An embodiment includes a system for controlling blade pitch in a rotorcraft having an engine; a drive shaft with a first end and a second end and connected at the first end to the engine; a rotor with two or more blades connected to the second end of the drive shaft; and one or more actuators positioned adjacent to the rotor blades operable to change a blade pitch of the rotor blades.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Mast Dampener and Collective Pitch for a Rotocraft


    Beteiligte:
    CARTER JAY W (Autor:in) / LEWIS JEFFREY R (Autor:in) / ROBINSON M KEITH (Autor:in)

    Erscheinungsdatum :

    2020-04-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    MAST DAMPENER AND COLLECTIVE PITCH FOR A ROTORCRAFT

    CARTER JR JAY W / LEWIS JEFFREY R / ROBINSON M KEITH | Europäisches Patentamt | 2016

    Freier Zugriff

    MAST DAMPENER AND COLLECTIVE PITCH IN A ROTORCRAFT

    CARTER JAY W JR / LEWIS JEFFREY R / ROBINSON M KEITH | Europäisches Patentamt | 2015

    Freier Zugriff

    MAST DAMPENER FOR A ROTORCRAFT

    CARTER JR JAY W / LEWIS JEFFREY R / ROBINSON M KEITH | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTOCRAFT-CONVERTIBLE MOTORCAR

    PERINI FILIPPO / GUELFO NICOLA / LAGO ENRICO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Rotocraft Airworthiness

    Klemin, A. | Engineering Index Backfile | 1948