Design of a six-phase fault-tolerant electric motor for an aircraft fuel pump

Flyur R. Ismagilov, Viacheslav Ye Vavilov, Ruslan D. Karimov, Valentina V. Ayguzina, Jorg Kammermann, Igor Bolvashenkov, Hans Georg Herzog

Publikation: Beitrag in Buch/Bericht/KonferenzbandKonferenzbeitragBegutachtung

5 Zitate (Scopus)

Abstract

This paper presents a multidisciplinary design algorithm of permanent magnet electric motors, which can be used in the design of six-phase fault-tolerant permanent magnet electric motors for aircraft fuel pumps. According to the the algorithm, a 15-kW 6000-rpm permanent magnet electric motor with a mass of 3.3 kg was calculated. Calculation steps were described by analytical methods and finite element method. Based on the analytical calculations, a three-dimensional model was created, which showed a high degree of convergence with the results of analytical calculations. A continuation of these studies will be the creation of a full-size permanent magnet electrical machine prototype for fuel pump and its tests, including tests as a part of a fuel pump.

OriginalspracheEnglisch
Titel2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Herausgeber (Verlag)Institute of Electrical and Electronics Engineers Inc.
ISBN (elektronisch)9781728137032
DOIs
PublikationsstatusVeröffentlicht - Mai 2019
Veranstaltung14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019 - Monte-Carlo, Monaco
Dauer: 8 Mai 201910 Mai 2019

Publikationsreihe

Name2019 14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019

Konferenz

Konferenz14th International Conference on Ecological Vehicles and Renewable Energies, EVER 2019
Land/GebietMonaco
OrtMonte-Carlo
Zeitraum8/05/1910/05/19

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