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:
Feb. 02, 2021

Filed:

Aug. 21, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sergio Filippi, Montgomery, OH (US);

Ryan Nicholas Porter, Jamestown, OH (US);

Craig Alan Gonyou, Blanchester, OH (US);

Scott Alan Schimmels, Miamisburg, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F01D 25/24 (2006.01); F01D 11/08 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 11/08 (2013.01); F01D 25/005 (2013.01); F01D 25/246 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/91 (2013.01); F05D 2260/201 (2013.01); F05D 2300/2112 (2013.01); F05D 2300/2261 (2013.01); F05D 2300/6033 (2013.01);
Abstract

Shroud assemblies and methods for cooling gas turbine engine shrouds are provided. For example, a shroud assembly comprises a shroud segment having hot and cold side portions. The hot side portion faces a gas flow path, and the cold side portion faces a cooling fluid flow path. The shroud assembly further comprises a shroud hanger for mounting the shroud segment in the gas turbine engine. The shroud hanger includes a conduit for receipt of a flow of cooling fluid that defines an outlet configured for the flow of cooling fluid to exit the conduit substantially tangential to the cold side portion of the shroud segment. The shroud and shroud hanger together define an annular cavity that forms the cooling fluid flow path, and fluid exits a plurality of conduits defined in the shroud hanger into the cavity substantially tangential to the shroud cold side to cool the shroud cold side.


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