Fuselage segment and method for manufacturing the fuselage...

B - Operations – Transporting – 64 – C

Patent

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B64C 1/40 (2006.01)

Patent

CA 2757143

The invention discloses a fuselage segment (2) of an aircraft fuselage with an outer skin (6) and an inner skin (4) that are spaced apart from one another by a core (8), wherein conduits (20, 22) for system installations are integrated into the core (8), as well as a method for manufacturing such a fuselage segment (2).

L'invention concerne un segment de fuselage (2) d'avion, comportant une peau extérieure (6) et une peau intérieure (4), séparées l'une de l'autre par un noyau (8). L'invention est caractérisée en ce que des conduits (20, 22) sont intégrés dans le noyau (8) pour le montage de systèmes. L'invention porte également sur un procédé de fabrication d'un segment de fuselage (2) de ce type.

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