“某型直升机向右压杆产生反向冲动”故障分析与处理  

“During the Flight of a Certain Type of Helicopter,the Right Lever Produces a Reverse Impulse” Analysis and Treatment

作　　者：杨海龙 郑竹林 袁功勋 张家鹏 YANG Hailong;ZHENG Zhulin;YUAN Gongxun;ZHANG Jiapeng(Daqing Aviation Rescue Detachment of Forest Fire Bureau of Ministry of Emergency Management,Daqing 163000,Heilongjiang,China)

机构地区：[1]应急管理部森林消防局大庆航空救援支队,黑龙江大庆163000

出　　处：《民航学报》2022年第4期106-108,122,共4页Journal of Civil Aviation

摘　　要：直升机操纵系统与自动飞行控制系统是直升机上非常关键的两个系统,其性能正常与否直接影响直升机与机组人员安全。本文从所在单位一起真实案例的排查入手,通过阐述操纵系统与自动飞行控制系统的工作原理以及交联情况,在分析飞行过程中驾驶杆操纵内在逻辑的基础上,提供了排除类似故障的思路及方法。The control system and the automatic flight control system are two very important systems of helicopter,and their performance directly affects the safety of helicopter and crew.Starting from the investigation of a real case in our unit,this paper provides ideas and methods to eliminate similar faults by expounding the working principle and cross-linking situation of the control system and the automatic flight control system,and analyzing the internal logic of the pilot lever operation during flight.

关 键 词：操纵系统 自动飞行控制系统 驾驶杆操纵 

分 类 号：V[航空宇航科学技术]