Aircraft wing vortex deflector

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244130, B64C 2102

Patent

active

039749860

ABSTRACT:
An aircraft wing vortex deflector constituting means for intercepting at least a part of the spiral flow of air around the tips of the wings during flight and directing the intercepted air rearwardly in a manner and direction tending to dissipate vortices in the wake of the aircraft.

REFERENCES:
patent: 2075817 (1937-04-01), Loerke
patent: 2406921 (1946-09-01), Stalker
patent: 2406923 (1946-09-01), Stalker
patent: 3596854 (1971-08-01), Haney, Jr.

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