Aircraft wing with internal flow control propulsion

Details Aircraft wing with internal flow control propulsion Aircraft wing with internal flow control propulsion

1975-06-05

1977-05-31

Blix, Trygve M.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244 53R, B64C 302, B64D 2718

Patent

active

040265005

ABSTRACT:
A jet thrust aircraft wing wherein the intake and exhaust are substantially coextensive with the leading and trailing edges, respectively; utilizing engine suction to induce intake of air and preventing build-up ahead of the wing by separating the same from the flow of air over and under the upper and lower wing surfaces; and utilizing engine exhaust thrust to induce controllable air flow through the wing and to induce longitudinal flow of air over and under the wing throughout its span.

REFERENCES:
patent: 2526941 (1950-10-01), Fishbein
patent: 2620622 (1952-12-01), Lundberg
patent: 2748564 (1956-06-01), Marchal et al.
patent: 2821351 (1958-01-01), Utgoff
patent: 2978204 (1961-04-01), Davidson
patent: 3482804 (1969-12-01), Pyptiuk

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