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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

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publication32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
PublisherInternational Council of the Aeronautical Sciences
ISBN (Electronic)9783932182914
StatePublished - 2021
Event32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 - Shanghai, China
Duration: 6 Sep 202110 Sep 2021

Publication series

Name32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021

Conference

Conference32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
Country/TerritoryChina
CityShanghai
Period6/09/2110/09/21

Keywords

  • Defect
  • Fatigue life
  • Life prediction
  • Nickel-based superalloy
  • Small crack

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