• DocumentCode
    1472133
  • Title

    D-C arc interruption for aircraft

  • Author

    Quill, J. S. ; Rader, L. T.

  • Author_Institution
    General Electric Company, Schenectady, N. Y.
  • Volume
    63
  • Issue
    12
  • fYear
    1944
  • Firstpage
    883
  • Lastpage
    888
  • Abstract
    THE present aircraft electric system uses 24 volts direct current; the future system will assuredly be of a higher voltage as aircraft and their generating systems increase in size. Whether it be direct current or alternating current depends on the relative merits of each.1 If the new system be alternating current the problem of arc interruption is not difficult. If the new system be direct current and above 24 volts, it has been assumed that the arc-interruption problem at altitude would be quite difficult. There is, however, little quantitative data available to bear this out. An investigation was therefore initiated to obtain preliminary data on arc-interruption problems introduced by the use of higher d-c voltages.
  • Keywords
    Aircraft; Humidity; Inductance; Interrupters; Resistance; Sea level; Switches;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1944.6440618
  • Filename
    6440618