B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 7/02 (2006.01) B64D 29/02 (2006.01)
Patent
CA 2647762
The invention relates to an aircraft wing arrangement (1) comprising a wing (2) and at least one aircraft engine attachment pylon (4) for attaching an engine suspended under the wing and comprising a forward region (8) protruding forward from an leading edge (10) of the wing. According to the invention, the forward region (8) comprises a lateral projection (12) delimiting a lateral airflow channel (14) extending towards a proximal end of the wing.
L'invention se rapporte à un agencement d'aile (1) d'aéronef comportant une aile (2) ainsi qu'au moins un mât d'accrochage (4) de moteur d'aéronef suspendu sous l'aile et comprenant une zone avant (8) située en saillie vers l'avant par rapport à un bord d'attaque (10) de l'aile. Selon l'invention, la zone avant (8) comporte une saillie latérale (12) délimitant un canal latéral d'écoulement d'air (14) en se projetant vers une extrémité proximale de l'aile.
Dantin Stephanie
Fol Thierry
Gerard Ludovic
Jimenez Philippe
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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