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. 04, 2019

Filed:

Jan. 13, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Kevin J. Ryan, Alfred, ME (US);

Terence P. Tyler, Jr., East Waterboro, ME (US);

Ken F. Blaney, Middleton, NH (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/12 (2006.01); F01D 25/12 (2006.01); F02C 3/04 (2006.01); F01D 5/02 (2006.01); F01D 5/12 (2006.01); F01D 11/08 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); F01D 5/02 (2013.01); F01D 5/12 (2013.01); F01D 11/08 (2013.01); F02C 3/04 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/202 (2013.01);
Abstract

A blade outer air seal for a gas turbine engine includes a gas path surface exposed to exhaust gas flow, a first side extending radially outward from the gas path surface, a second side extending radially outward from the gas path surface, and a plurality of film cooling holes disposed on at least one of the gas path surface. The first side and the second side, the film cooling holes are disposed at locations described by a set of Cartesian coordinates set forth in Table 1. The Cartesian coordinates are provided by an axial coordinate, a circumferential coordinate and a radial coordinate relative to a defined point of origin. A gas turbine engine is also disclosed.


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