Aircraft-fuselage assembly concept

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/06 (2006.01) B64C 1/00 (2006.01) B64F 5/00 (2006.01)

Patent

CA 2654646

The invention relates to an aircraft fuselage section (1 ), to an aircraft fuselage as well as to a method for producing a fuselage section (1). The fuselage section (1) is produced in that a first interior tube (2) as well as a second interior tube (3) are produced in an upstream production step, which interior tubes (2, 3) are subsequently enclosed by an exterior tube (4). For spacing and in order to provide more stability to the tubes (2, 3, 4) the interior tubes (2, 3) are enclosed by straps (5, 6) that are arranged between the interior tubes (2, 3) and the exterior tube (4).

L'invention concerne une section de fuselage d'aéronef (1), un fuselage d'aéronef tout comme un procédé de production d'une section de fuselage (1). La section de fuselage (1) est produite de manière à ce qu'un premier tube intérieur (2) ainsi qu'un second tube intérieur (3) soient produits dans une étape de production en amont, lesquels tubes intérieurs (2, 3) sont ensuite entourés par tube extérieur (4). Pour des motifs d'espacement et afin de conférer une stabilité accrue aux tubes (2, 3, 4), les tubes intérieurs (2, 3) sont entourés par des éléments d'armature (5, 6) qui sont disposés entre les tubes intérieurs (2, 3) et le tube extérieur (4).

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