초록 ▼

A method and system for shutting down a wind turbine is presented. The method includes determining one or more pitch positions for one or more rotor blades of the wind turbine such that a sum of potential energy and kinetic energy in the wind turbine is minimized. The method further includes pitchin

A method and system for shutting down a wind turbine is presented. The method includes determining one or more pitch positions for one or more rotor blades of the wind turbine such that a sum of potential energy and kinetic energy in the wind turbine is minimized. The method further includes pitching the one or more rotor blades from an operating position to the determined pitch positions.

대표청구항 ▼

1. A method for shutting down a wind turbine having a tower, a rotor and one or more rotor blades, the method comprising: receiving a shutdown command;determining real-time values of one or more parameters associated with the wind turbine or wind;determining a sum of potential energy and kinetic ene

1. A method for shutting down a wind turbine having a tower, a rotor and one or more rotor blades, the method comprising: receiving a shutdown command;determining real-time values of one or more parameters associated with the wind turbine or wind;determining a sum of potential energy and kinetic energy in the rotor and the tower of the wind turbine;receiving the real-time values of the one or more parameters associated with the wind turbine or the wind at discrete cycle steps;computing the one or more pitch positions at the discrete cycle steps based on the real-time values of the one or more parameters until the one or more rotor blades are disposed in a feathered parking position such that the sum of potential energy and the kinetic energy in the rotor and the tower of the wind turbine are maximally reduced over a predetermined time interval; andpitching the one or more rotor blades from an operating position to the feathered parking position. 2. The method of claim 1, wherein the one or more parameters comprise one or more of current pitch angle of the one or more rotor blades, a tip speed ratio, an effective wind velocity, a current rotor speed, and a tower top velocity. 3. The method of claim 1, wherein determining the one or more pitch positions comprises determining a pitch reference trajectory over a determined time interval until the one or more rotor blades are disposed in the feathered parking position. 4. The method of claim 1, further comprising: determining one or more pitch reference trajectories based on the one or more parameters associated with the wind turbine or wind;storing the one or more pitch reference trajectories; andretrieving a pitch reference trajectory corresponding to the real-time values of the one or more parameters associated with the wind turbine or the wind based on a received shutdown command. 5. The method of claim 1, further comprising: determining a pitch reference trajectory over a determined time interval based on the real-time values of the one or more parameters associated with the wind turbine or the wind; andimplementing a pitch position value from the pitch reference trajectory to position the one or more rotor blades according to the pitch position value. 6. The method of claim 1, further comprising: determining an aerodynamic torque acting on a rotor of the wind turbine based at least on the tip speed ratio and the current pitch angle of the one or more rotor blades; anddetermining an aerodynamic thrust acting on a tower of the wind turbine based at least a on the tip speed ratio and the current pitch angle of the one or more rotor blades. 7. The method of claim 6, wherein determining the one or more pitch positions comprises computing a pitch position in a first direction if the aerodynamic torque is greater than a determined value. 8. The method of claim 6, further comprising determining a value of work performed by the aerodynamic thrust in a discrete cycle step, wherein the work performed by the aerodynamic thrust is based on the aerodynamic thrust and the tower top velocity. 9. The method of claim 8, wherein determining the one or more pitch positions comprises computing a pitch position in a second direction if the aerodynamic torque is less than a determined value and the work performed by the aerodynamic thrust is greater than the determined value. 10. The method of claim 8, wherein pitching the one or more rotor blades comprises pitching the one or more rotor blades to the determined pitch position at a first rate if the aerodynamic torque is less than a determined value and the work performed by the aerodynamic thrust is between a first threshold value and a second threshold value, and wherein the determined pitch position is in a first direction. 11. The method of claim 8, wherein pitching the one or more rotor blades comprises pitching the one or more rotor blades to the determined pitch position at a second rate if the aerodynamic torque is less than a determined value and the work performed by the aerodynamic thrust is greater than a second threshold value, and wherein the determined pitch position is in a second direction.