Aerodynamic surface tip vortex attenuation system

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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244207, B64C 2108

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active

051582511

ABSTRACT:
Apparatus and method for attenuating fluid foil tip vortices, featuring a "Coanda tip" and a "Coanda curtain." The fluid foil tip has a Coanda surface and means for discharging compressed fluid adjacent thereto; a resultant fluid barrier is formed generally chordwise and perpendicular to the fluid foil plane and tangential to the fluid foil tip upon Coanda entrainment and deflection of the discharged compressed fluid. The fluid barrier prevents crossflow from the higher pressure fluid region to the lower pressure fluid region, the fluid regions being separated by the fluid foil when moving relatively through a fluid, the fluid barrier thereby stemming tip vortex generation at its source.

REFERENCES:
patent: 2163655 (1939-06-01), Zimmerman
patent: 2650781 (1953-09-01), Taylor
patent: 2925129 (1960-02-01), Yuan et al.
patent: 3446288 (1969-05-01), Yuan
patent: 3480234 (1969-11-01), Cornish, III
patent: 3692259 (1972-09-01), Yuan
patent: 3841587 (1974-10-01), Freed
patent: 3881669 (1975-05-01), Lessen
patent: 3889903 (1975-06-01), Hilby
patent: 3936013 (1976-02-01), Yuan
patent: 3984070 (1976-10-01), Patterson, Jr.
patent: 4017041 (1977-04-01), Nelson
patent: 4019696 (1977-04-01), Hirt et al.
patent: 4040578 (1977-08-01), Yuan
patent: 4099691 (1978-07-01), Swanson et al.
patent: 4108403 (1978-08-01), Finch
patent: 4146197 (1979-03-01), Grotz
patent: 4190219 (1980-02-01), Hackett
patent: 4382569 (1983-05-01), Boppe et al.
patent: 4387869 (1983-05-01), Englar et al.
patent: 4398687 (1983-08-01), Nicholas, Jr. et al.
patent: 4463920 (1984-08-01), Nichols, Jr. et al.
patent: 4477042 (1984-10-01), Griswold, II
patent: 4478380 (1984-10-01), Frakes
patent: 4674716 (1987-06-01), Moore
patent: 4682746 (1987-07-01), Thomas
patent: 4705240 (1987-11-01), Dixon
patent: 4736913 (1988-04-01), Bennett et al.
patent: 4770607 (1988-09-01), Cycon et al.
Wille, R., and Fernholz, H., "Report on the First European Mechanics Collum on the Coanda Effect," Journal of Fluid Mechanics, vol. 23, part 4, pp. 801-819, Cambridge at the University Press (1965).
Williams, R. M., Leitner, R. T., and Rogers, E. O. "X-Wing: A New Concept in Rotary Wing VTOL," David W. Taylor Ship Research and Development Center, Bethesda, Md. Presented to the American Helicoper Society Symposium on Rotor Technology, Aug. 1976.

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