运输类旋翼航空器飞行控制适航要求研究  

Research on airworthiness regulations of flight control system of transport rotorcraft

作　　者：陈宇金 李宏 CHEN Yujin;LI Hong(Jiang Xi Aircraft Airworthiness Certification Center,CAAC,Nanchang330072,China)

机构地区：[1]中国民用航空江西航空器适航审定中心,南昌330072

出　　处：《中国民航大学学报》2023年第2期27-32,共6页Journal of Civil Aviation University of China

基　　金：民航安全能力建设资金项目([2020]145)

摘　　要：运输类旋翼航空器飞行控制系统总则条款CCAR 29.671仅给出顶层的适航安全目标和要求,在面向工程实践所需的适航审定建议方面存在不足。在解析适航规章和技术标准的基础上,结合实际工程实践给出了该条款适航要求和符合性方法的定性和定量建议,并提出了在电传飞行控制方面的适航要求和符合性方法建议。The CCAR 29.671 general clause for flight control system of transport rotorcraft only gives the airworthiness safety objectives and requirements at the top level,which is insufficient in the airworthiness certification recommendations required for engineering practice.Based on the analysis of airworthiness rules and technical standards,combining with actual engineering practice,this paper gives qualitative and quantitative insights on the airworthiness requirements and compliance methods of this clause.Advices on the airworthiness requirements and compliance methods in the aspect of flight control of fly-by-wire are proposed.

关 键 词：飞行控制系统 旋翼航空器 总体要求 适航 电传飞控 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计] V275.1