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.


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    Title :

    AIRCRAFT PROPULSION SYSTEM HAVING HYBRID-ELECTRIC POWERPLANT AND COMBUSTION POWERPLANT


    Additional title:

    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


    Contributors:

    Publication date :

    2022-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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



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