巡航导弹可折叠弹翼支架中驱动装置工作状态的分析与研究  

Analysis and Study on Working Condition of Driving Device of Folding Bomb Wing Bracket for Cruise Missle

作　　者：钟世宏[1] 孙巍[1] 张崇耿[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》2011年第4期9-11,3,共4页Aerospace Manufacturing Technology

摘　　要：根据巡航导弹可折叠弹翼支架中驱动装置的工作条件,分析了不同安装形式的受力状态,指出现有机构的不足之处,提出了新的设计方案和实施新方案的具体措施,并对新方案中驱动装置的行程变化状况和动力特性进行了较为详细的分析。According to working condition of driving device of folding bomb wing bracket for cruise missle,force condition of the different installation types of the driving device is analyzed.New scheme and concrete measures are put forward based on shortages of existent framework.Detailed analysis is focused on journey variety and dynamical characteristics of driving device in new scheme.

关 键 词：支架部件 驱动装置 力学特性 

分 类 号：TJ761.6[兵器科学与技术—武器系统与运用工程]