B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 23/06 (2006.01) B64C 7/02 (2006.01)
Patent
CA 2620510
A device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface comprises a control means (8) which is arranged on the fixing element (11) of the oblong element (5) and on the bearing surface (4) in such a way that the base (12) thereof is brought into contact with the leading edge (6) of said bearing surface and which has a triangular shape on a plane perpendicular to the longitudinal axis thereof whose two adjacent sides form flanks interconnected by a rounded edge.
Dispositif de contrôle d'un sillage tourbillonnaire engendré par un élément oblong sur l'extrados d'une surface portante d'un aéronef. Le dispositif (1) comporte un moyen de contrôle (8) qui est agencé sur un élément de fixation (11) de l'élément oblong (5) et sur la surface portante (4) de sorte que sa base (12) est au contact du bord d'attaque (6) de la surface portante (4), et qui présente une forme triangulaire dans un plan perpendiculaire à son axe longitudinal avec deux côtés adjacents formant des flancs qui sont reliés ensemble par un bord arrondi.
Airbus France
Airbus Operations Sas
Robic
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