DocumentCode
1472509
Title
Design considerations for D-C aircraft generators
Author
Miner, J. D.
Author_Institution
Westinghouse Electric and Manufacturing Company, Lima, Ohio
Volume
63
Issue
12
fYear
1944
Firstpage
1234
Lastpage
1240
Abstract
Engine-mounted aircraft generators must fit within an envelope 6 1/2 inches in diameter by 14 inches long. Electric-power requirements on military airplanes are increasing so rapidly that the most urgent assignment confronting designers of aircraft generators is that of achieving the ultimate output possible from this envelope. In 1939 the maximum rating was 1,500 watts; in 1940 the maximum rating jumped to 3,000 watts; in 1942 to 6,000 watts. A rating of 9,000 is coming into use, and a rating of 12,000 watts is likely to be possible in 1944. A rating of 15,000 watts has been mentioned. New materials, new military demands, new design ingenuity, new manufacturing techniques, and new operating experiences have all had a part in introducing more advances in this field during the past four years than were made during the approximate 20 years of generator history prior to 1938. Methods by which these advances have been accomplished are described, and possibilities for future progress are indicated.
Keywords
Aircraft propulsion; Airplanes; Electron tubes; Engines; Generators; Materials;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1944.6440673
Filename
6440673
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