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:
Apr. 07, 2020

Filed:

Sep. 11, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Jonathan Jeffery Eastwood, West Hartford, CT (US);

Joseph F. Englehart, Gastonia, NC (US);

Graham Ryan Philbrick, Durham, CT (US);

Henry K. Webster, Jupiter, FL (US);

Richard Seleski, Palm Beach Gardens, FL (US);

ChaiDee Woods Brown, Boca Raton, FL (US);

Michael G. McCaffrey, Windsor, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/052 (2006.01); F01D 11/24 (2006.01); F02C 7/18 (2006.01); F01D 25/32 (2006.01); F01D 25/24 (2006.01); B64D 33/02 (2006.01); F02C 7/05 (2006.01);
U.S. Cl.
CPC ...
F02C 7/052 (2013.01); B64D 33/02 (2013.01); F01D 11/24 (2013.01); F01D 25/246 (2013.01); F01D 25/32 (2013.01); F02C 7/05 (2013.01); F02C 7/18 (2013.01); B64D 2033/0246 (2013.01); F05D 2230/642 (2013.01); F05D 2240/11 (2013.01); F05D 2250/184 (2013.01); F05D 2260/201 (2013.01); F05D 2260/205 (2013.01); F05D 2260/607 (2013.01);
Abstract

A turbine section for a gas turbine engine includes blade outer air seals and stator vanes that provide a core flow path. A turbine case supports blade outer air seals and stator vanes. An annular cavity is provided between an interior surface of the turbine case and the blade outer air seals and the stator vanes. A hole extends through the turbine case from an exterior surface to the interior surface. The annular cavity extends axially to an exit. A manifold circumscribes the exterior surface of the turbine case and provides an annular space therebetween. The annular space is in fluid communication with the exit of the annular cavity via the hole.


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