An aircraft system is provided that includes a first propulsor rotor, a first transmission, a second propulsor rotor, a second transmission and an intermittent combustion engine. The first propulsor rotor is rotatable about a first propulsor axis. The first transmission is coupled to the first propulsor rotor. The second propulsor rotor is rotatable about a second propulsor axis. The second transmission is coupled to the second propulsor rotor. The intermittent combustion engine is configured to drive rotation of the first propulsor rotor through the first transmission. The intermittent combustion engine is configured to drive rotation of the second propulsor rotor through the second transmission.


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    Titel :

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)


    Weitere Titelangaben:

    SYSTEME DE PROPULSION D'AERONEF AVEC MOTEUR(S) A COMBUSTION INTERMITTENTE


    Beteiligte:
    FREER RICHARD (Autor:in)

    Erscheinungsdatum :

    15.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | Europäisches Patentamt | 2024

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    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | Europäisches Patentamt | 2024

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    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

    FREER RICHARD | Europäisches Patentamt | 2024

    Freier Zugriff