Characterization of fatigue behavior of Al-Li alloy 2099

被引:19
作者
Cisko, A. R. [1 ]
Jordon, J. B. [1 ]
Avery, D. Z. [1 ]
McClelland, Z. B. [2 ]
Liu, T. [3 ]
Rushing, T. W. [2 ]
Brewer, L. N. [3 ]
Allison, P. G. [1 ]
Garcia, L. [2 ]
机构
[1] Univ Alabama, Dept Mech Engn, Tuscaloosa, AL 35487 USA
[2] US Army, Geotech & Struct Lab, Res & Dev Ctr, Vicksburg, MS USA
[3] Univ Alabama, Dept Met Engn, Tuscaloosa, AL 35487 USA
关键词
CRACK-GROWTH; STRESS; PRECIPITATION;
D O I
10.1016/j.matchar.2019.03.026
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Experiments and modeling were performed to quantify the microstructure-fatigue properties relationship of wrought aluminum-lithium alloy 2099 (AA2099) plate. Microstructural morphology was examined via optical microscopy, SEM, and TEM techniques. The mechanical properties were determined through monotonic tensile and fully reversed fatigue testing. The rolled AA2099 was shown to have large elongated columnar grains several millimeters long. Metastable secondary phases, T-1 and delta', were observed and provided strength to the material. Fractography determined fatigue cracks initiate from copper-rich constituent particles. These particles ranged from 1 to 25 pm in size, with an average size of 12 pm. The size of these intermetallic Cu-rich particles influenced the fatigue life of AA2099. Lastly, a microstructure-sensitive fatigue model was used to correlate the various effects of intermetallic particle sizes on the fatigue life of AA2099.
引用
收藏
页码:496 / 505
页数:10
相关论文
共 44 条
  • [1] Modelling and experimental study of fatigue of powder metal steel (FC-0205)
    Allison, P. G.
    Hammi, Y.
    Jordon, J. B.
    Horstemeyer, M. F.
    [J]. POWDER METALLURGY, 2013, 56 (05) : 388 - 396
  • [2] [Anonymous], 2000, J ENG MATER-T ASME, DOI DOI 10.1115/1.3225026
  • [3] Modelling of anisotropy for Al-Li 2099 T83 extrusions and effect of precipitate density
    Bois-Brochu, Alexandre
    Blais, Carl
    Goma, Franck Armel Tchitembo
    Larouche, Daniel
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2016, 673 : 581 - 586
  • [4] Chen D. L., 2000, NEAR THRESHOLD FATIG, V31
  • [5] Combinative hardening effects of precipitation in a commercial aged Al-Cu-Li-X alloy
    Chen, Zhongwei
    Zhao, Kai
    Fan, Li
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2013, 588 : 59 - 64
  • [6] Cisko A., 2015, ASME INT MECH ENG C, V14
  • [7] The influence of precipitation on plastic deformation of Al-Cu-Li alloys
    Deschamps, A.
    Decreus, B.
    De Geuser, F.
    Dorin, T.
    Weyland, M.
    [J]. ACTA MATERIALIA, 2013, 61 (11) : 4010 - 4021
  • [8] Strengthening mechanisms of T1 precipitates and their influence on the plasticity of an Al-Cu-Li alloy
    Dorin, Thomas
    De Geuser, Frederic
    Lefebvre, Williams
    Sigli, Christophe
    Deschamps, Alexis
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2014, 605 : 119 - 126
  • [9] Stress-corrosion cracking characterisation of the advanced aerospace Al-Li 2099-T86 alloy
    Goebel, J.
    Ghidini, T.
    Graham, A. J.
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2016, 673 : 16 - 23
  • [10] Fatigue crack growth and delamination behaviours of advanced Al-Li alloy laminate under single tensile overload
    Huang, Y.
    Liu, J. Z.
    Huang, X.
    Zhang, J. Z.
    Yue, G. Q.
    [J]. FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2016, 39 (01) : 47 - 56