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High-temperature fatigue cracking mechanism and microstructure evolution of aero-engine K4169 superalloy in service process
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作者 Song-jun WANG Jian-jun HE +6 位作者 Zhi-hui GONG Wei-ping LI Jun-gang YANG Ya-jun SHAO yu-hui cai Yue-xin DU Cheng-wei YANG 《Transactions of Nonferrous Metals Society of China》 2025年第2期499-510,共12页
By using fatigue crack propagation testing and microstructural characterization,the crack fracture and propagation mechanisms of K4169 superalloy under various loads were investigated.The results demonstrate that the ... By using fatigue crack propagation testing and microstructural characterization,the crack fracture and propagation mechanisms of K4169 superalloy under various loads were investigated.The results demonstrate that the grain sizes of K4169 superalloy significantly increase,and the precipitation of the needle-likeδphase and the Laves phase is observed.Voids and microcracks form at location of Laves phase enrichment,creating conditions for crack propagation.By the a−N(a is the crack length,and N is the number of cycles)relationship curve,the change in the fatigue crack growth rate with the increasing number of cycles progresses through three separate stages.The fracture process of K4169 superalloy under low-stress cyclic loading(3 kN)exhibits the ductile fracture.Subsequently,the fracture process starts to change from the ductile fracture to the brittle fracture as the stress increases to 4.5 kN.In the microstructures of fractures in both stress states,intergranular propagation is the mechanism responsible for crack propagation.Moreover,the Laves phase exists near the fracture crack,which is in line with the post-service structural phenomenon. 展开更多
关键词 K4169 superalloy high-temperature fatigue MICROSTRUCTURE crack propagation AERO-ENGINE
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