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某型飞机作动筒管接头结构分析及优化改进
引用本文:钟小宏,鲁胜,黄志军,裴华平.某型飞机作动筒管接头结构分析及优化改进[J].航空工程进展,2019,10(S1):67-71.
作者姓名:钟小宏  鲁胜  黄志军  裴华平
作者单位:江西洪都航空工业股份有限公司飞机设计所,江西洪都航空工业股份有限公司飞机设计所,江西洪都航空工业股份有限公司飞机设计所,江西洪都航空工业股份有限公司飞机设计所
摘    要:针对某型飞机主起落架收放作动筒管接头结构特点,本文从结构功能、连接强度方面对管接头进行分析,并提出了作动筒管接头配合结构优化改进措施, 改进后的管接头结构能满足预期使用要求。

关 键 词:收放作动筒  管接头  优化改进
收稿时间:2019/1/24 0:00:00
修稿时间:2019/3/6 0:00:00

Structural Analysis and Optimization on the Pipe Nipple of an Aircraft Actuating Cylinder
Zhong Xiaohong; Lu Sheng; Huang zhijun;Pei HuaPing,Lusheng,Huangzhijun and Peihuaping.Structural Analysis and Optimization on the Pipe Nipple of an Aircraft Actuating Cylinder[J].Advances in Aeronautical Science and Engineering,2019,10(S1):67-71.
Authors:Zhong Xiaohong; Lu Sheng; Huang zhijun;Pei HuaPing  Lusheng  Huangzhijun and Peihuaping
Affiliation:AVIC Hongdu Aviation Industry Group Aircraft Design Institute,NanChang,Jiangxi,330024,AVIC Hongdu Aviation Industry Group Aircraft Design Institute,AVIC Hongdu Aviation Industry Group Aircraft Design Institute,AVIC Hongdu Aviation Industry Group Aircraft Design Institute
Abstract:According to the structural characteristics of the pipe nipple which is located in the main landing gear actuating cylinder of an aircraft, combine with structural function and connection strength analysis, this article mainly put forward the measures to improve the pipe nipple, what can meet the requirement of expected goal.
Keywords:Actuating Cylinder  Pipe Nipple  Optimization
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