Fatigue life of titanium alloy thin-walled structure under thermal vibration environment

被引:0
作者
Jie X. [1 ]
Li L. [1 ]
Hu Y. [1 ]
Xie X. [1 ]
Wu Y. [1 ]
机构
[1] Beijing Institute of Structure and Environment Engineering, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation, Beijing
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2023年 / 38卷 / 01期
关键词
life prediction; thermal environment; thin-walled structure; titanium alloy; vibration fatigue;
D O I
10.13224/j.cnki.jasp.20210422
中图分类号
学科分类号
摘要
Titanium alloy thin-walled structures are in the thermal vibration environment for a long time. The constantly changing stress produced in the thermal vibration environment may cause structural fatigue failure. A high temperature vibration fatigue testing system was built with the help of vibration test bench, and the random vibration S-N fatigue curves of titanium alloy cantilever thin plate structure were obtained at 20, 150 ℃ and 300 ℃. The fatigue life prediction expression of titanium alloy cantilever thin plate structure at the above temperature was established, and the error between the predicted life and the actual life of the test piece was small, which was only 3.76% at the condition of 300 ℃,45.36 MPa stress level. The method can be used to study the fatigue performance and life prediction of structures under high temperature random vibration loads. © 2023 BUAA Press. All rights reserved.
引用
收藏
页码:55 / 60
页数:5
相关论文
共 19 条
[1]  
RIZZI S., Experimental research activities in dynamic response and sonic fatigue of hypersonic vehicle structures at NASA langley research center, (1993)
[2]  
JACOBS J H,, GRUENSFELDER C,, HEDGECOCK C E., Thermal acoustic fatigue of ceramic matrix composite materials, (1993)
[3]  
WU W F, TSEH C., Estimation of fatigue damage and fatigue life of components under random loading, International Journal of Pressure Vessels and Piping, 72, 3, pp. 243-249, (1997)
[4]  
MOON S, CHO I, YOON D., Fatigue life evaluation of mechanical components using vibration fatigue analysis technique, Journal of Mechanical Science and Technology, 25, 3, pp. 631-637, (2010)
[5]  
YU D, NGUYEN T T,, PARK S, Et al., High-cycle fatigue life prediction for Pb-free BGA under random vibration loading, Microelectronics Reliability, 51, 3, pp. 649-656, (2011)
[6]  
MALIGNO R,, WHALLEY D C,, SILBERSCHMIDT V V., Thermal fatigue life estimation and delamination mechanics studies of multilayered MEMS structures, Microelectronics Reliability, 52, 8, pp. 1665-1678, (2012)
[7]  
JIN Yishan, LI Lin, Discussion on the estimation method of acoustic fatigue life of aero-engine structure, Journal of Aerospace Power, 18, 3, pp. 373-377, (2003)
[8]  
LI Jing, SUN Qiang, LI Chunwang, Et al., Research on the vibration fatigue life of an aero-engine compressor blade, Chinese Journal of Applied Mechanics, 28, 2, pp. 189-193, (2011)
[9]  
LI Jiukai, LIU Yongjie, WANG Qingyuan, Et al., Ultra-high cycle fatigue test of TC17 titanium alloy at high temperature, Journal of Aerospace Power, 29, 7, pp. 1567-1573, (2014)
[10]  
LIU Wenguang, YAN Cheng, GUO Longqing, Et al., Vibration fatigue analysis of aircraft panel in thermal environment, Failure Analysis and Prevention, 9, 1, pp. 1-5, (2014)