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:
Dec. 11, 2018

Filed:

Jul. 26, 2013
Applicant:

Bruce L. Smith, Oviedo, FL (US);

Inventor:

Bruce L. Smith, Oviedo, FL (US);

Assignee:

Siemens Energy, Inc., Orlando, FL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B23P 6/00 (2006.01); F01D 5/00 (2006.01); F01D 5/28 (2006.01);
U.S. Cl.
CPC ...
B23P 6/002 (2013.01); F01D 5/005 (2013.01); F01D 5/186 (2013.01); F01D 5/187 (2013.01); F01D 5/288 (2013.01); F05D 2230/80 (2013.01); F05D 2240/122 (2013.01); Y10T 29/49238 (2015.01);
Abstract

An airfoil () including an internal cooling circuit () to direct cooling fluid () through an interior of the airfoil. The airfoil also includes a trailing edge (') defining plugged holes () and cooling holes () along a radial direction (). A selective group () of the cooling and plugged holes are based on a reduced cooling fluid requirement at the trailing edge (′) resulting from an improved thermal barrier coating (). A process () is also provided including removing () an airfoil from service in a gas turbine engine and adding or improving () a thermal barrier coating on the airfoil. The process also includes selectively () plugging holes in the airfoil in response to a reduced cooling fluid required through the airfoil as a result of the added or improved thermal barrier coating.


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