An aircraft propulsion system (100) includes at least one hybrid-electric power plant (101) for delivering power to an air mover (106) for propelling an aircraft (10). The at least one hybrid-electric power plant (101) includes a first thermal engine (102) and an electrical motor (104) arranged in a parallel drive configuration or in an in-line drive configuration. The aircraft propulsion system (100) includes a second thermal engine (108) operatively connected to the electrical motor (104) to power the electrical motor (104). A method for providing propulsion to an aircraft (10) includes delivering power to an air mover (106) for propelling the aircraft (10) with at least one hybrid-electric power plant (101).


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    Title :

    DUAL ENGINE HYBRID-ELECTRIC AIRCRAFT


    Additional title:

    ZWEIMOTORIGES HYBRID-ELEKTROFAHRZEUG
    AÉRONEF ÉLECTRIQUE HYBRIDE À DOUBLE MOTEUR


    Contributors:

    Publication date :

    2021-03-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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