Concept of a variable winglet for lateral load reduction for...

Details Concept of a variable winglet for lateral load reduction for... Concept of a variable winglet for lateral load reduction for...

B - Operations, Transporting

64

C

B64C 23/06 (2006.01)

Patent

CA 2602948

The present invention relates to a device for adapting aerodynamic characteristics of a wing element (1), wherein the device comprises a winglet (2), wherein the winglet (2) is movably attachable to the wing element (1), and wherein the winglet (2) or parts of the winglet is or are rotatable in relation to the wing element (1) such that an associated rotary axis (7) with a main direction of extension (6) of the wing element (1) encompasses an angle that differs from 90~.

La présente invention concerne un dispositif servant à adapter des caractéristiques aérodynamiques d'un élément de voilure (1). Le dispositif comprend un bout d'aile (2) qui se fixe de manière amovible à l'élément de voilure (1). Le bout d'aile (2) ou des parties du bout d'aile (2) peu(ven)t être mis en rotation par rapport à l'élément de voilure (1), de sorte qu'un axe rotatif (7) associé présentant une direction d'extension (6) principale de l'élément de voilure (1) recouvre un angle différent de 90°.

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