A landing gear system (100) for an aircraft includes a truss frame (102) pivotally connectable to a frame of the aircraft and configured to rotate about an axis; a retraction actuator (104) configured to rotate the truss frame about the axis; a first truss link (106) pivotally connected to the truss frame; a second truss link (110) pivotally connected to the first truss link; a truss locking link pivotally connected to the truss frame and to the second truss link; and an articulation actuator (128) configured to pivot the first truss link with respect to the truss frame.


    Access

    Download


    Export, share and cite



    Title :

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR


    Additional title:

    GELENKTRÄGERKONFIGURATION FÜR EIN FLUGZEUGFAHRWERK
    CONFIGURATION DE TREILLIS ARTICULÉ POUR TRAIN D'ATTERRISSAGE D'AÉRONEF


    Contributors:

    Publication date :

    2023-08-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Articulating truss configuration for aircraft landing gear

    ACKS JAMES | European Patent Office | 2024

    Free access

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | European Patent Office | 2024

    Free access

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | European Patent Office | 2021

    Free access

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | European Patent Office | 2021

    Free access

    Vertically retracting side articulating landing gear for aircraft

    ACKS JAMES P / MARTIN DENNIS W | European Patent Office | 2015

    Free access