民机电传飞控系统CCAR 25.672符合性验证思路研究  

Research on Compliance Verification Thinking of CCAR 25.672 for Civil Aircraft Fly-By-Wire Flight Control System

作　　者：张松[1] 房峰 李小光[1] ZHANG Song;FANG Feng;LI Xiaoguang(Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)

机构地区：[1]南京航空航天大学,南京210016

出　　处：《民用飞机设计与研究》2018年第4期100-103,共4页Civil Aircraft Design & Research

摘　　要：首先阐述民机电传飞控系统适航符合性验证的定义,然后详细介绍了民机电传飞控系统适航符合性方法和选用原则,最后以国内某型民用客机为研究对象,开展了针对CCAR25. 672条款的符合性验证思路的分析与研究。At first,this paper explained the definition of the compliance demonstration for airworthiness regulation.Then,the compliance demonstration methods and the selection principle of civil aircraft fly-by-wire flight control system were introduced.Finally,taking a civil aircraft of China as the research object,the analysis and research was carried out for compliance verification thinking of CCAR 25.672.

关 键 词：民用飞机 飞控系统 适航符合性 验证思路 

分 类 号：V249.122[航空宇航科学与技术—飞行器设计]