A locking device locks a landing gear mounted in rotation on an aircraft and includes a deployment hydraulic jack including a first chamber connected to a first hydraulic supply and a second chamber connected to a second hydraulic supply. The locking device includes a hydraulic actuator connected to a rotary distributor. The rotary distributor includes a coupling operationally connecting the rotary distributor to a strut of the landing gear, a first supply port fluidly connected to the first hydraulic supply, and a first outlet port fluidly connected to the hydraulic actuator.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Landing gear locking device


    Beteiligte:
    DUBOIS SÉBASTIEN (Autor:in) / DOUX AURÉLIEN (Autor:in) / HENRION PHILIPPE (Autor:in) / PAVOINE VINCENT (Autor:in)

    Erscheinungsdatum :

    06.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR LOCKING DEVICE

    DUBOIS SÉBASTIEN | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing gear locking device

    DUBOIS SEBASTIEN / DUX ALAIN / HENRION PHILIPPE et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing gear locking mechanism

    PITTS JEFFERY BEAUREGARD | Europäisches Patentamt | 2016

    Freier Zugriff

    Landing Gear Locking Mechanism

    PITTS JEFFERY BEAUREGARD | Europäisches Patentamt | 2016

    Freier Zugriff

    Device for locking aircraft landing gear

    FERNANDES PHILIP DOMINGUEZ / FARCY MARC / NICHOLAS LUDGER | Europäisches Patentamt | 2022

    Freier Zugriff