B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 7/00 (2006.01) B64D 29/06 (2006.01) F16B 35/00 (2006.01) F16B 37/04 (2006.01)
Patent
CA 2420352
An apparatus for fixing a member (8) to an aircraft structure including: firstly, fixing device having a shank with a head at one end, an externally machined portion of its peripheral wall at its other end, and a longitudinal interior thread at the same end as its externally machined portion (34), secondly, a bushing which cooperates with the machined portion of the shank so as to be fixed to the shank; and thirdly, an attachment device for attaching the member and having a threaded shank (48) cooperating with the longitudinal interior thread. Applies to the belly fairing of an aircraft.
Ce dispositif permet la fixation d'un carénage (8) sur une structure d'aéronef qui met en oeuvre des organes de fixation comportant d'une part une tige munie à l'une de ses extrémités d'une tête et présentant à son autre extrémité sur sa paroi périphérique un usinage extérieur et d'autre part une douille (34) coopérant avec l'usinage de la tige pour venir se fixer sur cette tige, la tige d'au moins l'un des organes de fixation présentant du côté de son usinage extérieur un taraudage longitudinal, caractérisé en ce qu'il comporte des moyens pour l'accrochage de l'élément présentant une tige filetée (48) coopérant avec ledit taraudage longitudinal. Application à la fixation d'un carénage ventral d'un aéronef.
Le Lay Loic
Rouyre Francois
Airbus France
Robic
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