DocumentCode :
3356373
Title :
High force linear actuator for an aeronautical application. Association with a fault tolerant converter.
Author :
Ziegler, N. ; Matt, D. ; Jac, J. ; Martire, T. ; Enrici, P.
Author_Institution :
Inst. d´´Electron. du Sud, Univ. Montpellier 2, Montpellier
fYear :
2007
fDate :
10-12 Sept. 2007
Firstpage :
76
Lastpage :
80
Abstract :
Electric actuators are replacing hydraulic actuators in the new aircrafts. A direct drive multi-airgap linear actuator has been designed and developed in order to replace a hydraulic actuator for a landing gear system application. The advantage of using a direct drive solution is to remove the mechanical transmission and consequently to increase the reliability. The experimental results show the high performances of this technology which reaches about 1000 N/kg and 5000 N/dm3. This article reports a special fault tolerant converter connected to the machine. This converter is also adapted to the constraints of reliability of the application.
Keywords :
air gaps; aircraft; electric actuators; fault tolerance; hydraulic actuators; power convertors; aeronautical application; direct drive multiairgap linear actuator; electric actuators; fault tolerant converter; high force linear actuator; hydraulic actuators; landing gear system application; mechanical transmission; Aircraft; Coils; Fault tolerance; Gears; Hydraulic actuators; Iron; Permanent magnets; Power system reliability; Prototypes; Saturation magnetization; direct drive; fault tolerant converter; high force mass ratio; linear actuator; multi-airgap; redundancy; reliability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Machines and Power Electronics, 2007. ACEMP '07. International Aegean Conference on
Conference_Location :
Bodrum
Print_ISBN :
978-1-4244-0890-0
Electronic_ISBN :
978-1-4244-0891-7
Type :
conf
DOI :
10.1109/ACEMP.2007.4510487
Filename :
4510487
Link To Document :
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