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Proposal of a Thermo-Mechanical Fatigue Life Prediction Method of Nickel Based Superalloy IN738LC

机译:镍基高温合金IN738LC热机械疲劳寿命预测方法的建议

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摘要

New biaxial thermo-mechanical fatigue testing machine, which can perform thermo-mechanical fatigue (TMF) tests under any selected conditions of axial loading, torsional loading and temperature history with arbitrary amplitude and phase, was developed. TMF tests were performed under complicated axial/torsional loading and temperature waveform (Blade waveform) that simulates strain and temperature histories imposed in actual gas turbine blades, as well as fundamental in-phase and out-of-phase tests. Test temperature was selected between 450-850 deg C. In case of without strain hold, failure life of the out-of-phase is comparable to that of the Blade waveform, while failure life of the in-phase is longer than that of the out-of-phase and the Blade waveform due to occurrence of negative mean stress. On the other hand, the largest life reduction was observed in the in-phase condition by introducing 6 minutes strain hold at the maximum temperature. Thermo-mechanical fatigue lives under various conditions were well correlated to uniaxial isothermal fatigue data by the equivalent total strain range, DELTA epsilon_(eq) proposed in this study. Then, time dependent TMF life prediction model was proposed based on the nonlinear damage accumulation model incorporating with DELTA epsilon_(eq) and failure lives of the Blade waveform with strain hold were accurately predicted by the TMF life prediction model.
机译:开发了一种新型的双轴热机械疲劳试验机,该试验机可以在任意选定的轴向载荷,扭转载荷和温度历史的任意选定条件下,以任意幅度和相位进行热机械疲劳(TMF)测试。 TMF测试是在复杂的轴向/扭转载荷和温度波形(叶片波形)下进行的,该波形模拟了实际燃气轮机叶片施加的应变和温度历史,以及基本的同相和异相测试。测试温度选择在450-850摄氏度之间。在没有应变保持的情况下,异相的故障寿命与Blade波形的故障寿命相当,而同相的故障寿命则比刀片波形的寿命长。由于出现负平均应力而异相和叶片波形。另一方面,通过在最高温度下保持6分钟来保持应变,在同相条件下观察到最大的寿命降低。通过本研究提出的等效总应变范围DELTA epsilon_(eq),将各种条件下的热机械疲劳寿命与单轴等温疲劳数据很好地相关。然后,在非线性损伤累积模型的基础上,结合DELTA epsilon_(eq),提出了随时间变化的TMF寿命预测模型,并通过TMF寿命预测模型准确预测了具有应变保持的叶片波形的失效寿命。

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