Wing tip device

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S199200

Reexamination Certificate

active

07988100

ABSTRACT:
An aircraft includes a wing having a positive dihedral, the wing having a tip and a wing tip device mounted in the region of the tip. The wing tip device is generally downwardly extending and has a region inclined at a cant of more than 180 degrees. The region is arranged to generate lift during flight. The region inclined at a cant of more than 180 degrees may be located at the distal end of the wing tip device. The wing tip may be swept and may aeroelastically deform during flight.

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International Search Report for PCT/GB2006/003373 mailed Dec. 8, 2006.
GB Search Report for GB0518755.4 dated Jan. 10, 2006.

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