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:
Sep. 22, 2020

Filed:

Jun. 18, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Kristofer L. Peterson, Charleston, SC (US);

Eileen E. Miller, Summerville, SC (US);

Mark Allen Ulvin, Brier, WA (US);

Ronald Leroy McGhee, Lynnwood, WA (US);

David A. Lilienthal, Summerville, SC (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 35/02 (2006.01); B29C 70/54 (2006.01); B32B 3/08 (2006.01); B32B 7/08 (2019.01); B32B 7/12 (2006.01); B32B 27/08 (2006.01); B29C 70/30 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 35/02 (2013.01); B29C 70/543 (2013.01); B32B 3/085 (2013.01); B32B 7/08 (2013.01); B32B 7/12 (2013.01); B32B 27/08 (2013.01); B29C 70/30 (2013.01); B29L 2031/3076 (2013.01); B32B 2250/03 (2013.01); B32B 2605/18 (2013.01);
Abstract

A method for fabricating a composite structure is provided. A first number of layers of composite material is laid up to form a first set of stiffeners. A second number of layers of composite material is laid up to form a panel. The first set of stiffeners is associated with a first side of the panel. A pre-cured composite strip is positioned on a second side of the panel, opposite the first side. A third number of layers of composite material is laid up on the second side of the panel to form a second set of stiffeners running perpendicular to the first set of stiffeners. The pre-cured composite lies at an intersection between one of the first set of stiffeners and one of the second set of stiffeners. All the layers of composite material are co-cured to form the composite structure.


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