• DocumentCode
    1346458
  • Title

    Aircraft tachometer indicator ¿ An analysis of design factors affecting starting performance

  • Author

    Akeley, L. T.

  • Author_Institution
    General Electric Company, Lynn, Mass.
  • Volume
    73
  • Issue
    6
  • fYear
    1955
  • Firstpage
    398
  • Lastpage
    403
  • Abstract
    FIFTY years of powered flight have brought changes to aircraft controls. A pilot cannot properly control the flight of today´s powerful machines without the use of instruments. Many of the newer instruments and control devices embody electronic elements for sensitivity and speed of response. Some have servo-system operation for highest accuracy. One of the oldest instruments, the engine speed indicator,1 still has an important place on the aircraft instrument panel. Without electronic components or servo elements the simple dragmagnet ¿ eddy-current disk type of tachometer instrument continues to provide a highly accurate and dependable service to the pilot.
  • Keywords
    Equations; Hysteresis motors; Magnetic hysteresis; Mathematical model; Rotors; Shafts; Torque;
  • 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.1955.6367089
  • Filename
    6367089