Flow-vectored trailing-edge for airfoils and jets

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 23D, 244 52, 244209, B64C 2104

Patent

active

055314066

ABSTRACT:
Apparatus and method for airflow vectoring control for an airfoil, a two dimensional jet, and the like. An airfoil or jet with a blunt open edge and a suction system for sucking air into the open edge. A blower system for blowing air out through the open edge. A control for changing the direction of flow through the open edge. A baffling arrangement for changing the magnitude and distribution of flow across the open edge.

REFERENCES:
patent: 2659552 (1953-11-01), Stalker
patent: 2708556 (1955-05-01), Smith et al.
patent: 2751168 (1956-06-01), Stalker
patent: 2968921 (1961-01-01), David
patent: 3478987 (1969-11-01), Dorand
patent: 4515101 (1985-05-01), Akerblom
patent: 4666104 (1987-05-01), Kelber

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