Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1978-11-15
1980-07-29
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244207, 244 73R, 60 3917, 60 3952, 60263, 416 20A, 416 90A, B64C 2102
Patent
active
042147220
ABSTRACT:
Aircraft engine exhaust is mixed with air and fuel and recombusted. Air is drawn into the secondary combustion chamber from suction surfaces on wings. Exhaust of the secondary combustion chamber is blown over wing and fuselage surfaces.
REFERENCES:
patent: 2478792 (1949-08-01), Trey
patent: 2516489 (1950-07-01), Stalker
patent: 3442082 (1969-05-01), Peterson
patent: 3887147 (1975-06-01), Grieb
Ernst, et al., "YC14 System for Leading Edge Boundary Layer Contral", CAS1/A1AA, Meeting, Toronto, Canada, 10/30/74.
Barefoot Galen L.
Creighton Wray James
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