A system (401) for use with a tripod landing gear assembly of an aircraft may comprise: a tension strut assembly (450) having a tension strut (452) extending from an upper end to a lower end; a drag brace assembly (402) having an upper brace and a lower brace, the upper brace pivotably coupled to the lower brace at a center point, the lower brace rotatably coupled to the lower end of the tension strut; and a jury linkage (414) pivotally coupled to the drag brace assembly at the center point rotatably coupled to a middle portion of the tension strut, the middle portion between the upper end and the lower end.


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    Titel :

    TRIPOD LANDING GEAR ASSEMBLY


    Weitere Titelangaben:

    DREIBEINIGE FAHRWERKSANORDNUNG
    ENSEMBLE TRÉPIED DE TRAIN D'ATTERRISSAGE


    Beteiligte:

    Erscheinungsdatum :

    30.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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