Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1987-04-03
1989-07-04
Barefoot, Galen
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
B64C 2104
Patent
active
048443859
ABSTRACT:
A pneumatic aerodynamic control surface is described for an aircraft having a region of upwash ahead of a powered-lift or high-lift wing, the control surface comprising blown engine nacelles immersed in the upwash region, and capable of generating moments about all three axes of the aircraft without any external moving parts.
REFERENCES:
patent: 2891740 (1959-06-01), Campbell
patent: 3584811 (1971-06-01), Leavy
patent: 3604661 (1971-09-01), Mayer, Jr.
patent: 3606213 (1971-09-01), Lubimov
patent: 3940092 (1976-02-01), Farris
patent: 4019696 (1977-04-01), Hirt et al.
patent: 4200252 (1980-04-01), Logan et al.
Bennett John A.
Englar Robert J.
Thomas Andrew S. W.
Barefoot Galen
Barton Robert P.
Corl Rodney
Katz Eric R.
Lockheed Corporation
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