A hybrid aircraft powerplant includes a turbine engine having a first shaft configured to output power from the turbine engine, a bypass fan, and an electric machine. The hybrid aircraft powerplant further includes a first mechanism configured to selectively engage the first shaft with a second shaft connected to the electric machine such that the power is output from the turbine engine to the electric machine. The hybrid aircraft powerplant further includes a second mechanism configured to selectively engage the first shaft with a third shaft connected to the bypass fan to output the power from the turbine engine to the bypass fan.


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    Title :

    PARALLEL HYBRID POWERPLANT WITH TURBOFAN ENGINE CORE



    Publication date :

    2024-10-31


    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



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