DocumentCode
2374420
Title
A Short-Stroke Permanent Magnet Aerospace Actuator with High Force-to-Mass Ratio
Author
Langley, F.L. ; Mellor, P.H.
Author_Institution
Dept. of Electr. & Electron. Eng., Bristol Univ.
fYear
2006
fDate
6-10 Nov. 2006
Firstpage
3199
Lastpage
3204
Abstract
High energy density rare earth permanent magnets have catalysed substantial improvements in the performance of linear actuators. The design of such a device using the 2D finite element method coupled to a particle swarm optimisation is described. A particular attribute of the design is that the pole shape has been optimised to ensure restoring magnetic forces act on the effector at zero current. A mathematical model is developed to study the dynamic performance of the device. A prototype was constructed from cobalt iron laminates and high energy product permanent magnets. Electrical winding tests and force measurements for the prototype are presented and compared with modelled values
Keywords
actuators; aerospace instrumentation; finite element analysis; magnetic forces; particle swarm optimisation; permanent magnets; 2D finite element method; cobalt iron laminates; high force-to-mass ratio; linear actuators; magnetic forces; particle swarm optimisation; short-stroke permanent magnet aerospace actuator; Design optimization; Finite element methods; Hydraulic actuators; Magnetic forces; Mathematical model; Particle swarm optimization; Permanent magnets; Poles and zeros; Prototypes; Shape;
fLanguage
English
Publisher
ieee
Conference_Titel
IEEE Industrial Electronics, IECON 2006 - 32nd Annual Conference on
Conference_Location
Paris
ISSN
1553-572X
Print_ISBN
1-4244-0390-1
Type
conf
DOI
10.1109/IECON.2006.347789
Filename
4153518
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