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Autor(en):
M.-C. Schwarze
Zusammenfassung:
In the scope of this technical paper a novel approach in the implementation of a hybrid-electric propulsion system is investigated on a standard short range airplane, in which the thrust of the aircraft engines is effectively combined with an electric-driven wheel propulsion system while the aircraft operates on the ground. The general system architecture, which could be effectively combined with Electric-Taxi systems, is shown both in principal and in detail with four sample architectures, including detailed weight estimation of the present and future system. Finally the impact of the E-Wheel system on the overall aircraft performance is evaluated. In this context the overall aircraft performance covers the field performance, mainly referring to the take-off and landing field-length, the accelerate-stop distance, the maximum payload capability and the impact of the system on overall fuel burn of the aircraft on standard short range missions.
Veranstaltung:
Deutscher Luft- und Raumfahrtkongress 2013, Stuttgart
Verlag, Ort:
Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2013
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 17 Seiten
URN:
urn:nbn:de:101:1-2013102515232
Stichworte zum Inhalt:
electric wheel, passenger aircraft
Verfügbarkeit:
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Kommentar:
Veröffentlicht am:
25.10.2013