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. 07, 2023

Filed:

Apr. 30, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Franklin Perley, Livonia, MI (US);

Jingting Xiao, Dallas, TX (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F03D 7/02 (2006.01); F03D 9/25 (2016.01); F03D 15/00 (2016.01); F03D 17/00 (2016.01); F03D 7/04 (2006.01); G01M 1/14 (2006.01);
U.S. Cl.
CPC ...
F03D 7/0264 (2013.01); F03D 7/0244 (2013.01); F03D 7/0288 (2013.01); F03D 7/042 (2013.01); F03D 7/047 (2013.01); F03D 9/25 (2016.05); F03D 15/00 (2016.05); F03D 17/00 (2016.05); G01M 1/14 (2013.01); F03D 7/0224 (2013.01); F05B 2260/901 (2013.01); F05B 2260/903 (2013.01); F05B 2260/904 (2013.01); F05B 2270/107 (2013.01);
Abstract

A system and method are provided for controlling a wind turbine in response to a blade liberation event. Accordingly, estimated response signatures for the wind turbine are determined. Sensor data indicative of at least two actual response signatures of components of the wind turbine to a rotor loading are collected. The actual response signatures are compared to the estimated response signatures. The two or more actual response signatures meeting or exceeding the estimated response signatures is indicative of a blade liberation event. In response to detecting the blade liberation event, a rapid shutdown control logic is initiated to decelerate the rotor at a rate which exceeds a nominal deceleration rate of the rotor.


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