High Temperature Deformation of Friction Stir Processed 7075
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Transcript of High Temperature Deformation of Friction Stir Processed 7075
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High temperature deformation of friction stir processed 7075
aluminium alloy
P. Cavalierea,*, A. Squillaceb
aDepartment of Ingegneria dellInnovazione, University of Lecce, Via per Arnesano I-73100 Lecce, ItalybDepartment of Materials and Production Engineering Faculty, University of Naples Federico II, Italy
Received 21 January 2005; received in revised form 18 April 2005; accepted 18 April 2005
Abstract
The mechanical and microstructural properties of 7075 aluminium alloy resulting from Friction Stir Processing (FSP), into
sheets of 7 mm thickness, were analysed in the present study. The sheets were processed perpendicularly to the rolling direction;
the tensile mechanical properties were evaluated at room temperature in the transverse and longitudinal directions with respect
to the processing one. Tensile tests were also performed at higher temperatures and different strain rates in the nugget zone, in
order to analyse the superplastic properties of the recrystallized material and to observe the differences from the parent material
as a function of the strong grain refinement due to the Friction Stir Process. The high temperature behaviour of the material was
studied, in the parallel direction, by means of tensile tests in the temperature and strain rate ranges of 150500 8C and 102
104 s1 respectively, electron microscopy (FEGSEM) observations were carried out to investigate more closely the fracture
surfaces of the specimens tested at different temperatures and strain rates.
D 2005 Elsevier B.V. All rights reserved.
Keywords: Friction stir processing; Microstructure evolution; Hot tensile tests; FEGSEM
1. Introduction
Friction Stir Welding (FSW) is being targeted bymodern industries for structurally demanding applica-
tions providing high-performance benefits [1]. FSW
has been shown to strongly decrease severe distortion
and residual stresses compared to the traditional weld-
ing processes[24].The Frictioned zone consists of a
weld nugget, a thermo-mechanically affected zoneand a heat affected zone. The process results in
obtaining a very fine and equiaxed grain structure in
the weld nugget causing a higher mechanical strength
and ductility[57].Jata and Semiatin[8]showed that
the microstructure in the weld nugget zone evolves
through a continuous dynamical recrystallization pro-
cess, the strong grain refinement produced by the
process leads the microstructure to the fine dimen-
1044-5803/$ - see front matterD 2005 Elsevier B.V. All rights reserved.
doi:10.1016/j.matchar.2005.04.007
* Corresponding author. Tel.: +39 832320324; fax: +39
832320349.
E-mail address: [email protected] (P. Cavaliere).
Materials Characterization 55 (2005) 136142
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The tensile response in the transverse direction of
the FSP 7075 aluminium alloy is shown inFig. 5.The
curve exhibits a classical behaviour; the mechanical
properties,compared to the parent metals, are reported
inTable 1.The material exhibits very good properties
of yield stress, UTS and ductility from a global point-
of-view even if the processed material exhibits a
lower 0.2% proof stress and elongation with respect
to the base metal, the mechanical results are very good
considering the drastic conditions to which the mate-
rial is subjected during the Friction Stir Process, the
elastic modulus results are very different with respect
to the parent material. All the specimens fractured in
the HAZ zones. This demonstrates the classical be-
haviour of this kind of material in which, from a
microstructural point-of-view, the mechanical re-
sponse of the centre is higher with respect to the
parent material and the HAZ because of the large
differences in grain dimensions. In this zone, in fact,
the mean grain equivalent diameter measured from
optical images was close to 4 Am.
The tensile response of the material was also in-vestigated by cutting small samples from the centre of
the samples. Such specimens were tested at room
temperature and higher temperatures up to 300 8C.
The room temperature tensile behaviour of the
material in the nugget zone is shown in Fig. 6. The
strength and ductility of the material increased strong-
ly in the nugget zone with respect to the material in
the transverse direction thanks to the uniform and very
fine structure consequent to the friction stir process.
The behaviour of the material at high temperatures
was studied by performing tensile tests in the temper-
ature range 150300 8C and 103 s1 strain rate. The
true stress vs. true strain response of the material is
shown in Fig. 7. The flow stress decreases with
increasing temperature and the strain to fracture
increases with increasing temperature up to very
high levels at 300 8C and 103 s1.
The very high strain to fracture values reached by
the studied material at high temperatures result in the
0.000 0.005 0.010 0.015 0.020 0.025 0.0300
50
100
150
200
250
300
350
400
7075 FSP 7mm
TrueStress[MPa
]
True Strain
Fig. 5. True stress vs. true strain tensile behaviour of the FSP sheets
perpendicularly to the processing direction.
Table 1
Mechanical properties in transverse direction of the FSP 7075 alloy
compared with the parent material
Material ry (MPa) UTS (MPa) Elongation (%)
7075 T6 524 587 11
7075 T6 FSP 325 (62%) 450 (77%) 7 (64%)
0.00 0.02 0.04 0.06 0.08 0.10 0.12 0.140
50
100
150
200
250
300
350
400
450
500
7075 FSP Nugget
y=355 MPa
TrueStress[MPa
]
True Strain
Fig. 6. True stress vs. true strain tensile behaviour of the FSP plates
parallel to the processing direction.
0.00 0.25 0.50 0.75 1.000
50
100
150
200
250
300
350
400
450
T=300 C
T=200C
T=150 C
T=25 C7075 FSP 7mm
10-3s
-1
TrueStress
[MPa]
True Strain
Fig. 7. True stress vs. true strain tensile curves at 103 s1 strain
rate at the lower temperatures investigated.
P. Cavaliere, A. Squillace / Materials Characterization 55 (2005) 136142 139
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very attractive superplastic behaviour exhibited by
such alloys after the Friction Stir Process.
Normally, to improve the formability leading to
superplastic properties for aluminium alloys belong-ing to the 7XXX series is complex involving overa-
ging and multiple warm rolling phases with re-heating
after each step and final forming at 104 s1 strain
rate. The widespread use of superplastic forming of
aluminium alloys is limited by the low optimum strain
rate for superplasticity. The possibility of obtaining a
material with a very fine and uniform grain structure
which could be directly formed in superplastic condi-
tions at lower strain rates results in a very useful tool
for the modern aerospace and automotive industries.
Considering that the material when tested in warmforming conditions exhibited high ductility, when the
deformation required for most forming operations is
lower (200%) the results are attractive also for normal
forging operations in which the high strength re-
quired is obtained thanks to the very fine starting
microstructure.
The results of hot tensile tests at different tempera-
tures and different strain rates are shown in Fig. 8.
There is no steady state exhibited by the curves for all
the temperatures and strain rates investigated; with
increasing temperature, the peak stress is shifted to
higher strains.
The flow stress as a function of the different strain
rates investigated in the temperature range 400500
8C is shown in Fig. 9, a sigmoidal relationship was
0.00 0.25 0.50 0.75 1.00 1.25 1.50 1.75 2.000
10
20
30
40
50
60
70
80
90
100
475 C
425 C
500 C
450 C
400 C
350 C
7075 FSP 7mm
10-3s
-1
TrueStress[M
Pa]
True Strain
0.0 0.5 1.0 1.5 2.0 2.50
5
10
15
20
25
30
35
40
5*10-4s-1
5*10-2s
-1
10-4s
-1
10-3s
-1
10-2s
-1
TrueStress[MPa]
True Strain
AA7075 FSP 500 C
(a)
(b)
Fig. 8. True stress vs. true strain tensile curves at 103 s1 strain
rate (a) and 500 8C (b) at the higher temperatures investigated.
1E-4 1E-3 0.01 0.1
10
100
AA7075 FSP Flow Stress
400 C
425 C450 C475 C500 C
FlowStress[MPa
]
Strain Rate [s-1]
Fig. 9. Flow stress behaviour as a function of strain rate calculated
in the superplastic regime exhibited by the FSP material.
1E-4 1E-3 0.01 0.1
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
400 C
425 C450 C475 C500 C
StrainRateSe
nsitivity[m]
Strain Rate [s-1]
Fig. 10. Strain rate sensitivity (m) variation as a function of strain
rate calculated in the superplastic regime exhibited by the FSP
material.
P. Cavaliere, A. Squillace / Materials Characterization 55 (2005) 136142140
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observed between stress and strain rate at high testing
temperatures. The strain rate sensitivity variation,
obtained by the hot tensile values at a true strain=1,
is shown in Fig. 10, the m value increases upon
increasing the strain rate from 104 s1 to 103
s1 and then decreases for the higher strain rates
investigated for all the temperatures chosen in thepresent study. The higher measured value (m =0.75)
was observed for a strain rate of 5*104 s1 at 500
8C; over the ranges 450500 8C and 5*104 s1 to
5*103 s1 temperature and strain rate respectively,
the Friction Stir Processed material exhibits superplas-
tic properties.
In the understanding of the microstructural effects
on fracture properties some FEGSEM observations
were performed on the fractured surfaces of the tested
samples.
The fracture surface of the FSP 7075 alloy tested intension in the longitudinal direction was covered with
a broad population of microscopic voids of different
Fig. 11. Fracture surface of the material tested perpendicularly to the
travelling direction showing voids due to the FS process.
Fig. 12. Microscopic voids observed in the specimen tested at 300
8C and 103 s1.
Fig. 13. Fracture surfaces of the specimens tested at 400 8C (a) and
500 8C (b) at 5*104 s1 strain rate.
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sizes and shapes (Fig. 11), at room temperature the
material showed some ductility with fracture, the
observations performed by employing FEGSEM
revealed local ductile mechanisms.Two different types of dimples were observed,
those immediately close to the voids and those asso-
ciated with the second phase coarse particles and
precipitates which were much smaller and shallower.
At the higher temperatures investigated, many dif-
ferent behaviours were observed in the material; at 300
8C many microscopic voids were observed on the
tensile fractured surfaces (Fig. 12a) around such
voids a broad population of very fine dimples were
recognized (Fig. 12b) for all the strain rates investigat-
ed. The fractographic analyses of the tensile testedsurfaces at higher temperatures (400 8C) revealed a
bimodal size distribution of dimples (Fig. 13a) and
the presence of some smooth zones, by increasing the
test temperature (500 8C) the size distribution of ductile
dimples became more uniform on all the observed
surfaces with a smaller and shallow aspect (Fig. 13b).
4. Conclusions
The 7075 aluminium alloy were successfully Fric-
tion Stir Processed in 7 mm thick sheets. The resultingmicrostructure was widely investigated by optical mi-
croscopy showing the grain structure differences
resulting by the process. The mechanical properties
of the material were evaluated by tensile tests in both
the longitudinal and transverse directions with respect
to the processing one resulting in retaining the high
mechanical properties with respect to the parent ma-
terial. The potential superplastic properties of the fric-
tion stirred material were evaluated by hot tensile tests
at different strain rates obtaining high values of the
strain rate sensitivity at the higher strain rates investi-gated in the present study. The fracture surfaces of the
specimens tested at different conditions of tempera-
tures and strain rates were extensively investigated by
using a FEGSEM microscope revealing the defects
resulting from the Friction process and the microscop-
ic mechanisms taking place during hot deformation.
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