An aircraft propulsion system having dual powerplants is disclosed that includes a combustion powerplant on one wing of the aircraft and a hybrid-electric powerplant on the other wing of the aircraft, wherein the combustion powerplant includes a gas turbine turboprop engine and the hybrid-electric powerplant includes a heat engine and an electric motor that are arranged in either a parallel drive configuration or an in-line drive configuration.
AIRCRAFT PROPULSION SYSTEM HAVING HYBRID-ELECTRIC POWERPLANT AND COMBUSTION POWERPLANT
ANTRIEBSSYSTEM FÜR FLUGZEUGE MIT EINEM HYBRID-ELEKTRISCHEN TRIEBWERK UND VERBRENNUNGSTRIEBWERK
SYSTÈME DE PROPULSION D'AÉRONEF COMPRENANT UNE CENTRALE ÉLECTRIQUE HYBRIDE ET UNE CENTRALE ÉLECTRIQUE À COMBUSTION
2022-11-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke |
AIRCRAFT PROPULSION SYSTEM HAVING HYBRID-ELECTRIC POWERPLANT AND COMBUSTION POWERPLANT
European Patent Office | 2020
|AIRCRAFT PROPULSION SYSTEM HAVING HYBRID-ELECTRIC POWERPLANT AND COMBUSTION POWERPLANT
European Patent Office | 2020
|