Full Electric Aircraft and The Electrical Motors of The Propulsion Systems
DOI:
https://doi.org/10.54097/kwj8jg33Keywords:
Full electric aircraft, electric motors, propulsion system.Abstract
With the increasing awareness of environmental protection and the increasing reduction of oil resources, full electric aircraft as a green transportation tool has attracted much attention. The use of electric drive systems instead of traditional fuel power systems for full electric aircraft not only reduces reliance on fossil fuels, but also reduces emissions and noise, improving aircraft performance and safety. Electric motors are a critical component of full electric aircraft propulsion systems, providing the necessary power to drive the aircraft. This paper introduces the development history and classification of full electric aircraft and provides a comprehensive review of the various types of electric motors used in full electric aircraft propulsion, including permanent magnet synchronous motors, switched reluctance motors, axial flux motors, superconducting motors, and multi-phase motors. Additionally, the paper discusses the future trend and challenges for electric motors in full electric aircraft propulsion systems.
Downloads
References
Y. Tani, S. Morimoto, and M. Sanada, "Influence of number of poles, magnet arrangement, and current density on characteristics of inner and outer rotor PMSMs," in IEEE Ninth International Conference on Power Electronics & Drive Systems, Singapore, 2011.
B. M. Song, K. C. Chang, and J. Y. Choi, "Design of an outer-rotor-type permanent magnet motor for electric scooter propulsion systems," in International Power Electronics Conference, Sapporo, Japan: IEEE, 2010, pp. 2736-2742.
J. B. Jonathon, B. Mantas, and S. P. Stephen, "Optimizing performance variables for small unmanned aerial vehicle co-axial rotor systems," in Engineering Psychology and Cognitive Ergonomics. 9th International Conference, Orlando, FL, USA: LNCS, 2011, pp. 494-503.
M. J. L. Michael, J. C. Julio, and M. A. M. Mark, "Small UAV research and evolution in long endurance electric powered vehicles," in AIAA Infotech Aerospace 2007 Conference and Exhibi, Rohnert Park, California: LEAPFROG, 2007.
X. Shan, " Lightweight design and simulation study of all-electric aircraft drive motor," master’s thesis, Harbin Institute of Technology, Harbin, China, 2015.
Xueqin Luo, "Research on High Power Density Permanent Magnet Synchronous Motor for All-Electric Aircraft," PhD thesis, Harbin Institute of Technology, Harbin, China, 2018.
A. Hebala, S. Nuzzo, G. Volpe, et al., "Feasibility Design Study of High-Performance, High-Power-Density Propulsion Motor for Middle-Range Electric Aircraft," in Proceedings of the 29th IEEE International Symposium on Industrial Electronics, Delft, Netherlands, 2020, pp. 300-306.
Neethu S, Nikam SP, Singh S, et al., "High-Speed Coreless Axial-Flux Permanent-Magnet Motor with Printed Circuit Board Winding," IEEE Transactions on Industry Applications, vol. 55, no. 2, pp. 1954-1962, 2019.
M. S. Islam, R. Mikail, and I. Husain, "Slotless Lightweight Motor for Aerial Applications," IEEE Transactions on Industry Applications, vol. 55, no. 6, pp. 5789-5799, 2019.
C. D. Manolopoulos, M. F. Iacchetti, A. C. Smith, et al., "Stator Design and Performance of Superconducting Motors for Aerospace Electric Propulsion Systems," IEEE Transactions on Applied Superconductivity, vol. 28, no. 4, pp. 1-5, 2018.
S. Ullah, S. P. McDonald, R. Martin, et al., "A Permanent Magnet Assist, Segmented Rotor, Switched Reluctance Drive for Fault Tolerant Aerospace Applications," IEEE Transactions on Industry Applications, vol. 55, no. 1, pp. 298-305, 2019.
W. P. Cao, B. C. Mecrow, G. J. Atkinson, et al., "Overview of Electric Motor Technologies Used for More Electric Aircraft (MEA)," IEEE Transactions on Industrial Electronics, vol. 59, no. 9, pp. 3523-3531, 2012.
Downloads
Published
Issue
Section
License
Copyright (c) 2024 Highlights in Science, Engineering and Technology

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.







