long-term self-annealing of copper and aluminium processed by high-pressure torsion
TRANSCRIPT
ULTRAFINEGRAINED MATERIALS
Long-term self-annealing of copper and aluminium processedby high-pressure torsion
Alexander P. Zhilyaev • Terence G. Langdon
Received: 29 January 2014 / Accepted: 27 March 2014
� Springer Science+Business Media New York 2014
Abstract High-pressure torsion (HPT) is recognized as
the most effective method for producing ultrafine-grained
and even nanocrystalline structures in metallic systems.
Although there are many reports on microstructural
refinement of pure metals and metallic alloys, several
important problems remain unresolved. For example, more
information is needed on the homogeneity of the processed
microstructure and on the heat release and temperature rise
during HPT processing. Recently, there were reports of
hardening in HPT-processed pure metals under conditions
of self-annealing. This report presents new experimental
data on the relaxation processes in HPT copper and alu-
minium processed at room temperature under loads of 6.0
and 1.0 GPa for zero and one turn. The experimental
results were obtained using X-ray diffraction and by
measuring the average Vickers microhardness after ageing.
Introduction
The thermal stability of materials processed by severe
plastic deformation (SPD) was a significant concern from
the first experiments in SPD processing, but it becomes of
paramount importance if the materials are tested at
elevated temperatures. These possible limitations on SPD
processing are addressed most readily by examining the
thermal stabilities of the ultrafine-grained (UFG) micro-
structures after processing using high-pressure torsion
(HPT) [1, 2] where HPT was selected because it is the
optimum procedure for achieving exceptional grain
refinement to the submicrometer or even the nanometer
level [3, 4].
An early report on thermostability described experi-
ments on Cu processed by HPT to give grain sizes of
*114 nm [5]. In these experiments, the densities of the
lattice dislocations were estimated from X-ray diffraction
(XRD) as *1014 m-2 and a series of annealing experi-
ments showed that the onset of grain growth began at
temperatures above *175 �C. These results were sup-
ported by differential scanning calorimetry using a heating
rate of 10 K min-1 where the onset of an exothermic peak
in the UFG Cu was detected at *120 �C [5]. The enthalpy
values were equal to *0.26 for the Cu sample, and the
annealing results were further confirmed by taking mea-
surements of the electrical resistance and the microhard-
ness where thermal stability was also evident up to
temperatures of *175 �C for HPT Cu. Later, the thermo-
stability of HPT copper was investigated as a function of
the numbers of whole revolutions applied to the material,
and in these experiments the temperatures for the onset of
recovery and grain growth were estimated as *180 �C [6].
Similar observations were also reported for HPT copper
using a pressure of 8 GPa and rotation through three turns
where there was a microhardness level of *150 MPa and a
crystallite size of *0.2 lm with high dislocation density of
*4 9 1015 m-2 [7]. Annealing at temperatures of 134,
269 and 405 �C for 1 h resulted in a monotonic decrease in
the microhardness and the dislocation density, and a cor-
responding increase in the crystallite size.
A. P. Zhilyaev (&) � T. G. Langdon
Materials Research Group, Faculty of Engineering and the
Environment, University of Southampton,
Southampton SO17 1BJ, UK
e-mail: [email protected]; [email protected]
A. P. Zhilyaev
Institute for Metals Superplasticity Problems, Khalturina 39,
Ufa 450001, Russia
123
J Mater Sci
DOI 10.1007/s10853-014-8208-1
At the same time, there exist some controversies con-
cerning the microhardness evolution during low-tempera-
ture annealing of HPT copper. Thus, there is a report of a
slight increase in the microhardness of HPT Cu after
annealing at low temperatures, and this was explained by the
formation of di-vacancies during low-temperature annealing
because of the abundance of vacancies in HPT copper [8].
Thus, the concentration of vacancies may be as high as the
value at the melting point (C1V & 1.5–3.0 9 10-4 [9]) or
even higher. The slight increase in the microhardness during
low-temperature annealing is supported by recent data where
there was a 5 % increase of Hv in commercial-purity copper
deformed by HPT and annealed at 100 �C for 1 h [10].
Room-temperature annealing of copper by electron back-
scattered diffraction after cryo-rolling has revealed abnor-
mal grain growth which was detected after natural ageing
over a period of 1.5 years [11]. Even in high melting point
materials, such as Ni–20 % Cr alloy, natural ageing over
7.5 years yielded a mean grain size which was reduced by
*30 % [12].
It is apparent from this brief overview that natural
ageing of the heavily deformed pure metals may invoke
relaxation processes including vacancy and dislocation
annihilation plus recrystallization and grain growth.
Accordingly, the aim of the present investigation was to
monitor the evolution in the Vickers microhardness, Hv,
and to use XRD to measure the evolution of appropriate
microstructural parameters including the lattice parameter,
a: the crystallite size, d: and the microstrain, he2i1/2. The
experiments were conducted on copper and aluminium of
commercial purity subjected either to compression under
an applied pressure for 1 min without torsional straining,
equivalent to N = 0 where N is the number of turns, or to
torsional straining under an applied pressure through
N = 1 turn. These parameters were monitored for periods
of time corresponding to 1, 12, 24, 48 and 96 h after HPT
processing.
Experimental materials and procedures
Disks of commercial-purity aluminium and copper were
obtained from Goodfellow Cambridge Ltd. (Huntingdon,
UK). The typical chemical compositions were given as (in
ppm) for copper: Ag 500, Bi \10, Pb \50, O 400, and
other metals \300; and for aluminium: Cu \500, Fe
\4000, Mn \500, Si \3000, and Zn \1000. Before HPT
processing, the aluminium and copper were annealed for
1 h at 650 and 950 �C, respectively. Measurements showed
that the initial Vickers microhardness values were
Hv & 18 for the annealed aluminium, and Hv & 40 for the
annealed Cu, and these values are in good agreement with
those reported in the literature. As in Fig. 1, X-ray analysis
showed that the full width at the half maximum (FWHM)
of the (111) peaks of the annealed Al and Cu specimens
are very close to that determined from the standard which
was used for measuring an instrumental broadening of
*0.06�.
The HPT specimens were cut in the form of disks having
diameters of 10 mm and thicknesses of about 1 mm. These
disks were processed at room temperature by HPT under
two different conditions. First, disks were held for 1 min
without torsional straining at an applied pressure, P, of
either 1.0 or 6.0 GPa for the aluminium and copper sam-
ples, respectively: this condition is henceforth designated
the samples where N = 0. Second, disks were held under
the same applied pressures and subjected to torsional
straining for one turn using a rotation speed of 1 rpm: these
samples are henceforth designated N = 1. The processing
was conducted under quasi-constrained conditions where
there is a small outflow of material between the two anvils
around the periphery of each disk during the processing
[13, 14]. In order to check on the increase in the temper-
ature during HPT, the temperature was monitored for
copper strained to a total of N = 10 turns under a pressure
of P = 6.0 GPa, and the result is shown in Fig. 2. It is
readily apparent from this plot that the temperature for the
HPT copper samples used in this investigation was below
30 �C after one revolution.
The microhardness was measured along two diameters
of all HPT disks with distances of 0.5 mm between each
indentation. These measurements were taken using a Ma-
tsuzawa Seiki MHT-1 microhardness tester equipped with
a Vickers indenter. The Hv values were recorded under
loads of 50 and 100 gf for aluminium and copper,
respectively, with the same dwell time of 15 s used for
both materials. A typical Hv profile for HPT copper pro-
cessed through one turn is shown in Fig. 3 where the
dashed line denotes the average microhardness value
obtained by averaging all the points along the two
diameters.
The analyses by XRD were undertaken using
a Bruker D2 Phaser instrument with Cu radiation
(Ka1 = 1.54060 A) and a Ni monochromator with a 1D
LYNXEYE detector. The scan step was 0.02�, and the
delay time was 2.5 s. A Rietveld analysis using MAUD
software [12] was performed in order to monitor the lattice
parameter, a; the microcrystallite size, d; and the micro-
strain he2i1/2. An example of fitted experimental and cal-
culated X-ray profiles is given in Fig. 4 where it is evident
that the calculated curve is in good agreement with the
experimental points.
Microhardness measurements and XRD analysis were
performed on the Al and Cu specimens after keeping the
disks at room temperature for periods of time of 1, 12, 24,
36, 48 and 96 h after HPT processing.
J Mater Sci
123
Experimental results
In order to investigate the effect of room-temperature
ageing, Fig. 5 shows the evolution of the average mi-
crohardness for (a) aluminium and (b) copper as a function
of the ageing time after HPT processing. In Fig. 5a for
aluminium, the errors bars are large, but there is a trend for
a small increase in the microhardness for Al specimens
after ageing for 24 h for the HPT disk processed by N = 1
turn and for 36 h for the disk subjected to compression
without torsional straining. It is necessary to note, however,
that this tendency lies within the range of the experimental
error. The situation is more complicated with the HPT
copper samples shown in Fig. 5b where there is an increase
in hardness after 12 h for the disk processed through one
turn. By contrast, there is no similar increase for the sample
processed in compression without torsional straining, and
instead the microhardness values decrease smoothly as a
function of the time of ageing. In the case of the copper
samples, the experimental data appear to be more reliable
because the error bars do not overlap over the whole range
of data.
0
100
200
300
400
500
Inte
nsity
(C
ount
s), 1
03
Inte
nsity
(C
ount
s), 1
03
2θ (°)38.2 38.4 38.6 38.8 39.0 43.2 43.4 43.6 43.8 44.0
0
50
100
150
200
2θ (°)
(a) (b)
Fig. 1 (111) Peak of annealed samples: a aluminium (FWHM = 0.07�), and b copper (FWHM = 0.08�)
0 2 4 6 8 1020
25
30
35
40
45
50
55
60
T (
°C)
Time (min) or N
P=6 GPa1 rpm
294
300
306
312
318
324
330
336
342
348
T (
K)
Fig. 2 Temperature as a function of number revolution for copper
processed at load of 6 GPa. Note: readings were taken from the
thermocouple located at 7 mm above the surface of upper anvil
-6 -4 -2 0 2 4 610
20
30
40
50
60
70
Average Hv=52.3±1.9
Hv
Distance (mm)
Fig. 3 Typical microhardness profile for HPT aluminium. Dashed
line denotes average Hv value
Fig. 4 An example of Rietveld refinement for copper samples
(P = 6 GPa, N = 0, 1 min)
J Mater Sci
123
Figure 6 depicts the values of the lattice parameters for
HPT aluminium in Fig. 6a and for HPT copper in Fig. 6b.
For the aluminium specimens, there are no significant
changes in the lattice constant with time. As shown in
Fig. 6a, the values of the lattice constant for the compressed
sample with N = 0 and the HPT specimen with N = 1 turn
both lie above the lattice parameter recorded in the litera-
ture where a = 4.0494 A [16]: this value is shown as a red
line in Fig. 6a. For the copper specimens, the situation is
again more complicated. For the compressed sample where
N = 0, the lattice constant is initially deflected but ulti-
mately comes to a final value of *3.63 A. By contrast, the
lattice parameter for the sample with N = 1 has a small
minimum after 36 h of ageing, and the relevant value is then
very close to the lattice constant given in the literature
where a = 3.6150 A [17]. In practice, however, the values
of the lattice parameters for both the samples are consis-
tently above this reported value, and this is due to the use of
a material having only commercial purity.
Similar variations are found also for the crystallite size
and the microstrain. Figure 7 shows the crystallite sizes of
(a) HPT aluminium and (b) HPT copper as a function of the
ageing time. For the compressed Al disk where N = 0, the
measurements show rapid deflections, and these changes
appear to have little or no correlation with the
microhardness evolution shown in Fig. 5a. Nevertheless,
the crystallite size of the HPT aluminium where N = 1 turn
appears to reasonably follow the microhardness trend, and
it slightly changes after 13 h of ageing. For the compressed
copper sample shown in Fig. 7b for N = 0, the crystallite
size correlates reasonably with the change in the lattice
parameter in Fig. 6b, but there appears to be no similar
correlation with the microhardness evolution in Fig. 5b.
Conversely, the Cu sample strained for N = 1 turn shows a
constant crystallite size of *120 nm which correlates
directly with the lattice constant in Fig. 6b but not with the
average microhardness in Fig. 5b.
The values of the measured microstrains are shown in
Fig. 8 for (a) HPT aluminium and (b) HPT copper. For the
compressed Al disk with N = 0, the evolution is the
inverse of the crystallite size, but there is a clear correlation
with the average microhardness in Fig. 5a. For the alu-
minium sample strained to one whole turn, the microstrain
initially increases but thereafter it decreases after about
36 h of ageing. For the copper samples in Fig. 8b, the
microstrain for the N = 0 sample increases with the
increasing ageing time, but for the HPT processed sample
where N = 1 turn there is a gradual decrease in the mi-
crostrain which correlates well with the average microh-
ardness in Fig. 5b.
0 10 20 30 40 50 60 70 80 90 10040
45
50
55
60
N=0N=1
Ave
rage
Hv
Time (h)
P=1 GPa
0 10 20 30 40 50 60 70 80 90 100100
110
120
130
140
P=6 GPaN=0N=1
Ave
rage
Hv
Time (h)
(a) (b)
Fig. 5 Average microhardness, Hv, for HPT samples: a aluminium, and b copper
0 20 40 60 80 1004.03
4.04
4.05
4.06
4.07
4.08
Latti
ce p
aram
eter
(Å
)
Time (h)
N=0N=1
P= 1 GPa
0 20 40 60 80 1003.60
3.61
3.62
3.63
3.64
3.65
Latti
ce p
aram
eter
(Å
)Time (h)
N=0N=1
P= 6 GPa
(a) (b)Fig. 6 Lattice parameter of
HPT samples: a aluminium, and
b copper
J Mater Sci
123
Discussion
All the above results, when considered together, show that
there are significant changes both in the microhardness
values and in the values of various microstructural
parameters in samples of aluminium and copper during
self-annealing at room temperature. It is also apparent that
more definitive studies are now required in order to obtain
closer correlations between the various effects that have
been recorded over relatively short self-annealing times of
up to a maximum of 96 h. It is appropriate to consider the
effect of self-annealing on each measured parameter.
Effect of self-annealing on microhardness
To some extent, there is a trend of a small increase in the
average microhardness after ageing for 12–24 h for alu-
minium, and copper samples strained for one whole turn
(Fig. 5). For the specimens subjected only to compression
with N = 0, there is a little or no increase in the average
microhardness. An unambiguous interpretation comes from
the fact that different areas of the HPT disks are strained to
different amounts, and therefore they have distinctive
recovery rates. This is evident from a set of Hv profiles for the
Al samples strained for one whole turn under a pressure of
1.0 GPa as shown in Fig. 9, where the profiles were taken
after ageing times of 1, 12, 24, 36 and 96 h. It is clear that the
recovery rate is the highest in the centre of the disk. Spe-
cifically, the microhardness in the centre measured after 96 h
of ageing is two times lower than that in the freshly processed
sample. This is an interesting result because in high-purity
aluminium subjected to HPT it was shown that the recovery
process is the highest at the periphery of the disk [18]. The
0 20 40 60 80 1000.2
0.4
0.6
0.8
Cry
stal
lite
size
(µ
m)
Time (h)
N=0N=1
P= 1 GPa
0 20 40 60 80 1000.1
0.2
0.3
0.4
Cry
stal
lite
size
(µ
m)
Time (h)
N=0N=1
P= 6 GPa
(a) (b)Fig. 7 Crystallite size of HPT
samples: a aluminium, and
b copper
0 20 40 60 80 1000.1
0.2
0.3
0.4
0.5
0.6
Mic
rost
rain
, 10
-3
Time (h)
N=0N=1
P=1 GPa
0 20 40 60 80 1000.2
0.3
0.4
0.5
0.6
Mic
rost
rain
, 10
-3
Time (h)
N=0N=1
P=6 GPa
(a) (b)Fig. 8 Microstrain of HPT
samples: a aluminium, and
b copper
-6 -4 -2 0 2 4 630
40
50
60
70
80
Time 96 h: Hv=52.8±1.0
Time 36 h: Hv=53.8±0.7Time 24 h: Hv=55.7±0.5
Time 12 h: Hv=55.3±0.7
Ave
rage
Hv
Distance (mm)
Time 1 h: Hv=53.4±0.7
Fig. 9 Detailed Hv profiles for HPT-strained aluminium (N = 1) as a
function of ageing time
J Mater Sci
123
difference in these results demonstrates the effect of the
purity level in controlling the recovery behaviour.
Effect of self-annealing on lattice parameters
The evolution in the lattice constant may reflect the level of
impurities or the presence of bi- and tri- vacancies in the
metal matrix. The level of vacancies estimated in HPT
copper by measuring the retained electroresistivity can be
comparable with or even higher than the vacancy concen-
tration near the melting point. The change in lattice
parameter as a function of vacancy and interstitials con-
centration is given as [19]
Da
a0
¼ C � ðv1 þ viÞ3 � X ;
where Da = (a - a0) is the change in the lattice parameter
in which a0 is due to the presence of vacancies and inter-
stitials in the matrix, C is their concentration, v1 and vi are
the vacancy and interstitial relaxation volumes, respec-
tively, and X is the atomic volume. The relaxation volume
of vacancies is always negative (thus, -6.6 A3 for alu-
minium and -3.5 A3 for copper [20]), and the sign of the
relaxation volume of the interstitials depends on the ionic
radius of the elements. This means that the change in the
lattice constant represents an interplay between the con-
centrations of vacancies and the concentration of intersti-
tials in the lattice. If the concentration of interstitials
remains unchanged then the lattice constant should
decrease with the annealing time, but this was not observed
for the strained metals where N = 1 turn. In practice, the
lattice constants of aluminium and copper determined in
this investigation are higher than those in the literature [16,
17] due to the presence of impurities in these commercial-
purity materials.
Effect of self-annealing on crystallite size
and microstrain
As indicated above, there is a small increase in microh-
ardness of HPT aluminium with N = 1 turn after ageing
for 12–24 h. However, the crystallite size in Fig. 7a and the
microstrain in Fig. 8a have corresponding maxima for the
same ageing condition. In order to explain the small
increase in the microhardness, it is possible to estimate the
dislocation density using the expression:
q ¼2ffiffiffi
3p� e2� �1=2
b � d ;
where b = 2.86 A is the Burgers vector [21] and d and
he2i1/2 are the crystallite size and microstrain, respectively.
The calculated dislocation density for HPT aluminium with
N = 1 as a function of ageing time is presented in Fig. 10.
Thus, the dislocation density is not high (*1013 m-2) and
decreases with ageing time such that there is a minimum at
a time of 36 h. More experiments will be needed to provide
a detailed explanation of these trends.
Summary and conclusions
(1) Samples of commercial-purity aluminium and cop-
per were processed by HPT and then aged for vari-
ous times at room temperature. A detailed analysis
was conducted using integrated XRD methods and
measurements of the average microhardness values.
(2) Aluminium and copper samples subjected only to
compression with no torsional straining (N = 0)
show no significant hardening, whereas for copper,
there is a continuously decreasing average microh-
ardness. After torsional straining through one turn,
there is noticeable hardening after ageing for
12–24 h. Integrated XRD analysis revealed no
significant correlation between microstructural
parameters (lattice constant, crystallite size and
microstrain) and increasing microhardness.
(3) Careful inspection of the microhardness profiles
along diameters of the disks showed that the
recovery rates are different in different positions on
the HPT disks. Specifically, the recovery was higher
at the centre of the disk than at the edge.
Acknowledgements This work was supported by the European
Research Council under ERC Grant Agreement number
267464-SPDMETALS.
0 20 40 60 80 1000.8
0.9
1.0
1.1
1.2
Dis
loca
tion
dens
ity (
m-2),
×10
13
Time (h)
Fig. 10 Calculated dislocation density for HPT Al strained for one
turn as a function of ageing time
J Mater Sci
123
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