Dislocation configurations in AuCu3 and AuCu type superlattices

Dislocation configurations in AuCu3 and AuCu type superlattices

DISLOCATION CONFIGURATIONS IN A&u, M. J. MARCINKOWSKIt, AND N. BROWNS AuCu and TYPE SUPERLATTICES* R. M. FISHER? Superlattice dislocations ...

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DISLOCATION

CONFIGURATIONS

IN A&u,

M. J. MARCINKOWSKIt,

AND

N. BROWNS

AuCu

and

TYPE

SUPERLATTICES*

R. M. FISHER?

Superlattice dislocations have been observed for the first time by transmission electron microscopy These consist of two pairs of partial dislocations held techniques carried out with thin films of AuCu,. The separation between the pairs is measured to be about together by an antiphase domain boundary. 130 A. A theoretical calculation has also been made of the expected spacing which involves the stacking fault energy, antiphase domain boundary energy and the elastic interaction energies between the The theoretical results are in good individual dislocations that constitute the superlattice dislocation. agreement with those observed experimentally. Further theoretical considerations of the AuCu type structure lead to two additional dislocation configurations characterized by the direction of their Burgers vectors with respect to the ordered lattice. This difference in the dislocation configurations between AuCu, and AuCu arises because the latter is a less symmetrical lattice. CONFIGURATION

DE

DISLOCATION DANS DES AuCu, et AuCu

SURSTRUCTURES

DU

TYP.E

Les auteurs observent pour la premiere fois par des techniques de transmission d’electrons sur des Ces super-dislocations sent constitue es de deux pellicules minces de AuCu, des super-dislocations. paires de dislocations partielles reunies par une frontier-e de domaine antiphase. La distance entre les paires mesure environ 13OA. Les auteurs calculent Bgalement theoriquement la distance. Dans ce calcul interviennent l’energie des fautes d’empilement, l’energie des frontieres des domaines antiphase et les energies d’interaction Blastique Les resultats theoriques de calcul entre les dislocations individuelles qui constituent la super-dislocation. sont en bon accord avec les valeurs trouvees experimentalement. Des considerations theoriques supplementaires sur la structure du type AuCu conduisent B deux configurations de dislocations additionnelles caracterisees par la direction de leurs vecteurs de Biirgers par rapport au reseau ordonne. Cette difference dans les configurations de dislocations entre AuCu, et AuCu provient de ce que ce dernier a un reseau moms symetrique. VERSETZUNGSANORDNUNGEN

IN

tfBERSTRUKTUREN

VOM

TYP

.hcu,

UND

AU&

Zum ersten Ma1 wurden mit elektronenmikroskopischen Durchstrahlungsmethoden in diinnen Filmen aus AuCu, ifberversetzungen beobachtet. Diese bestehen aus zwei Paaren van Halbversetzungen, die durch eine Antiphasen-Bereichsgrenze zusammengehalten wurden. Der Abstand zwischen den beiden Paaren wurde zu etwa 130 A gemessen. Eine theoretische Rechnung iiber den zu erwartenden Abstand wurde durchgefiihrt, in welche die Stapelfehlerenergie und die Antiphasen-Grenzflachenenergie eingehen sowie die elastischen Wechsel. Die welche die Uberversetzung bilden. wirkungsenergien zwischen den einzelnen Versetzungen, theoretischen Ergebnisse stimmen mit den experimentellen Beobachtungen gut uberein. Weitere theoretische Betrachtungen der Struktur vom Typ AuCu fiihren zu zwei zusatzlichen Versetzungsanordnungen, die durch die Richtung ihrer Burgersvektoren beziiglich dem geordneten Gitter charakterisiert sind. Dieser Unterschied in den Versetzungsanordnungen zwischen AuCu, und AuCu tritt auf, weil das letztere Gitter weniger symmetrisch ist.

INTRODUCTION

This paper is concerned

location

with the configuration

of

dislocations in the f.c.c. type of superlattice, e.g. Au&,. The original analysis of this type was treated theoretically superlattice, an ordered

by Brown

and Herman(l)

which consists

joined by an antiphase superlattice

dislocation

of two ordinary

dislocations

domain boundary. is similar

to

an

Thus, the extended

dislocation, which consists of two partial dislocations joined by a stacking fault. The superlattice disloca-

for the b.c.c.

e.g. CuZn. The perfect dislocation in lattice is the so-called superlattice dis-

tion in a f.c.c. lattice is complicated by the fact that it consists of a pair of extended dislocations connected

* Certain portions of this paper are based on a thesis by M. J. Marcinkowski presented to the Faculty of the School of Metallurgical Engineering, University of Pennsylvania. in partial fulfillment of the Degree of Doctor of Philosophy. Received April 4, 1960. t Edgar C. Bain Laboratory for Fundamental Research, U.S. Steel Corporation, Monroeville, Pennsylvania. $ Department of Metallurgical Engineering, University of Pennsylvania, Philadelphia, Pennsylvania.

configuration depends on the elastic interaction among four partial dislocations, the energy of the stacking

by an antiphase

ACTA

METALLURGICA,

VOL.

9, FEBRUARY

1961

129

boundary,

and thus, its equilibrium

fault and the energy of the antiphase domain boundary. In treating the general case, the orientation of the dislocation line with respect to its Burgers vector is another important variable.

ACTA

130

We first make dislocation type

a theoretical

arrangements

alloys.

investigation

in the AuCu,

The results obtained

are compared

METALLURGICA,

and

from

with direct observakions

VOL.

of the

9,

(ill)

1961 SLIP PLANE

LIES

IN

PLANE

OF DRAWING

AuCu

the former

obtained

from

thin films of AuCu, using the method of transmission electron microscopy. basic not only for

The present investigation is the interpretation of plastic

behavior in ordered structures: the dislocation

contribution

but also in calculating

to residual resistivity.

The variation of the antiphase boundary (APB)

ewergy

with order (8) The calculation antiphase

begins

boundary

of long-range order, S. observations of the f.c.c. f.c.c.

lattice

cubic

consists

sublattices

with the variation

(APB)

energy

First, a few preliminary lattice are necessary. The

of four interpenetrating

corresponding

atoms per unit cell.

of the

with the degree

to each of the four

For the purpose

the rhombus

which connects

(Fig. 1). Thus I,,

four atomic

11A4,III,

and IV,

are lattice sites

which will be taken on the stationary II,,

III,

and IV,

sites from

and which lie in the same plane

are the lattice

plane, and I,, sites which

are

initially occpuied by atoms in the movable plane above A prior to slip. I,, II,, III, and IV, are not only the sites occupied by atoms in a plane twice removed from the A-plane in the f.c.c. lattice, but I,, II,, III, and IV, also represent the alternate atomic sites for atoms when the B-plane fault

by slipping

the immediate

has created

by an amount

problem

of disorder associated

a stacking

1/6a(ll2).

is to determine

Thus,

the amount

with a stacking fault.

Referring to Fig. 1, we will consider a [Oli] dislocation which consists of four partial dislocations in the following order: 1/6a![112], 1/6a[121], l/Sa[ll2] and 1/6a[121]. Only changes in energy produced by changes in nearest neighbors will be considered. When plane B is displaced by 1/6a[112],

the following

changes in nearest neighbors rhombus take place:

to the basic

~ _

Site

:f

I& IV,

~~~~~-~

TABLE 1

_

__-

relative

Change in nearest neighbors ___ (I, - 13) - (I, - 11,) (II, - II,) - (11, - IB) (III, - III,) - (III, - IV,) (IV, - IV,) - (IV, - III,)

+ 1 + + 1

+

The above table means, for example, that an atom at a stationary IA site gains a nearest neighbor from a I, site since I, + II, and loses a II, neighbor since II, + I,. Table 1 can be simplified by observing

JR

IC z_

UNIT RHOMBUS I&, THAT LIE

of accounting

for changes in nearest neighbors, it is useful to consider each of the sublattices

I I

simple

IS.~E,m0.Irc,.Ic,nC~m,,~, JUST ABOVE ----

CONNECTING SITES OF TYPE IA. ItA. IIIA AND IN THE PLANE OF THE DRAWING (PLANE A) :ATOM THE

BONDS CONNECTING SLIP PLANE

PLANE

OF THE

NEAREST

SITES

LYING

IN PLANE

E

DRAWING

NEIGHBOR

SITES

ACROSS

THE

FIG. 1. Variation in bond types r_wxoss slip plane, with respect to & unit rhombus due to slip displacements of the type 1/6a(112).

that physically

there are only two types of sites in the

AuCu, type of superlattice,

wrong sites and right sites.

Three of the four sublattices

are physically

equivalent

so that we can designate a I, site as a I site, and IIB, III, and IV,, sites as a II site. Thus, substituting these designations in Table 1, the net change in nearest (I -

neighbors

I) + (II -

The following produced

for

a 1/6a[ll2]

II) -- 2[1 -

displacement

is

II].

table gives the change

in bonding

by each of the four partial dislocations: TABLE 2

Displacement

n[Oll

1. 1/6~~[112] -3. 1/6n[112] 2. 1/6n[l21] l/B@1211 4.

As expected, dislocation

Net change in bonding

1

(I -

I) + (II - II) -

2(1 -

II)

1 -81 - I) - (II ~ II) + 2(1 - II) the superlattice

which exactly

dislocation

reproduces

is a perfect

the lattice and

consequently produces no disorder. Fig. 2 shows a schematic of the superlattice dislocation, a[Oli]. The disorder associated with the APB is uniform between partial dislocations numbers 1 and 4 because partials 2 and 3 produce zero net change in bonding as shown in Table 2. It turns out that Table 2 is invariant with respect to the choice

of (011)

type

of dislocation

and the

MARCINKOWSKI, NUMBER

BROWN

AND

FISHER:

OF DISLOCATION

DISLOCATIONS

131

IN SUPERLATTICES

Similarly ANBB = S2 and ANll,

= --2S2.

(4)

The change in bond energy per unit rhombus is AE oR = S2( V&

-t V,,

-

2V,,)

(5)

where, for example,

V,, is the bond energy for a (Au-Au) bond. In order to get E,,, the energy per unit area of an APB, it is necessary to divide equation (5) by four times the area of the unit rhombus.

where a is the lattice Fro. Y.

sequence does

not

a[,Oli] superlattice dislocation in A&u,.

of its partial dislocations. hold

for

the

AuCu

This invariance

type

of

superlattice

Using the quasi-chemical

Yang(s)

which

the energy of the APB,

change in the number of Cu-Cu, Au-Cu and Au-Au The degree of long-range

order, R, in the AuCu, superlattice is defined as follows:

E OR- -

=

L-1 =

=

L-1=-

a l/2 a (Ill) same form(l)

when

5’) N

=

(1)

[-I--3(1 -

I

8) N

16

Average number of Cu atoms on 11 sites B =11[

l-

where the total number of atoms = N.

displacement

aN

for a l/Ba[llZ]

the quasi-chemical

Referring calculate

Substituting

to Fig.

approximation

S/l6 N2

is the width

of the 1/2a[Oli]

makes an arbitrary

16

When A! = 1,

= S2.

objective

is to

dislocation

and r the

angle, 8, with its Burgers vector. by the interaction

between pairs of dislocations,

3(3 + 8) N

stacking fault energy. The elastic interaction dislocations is given by

by E,, energy

energies

and by E,,

the

between

parallel

v is Poisson’s

ratio, R

E=2$~~[ln$-ilforedges

displacement E=g[ln:-l]forscrews

is a constant on the order of the crystal dimensions and r is the separation. The following table of

3116 N2

in terms of S, AN,,

of Lif3) is

spacings rr and r, where r,

where G is the shear modulus,

N2

by

on a -1 lo- plane has the

2, the present

the equilibrium

K12 + Kl' _,KlM* (2) AA =~___ l/l6

(8)

width of the superlattice dislocation. The caloulation is made for the general case where the dislocation

Thus, the total change in the number of Au-Au

bonds per unit rhombus is

92

--.--. a2

rl and r are determined

all the A atoms are on I sites, and when S = 0, all the atoms are randomly distributed between I and II sites.

1.41 kT,

(7)

The equilibrium cov$guration of the dislocation in AuCu,

16

Average number of Cu atoms on I sites B

= 2.44 kT,

used.

3(1 -

II

of

a2

Average number of Au atoms on II sites A

of

that

0.83 kT, S2 E OR=-----

1 + 3s --N. 16

I

with

The energy of an APB of a b.c.c. lattice produced

Average number of Au atoms on I sites A

approximation

agreement

2V,,)

( VA‘1 t- VBB -

the

bonds need to be calculated.

is in good

of the basic f.c.c.

Peierls

because it does not have the same degree of symmetry as the AuCu, type. In order to calculate

parameter

lattice.

(3)

interaction dislocations

energies is set up for the four partial with a separate column for the respective

ACTA

132

edge and screw interactions t,he interaction number

METALLURGICA,

and omitting

the part of

that does not depend on r or rl.

designating

each partial

The

is shown in Fig. 2 Screw interaction

in “*yt;Ifizz;

.

I co9 0 cm

l-2 1-3 1-4 2-3 2-4 3-4

(0 co92 e In (r co.! 0 cos (8 co* 0 cm (0

J

i

inuniteof[-_]

n/3) In rl VI) n/3) In r n/3) In (r - 29.1) cd (0 + */3 In (r - ?.I) COBB co9 (B + Tr/3)In 9.1

+ + +

where 0 is also defined. The total part of the energy which depends on rr and r is given by

e cos (e +

E total = 2 cos

[

+ +

sin

(

e

sin

1

n/3) __ 1-V

(e t

n/3)

VOL. I

so -

+

sin2

(e +

e

sin

(e +

47rEF rr -___-___. Gb2

Y

7~/3) In (rI

-

70

-

60

-

50

-

40

-

30

-

20

-

-10

-

-20

-

-30

-

-60

APPLY WHERE

I/

1

I



’ 200

’ 220

’ 240

TO 6 = 0

’ 40

’ 60

’ 60

’ 100

’ 120

’ 140

’ 160

(IN

Sri)]

(9) may be written in the form

E total = .w)

In rl + f2m

ln (r -- rA

has been assumed

=A(@

ln 5 +- rf2(e) + 2fs(e)] In (T -- ri)

-__ (2EF + E&277 Gb2

is the

only logical one that can be made at this time. from the equations

2rJl

(2EF + EofiP7 rl E,R 24r - 5) 662 __~ - ~ Gb2

Since no quantum mechanical between E, and E,,. calculations have been made for stacking fault energy assumption

’ 260

FIQ. 3. Graphical analysis of the equilibrium arrengement of dislocations in an A&u, type alloy over a wide range of Ep and EOR.

(9)

Gb2

’ 160

CM1

+ f3u3 In r + In (r -

r

or the ordering energy, the above

’ 20

Equation

1

It is to be noted that no interaction

r, and r are obtained

II

II

r X 106

ri)

57/3) [ln r + In (r -

27rE,,

I

ln rl

cos e c~s (e + n/3) I+-;

+ sin

I

RELATIONSHIPS DISLOCATION

60

0

e+

1961

1

[toss e + coss (e + n/3)] i_I’

+ sin2

9,

+

f,(e) ln

r-r1

Since -L

(r -

E,,

rl

hr(r -

rJ

Gb2

r12

rl)2 -

(r - rd2

(12)

~ 1 1

I.

< 1 (Fig. 3), thenln

and the last term in equation (12) may be neglected. Thus, r1 and r may be obtained from

The

above

equations

cannot

be solved

exactly.

However, a graphical solution was obtained for 0 = 0 as shown in Fig. 3 for a wide range of E, and E,,. Noting that the ratio of rJr is small compared to 1, an analytical solution of equations (10) and (11) may be obtained which is exceedingly accurate for all values of 0 and for a wide range of likely values of the physical parameters.

Gb2 ___-__2 rcos e r1 = 277(2EE, + EoIz) i X in,

-I- sin

cos (e + e

sin

‘IT/3)]

(8 +

n/3)]

1

(15)

MARCINKOWSKI.

(T - TX)= z-g-

numerical

(16) show excellent cal solution

corresponding action

sin (0 + r/3)12

calculations agreement

represented

of equation

. (16)

(15) and

with the exact graphi-

by Fig. 3.

Furthermore,

as

8 decreases, r increases more rapidly than r,, so that the degree of approximation increases. The accuracy of the approximate

solutions

the distance between 3(r - 2r,) is essentially

DISLOCATIONS

IN SUPERLATTICES

means physically

that

partial dislocations 2 and independent of the fact that

energy

between

presented,

in

edge

larger elastic intercompared

to

screw

dislocations, which in turn enables r to vary between 78 and 124 A when S = 1. The variation in rl with 0 is somewhat

smaller

although

appreciable.

Fig.

4

shows further tha>t the effect of order is to decrease ri by a fa’ctor of about 4 from its value in the disordered alloy.

The variation of r with 5’ is not shown. Howvaries as X2, r increases very ever, because E,, rapidly with decreasing S. The AuCu supcrlctttice The calculation

the &z[OlI] dislocations are extended. A few numerical results will be

133

to the pure edge and screw dislocations.

This results from the somewhat

1

kv + [sin 0 +

x

FISHER:

AND

[COBI9+ cos (0 + 77/3)12 OR

Detailed

JJBOWN

introduces

of E,,

for the AuCu supertattice

some new features

because

AuCu is less

particu1a.r for the case of AuCu,, to show the size of the various quantities which have been calculated.

symmetrical than AuCu,. In the AuCu lattice the I_* and III, sites are physically equivalent and may be

For this alloy E,,

referred to as I sites;

K&ter(3),

was assumed lo-l6

s

75 X2 while from the data of

G = 4.7 x lo11 dyn/cm2 and v = 0.33.

cm2.

to be 40 ergs/cm2

Consider

E,

while b2 = 2.34 x

first the variation

of r and r1

also physically

whereas the II,

equivalent

If a table similar to Table 2 is constructed,

and

minima

at

8 = -30”

and

60”,

respectively,

Displacement a(1101

Xet change in bonding

~..______

1. I/B@111

~

0

3. lp@ll] 4. 1/6rc[121] -.....

j /

0

2. 1/6a[121]

the

2((1 -

Table

5 100

-

following :

superdislocation

gives

a [Oli]

______-______

x

85 -

I. 2. 3. 4.

PURE EDGE DlSLOCPTlON T

1/6a./llT2j 1/6a[Bt] 1/6al.112] 1/6a[l21]

~ I -2[(I





1

-40 -30 -20 -10



0









10 20 JO 40 B (IN DEGREES)



SO



60



70

the same results



-.-

as the

.~. ~ _~ --___1

Ij + (II -- II) --. 2(1 - II)]

OF

I) + (11 -II] - 2(1 -II)] I) + (II - II) -- 2(1 - II)] DISLOCATION

4

FIG. 4. Variation of spacing between dislocations in A&u, with orientation of Burgers vector.

gives

as

4

f

80

II)]

symmetrical

s 0

2(1 -

- I) + (II - II) -. 2(1 - II)]

2[(1 -2[(I -

NUMBER

PURE SCREW DWCCATION

2(1 - II)]

Net change in bonding 21 (I -

I

II) -

displacement

-

Displacement a[Oli]

go-

75-

However,

is uot

TABLE

95-

80 -

3.

I) + (II -

--2[(I - I) + (II - II) -

shown in Fig. 5. A a[Oli] displacement -

L

j

-__

s 105 0

-2

it, is found

3

TABLE

Thus, ilO-

are

that

with 0. This is shown in Fig. 4 for several important cases. It will be noted that the separations are periodic with period rr, and that they possess maxima

and IV,

and are now called II sites.

90

Fro. 5. tc[ilOJ dislocation ik Au&.

ACTA

134 NUMBER

VOL.

9,

1961

OF DISLOCATION

1

T

i

METALLURGICA,

L-rr,4

i

I+--ri-4

FIG. 6. a[01 l] dish&ion in A&u. No coupling between 1!2a[OlT] dislocations.

The configuration

of the dislocation

The quasi-chemical

is shown in Fig. 6.

approximation

of Li(j) for an A3

f.c.0. lattice is 7 (k/U

i- V BB -

ZV,,)

FIG. 7. Dislocation arrang~~n~Atsindisordered AL&U,.

= 2.74 kT,.

gold.

The energy of the APB is

cooled

3.16 kT, 6 E OR = -_______--. a2 The calculation

for the equilibrium

l/Za[Olf]

dislocations

configuration

dislocations

of the type a[Oli]

of

dislocations extended

would

of the

the

width

in the disordered

state.

for the equilibrium

nonsymmetrical

more difficult

a[illO]

than for AuCu,.

by

The width of these

be less than

dislocations

The calculation

and the

consist of partials connected

both a stacking fault and APB.

of the

configuration

dislocation A graphical

will require a three surface analysis.

is much solution

An analytical

solution is not apparent because it requires the simultaneous solution of three equations, and one cannot

be assured that a simplifying

from

of the specimens

500°C

(T,

degree of disorder.

the a[Oli] displacement is trivial because there is no APB between dislocations 2 and 3. Thus, there are no superlattice

A portion

approximation

was then rapidly

= 390°C)

to insure a high

The remaining

specimens

were

then slowly cooled from 400 down to 180°C at a rate of 2.3’C/hr. Subsequent examination of t.he slowly cooled alloys by X-rays since the antiphase

showed S to be about 1, and

domain

size seas about

500 A,

nearly perfect long-range order exists. The specimens were then electropolished into thin sections with a chromic-acetic acid electrolyte using a procedure described by Fisher and Szirmae(a) which is a modificat.ion of that first proposed by Bollmann( These specimens were next examined by transmission electron microscopy’@ operating

using a Siemens Model 1 Elmiskop

with a double condenser at 100 kV.

Figure 7 shows an array of dislocations those observed

in the disordered

alloys.

typical

of

All of them

appear as single dislocations, however, they are probably dissociated into partials separated by a

will be discovered. The detailed calculation for the non-symmetrical case will be part of another paper,

distance rr. This distance, however, even in the most

however it appears qualitatively

38 A, or just below the resolution

that rr will be much

less than r2 and r. Direct observation

qf dislocatioxs

in both diswdered and

ordered AuCu, Copper of 99.9 per cent pnrity and an equal weight of 99.98 per cent pure gold were melted under vacuum in a zirconia crucible. The resulting ingot was rolled into &rips about 0.0015 in. thick and annealed for 2 hr at 900°C. The mean grain size resulting from this treatment was 0.1 mm and subsequent chemical analysis showed no detectable loss of either copper or gold, i.e. the final specimen contained 24.8 at.76

favorable

case (0 = 30”, S = 0, Fig. 4) is only about obtained

with the

present techniques. It will be further noted Fig. 7 represents a region within the specimen, has appa,rently undergone plastic deformation. of the dislocations

a considerable

The irregular such as those

that that

amount

of

shapes of many at point A are

probably explained by elastic interactions between dislocations on closely spaced slip planes. Jogs such as those at U are probably produced by combination with a dislocation in a different slip system as discussed by Whelan(g). Fig. 8 shows a slip band containing a large number of dislocations in a fully ordered specimen.

The norms1 to the surface is ]134]

MAHCINKOWKKI,

BROWX

AND

FISHER:

DISLOCATIONS

IN

SCPERLATTICES

135

TRACE OF SLIP PLANE

(UPPER SIDE OF FOIL)

PROJECTION OF DISLOCATION PAIR IN SLIP PLANE \\

t

FIG. 8.

Pile-up

of

superlatt,ice dislocations ordered AuCu,.

r, is too small to be resolved, and as Fig. 4 shows, r1 in the ordered alloy is expected to be nearly half that the

disordered

alloy.

between the dislocation

The

observecl

pairs is essentially

distance a measure

of r. A number of important features are to be not.ed in Fig. 8. First, the dislocations are quite irregular in shape,

while the This may

uniform. to their motion planes.

spacing be the

between them is not result of interference

by other dislocations

A few such dislocations

on different slip

which lie above

TRACE

DISLOCATION

bF

SLlP

PLANE

(UNDER

SIDE OF FOIL,

PAIR

FIG. 9. Geometrical relations needed to find true perpendicular distance y between coupled dislocation pairs in thin foils.

in fully

while the slip plane is (111). It can be seen that the dislocations are paired in agreement with the theory.

in

\

/

I/

COUPLED

+a+

the

r to compare with theory, the geometrical tion becomes quite important.

interpreta-

The three dimensional

analysis of the dislocation pairs giving rise to what is observed in Fig. 8 is shown in Fig. 9. From the angles and lengths

shown

in this figure,

given by the following

T is found

to be

relationship

r = a cos [tan-l (tan p cos y)]. Both a and /3 can be measured from the figure, while y can be found by a selected area diffraction

of this

same area. From Fig. 8, r is found to lie in most cases

main plane of slip are indicated

at point A in Fig. 8.

between

Most likely all the dislocations

were produced

since both y and 6 shown in Fig. 9 a.re known,

the ordering

transformation,

either

after

by handling

or

thickness

the values

of 90 and 135 8.

of the film can be measured,

In addition, the

and in its

by heating of the electron beam. Some of the irregularity in the spacing of the paired dislocations

present case is found to be 1000 8. Figure 10 shows a second array of coupled disloca-

may

tions in the ordered alloy lying in parallel slip planes.

be associated

interesting

feature

w-ith variations

in 8.

Another

of Fig. 8 is that the dislocations

In this case, the dislocations

appear to be piled up against some barrier to the right.

in appearance,

The stress field from the dislocations

little or no interference

at the heat of

the pile-up is sufficient to bring these dislocations such

close

identity

proximity

with

as pairs is virtually

that the antiphase boundaries pairs do not show contrast

one

another

eliminated.

that

indicating

are much more uniform

that they have moved with from neighboring

dislocations

to

their

The reasons

between the dislocation is not yet completely

understood. However, it is not expected that conditions for disloca,tion resolution will in general be the same as those for antiphase boundary resolution. The next

objective

is to compare

the measured

values of r with the theoretical results. At this point, however, it must be remembered that Pig. 8 represents a projection of a three-dimensional dislocation network onto a plane surface, and what appear to be perpendicular distances between dislocation pairs are not the true perpendicular distances. Because of the desirability of obtaining an accurate measurement of

FIG. 10. Superlattice dislocations of nearly equilibrium spacing in fully ordered Ad&,.

ACTA

136

METALLURGIC-A,

VOL.

FIG.

therefore

should

analysis.

be better

for

comparing

the

The value of r, which is nearly

constant between all of the dislocations, is found to be 130 d and is in good agreement with the calculated results.

Since 8 is not known,

it is not possible

make a more critical comparison theoretical

to

with theory, although

the measured T values agree surprisingly

have on the superlattice

over which the separated above again

is apparently

SUMMARY

have

shown

AND

both

theoretically

highly irregular due to interaction all of the dislocations

are

with one another. remain paired with

spacing.

It is to be concluded

dislocations

which are held togethether

on the elastic

which

high

in fully

and

experi-

ordered

AuCu,

The superdislocations

by an antiphase boundary.

The spacing between the individual partial dislocations

dislocations,

the superlattice repulsive

forces

dislocation between

the stacking fault energy, and the anti-

phase boundary energy. By using isotropic elastic dislocation theory and the quasi-chemical approximation for the ordering energy, the separations

dislocations

the

travel

in pairs.

A

second

interesting feature of Fig. 11 is the band running from left to right, near the center of the figure. Possibly,

the alternate

from an antiphase

light and dark contours

boundary

contrast

which

arise should

depends

the partial

from these results that even after large deformations, in AuCu,

stress

CONCLUSION

are present as superlattice dislocations. dislocation consists of a pair of partial

that constitute

constant

local

dislocations,

that

less random

a surprisingly

due to some

concentration.

We

of dislocations

line at B

superlattice dislocation has been its equilibrium spacing r, which

mentally

one of the foils

in agree-

Fig. 12 is the portion of the long dislocation

treated in this manner. It will be noted that the large complex deformation has resulted in a more or

However,

undissociated

Another interesting feature of

what effect cold work might

was heavily deformed by repeated bending. Fig. 11 shows an array of dislocations observed in a specimen

distribution

are virtually

ment with the theory.

well with the

results shown in Fig. 4.

In order to determine

Interference to the motion of superlattice dislocations in fully ordered AuCu,.

12.

the dislocations

that was subsequently cold worked.

theoretical

1961

near the leading edge. As the pinning points are approached, however, this separation vanishes and

FIG. 11. Super-latticedislocations in fully ordered Au&,

and

9,

four

partial

dislocations

that

between

constitute

the

superlattice dislocation has been calculated for dislocation possessing an arbitrary Burgers vector. An alloy

of composition

bulk, has been electropolished

AuCu,,

fully

ordered

to films about

a in

1000 A

be similar to the contrast observed for stacking faults.(lO) The contrast appears most pronounced in

thick. Examining these by transmission microscopy, we have observed superlattice

the vicinity

tions for the first time. The separation between the two pairs of partial dislocations was measured to be about 130 A and is in good agreement with the

of the dark extinction

contours.

Finally, Fig. 12 shows some very interest’ing features of moving superlattice dislocations. A segment of the large dislocation line at A has been pinned at two points. Nevertheless, this segment is able to expand outward between the pinning points as a superdislocation with a well defined separation

electron disloca-

spacing calculated theoretically. The energy of the antiphase boundary discussed above has been calculated for one which has been produced

by slip and whose structure is not changed

MARCINKOWSKI,

by a subsequent

BROWN

diffusion of atoms.

FISHER:

AND

The structure

DISLOCATIONS

of

an antiphase boundary which exists during thermal equilibrium is different from a boundary produced only by slip in that the equilibrium ary has a thickness varies continuously.

antiphase bound-

over which the degree of order The calculation for the variation

in thickness of an antiphase

boundary

ture has been made by Brown’li)

with tempera-

for CuZn.

the free energy of the equilibrium

In general

antiphase boundary

will be less than that of the slip produced boundary

antiphase

and the difference will be greater the closer

the temperature Consideration

small resistance in

Ardley(12).

configura-

increases

in AuCu type alloys, the superlattice

disloca-

tion may consist of an asymmetric array of four bound partial dislocations or a pair of partial dislocations similar to that in the disordered alloy. The difference AuCu,

in the dislocation

arrangements

The configuration

of the dislocations

could

have

an important bearing on the plastic behavior of the crystal. For example, since there are two distinct types

of superlattice

dislocations

in AuCu and only

one type in AuCu,, it is expected that ordered AuCu would plastically deform in a more anisotropic fashion than ordered AuCu,. No experiments been made to test this conclusion. From the result,s described little doubt

that dislocations

here, there seems to be in fully ordered AU&I,

travel through the lattice as superlattice When

the

antiphase

500 A) these dislocations

have

boundaries

are

dislocations. large

(about

should move with negligibly

however,

that

rapidly.

of the

Thus, at low degrees of order, it independently

as moving

In this case, it would

follow

that

This would

type

of one another. these imperfect

must do work against the ordering forces,

since they will leave behind an antiphase mean

degrees higher

that the alloys of

yield

order

should

points,

than

boundary.

possessing be

inter-

stronger,

either

i.e.

the fully

ordered or the completely disordered alloys. These very interesting speculations are being presently investigated

in both AuCu, and Ni,Mn. ACKNOWLEDGMENT

We are indebted carrying

in the latter.

be recalled,

This is

results

to think of the $a(llO)

between

and AuCu is a result of the smaller degree of

symmetry

forces.

experimental

dislocations

possess

location

It will

the

may be more correct

ing on the Burgers

dis-

with

decreases this energy decreases very rapidly and the separation between the component dislocations also

mediate

of the superlattice

137

energy of the antiphase boundary bounded by the superlattice dislocation varies as S2 so that as S

tions in the AuCu type ordered alloys leads to two additional types of dislocation arrangements. Dependvector

SUPERLATTICES

due to the ordering

agreement

dislocations

is to To. of the possible dislocation

IN

to A. Szirmae for his assistance in

out the experimental

portion

of this work

and to D. S. Miller for many helpful discussions concerning the interpretation of the results. REFERENCES 1. 2. 3. 4. 5.

N.BRowN~~~M.HERMAN,TT~~~.A~~~. Imt.

Engrs. 206, 1353 (1956). C. N. YANG, J. Chevn. Phys. 13,66 (1945). Y. Y. LI, Phys. Rev. 76, 972 (1949). W. KBSTER, 2. Met&k. 32,145 (1940). Y. Y. LI, J. Chem. Phys. 17, 447 (1949).

Min. (Metoll.)

6. R. M. FISHER and A. SZIRMAE,Syllzposium on Electron Metallography, ASTM STP 262, 103 (1959). 7. W. BOLLMANN, Phys. Rev. 103,1588 (1956). 8. P. B. HIRSCH,MetaZZurg. Rev. 4, 101 (1959). 9. M. J. WHELAN, PTOC. Roy. Sot. 249, 114 (1959).

10. M. J. WHELAN, J. Inst. Met. 87, 392 (195!3). 11. N. BROW, Phil. Msg. 4, 693 (1959). 12. G. W. ARDLEY, Acta Met. 3, 525 (1955).