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:
Mar. 12, 2019

Filed:

Oct. 29, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Stephen Lee Metschan, Black Diamond, WA (US);

Richard V. Phillips, Enumclaw, WA (US);

Kurtis S. Willden, Kent, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/30 (2006.01); B32B 37/14 (2006.01); B32B 37/10 (2006.01); B32B 37/06 (2006.01); B29C 70/54 (2006.01);
U.S. Cl.
CPC ...
B32B 37/14 (2013.01); B29C 70/30 (2013.01); B29C 70/541 (2013.01); B29C 70/543 (2013.01); B32B 37/06 (2013.01); B32B 37/1018 (2013.01); B32B 2305/74 (2013.01);
Abstract

Systems and methods of forming a skin for a composite structure and composite structures including the same. The systems and methods include operatively attaching a charge of composite material to a flexible substrate to define a composite-substrate assembly. The systems and methods further include deforming the composite-substrate assembly by conforming the composite-substrate assembly to a non-planar pre-forming surface of a pre-forming mandrel to define a non-planar skin surface contour on the charge of composite material. The systems and methods further include maintaining the charge of composite material in tension in a direction that is parallel to an interface between the charge of composite material and the flexible substrate during the deforming.


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