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:
Aug. 11, 2020

Filed:

Jan. 02, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Lane Thornton, Meriden, CT (US);

Matthew A. Devore, Cromwell, CT (US);

Dominic J. Mongillo, West Hartford, CT (US);

Steven Bruce Gautschi, Naugatuck, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F05D 2220/32 (2013.01); F05D 2240/303 (2013.01); F05D 2250/14 (2013.01); F05D 2250/312 (2013.01); F05D 2250/313 (2013.01); F05D 2250/314 (2013.01); F05D 2250/324 (2013.01); F05D 2250/38 (2013.01); F05D 2260/202 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

A gas turbine engine component comprises an airfoil with a suction side and pressure side extending from a leading edge to a trailing edge. There are a plurality of cooling holes adjacent the leading edge, with the cooling holes having a non-circular shape, with a longer dimension and a smaller dimension. The airfoil defines a radial direction from a radially outer end to a radially inner end, and radially outer of the cooling holes spaced toward the radially outer end, which have the longer dimension extending closer to parallel to the radial direction. Radially inner cooling holes closer to the radially inner end having the longer dimension extend to be closer to perpendicular relative to the radial direction compared to the radially outer cooling holes.


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