飞机机电管理系统综合化设计  

Integrated Design of Aircraft Electrome Chanical Management System

作　　者：艾铁柱[1] AI Tie zhu(Xi′an Aeronautics Computing Technique Research Institute,AVIC,Xi′an 710068,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710068

出　　处：《航空计算技术》2018年第5期236-240,共5页Aeronautical Computing Technique

基　　金：航空科学基金项目资助(2016ZC31004)

摘　　要：设计了机电管理系统,其是飞机公共设备管理系统的综合,是在基本不改变传统机电系统结构的基础上,采用分布式设计,就近连接各机电子系统,减少机上电缆长度和重量,降低电缆敷设难度,控制综合后也减少了控制器数量。对飞机机电分系统的综合控制,提高了对各机电分系统的故障诊断能力,有效降低虚警率,减轻飞行员工作负担,改善飞机平台性能,提高机电系统的可靠性和维修性。The electrome chanical management system is a synthesis of the aircraft public equipment management system,which is basically not changing the traditional electrome chanical system.On the basis of the structure,the sub-market design is adopted to connect the electrome chanical subsystems nearly,reducing the length and weight of the cable on the machine an reducing.The difficulty of cable laying,the number of controllers is reduced,and the comprehensive control of the aircraft electrome chanical subsystem is improved.The fault diagnosis capability of each electrome chanical subsystem effectively reduces the false alarm rate,reduces the workload of pilots,and effectively improves the aircraft platform.Performance,improve the reliability and maintainability of electrome chanical systems.

关 键 词：飞机机电管理 综合 分布式 

分 类 号：V243[航空宇航科学与技术—飞行器设计]