Method for fixing an engine strut to an airplane wing

Details Method for fixing an engine strut to an airplane wing Method for fixing an engine strut to an airplane wing

B - Operations, Transporting

64

D

B64D 27/26 (2006.01)

Patent

CA 2590514

The inventive fixing system comprises a front attachment (6), a rear attachment (7) and an intermediate attachment (8) connecting a strut (1) to a wing (2), wherein the lower fitting (17) of the rear attachment (7) is fixedly connected to the transversal rear face (1 G) of said strut on the extension thereof and said lower fitting (17) is substantially in flush with the top face of the strut.

Le système de fixation comporte une attache avant (6), une attache arrière (7) et une attache intermédiaire (8) reliant le mât (1 ) à l'aile (2) et, selon l'invention, la ferrure inférieure (17) de ladite attache arrière (7) est agencée fixement sur la face transversale arrière (1 G) dudit mât, dans le prolongement de celui-ci, ladite ferrure inférieure (17) venant au plus sensiblement à fleur de la face supérieure dudit mât.

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