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航空静止变流器技术

王帮亭 郑建

电子科技2011,Vol.24Issue(12):47-49,3.
电子科技2011,Vol.24Issue(12):47-49,3.

航空静止变流器技术

Research on the Aeronautical Static Inverter

王帮亭 1郑建1

作者信息

  • 1. 上海飞机设计研究院电气设计研究部,上海200235
  • 折叠

摘要

Abstract

Static Inverter is a key component of aircraft electrical power system(EPS).It is not only associated with the flight safety,but also a key element which affects the technology level of aircraft EPS.This paper focuses on the research on the realization methodology of the static inverter,and presents a double Buck inverter topology for the static inverter.A single phase double Buck circuit topology is used,which can eliminate the short circuit in one side of bridge.The diode attached to the switching device will not be involved in the operation.Therefore,there will be no large power loss of the switching device.The efficiency and reliability of the static inverter will be higher.The presented topology for the static inverter has been verified by simulation results

关键词

静止变流器/逆变器/飞机/拓扑/仿真

Key words

static inverter/inverter/aircraft/topology/simulation

分类

信息技术与安全科学

引用本文复制引用

王帮亭,郑建..航空静止变流器技术[J].电子科技,2011,24(12):47-49,3.

电子科技

1007-7820

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