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首页> 外文期刊>International Journal of Fatigue >Fatigue crack initiation and short crack growth in nickel-base turbine disc alloys--the effects of microstructure and operating parameters
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Fatigue crack initiation and short crack growth in nickel-base turbine disc alloys--the effects of microstructure and operating parameters

机译:镍基涡轮盘合金的疲劳裂纹萌生和短裂纹扩展-组织和工作参数的影响

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摘要

An assessment of the effects of microstructure and operating parameters on both crack initiation and propagation of short fatigue cracks is presented. The assessment was carried out on RR1000, U720Li and microstructural variants of U720Li. Fatigue tests were carried out at room temperature (20 Hz sinusoidal cycling) and at 650 deg C (1-1-1-1 trapezoidal cycling). Comparisons of the performance of the different microstructures revealed that initiation occurred predominantly at pores at both temperatures. At room temperature, stage I crack growth predominated and the presence of large primary gamma' precipitates on the grain boundaries, larger grains and larger coherent gamma' sizes gave improved fatigue crack growth resistance, whereas at 650 deg C, larger grains gave the most significant performance benefits.
机译:提出了对微观结构和操作参数对裂纹萌生和短疲劳裂纹扩展的影响的评估。对RR1000,U720Li和U720Li的微结构变体进行了评估。在室温(20 Hz正弦循环)和650摄氏度(1-1-1-1梯形循环)下进行疲劳测试。对不同微观结构的性能进行比较后发现,引发主要发生在两个温度的孔中。在室温下,第一阶段的裂纹扩展占主导地位,并且在晶界上存在较大的初级γ'析出物,较大的晶粒和较大的相干γ'尺寸可改善疲劳裂纹扩展性,而在650℃时,较大的晶粒表现出最大的疲劳裂纹扩展性能优势。

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