新型可折叠双弹翼支架的设计及其动力学研究  

Design and Dynamics Study of Two Bracket Device of New Type Folding Bomb Wing

作　　者：钟世宏[1] 孙巍[1] 张崇耿[1] 乔园园[1] 赵亮[1] 许强[1] 

机构地区：[1]西安长峰机电研究所,西安710065

出　　处：《航天制造技术》2015年第5期1-6,共6页Aerospace Manufacturing Technology

摘　　要：根据巡航导弹可折叠弹翼支架部件的工作特点和性能要求,提出弹翼转轴、展开机构、导向机构及燃气作动筒等部件的设计要点,对燃气作动筒安装型式和展开机构提出了新的设计思路,并对弹翼支架各主要构件的动力特性作了理论分析,给出支架部件全新的优化设计方案。According to the work condition and structure characteristic demand for the folding bomb wing bracket of cruise missle, design gists are presented, including the bomb wing rotation axis, expandedness device, guide device and gas-drive tube. New design idea is proposed for the setting type of gas-drive tube and its expandedness framework, and the dynamical characteristics of the main components of wing bracket are analyzed theoretically, which provide a new optimization design scheme.

关 键 词：可折叠弹翼 机构优化 动力特性 

分 类 号：TJ761.6[兵器科学与技术—武器系统与运用工程]