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:
Sep. 16, 2014

Filed:

Sep. 09, 2011
Applicants:

Philippe Giguere, Simpsonville, SC (US);

Stefan Herr, Greenville, SC (US);

Peter James Fritz, Greenville, SC (US);

Scott Gabell Riddell, Greer, SC (US);

Jeffrey Eric Bergman, Mechanicville, NY (US);

Inventors:

Philippe Giguere, Simpsonville, SC (US);

Stefan Herr, Greenville, SC (US);

Peter James Fritz, Greenville, SC (US);

Scott Gabell Riddell, Greer, SC (US);

Jeffrey Eric Bergman, Mechanicville, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F03D 1/06 (2006.01); F03D 7/02 (2006.01);
U.S. Cl.
CPC ...
F03D 7/0232 (2013.01); Y02E 10/723 (2013.01); Y02E 10/721 (2013.01); F03D 1/0633 (2013.01); F05B 2240/30 (2013.01);
Abstract

A rotor blade assembly for a wind turbine and a method for increasing a loading capability of a rotor blade within a maximum load limit for a wind turbine are disclosed. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade assembly further includes an extension connected to a surface of the rotor blade, the extension having at least one design characteristic configured for increasing a loading capability of the rotor blade within a maximum load limit for the wind turbine. The design characteristic is one of extension length, extension width, extension curvature, span-wise extension location, chord-wise extension location, or extension angle with respect to a chord line of the rotor blade.


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