A landing gear system uplock arrangement (300, 500) including: a hook (310) defining a gap (314), wherein the hook is movable between a first position, at which the hook is for retaining a movable element (299, 499) of a landing gear system in the gap, and a second position, at which the hook is for permitting movement of the element into and out from the gap; a lock (320) that is changeable between a locked state, in which the lock prevents movement of the hook from the first position to the second position, and an unlocked state, in which the lock permits movement of the hook from the first position to the second position; and a sensor arrangement (330) for sensing whether the element is present in the gap.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    LANDING GEAR SYSTEM UPLOCK ARRANGEMENT


    Beteiligte:
    WELLS CRAIG (Autor:in)

    Erscheinungsdatum :

    2021-12-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR SYSTEM UPLOCK ARRANGEMENT

    WELLS CRAIG | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing gear system uplock arrangement

    WELLS CRAIG | Europäisches Patentamt | 2023

    Freier Zugriff

    LANDING GEAR SYSTEM UPLOCK ARRANGEMENT

    WELLS CRAIG | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft landing gear uplock system

    Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft landing gear uplock system

    MCCAMBRIDGE OLIVER / BRIGHTON TREVOR ANTHONY | Europäisches Patentamt | 2020

    Freier Zugriff