摘要
综合动力系统是在机载导弹弹射发射装置中采用的一种新型气压传动系统,它以高压冷气作为动力源,整个系统本身既是传动装置又是储能装置,而其中关键的控制部件是高压内置式电磁先导气阀。本文对高压内置式电磁先导气阀的结构进行了分析并建立了数学模型,在此基础上进行了仿真分析并研制了样机。
The integrated power system is a new pneumatic transmission system used in the ejection launcher of airborne missile. The core of the integrated power system is the electromagnetic valve. The structure and mathematics model of the valve was analyzed, and the simulation was carried out. The prototype was developed.
出处
《机床与液压》
北大核心
2008年第2期94-96,共3页
Machine Tool & Hydraulics
关键词
弹射发射装置
电磁阀
仿真
Ejection launcher
Electromagnetic valve
Simulation
