WO2022110938A1 - Wake flow calculation method taking local environmental factors of wind power plant into consideration - Google Patents

Wake flow calculation method taking local environmental factors of wind power plant into consideration Download PDF

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WO2022110938A1
WO2022110938A1 PCT/CN2021/114698 CN2021114698W WO2022110938A1 WO 2022110938 A1 WO2022110938 A1 WO 2022110938A1 CN 2021114698 W CN2021114698 W CN 2021114698W WO 2022110938 A1 WO2022110938 A1 WO 2022110938A1
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wake
velocity
turbulence intensity
calculation method
local environmental
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程瑜
郭辰
邵振州
冯军
孔金良
史俊
米磊
刘阳
李建华
鞠景生
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中国华能集团清洁能源技术研究院有限公司
华能新能源股份有限公司山西分公司
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10Complex mathematical operations
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    • Y02E10/72Wind turbines with rotation axis in wind direction

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  • the invention belongs to the technical field of wind turbine wake calculation technology, and particularly relates to a wake calculation method considering local environmental factors of wind farms.
  • the most widely used wind turbine wake calculation method in engineering is the linear wake model developed by Jensen et al.
  • the model is based on the following two assumptions, one is that the wake width increases linearly with the distance from the downstream of the wind turbine, and the other is that the velocity in the wake plane perpendicular to the axial direction of the wind turbine is uniformly distributed (Top-hat assumption).
  • Pena et al. compared the Jensen model with the measured data of Sexbierum and the CFD simulation results, and found that the speed predicted by the Jensen model had a large gap compared with the actual situation, and believed that a more advanced wake model should be developed.
  • Frandsen et al. abandoned the Top-hat assumption and proposed a new wake model.
  • Tian et al. believed that the velocity distribution in the wake region of the wind turbine was cosine law, and considered the turbulence caused by the wind turbine, and developed a 2D_k wake model.
  • the wind tunnel experimental measurement and numerical simulation results show that the velocity in the wake region of the real wind turbine is approximately Gaussian. Therefore, Bastankhah et al. proposed a two-dimensional wake model based on a Gaussian distribution function, which obtained a series of wind Field measurements and validation of wind tunnel experiments. It can be seen that the Gaussian function can better describe the distribution characteristics of velocity deficit in the wake region.
  • the main defect of this model is that the parameters in the wake radius calculation model included in the model need to be obtained by fitting the experimental measurement or numerical simulation results.
  • Niayifar et al. suggested that the wake expansion coefficient is proportional to the environmental turbulence intensity after analyzing the large eddy simulation data. Fuertes et al. followed this idea and proposed a new model by fitting the wind field measured data. Ishihara et al. A nonlinear model of turbulence intensity and wind turbine thrust coefficient is obtained by fitting the hole measurements.
  • the wake expansion radius in the Gaussian wake model needs to be determined by empirical formulas. It is generally believed that the model parameters contained in the wake expansion radius are related to the flow direction turbulence intensity, while the wind turbine wake is mainly in the vertical direction. It expands laterally and laterally, so it is unreasonable to relate model parameters to flow turbulence intensity. In addition, it is very difficult to obtain accurate turbulence intensity in actual wind farms. Errors in calculating turbulence intensity usually lead to inaccurate calculation of model parameters, resulting in inaccurate prediction of wake velocity deficits.
  • the purpose of the present invention is to provide a wake calculation method considering the local environmental factors of the wind farm, which greatly expands the application range of the wake calculation method and improves the accuracy of the calculation results. sex.
  • a wake calculation method considering local environmental factors of wind farms including the following steps:
  • Step 1 According to the local environment of the wind farm, obtain the local environment parameters of the wind farm;
  • Step 2 Calculate the atmospheric stability function of the environment where the wind farm is located
  • Step 3 Using the atmospheric stability function obtained in Step 2 as input, use the Monin-Obukhov similarity theory to calculate the surface friction velocity;
  • Step 4 According to the surface friction velocity obtained in step 3, successively calculate to obtain the flow velocity fluctuation of the near-surface layer, the flow-direction turbulence intensity of the near-surface layer, and the spanwise turbulence intensity I v,s of the near-surface layer;
  • Step 6 According to the spanwise turbulence intensity I vh of the hub height obtained in step 5, calculate and obtain the wake expansion coefficient, the initial wake radius and the wake radius in turn;
  • Step 7 Calculate the velocity deficit in the wake region according to the wake radius obtained in step 6;
  • Step 8 Calculate the velocity distribution in the wake region according to the velocity deficit in the wake region obtained in step 7.
  • the local environmental parameters of the wind farm include the incoming flow velocity U ⁇ , the surface roughness z 0 , the Obukhov length L and the local latitude ⁇ .
  • step 2 the atmospheric stability function ⁇ m ( ⁇ ) is calculated by the following formula:
  • step 3 the surface friction speed u * is obtained by calculating the following formula:
  • is the von Karman constant and z h is the hub height of the unit.
  • f 2 ⁇ sin( ⁇ )
  • f is the Coriolis force
  • the wake radius ⁇ is based on Obtained, where x is the flow direction coordinate.
  • step 7 the velocity deficit ⁇ U in the wake region is obtained according to the following formula:
  • r is the distance from any point in the wake region parallel to the plane of the rotor to the height of the hub in the plane
  • D is the diameter of the rotor
  • C t is the thrust coefficient corresponding to the incoming wind speed.
  • step 5 Preferably, in step 5, 0.2 ⁇ 2.
  • the present invention has the following beneficial technical effects:
  • the wake calculation method that takes into account the local environmental factors of the wind farm disclosed in the present invention creatively introduces the MOST theory (Monin-Obukhov similarity theory).
  • the MOST theory includes surface roughness and atmospheric stability, so that the calculation method proposed by the present invention can At the same time, the influence of surface roughness and atmospheric thermal stability on the wake development of wind turbines is considered, which greatly expands the application range of the wake calculation method.
  • the traditional wake calculation method believes that the wake expansion coefficient is related to the flow direction turbulence intensity, and in the real situation, the wake of the wind turbine expands in the span direction. Establish a connection, so that the wake calculation method can reflect the real wake expansion and improve the accuracy of the calculation results.
  • the empirical coefficient ⁇ is determined according to the local atmospheric thermal stability, and usually takes a value between 0.2 and 2. The more stable the wind condition is, the smaller the value of ⁇ is, the more unstable the wind condition is, and the larger the value of ⁇ is, the further improvement is achieved. The accuracy of the calculation results.
  • Fig. 1 is the method flow chart of the present invention
  • FIG. 2 is a schematic diagram of a control body used in constructing a wake calculation method in an embodiment
  • Figure 3 shows the velocity deficit distribution in the wake region obtained by different wake calculation methods.
  • the wake velocity distribution under different working conditions calculated by the method is compared with the large eddy simulation results and wind tunnel experimental results reported in the literature, mainly to compare the wake expansion. Coefficients and velocity deficit distributions for different surface roughness and atmospheric stability conditions.
  • the example data for the comparison of the present invention is derived from reference [1].
  • the present invention adopts the control body shown in FIG. 2 and constructs a wake calculation method according to the steps shown in FIG. 1 .
  • U ⁇ is the incoming velocity
  • U w is the velocity in the wake region
  • r is the distance from any point in the wake region parallel to the plane of the rotor to the height of the hub in the plane
  • D represents the diameter of the rotor.
  • Step 7) According to the wake radius ⁇ obtained in step 6), the velocity deficit in the wake region can be calculated That is, the corresponding distribution law in Figure 3.
  • Figure 3 shows the comparison of the velocity deficit in the wake region obtained by different wake calculation methods with the results of the large eddy simulation.
  • the velocity deficits predicted by the wake calculation method proposed in the present invention are closer to the large eddy simulation results, and are better than the BP2014 method and the FMP2018 method.

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Abstract

A wake flow calculation method taking local environmental factors of a wind power plant into consideration, which method belongs to the technical field of wake flow calculation of wind turbine generators. The method comprises: firstly, acquiring local environmental parameters of a wind power plant according to the local environmental of the wind power plant; then, calculating an atmospheric stability function of the environment where the wind power plant is located; taking the obtained atmospheric stability function as an input, and calculating a surface friction velocity by using the Monin-Obukhov similarity theory; then, sequentially performing calculation to obtain a flow velocity pulsation of a surface layer, a flow turbulence intensity of the surface layer, and a spanwise turbulence intensity of the surface layer; establishing a proportional relationship between a spanwise turbulence intensity of the height of a wheel hub and the spanwise turbulence intensity of the surface layer, so as to obtain the spanwise turbulence intensity of the height of the wheel hub; then, sequentially performing calculation to obtain a wake flow expansion coefficient, an initial wake flow radius, and a wake flow radius; calculating a velocity loss of a wake flow area; and finally obtaining the velocity distribution in the wake flow area. By means of the method, the application range of a wake flow calculation method is greatly expanded, and the accuracy of a calculation result is improved.

Description

一种考虑风电场局地环境因素的尾流计算方法A wake calculation method considering local environmental factors of wind farms
本申请要求于2020年11月27日提交中国专利局、申请号为202011364566.4、发明名称为“一种考虑风电场局地环境因素的尾流计算方法”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。This application claims the priority of the Chinese patent application filed on November 27, 2020 with the application number 202011364566.4 and the invention titled "A wake calculation method considering local environmental factors of wind farms", the entire contents of which are Incorporated herein by reference.
技术领域technical field
本发明属于风电机组尾流计算技术领域,具体涉及一种考虑风电场局地环境因素的尾流计算方法。The invention belongs to the technical field of wind turbine wake calculation technology, and particularly relates to a wake calculation method considering local environmental factors of wind farms.
背景技术Background technique
目前工程中应用最为广泛的风电机组尾流计算方法是Jensen等人发展的线性尾流模型。该模型基于以下两个假设,一是尾流宽度随着离风力机下游的距离线性增长,二是垂直于风力机轴向的尾流平面内速度均匀分布(Top-hat假设)。Pena等人将Jensen模型和Sexbierum实测数据和CFD仿真结果进行对比,发现Jensen模型预测的速度和实际情况相比有较大的差距,认为应该发展更加高级的尾流模型。为此,Frandsen等人放弃了Top-hat假设,提出了一种新的尾流模型。Tian等人认为风力机尾流区内速度呈余弦规律分布,并考虑风力机引起的湍流作用,发展了一个2D_k尾流模型。风洞实验测量和数值仿真结果表明,真实的风力机尾流区内速度近似呈高斯分布,因此Bastankhah等人提出了一种基于高斯分布函数的二维尾流模型,该模型得到了一系列风场测量和风洞实验的验证。由此可以看出,高斯函数能较好的描述尾流区内的速度亏损分布特点。该模型的主要缺陷是模型包含的尾流半径计算模型中的参数需要通过对实验测量或数值仿真结果进行拟合得到,目前主要有三种不同的计算方法。Niayifar等人通过分析大涡模拟数据后建议尾流扩张系数和环境湍流强度呈正比,Fuertes等人沿用这一思想并采用风场实测数据拟合提出了一个新的模型,Ishihara等人通过对风洞测量结果进行拟合得到了一个关于湍流强度和风力机推力系数的非线性模型。At present, the most widely used wind turbine wake calculation method in engineering is the linear wake model developed by Jensen et al. The model is based on the following two assumptions, one is that the wake width increases linearly with the distance from the downstream of the wind turbine, and the other is that the velocity in the wake plane perpendicular to the axial direction of the wind turbine is uniformly distributed (Top-hat assumption). Pena et al. compared the Jensen model with the measured data of Sexbierum and the CFD simulation results, and found that the speed predicted by the Jensen model had a large gap compared with the actual situation, and believed that a more advanced wake model should be developed. To this end, Frandsen et al. abandoned the Top-hat assumption and proposed a new wake model. Tian et al. believed that the velocity distribution in the wake region of the wind turbine was cosine law, and considered the turbulence caused by the wind turbine, and developed a 2D_k wake model. The wind tunnel experimental measurement and numerical simulation results show that the velocity in the wake region of the real wind turbine is approximately Gaussian. Therefore, Bastankhah et al. proposed a two-dimensional wake model based on a Gaussian distribution function, which obtained a series of wind Field measurements and validation of wind tunnel experiments. It can be seen that the Gaussian function can better describe the distribution characteristics of velocity deficit in the wake region. The main defect of this model is that the parameters in the wake radius calculation model included in the model need to be obtained by fitting the experimental measurement or numerical simulation results. At present, there are mainly three different calculation methods. Niayifar et al. suggested that the wake expansion coefficient is proportional to the environmental turbulence intensity after analyzing the large eddy simulation data. Fuertes et al. followed this idea and proposed a new model by fitting the wind field measured data. Ishihara et al. A nonlinear model of turbulence intensity and wind turbine thrust coefficient is obtained by fitting the hole measurements.
从以上分析可以看出,高斯尾流模型中的尾流扩张半径需要采用经验公式来确定,通常认为尾流扩张半径包含的的模型参数和流向湍流强度有关,而风 力机尾流主要是在垂向和侧向扩张,因此将模型参数和流向湍流强度关联并不合理。另外,实际风电场中精确的湍流强度的获取非常困难,计算湍流强度的误差通常会导致模型参数计算不准确,导致尾流速度亏损预测不准。It can be seen from the above analysis that the wake expansion radius in the Gaussian wake model needs to be determined by empirical formulas. It is generally believed that the model parameters contained in the wake expansion radius are related to the flow direction turbulence intensity, while the wind turbine wake is mainly in the vertical direction. It expands laterally and laterally, so it is unreasonable to relate model parameters to flow turbulence intensity. In addition, it is very difficult to obtain accurate turbulence intensity in actual wind farms. Errors in calculating turbulence intensity usually lead to inaccurate calculation of model parameters, resulting in inaccurate prediction of wake velocity deficits.
发明内容SUMMARY OF THE INVENTION
为了解决上述现有技术中存在的缺陷,本发明的目的在于提供一种考虑风电场局地环境因素的尾流计算方法,极大地拓展了尾流计算方法的应用范围,提高了计算结果的准确性。In order to solve the above-mentioned defects in the prior art, the purpose of the present invention is to provide a wake calculation method considering the local environmental factors of the wind farm, which greatly expands the application range of the wake calculation method and improves the accuracy of the calculation results. sex.
本发明是通过以下技术方案来实现:The present invention is achieved through the following technical solutions:
一种考虑风电场局地环境因素的尾流计算方法,包括以下步骤:A wake calculation method considering local environmental factors of wind farms, including the following steps:
步骤1:根据风电场的局地环境,获得风电场的局地环境参数;Step 1: According to the local environment of the wind farm, obtain the local environment parameters of the wind farm;
步骤2:计算风电场所在环境的大气稳定度函数;Step 2: Calculate the atmospheric stability function of the environment where the wind farm is located;
步骤3:将步骤2得到的大气稳定度函数作为输入,利用Monin-Obukhov相似理论计算地表摩擦速度;Step 3: Using the atmospheric stability function obtained in Step 2 as input, use the Monin-Obukhov similarity theory to calculate the surface friction velocity;
步骤4:根据步骤3得到的地表摩擦速度依次计算得到近地层的流向速度脉动、近地层的流向湍流强度和近地层的展向湍流强度I v,sStep 4: According to the surface friction velocity obtained in step 3, successively calculate to obtain the flow velocity fluctuation of the near-surface layer, the flow-direction turbulence intensity of the near-surface layer, and the spanwise turbulence intensity I v,s of the near-surface layer;
步骤5:建立轮毂高度的展向湍流强度I v.h与步骤4得到的近地层的展向湍流强度I v,s的正比关系:I v.h=γI v,s,其中γ为经验系数,得到轮毂高度的展向湍流强度I v.hStep 5: Establish a proportional relationship between the spanwise turbulence intensity I vh of the hub height and the spanwise turbulence intensity I v,s of the near-surface layer obtained in step 4: I vh =γI v,s , where γ is an empirical coefficient, and the hub height is obtained The spanwise turbulence intensity I vh of ;
步骤6:根据步骤5得到的轮毂高度的展向湍流强度I v.h,依次计算得到尾流扩张系数、初始尾流半径和尾流半径; Step 6: According to the spanwise turbulence intensity I vh of the hub height obtained in step 5, calculate and obtain the wake expansion coefficient, the initial wake radius and the wake radius in turn;
步骤7:根据步骤6得到的尾流半径计算尾流区速度亏损;Step 7: Calculate the velocity deficit in the wake region according to the wake radius obtained in step 6;
步骤8:根据步骤7得到的尾流区速度亏损计算得到尾流区的速度分布。Step 8: Calculate the velocity distribution in the wake region according to the velocity deficit in the wake region obtained in step 7.
优选地,步骤1中,风电场的局地环境参数包括来流速度U 、地表粗糙度z 0、Obukhov长度L和当地纬度φ。 Preferably, in step 1, the local environmental parameters of the wind farm include the incoming flow velocity U , the surface roughness z 0 , the Obukhov length L and the local latitude φ.
进一步优选地,步骤2中,通过下式计算得到大气稳定度函数ψ m(ζ): Further preferably, in step 2, the atmospheric stability function ψ m (ζ) is calculated by the following formula:
Figure PCTCN2021114698-appb-000001
Figure PCTCN2021114698-appb-000001
其中,
Figure PCTCN2021114698-appb-000002
是无量纲稳定度参数,z为法向坐标,中间变量t=(1-15ζ) 1/4
in,
Figure PCTCN2021114698-appb-000002
is the dimensionless stability parameter, z is the normal coordinate, and the intermediate variable t=(1-15ζ) 1/4 .
进一步优选地,步骤3中,通过下式计算得到地表摩擦速度u *Further preferably, in step 3, the surface friction speed u * is obtained by calculating the following formula:
Figure PCTCN2021114698-appb-000003
Figure PCTCN2021114698-appb-000003
其中κ是冯卡门常数,z h是机组轮毂高度。 where κ is the von Karman constant and z h is the hub height of the unit.
进一步优选地,步骤4中,近地层的流向速度脉动:σ u,s=2.5u *Further preferably, in step 4, the flow velocity fluctuation of the near-surface layer: σ u, s =2.5u * ;
近地层的流向湍流强度:
Figure PCTCN2021114698-appb-000004
The flow direction turbulence intensity in the near-surface layer:
Figure PCTCN2021114698-appb-000004
近地层的展向湍流强度
Figure PCTCN2021114698-appb-000005
Spanwise turbulence intensity in the near-surface layer
Figure PCTCN2021114698-appb-000005
其中,f=2Ωsin(φ),
Figure PCTCN2021114698-appb-000006
f为科氏力,地球自转周期Ω=7.29×10 -5rad/s。
Among them, f=2Ωsin(φ),
Figure PCTCN2021114698-appb-000006
f is the Coriolis force, and the rotation period of the earth is Ω=7.29×10 -5 rad/s.
进一步优选地,步骤6中,尾流扩张系数k w=0.223I v,h+0.022; Further preferably, in step 6, the wake expansion coefficient k w =0.223I v, h +0.022;
初始尾流半径∈=-1.91k w+0.34; Initial wake radius ∈=-1.91k w +0.34;
尾流半径σ根据
Figure PCTCN2021114698-appb-000007
求得,其中x为流向坐标。
The wake radius σ is based on
Figure PCTCN2021114698-appb-000007
Obtained, where x is the flow direction coordinate.
进一步优选地,步骤7中,尾流区速度亏损ΔU根据下式求得:Further preferably, in step 7, the velocity deficit ΔU in the wake region is obtained according to the following formula:
Figure PCTCN2021114698-appb-000008
Figure PCTCN2021114698-appb-000008
其中,r为尾流区内平行于风轮平面内任一点到该平面内轮毂高度处的距离,D为风轮直径,C t为对应来流风速下的推力系数。 Among them, r is the distance from any point in the wake region parallel to the plane of the rotor to the height of the hub in the plane, D is the diameter of the rotor, and C t is the thrust coefficient corresponding to the incoming wind speed.
进一步优选地,步骤8中,尾流区的速度分布U w=U -ΔU。 Further preferably, in step 8, the velocity distribution in the wake region U w =U -ΔU.
优选地,步骤5中,0.2≤γ≤2。Preferably, in step 5, 0.2≤γ≤2.
与现有技术相比,本发明具有以下有益的技术效果:Compared with the prior art, the present invention has the following beneficial technical effects:
本发明公开的考虑风电场局地环境因素的尾流计算方法,创造性地引入MOST理论(Monin-Obukhov相似理论),MOST理论包含了地表粗糙度和大气稳定度,使得本发明提出的计算方法能同时考虑地表粗糙度和大气热稳定度对风电机组尾流发展的影响,极大地拓展了尾流计算方法的应用范围。传统的尾流计算方法认为,尾流扩张系数和流向湍流强度相关,而真实情况下风电机组尾流在展向进行扩张,本发明提出的尾流计算方法将尾流扩张系数和展向湍流强度建立联系,使尾流计算方法能反映真实的尾流扩张情况,提高计算结果的准确性。The wake calculation method that takes into account the local environmental factors of the wind farm disclosed in the present invention creatively introduces the MOST theory (Monin-Obukhov similarity theory). The MOST theory includes surface roughness and atmospheric stability, so that the calculation method proposed by the present invention can At the same time, the influence of surface roughness and atmospheric thermal stability on the wake development of wind turbines is considered, which greatly expands the application range of the wake calculation method. The traditional wake calculation method believes that the wake expansion coefficient is related to the flow direction turbulence intensity, and in the real situation, the wake of the wind turbine expands in the span direction. Establish a connection, so that the wake calculation method can reflect the real wake expansion and improve the accuracy of the calculation results.
进一步地,经验系数γ根据当地的大气热稳定度来确定,通常在0.2~2中取值,风况越稳定,γ取值越小,风况越不稳定,γ取值越大,进一步提高计算结果的准确度。Further, the empirical coefficient γ is determined according to the local atmospheric thermal stability, and usually takes a value between 0.2 and 2. The more stable the wind condition is, the smaller the value of γ is, the more unstable the wind condition is, and the larger the value of γ is, the further improvement is achieved. The accuracy of the calculation results.
附图说明Description of drawings
图1为本发明的方法流程图;Fig. 1 is the method flow chart of the present invention;
图2为实施例中构建尾流计算方法使用的控制体示意图;2 is a schematic diagram of a control body used in constructing a wake calculation method in an embodiment;
图3为不同尾流计算方法得到的尾流区速度亏损分布图。Figure 3 shows the velocity deficit distribution in the wake region obtained by different wake calculation methods.
具体实施方式Detailed ways
下面以附图和具体实施例对本发明做进一步的详细说明,所述是对本发明的解释而不是限定。The present invention will be further described in detail below with the accompanying drawings and specific embodiments, which are to explain rather than limit the present invention.
为了验证本发明提出的尾流计算方法的有效性,下面将该方法计算的不同工况下尾流速度分布与文献中报道的大涡模拟结果和风洞实验结果进行对比,主要对比尾流扩张系数以及不同地表粗糙度和大气稳定度工况下的速度亏损分布。本发明对比的实例数据来源于参考文献[1]。In order to verify the validity of the wake calculation method proposed in the present invention, the wake velocity distribution under different working conditions calculated by the method is compared with the large eddy simulation results and wind tunnel experimental results reported in the literature, mainly to compare the wake expansion. Coefficients and velocity deficit distributions for different surface roughness and atmospheric stability conditions. The example data for the comparison of the present invention is derived from reference [1].
本发明采用图2所示的控制体,按照图1所示步骤构建尾流计算方法。在图2中,U 是来流速度,U w是尾流区速度,r是尾流区内平行于风轮平面内任一点到该平面内轮毂高度处的距离,D表示风轮直径。 The present invention adopts the control body shown in FIG. 2 and constructs a wake calculation method according to the steps shown in FIG. 1 . In Figure 2, U is the incoming velocity, U w is the velocity in the wake region, r is the distance from any point in the wake region parallel to the plane of the rotor to the height of the hub in the plane, and D represents the diameter of the rotor.
下面以一个具体实施例对本发明的实施方式进行进一步的说明:Embodiments of the present invention are further described below with a specific example:
步骤1):给定输入参数Step 1): Given input parameters
U =8.5m/s,z h=70m,D=80m,z 0=0.05m,L=∞,φ=47°,C t=0.8。 U =8.5m/s, zh =70m, D=80m, z 0 =0.05m, L=∞, φ=47°, C t = 0.8.
步骤2):由L=∞可知ζ=0,代入大气稳定度函数得到ψ m(0)=0。 Step 2): From L=∞, it can be known that ζ=0, and substituted into the atmospheric stability function to obtain ψ m (0)=0.
步骤3):利用Monin-Obukhov相似理论计算地表摩擦速度u *=0.47m/s。 Step 3): Use the Monin-Obukhov similarity theory to calculate the surface friction velocity u * =0.47m/s.
步骤4):利用经验公式计算近地层内的流向速度脉动大小σ u,s=1.175m/s,并依据定义计算流向湍流强度I u,s=0.138,进一步可以算出展向湍流强度I v,s=0.11。 Step 4): Use the empirical formula to calculate the flow direction velocity fluctuation size σ u, s = 1.175m/s in the near-surface layer, and calculate the flow direction turbulence intensity I u, s = 0.138 according to the definition, and further calculate the spanwise turbulence intensity I v, s = 0.11.
步骤5):根据本发明提出的线性关系式,取γ=1.0,可以计算出I v,h=0.11。 Step 5): According to the linear relational formula proposed by the present invention, taking γ=1.0, I v, h =0.11 can be calculated.
步骤6):依据文献报道的公式计算尾流计算方法的扩张系数,得到k w=0.025,∈=0.293,进而可以计算出尾流半径随x的变化规律
Figure PCTCN2021114698-appb-000009
Step 6): Calculate the expansion coefficient of the wake calculation method according to the formula reported in the literature, and obtain k w =0.025, ∈ = 0.293, and then the variation law of the wake radius with x can be calculated
Figure PCTCN2021114698-appb-000009
步骤7):依据步骤6)得到的尾流半径σ可以计算尾流区速度亏损
Figure PCTCN2021114698-appb-000010
即图3中对应的分布规律。
Step 7): According to the wake radius σ obtained in step 6), the velocity deficit in the wake region can be calculated
Figure PCTCN2021114698-appb-000010
That is, the corresponding distribution law in Figure 3.
图3给出了不同尾流计算方法得到的尾流区速度亏损与大涡模拟结果对比情况。在整个尾流区内,本发明提出的尾流计算方法预测的速度亏损都与大涡模拟结果更接近,优于BP2014方法和FMP2018方法。Figure 3 shows the comparison of the velocity deficit in the wake region obtained by different wake calculation methods with the results of the large eddy simulation. In the entire wake region, the velocity deficits predicted by the wake calculation method proposed in the present invention are closer to the large eddy simulation results, and are better than the BP2014 method and the FMP2018 method.
[1]Cheng W-C,Porté-Agel F.A simple physically-based model for wind-turbine wake growth in a turbulent boundary layer.Bound-Layer Meteorol 2018:1-10.[1] Cheng W-C, Porté-Agel F.A simple physically-based model for wind-turbine wake growth in a turbulent boundary layer.Bound-Layer Meteorol 2018:1-10.
需要说明的是,以上所述仅为本发明实施方式的一部分,根据本发明所描述的系统所做的等效变化,均包括在本发明的保护范围内。本发明所属技术领域的技术人员可以对所描述的具体实例做类似的方式替代,只要不偏离本发明的结构或者超越本权利要求书所定义的范围,均属于本发明的保护范围。It should be noted that the above is only a part of the embodiments of the present invention, and equivalent changes made by the system described in the present invention are all included in the protection scope of the present invention. Those skilled in the art to which the present invention pertains can substitute the specific examples described in a similar manner, as long as they do not deviate from the structure of the present invention or go beyond the scope defined by the claims, they all belong to the protection scope of the present invention.

Claims (9)

  1. 一种考虑风电场局地环境因素的尾流计算方法,其特征在于,包括以下步骤:A wake calculation method considering local environmental factors of a wind farm, characterized in that it includes the following steps:
    步骤1:根据风电场的局地环境,获得风电场的局地环境参数;Step 1: According to the local environment of the wind farm, obtain the local environment parameters of the wind farm;
    步骤2:计算风电场所在环境的大气稳定度函数;Step 2: Calculate the atmospheric stability function of the environment where the wind farm is located;
    步骤3:将步骤2得到的大气稳定度函数作为输入,利用Monin-Obukhov相似理论计算地表摩擦速度;Step 3: Using the atmospheric stability function obtained in Step 2 as input, use the Monin-Obukhov similarity theory to calculate the surface friction velocity;
    步骤4:根据步骤3得到的地表摩擦速度依次计算得到近地层的流向速度脉动、近地层的流向湍流强度和近地层的展向湍流强度I v,sStep 4: According to the surface friction velocity obtained in step 3, successively calculate to obtain the flow velocity fluctuation of the near-surface layer, the flow-direction turbulence intensity of the near-surface layer, and the spanwise turbulence intensity I v,s of the near-surface layer;
    步骤5:建立轮毂高度的展向湍流强度I v.h与步骤4得到的近地层的展向湍流强度I v,s的正比关系:I v.h=γI v,s,其中γ为经验系数,得到轮毂高度的展向湍流强度I v.hStep 5: Establish a proportional relationship between the spanwise turbulence intensity I vh of the hub height and the spanwise turbulence intensity I v,s of the near-surface layer obtained in step 4: I vh =γI v,s , where γ is an empirical coefficient, and the hub height is obtained The spanwise turbulence intensity I vh of ;
    步骤6:根据步骤5得到的轮毂高度的展向湍流强度I v.h,依次计算得到尾流扩张系数、初始尾流半径和尾流半径; Step 6: According to the spanwise turbulence intensity I vh of the hub height obtained in step 5, calculate and obtain the wake expansion coefficient, the initial wake radius and the wake radius in turn;
    步骤7:根据步骤6得到的尾流半径计算尾流区速度亏损;Step 7: Calculate the velocity deficit in the wake region according to the wake radius obtained in step 6;
    步骤8:根据步骤7得到的尾流区速度亏损计算得到尾流区的速度分布。Step 8: Calculate the velocity distribution in the wake region according to the velocity deficit in the wake region obtained in step 7.
  2. 如权利要求1所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤1中,风电场的局地环境参数包括来流速度U 、地表粗糙度z 0、Obukhov长度L和当地纬度φ。 The wake calculation method considering the local environmental factors of the wind farm according to claim 1, wherein in step 1, the local environmental parameters of the wind farm include the incoming velocity U , the surface roughness z 0 , and the Obukhov length L and the local latitude φ.
  3. 如权利要求2所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤2中,通过下式计算得到大气稳定度函数ψ m(ζ): The wake calculation method considering the local environmental factors of the wind farm as claimed in claim 2, characterized in that, in step 2, the atmospheric stability function ψ m (ζ) is obtained by calculating the following formula:
    Figure PCTCN2021114698-appb-100001
    Figure PCTCN2021114698-appb-100001
    其中,
    Figure PCTCN2021114698-appb-100002
    是无量纲稳定度参数,z为法向坐标,中间变量t=(1-15ζ) 1/4
    in,
    Figure PCTCN2021114698-appb-100002
    is the dimensionless stability parameter, z is the normal coordinate, and the intermediate variable t=(1-15ζ) 1/4 .
  4. 如权利要求3所述的考虑风电场局地环境因素的尾流计算方法,其特征 在于,步骤3中,通过下式计算得到地表摩擦速度u *The wake calculation method considering local environmental factors of the wind farm as claimed in claim 3, characterized in that, in step 3, the surface friction velocity u * is obtained by calculating the following formula:
    Figure PCTCN2021114698-appb-100003
    Figure PCTCN2021114698-appb-100003
    其中κ是冯卡门常数,z h是机组轮毂高度。 where κ is the von Karman constant and z h is the hub height of the unit.
  5. 如权利要求4所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤4中,近地层的流向速度脉动:σ u,s=2.5u *The wake calculation method considering the local environmental factors of the wind farm according to claim 4, wherein in step 4, the flow velocity fluctuation in the near-surface layer: σ u, s = 2.5u * ;
    近地层的流向湍流强度:
    Figure PCTCN2021114698-appb-100004
    The flow direction turbulence intensity in the near-surface layer:
    Figure PCTCN2021114698-appb-100004
    近地层的展向湍流强度
    Figure PCTCN2021114698-appb-100005
    Spanwise turbulence intensity in the near-surface layer
    Figure PCTCN2021114698-appb-100005
    其中,f=2Ωsin(φ),
    Figure PCTCN2021114698-appb-100006
    f为科氏力,地球自转周期Ω=7.29×10 -5rad/s。
    Among them, f=2Ωsin(φ),
    Figure PCTCN2021114698-appb-100006
    f is the Coriolis force, and the rotation period of the earth is Ω=7.29×10 -5 rad/s.
  6. 如权利要求5所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤6中,尾流扩张系数k w=0.223I v,h+0.022; The wake calculation method considering local environmental factors of the wind farm according to claim 5, wherein in step 6, the wake expansion coefficient k w =0.223I v, h +0.022;
    初始尾流半径ε=-1.91k w+0.34; Initial wake radius ε=-1.91k w +0.34;
    尾流半径σ根据
    Figure PCTCN2021114698-appb-100007
    求得,其中x为流向坐标。
    The wake radius σ is based on
    Figure PCTCN2021114698-appb-100007
    Obtained, where x is the flow direction coordinate.
  7. 如权利要求6所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤7中,尾流区速度亏损ΔU根据下式求得:The wake calculation method considering the local environmental factors of the wind farm according to claim 6, characterized in that, in step 7, the velocity deficit ΔU in the wake region is obtained according to the following formula:
    Figure PCTCN2021114698-appb-100008
    Figure PCTCN2021114698-appb-100008
    其中,r为尾流区内平行于风轮平面内任一点到该平面内轮毂高度处的距离,D为风轮直径,C t为对应来流风速下的推力系数。 Among them, r is the distance from any point in the wake region parallel to the plane of the rotor to the height of the hub in the plane, D is the diameter of the rotor, and C t is the thrust coefficient corresponding to the incoming wind speed.
  8. 如权利要求7所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤8中,尾流区的速度分布U w=U -ΔU。 The wake calculation method considering local environmental factors of the wind farm according to claim 7, characterized in that, in step 8, the velocity distribution in the wake region U w =U -ΔU.
  9. 如权利要求1所述的考虑风电场局地环境因素的尾流计算方法,其特征在于,步骤5中,0.2≤γ≤2。The wake calculation method considering local environmental factors of a wind farm according to claim 1, wherein in step 5, 0.2≤γ≤2.
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