Method for monitoring a wind turbine, method for identifying ice on a wind turbine, acceleration sensor for a rotor blade, rotor blade comprising an acceleration sensor, and profile for a rotor blade

1. A method for monitoring a wind turbine, comprising:

measuring acceleration by means of a fiber-optic acceleration sensor in a rotor blade of the wind turbine, wherein a signal of the fiber-optic acceleration sensor is guided to a hub of the wind turbine via a light conductor;

opto-electronically converting an acceleration signal of the fiber-optic acceleration sensor; and

filtering the opto-electronically converted acceleration signal by means of an analog anti-aliasing filter having a cutoff frequency from 10 Hz to 40 Hz,

wherein the fiber optic acceleration sensor is provided at a radial position in the range of the outer 70% of the rotor blade radius.

2. The method according to claim 1 , wherein the light conductor is guided, in the region of the blade root, via a spiral permitting torsion of the light conductor.

3. The method according to claim 2 , wherein a distributor provides a plug connection to the light conductor.

4. The method according to claim 1 , wherein the light conductor is provided at the rear edge of the rotor blade.

5. The method according to claim 1 , wherein the light conductor is provided on a profile provided at the rear edge of the rotor blade.

6. The method according to claim 5 , wherein the profile extends along at least 30% of the rotor blade radius.

7. The method according to claim 5 , wherein the fiber-optic acceleration sensor is provided within the profile.

8. The method according to claim 1 , wherein the light conductor is guided into the rotor blade interior from outside at a radial position where the rotor blade can be walked in.

9. The method according to claim 1 , furthermore comprising:

evaluating the acceleration signal by means of Stochastic Subspace Identification for calculating Eigenvalues of the rotor blade.

10. The method according to claim 9 , furthermore comprising:

detecting ice formation on the rotor blade by means of the Eigenvalues.

11. The method according to claim 1 , furthermore comprising:

measuring a sound pressure level on the rotor blade.

12. The method according to claim 1 , wherein the measuring of the acceleration is performed in a wind turbine that is at standstill or turning at no load.

13. A method for identifying ice on a wind turbine, comprising:

measuring acceleration by means of a fiber-optic acceleration sensor in a rotor blade of the wind turbine, wherein a signal of the fiber-optic acceleration sensor is guided to a hub of the wind turbine via a light conductor;

opto-electronically converting an acceleration signal of the fiber-optic acceleration sensor;

filtering the opto-electronically converted acceleration signal by means of an analog anti-aliasing filter having a cutoff frequency from 10 Hz to 40 Hz;

evaluating the filtered acceleration signal by means of Stochastic Subspace Identification for calculating Eigenvalues of the rotor blade; and

detecting ice formation on the rotor blade by means of the Eigenvalues,

wherein the fiber optic acceleration sensor is provided at a radial position in the range of the outer 70% of the rotor blade radius.

14. The method according to claim 13 , furthermore comprising:

compensating the Eigenvalues by means of at least one measured parameter from the group consisting of: a temperature on the rotor blade of the wind turbine, a wind velocity, an output of the wind turbine, a rotational rate of a rotor of the wind turbine, and a pitch angle of the rotor blade.

15. A rotor of a wind turbine, comprising:

a fiber-optic acceleration sensor in a rotor blade of the wind turbine;

a light conductor for guiding a signal of the fiber-optic acceleration sensor to a hub of the wind turbine;

an opto-electronic converter for converting an acceleration signal of the fiber-optic acceleration sensor; and

an analog anti-aliasing filter configured to filter the opto-electronically converted acceleration signal and having a cutoff frequency from 10 Hz to 40 Hz,

wherein the fiber optic acceleration sensor is provided at a radial position in the range of the outer 70% of the rotor blade radius.

16. The rotor according to claim 15 , wherein the fiber-optic acceleration sensor is provided at a radial position in the range of the outer 70% of the rotor blade radius, and wherein the light conductor is guided from the fiber-optic acceleration sensor up to a radial rotor blade position where the rotor blade can be walked in.

17. The rotor according to claim 15 , wherein the fiber-optic acceleration sensor has a maximum extension of 10 mm in a cross-section perpendicular to the axis of the light conductor.