DocumentCode
965870
Title
Aircraft Secondary Power Generator with Direct Compensation Frequency Control
Author
Johnson, L.J. ; Rauch, S.E.
Author_Institution
Hallamore Electronics Co.,California.
Volume
6
Issue
4
fYear
1959
fDate
12/1/1959 12:00:00 AM
Firstpage
259
Lastpage
263
Abstract
The variable speed constant frequency alternator system provides accurate frequency control independent of the shaft speed. The method employed is completely electrical in contrast with the more conventional mechanical speed control systems. The principle of operation depends upon a constant angular velocity magnetic field in the alternator armature, the angular velocity being the vector sum of the mechanical velocity of the shaft and the velocity of an electromagnetic rotating field induced by the excitation of a polyphase field winding. The polyphase field winding is driven by a variable frequency polyphase exciter, its frequency being directly proportional to the speed deviation from synchronous speed of the alternator rotor and shaft. The frequency control system as described in this paper is the open-loop type and, as such, accomplishes absolute frequency control with no errors arising from load or speed transients. An experimental brushless, constant frequency, three-phase alternator is discussed.
Keywords
Aerospace control; Aircraft; Alternators; Angular velocity; Electromagnetic fields; Frequency control; Magnetic fields; Power generation; Shafts; Velocity control;
fLanguage
English
Journal_Title
Component Parts, IRE Transactions on
Publisher
ieee
ISSN
0096-2422
Type
jour
DOI
10.1109/TCP.1959.1136294
Filename
1136294
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