A semi-levered landing gear (200) including a shock strut (210) configured for coupling to an airframe (101) of an aircraft (100), a truck lever (220) being rotatably coupled to the shock strut, a tension link assembly (230) having a tension link assembly first end (230a), a tension link assembly second end (230b), and at least one tension link assembly rotation axis (TLA). The tension link assembly first end is coupled to the shock strut, and the tension link assembly second end is coupled to the truck lever. A positioning mechanism (240) is configured for coupling to one or more of the airframe and the shock strut and is coupled to the tension link assembly, wherein the tension link assembly is configured to rotate the truck lever about a truck pivot axis of rotation (TPA) between a truck lever extended position and a truck lever stowed position.


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    Titel :

    SINGLE AXLE, SEMI-LEVERED LANDING GEAR WITH SHORTENING MECHANISM


    Weitere Titelangaben:

    EINACHSIGES, HALBAUSGEHEBELTES FAHRWERK MIT VERKÜRZUNGSMECHANISMUS
    TRAIN D'ATTERRISSAGE SEMI-ARTICULÉ À ESSIEU UNIQUE COMPORTANT UN MÉCANISME DE RACCOURCISSEMENT


    Beteiligte:
    COTTET JUSTIN D (Autor:in) / MELLOR MITCHELL (Autor:in) / DRAKE MICHAEL L (Autor:in) / SONNENBURG GEORGE (Autor:in)

    Erscheinungsdatum :

    30.10.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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