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:
Feb. 02, 2016

Filed:

Jul. 05, 2012
Applicants:

Bowden Kirkpatrick, Niskayuna, NY (US);

Mark Ernest Vermilyea, Niskayuna, NY (US);

Derrick Wayne Lamm, Baltimore, MD (US);

Melissa Ann Marie Bramell, Baltimore, MD (US);

David Louis Callahan, Severna Park, MD (US);

Jason Michael Seabrease, Middle River, MD (US);

Inventors:

Bowden Kirkpatrick, Niskayuna, NY (US);

Mark Ernest Vermilyea, Niskayuna, NY (US);

Derrick Wayne Lamm, Baltimore, MD (US);

Melissa Ann Marie Bramell, Baltimore, MD (US);

David Louis Callahan, Severna Park, MD (US);

Jason Michael Seabrease, Middle River, MD (US);

Assignee:

General Electric Company, Niskayuna, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 33/50 (2006.01); B29C 57/00 (2006.01); B29C 70/44 (2006.01); B29C 70/22 (2006.01); B29C 67/00 (2006.01); B29C 70/76 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
B29C 33/505 (2013.01); B29C 57/00 (2013.01); B29C 70/222 (2013.01); B29C 70/44 (2013.01); B29C 67/0025 (2013.01); B29C 70/766 (2013.01); F01D 25/243 (2013.01); F05D 2300/603 (2013.01);
Abstract

A method of manufacturing a flanged composite component is provided. The method includes coupling a composite structure to s first composite material. The method includes coupling a second composite material to the composite structure and placing a first expansion device within the composite structure. A forming element is coupled to at least one of the first composite material, the composite structure, and the second composite material against the mold. The method includes coupling a pressure element to the forming element to define a space among the mold, the forming element, and the pressure element. The method includes expanding the first expansion device to impart a force to the second composite material to move the second composite material away from the composite structure and into the space to facilitate forming a first flange.


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