DocumentCode
1030590
Title
Electric Drive for Aircraft
Author
Crom, George C.
Author_Institution
Air Materiel Command at Wright Field, Dayton, Ohio.
Volume
66
Issue
1
fYear
1947
Firstpage
1359
Lastpage
1362
Abstract
The use of large amounts of power in aircraft becomes a power-handling problem; and electric transmission from the turbines mounted in the fuselage, to the propellers on the wings, has the same advantages as in handling very large amounts of power in industry. The advantages of electric power transmission are discussed, principally flexibility, reliability, ability to shut down prime movers, and lessened drag. Also the disadvantages¿principally weight. An outline of an acceptable airplane and the calculation of fuel savings resulting from electric operation of a given flight plan are given, showing that it is possible to save enough fuel to cancel out the extra weight of the electric drive. Also, a discussion of weights of apparatus is given.
Keywords
Aerodynamics; Aerospace industry; Aircraft propulsion; Airplanes; Alternators; Engines; Fuels; Power generation; Propellers; Turbines;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Transactions of the
Publisher
ieee
ISSN
0096-3860
Type
jour
DOI
10.1109/T-AIEE.1947.5059583
Filename
5059583
Link To Document