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. 15, 2025

Filed:

Dec. 13, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel S. Rogers, Lyman, ME (US);

Robert A. White, Iii, Meriden, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/28 (2006.01); F01D 11/12 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); F01D 9/04 (2013.01); F01D 11/122 (2013.01); F01D 25/005 (2013.01); F05D 2230/90 (2013.01); F05D 2240/55 (2013.01); F05D 2300/20 (2013.01); F05D 2300/611 (2013.01);
Abstract

A section of a gas turbine engine includes a ceramic component and a metallic component situated adjacent the ceramic component. The ceramic component and the metallic component are situated outside of a core flow path of the gas turbine engine. The section of a gas turbine engine also includes an interface between the ceramic component and a metallic component and a mullite-based coating disposed at the interface. The coating provides thermal protection to the ceramic component and the metallic component, and provides thermochemical protection against interaction between the ceramic component and the metallic component. A gas turbine engine and a method of protecting components in a gas turbine engine are also disclosed.


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