DocumentCode :
1123370
Title :
Nonsymmetrical, Nonlinear Aerospace Alternators on Nonlinear Loads
Author :
Jokl, A.L. ; Amstutz, L.I. ; Erdelyi, E.A.
Author_Institution :
U. S. Army Mobility Equipment, Research and Development Center, Ft. Belvoir, Va. 22060
Issue :
3
fYear :
1975
fDate :
5/1/1975 12:00:00 AM
Firstpage :
298
Lastpage :
315
Abstract :
A two-dimensional numerical analysis of the cross section of a homopolar inductor alternator supplying a rectifier load is developed. Besides the effects of the nonlinearities of the magnetic materials, the eddy currents induced in the rotor by the nonlinear load are considered. Results for a 95-kVA homopolar inductor alternator are presented and include magnetic induction and flux distribution at two instants of time, output voltage, eddy current densities, and loss. The theoretical results have been found to be in good agreement with available test data on the alternator.
Keywords :
Aerospace materials; Alternators; Eddy currents; Inductors; Magnetic flux; Magnetic materials; Numerical analysis; Rectifiers; Rotors; Voltage;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1975.308079
Filename :
4101409
Link To Document :
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