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Titel:

Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System

Autor(en): C. Perren, V. Vavra, A. Gutiérrez Muñoz, L. Knöppel, D. Jäger
Zusammenfassung: The Hummingbird Gas Turbines (HGT) student research group focuses on the research on small gas turbines. In line with global trends in aviation, HGT is exploring a possible path towards minimising noise and carbon emissions. To this aim, the group is developing the Hummingbird Hybrid, a series hybrid configuration test bench rated at 5 kW electric power, consisting of a gas turbine, battery, and electric propulsors. This paper introduces the concept of the Hummingbird Hybrid, its goals, and the milestones achieved in the individual development areas so far. Furthermore, it relates the investigations done to current research on hybrid powertrains for manned and unmanned aerial vehicles and presents preliminary results of component tests.
Veranstaltung: Deutscher Luft- und Raumfahrtkongress 2021
Verlag, Ort: Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2021
Medientyp: Conference Paper
Sprache: englisch
Format: 21,0 x 29,7 cm, 10 Seiten
URN: urn:nbn:de:101:1-2021091715252791162638
DOI:10.25967/550130
Stichworte zum Inhalt: Hybrid Aircraft Propulsion, Electric Propulsor, Student Research Group
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Zitierform:Perren, C.; Vavra, V.; et al. (2021): Hummingbird Hybrid - Micro Hybrid Electric Aircraft Propulsion System. Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.. (Text). https://doi.org/10.25967/550130. urn:nbn:de:101:1-2021091715252791162638.
Veröffentlicht am: 17.09.2021