| 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。 |
| 关键词: 折叠弹翼 展开机构 动力特性 |
| 基金项目: |
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| Design of Folding Wing Bracket of Cruise Missle and Its Dynamical Study |
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Zhong Shihong Wang Zhanli Sun Wei
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Xi’an Changfeng Research Institute of Mechanism and Electricity, Xi’an 710065
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| Abstract: |
| 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. |
| Key words: folding wing unfolding mechanism dynamical characteristics |
