Electric and hybrid-electric aircraft propulsion systems: development, difficulties and opportunities

Research Article
Open access

Electric and hybrid-electric aircraft propulsion systems: development, difficulties and opportunities

Zirui Huang 1*
  • 1 University of Leeds, Department of Electrical and Electronic Engineering, Leeds, UK, LS2 8DS    
  • *corresponding author el20z2h@leeds.ac.uk
TNS Vol.5
ISSN (Print): 2753-8826
ISSN (Online): 2753-8818
ISBN (Print): 978-1-915371-53-9
ISBN (Online): 978-1-915371-54-6

Abstract

As the world has grown rapidly over the past century, so has the aviation industry as a whole. This has led to a huge volume of aviation market and at the same time the aviation market excessive reliance on fuel, with a consequent huge environmental impact. As a global community, we are moving towards an electrified transport architecture. And some studies of aircraft propulsion systems have shown that electric and hybrid electric propulsion systems offer significant benefits over conventional fuel propulsion systems. However, there are also some researches have shown that while some electrified propulsion strategies can result in significant reductions in CO2 emissions, the overall cost of the aircraft can also increase significantly. The economic efforts made in terms of purely electric and hybrid propulsion have not been significant, so this technology is not yet in significant use in the aviation market. This paper considers some of these systems and analyses their structural advantages, technical requirements, etc. This is followed by a discussion of the current difficulties and future trends in the application of purely electric and hybrid propulsion systems. It is also significant to convey that the current immaturity of this technology and the areas for improvement.

Keywords:

all electric, hybrid electric, propulsion system, clean energy, aviation market, emission target.

Huang,Z. (2023). Electric and hybrid-electric aircraft propulsion systems: development, difficulties and opportunities. Theoretical and Natural Science,5,28-34.
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References

[1]. Hannah Ritchie, Climate change and flying: what share of global CO2 emissions come from aviation, by our world in data, October 22, 2020. https://ourworldindata.org/co2-emissions-from-aviation.

[2]. Lee D. S. & Fahey D. W. & Skowron A. et al. The contribution of global aviation to anthropogenic climate forcing for 2000 to 2018 [J] Atmospheric Environment, Vol. 244, 117843, 2021, pp. 1-28.

[3]. Wheeler P., Sirimanna T. S., Bozhko S. & Haran K.S., Electric/Hybrid-Electric Aircraft Propulsion Systems [J] IEEE, vol. 109, no. 6, 2021, pp. 1115-1127.

[4]. Guo Y., Zhu L., Wang X., Qiu X., Qian W., Wang L., Assessing environmental impact of NOX and SO2 emissions in textiles production with chemical footprint, Science of The Total Environment, Vol. 831, 154961, 2022.

[5]. Kellermann H., Fuhrmann S., Shamiyeh M., Hornung M., Design of a Battery Cooling System for Hybrid Electric Aircraft, American Institute of Aeronautics and Astronautics, May 2, 2022.

[6]. Xie Y., Savvarisal A., Tsourdos A., Zhang D., Gu J., Review of hybrid electric powered aircraft, its conceptual design and energy management methodologies, Chinese Journal of Aeronautics, Vol. 34, no. 4, 2021, pp.432-450.

[7]. Riboldi C.E.D, Gualdoni F., An integrated approach to the preliminary weight sizing of small electric aircraft, Aerospace Science and Technology, Vol. 58, 2016, pp.134-149.

[8]. IATA, Aircraft Technology Roadmap to 2050, https://www.iata.org/contentassets/8d19e716636a47c184e7221c77563c93/Technology-roadmap-2050.pdf.

[9]. Bowman C. L. & Felder J. L. & Marien T.V, Turbo- and Hybrid-Electrified Aircraft Propulsion Concepts for Commercial Transport, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), 2018, pp. 1-8.

[10]. Rendón, M. A. & Sánchez R.C.D., Gallo M. J. Anzai A. H. Aircraft Hybrid-Electric Propulsion: Development Trends, Challenges and Opportunities. J Control Autom Electr Syst 32, 1244–1268, 2021.

[11]. Donateo T., Ficarella A. & Spedicato L, A method to analyze and optimize hybrid electric architecture applied to unmanned aerial vehicles, June 19, 2018.

Cite this article

Huang,Z. (2023). Electric and hybrid-electric aircraft propulsion systems: development, difficulties and opportunities. Theoretical and Natural Science,5,28-34.

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The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.

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About volume

Volume title: Proceedings of the 2nd International Conference on Computing Innovation and Applied Physics (CONF-CIAP 2023)

ISBN：978-1-915371-53-9(Print) / 978-1-915371-54-6(Online)
Editor：Marwan Omar, Roman Bauer
Conference website: https://www.confciap.org/
Conference date: 25 March 2023
Series: Theoretical and Natural Science
Volume number: Vol.5
ISSN：2753-8818(Print) / 2753-8826(Online)

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References

[1]. Hannah Ritchie, Climate change and flying: what share of global CO2 emissions come from aviation, by our world in data, October 22, 2020. https://ourworldindata.org/co2-emissions-from-aviation.

[2]. Lee D. S. & Fahey D. W. & Skowron A. et al. The contribution of global aviation to anthropogenic climate forcing for 2000 to 2018 [J] Atmospheric Environment, Vol. 244, 117843, 2021, pp. 1-28.

[3]. Wheeler P., Sirimanna T. S., Bozhko S. & Haran K.S., Electric/Hybrid-Electric Aircraft Propulsion Systems [J] IEEE, vol. 109, no. 6, 2021, pp. 1115-1127.

[4]. Guo Y., Zhu L., Wang X., Qiu X., Qian W., Wang L., Assessing environmental impact of NOX and SO2 emissions in textiles production with chemical footprint, Science of The Total Environment, Vol. 831, 154961, 2022.

[5]. Kellermann H., Fuhrmann S., Shamiyeh M., Hornung M., Design of a Battery Cooling System for Hybrid Electric Aircraft, American Institute of Aeronautics and Astronautics, May 2, 2022.

[6]. Xie Y., Savvarisal A., Tsourdos A., Zhang D., Gu J., Review of hybrid electric powered aircraft, its conceptual design and energy management methodologies, Chinese Journal of Aeronautics, Vol. 34, no. 4, 2021, pp.432-450.

[7]. Riboldi C.E.D, Gualdoni F., An integrated approach to the preliminary weight sizing of small electric aircraft, Aerospace Science and Technology, Vol. 58, 2016, pp.134-149.

[8]. IATA, Aircraft Technology Roadmap to 2050, https://www.iata.org/contentassets/8d19e716636a47c184e7221c77563c93/Technology-roadmap-2050.pdf.

[9]. Bowman C. L. & Felder J. L. & Marien T.V, Turbo- and Hybrid-Electrified Aircraft Propulsion Concepts for Commercial Transport, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), 2018, pp. 1-8.

[10]. Rendón, M. A. & Sánchez R.C.D., Gallo M. J. Anzai A. H. Aircraft Hybrid-Electric Propulsion: Development Trends, Challenges and Opportunities. J Control Autom Electr Syst 32, 1244–1268, 2021.

[11]. Donateo T., Ficarella A. & Spedicato L, A method to analyze and optimize hybrid electric architecture applied to unmanned aerial vehicles, June 19, 2018.

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