Aircraft wing including a plurality of dismountable members

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/26 (2006.01) B64C 3/56 (2006.01)

Patent

CA 2676334

The invention relates to an aircraft wing (1) including two members (2, 3) removably connected end to end by a coupling means (4) including: a male coupling part (5) with spaced opposed upper (7) and lower (8) faces, a first face being planar while the second face has a longitudinal relief (9) with a V-shaped section, said first and second faces being mutually inclined towards each other at their free ends; a female coupling part (6) with spaced upper (10) and lower (11) faces facing each other, a first face being planar while the second face has a longitudinal relief (12) with a V-shaped section complementary to that of the relief (9), and said first and second faces being mutually inclined away from each other at their free ends; and means (19) for retaining the two parts (5, 6) coupled with their respective interacting faces in a mutual bearing relation.

Voilure (1) d'aéronef en deux éléments (2, 3) solidarisés bout à bout de façon démontable par un moyen (4) d'accouplement comprenant : une pièce d'accouplement (5) mâle ayant des faces (7) supérieure et (8) inférieure écartées et tournées à l'opposé l'une de l'autre, une première face étant plane, la seconde face ayant un relief (9) longitudinal à section en V et ces première et seconde faces étant mutuellement inclinées l'une vers l'autre vers leur extrémité libre; une pièce d'accouplement (6) femelle ayant des faces (10) supérieure et (11) inférieure écartées et disposées en vis-à-vis, une première face étant plane, la seconde face ayant un relief (12) longitudinal à section en V complémentaire de celle du relief (9) et ces première et seconde faces étant mutuellement inclinées pour s'écarter l'une de l'autre vers leur extrémité libre; et des moyens (19) de retenue des deux pièces (5, 6) accouplées avec leurs faces coopérantes respectives en appui mutuel.

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