Conference
Study of Different Architectures of Fault Tolerant Actuator Using a Double-Star PM Motor
Abstract
In the context of more electric aircrafts, the use of electric actuators instead of hydraulic ones is one of the main topics of research and development in electrical engineering. A high level of reliability, the redundancy and the compactness are required for aircraft electrical actuators. For achieving these purposes the classical solution consists in using two identical actuators motorized each by one PM motor supplied by a VSI. In this …
Authors
Takorabet N; Caron JP; Vaseghi B; Nahid-Mobarakeh B; Meibody-Tabar F; Humbert G
Pagination
pp. 1-6
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Publication Date
October 1, 2008
DOI
10.1109/08ias.2008.27
Name of conference
2008 IEEE Industry Applications Society Annual Meeting