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:
Dec. 21, 2021

Filed:

Apr. 30, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventor:

Agnieszka M. Wusatowska-Sarnek, Manchester, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 11/12 (2006.01); C23C 8/68 (2006.01); C23C 8/80 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); C23C 8/68 (2013.01); C23C 8/80 (2013.01); F01D 11/122 (2013.01); F05D 2220/3215 (2013.01); F05D 2230/312 (2013.01); F05D 2230/314 (2013.01); F05D 2230/90 (2013.01); F05D 2240/24 (2013.01); F05D 2240/55 (2013.01); F05D 2300/131 (2013.01); F05D 2300/132 (2013.01); F05D 2300/133 (2013.01); F05D 2300/134 (2013.01); F05D 2300/171 (2013.01); F05D 2300/174 (2013.01); F05D 2300/177 (2013.01); F05D 2300/506 (2013.01); F05D 2300/611 (2013.01);
Abstract

A gas turbine engine includes an engine static structure extending circumferentially about an engine centerline axis; a compressor section, a combustor section, and a turbine section within the engine static structure. At least one of the compressor section and the turbine section includes at least one airfoil and at least one seal member adjacent to the at least one airfoil. A tip of the at least one airfoil is metal having a wear resistant coating and the at least one seal member is coated with an abradable coating. The wear resistant coating is formed as a layer in a base metal surface of the airfoil, has a thickness less than or equal to 10 mils (254 micrometers) and includes metal boride compounds.


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