| 注册
首页|期刊导航|液压与气动|机体变形和压力冲击载荷下飞机液压导管强度分析

机体变形和压力冲击载荷下飞机液压导管强度分析

权凌霄 司梦贺 李涛 张琦玮 孔祥东

液压与气动Issue(5):20-25,6.
液压与气动Issue(5):20-25,6.DOI:10.11832/j.issn.1000-4858.2018.05.004

机体变形和压力冲击载荷下飞机液压导管强度分析

Strength Analysis of Aircraft Hydraulic Pipe Under the Coupling of Body Deformation and Pressure Impact

权凌霄 1司梦贺 2李涛 2张琦玮 3孔祥东2

作者信息

  • 1. 燕山大学河北省重型机械流体动力传输与控制实验室,河北秦皇岛066004
  • 2. 燕山大学机械工程学院,河北秦皇岛066004
  • 3. 上海飞机设计研究院,上海200232
  • 折叠

摘要

Abstract

The aircraft hydraulic pipe system is characterized by "scattered,messy,long and miscellaneous".It is one of the most common failures of aircraft.With the high pressure of aircraft hydraulic system,the strength analysis of hydraulic pipe is more important.Under the coupling of two loads of body deformation and pressure impact,a certain oil return pipe of a certain aircraft wing is introduced,through the comparison and analysis of the theoretical calculation of stress,simulation stress and experimental stress,the correctness of the analysis and simulation method of the strength analysis and the conclusion that the body deformation load has little influence on the strength of the catheter are obtained.Finally,the comprehensive evaluation of the three methods for the analysis of the strength of the ducts is made.The research contents have certain engineering practice and theoretical guidance significance for the strength analysis of aircraft hydraulic pipe.

关键词

飞机液压导管/强度分析/有限元仿真/实验分析

Key words

hydraulic pipeline of aircraft/strength analysis/finite element simulation/experimental analysis

分类

机械制造

引用本文复制引用

权凌霄,司梦贺,李涛,张琦玮,孔祥东..机体变形和压力冲击载荷下飞机液压导管强度分析[J].液压与气动,2018,(5):20-25,6.

基金项目

国家重点基础研究发展计划(973计划)(2014CB046405) (973计划)

国家自然科学基金(51775477,51505410) (51775477,51505410)

液压与气动

OA北大核心CSTPCD

1000-4858

访问量2
|
下载量0
段落导航相关论文