Fatigue crack growth behavior of X2095 Al-Li alloy

被引:34
作者
Chen, DL [1 ]
Chaturvedi, MC
Goel, N
Richards, NL
机构
[1] Univ Manitoba, Dept Mech & Ind Engn, Winnipeg, MB R3T 5V6, Canada
[2] Bristol Aerosp Ltd, Winnipeg, MB R3C 2S4, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
aluminum-lithium alloys; metal-matrix composites; texture; fatigue crack propagation; fatigue threshold; crack closure; stress ratio effect;
D O I
10.1016/S0142-1123(99)00087-0
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Microstructures and micro-textures of X2095 Al-Li alloy in as-received/superplastic state were characterized by means of SEM/BDS, X-ray diffraction and orientation imaging microscopy (OIM). It was observed that the microstructure of the alloy was typical of a particulate-reinforced composite material, consisting of aluminum matrix and homogeneously distributed T-B(Al7Cu4Li) particles with a volume fraction of about 10%. Brass-type texture was the dominant texture component. Both constant amplitude and near-threshold fatigue crack growth rates of the alloy in the L-T and T-L orientations were determined at different stress ratios. Particular attention was paid to the role of the T-B phase in the fatigue crack growth. When a fatigue crack approached a T-B particle, the crack basically meandered to avoid the particle. The T-B particles thus provided a strong resistance to the propagation of fatigue crack by promoting crack deflection and the related crack closure effects. The fatigue crack propagation behavior has been explained by the microstructural features, micro-textures, cracking characteristics and crack closure effects. (C) 1999 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1079 / 1086
页数:8
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