Disclosed is a hybrid propulsion system for an aircraft, comprising an internal combustion engine (1) and a dedicated electrical power circuit, which are connected in parallel to a transmission system (5) for rotating a propeller (7), characterized in that it further comprises a decoupling free wheeling unit (60) between the internal combustion engine (1) from the transmission system (5).


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    Title :

    SYSTEME DE PROPULSION HYBRIDE POUR UN AERONEF


    Contributors:

    Publication date :

    2022-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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