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On the dwell-fatigue crack propagation behavior of a high strength superalloy manufactured by electron beam melting

机译:关于电子束熔融制造的高强度超合金的疲劳裂纹裂纹传播行为

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摘要

To demonstrate the reliability of additively manufactured superalloys for critical turbine engine components, dynamic tests simulating in-service condition are required. The present study aims to study the dwell-fatigue crack propagation behaviors of IN718 manufactured via electron beam melting (EBM). The textured and columnar-grained microstructure of EBM IN718 shows anisotropic dwell-fatigue cracking resistance when loading axis is aligned parallel and perpendicular to the columnar grains. High and low angle grain boundaries interact differently with the dwell-fatigue cracking path. The effect of different heat treatments on the cracking behavior is also discussed. The dwell-fatigue crack propagation rate of EBM IN718 is compared with forged IN718 under both dwell-fatigue test condition and pure fatigue test condition. The superiority of dwell-fatigue cracking resistance of EBM IN718 to forged IN718 is shown and discussed.
机译:为了证明临界涡轮发动机部件的瘦性制造高温合金的可靠性,需要模拟局部条件的动态测试。本研究旨在研究通过电子束熔化(EBM)制造的IN718的耐疲劳裂纹传播行为。 EBM IN718的纹理和柱状颗粒显微组织显示了装载轴平行排列并垂直于柱状晶粒时的各向异性耐疲劳裂解性。高和低角度的晶界与耐疲劳裂化路径不同地相互作用。还讨论了不同热处理对裂化行为的影响。将EBM IN718的耐用疲劳裂纹裂纹扩展速率与耐用于疲劳试验条件和纯疲劳试验条件相比,与锻造。讨论并讨论了EBM IN718锻造的抗疲劳裂解性的优越性。

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