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
Link To Document :
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