Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1975-10-14
1977-09-06
Blix, Trygve M.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
B64C 338
Patent
active
040463389
ABSTRACT:
An airfoil for an aircraft having a first surface extending between the leading edge and the trailing edge, and a second surface joined to the first along the leading edge and projecting rearwardly in the direction of said trailing edge. The second surface of the airfoil terminates materially in advance of the trailing edge to define a step-like discontinuity of the airfoil. One or more lift generating members are pivotally mounted on the second surface of the airfoil adjacent the step-like discontinuity. The lift generating members are selectively movable to various positions relative to the airstream to alter the aerodynamic forces on the airfoil during conditions of flight.
REFERENCES:
patent: 1841804 (1932-01-01), Hall
patent: 2271226 (1942-01-01), Johnson
patent: 2346464 (1944-04-01), Tampier
patent: 3706430 (1972-12-01), Kline
Fogleman Floyd F.
Kline Richard L.
Barefoot Galen L.
Blix Trygve M.
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