期刊文献+

基于ANSYS Workbench某机载电子设备随机振动响应分析 被引量:16

Analysis on ANSYS Workbench based random vibration response of a certain airborne electronic equipment
下载PDF
导出
摘要 机载电子设备是飞机武器系统的重要组成部分,随机振动是使其结构失效的主要因素。为了提高机载电子设备的可靠性,基于ANSYS Workbench软件平台对某机载电子设备进行模态分析和随机振动的加速度PSD模拟分析,获得了应力分布云图和加速度功率谱密度响应曲线,并在此基础上通过随机振动环境试验对仿真分析结果进行验证。结果表明,有限元仿真计算结果与试验结果比较吻合,说明建模与仿真的合理性,并可为下一步的结构优化与新设计提供参考。 Airborne electronic equipment is an important component of the airborne weapon system,and the random vibration is a main factor of its structural failure. In order to improve the reliability of the airborne electronic equipment,the modal analysis for a certain airborne electronic equipment and acceleration PSD(power spectral density) simulation analysis for the random vibration based on ANSYS Workbench software platform are conducted to acquire the stress distribution cloud picture and acceleration PSD response curve. And on this basis,the simulation analysis results were verified by means of the random vibration environment test. The verification results show that the finite element simulating calculation result is identical with the experimental result,which proves that the modeling and simulation are reasonable. It provides a reference for further structural optimization and new design.
出处 《现代电子技术》 北大核心 2016年第10期96-99,103,共5页 Modern Electronics Technique
基金 西华大学研究生创新基金项目(ycjj2015076) 四川省教育厅重点项目(15ZA0126)
关键词 机载电子设备 模态分析 随机振动分析 飞机武器系统 airborne electronic equipment modal analysis random vibration analysis airborne weapon system
  • 相关文献

参考文献8

二级参考文献19

  • 1祝长生,陈拥军,朱位秋.不平衡线性转子-轴承系统的非平稳地震激励响应分析[J].计算力学学报,2006,23(3):285-289. 被引量:8
  • 2祝长生,陈拥军.机动飞行时航空发动机转子系统的振动特性[J].航空学报,2006,27(5):835-841. 被引量:33
  • 3苏翼林.材料力学[M].北京:人民教育出版社,1979.9-19.
  • 4贺兴书.机械振动学[M].上海:上海交通大学出版社,1988.45-50.
  • 5井町勇(日).-[J].机械振动学,1976,.
  • 6张胜兰,郑冬黎,郝琪,等.基于HyperWorks的结构优化设计技术[M].北京:机械工业出版社,2008.
  • 7顾世敏,顾桂兰,华国芳,等.GJB441-88机载电子设备机箱、安装架的安装形式和基本尺寸[S].北京:国防科工委军标出版发行部,1988.
  • 8Lin F S, Meng G. Study on the Dynamics of a Rotor in a Maneuvering Aircraft [J]. Journal of Vibration and Acoustics, 2003,125 ( 3 ) :324-327.
  • 9Groves K H, Bonello P. Improved Identification of Squeeze-Film Damper Models for Aeroengine Vibration Analysis [ J ]. Tribology International, 2010, 43 ( 9 ) : 1639- 1649.
  • 10Klauke T, Kiihhorn A, Beirow B,et al. Numerical Investigations of Localized Vibrations of Mistuned Blade Integrated Disks (Blisks) [ J ]. Journal of Turbomachinery, 2009,131(3): 1-11.

共引文献108

同被引文献91

引证文献16

二级引证文献39

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部