access icon openaccess Design, construction, and testing of an aero-engine starter-generator for the more-electric aircraft

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

    1. 1)
      • 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.
    2. 2)
      • 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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