DocumentCode :
157395
Title :
A switched-reluctance motor for aerospace application
Author :
Villani, M. ; Tursini, Marco ; Fabri, G. ; Di Leonardo, Lino
Author_Institution :
Dept. of Ind. & Inf. Eng. & Econ., Univ. of L´Aquila, L´Aquila, Italy
fYear :
2014
fDate :
2-5 Sept. 2014
Firstpage :
2073
Lastpage :
2079
Abstract :
This paper presents a five-phase switched reluctance motor designed to satisfy the requirements of flap actuators in medium size aircrafts. In normal operation the machine operates with two-phases conducting simultaneously but it is designed to satisfy the load specifications also with one or two phases faulted. The finite-element studies aiming to predict the faulty mode performance are presented. Experimental tests on the motor prototype are included, which confirm its capability to satisfy the planned degraded modes of operation.
Keywords :
actuators; aircraft; finite element analysis; reluctance motors; aerospace application; faulty mode performance; finite-element studies; five-phase switched reluctance motor; flap actuators; load specifications; medium size aircrafts; motor prototype; Inductance; Permanent magnet motors; Reluctance motors; Rotors; Stator windings; Torque; Aerospace; actuator; aircraft; design optimization; electric motor; fault-tolerant; finite element analysis; multi-phase; switched-reluctance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Machines (ICEM), 2014 International Conference on
Conference_Location :
Berlin
Type :
conf
DOI :
10.1109/ICELMACH.2014.6960470
Filename :
6960470
Link To Document :
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