镍基单晶/柱晶高温合金超高周疲劳研究进展

doi:10.7527/S1000-6893.2020.24340

Abstract

Abstract: As the current main material for advanced aero-engine turbine blades, nickel-based single crystal/directionally solidified superalloys have high high-temperature strength, strong oxidation resistance and excellent fatigue resistance. Very-high cycle fatigue (fatigue life>10⁸) is the major problem faced by turbine blades in the middle and late stages of service. This article reviews the very-high cycle fatigue of nickel-based single crystal/directionally solidified superalloys. The analysis results show that single crystal/directionally solidified superalloys have abnormal yielding phenomena at high temperature; comparing fatigue studies at different frequencies finds no obvious frequency effect; analyses of fatigue mechanism find that cracks mainly originate from casting defects such as pores. Finally, the fatigue life prediction model is summarized, and the trends of very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys are prospected.

Key words: nickel-based single crystal and directionally solidified superalloys, high cycle fatigue, fatigue mechanism, fatigue properties, life prediction

CLC Number:

V252.2

LI Qian, ZHANG Fulu, ZHAO Zihua. Very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys: Review[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524340-524340.

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Very high cycle fatigue of nickel-based single-crystal and directionally solidified superalloys: Review

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