TY - JOUR
T1 - Surface characterization and fatigue evaluation in GH4169 superalloy
T2 - Comparing results after finish turning; shot peening and surface polishing treatments
AU - Wu, Daoxia
AU - Yao, Changfeng
AU - Zhang, Dinghua
N1 - Publisher Copyright:
© 2018 Elsevier Ltd
PY - 2018/8
Y1 - 2018/8
N2 - In this study, shot peening was applied to the GH4169 superalloy, and the effect of surface polishing treatment on fatigue life of shot-peened specimens was investigated. The surface layer properties after five kinds of integrated processes were carefully characterized using a contact profilometer, 3 dimensional optical devices, vickers hardness tester, X-ray stress analyzer and scanning electron microscopy. The rotating bending fatigue tests were performed at room temperature to evaluate the effects of different integrated processes on the fatigue properties of GH4169 superalloy. The results showed that the longest fatigue life of 4.93 × 105 cycles and sub-surface fatigue crack nucleation are obtained after TS3P process. Compared with FT, TS1, TS2, TS3 process, the TS3P process improves approximately the 699%, 62.7%, 71.8%, and 48.9% fatigue life of GH4169 superalloy, respectively. This is because the TS3P process has the lowest surface roughness (Ra = 0.041 µm), the thicker compressive residual stress layer (hr = 100–330 µm) and hardening layer (hH = 95 µm).
AB - In this study, shot peening was applied to the GH4169 superalloy, and the effect of surface polishing treatment on fatigue life of shot-peened specimens was investigated. The surface layer properties after five kinds of integrated processes were carefully characterized using a contact profilometer, 3 dimensional optical devices, vickers hardness tester, X-ray stress analyzer and scanning electron microscopy. The rotating bending fatigue tests were performed at room temperature to evaluate the effects of different integrated processes on the fatigue properties of GH4169 superalloy. The results showed that the longest fatigue life of 4.93 × 105 cycles and sub-surface fatigue crack nucleation are obtained after TS3P process. Compared with FT, TS1, TS2, TS3 process, the TS3P process improves approximately the 699%, 62.7%, 71.8%, and 48.9% fatigue life of GH4169 superalloy, respectively. This is because the TS3P process has the lowest surface roughness (Ra = 0.041 µm), the thicker compressive residual stress layer (hr = 100–330 µm) and hardening layer (hH = 95 µm).
KW - Fatigue fracture
KW - Fatigue life
KW - GH4169 superalloy
KW - Shot peening
KW - Surface characterization
UR - http://www.scopus.com/inward/record.url?scp=85046513799&partnerID=8YFLogxK
U2 - 10.1016/j.ijfatigue.2018.04.009
DO - 10.1016/j.ijfatigue.2018.04.009
M3 - 文章
AN - SCOPUS:85046513799
SN - 0142-1123
VL - 113
SP - 222
EP - 235
JO - International Journal of Fatigue
JF - International Journal of Fatigue
ER -