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.
出处
《航天制造技术》
2015年第5期1-6,共6页
Aerospace Manufacturing Technology
关键词
可折叠弹翼
机构优化
动力特性
folding bomb wing
device optimization
dynamical characteristic
