On the Optimal Design of Coreless AFPM Machines with Halbach Array Rotors for Electric Aircraft Propulsion

Matin Vatani, Yaser Chulaee, Ali Mohammadi, David R. Stewart, John F. Eastham, Dan M. Ionel

Research output: Chapter or section in a book/report/conference proceedingChapter in a published conference proceeding

Abstract

This paper presents and evaluates the optimal design of a coreless axial flux permanent magnet (AFPM) motor for electric aircraft propulsion. Ferromagnetic cores are entirely removed from the machine's structure to improve the specific power density and efficiency. An approach for envelope design optimization of the proposed motor is introduced, considering the polarity as an independent variable and employing an evolutionary algorithm and 3D Finite Element Analysis (FEA). In addition to the proposed electric motor's electromagnetic performance, fault-tolerant capability and thermal management are considered in the optimization procedure. The optimization results and similar studies from power electronic and thermal management subsystems can be used to reach the system-level optimal performance. The optimization results are discussed through the evaluation of objectives' behavior and variables' trends toward the optimal design. It is shown that pole number and magnet-to-magnet gap are the essential geometric variables since they impact the active mass and efficiency of the machine, respectively.

Original languageEnglish
Title of host publication2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024
Place of PublicationU. S. A.
PublisherIEEE
ISBN (Electronic)9798350317664
ISBN (Print)9798350317671
DOIs
Publication statusPublished - 2024
Event2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 - Chicago, USA United States
Duration: 19 Jun 202421 Jun 2024

Publication series

Name2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024

Conference

Conference2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024
Country/TerritoryUSA United States
CityChicago
Period19/06/2421/06/24

Funding

This paper is based upon work supported by the National Aeronautics and Space Administration (NASA) through the University Leadership Initiative (ULI) #80NSSC22M0068. Any findings and conclusions expressed herein are those of the authors and do not necessarily reflect the views of NASA. The support of ANSYS Inc. and of University of Kentucky, the L. Stanley Pigman Chair in Power Endowment is also gratefully acknowledged.

FundersFunder number
National Aeronautics and Space Administration
University of Kentucky
Ansys
University Leadership Initiative80NSSC22M0068

    Keywords

    • 3D FEA
    • Axial flux PM machines
    • coreless AFPM
    • electric aircraft
    • Halbach array
    • number of poles

    ASJC Scopus subject areas

    • Energy Engineering and Power Technology
    • Automotive Engineering
    • Electrical and Electronic Engineering
    • Mechanical Engineering
    • Control and Optimization
    • Modelling and Simulation
    • Transportation

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