A landing gear for a vehicle includes a strut configured for reciprocating movement between a stowed position and a deployed position. A shock absorber has a first element slidingly disposed within the strut and a second element slidingly coupled to the first element. A trailing arm is rotatably coupled to the second element. A first linkage is coupled to the first element, wherein the first linkage drives the first element between a raised position when the strut is in the stowed position and a lowered position when the strut is in the deployed position. The landing gear further includes a second linkage coupled to the trailing arm. The second linkage rotates the trailing arm between a first trailing arm position when the strut is in the stowed position and a second trailing arm position when the strut is in the deployed position.


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    Title :

    LANDING GEAR WITH SHORTENING MOTION


    Contributors:

    Publication date :

    2022-03-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR WITH SHORTENING MOTION

    SCHMIDT ROBERT KYLE / AMBERG STEVE / SACCOCCIA MICHAEL | European Patent Office | 2023

    Free access

    Landing gear with shortening motion

    SCHMIDT ROBERT KYLE / AMBERGER STEVE / MICHAEL SACOCCIA | European Patent Office | 2023

    Free access

    Landing gear with shortening motion

    SCHMIDT ROBERT KYLE / AMBERG STEVE / SACCOCCIA MICHAEL | European Patent Office | 2022

    Free access

    LANDING GEAR WITH SHORTENING MOTION

    SACCOCCIA MICHAEL / SCHMIDT ROBERT KYLE / AMBERG STEVE | European Patent Office | 2022

    Free access

    LANDING GEAR WITH SHORTENING MOTION

    SCHMIDT ROBERT KYLE / AMBERG STEVE / SACCOCCIA MICHAEL | European Patent Office | 2022

    Free access