• DocumentCode
    1490220
  • Title

    Computational technique for eddy current driven actuator

  • Author

    Zieve, Peter B. ; Garbini, Joseph L.

  • Author_Institution
    Electroimpact Inc., Seattle, WA, USA
  • Volume
    24
  • Issue
    6
  • fYear
    1988
  • fDate
    11/1/1988 12:00:00 AM
  • Firstpage
    3147
  • Lastpage
    3149
  • Abstract
    The magnetic analysis of a new class of eddy-current driven impulse actuators is considered. Driven by capacitor discharge, these actuators generate synchronized force pulses in excess of 100 kN with under 1 kN of recoil force transmitted too the positioner. This technology is being applied to low-payload industrial robots and mechanical impact deicing of aircraft lead edges. These applications are difficult to duplicate experimentally, so there is a demand for computer simulation. The high speed and transient motion of these actuators result in a significant but not constant contribution from velocity-coupled Faraday terms that is not accounted for in conventional finite-element simulation routines. A new computational technique is presented and verified experimentally
  • Keywords
    eddy currents; electric actuators; electrical engineering computing; electromagnetic devices; industrial robots; aircraft lead edges; capacitor discharge; computer simulation; eddy current driven actuator; low-payload industrial robots; magnetic analysis; mechanical impact deicing; recoil force; synchronized force pulses; transient motion; velocity-coupled Faraday terms; Actuators; Aerospace industry; Aircraft; Application software; Capacitors; Computer simulation; Eddy currents; Magnetic analysis; Pulse generation; Service robots;
  • fLanguage
    English
  • Journal_Title
    Magnetics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9464
  • Type

    jour

  • DOI
    10.1109/20.92363
  • Filename
    92363