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Initiation and growth behavior of a small fatigue crack in nickel-base superalloy at elevated temperatures

机译:高温下镍基高温合金中小疲劳裂纹的萌生和生长行为

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Rotating bending fatigue tests were performed for nickel-base superalloy Inconel 718 at room temperature, 300 deg C, 500 deg C, and 600 deg C in air. The influence of temperature on the small fatigue crack behavior in the alloy was investigated. It has been found that the fatigue limit of a plain specimen is determined by the limiting stress for small crack growth and the fatigue strength is the long life region is higher at elevated temperatures than at room temperature, because the early growth of smal cracks is enormously suppressed at elevated temperatures. In the steadystate growth process, however, a crack grows faster at higher temperature due to the decrease of fatigue crack growth resistance. The small crack growth rate can be evaluated by the small crack growth law at both room and elevated temperatures.
机译:在室温,300摄氏度,500摄氏度和600摄氏度的空气中,对镍基高温合金Inconel 718进行了旋转弯曲疲劳测试。研究了温度对合金中小疲劳裂纹行为的影响。已经发现,普通试样的疲劳极限是由小裂纹扩展的极限应力决定的,疲劳强度是高温下的长寿命区域高于室温,这是因为小裂纹的早期扩展非常大。在高温下被抑制。但是,在稳态生长过程中,由于疲劳裂纹扩展阻力的降低,裂纹在较高的温度下增长更快。小裂纹扩展速率可以通过在室温和升高的温度下的小裂纹扩展定律来评估。

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