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:
Nov. 16, 2021

Filed:

Sep. 02, 2016
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel L. Gysling, South Glastonbury, CT (US);

Glenn N. Levasseur, Colchester, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/00 (2006.01); F01D 21/14 (2006.01); G01H 1/00 (2006.01); F01D 17/04 (2006.01); G01M 15/14 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F01D 17/04 (2013.01); F01D 21/14 (2013.01); G01H 1/003 (2013.01); G01H 1/006 (2013.01); G01M 15/14 (2013.01); F05D 2220/32 (2013.01); F05D 2220/36 (2013.01); F05D 2240/30 (2013.01); F05D 2260/83 (2013.01); F05D 2270/334 (2013.01); F05D 2270/808 (2013.01);
Abstract

A method of health monitoring of a gas turbine engine includes mounting a detection system configured to detect an aeromechanical damping characteristic of a row of airfoils of a gas turbine. An actual aeromechanical damping characteristic of the row of airfoils is measured with the detection system. An output signal is generated indicative of the actual aeromechanical damping characteristic of the row of airfoils. A current flutter characteristic is determined based on the output signal indicative of the actual aeromechanical damping characteristic of the row of airfoils. An airfoil health monitoring system for gas turbine engine and a gas turbine engine are also disclosed.


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