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. 11, 2023

Filed:

Sep. 04, 2019
Applicant:

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

Inventors:

Sukti Chatterjee, San Jose, CA (US);

Kenichi Ohno, Sunnyvale, CA (US);

Lance A. Scudder, Sunnyvale, CA (US);

Yuriy Melnik, San Jose, CA (US);

David A. Britz, San Jose, CA (US);

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

Thomas Knisley, Livonia, MI (US);

Mark Saly, Santa Clara, CA (US);

Jeffrey Anthis, San Jose, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C23C 16/56 (2006.01); C23C 16/40 (2006.01); C22C 19/03 (2006.01);
U.S. Cl.
CPC ...
C23C 16/56 (2013.01); C22C 19/03 (2013.01); C23C 16/405 (2013.01);
Abstract

Embodiments of the present disclosure generally relate to protective coatings on aerospace components and methods for depositing the protective coatings. In one or more embodiments, a method for producing a protective coating on an aerospace component includes depositing a metal oxide template layer on the aerospace component containing nickel and aluminum (e.g., nickel-aluminum superalloy) and heating the aerospace component containing the metal oxide template layer during a thermal process and/or an oxidation process. The thermal process and/or oxidation process includes diffusing aluminum contained within the aerospace component towards a surface of the aerospace component containing the metal oxide template layer, oxidizing the diffused aluminum to produce an aluminum oxide layer disposed between the aerospace component and the metal oxide template layer, and removing at least a portion of the metal oxide template layer while leaving the aluminum oxide layer.


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