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. 03, 2023

Filed:

Mar. 02, 2020
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Jonathan Ortiz, El Centro, CA (US);

Raymond Surace, Newington, CT (US);

Renee J. Jurek, Colchester, CT (US);

Tracy A. Propheter-Hinckley, Rocky Hill, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/20 (2006.01); F02C 3/04 (2006.01); F01D 5/02 (2006.01); F02C 9/18 (2006.01); F04D 29/54 (2006.01); F01D 11/24 (2006.01); F01D 9/06 (2006.01);
U.S. Cl.
CPC ...
F01D 11/20 (2013.01); F01D 5/02 (2013.01); F01D 9/065 (2013.01); F01D 11/24 (2013.01); F02C 3/04 (2013.01); F02C 9/18 (2013.01); F04D 29/542 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/213 (2013.01); F05D 2300/50212 (2013.01); Y02T 50/60 (2013.01);
Abstract

A gas turbine engine according to an example of the present disclosure include a compressor section, a combustor, and a turbine section. The combustor has a radially outer surface that defines a diffuser chamber radially outwardly of the combustor. The turbine section has a high pressure turbine first stage blade that has an outer tip, and a blade outer air seal positioned radially outwardly of the outer tip. A tap for tapping air has been compressed by the compressor and is passed through a heat exchanger. The air downstream of the heat exchanger passes through at least one pipe and into a manifold radially outward of the blade outer air seal, and then passes across the blade outer air seal to cool the blade outer air seal.


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