Hidden vortex generators

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

138 39, 244199, 244113, B64C 358, B64C 934

Patent

active

040391612

ABSTRACT:
An improvement to the controllability of aircraft wherein vortex generators are connected to a control surface in front of the hinge line of the control surface so that when the control surface is deflected, the vortex generators project into the airstream on the opposite side from the deflecting control surface. The action of the vortex generators causes the airflow to remain attached to the control surface at higher angles of attack than would otherwise be possible thus increasing the lift of the airfoil and control surface.

REFERENCES:
patent: 1862421 (1932-06-01), O'Malley
patent: 2800291 (1957-07-01), Stephens
patent: 2852209 (1958-09-01), Petre

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