摘要
航天飞行器管路结构在随机振动载荷作用下产生疲劳损伤,可能导致管路焊接结构的疲劳失效,影响飞行器正常飞行。为此,开展飞行器管路焊接结构的疲劳损伤分析研究。首先建立管路结构的有限元模型,并通过计算模态分析和试验模态分析验证模型的准确性;然后考虑材料疲劳特性的离散性,推导焊接材料的P-S-N曲线以及疲劳损伤的计算表达式;随后采用结构应力法开展复杂管路焊接结构的疲劳损伤分析,确定其薄弱环节的中位疲劳寿命为5.23×10^(4) s;进一步采用概率分析方法得到管路焊接结构疲劳寿命与可靠度的关系。以上研究结果可为管路及整体结构的可靠性设计提供支撑。
When the pipeline structure in the space vehicle is subjected to the random vibration load,the fatigue damage will be accumulated in the welding part,and the normal flight of the space vehicle will be in danger.This paper analyzes the dynamic strength of a pipeline structure with welded joints in the space vehicle.Firstly,the finite element model of the pipeline structure is established,and the accuracy of the model is verified by the computational modal analysis and the experimental modal analysis.In view of the scattering nature of the material fatigue characteristics,the P-S-N curve of the welding material and the expression of the fatigue damage are obtained.Then,the structural stress method is used to analyze the fatigue damage of the complex pipeline welded structure,and the median fatigue life of the weak link is determined to be 5.23×10^(4) s.Furthermore,the relationship between the fatigue life and the reliability of the welded parts of the pipeline structure is obtained by the probability analysis method.The calculation results can provide a support for the reliability improvement of the pipeline structures and the reliability design of the whole structure.
作者
李志强
于洋
刘艳
刘艺
张梦妍
LI Zhiqiang;YU Yang;LIU Yan;LIU Yi;ZHANG Mengyan(Science and Technology on Reliability and Environment Engineering Laboratory,Beijing Institute of Structure and Environment Engineering,Beijing 100076,China;Beijing Institute of Electronic System Engineering,Beijing 100854,China;Beijing Institute of Structure and Environment Engineering,Beijing 100076,China)
出处
《航天器环境工程》
北大核心
2022年第2期125-132,共8页
Spacecraft Environment Engineering
关键词
随机振动
焊接结构
可靠度
疲劳损伤
random vibration
welded structure
reliability
fatigue damage
