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:
Jul. 09, 2019

Filed:

Mar. 27, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Sameh Dardona, South Windsor, CT (US);

Cagatay Tokgoz, Beaumont, TX (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 5/28 (2006.01); G05B 23/02 (2006.01); G01M 15/14 (2006.01); F01D 21/00 (2006.01); F01D 21/14 (2006.01); F02C 9/00 (2006.01); G05B 9/02 (2006.01);
U.S. Cl.
CPC ...
G05B 23/0205 (2013.01); F01D 5/147 (2013.01); F01D 5/288 (2013.01); F01D 21/003 (2013.01); F01D 21/14 (2013.01); G01M 15/14 (2013.01); F02C 9/00 (2013.01); F05D 2220/36 (2013.01); F05D 2260/80 (2013.01); F05D 2260/83 (2013.01); F05D 2300/121 (2013.01); F05D 2300/133 (2013.01); G05B 9/02 (2013.01); Y02T 50/671 (2013.01);
Abstract

An apparatus and method for detecting a short in a blade of a gas turbine engine, the apparatus including: a first plate configured to form a first capacitor with the protective sheath when the apparatus is located proximate to the blade; a second plate configured to form another capacitor with a portion of the airfoil when the apparatus is located proximate to the blade; and a voltage source electrically connected to the first plate and the second plate.


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