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:
Jan. 25, 2022

Filed:

Sep. 18, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Benjamin Scott Huizenga, Cincinnati, OH (US);

Darrell Glenn Senile, Oxford, OH (US);

Robert Alan Frederick, West Chester, OH (US);

Paul Joseph Kreitzer, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/00 (2006.01); F01D 9/04 (2006.01); F01D 5/18 (2006.01); F01D 5/02 (2006.01); F01D 25/12 (2006.01); F02C 3/04 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F01D 9/041 (2013.01); F01D 5/02 (2013.01); F01D 5/186 (2013.01); F01D 5/189 (2013.01); F01D 25/12 (2013.01); F02C 3/04 (2013.01); F02C 7/18 (2013.01); F05D 2220/32 (2013.01); F05D 2240/128 (2013.01); F05D 2240/24 (2013.01); F05D 2240/35 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2300/6033 (2013.01); Y02T 50/60 (2013.01);
Abstract

One aspect the present subject matter is directed to a nozzle segment including a stator component having an airfoil. The airfoil includes a leading edge portion, a trailing edge portion, a pressure side wall and a suction side wall and a plurality of film holes in fluid communication with the radial cooling channel. A strut is disposed within the radial cooling channel and defines an inner radial cooling passage within the radial cooling channel. The strut defines a plurality of apertures that provide for fluid communication from the inner radial cooling passage to the radial cooling channel and the plurality of film holes provide for bore cooling of the airfoil of at least one of the pressure side wall or the suction side wall and provide for film cooling of the trailing edge portion of the airfoil between about fifty percent and one hundred percent of the chord length.


Find Patent Forward Citations

Loading…