• 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