Resumen
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.
| Idioma original | English |
|---|---|
| Título de la publicación alojada | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
| ISBN (versión digital) | 9798350317664 |
| DOI | |
| Estado | Published - 2024 |
| Evento | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 - Chicago, United States Duración: jun 19 2024 → jun 21 2024 |
Serie de la publicación
| Nombre | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
|---|
Conference
| Conference | 2024 IEEE Transportation Electrification Conference and Expo, ITEC 2024 |
|---|---|
| País/Territorio | United States |
| Ciudad | Chicago |
| Período | 6/19/24 → 6/21/24 |
Nota bibliográfica
Publisher Copyright:© 2024 IEEE.
Financiación
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.
| Financiadores | Número del financiador |
|---|---|
| National Aeronautics and Space Administration | |
| University of Kentucky | |
| ANSYS | |
| NASA University Leadership Initiative | 80NSSC22M0068 |
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Automotive Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering
- Control and Optimization
- Modeling and Simulation
- Transportation
Huella
Profundice en los temas de investigación de 'On the Optimal Design of Coreless AFPM Machines with Halbach Array Rotors for Electric Aircraft Propulsion'. En conjunto forman una huella única.Citar esto
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