摘要
主起落架舱门是起落架系统的重要组成部件,当舱门收放存在故障时,系统处于失效状态,将不能起到收放作用。本文对某型飞机主起落架舱门收放原理和故障原因进行了分析,深入研究上位锁的控制过程和逻辑,提高了对起落架舱门收放系统的认识和理解。
The main landing gear door is an important component of the landing gear system. When there is a fault in the cabin retraction, the system is in a failure state and it will not be able to play a retractable role. This paper analyzes the principles of retracting and releasing of the main landing gear of a cartain aircraft, analyzes the control process and logic of the upper lock in depth, and improves the understanding of the landing gear cabin retractable system.
引文
[1]《飞机设计手册》总编委会.《飞机设计手册》第14册起飞着陆系统设计[M].北京:航空工业出版社,2002.
[2]田佳杰,贾玉红.大型民机起落架收放系统建模与仿真[J].机械设计与制造,2016(5):48-52.
[3]游凡.主起落架舱门放下影响因素研究[J].科技视界,2017(5):114-115.