DocumentCode
1475846
Title
A 400-cycle aircraft motor
Author
Schwandt, G. O.
Author_Institution
Fractional-horsepower-motor engineering division, General Electric Company, Fort Wayne, Ind.
Volume
64
Issue
7
fYear
1945
fDate
7/1/1945 12:00:00 AM
Firstpage
508
Lastpage
512
Abstract
The ever-present need for lighter-weight and more compact aircraft electric motors is evident as any reduction in weight or space provides increased fuel, bomb, or pay-load capacity. Reliable 400-cycle motors more compact and approximately 40-per-cent lighter than existing 24-volt d-c motors have been developed recently. Present trends indicate that these motors will be used extensively aboard the airplane of tomorrow. This paper describes some of the 400-cycle motors that have been developed and discusses their requirements with the view of disseminating information so that others may better understand the motors and the performance to be expected from them.
Keywords
Aircraft; Iron; Rotors; Steel; Synchronous motors; Torque; Windings;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1945.6441164
Filename
6441164
Link To Document