Details
| Original language | English |
|---|---|
| Pages (from-to) | 114514-114539 |
| Number of pages | 26 |
| Journal | IEEE ACCESS |
| Volume | 10 |
| Publication status | Published - 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
ASJC Scopus subject areas
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In: IEEE ACCESS, Vol. 10, 26.10.2022, p. 114514-114539.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - Power Distribution and Propulsion System for an All-Electric Short-Range Commuter Aircraft
T2 - A Case Study
AU - Ebersberger, Janine
AU - Fauth, Leon
AU - Keuter, Ralf
AU - Cao, Yongtao
AU - Freund, Yannik
AU - Hanke-Rauschenbach, Richard
AU - Ponick, Bernd
AU - Mertens, Axel
AU - Friebe, Jens
N1 - Funding Information: This work was supported by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany's Excellence Strategy-EXC 2163/1-Sustainable and Energy Efficient Aviation under Project 390881007, and by the Open Access Publication Funds of the Leibniz Universität Hannover.
PY - 2022/10/26
Y1 - 2022/10/26
N2 - 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.
AB - 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.
KW - AEA
KW - aerospace electronics
KW - aircraft propulsion
KW - Aviation
KW - DC/DC converters
KW - electric power supply systems
KW - high voltage direct current
KW - power semiconductor devices
KW - reliability
KW - safety
KW - wide bandgap semiconductors
KW - wiring harness
UR - http://www.scopus.com/inward/record.url?scp=85141540797&partnerID=8YFLogxK
U2 - 10.1109/ACCESS.2022.3217650
DO - 10.1109/ACCESS.2022.3217650
M3 - Article
AN - SCOPUS:85141540797
VL - 10
SP - 114514
EP - 114539
JO - IEEE ACCESS
JF - IEEE ACCESS
SN - 2169-3536
ER -