DocumentCode
1346905
Title
Frequency modulation and load-division instability in 400-cycle aircraft electric systems
Author
Oman, Henry
Author_Institution
Boeing Airplane Company, Seattle, Wash.
Volume
75
Issue
3
fYear
1956
fDate
7/1/1956 12:00:00 AM
Firstpage
181
Lastpage
188
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;
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.1956.6367168
Filename
6367168
Link To Document