复合材料发射箱定向器结构设计  

Structural Design for Composite Guide of Launch Canister

作　　者：秦旭锋[1] 曹德垚 张哲良 赵耀辉[1] 徐淑权[1] 卓毅[1] 蔡建[1] QIN Xu-feng;CAO De-yao;ZHANG Zhe-liang;ZHAO Yao-hui;XU Shu-quan;ZHUO Yi;CAI Jian(No.59 Institute of China Ordnance Industry,Chongqing 400039,China;Military Representative Office of Army Aviation Military Representative Bureau in Chengdu,Chengdu 610036,China;Shanxi JinHeng Chemical Industry Group Co.,Ltd.,Jinzhong 030616,China)

机构地区：[1]中国兵器工业第五九研究所,重庆400039 [2]陆军航空兵军事代表局驻成都地区军事代表室,成都610036 [3]山西金恒化工集团有限公司,晋中030616

出　　处：《包装工程》2018年第23期237-241,共5页Packaging Engineering

摘　　要：目的针对复合材料发射箱定向器的结构进行优化设计。方法通过材料力学理论,计算并结合有限元仿真分析,对定向器进行结构优化设计。结果定向器的最大变形满足指标要求,最大应力低于材料屈服强度。结论该设计方法便捷可靠,为今后类似产品设计提供了思路参考。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.

关 键 词：发射箱 定向器 结构设计 

分 类 号：TB485.3[一般工业技术—包装工程]