巡航导弹可折叠弹翼展开过程的力学分析与研究  

Dynamical Analysis and Study of Unwinding Process of Folding Bomb Wing of Cruise Missile

作　　者：钟世宏[1] 孙巍[1] 葛莉娜[1] 张崇耿[1] 周旬[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》2012年第2期13-16,共4页Aerospace Manufacturing Technology

摘　　要：根据巡航导弹可折叠弹翼支架的结构特点和展开过程的工作状态,分别对弹翼支架在巡航导弹正常飞行和地面试验两种状态下的受力进行了详细分析,指出了两种工作状态产生差异的原因,分析了目前普遍使用的地面试验设备所存在的不足,给出解决问题的基本思路。According to the structure characteristic and the folding-process work condition of the folding bomb wing bracket of cruise missile,the two kinds of force condition were analyzed in detail under the flight and ground test of bomb wing bracket of cruise missile.The difference causes of two kinds of work conditions and the shortages of the commonly used equipments were introduced,as well as the basic ideas for the problems.

关 键 词：弹翼支架 地面试验 受力状态 差异 

分 类 号：TJ761.6[兵器科学与技术—武器系统与运用工程]