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:
Apr. 19, 2016

Filed:

Sep. 10, 2013
Applicant:

Technische Universität München, München, DE;

Inventors:

Mathias Müller, München, DE;

Rolf Wojtech, München, DE;

Thorbjörn Buck, München, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01N 3/20 (2006.01); F03D 11/00 (2006.01); G01M 11/08 (2006.01); G01P 15/093 (2006.01); G01M 5/00 (2006.01); F03D 7/02 (2006.01); G01M 15/14 (2006.01); G01M 7/02 (2006.01);
U.S. Cl.
CPC ...
G01N 3/20 (2013.01); F03D 11/0091 (2013.01); G01M 11/083 (2013.01); G01P 15/093 (2013.01); F03D 7/0296 (2013.01); F05B 2260/80 (2013.01); F05B 2260/83 (2013.01); F05B 2270/332 (2013.01); F05B 2270/334 (2013.01); F05B 2270/807 (2013.01); F05B 2270/808 (2013.01); F05B 2270/821 (2013.01); G01M 5/0016 (2013.01); G01M 5/0041 (2013.01); G01M 7/025 (2013.01); G01M 15/14 (2013.01); Y02E 10/722 (2013.01);
Abstract

A method for state monitoring of a rotor blade of a wind turbine is described. The method comprises: measuring an acceleration of the rotor blade with a first signal, wherein the acceleration is measured at a first position at a predetermined distance from the rotor blade root in at least one direction comprising a first directional component orthogonal to the axis of the rotor blade, measuring a strain of the rotor blade with a second signal, wherein the strain is measured at a second position disposed in the area of the first position to the rotor blade root, determining a first positional change at the first position on the basis of the acceleration, determining a first value corresponding to the rotor blade stiffness or to the rotor blade elasticity by means of calculation on the basis of the first positional change and the strain, and determining the rotor blade state from the first value.


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