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 language | English |
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Title of host publication | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
ISBN (Electronic) | 9798350317664 |
DOIs | |
State | Published - 2024 |
Event | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 - Chicago, United States Duration: Jun 19 2024 → Jun 21 2024 |
Publication series
Name | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
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Conference
Conference | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
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Country/Territory | United States |
City | Chicago |
Period | 6/19/24 → 6/21/24 |
Bibliographical note
Publisher Copyright:© 2024 IEEE.
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.
Funders | Funder number |
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National Aeronautics and Space Administration | |
University of Kentucky | |
ANSYS | |
NASA University Leadership Initiative | 80NSSC22M0068 |
Keywords
- 3D FEA
- Axial flux PM machines
- Halbach array
- coreless AFPM
- electric aircraft
- number of poles
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Automotive Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering
- Control and Optimization
- Modeling and Simulation
- Transportation