Assembly for aircraft comprising a wing system element as...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/18 (2006.01)

Patent

CA 2623797

The invention concerns an assembly for aircraft comprising a wing system element (2) as well as an attachment mast, the assembly further comprising means for attaching (8) the mast on the element (2), said means (8) including two front half-attachments (29a) each provided with a shackle (38) and designed to absorb stresses exerted along a vertical direction, said shackle being mounted articulated on a first fitting (50) integral with a front spar (34) of the element (2) extending along a wingspan direction (32) and mounted articulated on a second fitting (42) integral with a rigid structure (6) of the mast. The invention is characterized in that the two shackles (38) are arranged in a common plane (P) parallel to the direction (32).

L'invention se rapporte à un ensemble pour aéronef comprenant un élément de voilure (2) ainsi qu'un mât d'accrochage, l'ensemble comprenant également des moyens d'accrochage (8) du mât sur l'élément (2), les moyens (8) comportant deux demi-attaches avant (29a) chacune pourvue d'une manille (38) et conçue de manière à assurer la reprise des efforts s'exerçant selon une direction verticale, cette manille étant d'une part montée de façon articulée sur une première ferrure (50) solidaire d'un longeron avant (34) de l'élément (2) s'étendant selon une direction d'envergure (32), et d'autre part montée de façon articulée sur une seconde ferrure (42) solidaire de la structure rigide (6) du mât. Selon l'invention, les deux manilles (38) sont agencées dans un même plan (P) parallèle à la direction (32).

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