摘要
研究了喷丸后单晶合金的表面完整性和高温缺口疲劳性能。喷丸后表面形貌采用白光干涉仪表征,扫描电镜,2个方向观察(平行于受喷表面和截面方向)高分辨透射电镜和电子背散射衍射分析,疲劳性能采用旋转弯曲疲劳模式表征。采用旋转弯曲疲劳极限表征了强化增益作用,并与喷丸显微组织建立联系。结果表明,在760℃到850℃区间,喷丸强化较原始加工状态的疲劳极限增益达到14.8%,主要原因是高密度的缠结位错、加工硬化和晶粒错配。此外,通过表面应力集中系数计算表明,即使在平均粗糙度Ra升高的基础上,喷丸强化后表面应力集中系数也降低。
The surface integrity and notched fatigue property of a shot-peened single crystal superalloy were investigated. The surface texture of the peened material was determined using a white light interferometer, while the microstructural characterization was performed using a scanning electron microscopy, high resolution transmission electron microscopy from the plane and cross-section view directions and electron backscatter diffraction. The gains, expressed in term of high temperature fatigue limit, were established by rotating-bending fatigue tests and discussed in relation to the microstructure evolution in the shot peening states. Results show that the beneficial effect provided by shot peening is more than 14.8% against the as-machined in a temperature range from 760 ℃ to 850 ℃ because of the high-density tangled dislocation, cold work and disorientation. Furthermore, the stress concentration coefficient is reduced by the shot peening procedure while the average profile height Ra increases according to the calculation of the surface stress concentration.
作者
王欣
张涛
黄朝晖
汤智慧
赵振业
Wang Xin;Zhang Tao;Huang Zhaohui;Tang Zhihui;Zhao Zhenye(AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China;Aviation Key Laboratory of Advanced Corrosion and Protection on Aviation Materials, Beijing 100095, China;AECC Shenyang Institute of Aero-engine Design, Shenyang 561114, China;National Key Laboratory of Advance High Temperature Structural Materials, Beijing 100095, China)
出处
《稀有金属材料与工程》
SCIE
EI
CAS
CSCD
北大核心
2018年第6期1668-1676,共9页
Rare Metal Materials and Engineering
基金
Aeronautical Science Foundation of China(2015Z02117)
关键词
高周疲劳
喷丸
单晶合金
晶粒错配
high cycle fatigue
shot peening
single crystal superalloy
disorientation