• DocumentCode
    1471808
  • Title

    Requirements for low-voltage aircraft cable

  • Author

    Hedges, R. E.

  • Author_Institution
    Douglas Aircraft Company, Inc., Santa Monica, Calif.
  • Volume
    63
  • Issue
    11
  • fYear
    1944
  • Firstpage
    808
  • Lastpage
    809
  • Abstract
    ELECTRIC wiring designed for aircraft probably is required to withstand a wider range of operating conditions than most other types of electric wiring. This is not surprising since present airplanes, both combat and commercial types, are expected to be able to fly anywhere in the world under all kinds of weather conditions. Repair of a damaged airplane in remote parts of the world must be accomplished with a minimum of replacement parts, and probably only basic tools, such as screw driver, pliers, hammer, and wrench. In many cases repairs can be made only by salvaging parts from other airplanes. If the original electric wiring of an airplane is properly designed, installed, and protected against damage due to overloads, short circuits, insulation failure, abrasion, fluids, and fungus growth, and so forth, a great deal of wire replacement and maintenance will have been eliminated in both combat and commercial types of aircraft, although in combat airplanes the larger percentage of wire replacement is caused by gunfire damage.
  • Keywords
    Airplanes; Fires; Insulation; Materials; Wires; Wiring;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1944.6440566
  • Filename
    6440566