旋转展开弹翼地面试验设备行星轮式加载机构的设计与探究  

Design and Inquiry of Planets Wheel Loading Mechanism in Ground Test of Rotary Expansion Wing

作　　者：钟世宏[1] 孙巍[1] 乔园园[1] 郑莉[1] 赵海波[1] 张培[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》2015年第1期40-43,47,共5页Aerospace Manufacturing Technology

摘　　要：通过对巡航导弹旋转展开弹翼地面试验设备加载机构工作状态的分析,指出现有地面试验设备加载方式存在的不足,提出新的模拟气动升力加载方式,对新加载机构进行了动力学分析,并给出新型地面试验设备设计时应注意的具体问题。This paper points out the deficiency of the existing loading way in ground test equipment by analyzing the working state of the ground test load mechanism in cruise missile rotary expansion wing. A new simulating pneumatic loading way is put forward and the new loading mechanism is analyzed in dynamics. The specific problems that should be accounted are raised for designing new ground test equipments.

关 键 词：旋转展开弹翼 地面试验 加载机构 

分 类 号：TJ760.6[兵器科学与技术—武器系统与运用工程]