DocumentCode
1471609
Title
Some aspects of the application of induction motors to aircraft
Author
Braun, N. J.
Author_Institution
Westinghouse Electric and Manufacturing Company, Lima, Ohio
Volume
63
Issue
10
fYear
1944
Firstpage
769
Lastpage
772
Abstract
USE of electric power in aircraft has grown with each succeeding year. Aircraft have become larger, and with each succeeding increase in size new and greater demands have been made for electric power. To date these demands have been met magnificently by 12-volt and 24-volt d-c systems, and there seems even reason to suppose that these systems will be in use for a long time to come. However, there is a transmission-weight penalty for a 24-volt system on large airplanes, particularly when the total load is high. Therefore, with an eye to the very large planes of the future, the aircraft industry has been fostering the development of two new electric systems, namely, a 115-volt d-c system, and a 208-volt three-phase 400-cycle system. Either of these two proposed systems will reduce greatly the weight of the electric wiring, and each system has its own special merits.
Keywords
Acceleration; Aircraft; Friction; Generators; Induction motors; Synchronous motors; Torque;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1944.6440537
Filename
6440537
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