作动器止动器适航条款符合性验证分析

摘要

民用飞机适航条款验证是飞机型号研制过程中的重要阶段,通过分析适航条款中作动器止动器的每个细分条款的要求,针对某型飞机的止动器具体设计特征,提出了符合性验证思路和方法,并进行了验证分析,有力地支持了某型飞机的适航取证工作,对后续其他型号研制中该条款的验证工作具有一定的指导性和借鉴意义.%The verification of airworthiness conditions of civil aircraft is an important stage in the development of airplane models.It proposes a method on the verification of actuator stops based on the specified design feature of aircraft,analyzes the certification regular,describes the process of the verification of actuators stops.This provides the reference to the terms and conditions of the aircraft development.