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Aircraft with Means for a Premature Breakdown of the Wing Vortex Pair

Stuff, R. and Vollmers, H. (2002) Aircraft with Means for a Premature Breakdown of the Wing Vortex Pair. Other. US 6,422,518 B1, 10 S.

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Abstract

The invention relates to an aircraft comprising a symme- try plane, two wings, a fuselage, a horizontal tail plane (HTP) and with means for a premature breakdown of a wing vortex pair behind the aircraft in flight, which pair is generated in the tip area of the wings, has a first spin direction and descends in the near field behind the aircraft. The invention deals in particular with the premature breakdown of the wing vortex pair behind an aircraft in landing flight. However, it is also advisable to apply the invention to an aircraft in climbing or cruise flight.

Document Type:Monograph (Other)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Aircraft with Means for a Premature Breakdown of the Wing Vortex Pair
Authors:
AuthorsInstitution or Email of Authors
Stuff, R.UNSPECIFIED
Vollmers, H.UNSPECIFIED
Date:2002
Number of Pages:10
Series Name:Patent
Status:Published
Keywords:wing vortex , wake vortex allivation
Institution:United States Patent Office
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Flight Physics
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Ilka Micknaus
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:17

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