Two channel switched reluctance starter/generator results

Author

Radun, A.V. ; Ferreira, C.A. ; Richter, E.

Author_Institution

Kentucky Univ., Lexington, KY, USA

Volume

1

fYear

1997

fDate

23-27 Feb 1997

Firstpage

546

Abstract

Measured data and simulation results for a two channel experimental switched reluctance motor (SRM) based aircraft engine starter/generator system is presented. The two channels of the system provide power to two separate and independent loads. The results presented here document the performance capability of this system from load step response to output ripple voltage. Both measured and predicted system performance is presented and compared. In addition, operating characteristics that are unique to this SRM-based system are described. Of particular interest is the interaction between the two separate channels when one channel experiences a load transient and the other does not. The source of channel interactions is described and measured data are provided. The issue of clearing load faults is also addressed. Design results for adding this capability to the experimental system are described

Keywords

electrical faults; load (electric); machine testing; machine theory; reluctance motors; starting; transient analysis; aircraft engine applications; channel interactions; load fault clearing; load step response; load transient; operating characteristics; output ripple voltage; performance capability; switched reluctance starter/generator results; two-channel SRM; Aerospace simulation; Aircraft propulsion; Control systems; Filters; Postal services; Power generation; Reluctance generators; Reluctance machines; Reluctance motors; Wire;

fLanguage

English

Publisher

ieee

Conference_Titel

Applied Power Electronics Conference and Exposition, 1997. APEC '97 Conference Proceedings 1997., Twelfth Annual

Conference_Location

Atlanta, GA

Print_ISBN

0-7803-3704-2

Type

conf

DOI

10.1109/APEC.1997.581513

Filename

581513