According to a first embodiment of the present invention there is provided a retractable aircraft landing gear for an aircraft, the aircraft having a longitudinal X axis, a lateral Y axis, and a vertical Z axis, the landing gear comprising:a shock strut having a wheel assembly coupled at a first end;an upper yoke assembly pivotally arranged to be pivotally coupled to the aircraft about a first pivot axis, and coupled to a second end of the shock strut about a second pivot axis; anda drag stay pivotally coupled at a first end to the shock strut and arranged to be pivotally coupled at a second end to the aircraft,wherein one or more of the first and second pivot axes are non-orthogonal to the aircraft lateral Y axis.


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    Titel :

    RETRACTABLE AIRCRAFT LANDING GEAR


    Weitere Titelangaben:

    EINZIEHBARES FLUGZEUGFAHRWERK
    TRAIN D'ATTERRISSAGE RÉTRACTABLE POUR AÉRONEF


    Beteiligte:
    SIMONNEAUX YANN (Autor:in) / PADDOCK ANDY (Autor:in) / BENNETT IAN ROBERT (Autor:in)

    Erscheinungsdatum :

    09.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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