An aircraft system is provided that includes a first propulsor, a second propulsor, a drivetrain and an intermittent combustion engine. The first propulsor includes a first propulsor rotor and a first vane array. The second propulsor includes a second propulsor rotor and a second vane array. The drivetrain includes a drive structure and a transmission. An output of the transmission is coupled to the first propulsor rotor and the second propulsor rotor through the drive structure. The intermittent combustion engine is configured to drive rotation of the first propulsor rotor and the second propulsor rotor through the drivetrain.


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    Title :

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)


    Contributors:

    Publication date :

    2024-01-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | European Patent Office | 2024

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | European Patent Office | 2024

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | European Patent Office | 2024

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | European Patent Office | 2024

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | European Patent Office | 2024

    Free access