机载大功率综合化平台上、下电方法设计  

Design of Power Up and Down Method of Airborne High Power Integrated Platform

作　　者：杨柳 韩嫚莉[1] 湛文韬[1] YANG Liu;HAN Manli;ZHAN Wentao(Xi'an Aeronautics Computing Technique Research Institute,AVIC,Xi'an 710068,China)

机构地区：[1]中国航空工业集团西安航空计算技术研究所,陕西西安710068

出　　处：《通信电源技术》2020年第24期46-48,共3页Telecom Power Technology

摘　　要：随着航电子系统向高度综合化方向的发展,大功率综合化处理平台成为飞机航电系统中重要的任务处理平台。在平台系统架构设计过程中,从工作状态、供电以及网络拓扑等方面提出了多模式工作状态和可配置上、下电方法等需求。针对可配置上、下电的需求提出了一种针对大功率综合化平台的上、下电方法,从而保证产品处于当前最优处理能力状态,尽可能将大功率设备对飞机供电网络的影响降至最小,从而确保供电网络的可靠运作。With the development of avionics subsystem towards high integration,high power integration platform has become an important task processing platform in avionics system.In the process of platform system architecture design,from the aspect of word status,power supply and network topology,the requirements of multi-mode working status,power-on and power-off methods,and redundancy design are proposed.Aiming at the requirement of configurable power-up and down,this paper proposes a method for high-power integrated platform,so as to ensure that the products are in the current optimal processing capacity,and that the influence of high-power equipment on aircraft power supply network is minimized as far as possible to ensure the reliable operation of aircraft power supply network.

关 键 词：航空电子系统 综合化处理平台 供电模式 可靠性 

分 类 号：TP3[自动化与计算机技术—计算机科学与技术]