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. 12, 2019

Filed:

Feb. 07, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Scott D. Lewis, Vernon, CT (US);

Brandon M. Rapp, West Hartford, CT (US);

Jeffrey S. Beattie, South Glastonbury, CT (US);

Matthew Andrew Hough, West Hartford, CT (US);

Bret M. Teller, Meriden, CT (US);

Jeffrey Michael Jacques, East Hartford, CT (US);

Max Asterlin, Vernon, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 11/08 (2006.01); F23R 3/00 (2006.01); F23R 3/04 (2006.01); F01D 9/06 (2006.01); F01D 25/12 (2006.01); F23R 3/06 (2006.01); F01D 9/02 (2006.01); F23R 3/02 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 5/18 (2013.01); F01D 9/023 (2013.01); F01D 9/065 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F23R 3/002 (2013.01); F23R 3/02 (2013.01); F23R 3/04 (2013.01); F23R 3/06 (2013.01); F05D 2240/11 (2013.01); F05D 2240/35 (2013.01); F05D 2240/81 (2013.01); F05D 2260/202 (2013.01); F23R 2900/03041 (2013.01); F23R 2900/03042 (2013.01); Y02T 50/675 (2013.01); Y02T 50/676 (2013.01);
Abstract

A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a platform that axially extends between a leading edge and a trailing edge, circumferentially extends between a first mate face and a second mate face, and includes a gas path surface and a non-gas path surface. The component defines at least one cavity that extends at least partially inside of the component. A first plurality of cooling holes extends from the at least one cavity to at least one of the first mate face and the second mate face and a second plurality of cooling holes extends from either the at least one cavity or the non-gas path surface to the gas path surface.


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