运输类飞机适航标准25.785(b)(d)要求及符合性验证研究  

Study of the requirements and compliance verification of 25.785(b)(d)

作　　者：毛文懿[1] 李琪[1] 李杰[1] MAO Wenyi;LI Qi;LI Jie(Shanghai Aircraft Design and Research Institute,Shanghai 201210,China)

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》2024年第3期156-160,共5页Civil Aircraft Design & Research

摘　　要：CCAR25.785(b)(d)条款要求运输类飞机的设计能够保护乘员在遭受应急着陆惯性力等情况时不受到严重伤害。通过对FAA相关咨询通告和审定政策备忘录的研究,结合符合性验证工作实践,完成了对条款25.785(b)(d)要求的解析和对条款符合性验证考虑的梳理,形成了对条款25.785(b)(d)的符合性验证方法建议,可为运输类飞机针对条款25.785(b)(d)的适航性设计和符合性验证提供参考。25.785(b)(d)requires that transport category aircraft be designed to protect occupants from serious injury when subjected to emergency landing inertial forces.Based on the study of the relevant advisory circular and certification policy memorandum of FAA,combined with the compliance verification practice,this paper has completed the analysis of the requirements of 25.785(b)(d)and sorted out of the consideration of compliance verification of 25.785(b)(d),and formed the means of compliance of 25.785(b)(d).It can be used as a reference for the design and compliance verification of transport category aircraft with respect to 25.785(b)(d).

关 键 词：CCAR 25.785(b)(d) 适航 符合性方法 

分 类 号：V221.91[航空宇航科学与技术—飞行器设计]