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CN106150904B - A kind of wind driven generator unit yaw system control performance optimization method and system - Google Patents

A kind of wind driven generator unit yaw system control performance optimization method and system Download PDF

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CN106150904B
CN106150904B CN201610515518.8A CN201610515518A CN106150904B CN 106150904 B CN106150904 B CN 106150904B CN 201610515518 A CN201610515518 A CN 201610515518A CN 106150904 B CN106150904 B CN 106150904B
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wind
yaw
optimization
incoming
wind speed
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CN106150904A (en
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杨伟新
宋鹏
白恺
张扬帆
郑宇清
崔阳
刘喜梅
柳玉
杜军
任巍曦
邸帅
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State Grid Jibei Zhangjiakou Fengguang Storage And Transmission New Energy Co ltd
State Grid Corp of China SGCC
North China Electric Power Research Institute Co Ltd
State Grid Jibei Electric Power Co Ltd
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STATE GRID XINYUAN ZHANGJIAKOU SCENERY STORAGE DEMONSTRATION POWER PLANT CO Ltd
State Grid Corp of China SGCC
North China Electric Power Research Institute Co Ltd
State Grid Jibei Electric Power Co Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/0204Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for orientation in relation to wind direction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00Control
    • F05B2270/30Control parameters, e.g. input parameters
    • F05B2270/329Azimuth or yaw angle
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

本发明提供一种风力发电机组偏航系统控制性能优化方法及系统,方法包括:每隔固定时间间隔获取机舱前方的来流风数据,来流风数据包括来流风速、来流绝对风向及来流相对机舱的风向;将来流绝对风向按预定角度区间分扇区,将来流风速按预定风速区间分段;根据分扇区及分段对来流风数据进行第一次分组;根据来流相对机舱的风向计算对应组的偏航误差,得到偏航误差优化模型;偏航系统优化时,将实测的来流风速及来流绝对风向输入偏航误差优化模型,匹配对应的偏航误差,将该对应的偏航误差修正到偏航控制系统输入上。能够对不同型号的风力发电机组处于不同来流风速情况下采取不同的优化策略,提高了偏航误差的优化精度。

The present invention provides a method and system for optimizing the control performance of the yaw system of a wind power generating set. The wind direction of the engine room; the absolute wind direction of the future flow is divided into sectors according to the predetermined angle interval, and the wind speed of the future flow is divided into sections according to the predetermined wind speed interval; the first grouping of the incoming wind data is carried out according to the division of sectors and segments; according to the wind direction of the incoming flow relative to the engine room Calculate the yaw error of the corresponding group to obtain the yaw error optimization model; when optimizing the yaw system, input the measured wind speed and absolute wind direction of the incoming flow into the yaw error optimization model, match the corresponding yaw error, and use the corresponding The yaw error correction is applied to the yaw control system input. Different optimization strategies can be adopted for different types of wind turbines at different incoming wind speeds, which improves the optimization accuracy of yaw error.

Description

一种风力发电机组偏航系统控制性能优化方法及系统Method and system for optimizing control performance of yaw system of wind power generating set

技术领域technical field

本发明属于风电偏航控制领域,特别涉及一种风力发电机组偏航系统控制性能优化方法及系统。The invention belongs to the field of wind power yaw control, in particular to a method and system for optimizing the control performance of a yaw system of a wind power generating set.

背景技术Background technique

随着风电的大规模发展及检测手段和方法不断积累,厂家及风电场业主对风力发电机组的性能提出了更高的要求,偏航系统是水平轴风力发电机组控制系统的重要组成部分,其控制性能直接决定着风力发电机组的安全性和经济性。With the large-scale development of wind power and the continuous accumulation of detection methods and methods, manufacturers and wind farm owners have put forward higher requirements for the performance of wind turbines. The yaw system is an important part of the control system of horizontal axis wind turbines. Control performance directly determines the safety and economy of wind turbines.

现有技术中,偏航系统控制性能优化的一种方法是只要存有偏航偏差就启动偏航系统,这种优化方法存在动作频繁,降低偏航系统的使用寿命等缺陷。另现有技术的偏航系统性能优化方法,通常是对不同型号的风力发电机组、不同来流风速采取相同的优化策略,并不具有针对性,控制效果不理想、发电量提升低。In the prior art, one method of optimizing the control performance of the yaw system is to activate the yaw system as long as there is a yaw deviation. This optimization method has defects such as frequent actions and reduced service life of the yaw system. In addition, the performance optimization method of the yaw system in the prior art usually adopts the same optimization strategy for different types of wind turbines and different incoming wind speeds, which is not targeted, the control effect is not ideal, and the power generation increase is low.

发明内容Contents of the invention

本发明提供了一种风力发电机组偏航系统控制性能优化方法及系统,用于解决现有技术中频繁启动偏航系统降低相关设备的使用寿命,对不同型号的风力发电机组、不同来流风速采取相同的优化策略,并不具有针对性,控制效果不理想、发电量提升低的问题。The present invention provides a method and system for optimizing the control performance of the yaw system of a wind power generating set, which is used to solve the problem of reducing the service life of related equipment by frequently starting the yaw system in the prior art. Adopting the same optimization strategy is not targeted, the control effect is not ideal, and the power generation increase is low.

为了解决上述技术问题,本发明的一技术方案为提供一种风力发电机组偏航系统控制性能优化方法,包括:In order to solve the above technical problems, a technical solution of the present invention is to provide a method for optimizing the control performance of the yaw system of a wind turbine, including:

在预定时间段内,每隔固定时间间隔获取一待优化风力发电机组机舱前方的来流风数据,其中,来流风数据包括来流风速、来流绝对风向及来流相对机舱的风向;In a predetermined period of time, the incoming wind data in front of the nacelle of the wind power generating set to be optimized is obtained at regular intervals, wherein the incoming wind data includes the incoming wind speed, the absolute wind direction of the incoming flow, and the wind direction of the incoming flow relative to the nacelle;

将所述来流绝对风向按预定角度区间进行分扇区,将所述来流风速按预定风速区间进行分段;The absolute wind direction of the incoming flow is divided into sectors according to a predetermined angle interval, and the wind speed of the incoming flow is divided into sections according to a predetermined wind speed interval;

根据分扇区及分段对所述来流风数据进行第一次分组;Carrying out the first grouping of the incoming wind data according to sub-sectors and segments;

根据每组数据中所述来流相对机舱的风向计算对应组的偏航误差,得到偏航误差优化模型;Calculate the yaw error of the corresponding group according to the wind direction of the incoming flow relative to the nacelle described in each set of data, and obtain the yaw error optimization model;

所述待优化风力发电机组偏航系统优化时,将实测的来流风速及来流绝对风向输入所述偏航误差优化模型中,匹配对应的偏航误差,将该对应的偏航误差修正到所述偏航控制系统的输入上。When optimizing the yaw system of the wind power generating set to be optimized, input the measured incoming wind speed and incoming absolute wind direction into the yaw error optimization model, match the corresponding yaw error, and correct the corresponding yaw error to input to the yaw control system.

本发明另一技术方案为提供一种风力发电机组偏航系统控制性能优化系统,包括:Another technical solution of the present invention is to provide a control performance optimization system for a yaw system of a wind power generating set, including:

采样模块,用于在预定时间段内,每隔固定时间间隔获取一待优化风力发电机组机舱前方的来流风数据,其中,来流风数据包括来流风速、来流绝对风向及来流相对机舱的风向;The sampling module is used to obtain the incoming wind data in front of the nacelle of a wind power generating set to be optimized at regular time intervals within a predetermined period of time, wherein the incoming wind data includes the incoming wind speed, the absolute wind direction of the incoming flow, and the relative direction of the incoming flow relative to the nacelle. wind direction;

划分模块,用于将所述来流绝对风向按预定角度区间进行分扇区,将所述来流风速按预定风速区间进行分段;A dividing module, configured to divide the absolute wind direction of the incoming flow into sectors according to predetermined angle intervals, and divide the incoming wind speed into sections according to predetermined wind speed intervals;

第一分组模块,用于根据分扇区及分段对所述来流风数据进行第一次分组;The first grouping module is used to group the incoming wind data for the first time according to the sub-sectors and segments;

偏航误差优化模型计算模块,用于根据每组数据中所述来流相对机舱的风向计算对应组的偏航误差得到偏航误差的优化模型;The yaw error optimization model calculation module is used to calculate the yaw error of the corresponding group according to the wind direction of the incoming flow relative to the cabin described in each set of data to obtain an optimized model of the yaw error;

偏航误差优化模块,用于在所述待优化风力发电机组偏航系统优化时,将实测的来流风速及来流绝对风向输入所述偏航误差优化模型中,匹配对应的偏航误差,将该对应的偏航误差修正到所述偏航控制系统的输入上。The yaw error optimization module is used to input the measured incoming wind speed and incoming absolute wind direction into the yaw error optimization model to match the corresponding yaw error when optimizing the yaw system of the wind turbine to be optimized, The corresponding yaw error is corrected to the input of the yaw control system.

本发明能够对不同型号的风力发电机组处于不同来流风速情况下采取不同的优化策略,能够针对性的优化偏航系统的偏航误差,提高了偏航误差的优化精度,能够达到提升发电量的目的。The present invention can adopt different optimization strategies for different types of wind power generators at different incoming wind speeds, can optimize the yaw error of the yaw system in a targeted manner, improves the optimization accuracy of the yaw error, and can achieve an increase in power generation the goal of.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention. Those skilled in the art can also obtain other drawings based on these drawings without creative work.

图1为本发明一实施例的风力发电机组偏航系统控制性能优化方法的流程图;1 is a flow chart of a method for optimizing the control performance of a yaw system of a wind power generating set according to an embodiment of the present invention;

图2为本发明一实施例的计算偏航误差优化模型过程的流程图;Fig. 2 is the flow chart of calculating the yaw error optimization model process of an embodiment of the present invention;

图3为本发明一实施例的验证偏航误差优化模型是否有效的流程图;Fig. 3 is a flow chart of verifying whether the yaw error optimization model is valid according to an embodiment of the present invention;

图4为本发明另一实施例的风力发电机组偏航系统启动角优化的流程图;Fig. 4 is a flow chart of optimizing the start angle of the yaw system of the wind power generating set according to another embodiment of the present invention;

图5为本发明一实施例的风速段划分示意图;Fig. 5 is a schematic diagram of division of wind speed segments according to an embodiment of the present invention;

图6为本发明一实施例的验证启动角优化模型是否有效的流程图;Fig. 6 is a flow chart of verifying whether the starting angle optimization model is valid according to an embodiment of the present invention;

图7为本发明一实施例的风力发电机组偏航系统控制性能优化系统的结构图;Fig. 7 is a structural diagram of a control performance optimization system for a yaw system of a wind power generating set according to an embodiment of the present invention;

图8为本发明另一实施例的风力发电机组偏航系统控制性能优化系统的结构图。Fig. 8 is a structural diagram of a control performance optimization system for a yaw system of a wind power generating set according to another embodiment of the present invention.

具体实施方式Detailed ways

为了使本发明的技术特点及效果更加明显,下面结合附图对本发明的技术方案做进一步说明,本发明也可有其他不同的具体实例来加以说明或实施,任何本领域技术人员在权利要求范围内做的等同变换均属于本发明的保护范畴。In order to make the technical features and effects of the present invention more obvious, the technical solutions of the present invention will be further described below in conjunction with the accompanying drawings. The present invention can also be described or implemented in other different specific examples. The equivalent transformations done within all belong to the protection category of the present invention.

如图1所示,图1为本发明一实施例的风力发电机组偏航系统控制性能优化方法的流程图。本实施例可对不同型号的风力发电机组处于不同来流风速情况下采取不同的优化策略,能够针对性的优化偏航系统的偏航误差,提高了偏航误差的优化精度。As shown in FIG. 1 , FIG. 1 is a flowchart of a method for optimizing the control performance of a yaw system of a wind power generating set according to an embodiment of the present invention. In this embodiment, different optimization strategies can be adopted for different types of wind turbines at different incoming wind speeds, and the yaw error of the yaw system can be optimized in a targeted manner, improving the optimization accuracy of the yaw error.

具体的,风力发电机组偏航系统控制性能优化方法包括:Specifically, the method for optimizing the control performance of the wind turbine yaw system includes:

步骤101,在预定时间段内,每隔固定时间间隔获取一待优化风力发电机组机舱前方的来流风数据,其中,来流风数据包括来流风速、来流绝对风向及来流相对机舱的风向。Step 101, within a predetermined period of time, acquire the incoming wind data in front of the nacelle of a wind turbine to be optimized at regular intervals, wherein the incoming wind data includes incoming wind speed, incoming absolute wind direction, and incoming wind direction relative to the nacelle.

具体实施时,预定时间段如为30天。预定时间段还可根据优化精度而定,本发明对其具体取值不做限定。During specific implementation, the predetermined time period is, for example, 30 days. The predetermined time period may also be determined according to the optimization accuracy, and the present invention does not limit its specific value.

固定时间间隔如为10min。固定时间间隔可根据数据的稳定度而定,本发明对其具体取值不做限定。The fixed time interval is 10 minutes. The fixed time interval may be determined according to the stability of the data, and the present invention does not limit its specific value.

来流风数据中的各变量数据为固定时间间隔内采样(采样频率如为1s)获得的该变量瞬时值的平均值。进一步的,为了保证数据有用,来流风数据是在待优化风力发电机组正常运行状态下采集的,应将机组故障、检修等非正常状态下测得的数据剔除。The data of each variable in the incoming wind data is the average value of the instantaneous value of the variable obtained by sampling in a fixed time interval (for example, the sampling frequency is 1s). Furthermore, in order to ensure that the data is useful, the inflow wind data is collected under the normal operation state of the wind turbine to be optimized, and the data measured under abnormal conditions such as unit failure and maintenance should be eliminated.

详细的说,来流风速及来流相对机舱的风向是由安装于待优化风力发电机组机舱上的测风仪测得的,来流绝对风向是风力发电机组根据来流相对机舱的风向及机舱位置计算得到。In detail, the wind speed of the incoming flow and the wind direction of the incoming flow relative to the nacelle are measured by an anemometer installed on the nacelle of the wind turbine to be optimized. position is calculated.

步骤102,将所述来流绝对风向按预定角度区间进行分扇区,将所述来流风速按预定风速区间进行分段。Step 102, dividing the absolute wind direction of the incoming flow into sectors according to predetermined angle intervals, and dividing the incoming wind speed into sections according to predetermined wind speed intervals.

分扇区时,应尽可能减小扇区范围,使每个扇区受地形、障碍物等的影响相同,对于地形、障碍物情况特别复杂的机组,建议分组的角度范围应小于15°。预定角度可根据待优化风力发电机组所处地形、障碍物情况而定,本发明对预定角度的取值不做限定。When dividing sectors, the sector range should be reduced as much as possible so that each sector is affected equally by terrain and obstacles. For units with particularly complex terrain and obstacles, it is recommended that the grouping angle range should be less than 15°. The predetermined angle may be determined according to the terrain and obstacle conditions of the wind power generation unit to be optimized, and the present invention does not limit the value of the predetermined angle.

预定风速区间可为平均分配,如为6m/s。预定风速区间还可为低风速(启动风速-6m/s)、中风速(7m/s-额定风速)和高风速段(额定风速以上)。The predetermined wind speed range can be evenly distributed, such as 6m/s. The predetermined wind speed range can also be low wind speed (starting wind speed-6m/s), medium wind speed (7m/s-rated wind speed) and high wind speed section (above rated wind speed).

步骤103,根据分扇区及分风速对所述来流风数据进行第一次分组。分组后的数据可以以列表的形式存储。Step 103 , grouping the incoming wind data for the first time according to the sub-sectors and sub-wind speeds. Grouped data can be stored in the form of a list.

步骤104,根据每组数据中所述来流相对机舱的风向计算对应组的偏航误差,得到偏航误差优化模型。Step 104, calculate the yaw error of the corresponding group according to the wind direction of the incoming flow relative to the nacelle in each group of data, and obtain the yaw error optimization model.

该步骤得到的偏航误差为偏航系统受风向标(风力发电机组中的风向标)零位安装方位角、机舱风向标受叶轮尾流影响或控制策略有效性不足引起的综合误差。The yaw error obtained in this step is a comprehensive error caused by the yaw system being affected by the zero installation azimuth of the wind vane (the wind vane in the wind turbine), the wind vane in the nacelle being affected by the wake of the impeller, or the effectiveness of the control strategy is insufficient.

具体的,如图2所示,步骤104的详细过程为:Specifically, as shown in Figure 2, the detailed process of step 104 is:

步骤1041:统计每组中各来流相对机舱的风向出现的概率,按概率从大到小的顺序对每组中的来流相对机舱的风向进行排序。Step 1041: Count the occurrence probability of the wind directions of the incoming flows relative to the nacelle in each group, and sort the wind directions of the incoming flows relative to the nacelle in each group in descending order of probability.

步骤1042:计算每组前N个来流相对机舱的风向的平均值得到对应组的偏航误差。Step 1042: Calculate the average value of the wind direction of the first N incoming streams relative to the nacelle in each group to obtain the yaw error of the corresponding group.

步骤1043:将每组对应的偏航误差汇总到一起得到所述偏航误差优化模型。Step 1043: Summarize the corresponding yaw errors of each group to obtain the yaw error optimization model.

步骤105,在所述待优化风力发电机组偏航系统优化时,将实测的来流风速及来流绝对风向输入所述偏航误差优化模型中,匹配该实测的来流风速及来流绝对风向对应的偏航误差,将该对应的偏航误差修正到所述偏航控制系统的输入上。Step 105, when optimizing the yaw system of the wind turbine to be optimized, input the measured incoming wind speed and incoming absolute wind direction into the yaw error optimization model, and match the measured incoming wind speed and incoming absolute wind direction The corresponding yaw error is corrected to the input of the yaw control system.

本实施采用综合偏航误差的方式,在不考虑引起偏航误差的具体原因的情况下,直接进行补偿,提高了偏航优化的可执行性和降低其不确定性。This implementation adopts the method of comprehensive yaw error, and directly compensates without considering the specific cause of yaw error, which improves the feasibility of yaw optimization and reduces its uncertainty.

为了将一待优化的风力发电机组的偏航误差优化模型扩展到其他同型号的待优化风力发电机组,本发明一实施例中,得到偏航误差优化模型后还包括:In order to extend the yaw error optimization model of a wind power generation unit to be optimized to other wind power generation units of the same type to be optimized, in an embodiment of the present invention, after obtaining the yaw error optimization model, it also includes:

确定所述待优化风力发电机组的有效扇区;当另一风力发电机组的叶片法线(即机舱中心线)在有效扇区时,将所述偏航误差优化模型适用于所述另一风力发电机组,可根据偏航误差优化模型对所述另一风力发电机组进行偏航误差优化;其中,所述另一发电机组与所述待优化风力发电机组型号相同。Determine the effective sector of the wind power generating set to be optimized; when the blade normal (i.e. the centerline of the nacelle) of another wind generating set is in the effective sector, apply the yaw error optimization model to the other wind power The generating set may perform yaw error optimization on the other wind generating set according to the yaw error optimization model; wherein, the another generating set is of the same type as the wind generating set to be optimized.

实施时,待优化风力发电机组的有效扇区可通过现有技术实现,此处不再赘述。During implementation, the effective sector of the wind power generating set to be optimized can be realized through existing technologies, and will not be repeated here.

为了验证偏航误差优化的准确性,本发明一实施例中,如图3所示,通过如下方法验证偏航误差优化模型是否有效:In order to verify the accuracy of yaw error optimization, in one embodiment of the present invention, as shown in Figure 3, the following method is used to verify whether the yaw error optimization model is valid:

步骤301:待优化风力发电机组的偏航系统在优化前还包括统计优化前的功率特性曲线保证率。Step 301 : The yaw system of the wind power generating set to be optimized also includes the guarantee rate of the power characteristic curve before optimization.

步骤302:所述偏航系统优化后还包括统计优化后的功率特性曲线保证率。Step 302: After the yaw system is optimized, it also includes statistically optimized power characteristic curve guarantee rate.

所述功率特性曲线保证率通过如下公式计算:The guarantee rate of the power characteristic curve is calculated by the following formula:

K:风力发电机组的功率特性保证率;K: Guarantee rate of power characteristics of the wind turbine;

n:统计区间个数,按照风速范围为0.5m/s为一个统计区间,区间的中心为0.5m/s的整数倍;n: the number of statistical intervals, according to the wind speed range of 0.5m/s as a statistical interval, the center of the interval is an integer multiple of 0.5m/s;

Pi:风力发电机组处于有功功率为最大输出控制模式下,第i个统计区间内风机实际输出的平均有功功率值,单位为kW;P i : The average active power value actually output by the fan in the i-th statistical interval when the wind turbine is in the control mode of maximum active power output, the unit is kW;

Pi':标准大气密度条件下,厂家保证的对应第i个统计区间内的有功功率,单位为kW;P i ': Under standard atmospheric density conditions, the manufacturer guarantees the active power corresponding to the i-th statistical interval, in kW;

第i个统计区间的频率; The frequency of the i-th statistical interval;

Ni:风速落入第i个统计区间的数据个数;N i : the number of data whose wind speed falls into the i-th statistical interval;

N:风速数据的总数量。N: total number of wind speed data.

步骤303:比较优化后的功率特性曲线保证率与优化前的功率特性曲线保证率,如果优化后的功率特性曲线保证率大于优化前的功率特性曲线保证率,则所述偏航误差优化模型有效。Step 303: Comparing the guaranteed rate of the optimized power characteristic curve with the guaranteed rate of the power characteristic curve before optimization, if the guaranteed rate of the optimized power characteristic curve is greater than the guaranteed rate of the power characteristic curve before optimization, the yaw error optimization model is valid .

若优化后功率特性曲线保证率小于优化前功率特性曲线保证率,则需重新优化偏航误差,并对风力发电机组的转速进行频率分析,使得转速在偏航误差补偿前后控制平稳,避免出现较大的转速抖动和机组的异常振动。If the power characteristic curve guarantee rate after optimization is lower than the power characteristic curve guarantee rate before optimization, it is necessary to re-optimize the yaw error and perform frequency analysis on the speed of the wind turbine to make the speed control stable before and after yaw error compensation and avoid the occurrence of large Large speed jitter and abnormal vibration of the unit.

本发明一实施例中,还可通过比较优化前的功率特征曲线及优化后的功率特征曲线,当功率特征曲线整体向右偏移,则偏航误差优化模型有效。具体的,待优化机组的功率特征曲线可采用现有方法得到,如在获取所述待优化风力发电机组机舱前方的来流风数据的同时还获取环境温度、气压和待优化机组输出的电功率,结合来流风数据统计待优化机组的功率特性曲线。In an embodiment of the present invention, by comparing the power characteristic curve before optimization and the power characteristic curve after optimization, when the overall power characteristic curve shifts to the right, the yaw error optimization model is valid. Specifically, the power characteristic curve of the unit to be optimized can be obtained by using existing methods, for example, while obtaining the data of the incoming wind in front of the nacelle of the wind turbine unit to be optimized, the ambient temperature, air pressure and the electric power output by the unit to be optimized are also obtained, combined with The power characteristic curve of the unit to be optimized is counted by the incoming wind data.

本发明一实施例中,如图4所示,风力发电机组偏航系统控制性能优化方法还包括:In an embodiment of the present invention, as shown in FIG. 4, the method for optimizing the control performance of the yaw system of the wind power generating set further includes:

步骤401:按低风速段、中风速段及高风速段对来流数据进行第二次分组;其中,低风速范围为V0<V≤V1,中风速范围为V1<V≤V2,高风速范围为V>V2,V2为额定风速,V0为启动风速,V1为低风速段阈值,如为6m/s,V为来流风速。Step 401: Group the inflow data for the second time according to the low wind speed segment, the medium wind speed segment and the high wind speed segment; wherein, the range of low wind speed is V 0 <V ≤ V 1 , and the range of medium wind speed is V 1 <V ≤ V 2 , the high wind speed range is V>V 2 , V 2 is the rated wind speed, V 0 is the start-up wind speed, V 1 is the low wind speed threshold, such as 6m/s, and V is the incoming wind speed.

具体的,高、中、低风速段的分段依据可根据机组的不同运行特性、偏航的不同控制策略或桨距角、机组转速统计分析进行分段。如图5所示,根据叶轮转速和桨距角在机组不同运行阶段下的不同特点进行分段的事例,第一段为“叶片转速升高、桨距角不变”阶段,第二段为“叶轮转速和桨距角变化的临界”阶段,第三段为“叶轮转速不变,桨距角升高”阶段。根据图5所示分段,确定各分段临界点的风速,从而得到V1及V2Specifically, the segmentation basis for the high, medium, and low wind speed segments can be segmented according to different operating characteristics of the units, different control strategies for yaw or pitch angle, and statistical analysis of the unit speed. As shown in Figure 5, an example of segmenting according to the different characteristics of the impeller speed and pitch angle in different operating stages of the unit, the first segment is the stage of "the blade speed increases and the pitch angle remains unchanged", and the second segment is The stage of "the critical change of impeller speed and pitch angle", and the third stage is the stage of "the impeller speed is constant and the pitch angle increases". According to the segments shown in Figure 5, determine the wind speed at the critical point of each segment, so as to obtain V 1 and V 2 .

步骤402:对第二次分组的每组设定不同的偏航启动角优化准则,得到启动角优化模型。Step 402: Set different yaw start angle optimization criteria for each group of the second grouping to obtain a start angle optimization model.

如启动角优化准则为:For example, the starting angle optimization criterion is:

低风速启动角的优化准则为Dl±Cl,其中,Dl为低风速偏航启动角,Cl为调整量;The optimization criterion of the low wind speed starting angle is D l ± C l , where D l is the low wind speed yaw starting angle, and C l is the adjustment value;

中风速启动角的优化准则为Dm-Cm,其中,Dm为中风速偏航启动角,Cm为调整量;The optimization criterion of the start angle at medium wind speed is D m -C m , where D m is the yaw start angle at medium wind speed, and C m is the adjustment value;

高风速启动角的优化准则为Dh±Ch,其中,Dh为高风速偏航启动角,Ch为调整量。The optimization criterion for the high wind speed starting angle is D h ±C h , where D h is the high wind speed yaw starting angle, and C h is the adjustment value.

实施时,还可根据优化精度调整优化准则,本发明对优化准则不做具体限定。During implementation, the optimization criterion can also be adjusted according to the optimization accuracy, and the present invention does not specifically limit the optimization criterion.

步骤403:所述偏航系统优化时,将所述实测的来流风速输入所述启动角优化模型中,得到所述实测的来流风速对应的偏航启动角,待实测的来流相对机舱的风向达到所述对应的偏航启动角时,启动所述偏航系统动作。Step 403: When optimizing the yaw system, input the measured incoming wind speed into the starting angle optimization model to obtain the yaw starting angle corresponding to the measured incoming wind speed. When the wind direction reaches the corresponding yaw start angle, the yaw system action is started.

为了验证启动角优化的准确性,本发明一实施例中,如图6所示,通过如下方法验证启动角优化模型是否有效:In order to verify the accuracy of the starting angle optimization, in one embodiment of the present invention, as shown in Figure 6, the following method is used to verify whether the starting angle optimization model is valid:

步骤601:所述偏航系统优化前还包括统计优化前的功率特性曲线保证率,利用包络法或概率分布法对获取的来流相对机舱的风向及来流风速进行统计分析,得到优化前控制死区长度。Step 601: Before the optimization of the yaw system, it also includes statistical analysis of the power characteristic curve guarantee rate before optimization, using the envelope method or probability distribution method to statistically analyze the obtained wind direction and incoming wind speed of the incoming flow relative to the nacelle, and obtain Controls the deadband length.

具体的,包络法计算控制死区的过程为:设定来流风速为横坐标,来流相对机舱的风向为纵坐标,将来风数据按照来风速度的大小进行排练,利用包络法将统计的来流相对机舱的数据边缘进行包络,上包络减去下包络即得到控制死区长度。Specifically, the process of calculating the control dead zone by the envelope method is as follows: set the wind speed of the incoming flow as the abscissa, and the wind direction of the incoming flow relative to the nacelle as the vertical coordinate. The statistical incoming flow is enveloped relative to the data edge of the cabin, and the upper envelope is subtracted from the lower envelope to obtain the length of the control dead zone.

概率分布法计算控制死区的过程为:按照风速从小到大的顺序划分区间段,将需要计算的来流相对机舱的风向分配到风速各区间中计算,针对每个风速区间段,分别计算各相对机舱的风向出现的概率,然后以出现概率最高的相对机舱的风向为中心向左右进行递推形式风向区间,并计算风向区间的概率,当风向区间概率大于固定概率时,如为95%时,此风向区间差值即为控制死区长度。The process of calculating the control dead zone by the probability distribution method is as follows: divide the intervals according to the order of wind speed from small to large, assign the wind direction of the incoming flow relative to the engine room to be calculated in each wind speed interval, and calculate each wind speed interval for each wind speed interval. The probability of occurrence of the wind direction relative to the engine room, and then recursively form the wind direction interval around the wind direction with the highest probability of occurrence relative to the engine room, and calculate the probability of the wind direction interval. When the probability of the wind direction interval is greater than the fixed probability, such as 95% , the wind direction interval difference is the length of the control dead zone.

步骤602:所述偏航系统优化期间还包括统计所述待优化风力发电机组及一标杆风机的偏航控制次数,所述标杆风机为所述待优化风力发电机组周围任意一风力发电机组。Step 602: The yaw system optimization period also includes counting the yaw control times of the wind turbine to be optimized and a benchmark wind turbine, the benchmark wind being any wind turbine around the wind turbine to be optimized.

步骤603:所述偏航系统优化后还包括统计优化后的功率特性曲线保证率,统计第二次分风速段优化后的控制死区长度。Step 603: After the yaw system is optimized, it also includes statistics of the optimized power characteristic curve guarantee rate, and statistics of the length of the control dead zone after the second wind speed section optimization.

控制死区的计算方法参见步骤601,此处不再赘述。For the calculation method of the control dead zone, refer to step 601, which will not be repeated here.

步骤604:将优化后的控制死区长度分别与优化前控制死区长度比较,将优化后的功率特性曲线保证率与优化前的功率特性曲线保证率比较,将所述待优化风力发电机组的偏航控制次数与所述标杆风机的偏航控制次数比较。Step 604: Compare the length of the optimized control dead zone with the length of the control dead zone before optimization, compare the guaranteed rate of the power characteristic curve after optimization with the guaranteed rate of the power characteristic curve before optimization, and compare the guaranteed rate of the wind power generating set to be optimized The yaw control times are compared with the yaw control times of the benchmark fan.

步骤605:如果低风速段优化后的控制死区长度与优化前的控制死区长度差值小于第一预定阈值,中风速段优化后的控制死区长度小于优化前的控制死区长度,高风速段优化后的控制死区长度与优化前的控制死区长度差值小于第二预定阈值;优化后的功率特性曲线保证率大于或等于优化前的功率特性曲线保证率;所述待优化风力发电机组的偏航控制次数小于或等于所述标杆机组的偏航控制次数,则启动角优化模型有效。Step 605: If the difference between the optimized control dead zone length in the low wind speed section and the control dead zone length before optimization is less than the first predetermined threshold, the optimized control dead zone length in the medium wind speed section is smaller than the control dead zone length before optimization, and the high The difference between the optimized control dead zone length of the wind speed segment and the control dead zone length before optimization is less than the second predetermined threshold; the optimized power characteristic curve guarantee rate is greater than or equal to the power characteristic curve guarantee rate before optimization; the wind force to be optimized If the yaw control times of the generator set are less than or equal to the yaw control times of the benchmark unit, the start angle optimization model is valid.

具体实施时,第一预定阈值及第二预定阈值可根据机组具体确定。高风速段启动角优化时还要关注机组是否产生异常振动现象,所设定的第二预定阈值需能保证机组不出现异常振动。During specific implementation, the first predetermined threshold and the second predetermined threshold may be specifically determined according to the unit. When optimizing the start-up angle in the high wind speed section, it is necessary to pay attention to whether the unit generates abnormal vibration, and the second predetermined threshold must be able to ensure that the unit does not experience abnormal vibration.

本发明能够对运行风力发电机组偏航控制的偏航误差、启动角进行个性优化,在提高偏航系统可靠性的同时改善机组的功率特性曲线,提高机组的发电量。The invention can individually optimize the yaw error and starting angle of the yaw control of the running wind power generating set, improve the reliability of the yaw system, improve the power characteristic curve of the set, and increase the generating capacity of the set.

如图7所示,图7为本发明一实施例风力发电机组偏航系统控制性能优化系统的结构图。具体的,该系统700包括:As shown in FIG. 7 , FIG. 7 is a structural diagram of a control performance optimization system for a yaw system of a wind power generating set according to an embodiment of the present invention. Specifically, the system 700 includes:

采样模块701,用于在预定时间段内,每隔固定时间间隔获取一待优化风力发电机组机舱前方的来流风数据,其中,来流风数据包括来流风速、来流绝对风向及来流相对机舱的风向。The sampling module 701 is used to acquire the incoming wind data in front of the nacelle of a wind power generating set to be optimized at regular time intervals within a predetermined period of time, wherein the incoming wind data includes the incoming wind speed, the absolute wind direction of the incoming flow, and the incoming flow relative to the nacelle wind direction.

划分模块702,用于将所述来流绝对风向按预定角度区间进行分扇区,将所述来流风速按预定风速区间进行分段。The dividing module 702 is configured to divide the absolute wind direction of the incoming flow into sectors according to predetermined angle intervals, and divide the incoming wind speed into sections according to predetermined wind speed intervals.

第一分组模块703,用于根据分扇区及分段对所述来流风数据进行第一次分组。The first grouping module 703 is configured to perform a first grouping of the incoming wind data according to sectors and segments.

偏航误差优化模型计算模块704,用于根据每组数据中所述来流相对机舱的风向计算对应组的偏航误差得到偏航误差优化模型。The yaw error optimization model calculation module 704 is configured to calculate the corresponding set of yaw errors according to the wind direction of the incoming flow relative to the nacelle in each set of data to obtain a yaw error optimization model.

偏航误差优化模块705,用于在所述待优化风力发电机组偏航系统优化时,将实测的来流风速及来流绝对风向输入所述偏航误差优化模型中,匹配对应的偏航误差,将该对应的偏航误差修正到所述偏航控制系统的输入上。The yaw error optimization module 705 is used to input the measured incoming wind speed and incoming absolute wind direction into the yaw error optimization model to match the corresponding yaw error when optimizing the yaw system of the wind turbine to be optimized , correcting the corresponding yaw error to the input of the yaw control system.

本发明另一实施例中,如图8所述,所述系统还包括,In another embodiment of the present invention, as shown in FIG. 8, the system further includes:

第二分组模块706,用于按低风速段、中风速段及高风速段对来流数据进行第二次分组;其中,低风速范围为V0<V≤V1,中风速范围为V1<V≤V2,高风速范围为V>V2,V2为额定风速,V0为启动风速,V1为低风速段阈值,如为6m/s,V为来流风速。启动角优化模型计算模块707,用于对第二次分组的每组设定不同的偏航启动角优化准则,得到启动角优化模型;The second grouping module 706 is used to group the incoming flow data for the second time according to the low wind speed segment, the medium wind speed segment and the high wind speed segment; wherein, the range of low wind speed is V 0 <V ≤ V 1 , and the range of medium wind speed is V 1 <V≤V 2 , the high wind speed range is V>V 2 , V 2 is the rated wind speed, V 0 is the start-up wind speed, V 1 is the threshold of the low wind speed section, such as 6m/s, and V is the incoming wind speed. The starting angle optimization model calculation module 707 is used to set different yaw starting angle optimization criteria for each group of the second grouping to obtain the starting angle optimization model;

启动角优化模块708,用于所述偏航系统优化时,将所述实测的来流风速输入所述启动角优化模型中,得到所述实测的来流风速对应的偏航启动角,待实测的来流相对机舱的风向达到所述对应的偏航启动角时,启动所述偏航系统动作。The starting angle optimization module 708 is used for the optimization of the yaw system, inputting the measured incoming wind speed into the starting angle optimization model to obtain the yaw starting angle corresponding to the measured incoming wind speed, to be measured When the wind direction of the incoming flow relative to the nacelle reaches the corresponding yaw start angle, the yaw system action is started.

本发明能够对不同型号的风力发电机组处于不同来流风速情况下采取不同的优化策略,能够对运行风力发电机组偏航控制的偏航误差、偏航启动角进行个性优化,提高了偏航误差及启动角的优化精度,在提高偏航系统可靠性的同时改善机组的功率特性曲线,提高机组的发电量。The present invention can adopt different optimization strategies for different types of wind power generators at different incoming wind speeds, can perform individual optimization on the yaw error and yaw start angle of the yaw control of the running wind power generators, and improve the yaw error And the optimization accuracy of the starting angle, improve the power characteristic curve of the unit while improving the reliability of the yaw system, and increase the power generation of the unit.

以上所述仅用于说明本申请的技术方案,任何本领域普通技术人员均可在不违背本发明的精神及范畴下,对上述实施例进行修饰与改变。因此,本发明的权利保护范围应视权利要求范围为准。The above description is only used to illustrate the technical solution of the present application, and anyone skilled in the art can modify and change the above embodiments without departing from the spirit and scope of the present invention. Therefore, the protection scope of the present invention should be determined by the scope of the claims.

Claims (9)

1. a kind of wind driven generator unit yaw system control performance optimization method, which is characterized in that including,
Within a predetermined period of time, the incoming wind number in front of a wind generating set engine room to be optimized is obtained every Fixed Time Interval According to, wherein incoming wind data includes the wind direction of arrives stream wind speed, incoming true wind direction and incoming with respect to cabin;
By the incoming true wind direction, section carries out a point sector by a predetermined angle, by the arrives stream wind speed by predetermined wind speed interval into Row segmentation;
First time grouping is carried out to the incoming wind data according to sector and segmentation is divided;
The yaw error for calculating corresponding group with respect to the wind direction of cabin according to incoming described in every group of data, obtains yaw error optimization Model;
When the wind driven generator unit yaw system optimization to be optimized, the arrives stream wind speed of actual measurement and incoming true wind direction are inputted into institute It states in yaw error Optimized model, matches corresponding yaw error, which is adapted to the wind to be optimized In the input of power generator group yaw system;
Wherein, the yaw error for calculating corresponding group with respect to the wind direction of cabin according to incoming described in every group of data obtains yaw and misses Poor Optimized model includes:
Each incoming in every group is counted with respect to the probability that the wind direction of cabin occurs, by the sequence of probability from big to small to coming in every group The wind direction of the opposite cabin of stream is ranked up;
It calculates every group of top n incoming and is worth to the yaw error of corresponding group with respect to being averaged for the wind direction of cabin;
Every group of corresponding yaw error is gathered to obtain the yaw error Optimized model.
2. wind driven generator unit yaw system control performance optimization method as described in claim 1, which is characterized in that described next Flow the average value that each variable data in wind data is the variable instantaneous value that sampling obtains in Fixed Time Interval.
3. wind driven generator unit yaw system control performance optimization method as described in claim 1, which is characterized in that obtain institute Further include after stating yaw error Optimized model:
Determine effective sector of the wind power generating set to be optimized;
When the blade normal of another wind power generating set is in effective sector, the yaw error Optimized model is suitable for described Another wind power generating set;
Wherein, another generating set is identical as the wind power generating set model to be optimized.
4. wind driven generator unit yaw system control performance optimization method as described in claim 1, which is characterized in that described inclined It further include the power characteristic fraction before statistic op- timization before boat system optimization;
It further include the power characteristic fraction after statistic op- timization after the yaw system optimization;
Compare the power characteristic fraction after optimization and the power characteristic fraction before optimization, if the work(after optimization Rate characteristic curve fraction is more than the power characteristic fraction before optimization, then the yaw error Optimized model is effective.
5. wind driven generator unit yaw system control performance optimization method as described in claim 1, which is characterized in that the side Method further includes:
By low wind speed section, middle wind speed section and high wind speed section second of grouping is carried out to carrying out flow data;
Wherein, low wind speed range is V0< V≤V1, middle wind speed ranging from V1< V≤V2, high wind speed ranging from V > V2, V2It is specified Wind speed, V0For threshold wind velocity, V1For low wind speed section threshold value, V is arrives stream wind speed;
The yaws different to every group of setting of second of grouping start angle and optimizing criterion, obtain starting angle and optimizing model;
When the yaw system optimization, the arrives stream wind speed of the actual measurement is inputted in the startup angle and optimizing model, is obtained described The corresponding yaw of arrives stream wind speed of actual measurement starts angle, and incoming to be surveyed reaches the corresponding yaw with respect to the wind direction of cabin and opens When dynamic angle, start the yaw system action.
6. wind driven generator unit yaw system control performance optimization method as claimed in claim 5, which is characterized in that described to open Moving angle and optimizing criterion is:
The Optimality Criteria that low wind speed starts angle is Dl±Cl, wherein DlIt is yawed for low wind speed and starts angle, ClFor adjustment amount;
The Optimality Criteria that middle wind speed starts angle is Dm-Cm, wherein DmIt is yawed for middle wind speed and starts angle, CmFor adjustment amount;
The Optimality Criteria that high wind speed starts angle is Dh±Ch, wherein DhIt is yawed for high wind speed and starts angle, ChFor adjustment amount.
7. wind driven generator unit yaw system control performance optimization method as claimed in claim 6, which is characterized in that described inclined Further include the power characteristic fraction before statistic op- timization before boat system optimization, using envelope method or probability distribution method to obtaining Incoming it is for statistical analysis with respect to the wind direction of cabin and arrives stream wind speed, controlling dead error length before obtaining optimizing;
It further include the yaw control of the statistics wind power generating set to be optimized and a mark post wind turbine during the yaw system optimization Number processed, the mark post wind turbine are the wind power generating set around the wind power generating set to be optimized;
Further include the power characteristic fraction after statistic op- timization, second of grouping gained of statistics after the yaw system optimization Controlling dead error length after the optimization of wind speed section;
By the controlling dead error length after optimization respectively compared with controlling dead error length before optimization, by the power characteristic after optimization Fraction controls number compared with the power characteristic fraction before optimization, by the yaw of the wind power generating set to be optimized Compared with the yaw of mark post wind turbine control number;
If the controlling dead error length after low wind speed section optimization is less than the first predetermined threshold with the controlling dead error length difference before optimization Value, the controlling dead error length after middle wind speed section optimization are less than the controlling dead error length before optimization, the control after the optimization of high wind speed section Dead zone length is less than the second predetermined threshold with the controlling dead error length difference before optimization;Power characteristic fraction after optimization More than or equal to the power characteristic fraction before optimization;The yaw control number of the wind power generating set to be optimized is less than Or the yaw equal to the mark post unit controls number, then it is effective to start angle and optimizing model.
8. the wind driven generator unit yaw system control performance optimization method as described in claim 4 or 7, which is characterized in that institute Power characteristic fraction is stated to calculate by following formula:
K:The power characteristic fraction of wind power generating set;
n:Section number is counted, according to wind speed range be 0.5m/s is a statistics section, the center in section is the whole of 0.5m/s Several times;
Pi:It is under maximum output control model that wind power generating set, which is in active power, and i-th of statistics section inner blower is actually defeated The average active power value gone out, unit kW;
Pi':Under normal atmosphere density conditions, the active power in i-th of statistics section of correspondence that producer ensures, unit kW;
The frequency in i-th of statistics section;
Ni:Wind speed falls into the data amount check in i-th of statistics section;
N:The total quantity of air speed data.
9. a kind of wind driven generator unit yaw system control performance optimization system, which is characterized in that the system comprises:
Sampling module, within a predetermined period of time, a wind generating set engine room to be optimized being obtained every Fixed Time Interval The incoming wind data in front, wherein incoming wind data includes the wind of arrives stream wind speed, incoming true wind direction and incoming with respect to cabin To;
Division module presses the arrives stream wind speed for by the incoming true wind direction, section to carry out a point sector by a predetermined angle Predetermined wind speed interval is segmented;
First grouping module divides sector and segmentation to carry out first time grouping to the incoming wind data for basis;
Yaw error seismic responses calculated module is corresponded to for being calculated with respect to the wind direction of cabin according to incoming described in every group of data The yaw error of group obtains yaw error Optimized model;
Yaw error optimization module is used in the wind driven generator unit yaw system optimization to be optimized, by the incoming of actual measurement Wind speed and incoming true wind direction input in the yaw error Optimized model, match corresponding yaw error, this is corresponding partially In error correction to the input of the wind driven generator unit yaw system to be optimized of navigating;
Wherein, the yaw error for calculating corresponding group with respect to the wind direction of cabin according to incoming described in every group of data obtains yaw and misses Poor Optimized model includes:
Each incoming in every group is counted with respect to the probability that the wind direction of cabin occurs, by the sequence of probability from big to small to coming in every group The wind direction of the opposite cabin of stream is ranked up;
It calculates every group of top n incoming and is worth to the yaw error of corresponding group with respect to being averaged for the wind direction of cabin;
Every group of corresponding yaw error is gathered to obtain the yaw error Optimized model.
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WO2020097944A1 (en) 2018-11-18 2020-05-22 浙江大学 Real power curve-based method for discriminating and compensating yaw error inherent deviation of wind turbine generator set
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CN110886681B (en) * 2019-12-13 2021-04-27 北京三力新能科技有限公司 Yaw angle positioning control method based on time partition and yaw sector
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CN112031997B (en) * 2020-09-15 2021-08-13 华北电力科学研究院有限责任公司 Method and device for determining yaw static deviation of wind turbine
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2762721A2 (en) * 2013-02-01 2014-08-06 General Electric Company Method and apparatus for wind turbine noise reduction
CN104948384A (en) * 2015-06-16 2015-09-30 新疆金风科技股份有限公司 Calibration method and system for yaw angles of wind generating set
EP2927484A1 (en) * 2014-03-31 2015-10-07 ALSTOM Renewable Technologies Yaw and pitch angles
CN105257470A (en) * 2015-09-25 2016-01-20 南车株洲电力机车研究所有限公司 Wind direction compensation optimization method and device for wind turbine generator set

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2762721A2 (en) * 2013-02-01 2014-08-06 General Electric Company Method and apparatus for wind turbine noise reduction
EP2927484A1 (en) * 2014-03-31 2015-10-07 ALSTOM Renewable Technologies Yaw and pitch angles
CN104948384A (en) * 2015-06-16 2015-09-30 新疆金风科技股份有限公司 Calibration method and system for yaw angles of wind generating set
CN105257470A (en) * 2015-09-25 2016-01-20 南车株洲电力机车研究所有限公司 Wind direction compensation optimization method and device for wind turbine generator set

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