Designing an advanced electrical motor for propulsion of electric aircraft

Dmitry Golovanov; David Gerada; Zeyuan Xu; Chris Gerada; Andrew Page; Tadashi Sawata

doi:10.2514/6.2019-4482

Designing an advanced electrical motor for propulsion of electric aircraft

Dmitry Golovanov
, David Gerada
, Zeyuan Xu
, Chris Gerada
, Andrew Page
, Tadashi Sawata

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

24 Citations (Scopus)

Abstract

A prototype motor rated for 500 kW 3,000 rpm has been developed for aircraft electric propulsion. The design of the motor was optimized using a coupled parameter problem of electromagnetic, mechanical and thermal performances. A high power density of over 5 kW/kg is demonstrated without resorting to intensive direct liquid cooling. The design process considered variables including the winding conductor type, pole/slot combination, dimensions, winding layout and power electronics requirements. The final chosen design is a 3×3-phase 30-pole 36-slot surface permanent magnet motor with Cobalt-Iron laminations, Sm₂Co₁₇ Halbach array magnets and litz wire for an optimum performance.

Original language	English
Title of host publication	AIAA Propulsion and Energy Forum and Exposition, 2019
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624105906
DOIs	https://doi.org/10.2514/6.2019-4482
Publication status	Published - 2019
Event	AIAA Propulsion and Energy Forum and Exposition, 2019 - Indianapolis, United States Duration: 19 Aug 2019 → 22 Aug 2019

Publication series

Name	AIAA Propulsion and Energy Forum and Exposition, 2019

Conference

Conference	AIAA Propulsion and Energy Forum and Exposition, 2019
Country/Territory	United States
City	Indianapolis
Period	19/08/19 → 22/08/19

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

ASJC Scopus subject areas

General Energy
Aerospace Engineering
Electrical and Electronic Engineering
Control and Systems Engineering
Mechanical Engineering

Access to Document

10.2514/6.2019-4482

Cite this

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title = "Designing an advanced electrical motor for propulsion of electric aircraft",

abstract = "A prototype motor rated for 500 kW 3,000 rpm has been developed for aircraft electric propulsion. The design of the motor was optimized using a coupled parameter problem of electromagnetic, mechanical and thermal performances. A high power density of over 5 kW/kg is demonstrated without resorting to intensive direct liquid cooling. The design process considered variables including the winding conductor type, pole/slot combination, dimensions, winding layout and power electronics requirements. The final chosen design is a 3×3-phase 30-pole 36-slot surface permanent magnet motor with Cobalt-Iron laminations, Sm2Co17 Halbach array magnets and litz wire for an optimum performance.",

author = "Dmitry Golovanov and David Gerada and Zeyuan Xu and Chris Gerada and Andrew Page and Tadashi Sawata",

note = "Publisher Copyright: {\textcopyright} 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; AIAA Propulsion and Energy Forum and Exposition, 2019 ; Conference date: 19-08-2019 Through 22-08-2019",

year = "2019",

doi = "10.2514/6.2019-4482",

language = "English",

isbn = "9781624105906",

series = "AIAA Propulsion and Energy Forum and Exposition, 2019",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "AIAA Propulsion and Energy Forum and Exposition, 2019",

}

Golovanov, D, Gerada, D, Xu, Z, Gerada, C, Page, A & Sawata, T 2019, Designing an advanced electrical motor for propulsion of electric aircraft. in AIAA Propulsion and Energy Forum and Exposition, 2019. AIAA Propulsion and Energy Forum and Exposition, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, United States, 19/08/19. https://doi.org/10.2514/6.2019-4482

Designing an advanced electrical motor for propulsion of electric aircraft. / Golovanov, Dmitry; Gerada, David; Xu, Zeyuan et al.
AIAA Propulsion and Energy Forum and Exposition, 2019. American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (AIAA Propulsion and Energy Forum and Exposition, 2019).

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Designing an advanced electrical motor for propulsion of electric aircraft

AU - Golovanov, Dmitry

AU - Gerada, David

AU - Xu, Zeyuan

AU - Gerada, Chris

AU - Page, Andrew

AU - Sawata, Tadashi

PY - 2019

Y1 - 2019

N2 - A prototype motor rated for 500 kW 3,000 rpm has been developed for aircraft electric propulsion. The design of the motor was optimized using a coupled parameter problem of electromagnetic, mechanical and thermal performances. A high power density of over 5 kW/kg is demonstrated without resorting to intensive direct liquid cooling. The design process considered variables including the winding conductor type, pole/slot combination, dimensions, winding layout and power electronics requirements. The final chosen design is a 3×3-phase 30-pole 36-slot surface permanent magnet motor with Cobalt-Iron laminations, Sm2Co17 Halbach array magnets and litz wire for an optimum performance.

AB - A prototype motor rated for 500 kW 3,000 rpm has been developed for aircraft electric propulsion. The design of the motor was optimized using a coupled parameter problem of electromagnetic, mechanical and thermal performances. A high power density of over 5 kW/kg is demonstrated without resorting to intensive direct liquid cooling. The design process considered variables including the winding conductor type, pole/slot combination, dimensions, winding layout and power electronics requirements. The final chosen design is a 3×3-phase 30-pole 36-slot surface permanent magnet motor with Cobalt-Iron laminations, Sm2Co17 Halbach array magnets and litz wire for an optimum performance.

UR - https://www.scopus.com/pages/publications/85095979510

U2 - 10.2514/6.2019-4482

DO - 10.2514/6.2019-4482

M3 - Conference contribution

AN - SCOPUS:85095979510

SN - 9781624105906

T3 - AIAA Propulsion and Energy Forum and Exposition, 2019

BT - AIAA Propulsion and Energy Forum and Exposition, 2019

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - AIAA Propulsion and Energy Forum and Exposition, 2019

Y2 - 19 August 2019 through 22 August 2019

ER -

Designing an advanced electrical motor for propulsion of electric aircraft

Abstract

Publication series

Conference

UN SDGs

ASJC Scopus subject areas

Access to Document

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