A pusher rotorcraft is provided in one example embodiment and may include at least one engine in mechanical communication with a drop-down gearbox; a driveshaft in mechanical communication with the drop-down gearbox, a main rotor gearbox, and a tail system gearbox; a main rotor system in mechanical communication with the main rotor gearbox; an anti-torque system in mechanical communication with the tail system gearbox; and a pusher propeller system in mechanical communication with the tail system gearbox.


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    Titel :

    Pusher rotorcraft drivetrain


    Beteiligte:
    HEFNER LEVI C (Autor:in) / STAMPS FRANK B (Autor:in) / EWING ALAN C (Autor:in) / BURGESS JARET F (Autor:in) / CANNON CAREY W (Autor:in)

    Erscheinungsdatum :

    2020-12-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    PUSHER ROTORCRAFT DRIVETRAIN

    HEFNER LEVI C / STAMPS FRANK B / EWING ALAN C et al. | Europäisches Patentamt | 2020

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