• 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