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
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