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:
Jul. 10, 2018

Filed:

Oct. 23, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Michael J. Verrilli, Loveland, OH (US);

Mark Eugene Noe, West Chester, OH (US);

Mark Willard Marusko, Springboro, OH (US);

Paul Izon, Morrow, OH (US);

Robert Tyler, Harrison, OH (US);

Christopher Hasse, Kenwood, OH (US);

Assignee:

General Electric Company, schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/28 (2006.01); C04B 35/626 (2006.01); C04B 37/00 (2006.01); F01D 5/30 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/282 (2013.01); C04B 35/6269 (2013.01); C04B 37/001 (2013.01); F01D 5/147 (2013.01); F01D 5/30 (2013.01); F01D 11/00 (2013.01); C04B 2235/602 (2013.01); C04B 2235/604 (2013.01); C04B 2237/38 (2013.01); F05D 2220/32 (2013.01); F05D 2230/21 (2013.01); F05D 2230/60 (2013.01); F05D 2240/30 (2013.01); F05D 2300/6033 (2013.01);
Abstract

Methods for fabricating a component of a gas turbine engine are provided. In one embodiment, the method includes molding a CMC material to form a first portion of the gas turbine engine component, processing the first portion to form a first assembly, preparing the first assembly and a second portion of the gas turbine engine component for processing, and processing the first assembly and second portion to form a second assembly. In another embodiment, the method includes processing a first plurality of CMC plies to form a first assembly; positioning the first assembly and a second plurality of CMC plies on a tool for processing, the first assembly defining a first plane, the second plurality of plies defining a second plane, wherein the second plane is perpendicular to the first plane; and processing the first assembly and the second plurality of plies to form a second assembly.


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