Methods for controlling wind turbine with thrust control twist compensation
A method is provided for operation of a wind turbine having rotor blades attached to a hub, wherein a controller compensates for torsionally induced blade twist. The method includes operating the wind turbine according to a rated power output curve and maximum design thrust value, and periodically or continuously detecting for induced torsional twist in the rotor blades. Upon determination of torsional twist being induced in the rotor blades, the method includes adjusting the maximum thrust value in the control program to compensate for the induced twist. The wind turbine controller then controls pitch of the rotor blades as a function of the increased maximum thrust value so that power output of the wind turbine is not unnecessarily limited or increased by the induced twist on the rotor blades.
1. A method for operation of a wind turbine having rotor blades attached to a hub, wherein a controller compensates for torsionally induced blade twist, the method comprising:
operating the wind turbine according to a rated power output curve and programmed maximum thrust value;
periodically or continuously detecting for induced torsional twist in the rotor blades;
upon determination of torsional twist being induced in the rotor blades, adjusting the programmed maximum thrust value to compensate for the torsional twist; and
the controller controlling pitch of the rotor blades as a function of the adjusted programmed maximum thrust value so that power output of the wind turbine is not limited or increased by the induced twist on the rotor blades.
2. The method as in claim 1 , wherein the programmed maximum thrust value is adjusted proportionally with the amount of torsional twist induced in the rotor blades.
3. The method as in claim 1 , wherein the programmed maximum thrust value is adjusted by a predefined amount upon the determination of torsional twist in the rotor blades up to cutout wind speed of the rated power output curve.
4. The method as in claim 1 , wherein the induced torsional twist is directly detected by sensing a change in a physical aspect of the rotor blades resulting from the induced torsional twist.
5. The method as in claim 4 , wherein the induced torsional twist is directly detected by a sensor mounted on the rotor blade.
6. The method as in claim 4 , wherein the induced torsional twist is directly optically detected by a camera disposed to view a span-wise aspect of the rotor blade.
7. The method as in claim 4 , wherein the induced torsional twist is directly detected by a laser disposed to detect rotor blade distortion.
8. The method as in claim 1 , wherein the induced torsional twist is indirectly detected.
9. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by an actual measured blade load being less than or greater than an expected value at a given wind speed.
10. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by a measured rotor thrust being less than or greater than an expected value at a defined wind speed.
11. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by a measured tower bending being less than an expected value at a defined wind speed.
12. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by a measured noise at a defined wind speed being different than an expected value.
13. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by a difference at a defined wind speed on the power output curve between a measured blade pitch angle and an expected blade pitch angle.
14. The method as in claim 8 , wherein the induced torsional twist is indirectly detected by a difference between a Model Based Controller (MBC) estimated wind speed and an actual measured wind speed.