Device for controlling a vortex trail generated by the...

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S130000, C244S198000, C244S204000, C244S214000, C244S204100

Reexamination Certificate

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07866608

ABSTRACT:
A device for controlling a vortex trail generated by an oblong element of an aircraft bearing surface includes a control component arranged on a fixing element of the oblong element and on a bearing surface such that a base of the control component contacts the leading edge of the bearing surface. The control component has a triangular shape, on a plane perpendicular to the longitudinal axis thereof, whose two adjacent sides form flanks interconnected by a rounded edge.

REFERENCES:
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patent: 3968946 (1976-07-01), Cole
patent: 4323209 (1982-04-01), Thompson
patent: 4540143 (1985-09-01), Wang et al.
patent: 4643376 (1987-02-01), Vanderhoeven
patent: 4685643 (1987-08-01), Henderson
patent: 5156362 (1992-10-01), Leon
patent: 6126118 (2000-10-01), Fujino et al.
patent: 6964397 (2005-11-01), Konings
patent: 2004/0046086 (2004-03-01), Dixon
International Search Report dated Jan. 29, 2007 w/ English translation.
Written Opinion of the ISA w/ English translation.

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