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:
Dec. 04, 2018

Filed:

Sep. 16, 2009
Applicants:

Michael Shepshelovich, Ganei Tikva, IL;

Alex Nagel, Kiryat Ono, IL;

Danny Abramov, Rehovot, IL;

Inventors:

Michael Shepshelovich, Ganei Tikva, IL;

Alex Nagel, Kiryat Ono, IL;

Danny Abramov, Rehovot, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/14 (2006.01); B64C 3/48 (2006.01); B64C 3/44 (2006.01);
U.S. Cl.
CPC ...
B64C 3/48 (2013.01); B64C 3/14 (2013.01); B64C 3/44 (2013.01); B64C 2003/142 (2013.01); B64C 2003/148 (2013.01); Y02T 50/12 (2013.01); Y02T 50/14 (2013.01);
Abstract

Aerofoil accessories are provided, configured for selective attachment to a wing element, the wing element having an outer facing aerofoil surface and being based on at least one datum aerofoil section. Each accessory provides a modified geometric profile to a datum profile of the at least one aerofoil section when attached to the wing element. The accessories are each configured for having a substantially fixed geometric profile with respect to the at least one datum aerofoil section at least whenever said wing element is airborne with the respective accessory attached to the wing element. The modified geometric profile is such as to provide said wing element with the accessory attached thereto with a desired change in performance relative to a datum performance provided by the wing element absent the accessory. A kit is also provided for enhancing performance of a wing element in off-design conditions. A method is also provided for enhancing performance of a wing element in adverse conditions.


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