DocumentCode
1924320
Title
High power density switched reluctance motor drive for aerospace applications
Author
Radun, A.V.
Author_Institution
GE Corporate Res. & Dev., Schenectady, NY, USA
fYear
1989
fDate
1-5 Oct. 1989
Firstpage
568
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 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, the emerging power standard for future aircraft power. The intended load of the drive is a centrifugal pump, although all system testing is done on a dynamometer test stand.<>
Keywords
aerospace engines; aircraft; pumps; reluctance motors; variable speed drives; 120 hp; 270 V; aerospace applications; aircraft engine fuel pump; centrifugal pump; dynamometer test stand; reliability; variable-speed; Aerospace electronics; Aircraft propulsion; Engines; Fuel pumps; Inverters; Motor drives; Power system reliability; Reluctance machines; Reluctance motors; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Industry Applications Society Annual Meeting, 1989., Conference Record of the 1989 IEEE
Conference_Location
San Diego, CA, USA
Type
conf
DOI
10.1109/IAS.1989.96706
Filename
96706
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