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.

A switched-Reluctance motor for aerospace application

VILLANI, Marco;TURSINI, MARCO;FABRI, GIUSEPPE;DI LEONARDO, LINO
2014-01-01

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.
2014
978-1-4799-4775-1
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11697/37630
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