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Interaction of fatigue and creep in MAR-M247 superalloy

机译:疲劳和蠕变在MAR-M247超合金中的相互作用

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Lifetime of MAR-M 247 Ni-based superalloy was experimentally studied under high-frequency cyclic loading (120 Hz) with constant tensile mean stress σ_m = 300 MPa at temperature 900°C in air. The stress amplitude σ_a was changed in order to investigate the superalloy lifetime in a wide range of conditions, from pure creep to pure fatigue. The superposition of the stress amplitude on the mean stress does not influence the specimen lifetime until a threshold value is reached. Scanning electron microscopy was utilized for the fracture surface observation with the aim to identify the governing damage mechanisms for particular test conditions.
机译:在高频循环加载(120Hz)下实验研究MAR-M 247的Lifetime,在高温循环加载(120Hz)下,恒定拉伸平均应力σ_m= 300mPa在空气中温度900℃。 改变应力幅度σ_A以便在众多条件下研究超合金寿命,从纯粹的蠕变到纯疲劳。 在平均应力上的应力幅度的叠加不会影响样品寿命直到达到阈值。 扫描电子显微镜用于断裂表面观察,目的是识别特定测试条件的控制损伤机制。

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