Rotor flap apparatus and method

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244206, 114330, 2961805, B64C 2302, B62D 3702, B63G 820

Patent

active

051957027

ABSTRACT:
A rotor flap apparatus is attached to the trailing edge of a wing of a craft. The rotor flap apparatus includes a rotatable rotor mounted on an attachment arm, which is pivotally mounted on a trailing edge of the wing. The attachment arm can be raised or lowered to move the plane of the rotor up or down to vary the lift and thrust characteristics of the wing, to prevent stall and also to allow very low speed take off and landing. In one embodiment, propellers are provided at the leading edge of the wing, in conjunction with the rotor flap apparatus, to provide a system which allows vertical take off and landing of the aircraft. Other embodiments include wings with rotor flap apparatus attached to land craft and underwater craft as well.

REFERENCES:
patent: Re29023 (1976-11-01), Malvestuto, Jr.
patent: 2873710 (1959-02-01), Morel
patent: 2976077 (1961-03-01), Totton, Jr.
patent: 3179354 (1965-04-01), Alvarez-Calderon
patent: 3203649 (1965-08-01), Girard
patent: 3273827 (1966-09-01), Girard
patent: 3512825 (1970-05-01), Green
patent: 3521589 (1970-07-01), Kemp
patent: 3856238 (1974-12-01), Malvestuto, Jr.
patent: 3965836 (1976-06-01), Malvestato, Jr.

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