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摘要:
Multiaxial fatigue behavior of superalloy GH4169 was investigated by using the thin tubular multiaxial fatigue specimens under proportional and non-proportional loadings at high temperature. The relationship between the cyclic stress response and the cyclic number was studied by recording the experimental data. The experimental results showed that the fatigue life was decreased under non-proportional loading. In the entire fatigue process, the torsional stress response always showed the cyclic softening. The characteristics of cyclic hardening or softening for tensional stress response depended on the strain loading paths and the loading parameters. With the cyclic number increase, the creep phenomenon was gradually showed under multiaxial loading at high temperature.
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来源 :
Journal of Aeronautical Materials
ISSN: 1005-5053
年份: 2006
期: 6
卷: 26
页码: 6-11