An aircraft landing gear component comprising: a first base member and a second base member, separated along a first longitudinal axis, a plurality of first parallel hoops, the centre of each first hoop lying along the first longitudinal axis and each first hoop aligned in a plane oriented at a first non-zero angle to the first longitudinal axis, and a plurality of second parallel hoops, the centre of each second hoop lying along the first longitudinal axis and each second hoop aligned in a plane oriented at a second non-zero angle to the first longitudinal axis, the second non-zero angle being different from the first non-zero angle, wherein each of the first hoops intersects with and is fixed to at least one of the second hoops, such that the first and second hoops form a rigid structure extending between the first and second base members.


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    Titel :

    AIRCRAFT LANDING GEAR COMPONENT


    Weitere Titelangaben:

    FLUGZEUGFAHRWERKSKOMPONENTE
    COMPOSANT DE TRAIN D'ATTERRISSAGE D'AÉRONEF


    Beteiligte:
    SEXTON MATTHEW (Autor:in)

    Erscheinungsdatum :

    2021-03-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B33Y ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING , Additive (generative) Fertigung, d. h. die Herstellung von dreidimensionalen [3D] Bauteilen durch additive Abscheidung, additive Agglomeration oder additive Schichtung, z. B. durch 3D- Drucken, Stereolithografie oder selektives Lasersintern / B64C AEROPLANES , Flugzeuge



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