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:
Oct. 07, 2025

Filed:

Nov. 02, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

James T. Roach, Vernon, CT (US);

Jonas Banhos, West Hartford, CT (US);

Russell Kim, Temecula, CA (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 5/18 (2006.01); F01D 5/28 (2006.01); F01D 9/06 (2006.01); F01D 11/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 5/187 (2013.01); F01D 5/188 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); F01D 9/065 (2013.01); F01D 11/001 (2013.01); F05D 2240/81 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/6034 (2013.01);
Abstract

A combined gas turbine engine vane and blade outer air seal assembly includes a vane having an airfoil extending from the leading edge to a trailing edge, and has an outer platform. The outer platform has a cooling channel that extends into the airfoil to receive cooling air. The outer platform extends to an integral blade outer air seal to be positioned radially outwardly of a turbine blade in a gas turbine engine. At least a portion of the vane and the blade outer air seal are formed of ceramic matrix composite materials. A gas turbine engine is also disclosed.


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