• DocumentCode
    1471609
  • Title

    Some aspects of the application of induction motors to aircraft

  • Author

    Braun, N. J.

  • Author_Institution
    Westinghouse Electric and Manufacturing Company, Lima, Ohio
  • Volume
    63
  • Issue
    10
  • fYear
    1944
  • Firstpage
    769
  • Lastpage
    772
  • Abstract
    USE of electric power in aircraft has grown with each succeeding year. Aircraft have become larger, and with each succeeding increase in size new and greater demands have been made for electric power. To date these demands have been met magnificently by 12-volt and 24-volt d-c systems, and there seems even reason to suppose that these systems will be in use for a long time to come. However, there is a transmission-weight penalty for a 24-volt system on large airplanes, particularly when the total load is high. Therefore, with an eye to the very large planes of the future, the aircraft industry has been fostering the development of two new electric systems, namely, a 115-volt d-c system, and a 208-volt three-phase 400-cycle system. Either of these two proposed systems will reduce greatly the weight of the electric wiring, and each system has its own special merits.
  • Keywords
    Acceleration; Aircraft; Friction; Generators; Induction motors; Synchronous motors; Torque;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1944.6440537
  • Filename
    6440537