Effect of Shot-Peening on High-Temperature Notched Fatigue Property of FGH95 owder Metallurgy Superalloy
WANG Xin1, 2, WANG Kechang3, LUO Xuekun1, 2, ZENG Zhaojun3, WANG Xuqing1, 4, ANG Zhihui1, 2
1. Surface Engineering Institution, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
2. Aviation Key Laboratory of Advanced Corrosion and Protection on Aviation Materials, ECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;
3. Scientific and Technical Engineering Department, AECC South Industry Co., Ltd., Zhuzhou 412002, China;
4. National Key Laboratory of Advanced High Temperature Structural Materials, ECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
To promote the fatigue property of the disk’s stress-concentration structure made by powder metallurgy uperalloy, cast-iron shots, ceramic beads and the compound of the two kinds of shots are employed to peen the PM notched atigue sample. Strengthening layer is characterized by surface profile analysis using white light interfere, residual stress measurement ith X-ray diffraction and electrochemical corrosion, and micro-hardness profile research. Fatigue strengthening effect s compared with high-temperature notched (structure stress-concentration coefficient Kt=1.7) fatigue life of rotating-bending ode. The results show that strengthening layer is introduced by shot peening on the surface of FGH95 alloy. After shot eening, the surface average roughness and Kurtosis value are 0.9–1.5μm and close to 3 respectively. Surface residual stress s about –800 – –1150MPa, and the depth is 120~250μm. Moreover, compared with the as-received hardness 480–510HV0.2, he peening surface hardness increased to 575–625HV0.2, and the hardness layer depth is 175–250μm. The double shot peening ethod, firstly using the cast-iron shot in big intensity and secondly using the ceramic shot in small intensity, brings the aximum residual compressive stress, the highest hardness and biggest depth on the surface, and the smaller roughness with mooth bottom of crater, which obtains the best fatigue strengthening effect. The median fatigue life estimations of the double hot peening at 550MPa/650℃ is 20 times higher than original one.
王欣,王科昌,罗学昆,曾召军,王旭青,汤智慧. 粉末合金FGH95喷丸强化对高温缺口疲劳性能的影响[J]. 航空制造技术, 2018, 61(23/24): 40-45.
WANG Xin, WANG Kechang, LUO Xuekun, ZENG Zhaojun, WANG Xuqing, ANG Zhihui. Effect of Shot-Peening on High-Temperature Notched Fatigue Property of FGH95 owder Metallurgy Superalloy[J]. Aeronautical Manufacturing Technology, 2018, 61(23/24): 40-45.