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.

Patent No.:

US 9804058 B1

PDF
Full Text
Expired
Date of Patent:
Oct. 31, 2017

Filed:

Feb. 27, 2014
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Kin-Leung Cheung, Toronto, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); C23C 28/00 (2006.01); C23C 28/02 (2006.01); F01D 5/28 (2006.01); C23C 28/04 (2006.01); C23C 4/073 (2016.01);
U.S. Cl.
CPC ...
G01M 15/14 (2013.01); C23C 4/073 (2016.01); C23C 28/00 (2013.01); C23C 28/021 (2013.01); C23C 28/022 (2013.01); C23C 28/042 (2013.01); C23C 28/30 (2013.01); C23C 28/32 (2013.01); C23C 28/3215 (2013.01); C23C 28/44 (2013.01); F01D 5/28 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); F01D 5/286 (2013.01); F01D 5/288 (2013.01); F05D 2260/80 (2013.01);
Abstract

A component of a gas turbine engine comprises a substrate, a corrosion resistant top layer, and an intermediate corrodible layer disposed between the corrosion resistant top layer and the substrate. When corroding, the intermediate layer has a color contrasting with a color of the top layer. A method of detecting a crack when it penetrated the top layer in a component of a gas turbine engine having a corrosion resistant top layer and an intermediate corrodible layer comprises, in sequence, observing that at least one area of the component has a color contrasting with that of the top layer; determining that the color of the at least one area is a result of corrosion of the intermediate corrodible layer; and determining that the top layer has a crack as a result of determining corrosion of the intermediate layer. A method of facilitating crack detection in a component is also presented.


Find Patent Forward Citations

Cheung, Kin-Leung. (2017). Method of facilitating visual detection of a crack in a component of a gas turbine engine (U.S. Patent No. 9804058). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9804058

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

Loading…