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Small fatigue crack initiation and growth mechanisms of nickel-based superalloy GH4169 at 650 degrees C in air

机译:镍基高温合金GH4169在空气中650摄氏度时的小疲劳裂纹萌生和生长机理

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The aim of this paper is to identify the fatigue crack initiation and small crack growth mechanisms of GH4169 at 650 degrees C in air. Results show that fatigue cracks tend to initiate at oxidized inclusions. The crack incubation period takes up more than 90% of the fatigue lifetime. The delta phase can improve the crack initiation life and the total fatigue lifetime. The similarity between small crack and long crack growth data at relatively high Delta K can be attributed to the similarity of propagation mode. Two three-stage models are proposed to describe the cracks initiation and propagation processes. (C) 2015 Elsevier Ltd. All rights reserved.
机译:本文的目的是确定GH4169在空气中650摄氏度时的疲劳裂纹萌生和小裂纹扩展机制。结果表明,疲劳裂纹倾向于在氧化夹杂物处产生。裂纹的潜伏期占疲劳寿命的90%以上。 δ相可以改善裂纹萌生寿命和总疲劳寿命。在相对较高的Delta K下,小裂纹和长裂纹扩展数据之间的相似性可以归因于传播模式的相似性。提出了两个三阶段模型来描述裂纹的萌生和扩展过程。 (C)2015 Elsevier Ltd.保留所有权利。

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