DocumentCode
1471846
Title
Instrumentation of 400-cycle aircraft electric systems
Author
Corson, A. J. ; Stimson, A. G. ; Soley, W. A.
Author_Institution
General Electric Company, West Lynn, Mass.
Volume
63
Issue
11
fYear
1944
Firstpage
830
Lastpage
834
Abstract
THE use of 400-cycle alternating current1 as a power source on large aircraft originates the problem of adequate instrumentation at the distribution panel. Load conditions on a d-c system are determined by the simple parameters of voltage and current, whereas those of the a-c system include frequency and active and reactive power, in addition to voltage and current. Specifically, the flight engineer will require the following information for intelligent operation of the system:
Keywords
Ammeters; Brushes; Coils; Instruments; Resistance; Resonant frequency; Torque;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1944.6440572
Filename
6440572
Link To Document