模态方法下的悬臂梁/类悬臂梁弹性构件的动力学建模

薛志鹏; 厉明; 贾宏光; 罗泽勇

doi:10.3788/OPE.20152308.2250

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模态方法下的悬臂梁/类悬臂梁弹性构件的动力学建模

微纳技术与精密机械 | 更新时间：2020-08-12

- 模态方法下的悬臂梁/类悬臂梁弹性构件的动力学建模
- Modal method based dynamic analysis of cantilever type elastic structures
- 光学精密工程 2015年23卷第8期页码：2250-2257
- 作者机构：
  
  1. 中国科学院长春光学精密机械与物理研究所,吉林长春,中国,130033
  2. 中国科学院大学北京,中国,100049
- 作者简介：
- 基金信息：
  
  中国科学院知识创新工程国防科技创新基金资助项目(No.YYYJ-1122)()
- DOI：10.3788/OPE.20152308.2250
  中图分类号： V279;V215.3
- 收稿日期：2014-09-30，
  
  修回日期：2014-11-12，
  
  纸质出版日期：2015-08-25
- 稿件说明：
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薛志鹏, 厉明, 贾宏光等. 模态方法下的悬臂梁/类悬臂梁弹性构件的动力学建模[J]. 光学精密工程, 2015,23(8): 2250-2257

XUE Zhi-peng, LI Ming, JIA Hong-guang etc. Modal method based dynamic analysis of cantilever type elastic structures[J]. Editorial Office of Optics and Precision Engineering, 2015,23(8): 2250-2257
薛志鹏, 厉明, 贾宏光等. 模态方法下的悬臂梁/类悬臂梁弹性构件的动力学建模[J]. 光学精密工程, 2015,23(8): 2250-2257 DOI： 10.3788/OPE.20152308.2250.

XUE Zhi-peng, LI Ming, JIA Hong-guang etc. Modal method based dynamic analysis of cantilever type elastic structures[J]. Editorial Office of Optics and Precision Engineering, 2015,23(8): 2250-2257 DOI： 10.3788/OPE.20152308.2250.

摘要

针对扁簧式起落架这一类悬臂梁弹性结构的弹性变形

提出了一种克服传统模态方法计算精度受限的模态旋转方法。首先

基于有限元理论中的小变形运动学分析推导出变形中旋转部分的表述方法。然后

总结了传统线性模态理论

提出了一种将旋转变形引入到模态坐标下动力学方程的方法

从而在结构动力学分析中引入旋转变形的影响

使模态方法适用于旋转变形较大的情况。最后

进行了扁簧式起落架静力学仿真及实验的对比验证。结果显示:在设计载荷100 kg范围内

两种模态方法都能保证5%以内的计算精度;但在极限载荷180 kg情况下

线性模态方法产生了超过35%的计算误差

而模态旋转方法仍能够保证10%以内的计算精度。仿真过程中两种模态方法的计算步长均为1 ms。结果表明:与传统的模态方法相比

提出的模态旋转方法在相对旋转变形较大的情况下有更高的计算精度

同时保留了传统模态方法计算效率高的优点。

Abstract

For the elastic deformation of cantilever type elastic structures in a flat spring landing gear

a new modal warp method was proposed to improve the calculation precision of the traditional modal method. Firstly

the description of a rotational component in infinitesimal deformation was deduced based on the finite element theory. Then the general modal method was summarized and how to introduce the rotational deformation into the dynamic equation in a modal coordinate was proposed. By which

the rotational deformation was introduced into the analysis of structure dynamics

so that the modal method could simulate the large bending and/or twisting deformation. Finally

the static simulation and experiments were performed and compared on the flat spring landing gear. The analysis results show that when the load mass is less than 100 kg

the relative errors are below 5% for both the linear modal method and modal warping method. However

when the load reaches to 180 kg(which represents the maximum realistic condition for landing)

the error of the modal warp method remains within 10% and the error of linear modal has been more than 35%. Moreover

the time steps of both modal methods are 1 ms. As comparied with the traditional method

the modal warping method provides higher calculation and efficiency in the simulation of large rotational deformation.

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Keywords

references

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