导弹折叠翼展开机构运动功能可靠性分析

Movement Function Reliability of Mechanism of Deployable Folded Wings of Missile

通过建立等效动力模型得出导弹弹翼展开机构的运动规律 ,进而对弹翼展开机构进行动态静力分析。针对某型飞航导弹的折叠弹翼展开过程 ,对机构运动功能可靠性进行了较为全面的探讨和研究。该方法可用于飞行器分离机构。

A movement law of deployable folded mechanism of missile wing is gained through setting up equivalent dynamical model. Moreover, deployable mechanism of missile wing is analysized dynamicolly. This paper discusses and studies the mechanism's movement function reliability for some cruise missile. This method can be used for reliability analysis of separated, deployable and folded mechanism of aerocraft.