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:
Mar. 23, 2021

Filed:

Dec. 11, 2015
Applicants:

General Electric Company, Schenectady, NY (US);

William Forrester Seely, Greenville, SC (US);

Xu Fu, Shanghai, CN;

Mustafa Tekin Dokucu, Niskayuna, NY (US);

Ronghui Zhou, Shanghai, CN;

Inventors:

William Forrester Seely, Greenville, SC (US);

Xu Fu, Shanghai, CN;

Mustafa Tekin Dokucu, Niskayuna, NY (US);

Ronghui Zhou, Shanghai, CN;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/14 (2006.01); F04D 27/02 (2006.01); F04D 29/66 (2006.01); F01D 25/06 (2006.01); G01H 1/00 (2006.01); F01D 21/04 (2006.01); F02C 9/00 (2006.01); F01D 21/00 (2006.01); G01H 13/00 (2006.01); G05B 13/04 (2006.01);
U.S. Cl.
CPC ...
F01D 21/14 (2013.01); F01D 21/003 (2013.01); F01D 21/04 (2013.01); F01D 25/06 (2013.01); F02C 9/00 (2013.01); F04D 27/0261 (2013.01); F04D 29/665 (2013.01); G01H 1/006 (2013.01); G01H 13/00 (2013.01); G05B 13/042 (2013.01); F05D 2240/24 (2013.01); F05D 2260/81 (2013.01); F05D 2260/96 (2013.01); F05D 2270/11 (2013.01); F05D 2270/114 (2013.01); F05D 2270/304 (2013.01); F05D 2270/312 (2013.01); F05D 2270/313 (2013.01); F05D 2270/334 (2013.01); F05D 2270/54 (2013.01); F05D 2270/71 (2013.01);
Abstract

A flutter control system for a turbine includes a processor. The processor is configured to detect blade flutter of a turbine. The blade flutter indicates that blades of the turbine are in a deflected position different from a nominal operating position. The processor is configured to control operational parameters of the turbine that reduce or eliminate the blade flutter to improve the reliability and efficiency of the turbine.


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