航空学报 > 2024, Vol. 45 Issue (23): 230265-230265   doi: 10.7527/S1000-6893.2024.30265

固体力学与飞行器总体设计

基于功率谱分割的随机振动疲劳寿命估算方法

赵寿根1, 王显浩1,2, 谢瑞丽1(), 李名1, 程伟1   

  1. 1.北京航空航天大学 航空科学与工程学院,北京 100191
    2.中国航空工业集团有限公司 上海民用航空机电系统有限公司,上海 200241
  • 收稿日期:2024-01-30 修回日期:2024-04-07 接受日期:2024-06-07 出版日期:2024-07-16 发布日期:2024-06-14
  • 通讯作者: 谢瑞丽 E-mail:xierl@buaa.edu.cn
  • 基金资助:
    国家自然科学基金(12102019)

Fatigue life estimation method for random vibration based on power spectral density segmentation

Shougen ZHAO1, Xianhao WANG1,2, Ruili XIE1(), Ming LI1, Wei CHENG1   

  1. 1.School of Aeronautic Science and Engineering,Beihang University,Beijing 100191,China
    2.Shanghai Civil Aviation Electromechanical System CO. ,LTD. ,Aviation Industry Corporation of China,Ltd. ,Shanghai 200241,China
  • Received:2024-01-30 Revised:2024-04-07 Accepted:2024-06-07 Online:2024-07-16 Published:2024-06-14
  • Contact: Ruili XIE E-mail:xierl@buaa.edu.cn
  • Supported by:
    National Natural Science Foundation of China(12102019)

摘要:

机械结构在随机振动载荷的持续作用下易激起自身部分阶模态,从而引发共振导致疲劳破坏,而对其进行寿命估算分析可有效预防结构疲劳失效,具有重要的工程意义。本文区别于传统从概率密度函数出发建立经验模型的振动疲劳寿命估算方法,从功率谱密度分割角度着手,运用理论推导和数值仿真相结合的方法,探讨了功率谱密度共振与非共振区的划分依据,分割形式对损伤估算的影响,并研究了多模态响应之间的耦合效应。结果表明,仅考虑功率谱密度共振区能提高损伤的估算精度,其分割形式对损伤估算并无影响,相较于常用Dirlik法和T-B法,本文多模态耦合损伤估算表达式对随机振动疲劳的损伤估算具有更强的适用性。

关键词: 振动疲劳, 功率谱分割, 共振区域, 多模态响应, 模态耦合

Abstract:

In the presence of sustained random vibration loads, mechanical structures easily induce their own partial-order modes, leading to resonance and fatigue failure. Life expectancy analysis effectively prevents structural fatigue failure, exhibiting important engineering significance. Diverging from traditional approaches that establish empirical models based on probability density functions, this study focuses on the power spectral density segmentation. Combining theoretical derivation and numerical simulation, the research explores the dividing criteria for power spectral density resonance and non-resonance regions, investigates the impact of segmentation forms on damage estimation, and explores the coupling effects among multi-modal responses. The results indicate that considering only the power spectral density resonance region enhances damage estimation accuracy. The segmentation form has no effect on damage estimation. The proposed expression for multi-modal coupled damage estimation demonstrates superior applicability to random vibration fatigue compared to commonly used Dirlik and T-B methods.

Key words: vibration fatigue, power spectrum segmentation, resonance region, multimodal response, mode coupling

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