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:
Oct. 06, 2020

Filed:

Sep. 02, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Andrew Consiglio, Southbury, CT (US);

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

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 27/00 (2006.01); F01D 21/14 (2006.01); F01D 17/04 (2006.01); F01D 21/00 (2006.01); G01H 1/00 (2006.01); F04D 29/32 (2006.01); G01M 15/14 (2006.01);
U.S. Cl.
CPC ...
F04D 27/001 (2013.01); F01D 17/04 (2013.01); F01D 21/003 (2013.01); F01D 21/14 (2013.01); F04D 29/325 (2013.01); G01H 1/006 (2013.01); G01M 15/14 (2013.01); F05D 2220/36 (2013.01); F05D 2270/334 (2013.01); F05D 2270/808 (2013.01);
Abstract

An aeromechanical identification system for turbomachine includes at least one actuator mounted on a stationary structure to excite rotatable airfoils. At least one sensor is mounted proximate the airfoils for measuring a response of the airfoils responsive to excitation from the at least one actuator. A controller is configured to determine a damping characteristic of an aeromechanical mode of the rotating airfoils based on the excitation and the response. A gas turbine engine and a method of determining a flutter boundary for an airfoil of a turbomachine are also disclosed.


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