Structural Design for Composite Guide of Launch Canister
QIN Xu-feng1, ZHAO Yao-hui1, XU Shu-quan1, ZHUO Yi1, CAI Jian1, CAO De-yao2, ZHANG Zhe-liang3
Author information+
(1)1.No.59 Institute of China Ordnance Industry, Chongqing 400039, China; (2)2.Military Representative Office of Army Aviation Military Representative Bureau in Chengdu, Chengdu 610036, China; (3)3.Shanxi JinHeng Chemical Industry Group Co., Ltd., Jinzhong 030616, China
The work aims to optimize the structural design of composite guide of launch canister. Based on the theory of mechanics of materials, the calculation and simulation analysis combined with the finite element were carried out to optimize the structural design of the guide. The maximum deformation of the guide met the index requirements and the maximum stress was lower than the material's yield strength. The proposed design method is convenient and reliable, and provides a reference for future similar product design.