Aircraft fuselage element

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/06 (2006.01) B29C 70/48 (2006.01) B29C 70/68 (2006.01)

Patent

CA 2728179

The invention relates to an aircraft fuselage element. According to the invention, - said fuselage element being a one-piece component, it comprises a closed wall (1) defining an internal volume, the external surface (2) of said wall forming the external skin of said fuselage, - said wall has a cross section which has on the side facing the internal volume a planar central part (5), a male connecting element (7) at a first edge and a female connecting element (6) at its other edge, which connecting elements project, each connecting element being designed to engage with the corresponding connecting element of another fuselage element placed side by side with said fuselage element in order to connect these fuselage elements longitudinally to each other, and - one of said connecting elements includes a step (9) forming a frame for said fuselage.

L'invention concerne un élément de fuselage d'aéronef. Selon l'invention, ledit élément de fuselage étant d'un seul tenant, il comprend une paroi fermée (1) délimitant un volume interne, la surface externe (2) de ladite paroi formant la peau externe dudit fuselage; ladite paroi présente une coupe comportant du côté dudit volume interne une partie médiane (5) plane, un élément de liaison mâle (7) à une première extrémité et un élément de liaison femelle (6) à son autre extrémité, lesdits éléments de liaison étant placés en saillie, chacun desdits éléments de liaison étant destiné à coopérer avec l'élément de liaison correspondant d'un autre élément de fuselage placé bord à bord audit élément de fuselage en vue de solidariser longitudinalement l'un à l'autre ces éléments de fuselage; un desdits éléments de liaison comprend une marche (9) formant un cadre dudit fuselage.

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