Arrangement for generating vortexes

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S204000, C244S213000, C244S204100, C244S211000

Reexamination Certificate

active

10977478

ABSTRACT:
A spoiler and wing of an aircraft. A bottom surface of the spoiler has several longitudinal, elongated grooves. At least some of the grooves are equipped with one or more vortex generators. Further, the invention relates to a wing having in its back part at least one flap and having at least one spoiler of the invention arranged on the section between the wing and flap. The invention also relates to a method and control surface for generating vortexes.

REFERENCES:
patent: 3578264 (1971-05-01), Kuethe
patent: 4447028 (1984-05-01), Wang
patent: 4615497 (1986-10-01), Seeler et al.
patent: 4655419 (1987-04-01), van der Hoeven
patent: 5054720 (1991-10-01), Page
patent: 5253828 (1993-10-01), Cox
patent: 5598990 (1997-02-01), Farokhi et al.
patent: 5755408 (1998-05-01), Schmidt et al.
patent: 6105904 (2000-08-01), Lisy et al.
patent: 6123296 (2000-09-01), Mangalam
patent: 6345791 (2002-02-01), McClure
patent: 6461106 (2002-10-01), Rahier
patent: 2001/0032907 (2001-10-01), Borchers et al.

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