一种新型航空器固态配电装置模型  

A New Solide-State Power Distribution Unit Model of Aircraft

作　　者：张峰[1] 王承惠[1] 聂同攀[1] 

机构地区：[1]中航工业第一飞机设计研究院,陕西西安710089

出　　处：《测控技术》2014年第4期134-136,140,共4页Measurement & Control Technology

摘　　要：为扩大固态配电技术在飞机分布式配电系统中的应用范围,针对机载系统可能存在的控制需求,在已有固态配电装置架构基础上,提出兼有总线和硬线控制功能的固态配电装置模型。将机载控制系统中常见的硬线对总线的超控逻辑归纳为三类,设计了相应的逻辑表达式,并使用QuartusⅡ对每一种超控逻辑进行了仿真。仿真结果表明,该模型可以满足负载的高可靠性配电控制需求。In order to expand the range of applications of solid-state power distribution technology in distributed power systems for aircraft, based on the existing airborne system requirements and solid-state power distribution unit architecture, a model of solid-state power distribution unit with bus and hard-line control function is de- signed. The hard-line override logics in onboard control system are grouped into three categories and the corre- sponding logical expressions are designed. Each override logic is simulated with Quartus Ⅱ. Simulation results show that the model meets the power distribution requirements of high reliability load.

关 键 词：固态配电装置 总线 超控 逻辑 

分 类 号：V242.33[航空宇航科学与技术—飞行器设计]