摘要
以某型飞机辅助动力装置(APU)为控制对象,介绍了该控制系统的工作原理,详细设计了控制规律,并对控制系统设计了台架试车试验步骤。通过多次台架试车,验证了该系统的可行性和控制品质,证明该系统能够安全、可靠运行,并满足现代飞机对发动机起动、空中应急、电、液或其他辅助能源的不同需要。
The working principle of the control system is introduced for a certain type of Auxiliary Power Unit, the control law of the APU is detailed designed, and the bed test steps of the system are discussed. After many times of bed test the functions and performances of the control system are evaluated. The results show that this system can satisfy the needs of start emergency and other power source of engine safely and reliably.
出处
《航空兵器》
2008年第3期42-44,共3页
Aero Weaponry
