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. 07, 2023

Filed:

Dec. 02, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Kirk Douglas Gallier, Liberty Township, OH (US);

Darrell Glenn Senile, Oxford, OH (US);

John Calhoun, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); B28B 23/00 (2006.01); B32B 37/14 (2006.01); B32B 38/10 (2006.01); B32B 38/08 (2006.01); B32B 38/00 (2006.01); F01D 9/04 (2006.01); F01D 25/00 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); B28B 23/0068 (2013.01); B32B 37/142 (2013.01); B32B 38/10 (2013.01); F01D 5/147 (2013.01); F01D 5/284 (2013.01); F01D 5/288 (2013.01); B32B 38/0036 (2013.01); B32B 38/08 (2013.01); B32B 2305/80 (2013.01); B32B 2315/02 (2013.01); F01D 5/18 (2013.01); F01D 9/041 (2013.01); F01D 25/005 (2013.01); F01D 25/12 (2013.01); F05D 2220/32 (2013.01); F05D 2230/50 (2013.01); F05D 2230/90 (2013.01); F05D 2260/202 (2013.01); F05D 2260/204 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/611 (2013.01); Y02T 50/60 (2013.01);
Abstract

Airfoils for gas turbine engines are provided. In one embodiment, an airfoil formed from a ceramic matrix composite material includes opposite pressure and suction sides extending radially along a span and defining an outer surface of the airfoil. The airfoil also includes opposite leading and trailing edges extending radially along the span. The pressure and suction sides extend axially between the leading and trailing edges. The leading edge defines a forward end of the airfoil, and the trailing edge defining an aft end of the airfoil. Further, the airfoil includes a trailing edge portion defined adjacent the trailing edge at the aft end of the airfoil; a plenum defined within the airfoil forward of the trailing edge portion; and a cooling passage defined within the trailing edge portion proximate the suction side. Methods for forming airfoils for gas turbine engines also are provided.


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