The DOI matches its Crossref record; 114 of the 120 references it cites were found in a registry or an index.
Discussion on Electric Power Supply Systems for All Electric Aircraft
Open accessAbstract
The electric power supply system is one of the most important research areas within sustainable and energy-efficient aviation for more- and especially all electric aircraft. This paper discusses the history in electrification, current trends with a broad overview of research activities, state of the art of electrification and an initial proposal for a short-range aircraft. It gives an overview of the mission profile, electrical sources, approaches for the electrical distribution system and the required electrical loads. Current research aspects and questions are discussed, including voltage levels, semiconductor technology, topologies and reliability. Because of the importance for safety possible circuit breakers for the proposed concept are also presented and compared, leading to a initial proposal. Additionally, a very broad review of literature and a state of the art discussion of the wiring harness is given, showing that this topic comes with a high number of aspects and requirements. Finally, the conclusion sums up the most important results and gives an outlook on important future research topics.
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Citations
Cites
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“For a state-of-the-art MEA (Boing 787, 400 pax), the power demand of all electric loads is given as 1MVA [20].”
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“Hybrid circuit breakers are realizable in different topologies, [119], [127], [130]–[132].”
Background
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Cited by
Sorted by citations
A Review of Multilevel Inverter Topologies in Electric Vehicles: Current Status and Future Trends
Poorfakhraei, A., Narimani, M., & Emadi, A. (2021) · IEEE Open Journal of Power Electronics · doi:10.1109/ojpel.2021.3063550 · Cited by 424
“For example, in future all-electric aircrafts DC voltages of up to 3 kV will be utilized to supply the high-power electric motors [16].”
BackgroundElectric Power Systems in More and All Electric Aircraft: A Review
Barzkar, A., & Ghassemi, M. (2020) · IEEE Access · doi:10.1109/access.2020.3024168 · Cited by 360
“In [4], using an initial proposed schematic for an”
BackgroundMethodInfluentialComponents of Electrical Power Systems in More and All-Electric Aircraft: A Review
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“, CBs with arc chambers, are considered in the literature [7, 8, 38], but are not discussed in this article, since satisfying requirements for their work is too”
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“Conventionally, the insulation material can be a single layer made of PTFE, ethylene tetrafluoroethylene (ETFE), PI, or even materials used in cross-linked polyethylene (XLPE) [110].”
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“Inside the aircraft body with the environmental control system (ECS) intact, the critical electric field is 25 kV per cm [43], which informs the insulation design of individual power components.”
Background
Metadata
- Authors
- Schefer, H., Fauth, L., Kopp, T. H., Mallwitz, R., Friebe, J., & Kurrat, M.
- Affiliations
- Technische Universität Braunschweig (DE)
- Leibniz University Hannover (DE)
- Venue
- IEEE Access
- Published
- 2020
- Volume
- 8
- Pages
- 84188-84216
- ISSN
- 2169-3536 (ISSN-L)
- OpenAlex
- W3021371202
- Cited by
- 217
- References
- 120
- Citations by year
- 2026: 22 · 2025: 39 · 2024: 59 · 2023: 37 · 2022: 35 · 2021: 20 · 2020: 5
- FWCI
- 9.02
- Type
- journal article
- Language
- en
- Open access
- gold
- doi.org
- Licence
- Locations
- IEEE Access (publishedVersion, other-oa)
- DOAJ (DOAJ: Directory of Open Access Journals) (submittedVersion, cc-by-sa)
- Digitale Bibliothek Braunschweig (Verbundzentrale Göttingen (VZG)) (submittedVersion, cc-by)
- Funders
- Deutsche Forschungsgemeinschaft (German Research Foundation, DFG) through the Germany’s Excellence Strategy-EXC 2163/1-Sustainable and Energy Efficient Aviation (390881007)
- Open Access Publication Funds of the Technische Universität Braunschweig
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Advanced Aircraft Design and Technologies
- Physical Sciences › Engineering › Automotive Engineering › Electric and Hybrid Vehicle Technologies
- Physical Sciences › Engineering › Electrical and Electronic Engineering › Multilevel Inverters and Converters
- Keywords
- all-electric aircraft, power supply systems, aircraft electrification, electrical distribution systems, electrical load, voltage levels, semiconductor technology, power electronics topology, reliability, circuit breakers, wiring harness, short-range aircraft
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