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:
Jun. 22, 2021

Filed:

Apr. 20, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Steven D. Porter, Wethersfield, CT (US);

Shawn M. McMahon, West Hartford, CT (US);

Kevin Zacchera, Glastonbury, CT (US);

Noah Wadsworth, West Hartford, CT (US);

Christopher Whitfield, Rocky Hill, CT (US);

Sean D. Bradshaw, White Plains, NY (US);

Dennis M. Moura, South Windsor, CT (US);

David Bitzko, West Palm Beach, FL (US);

Alex J. Schneider, South Glastonbury, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 11/00 (2006.01); F01D 25/12 (2006.01); F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/023 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 25/12 (2013.01); F05D 2220/32 (2013.01); F05D 2240/11 (2013.01); F05D 2240/121 (2013.01); F05D 2240/55 (2013.01); F05D 2260/20 (2013.01);
Abstract

A gas turbine engine includes a combustor. A turbine section is in fluid communication with the combustor. The turbine section includes a first vane stage aft of the combustor. A plurality of vane cooling passages extending through a forward flange of the first vane stage to the radial inner surface for communicating cooling airflow into the core flow path forward of the leading edge. A seal assembly is disposed between the combustor and the forward flange of the vane stage. The seal includes a plurality of circumferentially spaced apart slots and a plurality of seal cooling passages that extend from the radially outer surface to the radially inner surface at each of the plurality of circumferentially spaced apart slots.


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