• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Wind turbine control method. A method for controlling wind turbines equipped with a blade pitch angle control system and which are determined to be positioned in a misaligned manner with respect to the direction of the incident wind is described. The method described here makes use of a series of data and measurements captured in the wind turbine itself or its environment to process said data and generate through a series of processes and calculations a series of values that are used in control commands on the control system angle of blade pitch of wind turbines to avoid anomalies and/or increase the efficiency of the same in said situation. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2538739A1
    申请号:ES201331903
    申请日:2013-12-23
    公开日:2015-06-23
    发明作者:José Luis LABORDA RUBIO；Alberto García Barace；Teresa Arlabán Gabeiras；José Luis ARÍSTEGUI LANTERO；Alejandro GONZÁLEZ MURUA；José Miguel García Sayés；Miguel Núñez Polo
    申请人:Acciona Windpower SA；
    IPC主号:
    专利说明:

    The present invention relates to the technical field of renewable energy, more specifically to the generation of electric energy from wind energy.
    The object of the invention is directed to a wind turbine control method that allows to efficiently manage its operation in situations of anomalies such as misalignment.
    STATE OF THE TECHNIQUE
    Nowadays, the use of renewable energies for electricity generation is common,
    15 Wind energy being among them one of the most efficient. Wind energy allows electricity to be generated from the wind by wind turbines. These wind turbines basically consist of a tower, a gondola that houses the electric generator, a rotor formed in turn by at least two blades, and a power train that transmits power from the rotor to the electric generator. The power train can comprise a multiplier
    20 that connects a low speed shaft connected to the rotor and a high speed shaft connected to the electric generator.
    In multi-megawatt wind turbines, there is a market trend towards larger rotors, which provide energy at a lower cost. In these configurations there is a
    25 increasing importance of the control system. This system maximizes the production of energy while limiting the mechanical loads produced by the wind. For this, the control system acts on the pitch angle of pitch-blade-angle and on the torque demanded from the generator.
    On the one hand, the pitch angle is controlled by a set of actuators that rotate the blade around its longitudinal axis. Said performance manages to vary the aerodynamic torque, either to obtain the maximum possible wind power in weather conditions, or to limit the mechanical loads produced on the wind turbine.
    On the other hand, the control system modulates the torque demanded to the generator from the converter. The torque modulation is also carried out with the double objective of obtaining the maximum possible wind power in given weather conditions, and to limit the mechanical loads produced on the wind turbine.
    Due to the three-dimensional and stochastic nature of the wind - along the area swept by the rotor, the wind is a non-uniform vector in space and random - the loads experienced by each blade and as a consequence of it by the wind turbine, They are variable over time. An example of this variability is observed in terms of the height with respect to the earth's surface, producing the phenomenon known as shear (wind shear). Another example is the variability of the wind direction, which forces us to consider the performance of a system that guides the nacelle to keep the rotor correctly oriented. It is the yaw system.
    The yaw system does not act continuously. It only orients the rotor in the direction of the wind when a system comprising a wind vane detects that the disorientation exceeds a certain threshold value for a certain time. In the course of the time in which the rotor remains disoriented, situations can occur where disorientation causes the equivalent behavior of a blade to be at a loss, producing high aerodynamics on the rotor, and losing control capacity by regulating the pitch of shovel. The present invention is designed to address this problem.
    In the current state of the art, the usual is the following:
    When a disorientation is detected, the control system acts with the gondola orientation system to correct it. However, yaw control is carried out based on average disorientation signals that have to exceed a threshold for a certain time (not short) to avoid over-action with the yaw system. In addition, the yaw system is a slow acting system (of the order of a few degrees per second), which means that, if the change in the wind direction is large and fast, it takes a long time until it is corrected. For example, for a 90 ° error at a normal speed of the yaw orientation system of 2 ° / s, it would take to correctly orient the machine about 45 s. This causes the loads to increase until the orientation is corrected. This is the state of the art that is taken as the closest state of the art to raise the invention.

    The curve that defines the minimum blade pitch angle ¡3min -see Figure 1-is predetermined, Le. for each wind speed (or power) a minimum blade pitch angle is set to avoid speed excursions. In the speed regulation zone where the power generated is equal to the nominal PN, the transients in the rotor speed caused by wind gusts can lead to overspeed (for example, after a decrease in wind speed that has led associated with a decrease in blade pitch angle, such a rapid increase in wind may occur that does not give time to increase the blade pitch angle accordingly). In that case the wind turbine control system causes the machine to be disconnected from the power grid. In order to prevent such overspeeds that cause the turbine to stop, there is the possibility of limiting the minimum angle of the blade pitch reached in transient phenomena. For this, the state-of-the-art control system uses a predetermined cUlVa whereby it sets a minimum threshold that is applied to the blade pitch setpoint at a minimum blade pitch angle value as a function of the blade pitch angle half the angle of the middle shovel is usually used as a signal indicative of the average wind speed or power). In this way, for a certain average blade pitch angle calculated in a time window, shovel pitch excursions below a certain blade pitch value are not allowed
    There are cases in which the minimum blade pitch angle (instead of being predetermined for each average wind speed or power or average blade pitch) is varied taking into account the modification of the aerodynamic efficiency of the blade due, for example , to the deposition of ice or dirt on it. Examples of these control techniques are found in the following documents:
    Thus, document US8096761 describes a control method that, in the presence of ice, modifies the value of the minimum blade pitch angle 3 min. This patent does not specify how the presence of ice is identified, speaking only of an estimate of the loss of aerodynamic efficiency. While in US4656362 a control method is presented that modifies the value of the minimum blade pitch angle 3min using a value related to aerodynamic performance.
    At present, the individual blade pitch control techniques use sensors to measure the loads on the blades, from which the loads on fixed axes are estimated.

    DESCRIPTION OF THE INVENTION
    In a first aspect, the present invention relates to a method of controlling wind turbines that are in circumstances such as those mentioned above. More specifically, the control method described here is especially useful when it is determined that there is a misalignment of the wind turbine with respect to the incident wind, which can cause non-optimal operations in terms of capture while also affecting anomalies in the wind itself. wind turbine and its components. A second aspect of the present invention relates to a wind turbine blade pitch control system adapted to carry out the method referred to the first first aspect of the present invention.
    Consequently, and in a preferred embodiment of the wind turbine control method with blade pitch control system, an action is carried out on the different control systems thereof when it is determined that there is a misalignment of the gondola with respect to the direction of the incident wind; In order to carry out the following steps of the preferred embodiment of the method described herein, it is possible to adapt the pitch angle value J3 from the disorientation value of the wind turbine cp, blade angle value J3 which allows, by means of a setpoint sent to the blade actuators, reduce the loads associated, for example, with excessive turbulence of the wind direction (there are gusty effects of wind direction that are harmful).
    The control method of the present invention carries out a series of data captures and from them one proceeds to carry out a calculation of the lower limit of pitch angle J3MIN from the value of the disorientation of the wind turbine <p. For this purpose, the value of at least one signal indicative of the wind speed incident in the wind turbine or an average thereof is obtained, for example, a signal referred to the average angle of the blade pitch angle and an indicative value of wind turbine disorientation <p.
    In order to obtain a value of the lower limit of pitch angle J3min from said indicative value of the disorientation of the wind turbine cp, initially it is made use of calculations that allow obtaining a correlation defining the minimum pitch angle of rotation J3min that mark an input threshold at loss for each value of the signal indicative of wind speed. This correlation is modeled in the form of a lip and is implemented in the wind turbine control system to have the correlation between the limit characterized
    lower than the angle of pitch of the PMIN blade that marks a threshold of entry into loss and each
    value of the signal indicative of wind speed A. This allows to obtain for each value
    signal indicative of wind speed At lower limit value of blade pitch angle
    PMIN to avoid operation in aerodynamic loss zone.
    Additionally, the method described here presents an addition to the value of the lower limit of the blade pitch angle 3min of an additional term -3min to the value of the lower limit of the blade pitch angle 3min obtained from the comparison of the signal indicative of the wind speed curve or table comprising a correlation that defines the minimum blade pitch angle ¡3min that marks a threshold of loss input for each value of the signal indicative of the wind speed. The addition of the aforementioned additional term -3min is
    it cancels in the case in which it is determined that the wind direction is maintained, after a time has elapsed since there has been a rapid variation in the indicative value of the disorientation as a result of a rapid change in the wind direction.
    Alternatively, different time constants are applied in a filter for the estimation of a value of the blade tip velocity ratio, used as an indicative signal of the
    wind speed to obtain the lower limit of the pitch angle j3MIN.
    BRIEF DESCRIPTION OF THE FIGURES
    Figure 1. Shows a graph where the state of the art is detailed: in which a minimum stick pitch curve is illustrated as a function of wind speed. It can be seen that below the nominal wind speed there is a partial load zone, while above the nominal power there is a rotation speed regulation with the blade pitch angle.
    Figure 2. Shows a block diagram of the control system that allows implementing the method of the invention.
    Figure 3. Shows a graph showing the curves Cp power coefficient
    blade pitch angle 13; for different speed ratios of blade tip A.
    Figure 4. Shows a graph showing a curve (PMIN-Á) that defines the angle of
    PMIN minimum blade pitch that marks the loss input threshold for each value of
    blade tip speed ratio Á.
    5 Figure 5. Shows a graph showing a power curve as a function ofwind speed (below nominal wind speed partial production area,above nominal wind: nominal production zone or speed regulation ofrotation with the pitch angle of the blade.
    10 Figure 6. Shows a graph showing the resulting PMIN in an embodiment that
    includes adding an additional value ~ PMIN to the minimum limit defined by the curve that marks
    the pitch angle of the entry paddle in loss for each A. PMIN (i).
    Figure 7. Shows a diagram where a detail of the calculation block of the minimum limit of the blade pitch angle 15 is shown as a function of the disorientation according to a preferred embodiment. In this case, an additional term ~ PMIN is added to the minimum limit defined by the
    curve that marks the angle of pitch of the input blade in loss for each A PMIN (i).
    Figure 8. It shows a diagram of a detail of the calculation block of the lower limit value 20 of the pitch angle PMIN as a function of the disorientation according to an alternative embodiment in which the time constant of modifying is modified according to the disorientation filter t of the F1 filter applied to the measurement of the blade tip speed ratio "which
    allows obtaining a filtered signal Ame <! used to obtain ¡3MIN defined by the curve that marks the angle of the blade pitch! 3 of loss input for each value 25 of the blade tip speed ratio A.
    EXAMPLE OF PREFERRED EMBODIMENT OF THE INVENTION
    The wind turbine to which the control method object of the invention is intended
    30 comprises, a series of blades, and a blade pitch angle control system 3 like that seen in Figure 2. Said blade pitch control system allows implementing the control method object of the invention, in which, depending on a disorientation value cp of the wind turbine with respect to an incident wind direction,
    calculates a lower limit value of the pitch angle of the PMIN blade in a calculation block of
    35 lower limit of the blade pitch angle ¡3MIN. In view of said figure 2 it is appreciated that an initial setpoint of pitch angle pref can be calculated as the sum of the contributions of two PI type regulators, one using as input signal the rotor rotation speed error (OOrerWmed ) and the other one using as input the difference between the maximum torque and the torque calculated in the speed regulator with torque (Trated-Tmed) 'The
    5 Initial setpoint of Pref blade pitch is bounded upper and lower between upper and lower blade pitch angle limits (! 3MAX,! 3MIN) to obtain a final Pref final blade pitch setpoint to be sent to the blade pitch actuators. For the calculation of the lower limit value of the blade pitch angle! 3MIN, the control system uses as information at least one indicative value of disorientation ql of the generator.
    10 In this way and using the control system mentioned above or a similar one, we proceed to calculate:
    • An indicative value of disorientation <p of the wind turbine from at least one signal indicative of the wind direction.
    15 • An initial setpoint of blade pitch angle 13 as a function of at least one value related to a rotor speed error (oorerWmed) 'To subsequently proceed to modify at least one initial setpoint of blade pitch angle if this is less than the lower limit value of blade pitch angle! 3MIN. calculated from the indicative value of the disorientation <p, so that a fine setpoint l of passage
    20 blade is greater than or equal to the lower limit value of the pitch angle PMIN to subsequently act on at least one of the wind turbine blades depending on the setpoint value of the final blade pitch.
    In addition, the control method comprises calculating the lower limit value of the angle of
    25 blade step! 3MIN from the indicative value of the disorientation <p. In this way, the lower limit value of the blade pitch angle! 3MIN is adapted to the wind turbine orientation conditions, to prevent excessive lift losses and / or loads.
    30 In order to calculate the lower limit value of the minimum blade pitch angle! 3MIN, a comparison is made of a signal indicative of the wind speed with a curve or table comprising a correlation between the blade pitch angle minimum! 3MIN and the indicative wind speed signal which defines the minimum pitch angle PMIN that determines an input threshold in aerodynamic loss for each value
    35 of the signal indicative of wind speed. The data that give rise to the table or the curve can be obtained by simulating the points related to the coefficient of
    Cp power for each blade pitch angle j3 at different blade tip speeds.
    In a possible embodiment a blade tip speed ratio is used as a signal
    indicative of wind, although in other possible embodiments the indicative signal of wind speed can be taken from data of instantaneous wind speed, average wind speed or from data related to the average power or the average blade pitch angle . However, the use of the blade tip speed ratio "allows to take into account not only the effects of the wind speed on the rotor, but also the rotation effects of the rotor itself, as the influence of the rotor's rotation speed on the profile lift (measured through the power coefficient Cp) is substantial. The blade tip speed ratio "is determined from wind speed measurements that can be taken using wind data capture means such as y-anemometers Rotor speed and is calculated using the following formula, such as the ratio between the linear speed of the blade tip and the wind speed according to the formula:
    A = (linear velocity pl / n shovel) wind speed
    Figure 3 shows curves that illustrate the relationship between the coefficient of
    Cp power and blade pitch angle J3 for different speed ratio values of
    blade tip A, It is further appreciated that said curves have respective maximum values
    that mark a transition between two areas of operation:
    • A first zone or zone of normal operation, for which the wind turbine control is tuned.
    • A second zone or zone of aerodynamic loss entry for which the wind turbine control is invalid. That is why the wind turbine control incorporates the lower limit value of J3MIN blade pitch angle to avoid operation in the area of aerodynamic loss. Thus, if the calculation of the initial setpoint of blade pitch angle j3 as a function of the rotor rotation speed error.
    These curves do not take into account losses of support associated with an eventual
    deposition of particles on the surface of the blade that alter the geometry of the
    aerodynamic profiles or other effects that vary the lift of the blades, such as
    disorientation and its corresponding ip value.

    The maximum points of the curves that relate the power coefficient [Cp] to the blade pitch angle p for different values of blade tip speed A define pairs of points ¡3-A that are used to characterize a curve (PMIWA), which can be seen in Figure 4, which in turn defines the minimum blade pitch angle ¡3MIN that marks a threshold value of loss input for each blade tip speed ratio value A. Said The curve is modeled in an embodiment in the form of the aforementioned table and is implemented in the wind turbine control system to have the correlation between the minimum blade pitch angle 3MIN that marks a threshold of loss input and each value of the signal indicative of the wind speed A .. This allows to obtain for each value of the blade tip speed ratio A. the lower limit value of the blade pitch angle 3MIN to avoid operation in aero loss zone dynamic. In hypothetical value of lambda at the moment i (AMed (i)), the
    corresponding lower limit value of blade pitch angle (J3MIN (i)) as can be seen after displaying figure 4.
    As the table implemented in the wind turbine control system comprises a limited number of pairs of points, for those measures of blade tip speed ratio values A. which do not correspond to any of the points in the table, it is performed an interpolation process between at least two of them using conventional interpolation techniques, such as a linear interpolation.
    Since the signals related to the wind speed and rotor rotation speed measurements necessary to obtain the blade tip speed ratio "can have noise and produce undesirable effects such as fluctuations; the method described here envisages applying at least one F1 filter to any signal that requires it, as in this case to the signals related to the blade tip speed ratio J in order to perform a filtering process and smooth said signal over time and that these fluctuations in the measurements are not reflected in the lower limit value of the angle of
    J3MIN shovel pitch '
    Said filters can be of any type that allows to obtain the desired result, such as a low pass filter that allows the passage of lower frequencies and attenuates those higher frequencies and which also has a configurable time constant, or a filter based in a moving average whose calculation can be carried out with a number of points number that is configurable.

    In a preferred embodiment, the method comprises adding an additional term of minimum blade pitch angle / J. PMIN (which can be predetermined or dependent on the value of the disorientation <p) to the lower limit value of the pitch angle PMIN obtained from the comparison of the signal indicative of the blade tip speed ratio "with the cUlVa or predetermined table defining the minimum pitch angle of the PMIN blade in which the blade is not lost, as illustrated in Figures 6 and 7. Thus, when disorientation exists, the minimum limit value of pitch angle of blade PMIN is greater than when it does not exist, allowing a higher limit to be used to prevent the blade from evolving towards a blade pitch angle j3 lower than the wind speed required (note that
    due to disorientation, the wind component perpendicular to the rotor plane is smaller than when the wind turbine is oriented, so the blade pitch angle 3 tends to decrease to maintain the speed of rotation; however, the pitch angle f3 in these circumstances is less than that corresponding to the same speed of rotation with the wind turbine oriented correctly). This is particularly advantageous in the nominal production zone, or what is the same, the area in which there is rotor rotation speed regulation with the blade pitch angle 3.
    According to an embodiment like the one shown in Figure 8; The method comprises modifying a filtering time constant t when there is disorientation. Thus, in one embodiment, the filtering time constant t when there is disorientation t _Oororiented used in the filter F1 to calculate the filtered value of the blade tip speed ratio "," med, is different than the filtering time constant when there is no disorientation. In particular, preferably the value of the filtering time constant when there is a significant disorientation t_Oororientada is greater than the filtering time constant when there is no toriented, that is (t_ooriented> t_Orienting). This has the technical effect of having a slower variation of the filtered signal of "," med, for the same input signal when there is disorientation than when there is not, and therefore a slower, more temporal evolution of the value of the lower limit of pitch angle of PMIN blade in such circumstances. This is especially advantageous in the area of partial load operation, or what is the same, the area in which the rotation speed of the rotor is regulated with the electric torque of the generator. In this case, when the wind turbine is in the zone of speed regulation with torque, the pitch angle f3 is the one with the highest production (or highest bearing coefficient). In this case, if a gust of wind suddenly occurs, the lower limit value of the pitch angle PMIN will increase its value as the wind speed (or the blade tip speed ratio A) increases at a speed dependent on a first filtering constant faster than the setpoint of the blade pitch angle for rotor rotation speed control due to the speed error. This has the effect that, since the initial pitch blade setpoint j3 is less than the lower limit value of the blade pitch angle f3MIN, the final setpoint takes the lower limit value of the blade pitch angle! 3MIN. However, if at that time there is a change of orientation, it is convenient to reduce the extreme loads, reduce the speed of action of the blade pitch system for which it is proposed to reduce the time constant applied to calculate the ratio of blade tip speed A.
    Furthermore, in a possible embodiment, it is possible to modify the calculation of the lower limit value of the pitch angle PMIN only if it is determined that the value of the disorientation <p is above a predefined disorientation threshold value, by a comparison of the disorientation value tp of the wind turbine with the threshold.
    Thus, for example, in a possible embodiment in which it is determined or known that there is no disorientation or that the disorientation is below the predefined threshold value, the calculation of the lower limit value of the pitch angle J3MIN is performed at from a signal indicative of the wind speed, preferably the blade tip speed ratio "" and a predetermined curve that defines the minimum blade pitch angle! 3MIN that marks the input threshold at loss for each ratio value of blade tip speed "', without the addition of any additional term or modification of filtering time constant 1. However, when the disorientation is significant, the loss of lift or variation of the actual Cp is relevant and protection against possible new changes of wind direction should be protected; therefore, if it is determined that the disorientation exceeds the threshold value of disorientation, the modification is carried out said calculation of the lower limit value of the pitch angle J3MIN, either by adding an additional term of minimum pitch angle .6. PMIN (which can be predetermined or dependent on the value of the disorientation) or by modifying the filtering time constant 1 in the filter F1.
    When the wind turbine is operating in the nominal production zone according to figure 5, the blade pitch control system is regulating the rotation speed of the rotor and the wind turbine will be operating with positive blade pitch angles.
    In one embodiment, when the wind turbine is operating in said zone, if the wind turbine disorientation value exceeds the predefined threshold value, lower limit value of the pitch angle PMIN is calculated by adding a predetermined value OPMIN to the value of the lower limit of the pitch angle of the PMIN blade initially obtained from the comparison of the signal indicative of the wind speed with the predetermined curve or table that defines the minimum pitch angle of the PMIN blade at which the blade does not enter loss for each value of the signal indicative of the wind speed, as shown in figure 7. Thus, when the wind turbine is operating in the speed regulation zone with blade pitch, if a sudden disorientation due to a change in the wind direction, it prevents the blade pitch angle j3 from being reduced below a value greater than the minimum limit Mo of loss entry, as illustrated in Figure 6. In this production area it is convenient to use a lower limit value of the pitch angle J3MIN above the value of the limit marking the loss entry then, if the wind direction changes again and becomes similar to the previous direction. and the pitch angle of blade J3 has already dropped
    As a result of the reduction in aerodynamic torque caused by the transient disorientation of the wind turbine, the blade is in an area where you will see a higher load. Therefore it is convenient to avoid excessive loads and in the described way a reduction of fatigue loads is achieved in windy situations with frequent changes of direction in short intervals of time.
    In addition, the higher the orientation error, the wind turbine should be more protected against new changes of direction and gusts of wind, so in one embodiment, the sum value is increased with the orientation error from an error. minimum threshold
    Obtaining said additional minimum limit value ÓI3MIN is carried out by means of the calculation block of the control system that allows calculating, among other things, the lower limit value of the J3MIN blade pitch angle depending on the disorientation such as shown in figure 7. As explained, there are different scenarios for the calculation than the additional term ÓJ3MIN:
    • Comparison of the disorientation value with the predefined disorientation threshold value so that if it exceeds or is equal, OPMIN adopts a positive predetermined value and if it does not exceed it, OPMIN is equal to zero.
    • Assignment of an OPMIN value for each disorientation value from a table or function.
    • Combination of the two, comparison of the disorientation value with the predefined disorientation threshold value and assignment of an OPMIN value for each value of
    5 disorientation from a table or function when the disorientation value exceeds the threshold value and when it does not exceed it, OPMIN is equal to zero.
    If the wind direction is maintained after a predefined time interval or T from an abrupt change in the wind direction (which can be determined by comparing the rate of change of disorientation with respect to time), the limit value The lower pitch angle PMIN is recalculated only from the comparison of a signal indicative of the wind speed with a predetermined curve or table that defines the minimum pitch angle PMIN marking an input threshold at loss for each value of the signal indicative of wind speed. Or what is the same, after one or T after a sudden change in wind direction, OPMIN is canceled or "" [returns to the original value. This is because, if the wind orientation is sustained for a while, it is not advisable to maintain a lower limit value of the pitch angle PMIN too high, as it may not be adequate to the incident wind speed. It is a protective measure of the transient machine, until it is determined
    20 that the wind turbine is in a stable situation.
    权利要求:
    Claims (14)
    [1]
    1. Wind turbine control method comprising a series of blades, and a blade pitch angle control system, the method comprising the following steps:
    • calculate an indicative value of wind turbine disorientation from at least one signal indicative of the wind direction,
    • calculate an initial setpoint of blade pitch angle ¡3 based on at least one value related to a rotor speed error;
    • modify at least one initial setpoint of blade pitch angle 3 if it is less than a lower limit value of blade pitch angle 3MIN so that a final setpoint of blade pitch is greater than or equal to the value of the lower limit of the step angle of
    PMIN shovel; Y
    • act on at least one of the wind turbine blades based on the value ofsetpoint of final blade pitch;the method being characterized in that the lower limit value of blade pitch anglePMIN is calculated from at least the indicative value of the disorientation.
    [2]
    2. Method according to claim 1, characterized in that the calculation of the limit valueLower angle of pitch of PMIN blade comprises carrying out a comparison of asignal indicative of wind speed with a curve or table comprising a
    correlation between the minimum blade pitch angle ¡3MIN that marks a threshold of loss input and each value of the signal indicative of the wind speed.
    [3]
    3. Method according to claim 2, characterized in that the signal indicative of the wind speed comprises a blade tip speed ratio A, defined as the ratio between the linear speed of the blade tip and the wind speed:
    A = (linear velocity tip blade) ve / ocity wind '
    [4]
    Four. Method according to claim 3, characterized in that the signal indicative of the wind speed is a filtered measure of the blade tip speed ratio) obtained by applying an F1 filter to the blade tip speed ratio A.
    [5]
    5. Method according to claim 4 characterized in that the filter F1 comprises a
    time constant T that is configurable.
    [6]
    6. Method according to claim 4 characterized in that the filter F1 is a moving average.
    [7]
    7. Method according to claim 6 characterized in that it comprises calculating the moving average with a configurable number of points used.
    [8]
    8. Method according to claim 2, characterized in that the calculation of the value of the lower limit of pitch angle PMIN comprises the step of adding an additional term .ó.PMIN to the value of lower limit of pitch angle of blade PMIN obtained from the comparison of the signal indicative of the wind speed with the curve or table comprising the correlation between the minimum pitch angle PMIN that marks an input threshold in loss for each value of the signal indicative of the wind speed, when the existence of disorientation is determined from the indicative value of disorientation.
    [9]
    9. Method according to claim 8 characterized in that the additional term .ó.PMIN is predetermined.
    [10]
    10. Method according to claim 8 characterized in that the additional term .ó.PMIN is dependent on the wind turbine disorientation value.
    [11]
    eleven. Method according to claim 4, characterized in that the step of calculating the lower limit value of the pitch angle PMIN comprises a modification of a filtering time constant 1 "for the filter F1 applied to the blade tip speed ratio f. ..
    [12]
    12. Method according to claim 11 characterized in that it comprises comparing the indicative value of disorientation of the wind turbine with a predefined disorientation threshold value and because the modification of the filtering time constant 1 "for the filter F1 is related to the indicative value of disorientation of the wind turbine such that a filter time constant 1 "for the filter F1 is greater when the indicative value of disorientation of the wind turbine is greater than the threshold value of disorientation and less when the indicative value of disorientation of the wind turbine is less than the value disorientation threshold.
    [13]
    13. Method according to any one of claims 11 or 12 characterized in that the
    Modification of the filtering time constant t for the F1 filter applied to the blade tip speed ratio A is carried out in a partial production zone.
    Method according to any one of claims 11 or 12 wherein the indicative valueof wind turbine disorientation is greater than the disorientation threshold value,characterized in that it comprises modifying the filtering time constant t for the filterF1 applied to the blade tip speed ratio A.
    A method according to any one of claims 8 to 12 wherein the wind direction is maintained, characterized in that it comprises canceling OPMIN after a range of
    predefined time or T, which begins at a time a sharp change in orientation.
    [16]
    16. A method according to any one of claims 10 to 15 characterized in that, after a predefined time interval or T has elapsed since a sudden change in the disorientation, if the wind direction is maintained, the filtering time constant t of the
    F1 filter returns to its original value t.

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    同族专利:
    公开号 | 公开日
    TR201901285T4|2019-02-21|
    ES2538739B1|2016-04-14|
    EP2886854B1|2018-11-28|
    DK2886854T3|2019-03-04|
    ES2714085T3|2019-05-27|
    EP2886854A1|2015-06-24|
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    ES201331903A|ES2538739B1|2013-12-23|2013-12-23|Wind Turbine Control Method|ES201331903A| ES2538739B1|2013-12-23|2013-12-23|Wind Turbine Control Method|
    EP14200075.1A| EP2886854B1|2013-12-23|2014-12-23|Wind turbine control method|
    TR2019/01285T| TR201901285T4|2013-12-23|2014-12-23|Wind turbine control system.|
    ES14200075T| ES2714085T3|2013-12-23|2014-12-23|Wind Turbine Control Method|
    DK14200075.1T| DK2886854T3|2013-12-23|2014-12-23|Method for controlling wind turbine|
    US14/580,948| US20150176568A1|2013-12-23|2014-12-23|Wind Turbine Control Method|
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