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:
Mar. 05, 2024

Filed:

Sep. 30, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Thomas E. Clark, Wells, ME (US);

Andrew E. Breault, Bolton, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/14 (2006.01); F01D 11/00 (2006.01); F02C 7/18 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 25/14 (2013.01); F01D 11/005 (2013.01); F02C 7/18 (2013.01); F02C 7/28 (2013.01); F05D 2250/75 (2013.01); F05D 2260/232 (2013.01); F05D 2260/31 (2013.01); F05D 2260/37 (2013.01);
Abstract

A gas turbine engine includes a primary flow path fluidly connecting a compressor section, a combustor section and a turbine section. A cooling air flowpath is positioned radially outward of the primary flowpath. A first seal spans from an inner diameter of the cooling air flowpath to an outer diameter of the cooling air flowpath. The first seal includes at least one axial convolution and a plurality of pass through features. A bifurcation feature is positioned downstream of the first seal. The bifurcation feature is configured to direct a portion of an airflow through the first seal into a cooling air passage. A second seal contacts the bifurcation and the first seal, such that fluid radially inward of the bifurcation feature.


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