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:
Apr. 21, 2025

Filed:

Jan. 19, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

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

Brian T. Hazel, Avon, CT (US);

Zhongfen Ding, South Windsor, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2005.12); C04B 41/50 (2005.12); C04B 41/89 (2005.12);
U.S. Cl.
CPC ...
F01D 11/00 (2012.12); C04B 41/5096 (2012.12); C04B 41/89 (2012.12); F01D 11/005 (2012.12); F05D 2220/32 (2012.12); F05D 2300/2261 (2012.12); F05D 2300/50211 (2012.12); F05D 2300/516 (2012.12); F05D 2300/6033 (2012.12); F05D 2300/611 (2012.12);
Abstract

A seal system a ceramic component having a surface region defining a first surface roughness, a metallic component situated adjacent the surface region, and a coating system disposed on the surface region. The coating system includes a silicon-containing layer on the surface region and a barrier layer on the silicon-containing layer. The silicon-containing layer has a surface in contact with the barrier layer. The barrier layer has a surface in contact with the metallic component. The surface of the barrier layer has a second surface roughness that is less than the first surface roughness. The barrier layer limits interaction between silicon of the silicon-containing layer and elements of the metallic component. The barrier layer has a coefficient of thermal expansion that is within about 60% of a coefficient of thermal expansion of the ceramic component. A gas turbine engine and a method are also disclosed.


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