• DocumentCode
    1471846
  • Title

    Instrumentation of 400-cycle aircraft electric systems

  • Author

    Corson, A. J. ; Stimson, A. G. ; Soley, W. A.

  • Author_Institution
    General Electric Company, West Lynn, Mass.
  • Volume
    63
  • Issue
    11
  • fYear
    1944
  • Firstpage
    830
  • Lastpage
    834
  • Abstract
    THE use of 400-cycle alternating current1 as a power source on large aircraft originates the problem of adequate instrumentation at the distribution panel. Load conditions on a d-c system are determined by the simple parameters of voltage and current, whereas those of the a-c system include frequency and active and reactive power, in addition to voltage and current. Specifically, the flight engineer will require the following information for intelligent operation of the system:
  • Keywords
    Ammeters; Brushes; Coils; Instruments; Resistance; Resonant frequency; Torque;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1944.6440572
  • Filename
    6440572