A landing gear assembly is disclosed having a trailing arm for carrying a wheel, a shock absorber pivotally coupled to the arm for damping movement of the arm, and an articulated lock mechanism. The mechanism includes an upper and lower lock links each with a distal end respectively pivotally coupled to the shock and arm. Proximal ends of the lock links are pivotally coupled about a common axis to enable a distance between the distal ends to vary. The mechanism is lockable to lock the assembly in an extended or retracted configuration. When the assembly is in the extended or retracted configuration, the mechanism is locked respectively in an extended or retracted locking configuration, such that the distance between the distal ends of the lock links is substantially the same in either extended or retracted locking configuration.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Landing gear assembly


    Beteiligte:

    Erscheinungsdatum :

    24.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR ASSEMBLY

    PERKINS CHRISTOPHER JAMES / BOSCOLO MARCO / WHITE NICHOLAS et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    LANDING GEAR ASSEMBLY

    PERKINS CHRISTOPHER / BOSCOLO MARCO / WHITE NICK et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    LANDING GEAR ASSEMBLY

    PERKINS CHRISTOPHER / BOSCOLO MARCO / WHITE NICK et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    LANDING GEAR ASSEMBLY

    BENNETT IAN ROBERT | Europäisches Patentamt | 2019

    Freier Zugriff

    LANDING GEAR ASSEMBLY

    KEMPPAINEN JEFFREY S | Europäisches Patentamt | 2023

    Freier Zugriff