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An approach to propulsion system modelling for the conceptual design of hybrid-electric general aviation aircraft

  • In this paper, an approach to propulsion system modelling for hybrid-electric general aviation aircraft is presented. Because the focus is on general aviation aircraft, only combinations of electric motors and reciprocating combustion engines are explored. Gas turbine hybrids will not be considered. The level of the component's models is appropriate for the conceptual design stage. They are simple and adaptable, so that a wide range of designs with morphologically different propulsive system architectures can be quickly compared. Modelling strategies for both mass and efficiency of each part of the propulsion system (engine, motor, battery and propeller) will be presented.

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Author:Felix FingerORCiD, R. Khalsa, Jörg Kreyer, Joscha MayntzORCiD, Carsten BraunORCiD, Peter Dahmann, Thomas EschORCiD, Hans Kemper, O. Schmitz, Michael Bragard
Parent Title (English):Deutscher Luft- und Raumfahrtkongress 2019, 30.9.-2.10.2019, Darmstadt
Document Type:Conference Proceeding
Language:English
Year of Completion:2019
Date of the Publication (Server):2020/04/23
Length:15 Seiten
Institutes:FH Aachen / Fachbereich Elektrotechnik und Informationstechnik
FH Aachen / Fachbereich Luft- und Raumfahrttechnik