Title :
Frequency modulation and load-division instability in 400-cycle aircraft electric systems
Author_Institution :
Boeing Airplane Company, Seattle, Wash.
fDate :
7/1/1956 12:00:00 AM
Abstract :
THE OUTPUT frequency of an alternator is proportional to the rotating speed of the field flux of the alternator. Variations in this field flux speed can be caused by torsional flexing of the alternator shaft and by instability in the speed of the prime mover.
Keywords :
Airplanes; Alternators; Frequency modulation; Shafts; Torque;
Journal_Title :
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
DOI :
10.1109/TAI.1956.6367168
