A landing gear system includes an axle having an internal cavity and a wheel rotatably coupled to the axle. A drive shaft is mounted within the cavity to be rotatable about an axis. The landing gear system further includes a rod slidably mounted within the drive shaft and a clutch. The clutch has a first portion that is coupled to the rod and rotates with the drive shaft. A second portion of the clutch is fixedly coupled to the wheel. The rod selectively reciprocates along the axis between a first position and a second position to engage and disengage the clutch.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Clutch assembly for autonomous taxiing of aircraft


    Beteiligte:
    SCHMIDT ROBERT KYLE (Autor:in) / AMBERG STEVE (Autor:in) / BROWN JASON (Autor:in)

    Erscheinungsdatum :

    2022-11-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    CLUTCH ASSEMBLY FOR AUTONOMOUS TAXIING OF AIRCRAFT

    SCHMIDT ROBERT KYLE / AMBERG STEVE / BROWN JASON | Europäisches Patentamt | 2024

    Freier Zugriff

    Clutch assembly for autonomous taxiing of aircraft

    ROBERT KYLE SCHMIDT / AMBERG STEVE / BROWN JASON | Europäisches Patentamt | 2022

    Freier Zugriff

    CLUTCH ASSEMBLY FOR AUTONOMOUS TAXIING OF AIRCRAFT

    SCHMIDT ROBERT KYLE / AMBERG STEVE / BROWN JASON | Europäisches Patentamt | 2021

    Freier Zugriff

    CLUTCH ASSEMBLY FOR AUTONOMOUS TAXIING OF AIRCRAFT

    SCHMIDT ROBERT KYLE / AMBERG STEVE / BROWN JASON | Europäisches Patentamt | 2021

    Freier Zugriff

    CLUTCH ASSEMBLY FOR AUTONOMOUS TAXIING OF AIRCRAFT

    SCHMIDT ROBERT KYLE / AMBERG STEVE / BROWN JASON | Europäisches Patentamt | 2021

    Freier Zugriff