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作 者:华铭 李新民[2] 李宏 HUA Ming;LI Xinmin;LI Hong(Jiangxi Aircraft Airworthiness Certification Center,CAAC,Nanchang 330024,Jiangxi,China;China Helicopter Design Institute,Jingdezhen 333000,Jiangxi,China)
机构地区:[1]中国民用航空江西航空器适航审定中心,江西南昌330024 [2]中国直升机设计研究所,江西景德镇333000
出 处:《民航学报》2022年第6期126-128,169,共4页Journal of Civil Aviation
摘 要:健康和使用监测系统(HUMS)的安装能够有效监测旋翼航空器关键部件(如发动机、旋翼系统、传动系统)的使用情况,并准确及时判断其可能产生的故障类型、故障部位和故障程度,从而大大提高旋翼航空器的安全性和使用效能。本文重点围绕HUMS系统的适航审定,通过对国外适航当局相关适航条款及符合性方法的研究,梳理总结HUMS适航审定中的关键要素,期望能为下一步制定我国旋翼航空器HUMS适航符合性验证方法提供帮助。The installation of the Health and Usage Monitoring Systems(HUMS) can effectively monitor the usage of key components(such as engine, rotor system and rotor drive system) of rotorcraft, and accurately diagnose the type, location and degree of possible faults, thus greatly improve safety and application performance of rotorcraft. This paper focuses on airworthiness certification of HUMS. Based on research on relevant airworthiness rules and compliance methods of foreign airworthiness authorities, it summarizes key elements which should be addressed in airworthiness certification of HUMS in order to provide help for developing China’s airworthiness compliance methods for HUMS of rotorcraft.
分 类 号:V275.1[航空宇航科学与技术—飞行器设计]
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