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:
Oct. 16, 2018

Filed:

Sep. 16, 2014
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Todd Alan Anderson, Niskayuna, NY (US);

Nicholas Joseph Kray, Mason, OH (US);

Gregory Carl Gemeinhardt, Park Hills, KY (US);

Michael Harvey Schneider, Loveland, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/38 (2006.01); F01D 5/28 (2006.01); F04D 29/32 (2006.01); B29C 70/20 (2006.01); B29K 105/08 (2006.01); B29K 63/00 (2006.01); B29K 105/00 (2006.01); B29L 31/08 (2006.01); B29D 99/00 (2010.01);
U.S. Cl.
CPC ...
B29C 70/382 (2013.01); B29C 70/202 (2013.01); F01D 5/282 (2013.01); F04D 29/324 (2013.01); B29D 99/0025 (2013.01); B29K 2063/00 (2013.01); B29K 2105/0005 (2013.01); B29K 2105/089 (2013.01); B29L 2031/08 (2013.01); F05D 2220/36 (2013.01); F05D 2300/224 (2013.01); F05D 2300/44 (2013.01); F05D 2300/6034 (2013.01); Y02T 50/672 (2013.01);
Abstract

An airfoil structure is presented. The airfoil structure includes an outer casing substantially surrounding a composite core. The composite core includes a plurality of fiber bands, each of the plurality of fiber bands is placed at a predetermined position and orientation at a time, wherein the plurality of fiber bands are interwoven in an in-plane and out-of-plane orientation by interleaving each of the plurality of fiber bands placed in a plane with one or more of the plurality of fiber bands of an adjacent plane to define an interleaved structure. A method for manufacturing an airfoil structure including the composite core is also presented.


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