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

机译:电子束熔化制备高强度高温合金的保疲劳裂纹扩展行为

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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:为了证明用于关键涡轮发动机部件的增材制造超级合金的可靠性,需要模拟使用条件的动态测试。本研究旨在研究通过电子束熔化(EBM)制造的IN718的保质疲劳裂纹扩展行为。当加载轴平行于柱状晶粒并垂直于柱状晶粒排列时,EBM IN718的织构和柱状晶粒组织显示出各向异性的疲劳疲劳开裂性能。高角和低角晶界与驻留疲劳裂纹路径的相互作用不同。还讨论了不同热处理对开裂行为的影响。将EBM IN718的疲劳疲劳裂纹扩展速率与锻造的IN718在疲劳疲劳测试条件和纯疲劳测试条件下进行了比较。示出并讨论了EBM IN718的耐疲劳疲劳开裂性能优于锻造的IN718。

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