DocumentCode
1457712
Title
Power equalizer systems for aircraft alternators
Author
Granath, J. A. ; Hawkes, A. K.
Author_Institution
Armour Research Foundation, Illinois Institute of Technology, Chicago, Ill.
Volume
72
Issue
10
fYear
1953
Firstpage
893
Lastpage
893
Abstract
THE 400-CYCLE 120/208-volt a-c electric system presently in use on operating aircraft uses both reactive and real power equalizers to assure equal division of load among the paralleled alternators. Use of analytical methods to predict conditions is desirable.
Keywords
Aircraft; Alternators; Associate members; Equalizers; Equations; Regulators; Voltage control;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1953.6438274
Filename
6438274
Link To Document