巡航导弹可折叠弹翼支架的设计及其动力学研究  

Design of Folding Wing Bracket of Cruise Missle and Its Dynamical Study

作　　者：钟世宏[1] 王占利[1] 孙巍[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》2010年第2期18-21,25,共5页Aerospace Manufacturing Technology

摘　　要：根据巡航导弹可折叠展开弹翼支架部件的工作特点和性能要求,对弹翼转轴、导向机构和展开机构等部件的设计方法进行深入分析,对燃气作动筒的安装型式和相关结构设计,提出了新的见解和解决方案,给出实施新方案的具体措施,并对展开机构的动力特性作出较为详细的分析,为支架部件整体的轻量化设计提供了新的思路。According to the working characteristic and performance requirements of the folding wing bracket of cruise missle, the design of wing spindle, guiding and unfolding mechanism is profoundly analyzed. New opinion and concrete scheme of fuel-canister installation model and its correlative structure are put forward as well as analysis of the dynamical characteristics of unfolding mechanism, so that new ideas of making the whole bracket assembly lighter in weight are presented.

关 键 词：折叠弹翼 展开机构 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]