System and method for reducing airfoil vortices

Details System and method for reducing airfoil vortices System and method for reducing airfoil vortices

B - Operations, Transporting

64

C

B64C 23/06 (2006.01)

Patent

CA 2598908

A system and a method according to the invention reduce wake turbulence of an aircraft in that a component (2) affixed to the extremity of the wing (3) of an aircraft disturbs the rolling action of the air in the region of the outer wing by periodic hingeing movements.

La présente invention a trait à un système et un procédé pour la réduction de la turbulence de sillage d'un aéronef caractérisés en ce qu'un composant (2) fixé à l'extrémité de l'aile (3) d'un aéronef perturbe l'action de roulis de l'air dans la zone de l'aile extérieure par des mouvements d'articulation périodiques.

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