Control force generator

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 91, 244 52, B64C 2100, B64C 506

Patent

active

046827463

ABSTRACT:
A control force generator for an aircraft using circulation control to a selectively produce lift on an otherwise non-lift surface. The generator employs a novel, double-slot single Coanda surface arrangement for selectively generating the aerodynamic lift.

REFERENCES:
patent: 271485 (1983-11-01), Tucson
patent: 2568812 (1951-09-01), Lee
patent: 3362660 (1968-01-01), Tyler
patent: 3367581 (1968-02-01), Kizilos et al.
patent: 4247062 (1981-01-01), Brueckner
patent: 4398687 (1983-08-01), Nichols, Jr. et al.

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