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:
Sep. 09, 2025

Filed:

Oct. 07, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Connor C. Perry, West Hartford, CT (US);

Xiaomei Fang, South Glastonbury, CT (US);

Bradley L. Paquin, Cheshire, CT (US);

Jacob Yochimowitz, East Haddam, CT (US);

Sushruth G. Kamath, Manchester, CT (US);

Jun Cao, Scarsdale, NY (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); C23C 4/11 (2016.01); F01D 9/02 (2006.01); F01D 25/00 (2006.01); F01D 25/08 (2006.01); F01D 25/14 (2006.01);
U.S. Cl.
CPC ...
F01D 25/005 (2013.01); F01D 9/02 (2013.01); F01D 25/08 (2013.01); F01D 25/145 (2013.01); F05D 2220/32 (2013.01); F05D 2230/31 (2013.01); F05D 2240/10 (2013.01); F05D 2240/128 (2013.01); F05D 2240/14 (2013.01); F05D 2240/15 (2013.01); F05D 2260/231 (2013.01); F05D 2300/211 (2013.01);
Abstract

A gas turbine engine component includes a structural component having a surface, the structural component having an organic matrix composite material; and a cured thermal barrier layer on the surface, wherein the cured thermal barrier layer is a pre-ceramic layer including inorganic matrix containing silicon oxides reinforced with glass or quartz fibers.


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