Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft: A Case Study

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Original languageEnglish
Pages (from-to)114514-114539
Number of pages26
JournalIEEE ACCESS
Volume10
Publication statusPublished - 26 Oct 2022

Abstract

To participate in the transition towards a sustainable use of energy, the aircraft sector needs to be transformed with respect to the energy carrier and propulsion methods. For smaller aircraft, a battery-electric approach is promising. While this will require extensive research and design as well as the application of advanced components which are partly not available to this date, general design rules and decisive parameters and components can already by deduced. This publication presents the exemplary design of the full propulsion system for a small commuter aircraft. This serves as a case study to highlight the influence of components and parameters on the overall efficiency and weight of the system. By that, future research can be directed towards the areas of high impact on the realization of all electric aircraft.

Keywords

    AEA, aerospace electronics, aircraft propulsion, Aviation, DC/DC converters, electric power supply systems, high voltage direct current, power semiconductor devices, reliability, safety, wide bandgap semiconductors, wiring harness

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Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft: A Case Study. / Ebersberger, Janine; Fauth, Leon; Keuter, Ralf et al.
In: IEEE ACCESS, Vol. 10, 26.10.2022, p. 114514-114539.

Research output: Contribution to journalArticleResearchpeer review

Ebersberger, J, Fauth, L, Keuter, R, Cao, Y, Freund, Y, Hanke-Rauschenbach, R, Ponick, B, Mertens, A & Friebe, J 2022, 'Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft: A Case Study', IEEE ACCESS, vol. 10, pp. 114514-114539. https://doi.org/10.1109/ACCESS.2022.3217650
Ebersberger, J., Fauth, L., Keuter, R., Cao, Y., Freund, Y., Hanke-Rauschenbach, R., Ponick, B., Mertens, A., & Friebe, J. (2022). Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft: A Case Study. IEEE ACCESS, 10, 114514-114539. https://doi.org/10.1109/ACCESS.2022.3217650
Ebersberger J, Fauth L, Keuter R, Cao Y, Freund Y, Hanke-Rauschenbach R et al. Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft: A Case Study. IEEE ACCESS. 2022 Oct 26;10:114514-114539. doi: 10.1109/ACCESS.2022.3217650
Ebersberger, Janine ; Fauth, Leon ; Keuter, Ralf et al. / Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft : A Case Study. In: IEEE ACCESS. 2022 ; Vol. 10. pp. 114514-114539.
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abstract = "To participate in the transition towards a sustainable use of energy, the aircraft sector needs to be transformed with respect to the energy carrier and propulsion methods. For smaller aircraft, a battery-electric approach is promising. While this will require extensive research and design as well as the application of advanced components which are partly not available to this date, general design rules and decisive parameters and components can already by deduced. This publication presents the exemplary design of the full propulsion system for a small commuter aircraft. This serves as a case study to highlight the influence of components and parameters on the overall efficiency and weight of the system. By that, future research can be directed towards the areas of high impact on the realization of all electric aircraft.",
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