航空学报 > 1992, Vol. 13 Issue (11): 627-632

自由振动优化平均和模态隔离

李岳锋, 吕民富   

  1. 南京航空学院振动工程研究所 南京 210016
  • 收稿日期:1991-04-19 修回日期:1992-04-27 出版日期:1992-11-25 发布日期:1992-11-25

OPTIMAL AVERAGING AND MODAL ISOLATION OF STRUCTURAL FREE VIBRATIONS

Li Yue-feng, Lli Min-fu   

  1. Vibration Engineering Research Institute, Nanjing Aeronautical Institute,Nanjing, 210016
  • Received:1991-04-19 Revised:1992-04-27 Online:1992-11-25 Published:1992-11-25

摘要: 对飞机颤振试飞等运行中的结构或机械在冲击激励下测到的高噪声多模态自由振动,提出一种优化平均方法,可以在大量抑制噪声的同时,充分突出某一感兴趣的模态。此方法基于自由振动频谱与结构频响函数在显示结构振动特性方面的“相似性”,以平均后的自由振动频谱具有最高共振峰作为自由振动平均时“初相角对齐”的优化平均判据。从优化平均自由振动频谱中,又可隔离出有更高信噪比的结构单模态自由振动来,从而使模态参数识别变得十分简单并有高精度。

关键词: 结构振动, 模态分析, 信号分析, 颤振, 动态测试

Abstract: The free vibration samplings rising from a running structure or machine excited by impulses, such as an aircraft in its flutter flight testing, are generally of multiple modes and high noise level. An optimal ensemble average method is presented by which a selected interesting structural modal element will be highlighted and the noises depressed greatly.The method is based on the similarity between the free vibration spectra and frequency response function in showing the vibration characteristics of structures. The optimized averaging implies that the original phases of the selected modal elements in all the free vibration samplings should be nearly the same. This fulfillment can be judged by making the selected modal resonant peak of the averaged free vibration spectra have its maximal value.From the optimal average free vibration spectra, a purer modal free vibration of the selected mode can be picked out furthermore, which makes the modal parameter identification become very simple and highly accurate at the same time.

Key words: structural vibration, modal analysis, signal analysis, flutter, dynamic testing