• DocumentCode
    1425489
  • Title

    Aircraft a.c. electrical systems using changeover contactors and rapid fault clearance

  • Author

    Sims, R.F. ; McKenzie, R.L.A.

  • Author_Institution
    Royal Aircraft Establishment, Farnborough, UK
  • Volume
    114
  • Issue
    8
  • fYear
    1967
  • fDate
    8/1/1967 12:00:00 AM
  • Firstpage
    1099
  • Lastpage
    1104
  • Abstract
    Conventional aircraft electrical systems are liable to interruptions or disturbances for up to several seconds under fault conditions. Such interruptions may be limited to substantially less than 100ms by the use of a very simple nonparalleled system employing changeover contactors and forms of undervoltage and overvoltage protection which do not depend on time delays to discriminate between real faults and switching transients. The overvoltage protection acts rapidly enough to prevent the voltage rising to destructive levels in the event of, say, a regulator fault. In its simplest form, with two generators or with four generators arranged in two subsystems, the total generator capacity must be twice the maximum load, to ensure, that the failure of one generator will not result in loss of load, in the 2-generator case, this can be reduced to four thirds if the load can be divided into three equal parts, one of which may be discarded in the event of a generator failure. In the 4-generator case, the factor may be four thirds, with no loss of load with one generator failure if it is possible to divide the load into six equal parts.
  • Keywords
    AC generators; aircraft; contactors; fault currents; power supplies to apparatus; relay protection;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineers, Proceedings of the Institution of
  • Publisher
    iet
  • ISSN
    0020-3270
  • Type

    jour

  • DOI
    10.1049/piee.1967.0211
  • Filename
    5249890