摘要
民用飞机辅助动力装置(APU)舱排液装置用于将APU舱内可能泄漏的可燃液体排出机外,对整个系统和飞机的安全具有重要意义。针对重力排液,总结了APU舱排液装置的设计要求及相关机型的排液设计方案,在此基础上研究了民用飞机APU舱排液装置相关的设计要素和设计流程,获得了民用飞机APU舱排液装置的初步设计方法。
Auxiliary power unit （APU） drainage system for civil aircraft is used to drain the possible leakage flammable liquid out of the aircraft, and is very impotent for the system and the aircraft safety. This paper summarizes the design requirements and related design layout of other civil aircraft＇ s drainage system. The design elements and process are studied, and a preliminary design method for APU compartment drainage system is obtained.
出处
《民用飞机设计与研究》
2016年第3期25-28,共4页
Civil Aircraft Design & Research
关键词
APU舱
排液装置
auxiliary power unit （APU） compartment
drainage system
