Device and method for operating a wind turbine
The controller estimates overspeed conditions in wind turbines to perform smooth pitch adjustments, reducing loads and vibrations, thereby extending operational life and enhancing power generation.
Patent Information
- Application Number
- DE102011052666
- Authority / Receiving Office
- DE · DE
- Patent Type
- Patents
- Current Assignee / Owner
- Priority Date
- 2010-08-16
- Filing Date
- 2011-08-12
- Publication Date
- 2025-10-02
- Estimated Expiration
- 2031-08-12
AI Technical Summary
Existing wind turbine control systems face issues with high loads and resonant vibrations during overspeed conditions, leading to potential shutdowns and reduced operational life, as they rely on abrupt pitch adjustments that increase loads and excite tower resonances.
A controller estimates overspeed conditions using multiple wind turbine variables, allowing for smooth pitch adjustments to aerodynamically brake the rotor, reducing transient loads and preventing resonant vibrations.
This approach extends the operational life of the wind turbine by minimizing high loads and avoiding shutdowns, while increasing power generation capacity.
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Abstract
Description
BACKGROUND TO THE INVENTION
[0001] The subject matter described herein relates generally to methods and systems for operating a wind turbine, and more particularly to methods and systems for operating a control device for a wind turbine.
[0002] At least some known wind turbines include a tower and a nacelle mounted on the tower. A rotor is rotatably mounted on the nacelle and is coupled to an electric generator via a shaft. In typical wind turbines, several blades extend from the rotor. The blades are oriented in such a way that wind passing over the blades spins the rotor and causes the shaft to rotate, driving the generator to produce electricity.
[0003] At least some known wind turbines are operated by a control system. Furthermore, at least some known control systems for wind turbines perform pitch control (pitch control) by rotating the rotor blades about a pitch axis. This means that these control systems are designed to regulate the rotor speed of the wind turbine by adjusting the angles of the blades, i.e., pitch adjustment or pitch adjustment of the blades, with respect to the airflow. Adjusting the pitch of the blades to reduce the rotor speed generally results in an increase in the load acting on some of the components of the wind turbine, such as the blades, the rotor, or the wind tower.
[0004] In general, an increase in the speed of the wind hitting the rotor blades causes an increase in the rotor speed. Under certain conditions, such as strong winds in the vicinity of the wind turbine, the rotor speed may exceed a threshold value corresponding to the maximum permissible speed of the wind turbine (i.e., an overspeed). US 2009 / 0278352 A1 relates to a variable-speed wind turbine with an exciter and current transformer that are not connected to the grid. JP 2005 / 042603 A relates to a torque control circuit for controlling overspeed in wind turbines using a PWM converter. DE 10 2008 012 957 A1 relates to a method for operating a wind turbine.
[0005] At least some known control systems that implement pitch control are designed to monitor the rotor speed by determining its actual values and to aerodynamically reduce the rotor speed (i.e., brake the rotor) by increasing the pitch of the blades whenever an actual value of the rotor speed exceeds the maximum allowable speed of the wind turbine. In this situation, reducing the rotor speed by pitching the blades can lead to a particularly significant increase in the load acting on wind turbine components. In general, such a significant increase in load adversely affects the operating life of the wind turbine. In at least some known blade pitch control systems, the blade pitch control forces the rotor speed below the maximum allowable speed of the wind turbine.At least some of these blade pitch control systems are designed to reduce the angle of attack once the rotor speed is below the maximum allowable speed of the wind turbine in order to maintain a high rotor speed, but within the safety limit of the wind turbine (i.e. below the maximum allowable speed of the wind turbine).
[0006] In such overspeed events, which are managed by known control systems, the increase and subsequent decrease in the angle of attack generally results in alternating forces acting on the tower. In some cases, these alternating forces can excite the tower's resonant modes and lead to a resonant vibration of the tower. Such a resonant vibration of the tower may require a shutdown of the wind turbine if the vibration exceeds a maximum allowable limit. A shutdown event results in a loss of the wind turbine's power generation capacity.
[0007] Accordingly, it is desirable to provide a method and / or apparatus capable of performing pitch control that avoids high stresses on the wind turbine components and / or reduces the risk of wind turbine shutdown due to an overspeed condition of the wind turbine. BRIEF DESCRIPTION OF THE INVENTION
[0008] The object of the disclosure is to provide a method for operating a wind turbine that is improved over the prior art. Furthermore, the object of the disclosure is to provide an improved control device for use in a wind turbine. This object is achieved by a method according to claim 1 and a control device according to claim 8.
[0009] The embodiments described herein include a controller that estimates the occurrence of an overspeed condition of the wind turbine based on actual values of several variables of the wind turbine and adjusts the pitch of at least one of the rotor blades based on the result of the estimate. By estimating the occurrence of an overspeed condition, the embodiments described herein enable smooth pitch adjustment (tilt) of a rotor blade. As a result, the pitch adjustment causes smooth braking of the rotor. Accordingly, transient loads acting on the wind turbine components are typically reduced, and the operating life of the wind turbine is typically extended. Furthermore, such smooth pitch adjustment typically reduces the risk of resonant vibration of the wind turbine and shutdown of the wind turbine.In particular, according to at least one embodiment, a rotor blade is adjusted in the angle of attack in such a way that a first variable of the wind turbine, for example the rotor speed, does not exceed a threshold value that indicates an overspeed condition of the wind turbine.
[0010] In one aspect, a method for operating a wind turbine is provided. The wind turbine includes a rotor having at least one rotor blade, and a pitch drive system coupled to the at least one rotor blade. The pitch drive system is configured to adjust the pitch of the at least one rotor blade. The method includes: determining an actual value of a first variable indicative of an overspeed condition of the wind turbine; determining an actual value of a second variable of the wind turbine correlated with the rate of change of the first variable over time; and estimating an occurrence of an overspeed condition of the wind turbine based on at least the determined actual values of the first and second variables.The estimation includes identifying a future rotor speed based on the determined actual values of the first and second variables. The pitch drive system tilts the at least one rotor blade to aerodynamically brake the rotor based on the result of the estimation. In some embodiments according to the present disclosure, the first variable indicates an overspeed condition of the wind turbine when it exceeds a threshold.
[0011] In another aspect, a control device for use in a wind turbine is provided. The wind turbine includes a rotor having at least one rotor blade. The control device includes a pitch control drive system coupled to the at least one rotor blade, wherein the pitch control drive system is configured to adjust the pitch of the at least one rotor blade. The wind turbine further includes a control system communicatively connected to the pitch control drive system.The control system is configured to: determine an actual value of a first variable indicative of an overspeed condition of the wind turbine; determine an actual value of a second variable of the wind turbine correlated with the time rate of change of the first variable; and estimate an occurrence of an overspeed condition of the wind turbine based on at least the determined actual values of the first and second variables. Estimating includes identifying a future rotor speed based on the determined actual values of the first and second variables. The control system is configured to control the pitch drive system in such a manner that, based on the result of the estimation, the pitch drive system adjusts the at least one rotor blade in terms of angle of attack for aerodynamic braking of the rotor.
[0012] Furthermore, a method for operating a wind turbine is described. The wind turbine includes a rotor having at least one rotor blade, and a pitch control drive system coupled to the at least one rotor blade, wherein the pitch control drive system is configured to adjust the pitch of the at least one rotor blade. The method includes: determining an actual value of a reference speed that is directly proportional to the speed of the rotor; determining an actual value of a rate of change of the reference speed over time; and evaluating the determined actual values of the reference speed and the rate of change of the reference speed over time to identify an overspeed condition of the wind turbine. The pitch control drive system rotates the at least one rotor blade if an overspeed condition of the wind turbine is identified during the evaluation.
[0013] Further aspects, advantages and features of the present invention are apparent from the dependent claims, the description and the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS
[0014] A comprehensive and practical disclosure, including the best mode thereof, for one skilled in the art is provided in greater detail in the remainder of the specification, which includes reference to the accompanying figures, in which: Fig. 1 shows a perspective view of an exemplary wind turbine. Fig. Figure 2 shows an enlarged sectional view of a portion of the Fig. 1 illustrated wind turbine. Fig. 3 shows a block diagram of an exemplary control device of the wind turbine according to Fig. 1; Fig. 4 shows a block diagram of an exemplary control system of a control device of the wind turbine according to Fig. 1; Fig. 5 shows a flowchart illustrating an exemplary method for operating the wind turbine according to Fig. 1 illustrates; Fig. 6 shows a flowchart illustrating another exemplary method for operating the wind turbine according to Fig. 1 illustrates; and Fig. Figure 7 shows a schematic graphical representation of the response to an identified overspeed condition of the wind turbine after Fig. 1 compared to the response of at least some known wind turbines. DETAILED DESCRIPTION OF THE INVENTION
[0015] Reference will now be made in detail to the various embodiments, one or more examples of which are illustrated in each figure. Each example is provided for purposes of illustration and is not intended to be limiting. For example, features illustrated or described as part of one embodiment may be used in or in conjunction with other embodiments to yield still further embodiments. The present disclosure is intended to encompass such modifications and variations.
[0016] According to embodiments described herein, a wind turbine operates a pitch drive system to rotate a rotor blade based on the result of estimating an occurrence of an overspeed condition of the wind turbine. The estimation is based on determined actual values of a plurality of wind turbine variables. At least one of these variables, referred to as the first variable, indicates an overspeed condition of the wind turbine. For example, the first variable may be the rotor speed, which indicates an overspeed condition of the wind turbine when it exceeds the maximum allowable speed of the wind turbine (i.e., an overspeed).Alternatively, the first variable may be an output power of the wind turbine, the deflection of one or more rotor blades, the wind speed in the vicinity of the wind turbine, or any other variable that indicates an overspeed condition of the wind turbine when it exceeds a threshold. Typically, the first variable of the wind turbine is a variable that is monotonically correlated with the rotor speed. At least one other of these variables, referred to as the second variable, is correlated with the rate of change of the first variable over time. In the above example, the second variable may be the rotor acceleration. Typically, the second variable is monotonically correlated with the rotor rotational acceleration. According to at least some embodiments, the estimation may be based on other variables of the wind turbine.In the above example, the second time derivative, the third time derivative or even further time derivatives of the first variable (e.g. the rotor speed) can be used for the estimation.
[0017] According to some embodiments, the pitch drive system rotates the rotor blade to aerodynamically brake the rotor if the result of the estimation is the occurrence of an overspeed condition within a predetermined time period. For example, the estimation may consist of calculating the value of the rotor speed within a predetermined time period (i.e., a future rotor speed) based on the determined actual values of the first and second variables and comparing the identified future rotor speed with a predetermined rotor speed value, which typically corresponds to the maximum permissible speed of the wind turbine.In this example, if the identified future rotor speed exceeds the predetermined rotor speed, the result of the estimation represents the occurrence of an overspeed condition within that time period, and consequently the pitch drive system will adjust the pitch of the rotor blade(s) to aerodynamically brake the rotor.
[0018] The embodiments described herein provide a wind turbine that enables a pitch control assembly to smoothly twist a rotor blade about a pitch axis (i.e., to smoothly tilt or pitch a rotor blade). In particular, the embodiments described herein enable pitch control to be performed before the wind turbine enters an overspeed condition. Furthermore, according to some embodiments, pitch control is performed in such a manner that an anticipated overspeed condition does not occur.
[0019] Consequently, the embodiments described herein typically enable a reduction in aerodynamic loading in the components of the wind turbine, which typically extends the operating life of the wind turbine. Furthermore, a wind turbine according to embodiments described herein typically enables the avoidance of a shutdown due to an overspeed condition. As a result, the embodiments described herein typically enable an increase in the power generation capacity of a wind turbine. As used herein, the term "overspeed condition" refers to a condition of the wind turbine in which the rotor of the wind turbine is rotating at a rotational speed at which possible damage to the rotor, including damage to the rotor blade or another component of the wind turbine, such as an electrical generator coupled to the rotor, may occur.
[0020] As used herein, the term "wind turbine variable" is intended to denote a quantity related to the wind turbine that varies over time. Some examples of wind turbine variables are rotor speed (i.e., the rotational speed of the rotor), rotor acceleration, such as the rotational or axial acceleration of the rotor, rotor blade deflection, or a wind turbine output, such as an output of an electrical generator that forms part of the wind turbine.
[0021] As used herein, the term actual value of a wind turbine variable is intended to indicate a value of the variable actually assumed by the wind turbine. For example, an actual value of rotor speed could be determined from a direct measurement of the rotor speed by a sensor. Alternatively, an actual value of rotor speed could be determined from an estimate of a wind turbine variable based on a measured value of another variable, such as, but not limited to, a rotational speed of the rotor shaft or a rotational speed of a rapidly rotating shaft connected to the rotor shaft by a gearing system. For example, an actual value of rotor acceleration may correspond to a direct measurement of the acceleration by a sensor coupled to the rotor.Alternatively, an actual value of the rotor acceleration may correspond to the rate of change of the actual values of the rotor speed over time, which can be derived from a time sequence of rotor speed values. Such wind turbine variables may be determined by any suitable method that enables operation of the wind turbine in the manner described herein.
[0022] As used herein, the term "blade" is intended to identify any device that provides a reaction force when in motion relative to a surrounding fluid. As used herein, the term "wind turbine" is intended to identify any device that generates rotational energy from wind energy, and in particular, converts wind kinetic energy into mechanical energy. As used herein, the term "wind generator" is intended to identify any wind turbine that generates electrical power from rotational energy generated by wind energy, and in particular, converts mechanical energy converted from wind kinetic energy into electrical power.
[0023] In the following description of the drawings, the same reference numerals refer to the same components. Generally, only the differences between the individual embodiments are described.
[0024] Fig. 1 shows a perspective view of an exemplary wind turbine 10. In the exemplary embodiment, the wind turbine 10 is a horizontal-axis wind turbine. Alternatively, the wind turbine 10 may be a vertical-axis wind turbine. In the exemplary embodiment, the wind turbine 10 includes a tower 12 extending from a support system 14, a nacelle 16 mounted on the tower 12, and a rotor 18 coupled to the nacelle 16. The rotor 18 includes a rotatable hub 20 and at least one rotor blade 22 coupled to and extending outwardly from the hub 20. In the exemplary embodiment, the rotor 18 has three rotor blades 22. In an alternative embodiment, the rotor 18 includes more or fewer than three rotor blades 22. In the exemplary embodiment, the tower 12 is constructed from steel tubing to form a (in Fig. 1) between the support system 14 and the nacelle 16. In an alternative embodiment, the tower 12 is a tower of any suitable design and of any suitable height.
[0025] The rotor blades 22 are spaced apart around the hub 20 to assist rotation of the rotor 18 to enable conversion of the kinetic energy from the wind into usable mechanical energy and subsequently into electrical energy. The rotor blades 22 are matingly connected to the hub 20 by coupling a blade root portion 24 to the hub 20 at a plurality of load transfer regions 26. The load transfer regions 26 include a hub load transfer region and a blade load transfer region (both of which are shown in Fig. 1 are not illustrated). Forces introduced into the rotor blades 22 are transferred to the hub 20 via the load transfer areas 26.
[0026] In one embodiment, the rotor blades 22 have a length ranging from about 15 meters (m) to about 91 m. Alternatively, the rotor blades 22 may have any suitable length that enables the wind turbine 10 to function as described herein. For example, further non-limiting examples of blade lengths include 10 m or less, 20 m, 37 m, or a length greater than 91 m. When wind passes the rotor blades 22 from a direction 28, the rotor 18 is rotated about a rotational axis 30. Further, when rotor blades 22 are rotated and subjected to centrifugal forces, the rotor blades 22 are subjected to various forces and moments. As such, the rotor blades 22 may deflect and / or twist from a neutral or undeflected position to a deflected position.
[0027] In addition, an angle of attack or pitch of the rotor blades 22, ie, an angle that determines a perspective of the rotor blades 22 with respect to the direction 28 of the wind, can be changed by a pitch adjustment system 32 in order to control the load and power generated by the wind turbine 10 by adjusting a rotational position of at least one rotor blade 22 with respect to wind vectors. In alternative embodiments, only the angle of attack of a portion of the rotor blades 22 is changed by the pitch adjustment system 32. Pitch axes 34 for the rotor blades 22 are shown in Fig. 1. During operation of the wind turbine 10, the pitch adjustment system 32 can change a blade pitch (blade pitch) of the rotor blades 22 such that the rotor blades 22 are feathered in a manner such that the perspective of at least one rotor blade 22 with respect to wind vectors results in a minimum surface area of the rotor blade 22 oriented toward the wind vectors, enabling a reduction in a rotational speed of the rotor 18 and / or enabling a stopping of the rotor 18.
[0028] In the exemplary embodiment, a blade pitch of each rotor blade 22 is controlled individually by a control system 36. Alternatively, the blade pitch for all rotor blades 22 may be controlled simultaneously by the control system 36. Further, in the exemplary embodiment, as the direction 28 changes, a yaw direction of the nacelle 16 may be controlled around a yaw axis 38 to position the rotor blades 22 with respect to the direction 28.
[0029] In the exemplary embodiment, the control system 36 is illustrated as being centralized in the nacelle 16, however, the control system 36 may be a distributed system throughout the wind turbine 10, on the support system 14, within a wind farm, and / or at a remote control center. The control system 36 includes a processor 40 configured to perform the methods and / or steps described herein. Furthermore, many of the other components described herein include a processor. As used herein, the term "processor" is not limited to integrated circuits, which are known in the art as a computer orThe term "computer" is not intended to be used as a "computer," but rather broadly refers to a controller, a microcontroller, a microcomputer, a programmable logic controller (PLC), an application-specific integrated circuit, and other programmable circuits, and these terms are used interchangeably herein. It should be understood that a processor and / or control system may also include memory, input channels, and / or output channels.
[0030] In the embodiments described herein, memory may include, without limitation, a computer-readable medium such as random access memory (RAM) and a computer-readable non-transitory medium such as flash memory. Alternatively, a floppy disk, a CD-ROM (Compact Disk Read-Only Memory), a magnetic-optical disk (MOD), and / or a digital versatile disk (DVD) may be used. Further, in the embodiments described herein, input channels include, without limitation, sensors and / or computer peripherals associated with a user interface, such as a mouse and a keyboard. Further, in the exemplary embodiment, output channels may include, without limitation, a controller, a user interface monitor, and / or a display.
[0031] Processors described herein process information transmitted from a plurality of electrical and electronic devices, which may include, without limitation, sensors, actuators, compressors, control systems, and / or monitoring devices. Such processors may be physically located, for example, in a control system, a sensor, a monitoring device, a desktop computer, a laptop computer, a programmable logic controller (PLC) cabinet, and / or a distributed control system (DCS) cabinet. The RAM and storage devices store and transmit information and instructions to be executed by the processor(s). The RAM and storage devices may further be used to store temporary variables, static (i.e.,To store and deliver non-changing information and instructions or other intermediate information to the processors. Instructions being executed may include, without limitation, control commands of the wind turbine control system. The execution of the sequences of instructions is not limited to any specific combination of hardware circuitry and software instructions.
[0032] Fig. 2 shows an enlarged sectional view of a portion of the wind turbine 10. In the exemplary embodiment, the wind turbine 10 includes the nacelle 16 and the hub 20 rotatably coupled to the nacelle 16. In particular, the hub 20 is rotatably coupled to an electric generator 42 positioned within the nacelle 16 via a rotor shaft 44 (sometimes referred to as either a main shaft or a low-speed shaft), a gearbox 46, a high-speed shaft 48, and a coupling 50. In the exemplary embodiment, the rotor shaft 44 is arranged coaxially with the longitudinal axis 116. Rotation of the rotor shaft 44 rotatably drives the gearbox 46, which subsequently drives the high-speed shaft 48. The rapidly rotating shaft 48 rotatably drives the generator 42 with the clutch 50, and rotation of the rapidly rotating shaft 48 enables the generator 42 to generate electrical power.The gearbox 46 and the generator 42 are supported by a carrier 52 and a support 54. In the exemplary embodiment, the gearbox 46 uses a dual-path geometry to drive the high-speed shaft 48. Alternatively, the rotor shaft 44 is directly coupled to the generator 42 by the coupling 50.
[0033] In the exemplary embodiment, the nacelle 16 further includes a yaw drive mechanism 56 that can be used to position the nacelle 16 and the hub 20 above the (in Fig. 1) to control the perspective of the rotor blades 22 with respect to the direction 28 of the wind. The nacelle 16 further includes at least one wind measurement mast 58 containing a wind vane and an anemometer (neither of which are shown in Fig. 2). Mast 58 provides information to control system 36, which may include wind direction and / or wind speed. In the exemplary embodiment, nacelle 16 further includes a forward main support bearing 60 and an aft main support bearing 62.
[0034] The front support bearing 60 and the rear support bearing 62 provide radial support and alignment of the rotor shaft 44. The front support bearing 60 is coupled to the rotor shaft 44 near the hub 20. The rear support bearing 62 is positioned on the rotor shaft 44 near the gearbox 46 and / or the generator 42. Alternatively, the nacelle 16 includes any number of support bearings that enable the wind turbine 10 to function in the manner disclosed herein. The rotor shaft 44, the generator 42, the gearbox 46, the high-speed shaft 48, the coupling 50, and any associated fastening, retaining, and / or securing device, including, but not limited to, the carrier 52 and / or the carrier 54, the front support bearing 60, and the rear support bearing 62, are sometimes referred to as a drivetrain 64.
[0035] In the exemplary embodiment, the hub 20 includes a blade pitch assembly 66. The blade pitch assembly 66 includes one or more blade pitch drive systems 68. In the exemplary embodiment, the nacelle 16 includes a sensor system that may include at least one sensor, such as a speed sensor 70, for sensing at least one variable of the wind turbine 10, such as a speed or acceleration of at least one rotor blade 22. Typically, as explained in more detail below, the at least one sensor in the sensor system is communicatively coupled to the control system 36. Typically, each blade pitch drive system 68 is connected to a respective (in Fig. 1) rotor blade 44 for influencing the blade pitch angle of the associated rotor blade 22 is coupled to the blade pitch adjustment axis 34. In Fig. 2 only one of the three blade pitch drive systems 68 is illustrated.
[0036] In the exemplary embodiment, the pitch assembly 66 includes at least one pitch bearing 72 that is connected to the hub 20 and to the respective (in Fig. 1) to rotate the associated rotor blade 22 about the pitch axis 34. The pitch drive system 68 includes a pitch drive motor 74, a pitch drive gear 76, and a pitch drive pinion 78. The pitch drive motor 74 is coupled to the pitch drive gear 76 in such a manner that the pitch drive motor 74 transmits a mechanical force to the pitch drive gear 76. The pitch drive gear 76 is coupled to the pitch drive pinion 78 in such a manner that the pitch drive pinion 78 is rotated by the pitch drive gear 76. The pitch bearing 72 is coupled to the pitch drive pinion 78 in such a manner that rotation of the pitch drive pinion 78 causes rotation of the pitch bearing 72.In particular, in the exemplary embodiment, the pitch drive pinion 78 is coupled to the pitch bearing 72 such that rotation of the pitch drive gear 76 rotates the pitch bearing 72 and the rotor blade 22 about the pitch axis 34 to change the pitch of the blade 22.
[0037] In the exemplary embodiment, the pitch drive system 68 is coupled to the control system 36 for adjusting the pitch of the rotor blade 22 upon receipt of one or more signals from the control system 36. The pitch drive motor 74 is any suitable motor driven by electric power and / or a hydraulic system that enables the pitch drive assembly 66 to function in the manner described herein. Alternatively, the pitch drive assembly 66 may include any suitable structure, configuration, device, and / or any suitable components, such as, but not limited to, hydraulic cylinders, springs, and / or servomechanisms.Additionally, the pitch assembly 66 may be driven by any suitable means, such as, but not limited to, hydraulic fluid and / or mechanical power, such as, but not limited to, induced spring forces and / or electromagnetic forces. In some embodiments, the pitch drive motor 74 is driven by energy extracted from the inertia of the hub 20 and / or a stored energy source (not illustrated) that supplies power to components of the wind turbine 10.
[0038] Fig. 3 shows a block diagram of an exemplary controller 92. In the exemplary embodiment, the controller 92 includes a pitch drive system 68, a control system 36, and a sensor system 94. The controller 92 may include any other suitable device that enables the controller 92 to function in the manner described herein. According to some embodiments, the pitch drive system 68 is coupled to at least one rotor blade 22 for rotating the rotor blade about a pitch axis 34. In the exemplary embodiment, the pitch drive system 68 corresponds to a pitch drive system as described above.The blade pitch drive system 68 is communicatively connected to the control system 36 such that the blade pitch drive system 68 is capable of adjusting the blade pitch of the rotor blade 22 upon receiving one or more signals from the control system 36.
[0039] According to some embodiments, the control system 36 is communicatively coupled to the pitch drive system 68 and configured to estimate the occurrence of an overspeed condition based on at least the determined actual values of a first and a second variable of the wind turbine 10. In the exemplary embodiment, the control system 36 determines the actual values using the sensor system 94.
[0040] According to some embodiments, the first variable is monotonically correlated with a rotational speed of the rotor 18, and / or the second variable is monotonically correlated with a rotational acceleration of the rotor 18. As used herein, the term monotonically correlated indicates a relationship between two variables of the wind turbine that implies their correlated increase and decrease. For example, as explained above, the wind turbine 10 may include a rotating shaft 48 coupled to the rotor shaft 44 by a gearbox 46. In these embodiments, the rotational speed of the rotating shaft 48 is usually directly proportional to the rotor speed. Therefore, as used herein, the rotational speed of the rotating shaft 48 is said to be monotonically correlated with the rotor speed.As another example, in the exemplary embodiment, the wind turbine 10 includes an electrical generator 42 for generating electrical output power. The electrical output power is typically proportional to the cube of the rotor speed. Therefore, as used herein, the output power is said to be monotonically correlated with the rotor speed.
[0041] According to at least some embodiments, control system 46 determines actual values of the first variable based on sensor system 94 and determines actual values of the second variable from the determined values of the first variable. For example, control system 36 may be configured to determine the actual value of the second variable by calculating the rate of change of the first variable over time. In particular, control system 36 may determine actual values of rotor speed (i.e., in this case, the first variable) using sensor system 94 and may determine actual values of rotor rotational acceleration (i.e., in this case, the second variable) by calculating the rate of change of the rotor speed values over time.
[0042] According to some embodiments, the pitch drive system 68 is configured to rotate the rotor blade 22 based on the result of the estimation performed by the control system 36. For example, the rotor blade 22 is rotated when the control system 36 detects, based on the determined actual values, that the wind turbine 10 is about to enter an overspeed condition. In the exemplary embodiment, the control system 36 communicates with the pitch drive system 68 to signal that an overspeed condition is about to occur. When the pitch drive system 68 receives an overspeed condition occurrence signal, it rotates the rotor blade 22 toward a feathered position to reduce the speed (i.e., to aerodynamically brake the rotor 18).
[0043] According to some embodiments, the sensor system 94 includes one or more sensors for measuring actual values of one or more variables of the wind turbine 10. In particular, the sensor system 94 is communicatively coupled to the control system 36 to typically provide measured values of the variables to the control system 36. Based on the received measured values, the control system 36 typically determines actual values of one or more variables of the wind turbine 10. According to at least some of the embodiments, the sensor system 36 is configured to measure an actual value of at least one of a first variable and / or a second variable of the wind turbine 10, for example, the rotor speed and / or the rotor acceleration.
[0044] According to some embodiments, the sensor system 94 is configured to be coupled to a rotatable part of the wind turbine 10, wherein the rotatable part is connected to the rotor 18, to determine an actual value of a first variable or a second variable of the wind turbine by measuring the rotational speed of the rotatable part. In the exemplary embodiment, the sensor system 94 includes the speed sensor 70 for detecting the rotor speed. In particular, in the exemplary embodiment, the speed sensor 70 is coupled to the rotor shaft 44 to measure its speed. According to some embodiments, the speed sensor 70 includes a proximity sensor configured to register rotation of the rotor shaft 44, such that the speed sensor 70 measures the speed of the rotor shaft 44. The speed of the rotor shaft 44 corresponds to the rotor speed.In alternative embodiments, the sensor system 94 may include a sensor suitable for measuring another variable of the wind turbine 10, for example, a speed sensor coupled to the rapidly rotating shaft 48 to measure its rotational speed. In alternative embodiments, the sensor system 94 may include any arrangement of sensors suitable for measuring multiple variables of the wind turbine 10, for example, a speed sensor coupled to the rapidly rotating shaft 48 to measure the rotational speed of the rapidly rotating shaft 48 and an acceleration sensor coupled to the rotor 18 to measure the rotor acceleration.
[0045] In general, the sensor system 94 may include any suitable sensor that provides a measurement of a variable of the wind turbine 10 suitable for enabling an estimation of the onset of an overspeed condition. For example, the sensor system 94 may include a sensor coupled to an electrical generator portion of the wind turbine 10, such as an output of the electrical generator 42, to determine at least one of an actual value of the first variable and an actual value of the second variable by measuring an output power and / or its rate of change over time from the electrical generator portion.
[0046] According to at least some embodiments, the sensor system 94 may be configured to measure an actual value of a wind speed in an area proximate the wind turbine 10. In the exemplary embodiment, the mast 58 forms part of the sensor system 94 and provides wind speed and direction data to the control system 36. In these embodiments, it is typical for the control system 36 to be configured to further identify an overspeed condition based on a determined actual value of the wind speed. This allows the control system 36 to detect an overspeed condition of the wind turbine by considering actual values of the wind speed to estimate an occurrence of an overspeed condition of the wind turbine 10.
[0047] According to some embodiments, the sensor system 94 is configured to measure an actual value of deflection of the rotor blade 22. In these embodiments, the sensor system 94 may include any suitable sensor that enables determination of deflection of the rotor blade 22, such as a strain gauge sensor or an optical strain sensor.
[0048] According to some embodiments, the sensor system 94 is configured to measure an acceleration of the rotor 18 in a direction perpendicular to a longitudinal axis of the hub 20 (i.e., an acceleration with respect to gravity). In such embodiments, the sensor system 94 typically includes one or more acceleration sensors (not shown) mounted on or near one of the rotor blades 22 to enable detection of a first acceleration of the rotor 18 in a first direction perpendicular to the longitudinal axis of the hub 20 and a second acceleration vector of the rotor 18 in a direction perpendicular to both the first direction and the longitudinal axis of the hub 20.In such embodiments, the measured value or values of the acceleration are used together with at least one actual value of another variable of the wind turbine 10 to estimate an occurrence of an overspeed condition.
[0049] In the exemplary embodiment, the control system 94 determines an actual value of a first variable of the wind turbine from a measured speed. In some embodiments, the actual value is determined directly from at least one measured value. In other embodiments, the actual values of the first variable are derived from at least one measured value of another variable. For example, in some embodiments, the first variable corresponds to the rotor speed, and the control system 36 determines the rotor speed by deriving it from measured values of the speed of the rotating shaft 48. In these embodiments, the control system 36 typically takes the gear ratio into account to derive the actual values of the rotor speed from the measured speed of the rotating shaft 48.In the exemplary embodiment, control system 36 determines an actual value of the second variable from the time rate of change of the measured rotor speed values. Alternatively, control system 36 determines an actual value of the second variable directly from measured rotor acceleration values provided by sensor system 94. As explained above, control system 36 evaluates the determined actual values of the first variable and the second variable to estimate the occurrence of an overspeed condition of wind turbine 10.
[0050] Fig. 4 shows a block diagram of an exemplary control system 36 which forms part of a control device of the wind turbine 10 according to Fig. 1. In the exemplary embodiment, the control system 36 includes a controller 102, a memory 104, and a communications module 106. The control system 36 may include any suitable device that enables the control system 36 to function in the manner described herein. In the exemplary embodiment, the communications module 106 includes a sensor interface 108 that enables the controller 102 to communicate with the sensor system 94. In one embodiment, the sensor interface 108 includes an analog-to-digital converter that converts an analog voltage signal generated by the sensor into a multi-bit digital signal usable by the controller 102.In alternative embodiments, the communication module 106 may include any suitable hard-wired and / or wireless communication device that enables transmission of signals to and / or reception of signals from any device disposed on the wind turbine, such as a device disposed on the rotor shaft 44 or inside or outside the rotor 18 and / or remote from the rotor 18. In the exemplary embodiment, the memory 104 may include any suitable storage device, including, but not limited to, flash memory, electrically erasable programmable memory, read-only memory (ROM), removable media, and / or other volatile and non-volatile storage devices. In one embodiment, executable instructions (i.e.Software instructions) are stored in memory 104 for use by controller 102 in controlling pitch drive system 68, as described below.
[0051] In the exemplary embodiment, controller 102 is a real-time controller including any suitable processor-based or microprocessor-based system, such as a computer system including microcontrollers, reduced instruction set integrated circuits (RISCs), application-specific integrated circuits (ASICs), logic circuits, and / or any other circuits or processors capable of performing the functions described herein. In one embodiment, controller 102 may be a microprocessor including read-only memory (ROM) and / or random access memory (RAM), such as a 32-bit microcomputer with 2 Mbit ROM and 64 Kbit RAM.As used herein, the term "real time" refers to results that occur in a substantially short period of time after a change in the inputs influencing the result, where the period of time is a design parameter that can be selected based on the importance of the result and / or the ability of the system to process the inputs to produce the result.
[0052] In the exemplary embodiment, a sensor of the sensor system 94, for example, a speed sensor 70, is coupled to the rotor shaft 44 to enable measurement of the speed of the rotor 18. The sensor system 94 may include a sensor mounted at any suitable location on the wind turbine 10 that allows the sensor to measure a variable of the wind turbine 10, for example, a speed of the rotor 18 or a speed directly proportional thereto, such as a speed of the rapidly rotating shaft 48.
[0053] According to some embodiments, the controller 102 is programmed to determine an actual value of a first variable indicative of an overspeed condition of the wind turbine 10. In the exemplary embodiment, a sensor of the sensor system 94 is communicatively coupled to the controller 102 via any suitable hard-wired and / or wireless communication medium through the sensor interface 108 of the communication module 106 to enable activation of the sensor to transmit signals to and / or receive signals from the controller 102. In the exemplary embodiment, the speed sensor 70 continuously measures actual values of a speed of the rotor 18, and the speed sensor 70 continuously transmits signals indicative of measured actual values of the rotor speed to the controller 102 in real time.In one embodiment, the controller 102 may be programmed to continuously receive and monitor the signals transmitted by the speed sensor 70. In an alternative embodiment, the controller 102 may not continuously receive and / or monitor the signals transmitted by the speed sensor 70, but rather may be programmed to repeatedly request signals from the speed sensor 70 at predetermined time intervals. In some embodiments, the controller 102 and / or the speed sensor 70 may send and / or receive signals from each other at any suitable time intervals. Alternative or additional sensors of the sensor system 94 communicate in an analog manner with the controller 102 to transmit actual measurements of variables of the wind turbine 10 thereto.
[0054] According to some embodiments, the controller 102 is programmed to determine an actual value of a second variable of the wind turbine 10 that is correlated with the time rate of change of a first variable. Typically, the second variable is correlated with the time rate of change of the first variable in such a way that a change in the time rate is accompanied by, and usually parallel to, a change in the second variable. In the exemplary embodiment, the controller 102 is programmed to determine a time rate of change of the rotational speed of the rotor 18 from measured actual values of the rotor rotational speed. In this manner, the exemplary controller 102 determines actual values of a second variable of the wind turbine 10, in this case, the rotational acceleration of the rotor 18, from the rate of change of the first variable (i.e., in this case, the speed of the rotor 18) over time. In other alternative embodiments, the controller 102 may determine actual values of a second wind turbine variable from data measured by sensors that form part of the sensor system 94. For example, the controller 102 may determine the actual values of rotational acceleration from data measured by an acceleration sensor that forms part of the sensor system 18. In other alternative embodiments, the controller 102 may determine actual values of the second wind turbine variable, such as rotor acceleration, from the time rate of change of other wind turbine variables, such as, but not limited to, the rotational speed of the rapidly spinning shaft 48 or an output power of the wind turbine 10.
[0055] During operation of the exemplary wind turbine 10, the controller 102 is programmed to receive signals corresponding to actual values of at least one wind turbine variable, such as measured data provided by the speed sensor 70, and the controller 102 is programmed to associate a value of a wind turbine variable with each signal to determine at least one actual value of that variable. For example, the controller 102 may be programmed to associate a value of the speed of the rotor 18 with a signal from the speed sensor 70 to determine an actual value of the speed of the rotor 18. According to some embodiments, the controller 102 is programmed to associate a value of a second wind turbine variable with a signal from a sensor of the sensor system 94.For example, the controller 102 may be programmed to associate a value of the rotational acceleration of the rotor 18 with a signal from an acceleration sensor to determine an actual value of the acceleration of the rotor 18.
[0056] In the exemplary embodiment, the controller 102 is programmed to store data indicative of an overspeed condition (i.e., an overspeed condition of the rotor 18) in the memory 102. For example, the controller 102 may store the maximum allowable speed of the wind turbine. At this speed, the rotor 18 is said to be in an overspeed condition. In another embodiment, the controller 102 stores a lookup table correlating values of a first and a second variable of the wind turbine 10 with the occurrence of an overspeed condition. For example, such a lookup table may correlate values of the rotor speed and the rotor acceleration that cause an overspeed condition of the wind turbine 10 to occur within a predetermined period of time.
[0057] According to some embodiments, the controller 102 is programmed to estimate the occurrence of an overspeed condition of the wind turbine 10 based on at least the determined actual values of the first and second variables. In particular, according to some embodiments, the controller 102 is programmed to, after determining the actual values of a first and a second variable of the wind turbine 10, evaluate these values for an estimation directed to identifying an overspeed condition of the wind turbine 10. In the exemplary embodiment, the controller 102 is programmed to evaluate at least one of the determined values of the rotor speed and / or the rotor acceleration to identify the occurrence of an overspeed condition of the wind turbine 10.As used herein, the term "identifying an overspeed condition" is intended to identify a process for inferring the occurrence of an existing overspeed condition or estimating the occurrence of an overspeed condition within a predetermined period of time or for identifying values of variables of the wind turbine that may cause an overspeed condition to occur within a predetermined period of time.
[0058] The controller 102 is programmed to identify a future rotor speed based on determined actual values of a first and a second variable of the wind turbine 10, and in particular to compare the identified future rotor speed with a predetermined rotor speed value to estimate an occurrence of an overspeed condition.
[0059] In one embodiment, the controller is programmed to evaluate the determined actual values of the first variable and the second variable to identify an overspeed condition. The controller is programmed to continuously input the actual values of the first and second variables into a mathematical model that enables identification of an overspeed condition. The controller 102 is programmed to identify a future rotor speed based on certain actual values of the first variable and the second variable. For example, in one embodiment, the controller 102 is programmed to determine an actual value of the rotor speed v i and an actual value of the rotor acceleration a i into the formula v i +a iT to identify a future rotor speed that will occur within a predetermined time period T. In one embodiment, the predetermined time period T is in the range of approximately 0.1 to 5 seconds, or more particularly 0.5 to 4 seconds, or even more particularly 1 to 3 seconds. In one embodiment, the predetermined time period T is in the range of 1 second to 3 seconds. Alternatively, the predetermined time period T may be any suitable time period that allows the controller 102 to appropriately identify a future rotor speed. According to at least some of these embodiments, the controller 102 is further programmed to compare the identified future rotor speed to a predetermined rotor speed value to identify an overspeed condition of the wind turbine 10.
[0060] Typically, the value of the predetermined rotor speed corresponds to the maximum permissible speed of the wind turbine, which speed is determined in advance by evaluating the specific characteristics of the wind turbine 10. Typically, the maximum permissible speed is determined in advance by taking into account the physical properties of the blade tips. In particular, the maximum permissible speed corresponds to a rotor speed at which the speed of an outer portion of the rotor blade 22 (i.e., the edge speed) does not exceed a speed between 70 and 110 m / s, or in particular between 80 and 100 m / s, for example 90 m / s.In some embodiments, the maximum allowable speed of the wind turbine 10 is determined in advance by taking into account the maximum allowable load on some components of the wind turbine 10, such as the rotor bearings, caused by rotation of the rotor 18, or the maximum allowable load acting on the tower 12 or the nacelle 16. In some embodiments, the maximum allowable speed is determined in advance by taking into account the maximum allowable noise generation of the wind turbine 10. In some embodiments, the maximum allowable speed may change depending on the specific conditions to which the wind turbine 10 is exposed. For example, according to some embodiments implemented in offshore wind turbines, the strength (ieforce) or the power density and / or the frequency of the sea waves acting on the wind turbine 10 are taken into account to determine the maximum permissible speed at a given time.
[0061] Alternatively, any suitable mathematical model may be used that enables the wind controller 102 to identify an overspeed condition, as described herein. Such a suitable mathematical model may be a model having as inputs the acceleration with respect to gravity, referred to above, and its rate of change over time. Alternatively, such a mathematical model may be a model having as further inputs the wind speed and its rate of change over time. Typically, the mathematical model has as input a combination of variables corresponding to a value of a particular quantity of the wind turbine 10 and its rate of change over time.According to some embodiments, a mathematical model with more than two variables of the wind turbine 10 as inputs is implemented in the controller 102 to identify a future value of the rotor speed. For example, such a mathematical model may have the second time derivative, the third time derivative, or even higher time derivatives of the rotor speed as inputs to accurately identify a future value of the rotor speed. Typically, such a mathematical model is based on a finite Taylor expansion that provides an approximation of a future value of the rotor speed after a certain time. In another example, a mathematical model having the output power and the rotor acceleration as inputs is implemented in the controller 102 to identify a future value of the rotor speed.
[0062] According to some embodiments, the controller 102 is programmed to identify the time required to reach a predetermined rotor speed value based on determined actual values of a first variable and a second variable of the wind turbine and usually to compare the identified time period with a predetermined time period. In one embodiment, the controller 102 is programmed to derive from the mathematical model the time required to reach a predetermined rotor speed value based on the determined actual values of the first variable and the second variable and to compare the identified time period with a predetermined time period. For example, the controller 102 can estimate the occurrence of an overspeed V by determining the time required to reach the maximum permissible speed of the wind turbine 10 by inputting an actual value of the rotor speed v iand an actual value of the rotor acceleration a i into the formula (Vv i ) / a i If the determined time period is less than a predetermined time period, the controller 102 identifies the occurrence of an overspeed condition and reports it accordingly to the pitch drive system 68 to rotate the rotor blades 22. Typically, the predetermined time period is in the range of approximately 0.1 to 5 seconds, or more specifically, 0.5 to 4 seconds, or even more specifically, 1 to 3 seconds.
[0063] According to some embodiments, the controller 102 is programmed to estimate the occurrence of an overspeed condition of the wind turbine by activating a logic algorithm when the value of the first variable indicating an overspeed condition of the wind turbine 10 exceeds a predetermined value. For example, according to some embodiments, the logic is activated when the rotor speed exceeds a value between 85% and 95%, for example, 90%, of the maximum allowable rotor speed. Alternatively, the logic is activated when an output power of the wind turbine 10 exceeds a value between 85% and 95%, for example, 90%, of the maximum allowable output power. Alternatively, the logic is activated when a wind speed in the vicinity of the wind turbine 10 exceeds a value between 8 m / s and 12 m / s, for example, 12 m / s.Once the logic is activated and as long as the first variable is greater than the predetermined value, the controller 102 estimates an occurrence of an overspeed condition by calculating a future value of the first variable that will occur within a predetermined time period. Typically, the predetermined time period is in the range of approximately 0.1 to 5 seconds, or more specifically, 0.5 to 4 seconds, or even more specifically, 1 to 3 seconds.
[0064] According to some embodiments, the controller 102 is programmed to validate determined actual values of a first and a second variable of the wind turbine 10 by comparing these values to a list of predetermined values to estimate the occurrence of an overspeed condition of the wind turbine 10. In one embodiment, the controller 102 may store a lookup table containing a list of predetermined values of the first and second variables of the wind turbine 10 to identify which combination of these values results in an overspeed condition within a certain period of time. In particular, the controller 102 may store a lookup table containing predetermined values of the rotor speed and the rotor acceleration.By validating the actual values of rotor speed and rotor acceleration in the lookup table, the controller 102 can estimate the occurrence of an overspeed condition of the wind turbine 10. In particular, the lookup table can indicate to the controller 102, based on certain combinations of the actual values, that it should signal the pitch drive system 68 to adjust the pitch of the rotor blades 22 to aerodynamically brake the rotor 18.
[0065] A lookup table, as referred to above, is typically determined in advance by appropriate modeling of the wind turbine dynamics and the maximum allowable parameters of the wind turbine 10, such as, but not limited to, the loads acting on certain components, such as the tower 12, the nacelle 16, or bearings within the wind turbine 10, as well as noise generation. Alternatively, the table is determined in advance by any suitable method that enables the wind controller 102 to estimate the occurrence of an overspeed condition, as described herein. In alternative embodiments, an evaluation is performed based on a table that correlates values of other variables, such as the output power and the rotor acceleration, or the rotor speed and the time rate of change of the output power.According to some embodiments, the lookup table has as input three or more variables of the wind turbine or other parameters related thereto, such as, but not limited to, wind speed. According to some embodiments, a lookup table and a mathematical model having as input at least one variable of the wind turbine 10 are implemented in the controller 102 to estimate the occurrence of an overspeed condition.
[0066] According to some embodiments, the controller 102 further bases the estimate on a determined actual value of the wind speed to identify an overspeed condition of the wind turbine 10. For example, the controller 102 may input actual values of the rotor speed, the rotor acceleration, and the wind speed into a suitable mathematical model to identify an overspeed condition of the wind turbine. This enables the controller 102 to estimate the occurrence of an overspeed condition in an accurate and reliable manner. In another example relating to an offshore wind turbine, the magnitude (i.e., force) or power density and / or frequency of ocean waves acting on a wind turbine 10 are taken into account to estimate an occurrence of an overspeed condition of a wind turbine 10.
[0067] According to some embodiments, controller 102 identifies an overspeed condition based on at least one of a deflection of a rotor blade 22, an output power of wind turbine 10, and / or a speed of wind turbine 10 directly proportional to a speed of the rotor. According to some embodiments, controller 102 bases the evaluation on the rate of change of at least one of these variables.
[0068] In the exemplary embodiment, the controller 102 is further programmed to control at least one pitch drive system 68 when the controller 102 positively assesses the occurrence of an overspeed condition to aerodynamically brake the rotor 18. In one embodiment, the controller 102 is programmed to identify a future rotor speed based on the determined actual values of the first variable and the second variable, compare the identified future rotor speed to a predetermined rotor speed value to identify an overspeed condition of the wind turbine 10, and control the pitch drive system 68 when an identified future rotor speed is at or exceeds the predetermined rotor speed value.In one embodiment, the controller 102 is configured, in response to an identified occurrence of a future overspeed condition, to control the pitch drive system 68 to move the rotor blade 22 to a feathered position such that rotation of the rotor 18 is retarded.
[0069] According to some embodiments, the pitch drive system 68 adjusts the angle of attack of the rotor blade 22 at a pitch rate, wherein the pitch rate is determined based at least on at least one determined actual value of the first variable and / or the second variable. In the exemplary embodiment, the controller 102 determines a pitch rate for controlling at least one pitch drive system 68. The controller 102 may determine the pitch rate based on the determined actual values of the rotor speed and the rotor acceleration. Typically, by considering the actual values of both variables, the blades 22 are adjusted at a lower pitch rate compared to a situation where only the actual rotor speed is considered.Consequently, these embodiments enable a smooth pitch adjustment of a rotor blade 22 in response to a condition of the wind turbine 10 that may or does result in an overspeed condition. The higher the pitch adjustment speed, the higher the number of resonant frequencies of the wind turbine 10 that are excited. Consequently, these embodiments enable only a small number of resonant frequencies to be excited during the pitch adjustment, so that tower vibration caused by the pitch adjustment is generally kept to a minimum.
[0070] According to certain embodiments, the controller 102 determines the pitch speed by considering a predetermined maximum gross braking speed. Typically, the pitch drive system 38 rotates the rotor blade 22 in such a way that braking of the rotor 18 does not exceed a predetermined maximum rotor braking speed. In one embodiment, the pitch speed is determined by considering a predetermined maximum load, such as, but not limited to, a maximum predetermined load on the rotor bearings, the tower 12, or the nacelle 16. Typically, in this embodiment, the pitch drive system 68 rotates the rotor blades 22 in such a way that a load acting on the wind turbine 10 does not exceed the predetermined maximum load.For example, the controller 102 may determine actual values of the load acting on certain components of the wind turbine 10, such as, but not limited to, a load on the rotor bearings, the tower 12, or the nacelle 16, and determine a pitch speed that affects the aerodynamic deceleration of the rotor 18 in such a way that the load does not exceed the predetermined maximum load. In some embodiments, the pitch drive system 68 rotates the rotor blades 12 in such a way that a first variable of the wind turbine 10, such as the rotor speed, does not exceed a threshold value, such as the maximum allowable rotor speed referenced above.
[0071] Fig. 5 shows a flowchart illustrating an exemplary method 500 for operating the wind turbine 10 according to Fig. 1. In the exemplary embodiment, the method 500 includes determining 502 an actual value of a first variable indicative of an overspeed condition of the wind turbine 10. Typically, the first variable is monotonically correlated with a rotational speed of the rotor 10. For example, the first variable corresponds to the rotor speed, the pre-bend of the rotor blade 22, an output power of the wind turbine 10, or a rotational speed of the wind turbine 10, where this rotational speed is directly proportional to a rotational speed of the rotor, such as the speed of the rapidly spinning shaft 48 or the speed of the electric generator 42. Alternatively, the first variable may correspond to the acceleration with respect to gravity referred to above.The exemplary method 500 further includes determining an actual value of a second variable of the wind turbine 10 that is correlated with the rate of change of the first variable over time. Typically, the second variable is monotonically correlated with a rotational acceleration of the rotor 18.
[0072] The exemplary method 500 further includes estimating 506 an occurrence of an overspeed condition of the wind turbine 10 based on at least the determined actual values of the first and second variables. The estimating 506 includes identifying a future rotor speed based on the determined actual values of the first variable and the second variable and optionally comparing the identified future rotor speed to a predetermined rotor speed value to identify an overspeed condition of the wind turbine 10. According to some embodiments, the estimating 506 includes identifying the time period until a predetermined rotor speed value is reached based on the determined actual values of the first variable and the second variable and comparing the identified time period to a predetermined time period.According to some embodiments, estimating 506 includes validating the determined actual values of the first and second variables by comparing these values to a list of predetermined values. This enables estimation of an occurrence of an overspeed condition.
[0073] The exemplary method 500 further includes adjusting the pitch 510 of the rotor blade 22 to aerodynamically decelerate the rotor 18 based on a result 508 of the estimate. Typically, the rotor blades 22 are rotated if the result 508 of the estimate is the occurrence of an overspeed condition within a predetermined time. According to some embodiments, when an overspeed condition is identified, the pitch drive system 68 rotates the rotor blade 22. In particular, it is typical for the pitch drive system 68 to adjust the pitch of the rotor blade 22 as soon as the occurrence of an overspeed condition has been identified in the estimate, or with a delay corresponding to a predetermined time.
[0074] Fig. 6 shows a flowchart illustrating another exemplary method 600 for operating the wind turbine according to Fig. 1. In the exemplary embodiment, the method 600 includes determining 602 an actual value of a reference speed that is directly proportional to the speed of the rotor. Typically, the reference speed corresponds to the rotor speed, the rotational speed of the rapidly rotating shaft 48, or the speed of a rotatable part of the wind turbine 10 coupled to the rotor 18. Typically, the reference speed indicates an overspeed condition of the wind turbine 10 when it exceeds a threshold value. Typically, the threshold speed corresponds to a maximum allowable speed of the reference speed. The exemplary method 600 further includes determining 604 an actual value of a rate of change of the reference speed over time. Typically, this rate of change corresponds to the acceleration of the rotor 18.The exemplary method 600 further includes evaluating 606 the determined actual values of the reference speed and the time rate of change of the reference speed to identify an overspeed condition of the wind turbine. The exemplary method 600 further includes identifying 608 an overspeed condition based on the result of the evaluation 606. If an overspeed condition is identified, the pitch drive system 68 rotates the rotor blade 22 in step 610.
[0075] Fig. Figure 7 shows a schematic graphical representation of the response to an identified overspeed condition of the wind turbine after Fig. 1 compared to the response of a prior art wind turbine to overspeed caused by an increase in wind speed. In particular, the graph shows the response of the wind turbines during a period of approximately 13 seconds (i.e., corresponding to the horizontal axis of the graphs). Graph A shows a time series plot of wind speed 700, which typically results in an increase in rotor speed. The wind speed is illustrated in graph A in units of meters per second (m / s). The increase in rotor speed caused by wind speed 700 is illustrated in graph B for at least one prior art wind turbine (line 702) and in graph C for a wind turbine according to the above exemplary embodiment (line 706). The rotor speed is illustrated in both graphs in units of revolutions per minute (1 / m).In the known wind turbine, the rotor speed 702 exceeds a predetermined rotor speed value 703 at a time T1, which corresponds to a rotor overspeed. In the known wind turbine, the blade angle (line 704) is varied to reduce the rotor speed as soon as the rotor speed 702 exceeds the predetermined value 703, ie, at time t1.
[0076] As shown in graph C after Fig.7, a blade angle (line 708) is varied in the exemplary embodiment to reduce rotor speed when the wind turbine controller identifies an overspeed condition based on the estimation discussed above. Specifically, at time t1', a time prior to t1, the exemplary wind turbine estimates the occurrence of a future wind turbine overspeed condition within a certain time based on actual values of rotor speed and rotor acceleration. In the exemplary embodiment, the pitch drive system 68 rotates the rotor blades 22 at time t1'. That is, in the exemplary embodiment, the wind turbine begins to adjust the pitch before the rotor speed 706 would reach the predetermined value 703 corresponding to a rotor overspeed.Accordingly, in the exemplary embodiment, controller 102 detects the occurrence of a future overspeed condition and reacts before the wind turbine enters the estimated overspeed condition. As a result, the exemplary wind turbine is capable of performing a smoother pitch adjustment than the prior art wind turbine to reduce the rotor speed in response to an increase in wind speed capable of causing an overspeed condition of the wind turbine. As a result, the pitch detection of the exemplary wind turbine results in a smoother rotor deceleration compared to the prior art wind turbine and consequently reduces the transient loads acting on wind turbine components.
[0077] Generally, adjusting the pitch of the blades in a wind turbine to reduce rotor speed implies that the wind turbine is pulled into the wind (i.e., it results in a wind tower deflection toward the wind). This pull usually increases with the pitch adjustment speed. Graph D shows a tower deflection 710 versus the change in blade angle 704 of the prior art wind turbine in graph B and a tower deflection 712 versus the change in blade angle 708 of the exemplary embodiment according to graph C. The prior art wind turbine is pulled into the wind during time t1 and time t2, while the wind turbine in the exemplary embodiment is pulled into the wind during time t1' and time t2'.Since the pitch adjustment is performed at a lower adjustment speed for the wind turbine in the exemplary embodiment, the corresponding deflection of the wind tower is smaller than for the known wind turbine. At time t2, the rotor speed 702 of the known wind turbine is reduced back below the predetermined value 703, and the blade angle 704 is changed in the opposite direction to keep the rotor speed as high as possible. Accordingly, the wind tower in the known wind turbine is pushed relative to the wind between time t2 and time t3, as illustrated by the tower deflection 710.
[0078] This pulling and pushing in the known wind turbine excites the resonance frequency of the tower, as illustrated by the tower deflection 710 in graph D. The tower vibration is shown in graph D in units of thousandths of the acceleration due to gravity (1g = 9.81 m / s 2). In general, such a resonant vibration of the known wind turbine requires shutdown of the wind turbine. In contrast, due to the lower pitch adjustment speed in the exemplary wind turbine, the associated tower deflection 712 is less than in the known wind turbine. In this example, the tower deflection 712 does not result in a resonant vibration of the tower. Accordingly, in this example, pitch adjustment of the exemplary wind turbine when an overspeed condition is identified does not require shutdown. Furthermore, loads acting on the exemplary wind turbine during pitch adjustment are significantly reduced compared to the known wind turbine.
[0079] Example embodiments of systems and methods for operating a wind turbine are described in detail above. The systems and methods are not limited to the specific embodiments described herein; rather, components of the systems and / or steps of the methods may be used independently and separately from other components and / or steps described herein. For example, the method may evaluate values of one variable determined by a sensor and values of another variable determined using a suitable mathematical model having as input the first variable and other dynamic variables, such as wind speed, and is not limited to implementation in only the wind turbine systems as described herein. Rather, the example embodiment may be implemented and utilized in connection with many other rotor blade applications.
[0080] This description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. While various specific embodiments have been disclosed in the foregoing, those skilled in the art will recognize that equivalent modifications are within the spirit and scope of the claims. In particular, non-exclusive features of the above-described embodiments may be combined. The patentable scope of the invention is defined by the claims and may include other examples that occur to those skilled in the art.Such further examples are intended to be included within the scope of the claims if they contain structural elements that do not differ from the literal meaning of the claims, or if they contain equivalent structural elements with insubstantial differences from the literal meaning of the claims.
[0081] A method for operating a wind turbine 10 is provided. The wind turbine 10 includes a rotor 18 having at least one rotor blade 22, and a pitch drive system 68 coupled to the at least one rotor blade 22. The pitch drive system 68 is configured to adjust the pitch of the rotor blade 22. The method includes: determining an actual value of a first variable indicative of an overspeed condition of the wind turbine 10; determining an actual value of a second variable of the wind turbine 10 that is correlated with the time rate of change of the first variable; and estimating an occurrence of an overspeed condition of the wind turbine 10 based on at least the determined actual values of the first and second variables. The estimating includes identifying a future rotor speed based on the determined actual values of the first and second variables.The blade pitch drive system 68 adjusts the angle of attack of the at least one rotor blade 22 for aerodynamic braking of the rotor 18 based on the result of the estimation. Parts list: 10 wind turbines 12 Tower 14 Support system 16 gondolas 18 Rotor 20 rotating hub 22 rotor blades 24 Leaf foot section 26 load transfer areas 28 direction 30 axis of rotation 32 blade pitch system 34 blade pitch axes 36 Tax system 38 Yaw axis 40 processor 42 electric generator 44 Rotor shaft 46 gearboxes 48 fast rotating shaft 50 clutch 52 bracket 54 bracket 56 Yaw drive mechanism 58 wind measurement mast 60 front support bearing 62 rear support bearing 64 Drivetrain 66 Blade pitch arrangement 70 speed sensor 72 blade pitch bearings 74 Blade pitch drive motor 76 blade pitch drive gears 78 Blade pitch drive pinion 82 cables 84 Power generator 86 cavity 88 inner surface 90 outer surface 92 Control device 94 Sensor system 116 Longitudinal axis 500 exemplary procedures 502 Determination step 504 Determination step 506 Evaluation step 508 Identification step 510 rotation step 600 exemplary procedure 602 Determination step 604 Determination step 606 Evaluation step 608 Identification step 610 rotation step 702 Line 703 predetermined rotor speed 704 Line
Claims
[1] A method for operating a wind turbine (10), wherein the wind turbine (10) has a rotor (18) containing at least one rotor blade (22) and a blade adjustment drive system (68) coupled to the at least one rotor blade (22), wherein the blade adjustment drive system (68) is configured to adjust the angle of attack of the at least one rotor blade (22), the method comprising: Determining an actual value of a first variable indicative of an overspeed condition of the wind turbine (10); Determining an actual value of a second variable of the wind turbine (10) that is correlated with the time rate of change of the first variable; and Estimating an occurrence of an overspeed condition of the wind turbine (10) based on at least the determined actual values of the first and second variables, wherein the estimating comprises identifying a future rotor speed based on the determined actual values of the first and second variables, and wherein the blade pitch drive system (68) adjusts the angle of attack of the at least one rotor blade (22) for aerodynamically braking the rotor (18) based on the result of the estimation. [2] The method of claim 1, wherein the blade pitch drive system (68) adjusts the angle of attack of the at least one rotor blade (22) to aerodynamically brake the rotor (18) when the result of the estimation is the occurrence of an overspeed condition within a predetermined time. [3] A method according to any one of the preceding claims, wherein the estimating comprises comparing the identified future rotor speed with a predetermined rotor speed value. [4] A method according to any one of the preceding claims, wherein the first variable corresponds to a magnitude of a deflection of the at least one rotor blade (22), an output power of the wind turbine (10) or a rotational speed of the wind turbine (10), the rotational speed being directly proportional to a rotational speed of the rotor. [5] A method according to any one of the preceding claims, further comprising determining a pitch adjustment rate for rotating the at least one rotor blade (22), wherein the pitch adjustment rate is determined at least based on the determined actual values of the first variable or the second variable. [6] A method according to any one of the preceding claims, wherein the blade pitch drive system (68) adjusts the angle of attack of the at least one rotor blade (22) in such a manner that the first variable does not exceed a threshold value. [7] A method according to any one of the preceding claims, wherein the actual value of the second variable of the wind turbine is determined by calculating the time rate of change of at least two actual values of the first variable. [8] A control device (92) for use in a wind turbine (10), the wind turbine (10) including a rotor (18) having at least one rotor blade (22), the control device comprising: a blade pitch drive system (68) coupled to the at least one rotor blade (22), the blade pitch drive system (68) being configured to adjust the angle of attack of the at least one rotor blade (22); a control system (36) communicatively connected to the blade pitch drive system (68), the control system (36) being configured to: to determine an actual value of a first variable indicative of an overspeed condition of the wind turbine (10); to determine an actual value of a second variable of the wind turbine (10) which is correlated with the time rate of change of the first variable; and to estimate an occurrence of an overspeed condition of the wind turbine (10) based on at least the determined actual values of the first and second variables, wherein the estimation comprises identifying a future rotor speed on the basis of the determined actual values of the first and second variables; and wherein the control system is configured to control the blade pitch drive system (68) in such a manner that the blade pitch drive system (68) adjusts the angle of attack of the at least one rotor blade (22) for aerodynamically braking the rotor (18) based on the result of the estimation. [9] The control device of claim 8, further comprising a sensor system (94) communicatively coupled to the control system (36), the sensor system (94) configured to measure at least one of the actual value of the first variable and the actual value of the second variable. [10] The control device according to claim 9, wherein the sensor system (94) is arranged to be coupled to a rotatable part of the wind turbine (10), the rotatable part being connected to the rotor (18) to determine at least one of the actual value of the first variable and the actual value of the second variable by measuring the speed of the rotatable part.
Citation Information
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