CN106762389A - Blade tip, blade of wind generating set and blade tip installation method - Google Patents
Blade tip, blade of wind generating set and blade tip installation method Download PDFInfo
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- CN106762389A CN106762389A CN201611186181.7A CN201611186181A CN106762389A CN 106762389 A CN106762389 A CN 106762389A CN 201611186181 A CN201611186181 A CN 201611186181A CN 106762389 A CN106762389 A CN 106762389A
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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
- 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
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape 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
- F05B2240/307—Blade tip, e.g. winglets
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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
- F05B2260/00—Function
- F05B2260/96—Preventing, counteracting or reducing vibration or noise
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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
- F05B2260/00—Function
- F05B2260/96—Preventing, counteracting or reducing vibration or noise
- F05B2260/962—Preventing, counteracting or reducing vibration or noise by means creating "anti-noise"
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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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- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Wind Motors (AREA)
Abstract
本发明提供一种叶尖、风力发电机组叶片及叶尖的安装方法。所述叶尖包括:主体,所述主体包括压力面和吸力面;小翼,所述小翼形成在所述主体的末端,并朝向所述吸力面或压力面弯倾;主梁,所述主梁包括设置于所述压力面和所述吸力面所构成的外壳内部的第一部分和延伸至所述外壳外部的第二部分。所述风力发电机组叶片包括叶根、叶身和所述叶尖。所述安装方法包括将风力发电机组叶片的原叶尖截掉;将所述叶尖安装到被截掉原叶尖后的叶身上。根据本发明的叶尖可利用流场特性增加小翼部分的气动升力分量的利用、增加对风能捕获的效率;此外,所述叶尖能够安装到现役风力发电机组的叶片上,从而提高风力发电机组的整体效率和性能。
The invention provides a blade tip, a wind turbine blade and an installation method of the blade tip. The blade tip includes: a main body, the main body including a pressure surface and a suction surface; a winglet, the winglet is formed at the end of the main body and is inclined toward the suction surface or the pressure surface; a main beam, the The main beam includes a first part disposed inside the housing formed by the pressure surface and the suction surface, and a second part extending to the outside of the housing. The wind turbine blade includes a blade root, a blade body and the blade tip. The installation method includes cutting off the original blade tip of the wind turbine blade; and installing the blade tip onto the blade body after the original blade tip is cut off. The blade tip according to the present invention can use the flow field characteristics to increase the utilization of the aerodynamic lift component of the winglet part and increase the efficiency of wind energy capture; in addition, the blade tip can be installed on the blades of the active wind turbine generator, thereby improving wind power generation. The overall efficiency and performance of the unit.
Description
技术领域technical field
本发明涉及风力发电技术领域,更具体地,涉及一种叶尖、风力发电机组叶片及叶尖的安装方法。The invention relates to the technical field of wind power generation, and more specifically, to a blade tip, a blade of a wind power generating set, and a method for installing the blade tip.
背景技术Background technique
风力发电机组叶片是现代风力发电机组中用来捕获风能的关键部件,风力发电机组叶片运行时,压力面的压强比吸力面高,在压强差的作用下,压力面的气流就绕过叶尖流向吸力面,这样就使压力面的流线由叶根向叶尖倾斜,而吸力面的流线则由叶尖偏向叶根。由于压力面和吸力面气流在后缘处具有不同的流向,于是就形成漩涡,向后流动形成叶尖涡在运行过程中由于吸力面和压力面的压差原因,在叶尖形成叶尖涡,从而导致产生叶尖噪声、降低风力发电机组整体气动效率。The blade of a wind turbine is a key component used to capture wind energy in a modern wind turbine. When the blade of a wind turbine is running, the pressure on the pressure side is higher than the suction side. Under the action of the pressure difference, the airflow on the pressure side bypasses the tip of the blade. Flow to the suction side, so that the streamline on the pressure side is inclined from the blade root to the blade tip, while the streamline on the suction side is biased from the blade tip to the blade root. Since the airflow on the pressure surface and the suction surface have different flow directions at the trailing edge, a vortex is formed, and the backward flow forms a tip vortex. During operation, due to the pressure difference between the suction surface and the pressure surface, a tip vortex is formed at the blade tip. , resulting in blade tip noise and reduced overall aerodynamic efficiency of the wind turbine.
借鉴民用飞机中普遍应用的翼稍小翼,带有叶尖小翼的叶片设计可以减少叶尖噪声、提高风力发电机组整体气动效率。但是,现有的带有叶尖小翼的叶片仍存在很多问题,例如,叶尖后缘在运行过程中存在湍流噪声等后缘噪声。Referring to the winglets commonly used in civil aircraft, the blade design with tiplets can reduce blade tip noise and improve the overall aerodynamic efficiency of wind turbines. However, there are still many problems in the existing blades with tiplets, for example, there are trailing edge noises such as turbulent flow noise at the trailing edge of the blade tip during operation.
此外,目前大部分在役的风力发电机组的叶片没有配置叶尖小翼,这将会大大降低风力发电机组的整体效率和性能,因此,需要研究一种能够安装到现役风力发电机组的叶片上的叶尖小翼。In addition, most of the blades of wind turbines currently in service are not equipped with tiplets, which will greatly reduce the overall efficiency and performance of wind turbines. Therefore, it is necessary to study a blade that can be installed on existing wind turbines. of leaflets.
发明内容Contents of the invention
为了解决叶尖涡导致的能量损失以及后缘产生的噪声等问题,根据本发明的一方面,提供一种叶尖、包括该叶尖的风力发电机组叶片及该叶尖的安装方法。In order to solve the problems of energy loss caused by blade tip vortex and noise generated by the trailing edge, according to one aspect of the present invention, a blade tip, a wind power generator blade including the blade tip, and a method for installing the blade tip are provided.
根据本发明的示例性实施例,提供一种用于风力发电机组叶片的叶尖,所述叶尖包括:主体,所述主体包括压力面和吸力面;小翼,所述小翼形成在所述主体的末端,并朝向所述吸力面或所述压力面弯倾;主梁,所述主梁包括设置于所述压力面和所述吸力面所构成的外壳内部的第一部分和延伸至所述外壳外部的第二部分。According to an exemplary embodiment of the present invention, there is provided a blade tip for a wind turbine blade, the blade tip comprising: a main body including a pressure surface and a suction surface; a winglet formed on the the end of the main body and bend towards the suction surface or the pressure surface; the main beam, the main beam includes a first part arranged inside the shell formed by the pressure surface and the suction surface and extends to the The second part on the outside of the enclosure.
根据本发明的示例性实施例,所述小翼以30°至80°之间的外倾角朝向所述吸力面或所述压力面弯倾。According to an exemplary embodiment of the invention, the winglet is bent towards the suction side or the pressure side with a camber angle between 30° and 80°.
根据本发明的示例性实施例,所述主体的后缘和/或所述小翼的后缘可设置有锯齿部。According to an exemplary embodiment of the present invention, the trailing edge of the main body and/or the trailing edge of the winglet may be provided with serrations.
优选地,所述锯齿部可包括连续或间断地设置的多个锯齿。Preferably, the sawtooth portion may include a plurality of sawteeth arranged continuously or discontinuously.
优选地,所述多个锯齿中的相邻锯齿间的夹角可设置在20°至60°之间。Preferably, the included angle between adjacent saw teeth among the plurality of saw teeth can be set between 20° and 60°.
优选地,所述多个锯齿中的相邻锯齿间的夹角可设置为40°。Preferably, the included angle between adjacent saw teeth among the plurality of saw teeth may be set to 40°.
优选地,所述第一部分可粘接到所述压力面和所述吸力面中的至少一个上。Preferably, said first portion is bondable to at least one of said pressure side and said suction side.
根据本发明的示例性实施例,所述叶尖还可包括:接线盒,设置在所述主梁的第一部分的侧面上。According to an exemplary embodiment of the present invention, the blade tip may further include: a junction box disposed on a side of the first part of the main spar.
根据本发明的示例性实施例,所述叶尖还包括:避雷接闪部,位于所述小翼的末端,所述避雷接闪部通过避雷导线连接到所述接线盒。According to an exemplary embodiment of the present invention, the blade tip further includes: a lightning arrester located at the end of the winglet, and the lightning arrester is connected to the junction box through a lightning conductor.
其中,所述避雷接闪部可与所述小翼一体成型;或者,所述避雷接闪部也可拆卸地安装到所述小翼上。Wherein, the lightning arrester can be formed integrally with the winglet; or, the lightning arrester can also be detachably mounted on the winglet.
优选地,所述避雷接闪部可设置有排水孔。Preferably, the lightning arrester may be provided with drainage holes.
根据本发明的示例性实施例,所述叶尖还可包括:操作孔,形成在所述吸力面或压力面上。According to an exemplary embodiment of the present invention, the blade tip may further include: an operation hole formed on the suction surface or the pressure surface.
根据本发明的另一示例性实施例,提供一种风力发电机组叶片,所述叶片包括叶根、叶身以及如上所述的叶尖。According to another exemplary embodiment of the present invention, a blade of a wind power generating set is provided, and the blade includes a blade root, a blade body, and the above-mentioned blade tip.
其中,如上所述的叶尖可与所述叶身通过一体成型而形成为一体,或者,也可将另外成型的所述叶尖安装到叶身上。Wherein, the above-mentioned blade tip can be integrally formed with the blade body through integral molding, or the additionally shaped blade tip can also be installed on the blade body.
根据本发明的另一示例性实施例,一种风力发电机组叶片的叶尖的安装方法,所述安装方法包括:将风力发电机组叶片的原叶尖截掉;将如上所述的叶尖安装到被截掉原叶尖后的叶身上。According to another exemplary embodiment of the present invention, a method for installing the tip of a blade of a wind power generating set, the installation method includes: cutting off the original tip of the blade of a wind generating set; To the leaf body after the original leaf tip has been amputated.
优选地,将叶尖安装到被截掉原叶尖后的叶身上的步骤可包括:将叶尖的主梁插入到被截掉原叶尖后的叶身的内腔中,使得所述主梁的靠近前缘和/或靠近后缘的侧面与叶身的内腔中的腹板的侧面相接触;将所述主梁和所述腹板的相接触的侧面利用粘接胶进行固定连接;将所述主梁的上下两个表面中的至少一个面与叶身的压力面和吸力面中的至少一个面接触并粘接。Preferably, the step of installing the blade tip on the blade body after the original blade tip has been cut off may include: inserting the main beam of the blade tip into the inner cavity of the blade body after the original blade tip has been cut off, so that the main The side of the beam near the front edge and/or the side near the trailing edge is in contact with the side of the web in the inner cavity of the blade body; the side of the main beam in contact with the web is fixedly connected by adhesive ; At least one of the upper and lower surfaces of the main beam is in contact with at least one of the pressure surface and the suction surface of the blade body and bonded.
根据本发明的用于风力发电机组叶片的叶尖通过将其小翼设置为朝向吸力面或压力面弯倾,可利用流场特性增加小翼部分的气动升力分量的利用、增加对风能捕获的效率;另外,通过在后缘设置锯齿部,可降低后缘湍流噪声。According to the tip of the blade of the wind power generator set according to the present invention, by setting its winglets to be inclined toward the suction surface or the pressure surface, the flow field characteristics can be used to increase the utilization of the aerodynamic lift component of the winglet part and increase the capture of wind energy. Efficiency; in addition, by setting serrations on the trailing edge, the trailing edge turbulent noise can be reduced.
另外,所述叶尖可安装到现役风力发电机组叶片上,从而可提高现役风力发电机组的整体效率和性能。当将叶尖安装到现役风力发电机组的被被截掉原叶尖后的叶身上时,通过叶尖的主梁与叶身的腹板之间的粘接、叶尖的主梁与叶身的压力面和吸力面之间的粘接,可使叶尖与叶身之间的准确定位更加准确,同时,可增加叶尖与叶身之间的连接强度,从而使安装质量及安装操作的可控性得到明显提高。In addition, the blade tips may be mounted to blades of existing wind turbines, thereby improving the overall efficiency and performance of the existing wind turbines. When the blade tip is installed on the blade body after the original blade tip of the active wind turbine is cut off, through the bonding between the main beam of the blade tip and the web of the blade body, the main beam of the blade tip and the blade body The bonding between the pressure surface and the suction surface can make the accurate positioning between the blade tip and the blade body more accurate, and at the same time, it can increase the connection strength between the blade tip and the blade body, so that the installation quality and installation operation are improved. Controllability has been significantly improved.
附图说明Description of drawings
下面结合附图对本发明的示例性实施例进行详细描述,本发明的以上和其它特点及优点将变得更加清楚,附图中:Exemplary embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, and the above and other features and advantages of the present invention will become clearer. In the accompanying drawings:
图1是根据本发明的示例性实施例的风力发电机组叶片的示意图;Fig. 1 is a schematic diagram of a wind turbine blade according to an exemplary embodiment of the present invention;
图2是根据本发明的示例性实施例的用于风力发电机组叶片的叶尖的示意图;Fig. 2 is a schematic diagram of a blade tip for a wind turbine blade according to an exemplary embodiment of the present invention;
图3是将图2中的吸力面移除之后的用于风力发电机组叶片的叶尖的示意图;Fig. 3 is a schematic diagram of a blade tip for a blade of a wind power generating set after the suction surface in Fig. 2 is removed;
图4是将根据示例性实施例的用于风力发电机组叶片的叶尖安装于被截掉原叶尖后的叶身上的局部示意图;Fig. 4 is a partial schematic diagram of installing a blade tip for a blade of a wind power generator set on a blade body after the original blade tip is cut off according to an exemplary embodiment;
图5A和图5B分别示出了没有设置小翼的常规叶尖对气流的作用效果和根据本发明的示例性实施例的用于风力发电机组叶片的叶尖对气流的作用效果;5A and FIG. 5B respectively show the effect of a conventional blade tip without winglets on airflow and the effect of a blade tip used for a wind turbine blade according to an exemplary embodiment of the present invention on airflow;
图6示出了根据本发明的示例性实施例的用于风力发电机组叶片的叶尖的后缘的锯齿部对气流的作用效果。Fig. 6 shows the effect of serrations on the airflow of the trailing edge of the blade tip of a wind turbine blade according to an exemplary embodiment of the present invention.
具体实施方式detailed description
现在将参照附图更全面的描述本发明的实施例,在附图中示出了本发明的示例性实施例。Embodiments of the invention will now be described more fully with reference to the accompanying drawings, in which exemplary embodiments of the invention are shown.
下面将结合图1至图3描述根据本发明的示例性实施例的用于风力发电机组叶片的叶尖和包括该叶尖的风力发电机组叶片。A blade tip for a wind power generator blade and a wind power generator blade including the blade tip according to an exemplary embodiment of the present invention will be described below with reference to FIGS. 1 to 3 .
图1是根据本发明的示例性实施例的风力发电机组叶片的示意图;图2是根据本发明的示例性实施例的用于风力发电机组叶片的叶尖3的示意图;图3是将图2中的吸力面6移除之后的用于风力发电机组叶片的叶尖3的示意图。Fig. 1 is a schematic diagram of a wind power generator blade according to an exemplary embodiment of the present invention; Fig. 2 is a schematic diagram of a blade tip 3 for a wind power generator blade according to an exemplary embodiment of the present invention; Fig. 3 is a schematic diagram of Fig. 2 A schematic diagram of a blade tip 3 for a wind turbine blade after removal of the suction face 6 in .
如图1所示,根据本发明的示例性实施例的风力发电机组叶片包括叶根1、叶身2以及叶尖3,其中,叶根1用于将叶片安装到轮毂上,叶身2从叶根1延伸,叶尖3相对于叶身2位于与叶根1相对的一端。叶身2包括压力面和吸力面,并且压力面和吸力面通过前缘和后缘的粘接而彼此连接。在根据本发明的一个示例性实施例中,叶尖3可以与叶身2彼此分开地形成,而后安装到叶身2上。然而,本发明不限于此,叶尖3与叶身2也可以通过一体成型而形成为一体。As shown in FIG. 1 , a wind turbine blade according to an exemplary embodiment of the present invention includes a blade root 1, a blade body 2 and a blade tip 3, wherein the blade root 1 is used for mounting the blade on the hub, and the blade body 2 is The blade root 1 extends, and the blade tip 3 is located at the end opposite to the blade root 1 relative to the blade body 2 . The airfoil 2 includes a pressure side and a suction side, and the pressure side and the suction side are connected to each other by bonding of the leading edge and the trailing edge. In an exemplary embodiment according to the present invention, the blade tip 3 may be formed separately from the airfoil 2 and then mounted on the airfoil 2 . However, the present invention is not limited thereto, and the blade tip 3 and the blade body 2 may also be integrally formed by integral molding.
参照图2和图3,根据本发明的示例性实施例的叶尖3可包括主体31和小翼32,主体31包括压力面5和吸力面6,并且压力面5和所述吸力面6在前缘8和后缘9处相连(可粘接)而形成主体31的外壳,小翼32形成在主体31的末端,并以预定外倾角α朝向吸力面6弯倾。在此,所述预定外倾角α可指主体31的中心轴线与小翼32的中心轴线之间所形成的夹角,也就是说,所述预定外倾角α表示的是小翼32偏离主体31的倾角。为便于参考,可以用如图3中所示的小翼32的后缘偏离主体31的后缘的倾角α来示意性地示出所述预定外倾角α。所述预定外倾角α可设置在约30°至80°之间。优选地,可将所述预定外倾角α设置为约40°、约45°或约60°。小翼32的长度可设置为约0.5m至1.5m,优选地,可设置为约1m或约0.8m。根据本发明的示例性实施例,可通过将主体31的末端部分按照预定外倾角朝向吸力面6弯倾而形成小翼32。前述的压力面和吸力面,不管是叶身上的,还是叶尖上的,均可以用蒙皮来构成。Referring to FIGS. 2 and 3 , a blade tip 3 according to an exemplary embodiment of the present invention may include a main body 31 and a winglet 32 , the main body 31 includes a pressure surface 5 and a suction surface 6 , and the pressure surface 5 and the suction surface 6 are positioned at The leading edge 8 and the trailing edge 9 are connected (bonded) to form the shell of the main body 31 , and the winglet 32 is formed at the end of the main body 31 and is inclined toward the suction surface 6 at a predetermined camber angle α. Here, the predetermined camber angle α may refer to the angle formed between the central axis of the main body 31 and the central axis of the winglet 32 , that is to say, the predetermined camber angle α indicates that the winglet 32 deviates from the main body 31 inclination. For ease of reference, the predetermined camber angle α may be schematically shown by the inclination angle α of the trailing edge of the winglet 32 from the trailing edge of the main body 31 as shown in FIG. 3 . The predetermined camber angle α may be set between about 30° and 80°. Preferably, the predetermined camber angle α may be set to about 40°, about 45° or about 60°. The length of the winglet 32 can be set to about 0.5m to 1.5m, preferably, can be set to about 1m or about 0.8m. According to an exemplary embodiment of the present invention, the winglet 32 may be formed by bending an end portion of the main body 31 toward the suction surface 6 at a predetermined camber angle. The aforementioned pressure surface and suction surface, no matter on the blade body or on the blade tip, can be formed with skins.
此外,叶尖3的后缘9可设置有锯齿部,所述锯齿部可通过切割后缘9而形成,或者,所述锯齿部也可与叶尖3分开地形成而后安装到后缘9上。在此,锯齿部可包括多个锯齿91,所述多个锯齿91可连续地设置在后缘9上。然而,本发明不限于此,多个锯齿91可间断地设置在后缘9上,例如,如图2和图3所示,在主体31和小翼32的后缘9均设置有包括多个锯齿91的锯齿部,而在主体31和小翼32之间的弯曲过渡部分上不设置锯齿部,这样可以增强弯曲过渡部分处的强度。Furthermore, the trailing edge 9 of the blade tip 3 may be provided with serrations, which may be formed by cutting the trailing edge 9, or alternatively, the serrations may be formed separately from the blade tip 3 and then mounted on the trailing edge 9 . Here, the serration may comprise a plurality of serrations 91 which may be arranged continuously on the trailing edge 9 . However, the present invention is not limited thereto, and a plurality of serrations 91 may be discontinuously arranged on the trailing edge 9. For example, as shown in FIGS. The sawtooth portion of the sawtooth 91, and no serration is provided on the curved transition portion between the main body 31 and the winglet 32, so that the strength at the curved transition portion can be enhanced.
其中,所述多个锯齿91中的相邻锯齿91间的夹角可设置为大约20°至60°。根据本发明的另一示例性实施例,相邻锯齿91间的夹角可设置为大约30°至50°。优选地,可将相邻锯齿91间的夹角设置为大约40°。Wherein, the included angle between adjacent saw teeth 91 among the plurality of saw teeth 91 may be set to about 20° to 60°. According to another exemplary embodiment of the present invention, the included angle between adjacent saw teeth 91 may be set at approximately 30° to 50°. Preferably, the included angle between adjacent saw teeth 91 can be set to about 40°.
根据本发明的示例性实施例的叶尖3还可包括主梁7,以增强叶尖的强度。主梁7可包括设置于压力面和吸力面形成的外壳内部的第一部分和延伸至所述外壳外部的第二部分,其中,第一部分可通过利用粘接胶固定粘接到压力面5和吸力面6中的至少一个上而设置于所述外壳内部,延伸至所述外壳外部的第二部分的长度在约0.3m至1m之间,优选地,可将第二部分的长度设置为约0.6m。在此,如果第二部分的长度太短,则在将叶尖3连接到叶身2上时,主梁7不能够提供足够强的辅助连接强度;如果第二部分的长度太长,则可能会影响主梁7与叶身2的连接操作。The blade tip 3 according to the exemplary embodiment of the present invention may further include a main spar 7 to enhance the strength of the blade tip. The main beam 7 may include a first part disposed inside the casing formed by the pressure surface and the suction surface and a second part extending to the outside of the casing, wherein the first part may be fixedly bonded to the pressure surface 5 and the suction surface by using an adhesive. At least one of the surfaces 6 is arranged inside the shell, and the length of the second part extending to the outside of the shell is between about 0.3m and 1m. Preferably, the length of the second part can be set to about 0.6m. m. Here, if the length of the second part is too short, the main spar 7 cannot provide sufficient auxiliary connection strength when the blade tip 3 is connected to the airfoil 2; if the length of the second part is too long, it may It will affect the connection operation between the main beam 7 and the airfoil 2 .
根据本发明的示例性实施例,如图2和图3中所示,主梁7可设置为长方体形状,即,端部呈矩形。然而,本发明不限于此,主梁7也可设置为端部呈D形、O形或C形等的其他形状。此外,主梁7的数量可根据实际情况而设置为一个或者更多个。另外,主梁7也可设置为腹板的形式。According to an exemplary embodiment of the present invention, as shown in FIGS. 2 and 3 , the main beam 7 may be configured in a cuboid shape, ie, the ends are rectangular. However, the present invention is not limited thereto, and the main beam 7 may also be arranged in other shapes such as a D-shape, an O-shape, or a C-shape at the end. In addition, the number of main girders 7 can be set to one or more according to actual conditions. In addition, the main girder 7 can also be arranged in the form of a web.
根据本发明的示例性实施例的叶尖3还可包括接线盒12和操作孔13,接线盒12可设置在主梁7的第一部分的侧面上,以便于在将叶尖3安装到叶身2时执行诸如避雷导线的连接等操作,在完成接线操作后再将操作孔13利用盖板进行密封。The blade tip 3 according to the exemplary embodiment of the present invention may also include a junction box 12 and an operation hole 13, and the junction box 12 may be arranged on the side of the first part of the main spar 7, so as to facilitate the installation of the blade tip 3 to the airfoil. At 2 o'clock, operations such as the connection of lightning conductors are performed, and the operation hole 13 is sealed with a cover plate after the wiring operation is completed.
根据本发明的示例性实施例的叶尖3还可包括避雷接闪部10,避雷接闪部10位于所述小翼32的末端,避雷接闪部10通过设置于所述外壳内部的避雷导线11连接到所述接线盒12。在此,避雷接闪部10可以与小翼32一体地形成。然而,本发明不限于此,避雷接闪部10也可与小翼32分开地形成而后可拆卸地安装到小翼32上,以方便进行更换。具体地,可将另外成型的避雷接闪部10通过螺栓固定到小翼32上。The blade tip 3 according to the exemplary embodiment of the present invention may also include a lightning protection and lightning receiving part 10, which is located at the end of the winglet 32, and the lightning receiving and receiving part 10 passes through a lightning protection wire arranged inside the casing 11 is connected to the junction box 12. Here, the lightning arrester 10 may be integrally formed with the winglet 32 . However, the present invention is not limited thereto, and the lightning arrester 10 may also be formed separately from the winglet 32 and then detachably mounted on the winglet 32 for easy replacement. Specifically, the additionally formed lightning arrester 10 may be fixed to the winglet 32 by bolts.
避雷接闪部10可利用铝或铝合金材料制成。然而,本发明不限于此,避雷接闪部10也可由其他耐腐蚀性强的导电材料形成。The lightning arrester 10 can be made of aluminum or aluminum alloy. However, the present invention is not limited thereto, and the lightning arrester 10 may also be formed of other conductive materials with strong corrosion resistance.
另外,避雷接闪部10上可设置有排水孔,从而避免了在叶片的吸力面或压力面上开排水孔而对叶片造成损害。In addition, the lightning arrester 10 may be provided with drainage holes, so as to avoid damage to the blade caused by opening drainage holes on the suction surface or pressure surface of the blade.
根据本发明的另一示例性实施例,叶尖3的小翼32可设置为朝向压力面5弯倾。根据所述另一示例性实施例的小翼32朝向压力面5弯倾的叶尖3除了在小翼32的弯倾方向方面不同于上述示例性实施例之外,其他特征均与小翼32朝向吸力面6弯倾的实施例相同或相似,因此,在此将省略对相同或相似的特征的描述。According to another exemplary embodiment of the invention, the winglet 32 of the blade tip 3 may be arranged to be bent towards the pressure face 5 . The blade tip 3 of the winglet 32 according to the other exemplary embodiment is bent towards the pressure surface 5 except that the direction of the winglet 32 is different from the above exemplary embodiment, and other features are similar to the winglet 32. Embodiments that are inclined toward the suction surface 6 are the same or similar, and therefore descriptions of the same or similar features will be omitted here.
在根据本发明的另一示例性实施例中,小翼32形成在叶尖3的主体31的末端,并以预定外倾角α朝向压力面5弯倾。在此,所述预定外倾角α可指主体31的中心轴线与小翼32的中心轴线之间所形成的夹角,也就是说,所述预定外倾角α表示的是小翼32偏离主体31的倾角。所述预定外倾角α可设置在约30°至80°之间。优选地,可将所述预定外倾角α设置为约40°、约45°或约60°。小翼32的长度可设置为约0.5m至1.5m,优选地,可设置为约1m或约0.8m。根据本发明的示例性实施例,可通过将主体31的末端部分按照预定外倾角朝向压力面5弯倾而形成小翼32。前述的压力面和吸力面,不管是叶身上的,还是叶尖上的,均可以用蒙皮来构成。In another exemplary embodiment according to the present invention, the winglet 32 is formed at the end of the main body 31 of the blade tip 3 and is inclined towards the pressure surface 5 at a predetermined camber angle α. Here, the predetermined camber angle α may refer to the angle formed between the central axis of the main body 31 and the central axis of the winglet 32 , that is to say, the predetermined camber angle α indicates that the winglet 32 deviates from the main body 31 inclination. The predetermined camber angle α may be set between about 30° and 80°. Preferably, the predetermined camber angle α may be set to about 40°, about 45° or about 60°. The length of the winglet 32 can be set to about 0.5m to 1.5m, preferably, can be set to about 1m or about 0.8m. According to an exemplary embodiment of the present invention, the winglet 32 may be formed by bending an end portion of the main body 31 toward the pressure surface 5 at a predetermined camber angle. The aforementioned pressure surface and suction surface, no matter on the blade body or on the blade tip, can be formed with skins.
图4是将根据示例性实施例的用于风力发电机组叶片的叶尖3安装于被截掉原叶尖后的叶身2上的局部示意图。下面将参照图4描述根据本发明的示例性实施例的风力发电机组叶片的叶尖3的安装方法。Fig. 4 is a partial schematic diagram of installing a blade tip 3 for a blade of a wind power generator set on the blade body 2 after the original blade tip is cut off according to an exemplary embodiment. The method for installing the blade tip 3 of the blade of a wind power generating set according to an exemplary embodiment of the present invention will be described below with reference to FIG. 4 .
根据本发明的示例性实施例,风力发电机组叶片的叶尖3的安装方法可包括:将风力发电机组叶片的原叶尖截掉;将根据本发明的示例性实施例的风力发电机组叶片的叶尖3安装到被截掉原叶尖后的叶身2上。According to an exemplary embodiment of the present invention, the installation method of the tip 3 of the blade of the wind power generating set may include: cutting off the original tip of the blade of the wind generating set; The blade tip 3 is installed on the blade body 2 after the original blade tip is cut off.
具体地,将叶尖3安装到被截掉原叶尖后的叶身2上的步骤可包括:将叶尖3的压力面5和吸力面6分别与被截掉原叶尖后的叶身2的压力面和吸力面对齐并利用粘接胶进行粘接;在完成粘接之后,再利用玻璃纤维将叶尖3和叶身2的所粘接的端面相连接,以起到加强连接和光顺外形的作用。在此需要注意的是,在截掉原叶尖的过程中,要注意保留原有的避雷导线,以便于和叶尖3上的避雷接闪部10相连。Specifically, the step of installing the blade tip 3 on the airfoil 2 after the original blade tip has been cut off may include: respectively connecting the pressure surface 5 and the suction surface 6 of the blade tip 3 with the airfoil body after the original blade tip has been cut off. The pressure surface and the suction surface of 2 are aligned and bonded with adhesive glue; after the bonding is completed, glass fibers are used to connect the bonded end faces of blade tip 3 and blade body 2 to strengthen the connection and smooth shape. It should be noted here that during the process of cutting off the original blade tip, attention should be paid to retaining the original lightning conductor so as to be connected to the lightning arrester 10 on the blade tip 3 .
在叶尖3设置有主梁7的情况下,将叶尖3安装到被截掉原叶尖后的叶身2上的步骤可包括:将叶尖3的主梁7插入到被截掉原叶尖后的叶身2的内腔中,使主梁7的靠近前缘8和/或靠近后缘9的侧面与叶身2的内腔中的腹板14的侧面相接触;将主梁7和腹板14的相接触的侧面利用粘接胶进行固定连接;将主梁7的上下两个表面中的至少一个面与叶身2的压力面和吸力面中的至少一个面接触并粘接;在完成粘接之后,再利用玻璃纤维将叶尖3和叶身2的所粘接的端面相连接,以起到加强连接和光顺外形的作用。在此同样需要注意的是,在截掉原叶尖的过程中,要注意保留原有的避雷导线,以便于和叶尖3上的避雷接闪部10相连。In the case that the blade tip 3 is provided with a main beam 7, the step of installing the blade tip 3 on the blade body 2 after the original blade tip has been cut off may include: inserting the main beam 7 of the blade tip 3 into the original blade tip that has been cut off. In the inner chamber of the airfoil 2 behind the blade tip, make the side of the main beam 7 near the leading edge 8 and/or the side near the trailing edge 9 contact with the side of the web 14 in the inner chamber of the blade air 2; 7 and the contacting side of the web 14 are fixedly connected by adhesive glue; at least one of the upper and lower surfaces of the main beam 7 is in contact with at least one of the pressure surface and the suction surface of the airfoil 2 and glued After the bonding is completed, glass fibers are used to connect the bonded end surfaces of the blade tip 3 and the blade body 2, so as to strengthen the connection and smooth the shape. It should also be noted here that in the process of cutting off the original tip, attention should be paid to retaining the original lightning conductor so as to be connected to the lightning arrester 10 on the tip 3 .
根据本发明的示例性实施例,通过叶尖的主梁和叶身的腹板的粘接以及叶尖的主梁与叶身的压力面、吸力面的粘接以及叶尖的压力面、吸力面分别与叶身的压力面、吸力面之间的粘接,从而可使叶尖与叶身的定位更加准确、连接强度更强,并且可提高叶尖的安装质量与操作可控性。According to an exemplary embodiment of the present invention, through the bonding of the main spar of the blade tip and the web of the blade body, the bonding of the main beam of the blade tip and the pressure surface and suction surface of the blade body, and the pressure surface and suction surface of the blade tip The bonding between the surface and the pressure surface and suction surface of the blade body can make the positioning of the blade tip and the blade body more accurate, the connection strength is stronger, and the installation quality and operation controllability of the blade tip can be improved.
根据本发明的示例性实施例,通过在叶尖的末端形成倾向于吸力面或压力面的小翼,可利用流场特性增加小翼部分对气动升力分量的利用,从而可增加对风能捕获的效率。图5A和图5B分别示出了没有设置小翼的常规叶尖3′对气流的作用效果和根据本发明的示例性实施例的用于风力发电机组叶片的叶尖3对气流的作用效果。如5A所示,对于没有设置小翼的常规叶尖3′来说,气流从压力面绕到吸力面,在吸力面形成漩涡,气流存在明显的分离现象。如图5B所示,由于根据本发明的示例性实施例的用于风力发电机组叶片的叶尖3包含倾向于吸力面的小翼,小翼可阻挡从压力面绕到吸力面的绕流、削弱叶尖涡强度,使得气流不产生分离,从而可减小诱导阻力、提升风力发电机组叶片气动效率。同时,也可降低叶尖涡产生的噪声。虽然将小翼倾向吸力面的叶尖有更贴近塔架的风险,但是考虑到部分风场实际风资源数据比设计参数更加安全,可以充分利用叶片净空的安全余量,以提高叶片使用效率。此外,根据本发明的示例性实施例的用于风力发电机组叶片的叶尖包含倾向于压力面的小翼也可对叶尖涡起到一定的阻滞作用,从而增加对风能捕获的效率,虽然倾向于压力面的小翼附加的气动升力分量可能不如倾向于吸力面的小翼大,但其避免了使叶尖贴近塔架的风险。According to an exemplary embodiment of the present invention, by forming a winglet inclined to the suction side or the pressure side at the end of the blade tip, the flow field characteristics can be used to increase the utilization of the winglet part for the aerodynamic lift component, thereby increasing the ability to capture wind energy. efficiency. Fig. 5A and Fig. 5B respectively show the effect of a conventional blade tip 3' without winglets on the airflow and the effect of the blade tip 3 for a wind turbine blade according to an exemplary embodiment of the present invention on the airflow. As shown in 5A, for a conventional blade tip 3' without winglets, the air flow goes around from the pressure surface to the suction surface, forming a vortex on the suction surface, and the air flow has obvious separation phenomenon. As shown in FIG. 5B, since the blade tip 3 for a wind power generator blade according to an exemplary embodiment of the present invention includes winglets inclined towards the suction side, the winglets can block the flow around from the pressure side to the suction side, Weaken the strength of the blade tip vortex so that the airflow does not separate, thereby reducing the induced resistance and improving the aerodynamic efficiency of the wind turbine blades. At the same time, the noise generated by the blade tip vortex can also be reduced. Although there is a risk of moving the tip of the winglet toward the suction side closer to the tower, considering that the actual wind resource data of some wind farms is safer than the design parameters, the safety margin of the blade clearance can be fully utilized to improve the efficiency of blade use. In addition, according to the exemplary embodiment of the present invention, the tip of the blade for a wind power generating set includes a winglet inclined to the pressure surface, which can also block the tip vortex to a certain extent, thereby increasing the efficiency of wind energy capture, Although the additional aerodynamic lift component of a winglet oriented towards the pressure side may not be as large as that of a winglet oriented towards the suction side, it avoids the risk of bringing the blade tip close to the tower.
根据本发明的示例性实施例,通过设置所述锯齿部,使得根据本发明的示例性实施例的风力发电机组叶尖可有效地降低后缘湍流噪声。图6示出了根据本发明的示例性实施例的用于风力发电机组叶片的叶尖的后缘的锯齿部对气流的作用效果。参照图6,后缘的锯齿结构会使气流在后缘处形成一列反向旋转的涡对、改变尾涡结构、减小噪声的远场辐射,并且可降低叶片气动噪声对环境的影响。According to an exemplary embodiment of the present invention, the blade tip of the wind power generating set according to the exemplary embodiment of the present invention can effectively reduce trailing edge turbulence noise by providing the sawtooth portion. Fig. 6 shows the effect of serrations on the airflow of the trailing edge of the blade tip of a wind turbine blade according to an exemplary embodiment of the present invention. Referring to Figure 6, the sawtooth structure of the trailing edge will cause the airflow to form a row of counter-rotating vortex pairs at the trailing edge, change the structure of the wake vortex, reduce the far-field radiation of noise, and reduce the impact of blade aerodynamic noise on the environment.
虽然已经参照本发明的示例性实施例具体示出和描述了本发明,但是本领域普通技术人员应该理解,在不脱离由权利要求限定的本发明的精神和范围的情况下,可以对其进行形式和细节的各种改变。While the invention has been particularly shown and described with reference to exemplary embodiments of the invention, it should be understood by those skilled in the art that modifications may be made thereto without departing from the spirit and scope of the invention as defined by the claims. Various changes in form and detail.
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