Journal article
Switched Reluctance Motor Design for a Light Sport Aircraft Application
Abstract
This paper presents the design of a switched reluctance motor (SRM) for a direct-drive propulsion application for a light sport aircraft. The SRM is designed to replace a 70 kW permanent magnet synchronous motor used in aerospace application with similar dimensional constraints. As a means of achieving high torque density and efficiency, a multi-objective design framework is used to optimize the geometry parameters of the motor. In order to …
Authors
Abdollahi ME; Zahid A; Vaks N; Bilgin B
Journal
Machines, Vol. 11, No. 3,
Publisher
MDPI
DOI
10.3390/machines11030362
ISSN
2075-1702