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. 22, 2017

Filed:

Dec. 05, 2013
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Philipp Witte, Seattle, WA (US);

Stanley Warren Stawski, Camano Island, WA (US);

Fedor A. Kleshchev, Seattle, WA (US);

Joshua William Zarfos, Renton, WA (US);

Parth R. Naidu, Seattle, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 23/06 (2006.01); B29C 70/44 (2006.01); B64C 5/08 (2006.01); B64D 45/02 (2006.01); B29C 70/34 (2006.01); B32B 5/02 (2006.01); B32B 27/08 (2006.01); B64F 5/00 (2017.01); B29K 105/08 (2006.01); B29K 307/04 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B64C 23/065 (2013.01); B29C 70/345 (2013.01); B29C 70/44 (2013.01); B32B 5/02 (2013.01); B32B 27/08 (2013.01); B64C 5/08 (2013.01); B64D 45/02 (2013.01); B64F 5/0009 (2013.01); B29K 2105/0872 (2013.01); B29K 2307/04 (2013.01); B29L 2031/3085 (2013.01); B32B 2262/106 (2013.01); B32B 2605/18 (2013.01); Y02T 50/164 (2013.01); Y02T 50/433 (2013.01);
Abstract

A method and apparatus for forming a winglet formed as a one-piece composite for an aircraft is presented. The winglet comprises a first blade, a second blade, and a root region. The first blade includes a first leading edge and a first trailing edge. The second blade includes a second leading edge and a second trailing edge. The second blade is positioned at an angle to the first blade. The root region is co-cured with the first blade and the second blade to form the winglet. The root region is configured to receive an attachment system for attaching the winglet to a wing of the aircraft.


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