• DocumentCode
    1370238
  • Title

    A new circuit breaker for aircraft electric system: 40¿125 amperes, 120 volts A-C or D-C

  • Author

    Beall, B. S. ; Reifschneider, P. J.

  • Author_Institution
    General Electric Company, Philadelphia, Pa.
  • Volume
    71
  • Issue
    2
  • fYear
    1952
  • fDate
    4/1/1952 12:00:00 AM
  • Firstpage
    109
  • Lastpage
    112
  • Abstract
    RECOGNITION of the need for better protection of aircraft electric systems is indicated by the increasing use of reverse current circuit breakers in d-c generator circuits. Improved protection, however, must be extended to the entire electrical system and not confined to the generating equipment. Protective equipment for low capacity circuits in 28-volt d-c systems has been available. There has been a lack of protective equipment, however, for similar and higher capacity circuits in both a-c and d-c 120-volt systems. A new circuit breaker with ratings up to 125 amperes, 115 volts, a-c or d-c, recently developed is described. The requirements for such a circuit breaker are: 1. Interrupting capacity, 5,000 amperes sea level to 50,000 feet. 2. Ultimate trip current, 138 per cent of rated current at 25 degrees centigrade. 3. Continuous current capacity, 115 per cent of rated current at 25 degrees centigrade. 4. Two hundred per cent current calibration, 10¿100 seconds at 25 degrees centigrade. 5. Ambient temperature range, ¿55 degrees centigrade to 71 degrees centigrade.
  • Keywords
    Aircraft; Circuit breakers; Electron tubes; Solenoids; Springs; Temperature distribution; Valves;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1952.6371253
  • Filename
    6371253