Structural Analysis and Optimization on the Pipe Nipple of an Aircraft Actuating Cylinder

doi:10.16615/j.cnki.1674-8190.2019.S1.013

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Home > Archive>Volume 10, Issue S1, 2019 >67-71. DOI:10.16615/j.cnki.1674-8190.2019.S1.013

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Structural Analysis and Optimization on the Pipe Nipple of an Aircraft Actuating Cylinder
DOI:
                        10.16615/j.cnki.1674-8190.2019.S1.013
                    
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Affiliation:1.AVIC Hongdu Aviation Industry Group Aircraft Design Institute,NanChang,Jiangxi,330024;2.AVIC Hongdu Aviation Industry Group Aircraft Design Institute
Clc Number:V航空、航天
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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.

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Zhong Xiaohong; Lu Sheng; Huang zhijun;Pei HuaPing, Lusheng, Huangzhijun, 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

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Received:January 24,2019
Revised:March 06,2019
Adopted:March 13,2019
Online: June 13,2019
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