A winglet

Details A winglet A winglet

B - Operations, Transporting

64

C

B64C 23/06 (2006.01) B64C 5/08 (2006.01) B64C 13/16 (2006.01)

Patent

CA 2450025

A winglet (12) for an aircraft wing is provided. The winglet (12) has an airflow control arrangement, for example in the form of a trailing edge flap (20) by means of which lift generated by the winglet can be varied. The control arrangement desirably forms part of a manoeuvre load alleviation system (22) for the aircraft.

La présente invention concerne une ailette (12) destinée à une aile d'aéronef. L'ailette (12) de bout d'aile comprend un système de régulation de l'écoulement de l'air, qui se présente par exemple sous forme d'un volet (20) de flanc arrière, lequel permet de varier la portance générée par l'ailette de bout d'aile. Le système de régulation fait de préférence partie d'un système (22) d'allégement de la charge pour la manoeuvre de l'aéronef.

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