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升降舵操纵系统是操纵飞机进行俯仰机动的重要操纵系统。对于无回力助力的升降舵操纵系统中的不平衡力会导致驾驶员产生额外的负担,且会诱导驾驶员对飞机姿态产生误判,对飞机有严重的安全隐患。本文对某型飞机升降舵操纵系统不平衡力产生的原因及坚决方案进行研究,为解决不平衡力问题提供一定的借鉴。
The elevator control system is an important control system for controlling the aircraft for pitching maneuvers. Unbalanced forces in the elevator control system without backlash can cause extra burden on the driver and induce the driver to misjudge the attitude of the aircraft and pose a serious safety hazard to the aircraft. This paper studies the reason and the resolute plan of the unbalance force of the elevator control system of a certain type of aircraft, and provides some reference for solving the imbalance force problem.