Effects of the exposure to moist air on crack-tip deformation and striation marking in a 7175 T7351 aluminum alloy

被引:0
作者
Saanouni, S. [1 ]
Henaff, G. [1 ]
Villechaise, P. [1 ]
Benoit, G. [1 ]
Billaudeau, T. [2 ]
de Araujo, M. [2 ]
Rousset, J. [2 ]
Bahsoun, H. [1 ]
机构
[1] ENSMA Univ Poitiers, CNRS, ISAE 3346, UPR,Prime Inst,Dept Phys & Mech Mat, Teleport 2-1 Ave Clement Ader, F-86961 Futuroscope, France
[2] Airframe Res & Technol, Airbus Operat SAS, 4 Rue Marius Terce, F-31060 St Martin Du Touch, France
关键词
Aluminum alloy; Fatigue striation; Moist air; Hydrogen; Lattice rotation; EBSD; FATIGUE BEHAVIOR; PROPAGATION; GROWTH; ENVIRONMENT; MECHANISMS; 7075-T651; HYDROGEN; VACUUM;
D O I
10.1016/j.mtla.2023.101753
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper investigates the effects of the exposure to moist air on the mechanisms of fatigue crack growth in 7175 T7351 aluminum alloy. A special attention is paid to the crack-tip deformation mechanisms, controlling the fatigue crack growth rate as well as the fatigue striation markings, firstly under moist air and at low loading frequency, corresponding to a high exposure rate, and then as compared to a low exposure rate condition obtained in an inert atmosphere. It is shown that a high exposure rate induces the development at the crack-tip of a 800 nm-thick surface layer, divided into subdomains characterized with a pronounced and highly localized lattice rotation. In contrast, under very low exposure rate, a significantly lower lattice rotation associated with a smoother gradient is observed. This suggests that the formation of subdomains at high exposure rate is actually induced by some environmental effect, presumably in relation with an assistance of hydrogen highly accumulated in a thin subsurface layer in the intense localization of crack-tip deformation resulting into lattice rotation. Finally, it is clearly established that fatigue striation spacing in moist air exactly coincides with the distance separating two successive subdomains exhibiting the highest lattice disorientation.
引用
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页数:10
相关论文
共 38 条
  • [1] Achter M.R., 1967, FATIGUE CRACK PROPAG, V415, P181
  • [2] Bowles C.Q., 1978, THESIS DELFT U TECHN
  • [3] FORMATION OF FATIGUE STRIATIONS
    BOWLES, CQ
    BROEK, D
    [J]. INTERNATIONAL JOURNAL OF FRACTURE MECHANICS, 1972, 8 (01): : 75 - 85
  • [4] BRADSHAW FJ, 1969, INT J FRACTURE, V5, P255
  • [5] Fatigue crack propagation of aerospace aluminum alloy 7075-T651 in high altitude environments
    Burns, J. T.
    Jones, J. J.
    Thompson, A. D.
    Locke, J. S.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2018, 106 : 196 - 207
  • [6] Effect of water vapor pressure on fatigue crack growth in Al-Zn-Cu-Mg over wide-range stress intensity factor loading
    Burns, J. T.
    Bush, R. W.
    Ai, J. H.
    Jones, J. L.
    Lee, Y.
    Gangloff, R. P.
    [J]. ENGINEERING FRACTURE MECHANICS, 2015, 137 : 34 - 55
  • [7] Gangloff R.P., 2002, FATIGUE 2002, P3401
  • [8] CHEMICAL AND METALLURGICAL ASPECTS OF ENVIRONMENTALLY ASSISTED FATIGUE CRACK-GROWTH IN 7075-T651 ALUMINUM-ALLOY
    GAO, M
    PAO, PS
    WEI, RP
    [J]. METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1988, 19 (07): : 1739 - 1750
  • [9] Fatigue mediated lattice rotation in Al alloys
    Goswami, R.
    Qadri, S. B.
    Pande, C. S.
    [J]. ACTA MATERIALIA, 2017, 129 : 33 - 40
  • [10] Effect of substrate strain on adsorption
    Gsell, M
    Jakob, P
    Menzel, D
    [J]. SCIENCE, 1998, 280 (5364) : 717 - 720