High-power density switched reluctance motor drive for aerospace applications
- 1 January 1992
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Industry Applications
- Vol. 28 (1) , 113-119
- https://doi.org/10.1109/28.120219
Abstract
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.Keywords
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