,bfarenals
Chemistry
and Physics,
SOLIDIFICATION
OF COPPER-RHODIUM
Chimie
Analytique,
Received
ALLOY
SINGLE CRYSTALS
and F. BOUILLON
Fat. Sci., C.P. 160, Brussels
27,
August
225
225-233
M. JARDINIER-OFFERGELD
DELPLANCKE,
M.P.
27 (1991)
1990;
accepted
1,
October
University,
Brussels
(Belgium)
1990
ABSTRACT Preparation method
of copper-rhodium
is described
in this
process
solidification
to characterize the
the
and
of
are
in agreement
of
1.5,
electron
(microindentation,
thermal
single
solute
4, 8.15
and and
of
the
by
structures 15 at.%
Rh
scanning A study
distribution.
existing
crystals
Dendritic
microprobe
stability
with
alloy
paper.
structures
the vertical are
microscopy)
the
is also
Bridgman
during
Various
alloys.
Auger of
formed
formation
the
methods are
used
conditions The
presented.
results
models.
INTRODUCTION The properties of the
the most elements For
cess. senting
in the a given
both
alloys,
turbines
In the
tation
over of
samples
surface of
the
02%0584/91/$3.50
of
can
of
last
these
segregation
exposed
are
be obtained
face.
related
the
Due
of many
five
copper-rhodium
and
years
Many
oxidation
A fundamental
the
or
sample
prop
parame-
in pure
melts
importance
machine
parts and
of
prey
solidification
theoretical
and
of like
experimental
[l-t?]. system,
properties rates
TWO
distribution
solidification
occur
of critical
thirty
alloys.
to the
factors.
the
to the practical
of
the
and
structures
properties subject
on various
material
by varying
solidification
been
a study
depend structure
homogeneous
non-metallic.
have
the
them
a completely
cellular
they
context
homogeneous
Both
and
materials
the crystalline
in the mechanical
blades,
investigations
energy,
bulk.
metallic
wrought
are
system,
and
structures
and
ones
microsegregation Dendritic
ters.
these
of cast
important
such
depend
study
0 Elsevier
of
on
we
tried
as
surface
to prepare free
the crystalline
the mechanisms
Sequoia/Printed
orien-
controlling
in The Netherlands
226
these phenomena line
requires
the preparation
of well
characterized
single
crystal-
samples.
A preliminary prepared
by
study,
the
performed
vertical
in this
Bridgman
method
laboratory presented
[91 showed visible
that
the
samples
solidification
struc-
tures. The
main
purpose
structures,
methods
dium system. the phase
this
paper
to characterize
analytical
system
of
and
published
is characterized
a partition
solute
to apply
the
1101.
of the solute towards
samples
of
are mainly
(rhodium) higher agents
these
by various
to the copper-rhoobtained
The copper-rhodium
gap between
chemical
stability
models
for this last point
by a large miscibility
coefficient
in the
theoretical
by Raub and al.
in the reactivity
thermal
distribution
existing
The data necessary
diagram
difference
the
is to examine
from
binary
20 and 90 at.% Rh, by
than 1 and by a great
as a function
of the rho-
dium concentration.
THEORIES The
growth
processes These
factors
the diffusion
imply that the crystal
ones
have
rate been
to allow
growth
in space.
the
the effects
of gravity
The oldest model,
slow rates of solidification.
of
true
proposed
by Chalmers
Our experimental
: diffusion
liquid-solid limited
in the solid is negligible,
interface
during
the partition
face. cooling
for very
(solidification
rates
Three main assumptions
equilibrium
is maintained
the study stats, and transport
the solute distribution
In these conditions,
induces
The recent
are
at the
in the liquid
is
to that by diffusion.
rate (R), the diffusion
phases.
the
with those ob-
I151 is valid
conditions
lower than 10-2cm s-l) allow the us8 of this model. made
results
with
Different
in alloys.
and compare
:
phenomenon
equilibrium.
the microsegregation
of
transformations.
is a non-equilibrium
establishment
to modal
proposed
Ill-141 introduce
tained
by the coupling
fluid flux and phase
rate of the solute in the solid is too low in comparison
solidification theories
from its melt is characterized
of a crystal
such as heat and mass transfer,
coefficient
The rejection the formation Tiller
coefficient
of one of the constituent
a criterion
on the solidification
in the liquid phase
(k,) of the solute between
of a supercooled
established
depends
of the solute
(D) and
the solid and the liquid
elements,
in our system copper,
zone in front of the solid-liquid of apparition
inter-
of the constitutional
super-
:
G E+(T) S R where G = the imposed
thermal
gradient
m = the slops of the liquidus C,= The
presence
the mean composition. of
lar or dandritic,
the
supercooled
dependent
tions wsrs developed
zone allows
the development
on the experimental
to model
the spacing
conditions.
of structures Precise
cell"-
calcula-
and the size Of these structures
14.
227 They are mainly
7,161.
based on the observation These
succinonitrile-acetone. drite as
li
studies
of transparent
established
systems
that the spacing
to 6 G and that the radius of the dendrite
arms is proportional
like
of the dentip varies
c,. d--
Despite
the practical
few studies model
interest
have been performed
based on a sinusoidal
the concentration concentration
repartition
treme values
is considered
Under
value.
ted by the relation
of the solute,
Another
area.
as completed
of the concentration
of the structured
Flemings
1171 developed maxima
the
(if k, > 1) and the minima
in the dendrites
of the interdendritic
homogenization
initial
of the homogenization
on this topic.
is reduced
representing
representing was made,
when the difference
in the sample
these conditions,
assumption
alloys,
a simple
between
the
that the
the ex-
to one tenth of its
the homogenization
time can be calcula-
:
L is the size of the cell, AC H,e/ACR,t is the ratio of the concentration
where
difference
at t = 0 and after an annealing
terdiffusion
of t hours and 6 represents
the in
coefficient.
EXPERIMENTAL The apparatus method
for the solidification
was designed
was the movement
of the oven along
The rate of the oven displacement a pumping
device
(mechanical
was measured
the alumina
the melting
by a Pt-PtRh
A more detailed
[18j.
was machined
and purified To obtain
macroscopically
crucible, a cavity.
it was necessary
first to prepare
in the graphite
of four fusions were necessary
99.999%
and origin of Hoboken
of Johnson-Matthey, The orientation
face, mina
rhodium wire
ning phosphoric
rod and machine
(Fig. 1).
to obtain
with the it to form
The assembly
was
samples.
Alloys
satisfactory
by this method.
was
determined
the following 99.9% and
: 'specpure' 99.997%
by Laue back reflection
the rods along
polished
isopropanol,
the desired
on metallographic
by a short electrochemical
acid, ethanol,
the mean concentra-
crucible.
rhodium powder
After cutting
the samples were mechanically ($4 lnm), followed
purity)
99‘99% of Ventron.
of the alloy rods
of one degree.
The
rod.
of the components
a copper
of the pure metals were (Belgium),
of
the alumina
(spectroscopic
that presented
The cavity was then filled with rhodium
The purity
precision
rod
of a copper
samples
processes. between
with
a pressure
can be found in the literature
out of a graphite
at 1.5, 4, 5.75 and 15 at.% Rh were prepared
copper
placed
part and to avoid any reaction
then fused and solidified A minimum
description
is equipped
able to maintain
thermocouple
Bridgman criterion
the crucible.
The system
and solidification
homogeneous
design
tube containing
pumps)
by the fusion and solidification
tion in their central
important
could be varied.
tube and the oven. The crucible
and the most
and diffusion
7 x 10-3 Pa at 1273 K during temperature
of the alloys by the vertical
in this laboratory
polishing
urea and water
with a
crystalline
papers
and alu-
in a bath contai[19].
228
Rhodium. m
Copper
rod.
m
Graphite
mould.
Fig. 1. Scheme of the graphite single crystals.
The bulk composition was used to determine The solution tion, scanning Energy
was monitored
distribution
X-ray
X-ray diffraction
: microindenta-
by three methods
(SAM) and electron
microprobe
analysis
(EDXRF,
system
(m = 15
Fluorescence).
of the Tiller
criteria
to the copper-rhodium
Rh. k, = 1.85) shows that in our experimental
stable
for rhodium
gradient
concentrations
Fig. 2, to prevent the formation lidification
Experimentally
the preparation
of materials
as it is very difficult structures dendritic
obtained
or dendritic.
the copper-rhodium are, of
influence
in a 1.5 at.% Rh alloy, the so-
course,
structures
: FCC.
dependent
of the structures of the crucible
rates that also allow
are not interesting
in our case
under these conditions.
The
at 1.5, 4. 8.15 and 15 at.% Rh are cellular-
The growth direction
alloys
at a rate of 5.5 x 1W5 cm s-1
single crystals
for the alloys
re-
by one order of magnitude.
without
are the axes of the crystals
regularity
interface
As shown in
The high solidification
to obtain
(solidification
lower than 0.18 at.% Rh.
a 1.5 at.% Rh alloy solidified any structure.
conditions
20 K cm.l) the solid-liquid
of structures
rate has to be reduced
does not present
drites
fluorescence.
present.
was characterized
rate = 8 x 10-4cm s-l, thermal mains
by X-ray
of the alloy
AND DISCUSSION
The application K/at.%
used for the preparation
the number of phases
Auger microscopy
Dispersive
RESULTS
mould
of the dendrites
in agreement The geometry
and of the arms
with the crystalline of the figures
on the examined
crystalline
over the whole crystal
system of
formed by the den-
face (Fig. 3). The
(Fig. 3b) indicates
wall is small in our experimental
device.
that the
229
cm”
G=20K
C.
4 R= 6.1E4 cm 1s
IO2 -
12.
I
1
'1 I
1
I
I
I
1
R (cm/s
1
+ 12
1-d' Ii3 ci2
11
1
10
IO2
IO3
Fig. 2. Representation of the formation conditions of the different types of solidification structures in function of the rhodium concentration (Co) and the solidification rate (R) for a temperature gradient of 20 K cm-'.
Fig. 3. a) Cu-Rh alloy, 15 at.% Rh single crystal, face (111) solidification structures magnification : 15 X Fig. 3. b) Cu-Rh alloy, 4 at.% Rh bicrystal, face (110) for the main crystal lidification structures magnification : 5 X.
so-
230
Table I.
Average size of dendritic arme L as a function of the rhodium
concentration. C (at.% Rh)
(cm)
L
3.1x10-2
1.50
(111) face
2,7x10-'
4.00
(110) face
2,5x10-*
a.75
(111) face
2.0x10-*
15.00
(111) face
Table II. Calculated and experimental time for homogenization. C(at.% Rh)
L (cm)
1.50
3.1x10-*
D (~rn~.s-~)
t theor.
3X16'O
(h)
t exper.
210
4.00
2.7x10+
3xl6'O
157
114
a.75
2.5~16~
3x1ci'"
135
138
15.00
1.9x16*
3xuY0
78
93
An average
size of the dendrite
for each alloy. the rhodium
arms
(L) was measured
Table I shows the evolution
concentration.
this is related
to the higher
which
allows
Table
II presents
concentration
from microscopy
of this parameter
The size decreases
pictures
as a function
with increasing
gradient
(h)
98
of
concentration;
in front of the interface,
for the growth of a higher number of dendrites.
time necessary
the results
to obtain
at 1263 K either
in vacuum
tion is the bette;
of the annealing
homogenization.
or under atmospheric
one as it reduces
experiments
The thermal
and the calculated
treatments
pressure
copper evaporation
of
Hz.
were performed The later condi-
(vapor pressure
of cop-
per at 1300 K is 1.3 x 1O-2 Pa). The lack of diffusion
data required
obtain
times.
the calculated
fusion coefficient mate
To estimate presenting
is barely
coefficient
fulfilled
it is not credible
proximation,
the error similar
induced
earlier
and extrapolations
to
for highly
dilute
solid solution.
by the 1.5 at.% Rh alloy
in a first ap-
for the alloys at 4, 8.75 and 15 at.% Rh.
by this shortcoming,
characteristics,
system, whose
copper-nickel were studied tion
of rhodium
that of the interdiffusion
If this condition
some approximations
The only published value is that of the heterodifcu in copper DRhe 1201. This value could approxi-
which
solidification
in our laboratory
we looked
for a binary
was studied more extensively. morphological
and structural
[21,221, seems to fit with
system The
aspects
this descrip-
: the solute diffuses much more slowly in copper than copper itself does.
The evolutions solutes
CU of DRh*
and
dir* with temperature
are in the same group in the periodical
For the copper-nickel
system,
the literature
ween D and the solute concentration.
are similar
1231 and the two
table. [231 reports
the relationship
At 1273 K, for a Ni concentration
than 1 at.%, D = 5 x 10e10 cm2 se1 but at the same temperature to 5 x 10.11 cm2 s-1 for a Ni concentration
of 50 at.%.
bet
SmallSr
the D value drops
If the evolution
is si-
milar for the copper-rhodium system, we can expect an error induced by the use cu This factor could explain the longer Of DRh* in place of b as high as 150%.
231 time necessary
to homogenize
theory and experiment rection.
This could be due to the estimation
is well defined
for a cellular
structure,
The use of the size of a dendrite
one.
The
tance.
second power
ment between Rhodium penetration variations
theory
presence
regions,
arm overestimates relation
size.
di-
Although
the diffusion
amplifies
of the two factors
in copper
increases
This effect
I,
dis-
the influence
contributes
the resistance
increases
as high as 30% can be observed A line scan, crossing
clearly
of the dendrite
of the
to the disagree-
and experiment.
of the tip.
tion of the tip.
between
are in the opposite
this is not the case for a dendrite
in the Flemings
The combination
approximation.
But the differences
the 15 at.% Rh alloy.
for the 1.5 and 4 at.% Rh alloys
indicates
of the solute distribution
an oscillation
to the
concentration.
depending
in our samples,
the dendrite
was established
of the material
with the rhodium
on the posi-
arms and the interdendritic
of the hardness
value
(Fig. 4).
A man
by this method.
dendrite
Fig. 4. vickers hardness variation along a line crossing the interdendritic regions. 15 at.% Rh alloy.
A more precise EDXRF.
Figure
isoconcentration with
description
of this distribution
5 shows simultaneously lines.
Scanning
the scanning
Auger microscopy
of
the dendrites
arms and
the solute was obtained
electron
microscopy
at low magnification
by
and the agrees
these results.
Among
the three methods
the microindentation surface
and better
used to characterize
is the least sensitive represents
the solidification
to the preparation
the bulk mechanical
properties
structures,
procedure
of the
of the samples.
232
Fig. 5. Scanning electron microscopy of a dendrite in 8.15 at.% Rh alloy, face lines obtained by EDXRF are represent ed simulta(111). The isoconcentration neously.
CONCLUSIONS The copper-rhodium
system presents
constitutional
supercooling
solidification
structures
8.75 and 15 at.%. a drastic vations
To prevent
structure
the validity
Microindentation,
the absence
of structures
rate is required. models
dendritic
of 1.5, 4,
in the dilute
alloys,
The experimental
obser-
predicting
Auger microscopy
the conditions
and electron
the solute distribution
of the samples
This problem
of homogenization
the error induced
of the interdiffusion diffusion
homogenization Another
concentrations
of
microprobe
analysis
that is in agreement
with the
model.
The homogenization
rhodium
the formation
of existing
scanning
to characterize
cult to model.
timate
at rhodium
range where
conditions,
formation.
are useful Flemings
concentration
In our experimental
were observed
drop of the solidification
confirm
an extended
prevails.
error
by annealing
is mainly models
treatments
for dendritic
structures.
by the use of the heterodiffusion
coefficient
behaviour
in the Flemings
is the determination
data and to
In order
coefficient
model, we compared
with that of the copper-nickel
time as high as 150% could be induced factor
is long and diffi-
due to the lack of diffusion
system.
the copperError in the
by the shortcoming.
of the diffusion
distance.
to es-
in place
233
ACKNOWLEDGEMENTS This
work was financially
(Grant 48.81)
and the
of the authors la Recherche
supported
like to thank the 'Institut
(MPD) would
dans 1'Industrie
The authors
by the North Atlantic
*Fends de la Recherche Fondamentale
are indebded
Organization One
pour 1'Encouragement
de
for three scholarships.
et 1'Agriculture' to P. Delcambe
Treaty
et Collective'.
and L. Binst for their technical
as-
sistance.
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