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:
Nov. 26, 2024

Filed:

Jun. 08, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Herbert Chidsey Roberts, Middletown, OH (US);

Glenn Curtis Taxacher, Simpsonville, SC (US);

Timothy P. Coons, Cincinnati, OH (US);

Jared Hogg Weaver, Clifton Park, NY (US);

Daniel Gene Dunn, Guilderland, NY (US);

Jerome Geoffrey Magnant, Woodbury, MN (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/00 (2006.01); C04B 37/00 (2006.01); C04B 41/45 (2006.01); C04B 41/81 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/005 (2013.01); C04B 37/001 (2013.01); C04B 41/459 (2013.01); C04B 41/81 (2013.01); F01D 25/005 (2013.01); F05D 2220/32 (2013.01); F05D 2230/80 (2013.01); F05D 2240/11 (2013.01); F05D 2240/12 (2013.01); F05D 2240/128 (2013.01); F05D 2240/14 (2013.01); F05D 2240/30 (2013.01); F05D 2240/35 (2013.01); F05D 2300/6033 (2013.01);
Abstract

Composite components and methods for adding a composite material to a composite component are provided. For example, a method comprises positioning a composite material segment against the composite component to form a component layup; applying an insulating material around at least a portion of the component layup to form an insulated layup; and densifying the insulated layup, where the composite component was previously densified before positioning the composite material segment against the composite component. In some embodiments, the composite material is ceramic matrix composite (CMC) and the composite material segment is a plurality of CMC plies. The composite component may be a CMC gas turbine engine component that comprises an original CMC component and a new CMC material segment joined to the original CMC component through the transfer of silicon between the original CMC component and the new CMC material segment during melt infiltration.


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