HIGH-POWER DENSITY SWITCHED RELUCTANCE MOTOR DRIVE FOR AEROSPACE APPLICATIONS

被引：66

作者：

RADUN, AV

机构：

[1] General Electric Corporate Research and Development, Schenectady, NY

来源：

IEEE TRANSACTIONS ON INDUSTRY APPLICATIONS | 1992年 / 28卷 / 01期

关键词：

Aircraft Engines--Fuel Pumps - Electric Drive;

D O I：

10.1109/28.120219

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

An advanced-development, variable-speed, 120-hp motor drive system for an electric-motor-driven, large aircraft engine fuel pump application is described. The system is designed to demonstrate advanced technologies that will allow the design of motor drive systems with the necessary power densities, reliability, and environmental specifications for aerospace applications. The drive runs from 270 Vdc, which is the emerging power standard for future aircraft power. The intended load of the drive is a centrifugal pump, although all system testing was done on a dynamometer test stand.

引用

页码：113 / 119

页数：7

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