A high performance switched reluctance drive for aerospace applications
This thesis describes the work done in designing, building and testing a high speed, high power, switched reluctance drive as a possible candidate for a starter/generator application within a modem regional jet airframe. The machine was designed for a very wide constant power speed range and as such...
Main Author: | Borg Bartolo, James |
---|---|
Published: |
University of Nottingham
2016
|
Subjects: | |
Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.716368 |
Similar Items
-
Improving fault tolerant drives for aerospace applications
by: Wechsler, Andrew Philip
Published: (2013) -
High power factor rectification for aerospace systems
by: Chivite-Zabalza, F. Javier
Published: (2006) -
Comparative study of joining methods for a SMART aerospace application
by: Chau, Eric T. F.
Published: (2007) -
Application of context aware systems to support knowledge work in the aerospace
by: Xie, Yifan
Published: (2013) -
Development of a decision support framework for systems architecting in aerospace applications
by: Surendra, Amrith
Published: (2015)