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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR


    Weitere Titelangaben:

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


    Beteiligte:
    ACKS JAMES P (Autor:in)

    Erscheinungsdatum :

    23.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Articulating truss configuration for aircraft landing gear

    ACKS JAMES | Europäisches Patentamt | 2024

    Freier Zugriff

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | Europäisches Patentamt | 2021

    Freier Zugriff

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | Europäisches Patentamt | 2021

    Freier Zugriff

    ARTICULATING TRUSS CONFIGURATION FOR AIRCRAFT LANDING GEAR

    ACKS JAMES | Europäisches Patentamt | 2024

    Freier Zugriff

    Vertically retracting side articulating landing gear for aircraft

    ACKS JAMES P / MARTIN DENNIS W | Europäisches Patentamt | 2015

    Freier Zugriff