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EXPERIMENTAL INVESTIGATION AND LIFE PREDICTION FOR DEFECT INDUCED CRACK OF A P/M NICKEL BASED SUPERALLOY

  • Beihang University
  • Shanghai Jiao Tong University
  • Chengdu Holy Industry and Commerce Corp. LTD (GROUP)
  • Civil Aviation Flight University of China

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper presents the effect of natural and artificial defects on fatigue life of FGH96 at 600°C. The artificial defects were machined by EDM (electron discharge maching) technique. First the fractography of specimens were examined by SEM to obtain defect size and analyse the failure process. Since defects were the fatigue source and a fracture mechanic-based life prediction model was proposed. The shape of natural defects is irregular and the concept of effective area proposed by Murakami was applied. The corresponding maximum K calculation was modified by considering the influence of shape ratio. The small crack growth behaviour was also considered and by integrating the rate equation with initial defect size, and good life prediction was obtained for both two kinds of surface defect.

源语言英语
主期刊名32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
出版商International Council of the Aeronautical Sciences
ISBN(电子版)9783932182914
出版状态已出版 - 2021
活动32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 - Shanghai, 中国
期限: 6 9月 202110 9月 2021

出版系列

姓名32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021

会议

会议32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
国家/地区中国
Shanghai
时期6/09/2110/09/21

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