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. 21, 2022

Filed:

Oct. 07, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Jacob Biernat, Lasalle, CA;

Mohammed Ennacer, St-Hubert, CA;

Remy Synnott, St-Jean-sur-Richelieu, CA;

Andrey Potiforov, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 25/24 (2006.01); F02C 7/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 25/24 (2013.01); F02C 7/12 (2013.01); F05D 2240/11 (2013.01); F05D 2240/127 (2013.01); F05D 2260/201 (2013.01); F05D 2260/2212 (2013.01);
Abstract

A turbine shroud segment for a gas turbine engine having an annular gas path extending about an engine axis. The engine has a turbine rotor mounted for rotation about the axis and having a plurality of blades extending into the gas path. The turbine shroud segment includes a body extending axially between a leading edge and a trailing edge and circumferentially between a first and second lateral edges. The body has a radially outer surface and a radially inner surface. The radially outer surface includes a textured surface exposed to a cooling flow. The radially inner surface defines an outer flow boundary surface of the gas path next to a tip of one of the blades. A cooling flow passageway is defined in the body and extends axially between one or more cooling inlets receiving the cooling flow from the textured surface and one or more cooling outlets.


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