The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 20, 2019

Filed:

Mar. 01, 2017
Applicant:

Airbus Group Limited, London, GB;

Inventor:

Stephen Rolston, London, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/10 (2006.01); B64C 3/00 (2006.01); B64C 3/26 (2006.01); B64C 30/00 (2006.01); B64C 3/10 (2006.01); B64C 39/02 (2006.01); B64C 3/14 (2006.01);
U.S. Cl.
CPC ...
B64C 21/10 (2013.01); B64C 3/00 (2013.01); B64C 3/10 (2013.01); B64C 3/26 (2013.01); B64C 30/00 (2013.01); B64C 39/024 (2013.01); B64C 2003/148 (2013.01); B64C 2003/149 (2013.01); B64C 2230/08 (2013.01); Y02T 50/12 (2013.01); Y02T 50/166 (2013.01);
Abstract

A fixed wing aircraft has a wing with an aerofoil cross-section defining an upper and lower geometric surfaces which meet at a geometric leading edge of the wing. The wing has an upper and lower aerodynamic surfaces while in flight. The upper aerodynamic surface and the lower aerodynamic surface meet at an aerodynamic leading edge at the intersection with an attachment line dividing the air that passes over the upper aerodynamic surface from the air that passes over the lower aerodynamic surface. The lower geometric surface adjacent the geometric leading edge has a roughness strip with a step height of at least 50 microns over the lower geometric surface. The roughness strip is located on the lower aerodynamic surface of the wing when the aircraft is flown at a load factor of 1 g and is located on the upper aerodynamic surface when the load factor is above 1.2 g.


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