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. 27, 2016

Filed:

Nov. 26, 2012
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

John H. Moselage, III, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/22 (2006.01); B29C 70/28 (2006.01); B64C 3/18 (2006.01); B29C 70/34 (2006.01); B64C 1/26 (2006.01); B64C 3/20 (2006.01);
U.S. Cl.
CPC ...
B64C 3/185 (2013.01); B29C 70/347 (2013.01); B64C 1/26 (2013.01); B64C 3/20 (2013.01); Y02T 50/433 (2013.01);
Abstract

Apparatus and methods provide for the construction of wing sections having multi-box wing spars. According to one aspect of the disclosure provided herein, an aircraft wing may be constructed by applying one or more layers of composite material onto a plurality of wing mandrels. The wing mandrels, when placed together, form the shape of the wing. After the layers of composite material are applied to each individual mandrel, the mandrels are abutted together. Thereafter, the mandrels are compressed using wing surface tooling applied to the plurality of wing mandrels. The composite material is thereafter cured. After curing, the wing surface tooling and mandrels are removed, resulting in a wing having multi-box wing spars and skin.


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