TY - JOUR
T1 - Effects of laser shock processing on high temperature fatigue properties and fracture morphologies of k403 nickel-based alloy
AU - Luo, Sihai
AU - He, Weifeng
AU - Zhou, Liucheng
AU - Lai, Zhilin
AU - Chai, Yan
AU - He, Guangyu
PY - 2014/9/10
Y1 - 2014/9/10
N2 - Laser shock processing (LSP) is carried out on K403 nickel-based alloy turbine blades and the high temperature high and low cycle complexed fatigue tests are conducted to verify the reinforcement effect. The results of the fatigue experiments show that a greater flatness area near the fatigue crack initiation (FCI) is induced by LSP, the fatigue striation spacing on the fatigue crack growth (FCG) area decreases and lots of second cracks are generated after LSP. Grain refinement and high residual compressive stress on the surface layer are induced by LSP. But when the K403 nickel-based alloy after LSP is subjected to heat treatment at 550℃ for 150 min, a part of residual compressive stress has got relaxation while the refined structure has still remained good thermal stability. Compared with the untreated samples, the fatigue life of turbine blades is increased by 140% after LSP. The grain refined structure and residual compressive stress after relaxation are the main causes of improvement of nickel-based alloy fatigue life.
AB - Laser shock processing (LSP) is carried out on K403 nickel-based alloy turbine blades and the high temperature high and low cycle complexed fatigue tests are conducted to verify the reinforcement effect. The results of the fatigue experiments show that a greater flatness area near the fatigue crack initiation (FCI) is induced by LSP, the fatigue striation spacing on the fatigue crack growth (FCG) area decreases and lots of second cracks are generated after LSP. Grain refinement and high residual compressive stress on the surface layer are induced by LSP. But when the K403 nickel-based alloy after LSP is subjected to heat treatment at 550℃ for 150 min, a part of residual compressive stress has got relaxation while the refined structure has still remained good thermal stability. Compared with the untreated samples, the fatigue life of turbine blades is increased by 140% after LSP. The grain refined structure and residual compressive stress after relaxation are the main causes of improvement of nickel-based alloy fatigue life.
KW - Fatigue fracture
KW - High temperature fatigue
KW - K403 nickel-based alloy
KW - Laser optics
KW - Laser shock processing
KW - Residual compressive stress
UR - https://www.scopus.com/pages/publications/84907494693
U2 - 10.3788/CJL201441.0903001
DO - 10.3788/CJL201441.0903001
M3 - 文章
AN - SCOPUS:84907494693
SN - 0258-7025
VL - 41
JO - Zhongguo Jiguang/Chinese Journal of Lasers
JF - Zhongguo Jiguang/Chinese Journal of Lasers
IS - 9
M1 - 0903001
ER -