某型直升机载荷补偿器操纵摇臂磨损分析与排除  

The Analysis and Solution of the Control Bellcrank's Abrasion of Some Type Helicopter's Load-compensating Servo

作　　者：周志文[1] 方丽颖[1] 邓海侠[1] 

机构地区：[1]中国直升机设计研究所,江西景德镇333001

出　　处：《直升机技术》2010年第4期45-47,共3页Helicopter Technique

摘　　要：分析了某型直升机操纵系统尾桨载荷补偿器操纵摇臂在部队使用中产生磨损的原因,提出了改进的措施,并在使用部队得到了贯彻落实,提高了该操纵摇臂的使用寿命和直升机的安全。This paper analyzes the cause the control bellcrank's abrasion of some type helicopter's control system's tail rotor load-compensating servo which occurred during the employment in the armed forces.The improvement measure,therefore,is bought forward,and is implemented.Consequently,it is increased the working life of the control bellcrank,and enhanced the Helicopter's security.

关 键 词：直升机 操纵系统 载荷补偿器 操纵摇臂 磨损 

分 类 号：V22[航空宇航科学与技术—飞行器设计]