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Testing and evaluation for fatigue crack propagation of Ti-6Al-4V/ELI and 7050-T7452 alloys at high temperatures

  • Beihang University
  • Beijing Institute of Aeronautical Materials

Research output: Contribution to journalArticlepeer-review

Abstract

This paper seeks to evaluate crack propagation properties and residual lives of metallic alloys subjected to fatigue loading at room and high temperatures. Fatigue crack growth tests were performed on Ti-6Al-4V/ELI and 7050-T7452 subjected to constant-amplitude and actual random-spectra loading at room temperature of about 25 °C and at high temperatures of 250 °C and 150 °C to determine their crack growth properties and residual lives. The damage mode and mechanisms at high temperature were compared with those at room temperature on the basis of the results of fractographic analysis. Temperature-dependent residual lives under actual random-spectra load history were evaluated based on a modified accumulation damage rule accounting for the load interaction. Good correlation was achieved between the predictions and actual experiments, demonstrating the practical and effective use of the proposed method.

Original languageEnglish
Pages (from-to)1388-1398
Number of pages11
JournalChinese Journal of Aeronautics
Volume31
Issue number6
DOIs
StatePublished - Jun 2018

Keywords

  • Crack growth
  • Fatigue
  • High temperature
  • Metallic alloy
  • Residual life

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