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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
引用本文:钟世宏,孙巍,张崇耿.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[J].航天制造技术,2011(4).
作者姓名:钟世宏  孙巍  张崇耿
作者单位:西安长峰机电研究所;
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。

关 键 词:支架部件  驱动装置  力学特性  

Analysis and Study on Working Condition of Driving Device of Folding Bomb Wing Bracket for Cruise Missle
Zhong Shihong Sun Wei Zhang Chonggeng.Analysis and Study on Working Condition of Driving Device of Folding Bomb Wing Bracket for Cruise Missle[J].Aerospace Manufacturing Technology,2011(4).
Authors:Zhong Shihong Sun Wei Zhang Chonggeng
Institution:Zhong Shihong Sun Wei Zhang Chonggeng(Xi'an Changfeng Research Institute of Mechanism and Electricity,Xi'an 710065)
Abstract: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.
Keywords:bracket components  driving device  dynamical characteristics  
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