摘要
本文论述了直升机在各种用途及使用状态下,自由涡轮轴发动机工作状态和旋翼工作状态的最优化匹配的规律,对直升机动力装置控制系统的四种控制模式进行了优化分析,并介绍了典型直升机动力装置全权限数字电子控制系统的控制特点及直升机动力装置控制系统的发展趋势。
This paper discussed the optimizing match law of free turboshaft engine and rotor operating state when the helicopter was in all kinds of uses and used states. Four kinds of control modes were anilyzed optimizing for helicopter power device control system. Then it introduced the control charcteristics of full authority electronic control system for helicopter power device and expand trend of helicopter power device control system.
出处
《沈阳航空工业学院学报》
1994年第3期21-27,共7页
Journal of Shenyang Institute of Aeronautical Engineering
关键词
直升机
动力装置
航空发动机
控制系统
Control of helicopter power plant,full authority digital electronic control
