APU飞机级控制系统设计研究  

Research on APU Aircraft Level Control System Design

作　　者：李彦双[1] 唐宏刚[1] 殷海涛[1] 唐力[1] 

机构地区：[1]上海飞机设计研究院动力燃油系统设计研究部,上海200436

出　　处：《民用飞机设计与研究》2011年第4期8-12,共5页Civil Aircraft Design & Research

摘　　要：为充分发挥APU(辅助动力装置)在民用飞机上的作用,设计一个好的APU控制系统显得尤为重要。对APU飞机级控制系统的设计进行了相关研究,论述了APU控制板、APU控制器供电、燃油控制、应急停车、APU引气、起动/发电、风门控制和指示告警等控制子系统在设计时所要考虑的因素,并给出了相应的设计样例,然后从功能实现和电气原理的角度进行了详细地分析,可为APU飞机级控制系统的方案设计提供参考。In order to sufficiently realize the functions of Auxiliary Power Unit （APU） to an aircraft, it is very important to design a good APU control system. This paper was a research on the APU aircraft level control system design and discussed the aspects which should be consid- ered when control subsystems were designed, such as APU control panel, APU controller power supply, fuel control, emergency stop, APU air bleed, starter/generator, air inlet door control and indication/warning, etc. Some examples of design were provided and detailedly analyzed from the perspectives of function realization and electrical principle. This paper provided a recommendation for outline design and detail design of APU aircraft level control system.

关 键 词：辅助动力装置 控制系统 控制器 控制逻辑 

分 类 号：V271.1[航空宇航科学与技术—飞行器设计]