直升机操纵系统操作试验研究

本文提出的操纵系统操作试验是以直升机在恶劣飞行条件下、且在操纵系统助力器失效时,判断直升机操纵系统本身有无过度变形、过度摩擦和卡阻现象发生以确保直升机在恶劣气象条件下的安全飞行。此试验是在某型直升机上严格按适航条例规定,在动平衡加载状态下全行程范围内往返运动进行测试研究的。

Handling Test Methods Research for the Helicopter Handling System

This paper present handling test methods for the helicopter handling system in abomina- bie meteorological condition and the handling system booster failure,identifying helicopter handling system self has or without excessive deformation and excessive friction and the block phenomenon oc- currence and whether or not can ensure the helicopter safe flight in in abominable meteorological condition.The test on the helicopter is in accord with the airworthiness regulations requirements. The measure and test is completed in whole procedure under dynamic loading condition.