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The influence of oxygen partial pressure on the crack propagation of superalloy under fatigue-creep-environment interaction

机译:氧分压对疲劳 - 蠕变环境相互作用下超合金裂纹繁殖的影响

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摘要

We elucidate here the effect of low oxygen partial pressure on the dwell fatigue crack growth rate (DFCGR) of 718Plus alloy at high temperature. In comparison under the air and vacuum conditions with lower oxygen partial pressure, the DFCGR of 718Plus alloy reduced by three orders of magnitude at 704°C at lower oxygen partial pressure than that of in air condition. By analysis of microstructure, oxide, and crack path under different conditions, it was considered that the oxygen-induced dynamic embrittlement (DE) was the dominant impact mechanism for fatigue crack propagation at high-temperature in 718Plus alloy. Meanwhile, the stress-accelerated grain boundary oxidation (SAGBO) mechanism also played a significant role, especially in the long step-wise period. In addition, the types of oxide formed in creep process were directly related to the oxygen partial pressure and oxidation time.
机译:我们阐明了低氧分压对高温下718pl合金疲劳裂纹生长速率(DFCGR)的影响。在空气和真空条件下具有较低氧分压的真空条件下,718plus合金的DFCGR在704℃下在较低的氧气部分压力下减少三个数量级,而不是空气条件。通过分析不同条件下的微观结构,氧化物和裂纹路径,认为氧诱导的动态脆化(DE)是718pl合金中高温疲劳裂纹繁殖的显性冲击机理。同时,应力加速的晶界氧化(SAGBO)机制也发挥了重要作用,特别是在长时间的期间。另外,在蠕变过程中形成的氧化物类型与氧分压和氧化时间直接相关。

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