TY - JOUR
T1 - Surface integrity and fatigue failure behavior of nickel based alloy blades
T2 - After cutting, vibration finishing and shot peening
AU - Sun, Yunqi
AU - Yao, Changfeng
AU - Tan, Liang
AU - Cui, Minchao
AU - Fan, Tao
AU - Cao, Yilong
AU - Ma, Yaoguo
N1 - Publisher Copyright:
© 2024
PY - 2025/1
Y1 - 2025/1
N2 - This article selected three processes to prepare nickel based alloy GH4169G blades, tested the surface integrity changes of different processes, conducted high cycle vibration fatigue tests, and studied their failure mechanisms. The results indicate that the milling polishing vibration precision machining (MV) process can effectively reduce the surface roughness of milling (M) process blades, while the milling polishing vibration precision machining shot peening (MVSP) process significantly improves the residual compressive stress and hardening layer level of blades. The MVSP process blades have the best vibration fatigue life, with an average life of 4.91 × 106, which is 775.2 % higher than the M process blades. The fatigue life of the blades has been significantly improved. After MV process treatment, the blade undergoes a transition from multi-source fatigue caused by M process to surface single source fatigue crack initiation. The crack initiation location of MVSP process blades shifted from the surface to about 0.097 mm below the surface, and shot peening significantly improved the fatigue crack initiation life of the blades.
AB - This article selected three processes to prepare nickel based alloy GH4169G blades, tested the surface integrity changes of different processes, conducted high cycle vibration fatigue tests, and studied their failure mechanisms. The results indicate that the milling polishing vibration precision machining (MV) process can effectively reduce the surface roughness of milling (M) process blades, while the milling polishing vibration precision machining shot peening (MVSP) process significantly improves the residual compressive stress and hardening layer level of blades. The MVSP process blades have the best vibration fatigue life, with an average life of 4.91 × 106, which is 775.2 % higher than the M process blades. The fatigue life of the blades has been significantly improved. After MV process treatment, the blade undergoes a transition from multi-source fatigue caused by M process to surface single source fatigue crack initiation. The crack initiation location of MVSP process blades shifted from the surface to about 0.097 mm below the surface, and shot peening significantly improved the fatigue crack initiation life of the blades.
KW - Failure mechanism
KW - High cycle vibration fatigue
KW - Multi process composite
KW - Nickel based alloy blade
KW - Surface integrity
UR - http://www.scopus.com/inward/record.url?scp=85208248754&partnerID=8YFLogxK
U2 - 10.1016/j.engfailanal.2024.109034
DO - 10.1016/j.engfailanal.2024.109034
M3 - 文章
AN - SCOPUS:85208248754
SN - 1350-6307
VL - 167
JO - Engineering Failure Analysis
JF - Engineering Failure Analysis
M1 - 109034
ER -