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. 19, 2023

Filed:

May. 06, 2021
Applicant:

Applied Materials, Inc., Santa Clara, CA (US);

Inventors:

David Britz, Los Gatos, CA (US);

Pravin K. Narwankar, Sunnyvale, CA (US);

David Thompson, San Jose, CA (US);

Yuriy Melnik, San Jose, CA (US);

Sukti Chatterjee, San Jose, CA (US);

Assignee:

APPLIED MATERIALS, INC., Santa Clara, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); C23C 28/00 (2006.01); F01D 5/18 (2006.01); C23C 16/455 (2006.01); C23C 16/52 (2006.01); C23C 28/04 (2006.01); C23C 16/40 (2006.01); C23C 14/08 (2006.01);
U.S. Cl.
CPC ...
C23C 28/3455 (2013.01); C23C 16/45525 (2013.01); C23C 16/52 (2013.01); C23C 28/3215 (2013.01); C23C 28/345 (2013.01); F01D 5/186 (2013.01); F01D 5/288 (2013.01); C23C 14/083 (2013.01); C23C 16/40 (2013.01); C23C 28/042 (2013.01); F05D 2230/31 (2013.01); F05D 2240/24 (2013.01); F05D 2260/95 (2013.01); F05D 2300/121 (2013.01); F05D 2300/132 (2013.01); F05D 2300/134 (2013.01); Y10T 428/2462 (2015.01);
Abstract

Using the systems and methods discussed herein, CMAS corrosion is inhibited via CMAS interception in an engine environment and/or is prevented or reduced by the formation of a metal oxide protective coating on a hot engine section component. The CMAS interception can occur while the engine is in operation in flight or in a testing or quality control environment. The metal oxide protective coating can be applied over other coatings, including Gd-zirconates (GZO) or yttria-stabilized zirconia (YSZ). The metal oxide protective coating is applied at original equipment manufacturers (OEM) and can also be applied in-situ using a gas injection system during engine use in-flight or during maintenance or quality testing. The metal oxide protective coating contains a rare earth element, aluminum, zirconium, chromium, or combinations thereof and can have a thickness from 1 nm to 3,000 nm.


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