DocumentCode
1370723
Title
Power equalizer systems for aircraft alternators
Author
Granath, John A. ; Hawkes, Albert K.
Author_Institution
Armour Research Foundation of Illinois Institute of Technology, Chicago, Ill.
Volume
72
Issue
4
fYear
1953
Firstpage
209
Lastpage
217
Abstract
For efficient parallel operation of alternators it is necessary that both real and reactive load be distributed equally among the alternators. A 400-cycle a-c aircraft electric system presently in use employs both reactive and real power equalizers which are interconnections of the respective voltage and speed regulating systems of the paralleled alternators, giving an automatic correction for load unbalance while maintaining best system voltage and frequency regulation.
Keywords
Alternators; Equalizers; Equations; Inductors; Reactive power; Regulators; Voltage control;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1953.6371335
Filename
6371335
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