• DocumentCode
    965870
  • Title

    Aircraft Secondary Power Generator with Direct Compensation Frequency Control

  • Author

    Johnson, L.J. ; Rauch, S.E.

  • Author_Institution
    Hallamore Electronics Co.,California.
  • Volume
    6
  • Issue
    4
  • fYear
    1959
  • fDate
    12/1/1959 12:00:00 AM
  • Firstpage
    259
  • Lastpage
    263
  • Abstract
    The variable speed constant frequency alternator system provides accurate frequency control independent of the shaft speed. The method employed is completely electrical in contrast with the more conventional mechanical speed control systems. The principle of operation depends upon a constant angular velocity magnetic field in the alternator armature, the angular velocity being the vector sum of the mechanical velocity of the shaft and the velocity of an electromagnetic rotating field induced by the excitation of a polyphase field winding. The polyphase field winding is driven by a variable frequency polyphase exciter, its frequency being directly proportional to the speed deviation from synchronous speed of the alternator rotor and shaft. The frequency control system as described in this paper is the open-loop type and, as such, accomplishes absolute frequency control with no errors arising from load or speed transients. An experimental brushless, constant frequency, three-phase alternator is discussed.
  • Keywords
    Aerospace control; Aircraft; Alternators; Angular velocity; Electromagnetic fields; Frequency control; Magnetic fields; Power generation; Shafts; Velocity control;
  • fLanguage
    English
  • Journal_Title
    Component Parts, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-2422
  • Type

    jour

  • DOI
    10.1109/TCP.1959.1136294
  • Filename
    1136294