Fuselage section having an integral pressure bulkhead formed...

Details Fuselage section having an integral pressure bulkhead formed... Fuselage section having an integral pressure bulkhead formed...

B - Operations, Transporting

64

C

B64C 1/20 (2006.01)

Patent

CA 2733664

A fuselage section 1a for the pressure fuselage of an aircraft is disclosed which comprises a fuselage shell structure 4 and at least one pressure bulkhead 6 made of a fibre composite material, the pressure bulkhead 6 being formed in one piece with the fuselage shell structure 4. A fuselage shell 2 comprising at least one fuselage section 1a of this type is also disclosed.

Linvention concerne une section de fuselage (1a) pour le fuselage pressurisé dun aéronef, comprenant une structure de fuselage en coque (4) et au moins une cloison de pression (6) en un matériau renforcé de fibres. Selon linvention, la cloison de pression (6) est réalisée dune seule pièce avec la structure de fuselage en coque (4). Linvention concerne également une coque de fuselage (2) comprenant au moins une section de fuselage (1a) de ce type.

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