Design and initial testing of a high speed 45 kW switched reluctance drive for aerospace application
This paper presents innovative research towards the development of a 45 kW high speed switched reluctance drive as an alternative starter-generator for future aero-engines. To perform such a function the machine had to be designed with a very wide constant power-speed range. During engine-start/moto...
| Main Authors: | , , , |
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| Format: | Article |
| Published: |
Institute of Electrical and Electronics Engineers
2017
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| Subjects: | |
| Online Access: | https://eprints.nottingham.ac.uk/43796/ |