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Non-Salient Brushless Synchronous Generator Main Exciter Design for More Electric Aircraft

Author

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  • Filip Kutt

    (Faculty of Electrical and Control Engineering, Gdańsk University of Technology, 80-233 Gdańsk, Poland
    These authors contributed equally to this work.)

  • Michał Michna

    (Faculty of Electrical and Control Engineering, Gdańsk University of Technology, 80-233 Gdańsk, Poland
    These authors contributed equally to this work.)

  • Grzegorz Kostro

    (Faculty of Electrical and Control Engineering, Gdańsk University of Technology, 80-233 Gdańsk, Poland
    These authors contributed equally to this work.)

Abstract

This paper presents a prototype of high speed brushless synchronous generators (BSG) design for the application in autonomous electric power generation systems (e.g., airplane power grid). Commonly used salient pole field of the main generator part of BSG was replaced with a prototype non-salient pole field. The main objective of the research is an investigation into the advantages and disadvantages of a cylindrical field of the main generator part of BSG over the original salient pole field. The design process of the prototype generator is presented with a focus on the electromagnetic and mechanical finite element method (FEM) analysis. The measurements of prototype and commercial BSG were conducted for the nominal speed of 8 krpm. The advantages and disadvantages of the proposed solution were established based on measurements in load and no-load conditions.

Suggested Citation

  • Filip Kutt & Michał Michna & Grzegorz Kostro, 2020. "Non-Salient Brushless Synchronous Generator Main Exciter Design for More Electric Aircraft," Energies, MDPI, vol. 13(11), pages 1-17, May.
  • Handle: RePEc:gam:jeners:v:13:y:2020:i:11:p:2696-:d:363507
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    References listed on IDEAS

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    1. Giampaolo Buticchi & David Gerada & Luigi Alberti & Michael Galea & Pat Wheeler & Serhiy Bozhko & Sergei Peresada & He Zhang & Chengming Zhang & Chris Gerada, 2019. "Challenges of the Optimization of a High-Speed Induction Machine for Naval Applications," Energies, MDPI, vol. 12(12), pages 1-20, June.
    2. Markus Henke & Gerrit Narjes & Jan Hoffmann & Constantin Wohlers & Stefan Urbanek & Christian Heister & Jörn Steinbrink & Wolf-Rüdiger Canders & Bernd Ponick, 2018. "Challenges and Opportunities of Very Light High-Performance Electric Drives for Aviation," Energies, MDPI, vol. 11(2), pages 1-25, February.
    3. Yerai Moreno & Gaizka Almandoz & Aritz Egea & Patxi Madina & Ana Julia Escalada, 2020. "Multi-Physics Tool for Electrical Machine Sizing," Energies, MDPI, vol. 13(7), pages 1-18, April.
    4. Ounis, H. & Sareni, B. & Roboam, X. & De Andrade, A., 2016. "Multi-level integrated optimal design for power systems of more electric aircraft," Mathematics and Computers in Simulation (MATCOM), Elsevier, vol. 130(C), pages 223-235.
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    Cited by:

    1. Massimo Caruso & Antonino Oscar Di Tommaso & Giuseppe Lisciandrello & Rosa Anna Mastromauro & Rosario Miceli & Claudio Nevoloso & Ciro Spataro & Marco Trapanese, 2020. "A General and Accurate Measurement Procedure for the Detection of Power Losses Variations in Permanent Magnet Synchronous Motor Drives," Energies, MDPI, vol. 13(21), pages 1-19, November.

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