科技创新与应用2024，Vol.14Issue(1)：164-167,4.DOI:10.19981/j.CN23-1581/G3.2024.01.039
正常类飞机CCAR23.2205符合性验证方法分析
摘要
Abstract
To promote the compliance verification work of the airworthiness requirement CCAR23.2205"Interactions between Systems and Structures"for normal category aircraft,a set of compliance verification methods for the"Interactions between Systems and Structures"requirement have been developed based on the domestic aircraft strength design work.The methods include five specific steps:filtering of failure types,evaluation of system performance under normal conditions,evaluation of system performance under failure conditions,indication of system failure and dispatch of aircraft under failure conditions.This method provides a detailed explanation of the compliance verification approach and the necessary computational analysis work to be carried out in each step,which provides some inspiration for the verification of airworthiness clause compliance of normal aircraft structural strength specialty.关键词
正常类飞机/结构强度/适航/符合性验证方法/系统Key words
normal-category aircraft/structural strength/airworthiness/conformity verification method/system分类
航空航天引用本文复制引用
赵佶男..正常类飞机CCAR23.2205符合性验证方法分析[J].科技创新与应用,2024,14(1):164-167,4.基金项目
国家民用飞机专项科研项目(MJZ3-2N21) （MJZ3-2N21）
