DocumentCode :
1346531
Title :
A weight analysis of modern aircraft electric systems
Author :
Garbarino, H. L. ; Hawkes, A. K. ; Granath, J. A.
Author_Institution :
Armour Research Foundation of Illinois Institute of Technology, Chicago, Ill.
Volume :
73
Issue :
6
fYear :
1955
Firstpage :
463
Lastpage :
469
Abstract :
THE problem of choosing suitable electric systems for aircraft has been the subject of investigation and discussion for many years. To meet general or specialized requirements, the aircraft industry has had to choose between primary a-c and d-c systems. The magnitude of system voltage has been a variable. For the a-c system, a choice must be made between variable and constant frequency, and for the latter the selection of a nominal value and tolerances are required.
Keywords :
Aircraft; Fuels; Induction motors; Insulation; Relays; Reliability; 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.1955.6367100
Filename :
6367100
Link To Document :
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