Curved wing tip

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/10 (2006.01)

Patent

CA 2728765

A wing incorporating a wing tip with a curved leading edge and a curved trailing edge to minimize induced drag for a given wing form is disclosed. The curve of the leading and trailing edges of the wing tip may be described generally as parabolic, elliptic, or super elliptic. A finite tip segment may be included with a sweep angle between the end of the curved leading edge and the end of the curved trailing edge. The wing tip may also include a spanwise camber.

L'invention concerne une aile comprenant une pointe d'aile avec un bord d'attaque incurvé et un bord de fuite incurvé pour réduire au minimum la traînée induite pour une forme d'aile donnée. La courbure des bords d'attaque et de fuite de la pointe d'aile peut être décrite généralement comme étant parabolique, elliptique ou super-elliptique. Un segment de pointe fini peut être inclus avec un angle de flèche entre l'extrémité du bord d'attaque incurvé et l'extrémité du bord de fuite incurvé. La pointe d'aile peut également comprendre une cambrure dans le sens de l'envergure.

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