Method for monitoring a static and/or dynamic stability of a wind turbine
The invention relates to a method for monitoring a static and/or dynamic stability of a wind turbine. The wind turbine has a tower, a nacelle, which is supported by the tower, and a rotor, which is mounted in or on the nacelle and has at least one rotor blade which can be adjusted about its longitudinal axis. The method includes the following steps: the wind turbine is excited to oscillate in at least one direction. A frequency (f m ) of the excited oscillation is detected. The detected frequency is compared with a predetermined frequency (f ref ) and an alarm signal is generated if the detected frequency deviates from the predetermined frequency by more than a difference value (Δf).
1. A method for monitoring a static and/or dynamic stability of a wind turbine having a tower, a nacelle which is supported by the tower, and a rotor which is mounted in or on the nacelle and has at least one rotor blade defining a plane as the rotor blade rotates over an area and said rotor blade being adjustable about its longitudinal axis, the method comprising the steps of:
exciting the wind turbine to oscillate with said tower thereof in a z-direction at right angles to said plane by adjusting a blade pitch angle of said at least one rotor blade to its feathered position;
detecting a frequency (f m ) of the excited oscillation of said wind turbine including said tower;
comparing the detected frequency with a predetermined frequency (f ref ); and,
generating an alarm signal when the detected frequency deviates from the predetermined frequency by more than a difference value (Δf).
2. The method of claim 1 , wherein the blade pitch angle is adjusted by at least a predetermined angle.
3. The method of claim 1 , wherein the at least one rotor blade is adjusted at a predetermined blade pitch adjustment rate, which is selected to be sufficiently high that the tower is excited to oscillate.
4. The method of claim 1 , wherein the frequency of the excited oscillation is detected by evaluating a sensor signal from an acceleration sensor arranged in the nacelle.
5. The method of claim 1 , wherein the detected frequency is low-pass filtered.
6. The method of claim 1 , wherein a first tower natural frequency is provided as the predetermined frequency.
7. The method of claim 1 , wherein the alarm signal is generated if the detected frequency is greater than the predetermined frequency by more than a first difference value or is less than the predetermined frequency by more than a second difference value.
8. The method of claim 1 , wherein the alarm signal is generated when the detected frequency drops below a predetermined excitation frequency by more than a minimum amount.
9. The method of claim 1 , wherein an amplitude of the excited oscillation is detected and the alarm signal is generated only if the amplitude exceeds a predetermined minimum value.