B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/26 (2006.01) F16B 5/02 (2006.01) F16B 17/00 (2006.01)
Patent
CA 2612593
This invention relates to a lateral force joint, with which a plate-like spar (2) can be fastened to a fuselage strap (3) mounted on an airplane fuselage (8). For this purpose, the plate-like spar (2) has a through bore (14), into which a fastening cylinder (1) mounted on the flange can be inserted for connecting both components (2, 3). In order to allow for the location of the spar (2) to be adjusted with respect to the fuselage strap (3), a bearing bush (5) of the spar is eccentrically fitted into the through bore (14). Correspondingly, the fastening cylinder (13) of the fuselage strap (3) is mounted eccentrically on a bearing bush (4) so that a rotation of the bearing bushes (4, 5) allows the lateral force joint to be adjusted.
L~invention concerne un joint de compression latéral, permettant de fixer un longeron en forme de plaque (2) sur une armature (3) de fuselage montée sur le fuselage (8) d~un aéronef. Pour ce faire, le longeron en forme de plaque (2) comporte un alésage traversant (14) dans lequel peut être inséré un cylindre d~attache (1) monté sur la bride afin d~assembler les deux composants (2, 3). Pour permettre le réglage de la position du longeron (2) par rapport à l~armature (3) de fuselage, un coussinet (5) du longeron est ajusté de façon excentrique dans l~alésage traversant (14). Le cylindre d~attache (13) de l~armature (3) de fuselage est lui aussi monté de façon excentrique sur un coussinet (4) de façon à permettre le réglage du joint de compression latéral par rotation des coussinets (4, 5).
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Borden Ladner Gervais Llp
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