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:
Apr. 09, 2019

Filed:

Feb. 16, 2015
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Bartolomeo Palmieri, Guilford, CT (US);

John P. Rizzo, Jr., Vernon, CT (US);

Kaitlin M. Tomeo, Middletown, CT (US);

Alan C. Barron, Jupiter, FL (US);

Christopher J. Millea, Coventry, CT (US);

Henry H. Thayer, Wethersfield, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B24B 29/00 (2006.01); B24B 19/14 (2006.01); B24B 27/00 (2006.01); B24B 49/16 (2006.01); C23C 4/18 (2006.01); F01D 5/28 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
B24B 29/005 (2013.01); B24B 19/14 (2013.01); B24B 27/0038 (2013.01); B24B 49/16 (2013.01); C23C 4/18 (2013.01); F01D 5/288 (2013.01); F01D 9/02 (2013.01); F05D 2220/323 (2013.01); F05D 2230/90 (2013.01); F05D 2300/20 (2013.01);
Abstract

A method of polishing an outer surface of a ceramic coated gas turbine engine component includes applying a rotating diamond brush to the outer surface. The brush is configured to achieve a uniform finish of 150 microinches Ror less over the surface. The brush contains diamond impregnated bristles, and is affixed to a rotary head of a robotic arm. A force sensing controller limits brush forces against the component. The component disclosed is a hot section turbine vane designed for directional control of high temperature, high-pressure combustion gases, but the method may be applied to other components contained within such aerospace applications. The polished coating provides an improved thermal barrier for maintaining structural integrity of the component in environments having temperatures ranging up to 2,000 degrees Celsius. The method limits abrasive removal of ceramic material to only 0.0005 to 0.00075 inch, and saves time and expense over past practices.


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