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. 31, 2018

Filed:

Nov. 13, 2014
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Franklin Perley, Simpsonville, SC (US);

Brandon Shane Gerber, Charleston, SC (US);

Tim Robert Gerloff, Berlin, DE;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F03D 7/02 (2006.01); G01N 3/24 (2006.01); F03D 7/04 (2006.01); F03D 17/00 (2016.01); F03D 1/06 (2006.01);
U.S. Cl.
CPC ...
G01N 3/24 (2013.01); F03D 1/06 (2013.01); F03D 7/043 (2013.01); F03D 17/00 (2016.05); F05B 2260/821 (2013.01); F05B 2270/331 (2013.01); Y02E 10/721 (2013.01); Y02E 10/723 (2013.01);
Abstract

The present subject matter is directed to a method for estimating rotor blade loads, e.g. a blade root resultant moment, of a wind turbine. In one embodiment, the method includes measuring, via one or more sensors, a plurality of operating parameters of the wind turbine. Another step includes estimating out-of-plane and in-plane forces acting on the rotor blade based at least partially on the plurality of operating parameters. Further, the method includes determining an application point for the out-of-plane and in-plane forces along a span of the rotor blade. A further step includes estimating out-of-plane and in-plane moments of the rotor blade based at least partially on the out-of-plane and in-plane forces and the respective application points. Thus, the method includes calculating the load acting on the rotor blade based at least partially on the out-of-plane and in-plane moments.


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