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外物损伤对不锈钢模拟叶片疲劳强度的影响研究
王凌峰,许祥胜,赵振华,陈伟
南京航空航天大学 能源与动力学院 航空发动机热环境与热结构工业和信息化部重点实验室, 江苏 南京 210016
摘要:
为了研究不锈钢叶片在承受外物损伤后的剩余疲劳强度,开展了1Cr15Ni4Mo3N不锈钢模拟真实前缘叶片的外物损伤(FOD)与高周疲劳(HCF)试验。使用空气炮法对模拟叶片进行了FOD试验,结果表明,损伤主要可分为半圆型、V型和撕裂型三类,且损伤深度随着钢珠直径、入射速度的增大而增大。基于步进法开展了FOD试样的HCF试验,试验结果表明,FOD试样的振幅疲劳强度下降了70%以上,且随着损伤深度、入射速度的增大表现出明显的下降趋势。不同类型缺口的高周疲劳强度存在差异,半圆型缺口疲劳强度较高,V型缺口稍低,撕裂型缺口最低。使用SEM观测了FOD缺口及断口微观特征,疲劳裂纹源区均位于缺口根部表面附近,说明高速冲击造成的材料丢失、剪切带与剪切韧窝等微观特征促使了疲劳裂纹的萌生。
关键词:  外物损伤  高周疲劳强度  不锈钢  缺口类型  微观损伤
DOI:10.13675/j.cnki.tjjs.200120
分类号:V231.95
基金项目:
Effects of Foreign Object Damage on Fatigue Strength of Stainless Steel Simulated Blades
WANG Ling-feng, XU Xiang-sheng, ZHAO Zhen-hua, CHEN Wei
Key Laboratory of Aero-Engine Thermal Environment and Structure,Ministry of Industry and Information Technology,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Abstract:
In order to study the residual fatigue strength of stainless steel blade after foreign object damage (FOD), FOD and high cycle fatigue (HCF) tests of 1Cr15Ni4Mo3N stainless steel simulation specimens of real blade leading edge were carried out. FOD tests of simulation blades were performed by the air cannon system and the results show that the damage can be divided into three types: semicircle type, V type and tearing type. The damage depth increases with the enlargement of the steel ball diameter and the incident velocity. HCF tests of test samples subjected to FOD were conducted by a step-loading method. The results show that the amplitude fatigue strength of test samples subjected to FOD has decreased by more than 70%. It shows a significant downward trend with the increase of damage depth and incident speed. The HCF strength of three notch types is different. The fatigue strength of semicircle type notch is higher, while of V type notch is slightly lower, and of tearing type notch is the lowest. The micro characteristics of damage notches and fatigue fractures were observed by SEM. The fatigue source area is near the notch root surface, which indicates that the loss of material, shear bands and shear dimples caused by high-speed impact promote the initiation of fatigue crack.
Key words:  Foreign object damage  High cycle fatigue strength  Stainless steel  Notch type  Micro damage