机载简单电子硬件的适航考虑  

Consideration on Airborne Simple Electronic Hardware Certification

作　　者：刘文[1] 高瑞坤 刘媛 LIU Wen;GAO Rui-kun;LIU Yuan(Xi′an Aeronautics Computing Technique Research Institute,AVIC,Xi′an 710000,China)

机构地区：[1]航空工业西安航空计算技术研究所,陕西西安710000

出　　处：《航空计算技术》2021年第4期127-129,共3页Aeronautical Computing Technique

基　　金：航空基金项目资助(2017ZC31008)。

摘　　要：针对RTCA DO-254中对于简单电子硬件的符合性表明方式定义不明确的问题,为了解决机载电子设备适航过程中简单电子硬件如何表明对DO-254符合性的问题,通过分析FAA Order 8110.105A中的关于简单电子硬件的符合性验证考虑,重点讨论简单电子硬件的判定方式,符合性验证要求,并结合工作经验探讨具体符合性验证工作。Considering the unclear definition of the compliance means of simple electronic hardware in RTCA DO-254,in order to solve the problem of how simple electronic hardware demonstrates compliance to DO-254 in the certification process of airborne electronic equipment,this article analyzes the compliance verification considerations for simple electronic hardware in FAA Order 8110.105A,mainly focusing on the determination of simple electronic hardware.The compliance verification demands and specific compliance verification work based on experience.

关 键 词：简单电子硬件 符合性验证 RTCA DO-254 硬件验证 

分 类 号：V241[航空宇航科学与技术—飞行器设计]