航空学报 > 1989, Vol. 10 Issue (11): 545-552

含非线性联接的组合结构动态子结构分析

胡海岩, 李岳锋, 张阿舟   

  1. 南京航空学院
  • 收稿日期:1988-11-07 修回日期:1900-01-01 出版日期:1989-11-25 发布日期:1989-11-25

DYNAMIC SUBSTRUCTURING ANALYSIS OF COMPOSITE STRUCTURES WITH NONLINEAR LINKS

Hu Haiyan Li Yuefeng, Zhang Azhou   

  1. Nanjing Aeronautical Institute
  • Received:1988-11-07 Revised:1900-01-01 Online:1989-11-25 Published:1989-11-25

摘要:

本文研究由非线性隔振器耦联线性子结构形成的组合结构的动响应预估。基于实测子结构的脉冲响应函数,建立了组合结构的对接边界积分型动力学方程;找到了将其转化为标准常微分方程组的途径;用实验考核了上述方法。

关键词: 非线性, 动态子结构法, 振动控制

Abstract:

The paper deals with dynamic response prediction of composite structures which consists of two linear components coupled by some nonlinear vibration isolators. Based on the measured impulse response functions of the linear substructures, three kinds of dynamic equations of interfacial integeration are proposed and a procdure to transfrom the dynamic equations of integeral type into a set of ordinary differential equations is suggested. Computer simulations and a real test are given to verify the effectiveness of the theoretical results.

Key words: nonlinearity, dynamic substructuring analysis, vibration control