Air craft wing

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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B64C 2104

Patent

active

061095656

ABSTRACT:
An aircraft having a wing with a top surface and a bottom surface, with the top surface having a first plurality of jets containing flow straighteners integrally hinged to the skin of the aircraft and positioned to direct air rearwardly along the top surface of the wing and the bottom surface having a second plurality of jets containing flow straighteners integrally hinged to the skin of the aircraft and positioned for directing air forwardly along the bottom surface of the wing and a compressor for receiving outside air and pressurizing the air which is then directed rearwardly along the top of the wing to decrease the pressure on top of the wing and forwardly along the bottom surface of the wing to increase the pressure on the bottom of the wing to increase the lift of the wing and thereby increase the lift and permit the aircraft to takeoff and land at a ground speed slower than if the pressurized air was not directed over the wing.

REFERENCES:
patent: 1810693 (1931-06-01), Alfaro
patent: 2267927 (1941-12-01), Kightlinger
patent: 2437732 (1948-03-01), Ferrel
patent: 2479487 (1949-08-01), Goembel
patent: 2646945 (1953-07-01), Perry
patent: 2873931 (1959-02-01), Fleischmann
patent: 3010680 (1961-11-01), Kaplan
patent: 3128063 (1964-04-01), Kaplan
patent: 3142457 (1964-07-01), Quenzler
patent: 3317162 (1967-05-01), Grant
patent: 3326500 (1967-06-01), Lanier
patent: 3840199 (1974-10-01), Tibbs
patent: 3887146 (1975-06-01), Bright
patent: 3915412 (1975-10-01), Tibbs
patent: 3974987 (1976-08-01), Shorr
patent: 4674716 (1987-06-01), Moore
patent: 5255881 (1993-10-01), Rao

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