CROSS
SLIP,
ANTIPHASE IN
DEFECTS ORDERED
AND
WORK
HARDENING
Cu,Au*
B. H. KEAR? Superlattice dislocation and antiphase boundary structures have been examined in thin foils of deformed ordered Cu,Au. The observations point to the important role of forest intersection jogs in controlling the slip distance and work hardening of the ordered alloy. Jogs are considered to contribute to the frictional component of the flow stress through the generation of point defects and antiphase defects, and to the internal stress component through the trapping of glide dislocations by the jog mechanisms of dipole formation and ‘intermediate’ cross slip. Temperature dependent work hardening in the ordered alloy is discussed in terms of several different models. GLISSEMENT-CROISE, DEFAUTS D’ANTIPHASE DEFORMATION DANS LE COMPOSE
ET DURCISSEMENT ORDONNE Cu,Au
DE
Des structures de dislocations de sur-reseau et de frontieres d’antiphase ont 6th examinees dans des lames minces du compose ordonne Cu,Au deform& Les observations indiquent le role important joue par la foret d’intersections de crans dans le controle de la distance de glissement et du durcissement de deformation de l’alliage ordonne. Les crans sont consider& comme contribuant it la composante de friction de la limite Blastique par l’intermediaire de la production de defauts ponctuels et de defauts d’antiphase, et a la composante de tension interne grace au piegeage de dislocations en glissement par les mecanismes de m-an, de formation de dipole et de glissement croise “intermediaire”. QUERGLEITUNG,
ANTI-PHASEN-DEFEKTE UND GEORDNETEM Cu,Au
VERFESTIGUNG
IS
Die Anordnung der Uberstrukturversetzungen und die Struktur der Anti-Phasen-Grenzflachen sind in dunnen Folien einer verformten geordneten Cu,Au-Leigierung untersucht worden. Die Beobachtungen zeigen, da6 die durch Waldversetzungen erzeugten Durchschneidungssprige den Laufweg und die Verfestigung der geordneten Legierung entscheidend beeinflussen. Es wird angenommen, da6 die Spriinge infolge der Erzeugung von Punktfehlern und Anti-Phasen-Defekten zur Reibungskomponente der Fliel3spannung beitragen und infolge des Einfangens gleitender Versetzungen durch die Sprungmechanismen der Dipolbildung und der intermediaren Quergleitung die innere Spannungskomponente der FlieDspannung beeinflussen.
1. INTRODUCTION
In a previous
paper,(l)
account
for differences
crystals
due to ordering
on dislocation
was made to
in work hardening by correlating
configurations
with stress/strain
As in the earlier work, the present study has been
an attempt
and lattice
in Cu,Au
between motion
accumulating
as a result
of
work
in
to be associated
slip.
with the trapping The present
with
of high purity
was
PROCEDURE
stoichiometric
composition
CusAu
copper
and gold under vacuum
in a
graphite mould. Using this material a single crystal with dimensions $ in. x 4 in. x 6 in. was grown from the melt by the Bridgman homogenized annealing
method.
The crystal was
by heating at 900°C for several hours,
and fully ordered (S -
* Received April 15, 1965; revised November 18, 1965. t Advanced Materials Research and Development Laboratory, Pratt & Whitney Aircraft Plant N, North Haven, Connecticut. 1966
occurs at a critical The strongest work
in material with maximum
EXPERIMENTAL
An alloy
mine its role in work hardening.
VOL. 14, MAY
stress and
on the domain
was prepared by melting together the required amounts
cross
undertaken primarily to provide more evidence for intermediate cross slip in the superlattice, and to deter-
ACTA METALLURGICA,
of about 40 A.
is experienced
2.
of screw segments investigation
the yield
sensitively
order and largest domain size.
On the other
loops in intermediate
that
depend
A yield stress maximum
hardening
dislocation
in the ordered alloy appeared
dislocation
slip configurations.
of
established
hardening
size.(2-6)
between
and the grown-in domain structure.
domain diameter
in the primary
blocking
by the onset of conjugate
hand. work hardening of expanding
It has been
It was
alloy was due to elastic interactions
dislocations
slip planes
glide dislocations
crystals
data.
shown that the major part of the work hardening the disordered
so as to minimize effects due to interactions
observations
in the deformed rotation
restricted to material with relatively large domain size,
1 .O; domain size -0.1
at 350°C for several
hours,
,M) by
followed
by
slow cooling at intervals of a few degrees every 24 hr 659
ACTA
660
in the
range
350”-150°C.
sample of the annealed
Chemical
analysis
of a
crystal gave 25.1 at. y0 gold.
Spectrographic
analysis
purities
aluminum
silver,
METALLURGICA,
gave
as the
principal
and iron,
totaling
im0.015
wt. %. machine.
crystal was pulled in an Instron
The testing procedure
steps, as follows:
involved
three main
(i) the entire 6 in. length of crystal
was strained to marker 1 on the stress/strain 1, and, after unloading.
curve,
a 2 in. length
sample
14,
1966
operation several different operating reflections. it was possible dislocations The
to determine of each
samples
was
with
by
system.
back-
rotation
of the tensile axis,
1. 2 and 3 on the stress/strain
curve, was found to be in agreement lated rotation,
differently the
The data is given in the inset
of Fig. 1. The observed corresponding
contrast method.@) of the three
determined
reflection Laue method.
Thus, vector of
the Burgers
by the diffraction
orientation
strained
The electropolished
Fig.
VOL.
with the calcu-
assuming slip in the predicted
primary
In agreement with the X-ray lattice rotation
data, optical examination
of slip lines in specimens 1,
2 and 3 showed evidence for slip only in the predicted primary system.
The slip lines were long and straight
in the crystal face parallel to the Burgers vector, and they were short, diffuse and somewhat
wavy
in the
crystal face at right angles to the first, Figs. 2(a) and (b).
These particular micrographs
after unloading stress/strain
SHEAR
are for specimen 3,
and repolishing
at stage S on the
curve.
STRAIN-PERCENT
Fm. 1. Interrupted stress/strain curve and rotation of the tensile axis for a crystal of ordered Cu,Au.
was cut
from
the
crystal
using
(ii) the crystal was remounted an additional another
strain
jeweler’s
a
saw;
in the grips and given
to marker
2, and,
as before,
2 in. sample was cut from the crystal ; and
(iii) the remainder marker 3.
of the crystal
was strained
In each case, on reloading,
mation recommenced
in a discontinuous
little or no work hardening Some characteristics
to
plastic deformanner, with
for a few percent strain.
of this reloading effect have been
reported elsewhere.(7) Each after
sample
suitably
reflection
was mounted orienting
Laue method,
the
in a goniometer, crystal
by
and
the
back
$ in. thick sections were cut
parallel to the slip plane, and also perpendicular the slip plane, parallel to the Burgers vector. cutting
operations
Thin foils suitable
microscopy
These
were carried out using a jeweler’s
saw, with the sample firmly supported block.
to
in a plastic
for transmission
electron
were prepared from these bulk samples by
a two-stage electropolishing procedure.(l) The foils were mounted directly in a modified specimen holder for the Philips
EM
100-B
electron
viewed at 100 kV operating potential. trast conditions holder.
degrees about
cases the available
3. DISCUSSION
OF
The most characteristic
feature
slip plane was the elongation the direction
loops in
with the loops
consisting of straight segments in the screw orientation and somewhat orientations, work.(l) primary
wavy segments in the edge, or mixed Fig.
4,
in
agreement
with
previous
In a few cases the Burgers vector of the dislocations was confirmed by the g*b = 0
and
criterion,
other cases the orientation
one axis) was sufficient to bring into
of dislocation
of the Burgers vector,
con(-&6
of the dislocation
structure in thin foils of sections taken parallel to the
Optimum rotation
RESULTS
3.1 General dislocation structure
microscope
were achieved by tilting the specimen
In most
(b)
(a)
FIG. 2. Surface slip markings at stage S on the stress/strain curve; (a) edge bands, and (b) screw bands. x 250
using the 131 reflection,
Fig. 3(a).
In all
of the primary slip vector
in the micrographs was deduced from the known orientation of the foil in the electron microscope. A careful examination
of all micrographs
showed no
KEAR:
WORK
HARDENING
IN
ORDERED
ti61
Cu,Au
( bl
(0)
FIG. 3. Stereographic projections of the two different orientation thin foils examined; (a) parallel to the primary slip plane, and (b) perpendicular to the primary slip plane, parallel to the slip vector.
evidence
for classical
dislocation
pile-up
tions.
On the other hand, numerous
found
of fairly
orientation
uniform
dislocation
arrays
of edge,
dislocation
arrays
are shown
half of Fig. 4(c) for specimen (b) for specimens for neighbouring they
1 and 2. of the
lap of neighbouring
in the upper
the dislocation
in the inset of Fig.
tilt of the foil.
dislocations
Frequent
in a family
of the bursts of slip that invariably in an interrupted
Here the stopping
of slip planes.
3.5.
This interpretation
such groups, associated defects,
with
see section
contribute
predominantly Evidence
ally in specimen words,
appeared mentioned 7
see section
by the fact that are generally
activity
localized
primary
secondary
slip in specimen
effect of additional cause
dislocation
dislocation
of primary
dislocations
Figure 6(a) shows a region of 3.
slip
associated
slip in the secondary tangling.
with
It can be seen that the Figure
structure in the vicinity
system is to
6(b)
shows
the
of a region of the
foil where limited activity had occurred in a secondary system.
The very
superlattice
complex
dislocations
structure
of individual
in this micrograph
is not
understood. dislocation
dipoles
in various
tations were found in all three specimens.
factor
crystal
have their origin in
mechanism,
Fig.
15.
on the other hand, are considered
result of elastic interactions dislocation
loops
and
much
Screw
to be the
between newly expanding
screw
segments
by slip
in localized 1; in
systems
in stage II.
As
accompanying
cross slip,
previously
7(a) shows, at A, a stage in the overlap
secondary
earlier, the lattice rotation
dipoles,
superjog
were
Figure
deforming
to increase with prestrain
Edge dipoles probably
familiar
dipoles
that would
in specimen 3, occasionof
Fig. 4(a). the
orientation
by intermediate
for flexural glide to
slip, generally
or near edge
orien-
In general,
pinned
2, and not at all in specimen the
stage II.
antiphase
induced
of fairly uniform arrays of
regions, was found frequently other
drag,
avalanches slip
of jogs and
in the array, i.e.
in one system.
for secondary
intensive
therefore, must have remained
with that
shorter than screw dipoles ; cf. dipoles at A and B in
is the tendency
in a constrained
throughout
in for
edge
Another
to the trapping
edge dislocations develop
3.4.
compared
slip distance
is
is supported
observable
secondary dislocations, small
of slip exclusively
The average
1.
frictional
or dislocation
was indicative
system.
Fig.
considered to be primarily the accumulation dislocation
the primary
for the dislocations
point defects on all the dislocations an enhanced
the deformation
Superlattice
characteristic
occur on reloading
deformation,(7)
mechanism
over-
in a group, as at A in
Such groups may be the configurations a crystal
features
in these arrays show that
same sign;
Fig. 5(b), shows activity
slip planes.
Similar contrast
has been exaggerated
5(a) by an appropriate
or mixed
3, and in Figs. 5(a) and
dislocations
are mostly
contrast
were
segments in excess of one sign,
usually lying in a family of neighbouring Typical
configura-
examples
two near edge orientation of somewhat
arbitrary
see section
3.3. of
segments to form a dipole
shape by the jog mechanism ;
here the jog pair in the superlattice dislocation is indicated by the arrow. In thin foils of sections taken perpendicular
to the slip plane, parallel to the slip
vector, the edge orientation dipoles are visible as two pairs of dots lying in neighbouring (111) slip planes, as at C in Fig. 9(b).
Figure 7(b) shows an unusual case
of what
to be the approach
appears
of two
edge
segments of the same loop just prior to the formation
ACTA
METALLURGICA,
VOL.
14,
19G6
(b)
Fxa. 4. Changing
ctisloration structure w&h increasing prestrain soctiorls token parallel to the primary slip plane.
(epccimcns
J-3) in
KEAR:
WORK
HARDENING
IS
ORDERED
663
Cu,Au
(b) FIG. 5. Uniform arrays of primary dislocations
in specimens
(b)
(a) FIG. 6. Dislocation
1 and 2.
structure in regions of localized activity
in serondary
systems.
ACTA
664
METALLURGICA,
VOL.
14,
1966
on the loss and rearrangement foils of deformed after electrolytic have concluded
(a)
aluminium
of dislocations
thinning.
Wilsdorf
that electrolytic
in thicker
foils the dislocation
observations
have
In very thin foils evidence
in the
dislocations surface
line
energy
of the in the
foil.
by rearrangement
of to
Such
rearrangements
of
the
of
foil involved
or so, an entirely
consistent
taken
were reasonably
it should be mentioned
the
contrast
of a dipole. contrast
In these and other cases the fact that the the
dislocations
they have opposite
signs-in
all change in contrast of the almost
edge orientation wide variations dipoles
2.
changes from light to dark in opposite senses
on crossing
outside
1 and
is clear particular
evidence
that
note the over-
on going from the inside to the closed
dipoles
loop in Fig.
7(b).
in all micrographs
in equilibrium
F and G in Fig.
widths,
4(b).
The
exhibit
e.g. compare
No calculations
have
difference
between
for superlattice
anomalous
single
phenomena
have
that
observing
dislocations,
line
Such
analyzed
by
The
dislocation
structures
parallel
to the Burgers
relatively
long
orientation,
vector,
dislocation
dipole.(34) occurrence
Anot’her effect’ worth not’ing is the frequent of weakly contrasting
to t’he primary lines probably
lines inclined at 60”
slip vector, as at C in Fig. 4(a). These represent some special form of dis-
location debris produced locations, similar to that
by dragging jogs in disdescribed by Hirsch and
Steedscg) for copper crystals. Several workers(i0-i2) have
observations
thin
in
mainly the
Figs. 8 and 9, as would be expected
the observed
structures
of
screw from
in thin foils of sections taken
parallel to the slip plane, Figs. 4 and 5. In most cases, the
Burgers
In Figs. dislocations
vector
of the
dislocations
8 and 9, the segments
interesting 8(a), mixed
9(a).
dislocation
orientation
The middle (arrow)
(111)
are resolved
as
they have undergone (111) slip planes. An
case of cross slip is indicated
see also Fig.
was readily
using the
of the superlattice
in the screw orientation
pairs, which must mean that cross slip out of their original
superlattice reported
in the
consisted
segments
Figs. 3(b) and 10.
the
and
to the slip plane,
reflection,
narrower
contrast
Wilkens
observed
foils of sections taken perpendicular
the
the
to
3.2 Evidence for cross slip
by the g-b = 0 criterion,
slip planes
line
Hornbogen.(13)
confirmed
of the
frequently double
as opposed
contrast.
been
small tilts of
reflection,
been made so far, but it seems likely that the smaller separation
repre-
of the bulk sample.
Finally
loops and dipoles in specimrns
from to the
was taken to be evidence
structures
the foil, for a given operating
FIG. 7. Dislocation
was obtained
parallel and perpendicular
the observed
made
as will be shown
picture of the dislocation
slip plane, which correlation sentative
and pos-
in excess of 2000 A
in the deformed material
both sections
production
dissociation
In thin foils with thickness
that
foil,
nearly perpendicular
defects by dislocation
structure
study.
slip out of the
sibly by dragging jogs on dislocations, later.
(b)
Similar
has been found for (i) loss
by cross
into orientations
dislocations antiphase
are considered
sample.
under the action of image forces. and (ii)
reduction the
bulk
2000 A;
been made in the present
of screw dislocations presumably
only if
less than
patterns
of the
density
arrangement
of the foil becomes
be representative
of deformed
in dislocation
and to changes in the dislocation
to
and Schmitz(12)
thinning
leads to a reduction
the thickness
in thin
metals and alloys during or shortly
at A in Fig.
segment
is evidently
lying in the primary
of the in the
plane (ill),
KEAR:
WORK
HARDENING
IS
ORDERED
Cu,Au
(b)
Fra. 8. Dislocation and antiphase structures in the same area of a thin foil of a section taken perpendicular to the primary slip plane, parallel to the slip vector. since it is visible trace
(dotted
as a single line parallel
line), whereas
screw orientations opposite
dislocation slip plane,
apparently
are in
cross slip in
In this case the trailing
the superlattice in the original
the end segments
and have undergone
senses.
to a (111)
partial
is dissociated
since it lies parallel
(111) trace of the mixed dislocation
of
to the
Another
segment.
3.3 Jog mechanimls
Jbr CPOM slip
Some of t,he possible intersection
configurations
jogs in superlattice
orientation
are illustrated
in Fig. 12.
state for jogs in dislocations be visualized t,he jogs;
by rotating
of other orientations
for details see Hirsch.(15)
the so-called
sessile jog,(16) results
pinch together
which must be the
with Burgers
vectors
segment in the edge
whereas
case
between
dislocations
at a point (arrow),
orientation
lying
configurations superlattice mediate
of a dislocation in the
(111) primary
involving partial
cross
only,
slip
hereafter
Such inter-
glide
with
study,“)
was found
on
a
a reduction
so that
the
equilibrium
dislocation width;
Such
in energy,
the antiphase
pair
dependence
dislocation.
In Fig.
oriented
can
cross
cross slip may
since
boundary
see Flinn(14)
orientation
similarly
for intermediate
slip into the cube orientation. orientation
their
in the
cube
energy
is small.
assume
a larger
for details
on the
of the energy of a superlatticc
9(b),
at B, the unusually
width of the superlattice dislocation cross slip into the cube orientation.
strongly
large
suggests
the
other
dissociated
only
at 80” or
(b) the jogs can if they
become
to form a short segment
that can glide in the cube plane.
hand.
jogs
state.
cause the stair-rod direction
vectors
of type
dislocation
i.e. combine
edge dislocation
crystal,
evidence
constricted,
one another,
of intersections
with Burgers
In the configurat’ions
termed
Case (b), Fig. 12,
at 90” cut through
120”.
can
lines about
when dislocations
(a) is a consequence
leading
cross slip, seemed to be quite characteristic
of the material. In an earlier
involve
plane.
of the
of edge
The dissociated
the dislocation
case at B in Fig. 8(a) shows paired screw segments that point of emergence
for dissociated
dislocations
of t’ype (a) can
since
the
bowing
dislocations
of the slip vect’or.
glide
The
in the
segments
to zip-fasten actual
of On will
in the
result
of
dislocation intersection in the superlattice also depends on whether a given dislocation, say a glissile primary
dislocation,
dislocation, dislocation.
cuts through
a stationary
forest
or is itself cut by a moving secondary The former yields a parallel jog con-
figuration xith neighbouring jogs having the same glide plane, Fig. 13(a), whereas the latter gives an
ACTA
666
METALLURGICA,
VOL.
14,
1966
(b)
Frc. 9. Changing dislocation structure with increasing 1)restrain (specimens l-3) in sections taken perpendicular to the primary slip planr, parallel to the slip vet3tor.
KEAR:
WORK
HARDENING
IN
ORDERED
667
Cu,Au
(b)
(a)
Fro. 10. Changing dislocation contrast with operating reflection in a section taken perpendicular to the primary slip plane, parallel to the slip vector, (a) 202 reflection, and (b) 111 reflection. In (b) the primary dislocations are invisible since g.6 = 0.
observed
dislocation
of intermediate on an expanding the points
structure in terms of nucleation
cross slip at random intersection dislocation
indicated
loop.
by arrows
on the loop
considered to be the sites where intersection just initiated
cross slip.
jogs
Thus, in Fig. 4(a),
The elongated
D are
jogs have loop
at E
represents a much later stage in the cross slip process, after extensive
glide of the leading jogs in each pair.
Intermediate
cross slip by the jog splitting mecha-
nism IO)
(bl
11. Illustrating orientation of Thompson’s’32’ FIG. reference tetrahedron ABCD for specif.ying the slip plane and Burgers vector of (a) a supeilattice dislocation pair, and (b) a superlattice dislocation pair with associated condensed vacancy dislocation loop. Burgers vectors are defmed after the manner proposed by Frank,‘33’ with the positive direction of the dislocation indicated by an arrow.
“oblique” tubular
jog configuration, antiphase
Fig. 13(b),
as pointed
and independently Figure
defect
by Vasil’yev
from
First,
orientation
for
crystal, the shear stress
dislocation,
apart of a jog
edge to screw.
dislocation
of the dislocation
It follows
that
if a
line assumes by chance
at a dragging jog pair, the
jogs may separate to yield an intermediate configuration,
inter-
in this particular
favourable
and Brown,(17)
in a superlattice
segment of mobile dislocation the near screw orientation
90”
section jogs, i.e. sessile jogs, for three reasons.
and Orlov.(ls)
14 shows that the distance
tends to increase as the orientation changes
particularly
which is the source of
in the slipping
out by Vidoz
pair (parallel or oblique)
seems
cross slip
as shown in sequence l-2 Fig. 15. It is
easy to envisage on this model the formation
of the
FAG. 12. Possible configurations for dissociated intersection jogs in a superlattice dislocation of edge character; (a) 60” intersection jog, (b) 90’ intersection jog.
x ,-\CTA
T”WW
METALLlTKGl(‘A,
VOL.
14,
1966
ANTLRLSE
_______
v----cr._-____-___ ,,-
..\ f
______
c____-_
___
CeLIWE JOG UMIFIGURATIZI
101
Ib,
FIG. 13. Parallel and oblique jogs in a superlattice edge dislocation pair. The oblique jog is a source of tubular antiphase defect in the slipping dislocation.“7~‘s’
in the cube plane is large, whereas that in the octahedral
cross slip plane is negligible.
trailing jog of the glissile constricted redissociate effectively
during anchor
one continues
slip
if the
process,
this
would
the trailing jog while the leading
its original motion.
of a slip induced orientation
the
Second,
pair happens to
antiphase
is a minimum,
Third, the energy
boundary
in the cube
so that the drag exerted on
the leading jog is a minimum. In sequence
2, Fig. 15(a), the trailing superlattice
I
*
,:I
*
I
FIG. 15. Illustrating possible slip motions for jogged superlattice dislocations. Sequence l-2 shows splitting of a jog pair to yield a pinned screw configuration, where neighbouring superlattice partials are dissociated in parallel slip planes. Sequence P5 shows the formation of a superlattice edge dipole by pivotal action at a stationary jog pair.
dragging
its jog along
with it.
The final sequence,
partial is shown to be parallel to the trace of cross slip
Fig. 15(a), shows that if the jog pair remains together,
generated
the advancing
by the leading
jog.
A variation
scheme
is that wherein
partial,
under the action of the applied
up the position the
the dissociated
on this
superlattice stress, takes
shown in sequence 4, Fig. 16(a).
intermediate
stage,
sequence
3, Fig.
In
16(a),
a
three-fold antiphase junction must be formed between the two Shockley partial dislocations, not constitute
As emphasized
final configuration superlattice
is a pinned
dislocation,
tials are connected boundary one. pinned
but this should
a serious obstacle to cross-over into the
final configuration.
since
together
previously,(l)
configuration
6he
for the
the superlattice
par-
by a strip of antiphase
that bends from one plane to a neighbouring
Figure
E(a),
sequence
configuration
eliminated
if the
3-4,
shows
that
for the screw segment trailing
edge
segment
the
(0,
FIQ. 14. Illustrating
by
formation
are believed
controlling
intermediate
slip
and
are several variations Thus, the movement
loop.
it is easily seen that there
on configuration
on the path
dipole
mechanisms
the slip distance of a dislocation
On further consideration depending
cross
to be important
taken
2, Fig. 15(a),
by the leading
jog.
of the jog may yield a segment
that bows out in the cube plane, such that the screw dislocation
pair takes up a configuration with maximum
corresponding
energy, width, in the cube orientation. Such behaviour
of minimum equilibrium
sequence 2, Fig. 16(b).
would account for the unusually large
may be
advances.
,bl
tendency for jog separation screw orientation.
dipole. Trapping of dislocation
segments
FIG.
I
segment may swing around to form a
stable edge orientation
in near
16. Some of the possible configurations that can result from cross slip of a superlattice dislocation. (a) Sequence showing the development of a pinned configuration for the superlattice screw dislocation, and (b) sequence showing dislocation multiplication by double cross slip via a cube plane.
KEAR:
widths of certain dislocation Another
possibility
WORK
HARDENING
pairs, as at B in Fig. 9(b).
is that the second jog follows the
IFi
ORDERED
Somewhat
669
Cu,Aa
similar behaviour
intersection
may occur also for 60”
jogs, at least in appropriate
path of the leading one, such that both segments tend
when the shear stress in the normal
to bow out in the cube plane.
is high, i.e. for crystal
frictional large,
stress,
slip in a cube
particularly
favourable
plane
may
such
as in
aplitt’ing
of superlattice
dislocations
sign in neighbouring at D, Fig. 9(b),
this manner.
slip planes.
Here the dotted line represents
of the
contrast
two
(light
the trace
Several
perpendicular
examples
are to be found
appears that a superlattice plane
to an adjacent
signs by
will be generated slip plane.
(arrows),
segments
and at E it loops from one
A third
case.
Fig.
17.
in
new
by
analysis
segments
cross slip plane,
regenerative
plane
cross slip at a dissociated
dislocation
the
Frank-Read
of the nucleation
Other mechanisms
for
by Fleischer,‘20)
and
been discussed and Seeger.(21)
In an earlier
paper, (l) it was suggested
slip may be nucleated
at points
that
of favourable
dislocation
loop and the
grown-in
structure,
and proceed
from
antiphase
these
domain
points
dislocation
nodes.
now considered
by
zip-fastening
of constricted
This mechanism
to be of doubtful
for cross slip is
significance,
evidence
has been found in this study
struction
of segments
The
most
antiphase
since no
for the
of the domain structure
of cross slip, as required
3.4 Antiphase
by the model.
defects important
boundary
parameter
contrast
associated
is the phase
vector and R is the boundary Antiphase frr,
contrast
occurs
with
angle,
a segment
the cube plane is necessarily happen
to
redissociate
assume
the
in the
bowing
constricted,
screw
original
out in
when
cc takes
Antiphaso boundary displacement vector, R
~
vector.(22) the
value
reflections.
1
Phase angle x = 2~ g.R for different operating reflections g = I10
g = 701
g = 01i
+H
+ 277
n
-7r
0
+a
77
but should it
orientation
it
may
slip plane.
When this happens over a sufficient length the new segment could be
reactivated
process
as
a secondary
may be described
superlattice
dislocation.
source-the
as double
entire
cross slip for a
; [TOI]
The noteworthy
feature
of
such double cross slip is that the average
distance
of
; [loll
cross slip tends to be small, since slip in (100) is likely to be difficult. Dislocation multiplication by
; [Oli]
such a mechanism for
the
structure
(010)
of double cross slip would account
characteristic
fine
in the deformed
and
homogeneous
ordered alloy.dg)
slip
1
i[Oll]
1 1 i
7T
{-
2?r
(109) +?f
-i T
LX,
lattice
1 gives values of tc for all possible combinations TABLE
follows from the fact that
displacement
which is the case only for superlattice
Table
de-
at sites
given by CC= 2rg*R, where g is the reciprocal
multiplication
cross inter-
action between an expanding
of nucleation
FIG. 17. Jog mechanism for dislocation by double cross slip.
of
jog in the regular f.c.c. lattice
has been given by Hirsch.(15) also by Schoeck
of opposite
result octahedral
of
that
A detailed
mechanism.
In the event of mutual
dislocation
one.
in
cross slip have
to the primary 9(b)
possibility
the
shows
of such edge orientation in Fig.
with
multiplication
in the
such cross slip, short edge segments in directions
and the
will
in the normal
dark)
of screw segments
to
in
mechanism
dissociated
dislocations
superlattice
that they have opposite signs. annihilation
The
could be interpreted
of the original plane of one bowing segment, in overall
state
of the glissile jog pair, Fig. 12(a), cross slip by the jog
of opposite
change
[loo]
In this case, in view of the dissociated
under
circumstances,
to the attraction
or [ill].
plane
approaching
orientations
occur
arrangement
vicinity
or
stress for motion in the cube plane should be
but
response
The Peierls
orientations
octahedral
0
ACTA
6’70
METALLURGICA,
VOL.
14,
1966
the foil has been tilted so as to give contrast with the i01 reflection only, and the effect is to cause most of the
(010)
junction
(4
boundaries
to
disappear-the
three-fold
at A becomes an apparent two-fold
According
junction.
to Table 1 this must mean that the (010)
boundaries
have
displacement
vectors
parallel to (OlO), i.e. the boundaries shear type.(23) operating
Similarly,
reflection,
by appropriate
identical
for boundaries
Fig.
It may be concluded,
grown-in
domain
approximating low energy
have
in (001) and (loo),
structure
therefore,
consists
of
to cube orientations,
shear type,
are
choice
results
obtained 18.
that
are of low energy
e.g. see that the
boundaries
and mostly
in agreement
of
been
of
with previous
work,(1n22) In most antiphase
(b)
original
cases, new crystallographic boundary
segments
were found associated
grown-in
domain
these new antiphase
structure.
In
general,
defects were most prominent
the thinnest regions of the foil, and it appeared the majority ment 3.1).
or shortly
FIG. 18. Entire grown-in antiphase domain structure in a section taken parallel to the slip plane, as revealed by using two different operating reflections. (a) TlO reflection, and (b) Oli reflection.
of displacement available
vector
operating
foil, Fig. 3(a). superlattice in
reflections
a/2(110)
with
in an [111] orientation
It is clear from Table 1 that a single
reflection is not sufficient to give contrast
for all possible +2x
of the type
types
certain
reflections
of boundary,
cases;
are required
at
least
since two
u = 0 or
superlattice
to reveal the entire domain
Figure
19(a)
structure
shows
the
in a region
where contrast superlattice although
entire
grown-in
of an [ill]
orientation
is due to at least two
reflections.
somewhat
The
irregular
domain foil.
after electro-thinning defects
characteristic discernible
Again,
profusion
of antiphase
foil of specimen structure. antiphase
is no longer in
Fig. 21 shows another
example of a
defects in a particularly
3, with no recognizable
Careful examination
micrographs
structure
region of the foil (just
at top left of micrograph)
evidence.
thin
dislocation
of these and similar
shows at least two types of slip induced
defect.
Figure
19 shows ribbons
of anti-
phase defect (arrows) that have been formed tions ; here the are recognizable dot
dissociation
of superlattice
superlattice
partials
contrast
for
locations.
tend
many faintly contrasting
regular
simply disloca-
in Fig.
as single dot contrast,
boundaries, to be
(white traces parallel to
of the thicker
overlapping
in shape,
(see section
the edge of the foil, where the dislocation
double
domain
in the foil
clearly occurs only in the thinnest region near
by the complete
structure.
occurring
This is shown in Fig. 20, where a high concen-
t,ration of antiphase [iOl]
in
that
of them were formed by the rearrange-
and loss of dislocations
during,
of
with the
19(b)
as opposed
superlattice
to dis-
On the other hand, Figs. 18 and 22 show lines parallel to [iOl] which
oriented parallel to cube planes, e.g. the segments of
are considered
boundary
have been formed by dragging oblique jogs on super-
forming
approximately
the three-fold
parallel
to
junction
(OOl),
(100)
at A are and
(010)
lattice
to be tubular
dislocations,
Fig.
antiphase
defects that
13(b).(17*1s) This explana-
Marcin-
tion is consistent with the fact that antiphase defects
kowski(22) have reported much more crystallographic cube oriented boundaries in homogeneous, recrystal-
sometimes extend from top to bottom of the foil, and are not necessarily associated with the points of
tracts,
lized
Fig.
3(a).
polycrystalline
irregular material
domain
Previously,
material. structure
is a consequence
from the ideal stoichiometric be expected
Fisher
in a melt-grown
and
Possibly characteristic
of
localized
composition, crystal.
the of
more this
deviations which is to
In Fig. 19(b),
emergence primary vector
of dislocations. Further, as required for slip induced defects with displacement
a/2[iOl]
reflection,
Fig.
they become 22(a),
invisible
using the iO1
since the phase angle a = 2~,
see Table 1. Note that this contrast
effect tends to
KEAR:
WORK
HARDENING
IX
ORDERED
contrast
at
almost
superlattice
of Fig.
antiphase
(4
exactly
reflection,
inspection
671
Cu,Au
the
as
24(b),
in
Bragg Fig.
however,
angle
24(a).
Careful
shows
that
large deviations
where in fact structure
the contrast
has actually
anomalous
contrast
from the Bragg at the grown-in
disappeared. effect
is
is a micrograph
understood.
of the micrographs
and antiphase
contrast
the motion
24, the fact that the dislocation
an obstacle
exhas
In Fig.
segment at A appears itself around
boundary
indicates
to dislocation
motion,
a seg-
that the latter is which
is to
when the dislocation
in Fig. 24, the fact that
location antiphase
at B correlates boundary
dislocation/domain
cuts through it.
t’hc kink in the dis-
with the presence loop
suggests
of a closed
some
kind
interaction.
Fro. 19. Antiphase domain structure in a section of specimen 2 taken parallel to the slip p&m. (a) Two overlapping superlattice reflections, (b) 101 reflection. In (b) one set of boundaries lying approximately parallel to (010) is not visible since the phase angle a = 271.
rule out an alternative
explanation
in terms of the formation by screw dislocations
of the phenomenon
of diffuse slip traces, or tracks
escaping
through
the surface of
the foil. Antiphase
defects
regular dislocation the
foil,
were found also associated structures
indicating
structures
that
in the thicker
in these
were representative
Figure 23 shows antiphase to terminate dislocation location,
at points
areas
of the
defects (arrows) that appear
in sequence
3, Fig.
high concentration
defects at the bottom
right-hand
correlates
As mentioned oblique
an
of
jogs
when
on glide
dislocations
mechanism
contrast the
of
foil
(b).
suggests that an of
is an important
in the superlatltice.
of antiphase was
In
dislocation
in micrograph
drag due to the accumulation
stopping
Optimum
15(b).
of antiphase
corner of micrograph
avalanche
earlier, this correlation
frictional
dislocation tained
with
in near edge orientation
enhanced
defect’ sample.
loops, i.e. at the sites of jogs in the disas illustrated
segments
the
of cross slip in segments
Fig. 24 an unusually (a)
with
regions of
bulk
oriented
defects for
was obdiffraction
be
since energy must be supplied to create a step
in the boundary Again,
boundary
of glide dislocations.
to be in the process of wrapping ment of domain
in both
shows many
amples where the presence of antiphase influenced
A
the latter
of a region to the right of Fig. 24(b).
A careful examination dislocation
angle, domain
The origin of this
not
similar effect is shown in Figs. 5(b) and 25;
expected
the
defects are still just visible under conditions
of relatively
(b)
for a
Fra. 20. Concentration of antiphase defects (bottom right of micrograph) near the very thin edge of a foil of specmnen 2.
of
ACT.4
672
JIETALLURGICA,
14,
1-OL.
this
1966
case has been developed
recently
by Vidoz,(24)
and the results show that such a conclusion As mentioned curve at 77°K the
briefly elsewhere,t7)
shows much less work hardening
corresponding
StoloP25)
curve
have confirmed
have shown that tinuously
result is indicative Vidoz
to a maximum
of a diminishing model
activated
of secondary
ljrimary
dislocations
conThis
slip distance
foi
On the by
of localized secondary mainly by primary
process;
the low work hardening
inability
increases at 350°K.
can be explained
that the penetration
is a thermally
and
and moreover
temperature.
this
than
Davies
this result,
slip into the crystal deforming 77’K
298°K.
loops with increasing
and Brown
assuming
at
the work hardening
from 77°K
dislocation
is justified.
the stress/strain
slip
in other
words at
is identified
with the
dislocations
to cut through the
and form oblique
jogs in them.
Davies and Stoloff,(25) on the other hand, suggest that as a dislocation PI(:. “1. High &n&y of a&phase defects in u particularly thin foil of specimen 3.
that cross slip will occur, so that a
barrier
as in sequence
is formed,
increase explained Vidoz and Brown(l’)
have proposed
rapid rate of work hardening alloy,
compared
disordered produce
jogs for
cations the
that
in
antiphase
the
defects
in superlattice
antiphase
that
the
studies(‘)
in the
wake
of an
since nucleation
pre-strain
in the disordered
value for the coefficient which is comparable difference
are jogs on anelastic frictional
proportionally
CusAu,
of the frictional
for ordered and disordered
coefficients
for the
in stage
I1
Cu,Au.(l)
The specific model proposed
by Vidoz and Brown
slip in at least two intersecting in thin
component
with the value of -G/750
Burgers
of
The measured
in the ordered alloy is -G/1000.
in work hardening
appropriate
with the
but is independent material.
(a)
indi-
the dislocation
vectors.
In this
systems study,
foils has been obtained
ih
with direct
for an in-
creasing activity in secondary systems throughout stage II, but in amounts small compared with that in the
primary
system.
To reconcile
this
observation
with the intersection jog model, therefore, it must be argued that even relatively small amounts of slip in secondary t,he primary
systems system.
have a profound The mathematical
effect on slip in treatment
foi
FIG. 12. Chang_ in antiphase contrast with operating reflection. (a) 101 reflection, (h) overlapping 101 and 110 reflections.
is
increasing
of
previous
roughly
in ordered
of the work hardening
with
of the defects
have shown that
rp, increases
evidence
in terms
of forming such barriers
The
In agree-
production,
Furthermore,
pre-strain
requires
simply
16(a).
corresponding
dislocations.
defect
sources
dislocations.
stress,
quite
4, Fig.
with temperature
in the deformed ordered
ment with this model, evidence has been found in this study
likelihood
in the work hardening
alloy, is due to the extra energy required to tubular
oblique
with
that the more
loop expands in the slip plane there is
a finite probability
of
KEAR:
WORK
HARDEKING
(4 FIG. 23. Antiphase
ORDERED
Cu,Au
673
(b)
and dislocation
structures in the same area of a thin foil of specimen 2.
(a) FIG. 24. Antiphase
IN
011: reflection.
(b) and dislocation
structures in a thin foil of specimen 2.
Oli reflection.
ACTA
674
METALLURGICA,
VOL.
section their
14,
1966
jogs, since these jogs are constricted glide
motion;
60” intersection
favorable sites for vacancy condensation dissociated
state.
Figure
lattice dislocation tion of vacancies boundary. 6A-t
jogs
during are less
owing to their
11(b) shows that a super-
may become
pinned by condensa-
on its connecting
The dislocation
loop
strip of antiphase with vector
DA can react with the inner Shockley
of the dissociated
superlattice
sessile dislocations,(26-28) loop probably
dislocation
Fig. 26.
will occur
Dd + partials
to form
Nucleation
of the
on that partial giving the
lowest energy sessile configuration,
e.g. on the inner
partial B6 in Fig. 26(a) to give a stair-rod dislocation with vector
AB/yB.
The attractive
feature
of this
mechanism is that pinning can occur along three (110) directions
in the slip plane, so that the expansion
the entire dislocation
loop may be inhibited.
the slip distance may be controlled temperature
dependent
fluctuations
FIG. 25. Dislocation avalanche exhibiting deep cusps (arrows) in individual dislocation segments of near edge Note also faintly contrasting lines lying character. parallel to the slip vector.
could be important
constriction
should be thermally
assisted.
tions for temperature as follows:
required
for
cross
of intermediate
between
glide
and
cross slip, Fig. 15(a), (ii) in promoting
of superlattice
Fig. 16(a) sequence
4, spontaneously
excess
neighboring
slip plane, thereby
defect/oblique
jog
in Figs. 11(b) and 15(b).
mechanisms,
together
densation
frictional
Figure 15(b) shows that the
stress may be enhanced
of excess vacancies
with that
temperature
dependent
sources of antiphase
disloca-
one to retain the attractive
even at
hardening,
This mechanism
low vacancy
should
supersaturations,
BC-BB W-Do uIc+
+ +
**c +
ac as+*a
y*+z,a yD
+ns/,a
(al FIG. 26. Illustrating condensed vacancy
The
latter
illustrated
two
in Fig.
as proposed
in one system, and allows idea of antiphase
defect
by Vidoz and Brown.07)
To
be more specific, the source of antiphase defects in the
at least for 90” inter-
DA)rt)B +
IBC+*M
be important
and
strain hardening under condi-
tions of slip predominantly
tion.
constricts
creating an antiphase
arrangement.
this may transform them to oblique jogs and therefore in the slipping
dipoles
1 l(b), are of particular interest, since they can explain
by con-
on parallel jogs, since
defects
screw dislocation
follows a different path from the leading one into the
point defects generated by the dragging jog or dislocation coalescence mechanisms. Two cases are illustrated dislocation
the
antiphase defects, and (iii) in causing a modified form
work hardening are
dislocations
thermal
of double cross slip, wherein the trailing screw segment,
First, the slip distance may be influenced by
interactions
Thus,
(i) in determining
in such a manner as to form oblique jogs and associated
slip
Other possible explana-
dependent
by some form of
slip.
frequency of dislocation pinning by the jog mechanism annihilation
the dislocation
cross
of
Second,
.!.C-SBB+BC mcOo+.a ~BC+Dl\)r88+DS
lBc+aorac+n6+2ss
tb)
+ap. +BD,.~
nc-4a+ec DA-D,%-SA I&z+DbWa+d
+2.a
I&+Ao)-BC+Eo+2~o
(cl
products of dislocation reactions involving a dislocation loop and a superlattice dislocation.
KEAR:
slipping dislocations of point
defect
dipoles,
WORK
HARDENING
may be considered to be the result
interaction,
or double
annihilation
cross slip, rather
of screw
than
dislocation
IN
ORDERED
The
preceding
intersection
discussion
jogs
dislocation
675
C&Au
has
acquired
shown
by
loops can have a profound
slip process.
Thus,
it is considered
through the
mechanisms
of dipole formation
tion
slip (section
3.3), and also through
following
dislocations.
the
motion
It follows that
of the
a back
on the source will soon develop as successive tions get held up, and therefore tions
will emerge
stress
from
the
relatively
source
builds up to the point
disloca-
few disloca-
before
where
stress
the back
the source
on the
control the average slip distance
locations
will impede
effect
jogs on dis-
phase defects in the slip plane by the leading dislocaa source
forest
primary
that
intersection, as originally proposed. In this connection, it should be mentioned that the formation of antifrom
how
expanding
point defects and antiphase
and intermediate
of
defects, and interaction
of
these defects with glide dislocations. expression
cross
the generation
A simple general
for the flow stress that takes these factors
into consideration
is
can
no longer operate, which is in accord with the relatively small slip offsets observed. dislocations
course, another oriented
slip
direction
Interactions
and slip induced
dislocations.
mostly
Evidence
for
the creation
[iOl] in this particular defect
Fig.
double
micrograph
cross
there
CusAu.
for double
slip of the
At present,
from tensile
work
cross slip, probably
involving
much more experimental At
elevated
location/point important
the
of anti-
defect interaction
deformation,
and
FlinnZo4) who also emphasized
more
sources
extensive
This point was recognized
possible.
dis-
should become
tend to become
climb first by
that the climb process
favourable-the
lowest
energy
parallel
trapped
mechanisms. that
the
Previous
anelastic
con-
by the different
work(‘)
dislocation
(TV + TV’) accounts
for about
Moreover,
has shown
frictional
a similar
contribution
to the
from observed
densities after various pre-strains of -l/3
explanation
for this
discrepancy
although
it does seem possible that 7Q may have been
underestimated. densities
This
be offered
in stage
of the flow
No satisfactory can
stress
Q of the flow stress
flow stress from 7. has been estimated dislocation
stresses in neigh-
stress set up by
in the crystal
combined
in stage II.
and ho the
dislocations
bouring slip planes, i.e. the interaction dislocations
is
because
at
this
the
time,
dislocation
in the thin foils may not be representative
of the bulk sample. temperatures
To be more specific,
some of the narrower
at ambient
edge dislocation
dipoles may anneal out by climb and unstable dislocation
dipoles may annihilate
Interactions induced
between
point
scribed of
since dislocations
is energetically
dependent
work.
as well as sinks for vacancies, becomes
for
of the details will require
temperatures
for nearly
to be explained.
in ordered
creation
on the dislocation,
stress
it is believed that the experimental
Clarification
considered)
stress,
(both long- and short-range
in
tests will be
to account
hardening
stress”
frictional
drag due to the presence
No
it seems clear that
of mechanisms
of jogs and defects “passing
dislocation
frictional
This leaves a component
shown above.
where 7p is the intrinsic 7p’ the additional
II.(l)
defect interactions,
evidence favours some type of temperature phase defects.
cross
from thin foil observations
evidence
dependent
type
form discussed
In sum, therefore,
is no shortage
temperature
are considered to be
dislocation/point
but some indirect
in its
but it is not clear whether this
evidence has been obtained
discussed later.
possibly
defect
lines parallel to
Evidence
17, or the modified
for supperlattice
dipole
The deep
of annihilation,
contrasting
trails.
slip has been discussed, represents
(110)
screw
of an antiphase
The many faintly
antiphase
of
at B in Fig. 5(b) seems to be a
screw dipole in the process wake.
is, of
of a highly
consisting
has already been mentioned.
cusp in the dislocation involving
defects
reason for the development structure
configurations
between glide
antiphase
defects
as a dynamic
therefore,
glide
dislocations
represent
what
and
may
significance
slip
be de-
source of work hardening,
of permanent
uous deformation.
screw
by cross slip.
and
only in a contin-
If the deformation
is interrupted,
so as to allow the excess point defects to be eliminated completely
by diffusion,
location
sources
structure
should
glide,
at
least
on reloading
developing
from
experience
the new dis-
the
a reduced
temporarily,
and
pre-existing resistance
the
to
dislocation
figuration for an edge dislocation pair with slip vector a (110) is with one segment above the other in
velocity and slip distance will be enhanced. The slip distance and dislocation velocity will be reduced to
neighbouring
the original value characteristic
slip
planes.
A
reduction
in
energy
would be achieved also by the mechanism illustrated in Fig. 26. where glissile u (110) type superlatt,ice dislocations with
are
t,he shorter
t’ransformcd slip
vector
to
sessile
n 1100).
dislocat,ions
only after
a burst
priate excess concentration required frictional drag. explain
the repeated
of the applied stress
of slip has recreated of defects Such
yielding
the approto give
behaviour
phenomenon
the
would observed
676
in the yield
interrupted point
through
deformation,
representing
the crystal
consistent
also
Fig.
a burst
1, with
as a Luders front.
with
the
each
of slip spreading
absence
This model is
of the
reloading
neighbouring
dislocations
phase and point latter
point,
avalanche
defects.
consider
and the presence
of anti-
As an illustration
of this
the
in Fig. 4(c).
case
effect at 80”K, and the fact that it makes its appearance only after a few minutes ageing at room temperature.“)
lished
It
10M8 cm,
be
mentioned,
also,
process at room temperature
that
the
may involve the elimina-
tion of some of the slip plane debris unstable
dipoles and antiphase
of course, diminish good reason defect
consists
one-half
defects.
This would,
avalanches,
In the limiting
or bursts
translation
In principle,
can be eliminated
distance
therefore,
by
in the slip
an antiphase
by diffusion
of
case, an antiphase
of a single row of atoms displaced
a complete
direction.
in the form of
both rF’ and TV, which is another
for dislocation
slip on reloading.
recovery
defect
of a single vacancy
along its entire length. Previously,(l)
that
the flop
stress in the deformed ordered alloy may be expressed in the form
ho -
7F
by -4
musb also be acting account
for this
is the
dislocation
Gb/L is th e critical
stress
and
In sum, therefore, stress
formula
The
present
importance
of intermediate
work
cross slip in the
mation process, but no clear indication for a diminishing model, effect
except
L with pre-strain, perhaps
in dislocation
4(c) and 5(b). correlation expected,
for some
avalanches,
the defor-
has been found
can influence
segment
L, and (ii) other factors influence the bowing pinning points, such
the bowing
out of a dislocation
in the slip plane.
Finally,
it’ should discussion
perhaps
and involves
ordered
(X N 0.8)
the motion
In the disordered
be stressed phases
of the
alloy,
of superlattice
dislocations.
alloy, where slip is very coarse and motion
of many
type,
dislocations
the decisive
and short-range
recent theoretical
the
fine and homogeneous,
slip process seems to be the interaction dislocations
that
applies only to the fully ordered,
order.
of the
factor
in the
between
glide
According
to a
study of this problem by Cohen and
Cottrell,(31)
e.g.
of this
compare that
Figs.
a definite
can hardly
be
slip to give an observable besides the line tension
out of a as elastic
since it does not take
Fine,(2g) based on earlier work by FishercN) and also
L and pre-strain cross
stress must be involved.
as required by the
since (i) not all the jogs on the dislocation
loop will nucleate
7c and the
indication
It is now recognized
between
confirms
60
In other
other factors besides the line tension
dissociated
slip in a
segments
calculated
is inadequate,
into consideration
group
loop.
between
3
stress
it now seems clear that’ the bowing
ordinary
cross
x
value
opposing
configuration.
from other sources of internal
involves
of intermediate
This
shear stress in specimen some other
where slip is characteristically
stress to bow out the glissile
dislocation
7 kg/mm2.
on the dislocation
cases, t,he discrepancy
or partially
frictional
,u. From pub-
flow stress is larger, so that even greater contributions
edge (or mixed) segments of average length L between at points
7e -
particular
the
jogs
is ~0.25
1O’l dyn/cm2 and b = 5.3
x
gives
kg/mm2, so that
preceding 7 = Tp + Tc
where
G = 3.3
which
falls short, of the operative
that
it has been proposed
data
dislocation
The average width of the glissile
edge segments in the avalanche
should
of the
can
segment between interactions with
the leading
dislocat’ion
in a sequence,
group should occur in pairs, and the spacing pa.irs should
increase
because
passage
the
for successive of a sequence
across a slip plane in a material order causes oscillations
pairs.
or
of the This
is
of dislocations
containing
short-range
in the local order across that
plane, which are large initially but get progressively smaller-about 6-8 dislocations through a region bring3 the value for local order to it)s final value.
The
KEAR:
driving
force
accelerating
the lead dislocation, numbers,
successive
therefore,
second,
etc.
release, Figure
in the deformed
in striking
agreement
rapidly
the third
arrangements
disordered
short-range
must
above
more extensive partly
have
T,,such
clarified
material
of dislo-
directions,
have not been with
minimum
order following a rapid quench from above
is believed,
T,. It sample
in
of
analysis.
the groups
by arrows. Such groupings
previously(l)
to
alloy that are
cations at A and B are moving in opposite as indicated
to the
less rapidly
with the theoretical
It follows from the model that
observed
to
gets less with increasing
27 shows
dislocations
HARDENIXG
dislocations
i.e. the second is accelerated
first by t,he energy the
WORK
therefore,
that
been imperfectly
that
the local
than
usual.
by further
this
particular
quenched
order developed
This point
investigation
from was
needs to be
on quenched
and
ordered alloys. ACKNOWLEDGMENTS
The
author
is indebted
to Dr.
many
helpful
discussions.
and to Mr. M. E’. Horn-
S. M. Copley
for
becker
for valuable
assistance. REFERENCES
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IX
ORDERED
Cu,Au
6i7
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