CN110173391A - A kind of Large marine Axis Wind Turbine With A Tip Vane fusion winglet and wind energy conversion system - Google Patents
A kind of Large marine Axis Wind Turbine With A Tip Vane fusion winglet and wind energy conversion system Download PDFInfo
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- CN110173391A CN110173391A CN201910438912.XA CN201910438912A CN110173391A CN 110173391 A CN110173391 A CN 110173391A CN 201910438912 A CN201910438912 A CN 201910438912A CN 110173391 A CN110173391 A CN 110173391A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
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Abstract
本发明涉及一种大型海上风力机叶尖融合小翼及风力机,其中小翼与风力机的叶片叶尖部分的翼型相同并光滑过渡,小翼朝向叶片吸力面弯曲,且小翼的弯曲倾斜角度为50°~60°。与现有技术相比,本发明在深远海风力机受到海洋环境的影响产生艏摇、纵摇、纵荡等运动条件下,能够有效减小叶尖涡对叶尖部分功率的降低,同时叶尖小翼具有良好的气动性能,能够提高风力机叶片的转矩。显著提高风力机总输出功率。
The invention relates to a large-scale offshore wind turbine blade tip fusion winglet and a wind turbine, wherein the winglet and the blade tip part of the wind turbine have the same airfoil shape and a smooth transition, the winglet bends toward the suction surface of the blade, and the curvature of the winglet The inclination angle is 50°~60°. Compared with the prior art, the present invention can effectively reduce the reduction of blade tip vortex to the power of blade tip when the deep-sea wind turbine is affected by the ocean environment and produces motion conditions such as yaw, pitch, and surge. The tip winglet has good aerodynamic performance and can increase the torque of the wind turbine blade. Significantly increase the total output power of the wind turbine.
Description
技术领域technical field
本发明涉及一种,尤其是涉及一种大型海上风力机叶尖融合小翼及风力机。The invention relates to a large-scale offshore wind turbine blade tip fusion winglet and a wind turbine in particular.
背景技术Background technique
对于有限长度的风力机叶片,在风力机运行条件下叶片上下表面会产生压力 差,在风力机的三维旋转效应和叶片表面压差的作用下会使压力面的气流绕过叶尖 向吸力面流去,造成吸力面压力增加而压力面压力减小,从而叶尖表面压差减小, 叶片转矩下降。同时产生的叶尖涡也会产生诱导阻力,使叶片升力减小,对叶片的 功率输出产生不利的影响,对于大型风力机,其叶片尺寸很大,叶尖涡对叶片功率 的影响不可忽略。For wind turbine blades of limited length, pressure differences will occur on the upper and lower surfaces of the blades under the operating conditions of the wind turbine. As the flow goes away, the pressure on the suction side increases and the pressure on the pressure side decreases, so the pressure difference on the surface of the blade tip decreases, and the blade torque decreases. At the same time, the blade tip vortex will also generate induced resistance, which will reduce the lift force of the blade and have an adverse effect on the power output of the blade. For large wind turbines, the blade size is very large, and the impact of the blade tip vortex on the blade power cannot be ignored.
在风力机叶尖安装小翼结构是提升风力机气动性能的一种重要手段。安装叶尖小翼后,可有效抑制叶尖涡的强度,小翼的向外弯曲延伸使叶尖涡的生成位置向风 轮外侧转移,减小了叶尖扰流对叶尖部分压差的影响,提高了叶尖功率输出。由于 叶尖小翼与叶片本体部分光滑过渡,相当于对叶片的延伸和弯曲,所以小翼也能产 生转矩,使风力机的总功率输出提高。与陆地固定式基础风力机相比,深远海风力 机受到海洋环境的影响会产生艏摇、纵摇、纵荡等运动,会影响风轮平面处的入流 风速,从而影响风力机的气动性能,因此在运动条件下的风力机功率响应与陆地固 定式风力机存在较大差异。Installing the winglet structure on the blade tip of the wind turbine is an important means to improve the aerodynamic performance of the wind turbine. After installing the blade tip winglet, the strength of the blade tip vortex can be effectively suppressed. The outward bending and extension of the blade tip vortex shifts the generation position of the blade tip vortex to the outside of the wind rotor, reducing the impact of the blade tip turbulence on the pressure difference of the blade tip. impact, increasing tip power output. Since the blade tip winglet and the blade body are in a smooth transition, which is equivalent to the extension and bending of the blade, the winglet can also generate torque to increase the total power output of the wind turbine. Compared with fixed-based wind turbines on land, deep-sea wind turbines will produce yaw, pitch, surge and other movements under the influence of the marine environment, which will affect the inflow wind speed at the plane of the wind rotor, thereby affecting the aerodynamic performance of the wind turbine. Therefore, the power response of wind turbines under motion conditions is quite different from that of fixed land wind turbines.
由于叶尖小翼安装的叶片的端部,对叶片的根部会产生一个较大的挥舞力矩, 对风力机叶片的结构强度提出了更高的要求,现有的叶尖小翼设计都没有将叶尖结 构重量增加以及叶片受力一起综合平衡考虑,导致叶尖小翼的性能没有得到充分发 挥。Because the end of the blade where the tiplet is installed will generate a large swinging moment to the root of the blade, which puts forward higher requirements for the structural strength of the wind turbine blade. The existing design of the tiplet does not incorporate The weight increase of the blade tip structure and the force on the blade are considered in a comprehensive balance, resulting in the performance of the blade tip winglet not being fully utilized.
发明内容Contents of the invention
本发明的目的就是为了克服上述现有技术存在的缺陷而提供一种大型海上风 力机叶尖融合小翼及风力机。Purpose of the present invention is exactly to provide a kind of large offshore wind turbine blade tip fusion winglet and wind turbine in order to overcome the defective that above-mentioned prior art exists.
本发明的目的可以通过以下技术方案来实现:The purpose of the present invention can be achieved through the following technical solutions:
一种大型海上风力机叶尖融合小翼,该小翼与风力机的叶片叶尖部分的翼型相同并光滑过渡,所述小翼朝向叶片吸力面弯曲,且小翼的弯曲倾斜角度为50° ~60°。A large-scale offshore wind turbine blade tip fusion winglet, the winglet has the same airfoil shape as the blade tip part of the wind turbine and has a smooth transition, the winglet is curved toward the suction surface of the blade, and the angle of inclination of the winglet is 50° ° ~ 60 °.
所述小翼的翼型为NACA64翼型。The airfoil of the winglet is NACA64 airfoil.
所述小翼的展向长度为风轮半径的3%~5%。The spanwise length of the winglet is 3%-5% of the radius of the wind rotor.
所述小翼的弯曲半径为风力机的风轮半径的1%~3%。The bending radius of the winglet is 1%-3% of the radius of the rotor of the wind turbine.
一种大型海上风力机,包括多个叶片,所述叶片的叶尖部分上设有小翼,该小 翼与叶尖部分的翼型相同并光滑过渡,所述小翼朝向叶片吸力面弯曲,且小翼的弯 曲倾斜角度为50°~60°。A large offshore wind turbine, comprising a plurality of blades, the tip of the blade is provided with a small wing, the winglet is the same as the airfoil of the tip and transitions smoothly, and the winglet is bent towards the suction surface of the blade, And the bending angle of the winglet is 50°-60°.
所述小翼的翼型为NACA64翼型。The airfoil of the winglet is NACA64 airfoil.
所述小翼的展向长度为风轮半径的3%~5%。The spanwise length of the winglet is 3%-5% of the radius of the wind rotor.
所述小翼的弯曲半径为风力机的风轮半径的1%~3%。The bending radius of the winglet is 1%-3% of the radius of the rotor of the wind turbine.
与现有技术相比,本发明具有以下有益效果:Compared with the prior art, the present invention has the following beneficial effects:
1)与叶片的叶尖部分平滑过渡且翼型相同,朝向叶片吸力面弯曲,且小翼的 弯曲倾斜角度为50°~60°,实现了小翼与叶尖的融合设计,可以提升叶片叶尖功 率输出,显著提高海上风力机总输出功率。1) It has a smooth transition and the same airfoil shape as the tip of the blade, and is bent towards the suction surface of the blade, and the bending angle of the winglet is 50°-60°, which realizes the fusion design of the winglet and the tip, and can improve the Sharp power output, significantly increasing the total output power of offshore wind turbines.
2)展向长度为风轮半径的3%~5%,弯曲半径为风力机的风轮半径的1%~3%,融合小翼具有良好的气动外形,产生功率提升的作用。2) The spanwise length is 3% to 5% of the radius of the wind rotor, and the bending radius is 1% to 3% of the radius of the wind rotor of the wind turbine. The fused winglet has a good aerodynamic shape and can increase power.
附图说明Description of drawings
图1是带叶尖融合小翼的叶片;Fig. 1 is the blade with tip fusion winglet;
图2是翼尖小翼局部示意图;Fig. 2 is a partial schematic view of the winglet;
图3(a)是无叶尖小翼叶片压力面压力云图;Fig. 3(a) is the pressure cloud diagram of the pressure surface of the tipless winglet;
图3(b)是有叶尖小翼叶片压力面压力云图;Fig. 3(b) is a cloud diagram of the pressure surface of the blade with tiplet;
图3(c)是无叶尖小翼叶片吸力面压力云图;Fig. 3(c) is a cloud diagram of pressure on the suction surface of a blade without a tip;
图3(d)是有叶尖小翼叶片吸力面压力云图;Fig. 3(d) is a cloud diagram of pressure on the suction surface of a blade with a tiplet;
图4是有叶尖小翼叶片叶尖截面上下表面压力值。Figure 4 shows the pressure values on the upper and lower surfaces of the tip section of the tipped winglet blade.
具体实施方式Detailed ways
下面结合附图和具体实施例对本发明进行详细说明。本实施例以本发明技术方案为前提进行实施,给出了详细的实施方式和具体的操作过程,但本发明的保护范 围不限于下述的实施例。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation and specific operation process are provided, but the protection scope of the present invention is not limited to the following embodiments.
一种大型海上风力机叶尖融合小翼,如图1所示,该小翼与风力机的叶片叶尖 部分的翼型相同并光滑过渡,小翼朝向叶片吸力面弯曲,且小翼的弯曲倾斜角度为 50°~60°。小翼的翼型为NACA64翼型。小翼的展向长度为风轮半径的3%~5%, 小翼的弯曲半径为风力机的风轮半径的1%~3%。A large-scale offshore wind turbine blade tip fusion winglet, as shown in Figure 1, the winglet has the same airfoil shape as the blade tip part of the wind turbine and has a smooth transition, the winglet is curved towards the suction surface of the blade, and the curvature of the winglet The inclination angle is 50°~60°. The airfoil of the winglet is NACA64 airfoil. The spanwise length of the winglet is 3% to 5% of the radius of the rotor, and the bending radius of the winglet is 1% to 3% of the radius of the rotor of the wind turbine.
在保持风轮扫风面积不变的条件下,最优小翼倾斜角度,使得叶片和小翼所产 生的总功率最大。Under the condition of keeping the sweeping area of the wind rotor constant, the optimal winglet inclination angle maximizes the total power generated by the blade and the winglet.
如图1为本申请的叶尖融合小翼,小翼朝向吸力面弯曲,如图2为海上风力机 叶片叶尖小翼的局部图。Fig. 1 is the blade tip fusion winglet of the present application, and the winglet is bent towards the suction surface, and Fig. 2 is a partial view of the blade tip winglet of an offshore wind turbine blade.
本申请的叶尖融合小翼由翼根和翼尖翼型及等效长度、弯曲半径和倾斜角度决定,该叶尖小翼的重要平面几何参数为:The blade tip fusion winglet of the present application is determined by the wing root and wing tip airfoil and the equivalent length, bending radius and inclination angle. The important plane geometric parameters of the blade tip winglet are:
1)小翼朝向:小翼朝向吸力面,即朝向风力机下游;1) Winglet orientation: the winglet faces the suction surface, that is, toward the downstream of the wind turbine;
2)弯曲半径:小翼与叶片本体连接处的弧形弯曲半径;2) Bending radius: the arc bending radius of the connection between the winglet and the blade body;
3)等效长度:小翼在叶片长度方向上的投影长度;3) Equivalent length: the projected length of the winglet in the length direction of the blade;
4)倾斜角度:小翼弯曲长度方向与叶片的夹角;4) Inclination angle: the angle between the bending length direction of the winglet and the blade;
5)小翼翼型:指叶尖小翼采用NACA64翼型。5) Small wing airfoil: Refers to the blade tip winglet adopting NACA64 airfoil.
对含有本申请小翼的叶片进行测试,在深远海风力机受到海洋环境的影响产生艏摇、纵摇、纵荡等运动条件下,添加该新型融合叶尖小翼,具体参数如表1所示。 风力机A表示未添加叶尖融合小翼的海上风力机,风力机B表示添加叶尖融合小 翼的风力机。在风力机额定风速11.4m/s条件下,分别对这两种风力机用CFD (Computational FluidDynamic)方法计算其功率系数Cp、轴向推力系数Ct,对比 分析其气动性能,计算结果如表1所示。The blades containing the winglets of the present application were tested, and the new fusion tip winglets were added under the conditions of yaw, pitch, surge and other motions of the deep-sea wind turbine under the influence of the marine environment. The specific parameters are shown in Table 1. Show. Wind turbine A represents an offshore wind turbine without tip fusion winglets, and wind turbine B represents a wind turbine with blade tip fusion winglets added. Under the condition of wind turbine rated wind speed of 11.4m/s, CFD (Computational FluidDynamic) method is used to calculate the power coefficient C p and axial thrust coefficient C t of these two wind turbines, and compare and analyze their aerodynamic performance. The calculation results are shown in the table 1.
表1 有无融合小翼海上风力机气动性能结果Table 1 Aerodynamic performance results of offshore wind turbines with or without fused winglets
由表1可以看出,在风力机额定运行工况条件下,相对于A风力机,B风力 机功率系数提高4.30%,轴向推力系数提高4.29%,表明加装了融合小翼以后,风 力机的功率提升率大于轴向推力提升率。It can be seen from Table 1 that under the rated operating conditions of the wind turbine, compared with the wind turbine A, the power coefficient of the B wind turbine is increased by 4.30%, and the axial thrust coefficient is increased by 4.29%. The power increase rate of the engine is greater than the axial thrust increase rate.
在深远海风力机受到海洋环境的影响产生艏摇、纵摇、纵荡等运动条件下,如 图3(a)、3(b),在叶片压力面,两种叶片的压力分布基本相同,融合小翼表 面的压力值大于叶片表面压力值;如图3(c)、3(d),在叶片吸力面,带叶尖 融合小翼叶片的负压区较大且压力值低于无小翼叶片,因此带融合小翼叶片的表面 压差更大,功率输出增大。如图4所示为截取距叶尖1m处的叶片截面翼型表面压 力分布,可以看到在翼型前部,有融合小翼叶片的吸力面压力值低于无小翼叶片。Under the conditions of yaw, pitch, surge and other motions of deep-sea wind turbines affected by the marine environment, as shown in Figure 3(a) and 3(b), on the pressure surface of the blade, the pressure distribution of the two blades is basically the same, The pressure value on the surface of the fused winglet is greater than that on the surface of the blade; as shown in Figure 3(c) and 3(d), on the suction surface of the blade, the negative pressure area of the blade with the tip fused winglet is larger and the pressure value is lower than that without the small winglet. Wing blades, so with fused winglet blades the surface pressure difference is greater and the power output is increased. As shown in Figure 4, the airfoil surface pressure distribution of the blade section at 1m from the blade tip is intercepted. It can be seen that at the front of the airfoil, the suction surface pressure value of the blade with fused winglets is lower than that of the blade without winglets.
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US20190145375A1 (en) * | 2017-11-13 | 2019-05-16 | Wichita State University | Retrofit winglets for wind turbines |
CN210483953U (en) * | 2019-05-24 | 2020-05-08 | 上海电力学院 | A large offshore wind turbine blade tip fusion winglet and wind turbine |
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CN111550363B (en) * | 2020-05-22 | 2021-07-30 | 北京博比风电科技有限公司 | Blade tip winglet, wind turbine blade and blade synergy calculation method thereof |
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