Method of operating a wind turbine
View Patent ↗In a first aspect, the present invention provides a method of operating a wind turbine having a rotor with a plurality of blades, a nacelle, one or more pitch systems for pitching the blades, a system for determining a speed of the rotor, and a system for determining a fore-aft speed of the nacelle. The method comprises determining the speed of the rotor, determining the fore-aft speed of the nacelle, and calculating a difference between the determined speed of the rotor and a predefined speed of reference of the rotor. After, pitch commands are obtained by performing a PID control of this calculated difference of speeds, said PID control being tuned for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle. Then, the one or more pitch systems pitch the blades in accordance with said obtained pitch commands.
1. A method of operating a wind turbine having a rotor with a plurality of blades, a nacelle, one or more pitch systems for pitching the blades, a system for determining a speed of the rotor, and a system for determining a fore-aft speed of the nacelle;
the method comprising:
determining the speed of the rotor;
determining the fore-aft speed of the nacelle;
calculating a difference between the determined speed of the rotor and a predefined speed of reference of the rotor;
obtaining pitch commands by performing a PID control of the calculated difference of speeds, wherein the PID control is tuned for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle; and
the one or more pitch systems pitching the blades in accordance with the obtained pitch commands.
2. A method according to claim 1 , wherein tuning the PID control for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle comprises obtaining a first gain as a function of the determined fore-aft speed of the nacelle, and tuning the PID control by applying the obtained first gain to the PID control.
3. A method according to claim 2 , wherein the first gain is equal to a first variable gain value, which continuously increases from a lower value to a higher value of a first predefined range of gain values as the determined fore-aft speed of the nacelle increases from a lower value to a higher value of a first predefined range of fore-aft speed values.
4. A method according to claim 3 , wherein the first gain is equal to the lower value of the first predefined range of gain values when the determined fore-aft speed of the nacelle is below the lower value of the first predefined range of fore-aft speed values; and wherein the first gain is equal to the higher value of the first predefined range of gain values when the determined fore-aft speed of the nacelle is above the higher value of the first predefined range of fore-aft speed values.
5. A method according to claim 4 , wherein applying the obtained first gain to the PID control comprises applying the obtained first gain to the PID control for adapting both the proportional constant and the integral constant of the PID control.
6. A method according to claim 4 , wherein tuning the PID control for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle further comprises obtaining a second gain as a function of the determined fore-aft speed of the nacelle, and tuning the PID control by further applying the obtained second gain to the PID control.
7. A method according to claim 3 , wherein applying the obtained first gain to the PID control comprises applying the obtained first gain to the PID control for adapting both a proportional constant and an integral constant of the PID control.
8. A method according to claim 3 , wherein tuning the PID control for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle further comprises obtaining a second gain as a function of the determined fore-aft speed of the nacelle, and tuning the PID control by further applying the obtained second gain to the PID control.
9. A method according to claim 2 , wherein applying the obtained first gain to the PID control comprises applying the obtained first gain to the PID control for adapting both a proportional constant and an integral constant of the PID control.
10. A method according to claim 2 , wherein tuning the PID control for adapting the sensitivity of the PID control as a function of the determined fore-aft speed of the nacelle further comprises obtaining a second gain as a function of the determined fore-aft speed of the nacelle, and tuning the PID control by further applying the obtained second gain to the PID control.
11. A method according to claim 10 , wherein the second gain is equal to a second variable gain value which continuously decreases from a higher value to a lower value of a second predefined range of gain values as the determined fore-aft speed of the nacelle increases from a lower value to a higher value of a second predefined range of fore-aft speed values.
12. A method according to claim 11 , wherein the second gain is equal to the higher value of the second predefined range of gain values when the determined fore-aft speed of the nacelle is below the lower value of the second predefined range of fore-aft speed values; and wherein the second gain is equal to the lower value of the second predefined range of gain values when the determined fore-aft speed of the nacelle is above the higher value of the second predefined range of fore-aft speed values.
13. A method according to claim 11 , wherein applying the obtained first gain to the PID control comprises applying the obtained first gain to the PID control for adapting a proportional constant of the PID control; and wherein applying the obtained second gain to the PID control comprises applying the obtained second gain to the PID control for adapting an integral constant of the PID control.
14. A method according to claim 10 , wherein applying the obtained first gain to the PID control comprises applying the obtained first gain to the PID control for adapting a proportional constant of the PID control; and wherein applying the obtained second gain to the PID control comprises applying the obtained second gain to the PID control for adapting an integral constant of the PID control.
15. A method according to claim 1 , wherein the one or more pitch systems are adapted to follow pitch commands under a maximum pitch rate; and wherein the method further comprises adapting the maximum pitch rate as a function of the determined fore-aft speed of the nacelle.
16. A method according to claim 1 , wherein the wind turbine further comprises a system for determining blade pitch angles; wherein the method further comprises determining the blade pitch angles; and wherein the PID control is further tuned in accordance with the determined blade pitch angles.
17. A method according to claim 1 , further comprising applying to the calculated difference of speeds at least one filter for removing, from the calculated difference of speeds, frequencies different from those theoretically caused by a sudden wind push.
18. A method according to claim 1 , further comprising applying to the determined fore-aft speed of the nacelle at least one filter for removing, from the determined fore-aft speed of the nacelle, frequencies different from those theoretically caused by a sudden wind push.
19. A method according to claim 1 , wherein the system for determining the fore-aft speed of the nacelle comprises at least one accelerometer and/or at least one inclinometer.
20. A wind turbine configured to perform the method according to claim 1 .