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.

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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.

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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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