DocumentCode :
1433931
Title :
Two-channel switched reluctance starter/generator results
Author :
Radun, Arthur V. ; Ferreira, Caio A. ; Richter, E.
Author_Institution :
Kentucky Univ., Lexington, KY, USA
Volume :
34
Issue :
5
fYear :
1998
Firstpage :
1026
Lastpage :
1034
Abstract :
Measured data and simulation results for a two-channel experimental switched-reluctance-motor (SRM)-based aircraft engine starter/generator system are presented. The two channels of the system provide power to two separate and independent loads. The results presented document the performance capability of this system with both channels operating simultaneously. Both measured and predicted system performance are presented and compared. In addition, operating characteristics that are unique to this SRM-based system are described. Of particular interest are the interactions between the two separate channels when one channel experiences a load transient and the other channel does not. The source of channel interactions is described, and measured data is provided. The issue of clearing load faults is also addressed. Design results for adding this capability to the experimental system are described
Keywords :
aerospace engines; aerospace simulation; aerospace testing; aircraft; load (electric); machine testing; machine theory; reluctance generators; reluctance motors; starting; SRM; aircraft engine; channel interactions; design results; load fault clearing; load transient; operating characteristics; performance capability; two-channel switched reluctance starter/generator; Aerospace electronics; Aircraft propulsion; Electromagnetic interference; Filters; Power electronics; Power generation; Reluctance generators; Reluctance machines; Reluctance motors; Strontium;
fLanguage :
English
Journal_Title :
Industry Applications, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-9994
Type :
jour
DOI :
10.1109/28.720442
Filename :
720442
Link To Document :
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