Airfoil

B - Operations – Transporting – 64 – C

Patent

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244/34

B64C 3/26 (2006.01)

Patent

CA 1282768

ABSTRACT OF THE DISCLOSURE An airfoil having improved aerodynamic charac- teristics incorporates a leading edge (13) and a trailing edge (14) longitudinally displaced therefrom. A continuous lower surface (21), defining the lower camber of the air- foil, extends from the leading edge (13) to the trailing edge (14). The upper surface of the airfoil incorporates a first upper surface (22) extending rearwardly from the loading edge (13) and terminating in an offset (20), and at least a second upper surface (23) extending rearwardly therefrom. The first upper surface (22) defines a first upper camber portion of the airfoil and the second upper surface (23) defines a second upper camber portion thereof.

510149

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