“…High-temperature parts like aeroengine compressor disk bear the combined action of centrifugal loading, torsional loading, aerodynamic loading, and so on during service, that is, multiaxial thermomechanical fatigue (MTMF), which will lead to material fatigue, creep, and oxidation. [1][2][3][4][5][6][7][8][9] Moreover, the amount of these damages will change with the change of material type or loading path, which seriously affects the failure life of hightemperature equipment. [10][11][12] At present, modern aeroengines continue to pursue high thrust weight ratio, and their service reliability and safety need to be guaranteed; therefore, damage calculation and life assessment for MTMF have become a new hot issue.…”