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
Link To Document :
بازگشت