Fatigue deformation behavior of FGH96 superalloy under low cycle fatigue loading
Low cycle fatigue failure tests of the powder metallurgical nickel based superalloy FGH96 at 550℃ and 720℃ were carried out under total strain-controlled mode (R=-1).The fatigue failure behaviors were investigated by analyzing cyclic stress response and observing microstructure after fatigue through scanning electron microscopy (SEM) and electron backscatter diffraction (EBSD).The results show that FGH96 superalloy exhibits cyclic stability at 550℃,and cyclic softening afterwards at 720℃ with Aε/2=0.4%,and of cyclic softening at 720℃ with Aε/2=0.7%.After high temperature low cycle fatigue,the γ precipitates are cuboidal for all samples.No coarsening ofγ precipitates was detected at 550℃ and at 720℃ with Aε/2=0.4%,but small γ precipitates get together to be larger precipitates at 720℃ with Aε./2=0.7%.EBSD shows that the continuous small angle grain boundaries are produced during the fatigue.The small angle grain boundaries have a significant increase at 720℃,especially that case at Aε/2=0.7%.
powder metallurgical nickel based superalloy low cycle fatigue fatigue deformation electron backscatter diffraction
GU Yu-li HE Yu-huai LIU Chang-kui TAO Chun-hu
Beijing Institute of Aeronautical Materials, Beijing Key Laboratory of Aeronautical Materials Testin Beijing Institute of Aeronautical Materials, Beijing Key Laboratory of Aeronautical Materials Testin
国际会议
厦门
英文
418-422
2012-12-28（万方平台首次上网日期，不代表论文的发表时间）