民用飞机机身燃油管路适坠性适航要求和验证方法研究  

Research on the Crashworthiness Airworthiness Requirement and Compliance Method for Civil Airplane Fuselage Fuel Line

作　　者：朱德轩[1] 葛锐[1] 卞刚[1] 周伟[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2016年第4期56-60,共5页Civil Aircraft Design & Research

摘　　要：民用运输类飞机机身内燃油管路系统的适坠性设计是提供飞机在坠撞情况下的安全性和乘员生还率的重要技术。通过对相关适航规章立法背景的研究以及行业实践,总结分析了条款的适航要求,形成了机身燃油管路的适坠性设计指南和符合性验证方法。The crashworthiness design of fuselage fuel line system for civil transport airplane is critical to enhance the airplane safety and increase passenger survivability during crash condition. By analyzing the legislation history for related regulations and industry practice, this paper summarizes the airworthiness requirement, and forms the crashworthiness design guideline and compliance method for fuselage fuel line.

关 键 词：民用飞机 燃油系统 燃油管路 适坠性 

分 类 号：V228[航空宇航科学与技术—飞行器设计]