Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1992-07-17
1993-10-19
Huppert, Michael S.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244212, 244214, B64C 2306
Patent
active
052538281
ABSTRACT:
A concealable flap actuated vortex generator for generating a vortex on a lifting surface assembly, and an improved aircraft flight lifting surface having such concealable flap actuated vortex generators. When the flap of the lifting surface assembly is in the nominal (non-extended or non-deflected) position, the vortex generator is unexposed. When the flap is actuated by a flap actuator, the flap is extended or deflected from the nominal position, thereby projecting or exposing the vortex generator into an operational position and enabling the generation of a vortex.
REFERENCES:
patent: 3263945 (1966-08-01), Wimpenny
patent: 4032087 (1977-06-01), Cleaves
patent: 4039161 (1977-08-01), Bauer
patent: 4669687 (1987-06-01), Rudolph
patent: 4702441 (1987-10-01), Wang
patent: 4784355 (1988-11-01), Brine
Bidwell Anne E.
Huppert Michael S.
The Board of Regents of the University of Oklahoma
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