• DocumentCode
    1307171
  • Title

    Solid-state switching for aircraft electric systems

  • Author

    Dickey, Lee D. ; Jones, Clyde M.

  • Author_Institution
    LTV Aerospace Corporation
  • Volume
    7
  • Issue
    11
  • fYear
    1970
  • Firstpage
    73
  • Lastpage
    79
  • Abstract
    An aircraft electric system designed around a solid-state approach offers many potential advantages over an electromechanical counterpart. These include higher reliability, longer life, more ruggedness, more versatility, and better compatibility. To achieve these advantages, however, it is not merely sufficient to replace electromechanical components with their solid-state equivalents. Here is one approach that has been tested in the laboratory and in aircraft during the past ten years¿with success. Included is a report on an advanced system undergoing evaluation.
  • Keywords
    Aerospace control; Aerospace electronics; Aircraft; Circuit breakers; Power semiconductor switches; Power system protection; Solid state circuits; Switching circuits; Voltage; Wiring;
  • fLanguage
    English
  • Journal_Title
    Spectrum, IEEE
  • Publisher
    ieee
  • ISSN
    0018-9235
  • Type

    jour

  • DOI
    10.1109/MSPEC.1970.5213040
  • Filename
    5213040