摘要

Compression tests at room temperature are used to estimate the critical strain to spallation of EBPVD thermal barrier coating deposited on Ni based single crystals for blades used in aero-engines. The observation of fracture surfaces allows for investigating the location of delamination events leading to spallation, the eventual porosity at bond coat-alumina interface and kinetics of damage evolution. The effect of isothermal oxidation at 1,100 A degrees C is presented for standard or low sulfur AM1 superalloy, and coating process variants. The degradation is shown to depend on the thermal-mechanical loading and varies from isothermal oxidation, cyclic oxidation and thermal-mechanical fatigue with hold time. These observations are consistent with the damage observed in blades in engine tests or in service. These tests are a useful complement to standard cyclic oxidation tests to identify engineering lifetime models.

  • 出版日期2014-2
  • 单位中国地震局