B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01) B64F 5/00 (2006.01)
Patent
CA 2761654
The invention relates to a method for producing an aircraft fuselage (2) comprising at least two fuselage tubes (8, 10, 12). According to the invention, the connecting sections (20, 22) used for forming a transversal joining region (18) are initially prepared for a different transversal join and then the fuselage tubes (8, 10) are mounted about the connecting sections (20, 22). The invention also relates to an aircraft fuselage (2) comprising annular connecting sections (20, 22) used for forming said type of transversal join.
L'invention concerne un procédé de fabrication d'un fuselage d'avion (2) comportant au moins deux tubes de fuselage (8, 10, 12). Selon le procédé, des segments de liaison (20, 22) destinés à former une zone de jointure transversale (18) sont d'abord préparés pour une jointure ultérieure, puis les tubes de fuselage (8, 10) sont montés autour des segments de liaison (20, 22). L'invention concerne également un fuselage d'avion (2) comportant des segments de liaison annulaires (20, 22) pour la création d'une telle jointure transversale.
Bense Rolf
Gorr Eugen
Airbus Operations Gmbh
Marks & Clerk
LandOfFree
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