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:
Jun. 29, 2021

Filed:

Oct. 23, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Steven P. Walker, Arlington, WA (US);

Perlas G. Martinez, Everett, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/00 (2006.01); B32B 1/04 (2006.01); B32B 1/08 (2006.01); B32B 3/04 (2006.01); B32B 3/24 (2006.01); B64C 9/02 (2006.01); B64F 5/10 (2017.01); B32B 37/18 (2006.01); B32B 38/00 (2006.01); B32B 3/26 (2006.01); B29C 70/30 (2006.01); B32B 5/02 (2006.01); B29C 70/06 (2006.01); B64C 3/20 (2006.01); B64C 9/16 (2006.01); B64C 3/26 (2006.01); B64C 3/18 (2006.01); B29L 24/00 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B64C 9/00 (2013.01); B29C 70/30 (2013.01); B32B 1/08 (2013.01); B32B 3/04 (2013.01); B32B 3/266 (2013.01); B32B 37/18 (2013.01); B32B 38/0004 (2013.01); B64C 9/02 (2013.01); B64F 5/10 (2017.01); B29C 70/06 (2013.01); B29L 2024/00 (2013.01); B29L 2031/3085 (2013.01); B32B 1/04 (2013.01); B32B 5/02 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2605/18 (2013.01); B64C 3/185 (2013.01); B64C 3/20 (2013.01); B64C 3/26 (2013.01); B64C 9/16 (2013.01); B64C 2009/005 (2013.01); Y02T 50/40 (2013.01); Y10T 428/13 (2015.01); Y10T 428/1369 (2015.01); Y10T 428/1393 (2015.01); Y10T 428/2419 (2015.01); Y10T 428/24331 (2015.01);
Abstract

An aircraft flap is constructed of nested layers of composite material in the aircraft flap that include an inner layer, a middle layer and an outer layer. The aircraft flap is constructed with the inner layer laid up around a central mandrel, the middle layer laid up around the middle layer and the outer layer laid up around the middle layer. The inner layer, the middle layer and the outer layer are co-cured on the mandrel, removed from the mandrel and then assembled together with the inner layer formed in a folded over configuration around a hollow interior volume of the aircraft flap, the middle layer formed in a folded over configuration over the inner layer, and the outer layer formed in a folded over configuration around the middle layer.


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