DocumentCode
1023880
Title
Design Considerations for D-C Aircraft Generators
Author
Miner, J.D., Jr.
Author_Institution
Engineering manager, small-motor division, 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¿ 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
Acceleration; Aircraft manufacture; Aircraft propulsion; Airplanes; Engines; Manufacturing; Military aircraft; Power generation; Spline; Temperature distribution;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Transactions of the
Publisher
ieee
ISSN
0096-3860
Type
jour
DOI
10.1109/T-AIEE.1944.5058869
Filename
5058869
Link To Document