摘要
介绍了飞机辅助动力装置控制系统的硬件设计与实现,该控制系统包含速度控制回路、压力控制回路、温度控制回路,具有体积小可靠性高的特点.经过长时间的实验证明,该系统能,全、可靠运行,能满足飞机对发动机起动、空中应急、电、液或其它辅助能源的不同需要。
Hardware of APU （Auxiliary Power Unit） control system is introduced, Speed loop, pressure loop and temperature loop are included, it has high reliability and small volume feature. The result of long times operation shows that it can satisfy the needs of start, emergency, and other power source of engine safely and reliably.
出处
《制造业自动化》
北大核心
2007年第10期50-53,共4页
Manufacturing Automation
关键词
辅助动力装置
数字电子控制
调理电路
auxiliary power unit
digital electronic controller
conditional circuit
