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RA-based fretting fatigue life prediction method of Ni-based single crystal superalloys

机译:基于Ni的单晶高温合金的RA基微动疲劳寿命预测方法

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摘要

Fretting fatigue damage can significantly reduce the service life of Ni-based single crystal (NBSX) superalloys turbine blades. In this work, we proposed a fretting fatigue life prediction method by considering cracking, wear and their mutual interaction. Specifically, a parameter, denoted as RA, is developed with combination of Resolved shear stress based damage factor and Accumulated dissipated energy based damage factor, by which the contribution from cracking and wear are described respectively. The proposed method is validated with experimental data in the literature. Finite element analyses are performed to study the distribution of stresses and strains. Results show that the predicted crack initiation site, failure plane and life cycles are consistent with the experimental results.
机译:微动疲劳损坏可以显着降低基于NI的单晶(NBSX)超合金涡轮叶片的使用寿命。 在这项工作中,我们通过考虑开裂,磨损和相互互动来提出疲劳寿命预测方法。 具体地,表示为Ra的参数是用基于分辨的剪切应力的损伤因子和积累的散射能量的损伤系数进行开发,分别描述了裂缝和磨损的贡献。 该方法用文献中的实验数据验证。 进行有限元分析以研究应力和菌株的分布。 结果表明,预测的裂缝启动位点,失效平面和生命周期与实验结果一致。

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