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.
出处
《航天制造技术》
2011年第4期9-11,3,共4页
Aerospace Manufacturing Technology
关键词
支架部件
驱动装置
力学特性
bracket components
driving device
dynamical characteristics
