Wing modification method and apparatus

Aeronautics and astronautics – Aircraft structure – Details

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Details

244198, 244215, 244199, 244 91, B64C 316, B64C 2300

Patent

active

052132870

ABSTRACT:
A modification kit for the DeHavilland DH-2 Beaver and the DH-3 Otter aircraft. A replacement leading edge is provided for the wing together with replacement droop wing tips and a wing fence. A flap gap seal is provided to close the gap between the trailing edge of the wing and the leading edge of the flaps when the flaps are extended. The addition of these modifications modifies the performing characteristics of the airplane in an enhanced manner, particularly during take off and landing.

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patent: 4667906 (1987-05-01), Suarez et al.
patent: 4880355 (1989-11-01), Vuillet et al.
Hicks et al., "Effects of Forward Contour Modif. on the Aerody. Charac. of NACA 64.sub.1 -212 Airfoil Section", NASA TM X-3293, Sep. 1975.
Abstract from NASA research publication entitled "Wind Tunnel Results of the Low-Speed NLF (Natural Flow Control) (1)-0414F Airfoil", Dec. 1987.

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