

 





= d τ d τ

df

_e

( )

[ ] ( )

0

0 3

3 4

V

d IV t

v df

_e

τ τ

π − ×

=

( )

[ ]

∫ ^⋅ ⁻

=

^t ³

3 ) 4

(

o

e

t I v t d

f π τ τ

( )

³ ⁴

0 3 4

3 1 4

1 3

4 v t Iv t

I

t

π τ

π =

 

  − −

⋅

=

- do not consider impingement

& repeated nucleation - only true for f ≪ 1

As time passes the β cells will eventually impinge on one another and the rate of transformation will decrease again.

(71)

Constant Nucleation Rate Conditions



) ( exp

1 )

( t f t Iv t

f

_e

π

Johnson-Mehl-Avrami Equation

f

t 1

t

4

∝

before

impingement

1-exp(z)~Z (z ≪1 )

( ) ^kt

ⁿ

f = 1 − exp −

k: _T _sensitive f(I, v)

n: 1 ~ 4 (depend on nucleation mechanism) Growth controlled. Nucleation-controlled.

i.e. 50% transform

Exp (-0.7) = 0.5

kt

₀ⁿ_.₅

= 0 . 7

_n

t

₀_.₅

= k 0

₁

.

_/

7

₀_.₅ ₁

⁰

_/₄

^. ⁹

₃_/₄

v t = N

Rapid transformations are associated with (large values of k), or (rapid nucleation and growth rates)

* Short time:

t→∞, f →1

* Long time:

If no change of nucleation mechanism during phase transformation, n is not related to T.

(72)

Rate of Phase Transformation

Avrami rate equation → y = 1- exp (-kt

ⁿ

) – k & n fit for specific sample

All out of material - done

log t

Fraction transformed, y

Fixed T

fraction

transformed

time 0.5

By convention rate = 1 / t

_0.5

Adapted from Fig. 10.10, Callister 7e.

maximum rate reached – now amount unconverted decreases so rate slows t_0.5

rate increases as surface area increases

& nuclei grow

28

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Rate of Phase Transformations

• In general, rate increases as T ↑

r = 1/t _0.5 = A e ^-Q/RT

– R = gas constant – T = temperature (K)

– A = preexponential factor – Q = activation energy

Arrhenius expression

• r often small: equilibrium not possible!

Adapted from Fig.

10.11, Callister 7e.

(Fig. 10.11 adapted from B.F. Decker and D. Harker,

"Recrystallization in Rolled Copper", Trans AIME, 188, 1950, p.

888.)

135°C 119°C 113°C 102°C 88°C 43°C

1 10 10² 10⁴

29

(74)

Time–Temperature–Transformation Curves (TTT)



How much time does it take at any one temperature for a given fraction of the liquid to transform

(nucleate and grow) into a crystal?



f(t,T) ~πI(T)µ(T)

³

t

⁴

/3

where f is the fractional volume of crystals formed, typically taken to be 10

^-6

, a barely observable crystal volume.







 ∆−











 



 





 ∆



 



 ∆

= RT

E T

T RT

n H

I ^cryst ^m exp ^D

81 exp 16

π 2

ν 









 



 



 

 



 ∆



 



−  ∆



 



=

m m

T T RT

H T

a N

T fRT 1 exp

) ( ) 3

( ₂

η µ π

Nucleation rates Growth rates

30

(75)

Nucleation and Growth Rates

Nulceation and Growth for Silica

0.E+00 2.E+07 4.E+07 6.E+07 8.E+07 1.E+08 1.E+08 1.E+08

1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100

Temperature (K)

Nucleation Rate (sec-1 )

0 5E-26 1E-25 1.5E-25 2E-25 2.5E-25

Growth Rate (m-sec-1 )

Nucleation rate (sec-1) Growth rate (m/sec)

31

(76)

Time Transformation Curves for Silica

T-T-T Curve for Silica

200 400 600 800 1000 1200 1400 1600 1800 2000

1 1E+13 1E+26 1E+39 1E+52 1E+65 1E+78

Time (sec)

T em p er at u r e ( K )

32

(77)

33

* Time-Temperature-Transformation diagrams

TTT diagrams

33

(78)

34

* Continuous Cooling Transformation diagrams

CCT diagrams

34