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飞机起落架有限元模态分析

张铁军 李曙林 常飞 王旺元 胡金海

现代制造工程Issue(11):10-13,45,5.
现代制造工程Issue(11):10-13,45,5.

飞机起落架有限元模态分析

Vibration modal analysis on the airplane landing gear

张铁军 1李曙林 1常飞 1王旺元 1胡金海1

作者信息

  • 1. 空军工程大学工程学院,西安710038
  • 折叠

摘要

Abstract

The finite element model of the airplane landing gear was established with ABAQUS. Inhere frequencies and mode shapes of landing gear under fixed boundary conditions were worked out by. using Lanczos which is the most popular method to solve modal analysis in engineering; the low-level natural frequency was analyzed by the brake-induced vibration test. The simulation and test results showed the first natural frequency is about 30Hz. The result of modal analysis can be used to the design and improvement of landing gear.

关键词

起落架/有限元法/Lanczos法/模态分析

Key words

landing gear/finite element method/Lanczos/modal analysis

分类

交通工程

引用本文复制引用

张铁军,李曙林,常飞,王旺元,胡金海..飞机起落架有限元模态分析[J].现代制造工程,2012,(11):10-13,45,5.

基金项目

国家自然科学基金项目(51105374) (51105374)

现代制造工程

OA北大核心CSCDCSTPCD

1671-3133

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