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. 28, 2021

Filed:

Aug. 10, 2020
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Reza Oboodi, Morris Plains, NJ (US);

James Piascik, Randolph, NJ (US);

Donald M. Olson, Dover, NJ (US);

Natalie Kruk, Tempe, AZ (US);

Terence Whalen, Morristown, NJ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C23C 18/12 (2006.01); C23C 18/04 (2006.01); F01D 5/22 (2006.01); F01D 25/00 (2006.01); C04B 41/50 (2006.01); F23R 3/00 (2006.01); C04B 41/00 (2006.01); F01D 5/00 (2006.01); F01D 5/28 (2006.01); C04B 41/85 (2006.01);
U.S. Cl.
CPC ...
C23C 18/125 (2013.01); C04B 41/009 (2013.01); C04B 41/5024 (2013.01); C04B 41/85 (2013.01); C23C 18/04 (2013.01); F01D 5/005 (2013.01); F01D 5/225 (2013.01); F01D 5/284 (2013.01); F01D 5/288 (2013.01); F01D 25/005 (2013.01); F23R 3/007 (2013.01); F01D 5/282 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/22 (2013.01); F05D 2230/31 (2013.01); F05D 2230/40 (2013.01); F05D 2230/90 (2013.01); F05D 2240/11 (2013.01); F05D 2300/222 (2013.01); F05D 2300/6033 (2013.01); F23R 2900/00018 (2013.01); Y10T 428/249981 (2015.04);
Abstract

Methods for forming sintered-bonded high temperature coatings over ceramic turbomachine components are provided, as are ceramic turbomachine components having such high temperature coatings formed thereover. In one embodiment, the method includes the step or process of removing a surface oxide layer from the ceramic component body of a turbomachine component to expose a treated surface of the ceramic component body. A first layer of coating precursor material, which has a solids content composed predominately of at least one rare earth silicate by weight percentage, is applied to the treated surface. The first layer of the coating precursor material is then heat treated to sinter the solids content and form a first sintered coating layer bonded to the treated surface. The steps of applying and sintering the coating precursor may be repeated, as desired, to build a sintered coating body to a desired thickness over the ceramic component body.


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