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Thermomechanical fatigue experiment and failure analysis on a nickel-based superalloy turbine blade

  • Beijing Key Laboratory of Aero-Engine Structure and Strength
  • Collaborative Innovation Center of Advanced Aero-Engine
  • Aero Engine Corporation of China
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

Thermomechanical fatigue (TMF) experiment with dwell times on a nickel-based superalloy turbine blade was conducted. The strain field and temperature field of the test section were simulated well through adjusting gripping fixture and induction coil. In addition to the loading, heating, cooling and control subsystems, high temperature strain measurement subsystem was introduced into the experiment to ensure the accuracy of the simulation results of service condition for the test section. In the whole experiment, the service condition of the test section was reproduced. The experiment result showed that TMF crack initiated at the trailing edge of the test section and propagated along the leading edge direction. Using the scanning electron microscope (SEM), multiple crack sources at the surface of turbine blade were observed and the crack surface was oxidized seriously. In addition, based on the fractographic and metallographic observation, the mixed features of intergranular fracture and transgranular fracture were found. The interaction of oxidation, creep damage and fatigue damage is an important reason for the TMF failure of the turbine blade.

Original languageEnglish
Pages (from-to)35-45
Number of pages11
JournalEngineering Failure Analysis
Volume102
DOIs
StatePublished - Aug 2019

Keywords

  • Failure analysis
  • Fractography
  • Metallography
  • Nickel-based superalloy
  • Thermomechanical fatigue
  • Turbine blade

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