民用飞机高强度辐射场(HIRF)防护适航验证方法研究  

Research on Airworthiness Verification Means for HIRF Protection

作　　者：章光灿 

机构地区：[1]上海飞机设计研究院液压系统设计研究部,中国上海201210

出　　处：《科技视界》2016年第6期97-98,共2页Science & Technology Vision

摘　　要：随着飞机安全飞行与着陆对电子/电气设备依赖性越来越强,而空间HIRF环境日益严酷,飞机HIRF防护设计及适航验证也变得日益重要。本文首先比较了目前国内外适用的HIRF防护适航条款,并解析了相应适航条款。其次,根据适航咨询通告AC20-158详细介绍了民用飞机HIRF防护适航验证的具体流程及试验要求。最后介绍HIRF适航验证过程中局方的适航审查内容及关注点。With the safe flight and landing of aircraft becoming increasingly dependent upon the electrical/electronic equipment, and the HIRF environment becoming much more severe, it is more meaningful to do research on the airworthiness verification methods for HIRF protection. Firstly,this paper compares the airworthiness HIRF protection regulations establish by FAA, EASA and CAAC and analyzes it. Secondly, according to the Airworthiness Advisory Circular AC20-158, this paper introduces the verification procedures and test requirements for HIRF protection. Finally, it discusses the concerns which the airworthiness authorities may pay an attention to.

关 键 词：HIRF 试验 合格审定 

分 类 号：V223.2[航空宇航科学与技术—飞行器设计]