• DocumentCode
    1026647
  • Title

    A 280y/120-Volt 120-Ampere Three-Pole 400-Cycle Electrically Operated Aircraft Circuit Breaker

  • Author

    Titus, C.H. ; Reifschneider, P.J.

  • Author_Institution
    Genral Eletric Company, Philadelphia, Pa.
  • Volume
    64
  • Issue
    8
  • fYear
    1945
  • Firstpage
    551
  • Lastpage
    555
  • Abstract
    With the selection of the 208Y/120-volt three-phase 400-cycle a-c system by the Army Air Forces for large aircraft, there has arisen the need for appropriate switchgear. In order to be applicable to the electric systems of such planes, swichgear must be able to perform its normal and emergency functions under the encountered conditions of temperature, pressure, humidity, vibration, and acceleration. This paper describes a 120-ampere remotely controlled electrically operated air circuit breaker designed for use as a bus sectionalizing, ring tie, or generator breaker on the 400-cycle grounded-neutral system. The interrupting rating of this breaker is 3,800 amperes at all pressures from sea level to 50,000 feet altitude. The closing solenoid and shunt trip coils have been designed to operate over a wide range of ambient temperature and control voltage. Weight and size, being primary considerations in aircraft equipment, have been held to a minimum.
  • Keywords
    Acceleration; Circuit breakers; Coils; Control systems; Humidity; Military aircraft; Ocean temperature; Sea level; Solenoids; Switchgear;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Transactions of the
  • Publisher
    ieee
  • ISSN
    0096-3860
  • Type

    jour

  • DOI
    10.1109/T-AIEE.1945.5059172
  • Filename
    5059172