Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft
- Author(s): Ajith Balachandran 1 ; Mark Boden 1 ; Zhigang Sun 1 ; Stephen J. Forrest 2 ; Jason D. Ede 2 ; Geraint. W. Jewell 2
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View affiliations
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Affiliations:
1:
Rolls-Royce Electrical , UK ;
2: Rolls Royce University Technology Centre in Advanced Electrical Machines, The University of Sheffield , UK
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Affiliations:
1:
Rolls-Royce Electrical , UK ;
- Source:
Volume 2019, Issue 17,
June
2019,
p.
3474 – 3478
DOI: 10.1049/joe.2018.8235 , Online ISSN 2051-3305
This is an open access article published by the IET under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/3.0/)
Received
26/06/2018,
Accepted
30/07/2018,
Published
22/01/2019
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Inspec keywords: jet engines; aerospace engines; permanent magnet machines; starting; power electronics; aircraft power systems; avionics; aircraft; gas turbines
Other keywords: more-electric architecture; aero-engine starter-generator; power 95.0 kW; dual-channel machine-facing converter; electrical power offtake rating; permanent magnet machine; testing; associated power electronic converter; more-electric aircraft
Subjects: Power convertors and power supplies to apparatus; a.c. machines; Aerospace industry; Engines; Aerospace propulsion; d.c. machines; Control of electric power systems; Aerospace and avionic power supplies; Applied fluid mechanics
References
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1)
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1. Balachandran, A., Boden, M., Sun, Z., et al: ‘The design and development of an electrical power offtake solution for a more-electric concept’. Proc. of MEA2017 More-Electric Aircraft, Bordeaux, February 2017.
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2)
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2. Atallah, K., Zhu, Z.Q., Howe, D.: ‘An improved method for predicting iron losses in brushless permanent magnet DC drives’, IEEE Trans. Magn., 1992, 28, (5), pp. 2997–2999.
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http://iet.metastore.ingenta.com/content/journals/10.1049/joe.2018.8235
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