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. 29, 2022

Filed:

Sep. 15, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

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

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

Atul Kohli, Tolland, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 25/12 (2006.01); F04D 29/58 (2006.01); F01D 9/02 (2006.01); F01D 11/08 (2006.01); F04D 29/08 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 5/187 (2013.01); F01D 25/12 (2013.01); F04D 29/582 (2013.01); F01D 9/02 (2013.01); F01D 11/08 (2013.01); F04D 29/083 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F05D 2220/32 (2013.01); F05D 2240/303 (2013.01); F05D 2250/38 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); Y02T 50/60 (2013.01);
Abstract

An airfoil for a gas turbine engine includes pressure and suction side walls joined to one another at leading and trailing edges to provide an exterior airfoil surface. The pressure and suction side walls are spaced apart from one another in a thickness direction. A stagnation line is located near the leading edge. A cooling passage is provided between the pressure and suction side walls. The showerhead cooling holes are arranged at least one of adjacent to or on the stagnation line. At least one of the showerhead cooling holes has a metering hole fluidly connecting the cooling passage to a diffuser arranged at the exterior airfoil surface. At least one showerhead cooling hole is arranged on each of opposing sides of the stagnation line. Each showerhead cooling hole has the diffuser with a first diffuser angle that expands downstream in the thickness direction in opposing directions from one another when separated by the stagnation line.


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