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Publication numberCN102549258 B
Publication typeGrant
Application numberCN 201080045200
PCT numberPCT/EP2010/065078
Publication date12 Aug 2015
Filing date8 Oct 2010
Priority date8 Oct 2009
Also published asCN102549258A, EP2343450A1, US9303621, US20120201689, WO2011042530A1
Publication number201080045200.9, CN 102549258 B, CN 102549258B, CN 201080045200, CN-B-102549258, CN102549258 B, CN102549258B, CN201080045200, CN201080045200.9, PCT/2010/65078, PCT/EP/10/065078, PCT/EP/10/65078, PCT/EP/2010/065078, PCT/EP/2010/65078, PCT/EP10/065078, PCT/EP10/65078, PCT/EP10065078, PCT/EP1065078, PCT/EP2010/065078, PCT/EP2010/65078, PCT/EP2010065078, PCT/EP201065078
InventorsP.富格尔桑格, S.博韦, P.格劳鲍, V.v.苏布拉曼亚姆, B.伦德, L.E.詹森, S.K.拉达克里什南
ApplicantLm 玻璃纤维制品有限公司
Export CitationBiBTeX, EndNote, RefMan
External Links: SIPO, Espacenet
具有带板形元件的沿纵向延伸的流动引导装置的风力涡轮机叶片 Flow along with the plate-shaped member having a longitudinally extending guide a wind turbine blade translated from Chinese
CN 102549258 B
Abstract  translated from Chinese
公开了一种用于具有大致水平的转子轴的风力涡轮机(2)转子的风力涡轮机叶片(10),所述转子包括桨毂(8),叶片(10)在安装到桨毂(8)上时从桨毂(8)大致沿径向方向延伸,叶片具有带末梢端(14)和根部端(16)的纵向方向以及横向方向。 Discloses a rotor having a substantially horizontal axis wind turbine (2) of the wind turbine rotor blade (10), said rotor comprises a hub (8), the blade (10) mounted to the hub (8) generally radially extending from the hub (8), the blade having a distal end with (14) and the root end (16) of the longitudinal direction and the transverse direction. 该叶片还包括:仿形轮廓(40,42,50)以及前缘(18)和后缘(20),仿形轮廓包括压力侧和吸入侧,其中翼弦具有在前缘和后缘之间延伸的弦长,仿形轮廓在由入射气流冲击时产生升力。 The blade further comprising: a contoured profile (40,42,50), and a leading edge (18) and a trailing edge (20), profiled contour comprising a pressure side and a suction side, wherein the chord having a leading edge and a trailing edge between extension chord, profile outline generate lift when air impact from the incident. 风力涡轮机叶片设有附接到仿形轮廓上的沿纵向延伸的流动引导装置(70,170)。 A wind turbine blade with attached flow along the contour contoured longitudinally extending guide means (70, 170). 流动引导装置包括:底座(90,190),其具有最接近根部端(16)的第一纵向端(91,191)和最接近末梢端(14)的第二纵向端(92,192),最接近前缘(18)的第一侧(93,193)和最接近后缘(20)的第二侧(94,194),以及第一表面(95,195)和第二表面(96,196),底座的第一表面附接到仿形轮廓上,而第二表面背对仿形轮廓。 Flow directing means comprising: a base (90, 190), which is closest to the root end having (16) a first longitudinal end (91, 191) closest to the distal end (14) of the second longitudinal end (92,192) closest to the leading edge (18 ) a first side (93,193) closest to a trailing edge (20) of the second side (94,194), and a first surface (95,195) and a second surface (96,196), a first surface of the base is attached to the profiled contour on the second surface facing away from the contoured profile. 大致沿纵向延伸的板形元件(97,197)从底座(90,190)的第二表面(96,196)突出。 Substantially along the longitudinally extending plate-shaped element (97,197) from the base (90, 190) a second surface (96,196) outstanding.
Claims(18)  translated from Chinese
1.一种用于具有大致水平的转子轴的风力涡轮机(2)的转子的风力涡轮机叶片(10),所述转子包括桨毂(8),所述叶片(10)在安装到所述桨毂(8)上时,从所述桨毂(8)大致沿径向方向延伸,所述叶片具有带末梢端(14)和根部端(16)的纵向方向(r)以及横向方向,所述叶片还包括: -仿形轮廓(40,42,50),所述仿形轮廓包括压力侧和吸入侧,以及前缘(18)和后缘(20),其中翼弦具有在前缘和后缘之间延伸的弦长,所述仿形轮廓在由入射气流冲击时产生升力,其特征在于, -所述风力涡轮机叶片设有附接到所述仿形轮廓上的沿纵向延伸的流动引导装置(70,170),所述流动引导装置包括: -底座(90,190),所述底座具有: -最接近所述根部端(16)的第一纵向端(91,191)以及最接近所述末梢端(14)的第二纵向端(92,192), -最接近所述前缘(18)的第一侧(93,193),以及最接近所述后缘(20)的第二侧(94,194),以及-第一表面(95,195)和第二表面(96,196),所述底座的第一表面附接到所述仿形轮廓上且所述第二表面背对所述仿形轮廓,其中-大致沿纵向延伸的板形元件(97,197)从所述底座(90,190)的所述第二表面(96,196)沿从所述第一纵向端(91,191)朝所述第二纵向端(92,192)的方向突出,以及其中-所述流动引导装置(70,170)布置成以便在所述叶片由所述入射气流冲击时,在所述流动引导装置(70,170)与所述叶片的所述后缘(20)之间的点处产生气流与所述叶片的压力侧的分离,其中,所述流动引导装置(70,170)永久性地附接到所述仿形轮廓上,且板形元件的前表面(98,198)是非可调的。 1. A rotor shaft having a substantially horizontal wind turbine (2) of a wind turbine rotor blade (10), said rotor comprising a hub (8), the blade (10) mounted to the paddle at When the hub (8), extending substantially radially from the hub (8), said blade having a distal end tape (14) and the root end (16) in the longitudinal direction (r) and a transverse direction, the blade further comprising: - contour profiling (40,42,50), said profiled contour comprising a pressure side and a suction side, and a leading edge (18) and a trailing edge (20), wherein the chord having a leading edge and a rear chord length extending between the edges, the profiled contour when lift generated by the impact of the incident airflow, wherein - the wind turbine blade with the flow direction is attached on the contour of the contoured longitudinally extending guide means (70, 170), said flow directing means comprises: - a base (90, 190), said base having: - closest to the root end (16) of a first longitudinal end (91, 191) and the closest the distal end (14) of the second longitudinal end (92,192), - closest to the leading edge (18) of the first side (93,193), and closest to the trailing edge (20) of the first Two side (94,194), and - a first surface (95,195) and a second surface (96,196), a first surface of the base attached to said contoured surface and said second contour facing away from the profile contour, wherein - a generally longitudinally extending plate-shaped member (97,197) from said base (90, 190) a second surface (96,196) from said first longitudinal direction end (91, 191) toward the second longitudinal end (92,192) projecting in a direction, and wherein - the flow guide means (70, 170) is arranged so that the blade by the impact of air at the time of the incident, separating the said flow directing means (70, 170) and the blade rear edge at a point (20) between the gas stream and generating pressure side of the blade, wherein said flow directing means (70, 170) is permanently attached to the profile contour, and the front surface of the plate-shaped element (98,198) non-adjustable.
2.根据权利要求1所述的风力涡轮机叶片,其特征在于,所述仿形轮廓分成: -根部区(30),其具有最接近所述桨毂的大致圆形或椭圆形的轮廓, -翼型区(34),其具有最远离所述桨毂的升力产生轮廓,以及-所述根部区(30)与所述翼型区(34)之间的过渡区(32),所述过渡区(32)具有沿径向方向从所述根部区的圆形或椭圆形轮廓逐渐地变成所述翼型区的升力产生轮廓的轮廓。 The wind turbine blade according to claim 1, characterized in that said profiled contour is divided into: - the root region (30), having a substantially circular or oval-shaped profile closest to the hub, and - airfoil region (34), having the most remote from the hub of lift generating contour, and - the root region (30) and the airfoil region (34) between the transition region (32), the transition region (32) having a radial direction becomes gradually lift the airfoil region from circular or elliptical profile of the root region profile contour generated.
3.根据权利要求2所述的风力涡轮机叶片,其特征在于,所述流动引导装置(70,170)布置在所述仿形轮廓的所述过渡区(32)中,处于所述叶片(10)的压力侧上。 3. A wind turbine blade according to claim 2, characterized in that said flow directing means (70, 170) is arranged in the transition region of said contoured profile (32), in the blade (10 ) on the pressure side.
4.根据权利要求3所述的风力涡轮机叶片,其特征在于,所述流动引导装置大致沿所述过渡区的整个纵向范围延伸。 The wind turbine blade according to claim 3, characterized in that said flow directing means along substantially the entire longitudinal extent of said transition region extends
5.根据权利要求2至权利要求4中任一项所述的风力涡轮机叶片,其特征在于,所述流动引导装置延伸入所述翼型区中。 According to claim 2 to claim wind turbine blade according to any one of claims 4, characterized in that said flow directing means extending into said airfoil area.
6.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件大致沿所述底座的整个纵向范围延伸。 The wind turbine blade according to any one of claims 1 to 3 claims, wherein said plate-shaped member extending substantially along the entire longitudinal extent of the base.
7.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件从所述底座的第一侧或第二侧突出。 As claimed in Claim 1 to a wind turbine blade according to any one of claims 3, wherein said plate-shaped member from a first side or a second side of said base projection.
8.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件从所述底座的第一侧与第二侧之间的点突出。 8. A wind turbine blade according to any one of claims 1 to 3 claims, wherein said plate-shaped member from a point between the first side and the second side of said base projection.
9.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件从所述底座的第一侧与第二侧之间的中部突出。 9. The wind turbine blade according to any one of claims 1 to 3 claims, wherein said plate-shaped member from the middle between the first side and the second side of said base projection.
10.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件大致为平面。 According to claim 1 to claim wind turbine blade according to any one of claims 3, wherein said plate-shaped member is substantially planar.
11.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件为弯曲的。 According to claim 1 to claim wind turbine blade according to any one of claims 3, wherein said plate-shaped member is curved.
12.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件为凸出的或凹入的。 According to claim 1 to claim wind turbine blade according to any one of claims 3, wherein said plate-shaped member is convex or concave.
13.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述板形元件在附接点处与所述底座形成第一角,所述第一角为最大80度,或为最大70度,或为最大60度。 13. A wind turbine blade according to any one of claims 1 to 3 claims, wherein said plate-shaped member at the attachment point and said base forming a first angle, the first angle is the maximum 80 degrees, or 70 degrees maximum, or a maximum of 60 degrees.
14.根据权利要求13所述的风力涡轮机叶片,其特征在于,所述板形元件朝所述叶片的所述后缘成角。 14. The wind turbine blade according to claim 13, characterized in that, after the plate-shaped member toward the edge of the blade is angled.
15.根据权利要求13所述的风力涡轮机叶片,其特征在于,所述板形元件朝所述叶片的所述前缘成角。 15. The wind turbine blade of claim 13, wherein said plate-shaped member toward the leading edge of the blade at an angle.
16.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述底座由挠性材料形成。 According to claim 1 to claim wind turbine blade according to any one of claims 3, characterized in that said base is formed of a flexible material.
17.根据权利要求1至权利要求3中任一项所述的风力涡轮机叶片,其特征在于,所述底座的第一表面是弯曲的。 17. The claim of claims 1 to wind turbine blade according to any one of claims 3, characterized in that the first surface of the base is curved.
18.根据权利要求17所述的风力涡轮机叶片,其特征在于,所述第一表面的弯曲沿所述底座的纵向方向变化。 18. The wind turbine blade of claim 17, wherein said first surface is bent along the longitudinal direction of the base changes.
Description  translated from Chinese
具有带板形元件的沿纵向延伸的流动引导装置的风力涡轮机叶片 Flow along with the plate-shaped member having a longitudinally extending guide a wind turbine blade

技术领域 TECHNICAL FIELD

[0001] 本发明涉及一种用于具有大致水平的转子轴的风力涡轮机转子的风力涡轮机叶片,所述转子包括桨毂,叶片在安装到桨毂上时大致沿径向方向从桨毂延伸,叶片具有带末梢端和根部端的纵向方向以及横向方向,叶片还包括仿形轮廓以及前缘和后缘,其中仿形轮廓包括压力侧和吸入侧,其中翼弦具有在前缘和后缘间延伸的弦长,仿形轮廓在由入射气流冲击时产生升力。 [0001] The present invention relates to a blade for a wind turbine having a substantially horizontal rotor shaft of the wind turbine rotor, said rotor comprises a hub, the blades when mounted to the hub extending from the hub substantially in a radial direction, blade having a distal end and a longitudinal direction of the tape and the root end of the lateral direction, further comprising a profiling blade contour and a leading edge and a trailing edge, wherein the profiled contour comprising a pressure side and a suction side, wherein the chord extending between the leading and trailing edges chord, profile outline generate lift when air impact from the incident.

背景技术 Background technique

[0002] 理想的是,翼型的风力涡轮机叶片形状类似于飞机机翼的轮廓,其中叶片的翼弦平面宽度及其一阶导数随离桨毂距离减小而连续地增大。 [0002] Preferably, the wind turbine blade airfoil shape similar to the outline of an airplane wing, where the chord width of the blade plane and a first derivative with decreasing distance from the hub continuously increased. 这导致叶片理想的是在桨毂附近较宽。 This results in the blade is preferably wider near the hub. 这在必须将叶片安装到桨毂上时又引发了问题,且此外,这在叶片操作期间由于叶片较大表面面积而引起了较大的负载,诸如暴风负载。 This must be mounted on the blade hub Shiyou raises problems, and in addition, since it leaves a large surface area to cause a larger load during blade operation, such as storm loads.

[0003] 因此,多年来,叶片的构造已朝一定形状发展,其中叶片由最接近桨毂的根部区、包括最远离桨毂的升力产生轮廓的翼型区,以及根部区与翼型区之间的过渡区构成。 [0003] Thus, over the years, has been constructed blade towards the development of a certain shape, wherein the blade from the root area closest to the hub, including the most remote from the hub of the airfoil lift generating contour area, as well as the root area and the airfoil zone constitute the transition zone between. 翼型区具有相对于产生升力理想或几乎很理想的叶片形状,而根部区具有大致圆形的截面,这减小了暴风负载,且使得将叶片安装至桨毂较为容易和安全。 Airfoil region with respect to generating lift or over almost ideal blade shape, whereas the root region has a substantially circular cross-section, which reduces storm loads, and such that the blade is mounted to the hub relatively easy and safe. 根部区的直径优选为沿整个根部区恒定。 Root area diameter is preferably constant along the entire root area. 由于圆形截面,故根部区不会有助于风力涡轮机的发电,且实际上由于阻力而使其降低了少许。 Since the circular cross-section, so the root zone does not contribute to generation of wind turbines, and in fact due to the resistance and it reduces a little. 如其名称暗含的那样,过渡区具有从根部区的圆形形状逐渐地变至翼型区的翼型轮廓的形状。 As its name implies it, the transition zone has a shape changes from a circular shape to the root zone gradually airfoil profile of the airfoil region. 通常,过渡区中的叶片宽度随离桨毂距离增大而大致线性地增大。 Typically, the transition zone blade width and approximately linearly with increasing distance from the hub increases.

[0004] 举例来说,用于风力涡轮机的叶片经过一定时间已变得越来越大,且它们现在可能大于60米长,故对优化空气动力性能的需求就在增加。 [0004] For example, a blade for a wind turbine after a certain time has become bigger and bigger, and they may now be more than 60 meters long, it needs to optimize aerodynamic performance on the rise. 风力涡轮机叶片设计成具有至少20年的操作寿命。 Wind turbine blade is designed to have at least 20 years of operating life. 因此,叶片总体性能甚至较小的变化在风力涡轮机叶片的寿命内都可累积高度增长的经济利益,这超过了与这些变化相关的附加制造成本。 Thus, the overall performance of the blade even small changes in the lifetime of a wind turbine blade can accumulate high growth economic benefits, which exceeds the changes associated with these additional manufacturing costs. 多年来,研究的焦点区域已集中于改善叶片的翼型区,但在最近几年间,越来越多的焦点已集中于还改善叶片根部和过渡区的空气动力性能。 Over the years, the focus of regional studies have focused on improving the blade airfoil region, but in recent years, more and more focus has been on further improving the aerodynamic performance of the blade root and the transition zone.

[0005] W02007/065434公开了一种叶片,其中根部区设有缺口和/或凸起,以便从此叶片的部分上减少阻力。 [0005] W02007 / 065434 discloses a blade, wherein the root area with gaps and / or raised in order to reduce drag on the blades from this section.

[0006] W02007/045244公开了一种叶片,其中根部区和过渡区设计成以便具有至少两个单独的翼型轮廓,以便增大这些区的升力。 [0006] W02007 / 045244 discloses a blade, wherein the root area and the transition area is designed so as to have at least two separate airfoil profile, so as to increase the lift of these regions.

[0007] W00208600描述了一种风力涡轮机,其中风力涡轮机的输出通过向风力涡轮机的根部区段提供部件来增大,该部件以由该部件和根部区段构成的组件可吸收风能且增大风力涡轮机的总体效率的方式设计。 [0007] W00208600 describes a wind turbine, wherein the output of the wind turbine components by providing root section of a wind turbine to be increased, the assembly member to the root section of the member and may be formed to increase the absorption of wind energy and wind The overall efficiency of the turbine design approach.

[0008] W02007/118581公开了一种叶片,其中叶片的内侧部分在叶片压力侧上设有流动引导装置,以便通过增加升力来提高叶片的空气动力性能。 [0008] W02007 / 118581 discloses a blade, the inner portion of the blade which is provided with flow guiding means on the blade pressure side in order to improve the aerodynamic performance of the blade by increasing the lift. 然而,提出的设计由于三角形截面而刚性很大,且因此流动引导装置在叶片弯曲时具有与叶片表面分开的趋势。 However, due to the design of the proposed triangular cross-section and very rigid, and thus the flow guide means having a tendency to separate from the blade surface at the curved blade.

[0009] DE102008002930公开了一种风力涡轮机叶片,其设有流动引导装置,该流动引导装置包括底座和板形元件,板形元件在叶片的横向方向上沿叶片翼弦延伸。 [0009] DE102008002930 discloses a wind turbine blade, which has a flow directing device, the flow guide means comprises a base and a plate-shaped member, the plate-shaped member extending in the transverse direction of the blade along the blade chord.

发明内容 SUMMARY OF THE INVENTION

[0010] 本发明的目的在于获得一种新型的叶片,且该新型的叶片克服或改善了现有的技术的至少一个缺点,或提供了有用的备选方案。 [0010] The present invention is to obtain a new type of blade, and the new blade to overcome or ameliorate at least one of the disadvantages of the prior art, or to provide a useful alternative.

[0011] 根据本发明的第一方面,一种风力涡轮机叶片设有附接到仿形轮廓上的沿纵向延伸的流动引导装置,该流动引导装置包括:底座,其具有最接近根部端的第一纵向端和最接近末梢端的第二纵向端,最接近前缘的第一侧和最接近后缘的第二侧以及第一表面和第二表面,底座的第一表面附接到仿形轮廓上,而第二表面背对仿形轮廓,其中沿从第一端到第二端的方向大致沿纵向延伸的板形元件从底座第二表面突出,其中流动引导装置布置成以便在叶片由入射气流冲击时,在流动引导装置与叶片后缘之间的点处产生气流与叶片压力侧的分离。 [0011] According to a first aspect of the present invention, a wind turbine blade attached to the flow guiding means is provided along the contour of the contoured longitudinally extending, the flow directing means comprising: a base having a first end closest to the root longitudinal end and a second longitudinal end closest to the distal end, closest to the leading edge of a first side and a second side closest to the rear edge and the first surface and a second surface, the first surface of the base is attached to the profile contour and the second surface facing away from the profile contour, wherein a direction from a first end to a second end along a generally plate-shaped member extending longitudinally from the base of the second surface of the projection, wherein the flow directing means arranged to the blade by the impact of the incident airflow When, after the flow guide means and the blade edge is generated at the point of separation of the air flow and pressure side of the blade. 因此,应当认识到的是,流动引导装置以离后缘一定距离(即,以一定间隔)布置在前缘与后缘之间。 Thus, it should be appreciated that the flow directing means a certain distance away from the trailing edge (i.e., at certain intervals) disposed between leading and trailing edges.

[0012] 相比于W02007/118581中所述的扰流器的已知结构,该结构具有的优点在于其更为灵活,且将减小流动引导装置部分端部处的剥落力。 [0012] Compared to the spoiler of known structure W02007 / 118581, the structure has an advantage in that it is more flexible, and the peel force decreases flow guide portion of the end portion of the apparatus. 因此,底座具有较小与叶片表面断开的趋势。 Thus, the base has a smaller blade surface and disconnected trend. 类似于W02007/118581中所述的扰流器装置,本装置可用作高升力装置,其用于将升力加至叶片的某些纵向区域,因此有助于年能量产能。 Similar to the spoiler device in W02007 / 118581, the present apparatus can be used as high-lift device for the lift was added to some of the longitudinal area of the blade, thus contributing to annual energy production.

[0013] 流动引导装置有利的是布置成大致平行于风力涡轮机叶片的纵轴线,例如,桨距轴线。 [0013] Advantageously flow directing means is arranged substantially parallel to the wind turbine blade longitudinal axis, e.g., pitch axis. 因此,流动引导装置的纵向方向和叶片的纵轴线形成小于30度或小于20度的角。 Thus, the flow guide means and the longitudinal axis of the longitudinal direction of the blade form less than 30 degrees or less than 20 degrees.

[0014] 流动引导装置优选为永久性地附接到风力涡轮机叶片的表面上,且可能未主动地受控制。 [0014] the flow guide means is preferably permanently attached to the wind turbine blade surface, and may not be actively controlled. 因此,前表面的定向是非可调的。 Thus, the front surface of the non-directional adjustable. 另外,还认识到流动引导装置用于增大升力和能量产能。 Also, recognize that the flow guide means for increasing the lift and energy production. 因此,流动引导装置作为备选可表示为高升力装置。 Thus, the flow guide means alternatively may be expressed as lift device.

[0015] 其中入射流的意思是叶片正常使用(即,在风力涡轮机转子上旋转)期间叶片区段处的入流状态。 [0015] where the jet meant blade normal use (ie, rotate in the wind turbine rotor) inflow during the state sector at the blade. 因此,进入流为由轴向风速和叶片局部区段经历的旋转分量的合成形成的入流。 Therefore, synthetic components into the partial segment axial flow rotary speed and blade formed by experienced inflow. 其中到来流意思是撞击流动引导装置的流,即,接触和冲击流动引导装置的叶片压力侧上的局部流。 Which means the arrival of the stream flow impingement flow guide means, namely, touch and impact the local stream flow guide vanes on the pressure side of the device.

[0016] 根据有利的实施例,仿形轮廓分成:根部区,其具有最接近桨毂的大致圆形或椭圆形的轮廓、具有最远离桨毂的升力产生轮廓的翼型区以及根部区与翼型区之间的过渡区,过渡区具有沿径向方向从根部区的圆形或椭圆形轮廓逐渐地变成翼型区的升力产生轮廓的轮廓。 [0016] According to an advantageous embodiment, the profiled contour is divided into: the root area, which has a substantially circular or elliptical contour closest to the hub, the hub having farthest from the lift generating profile of the airfoil and the root zone area and transition zone between the airfoil region, having a transition zone in the radial direction into a gradually lift airfoil region from circular or elliptical profile of the root region profile contour generated. 这对应于常规现代风力涡轮机叶片的设计。 This corresponds to a conventional modern wind turbine blade design.

[0017] 根据特别有利的实施例,流动引导装置布置在仿形轮廓的过渡区中,优选是在叶片的压力侧上。 [0017] According to a particularly advantageous embodiment, the flow guide means is arranged in the transition zone of the profile contour, preferably on the pressure side of the blade. 该装置可增大过渡区中的升力,且因此有助于能量产能。 The device can be increased in the transition region lift, and thus contribute to energy production. 有利的是,流动引导装置大致沿过渡区的整个纵向范围延伸,因此有助于沿整个过渡区增大升力。 Advantageously, the flow guide means extending substantially along the entire longitudinal extent of the transition zone, thereby helping to increase the lift force along the entire transition region.

[0018] 再有,流动引导装置可有利地延伸到翼型区中。 [0018] Furthermore, flow guiding means may advantageously extend into the airfoil region. 这将升力加至翼型区,且因此增大了年能量产能。 This will lift was added to aerofoil region, and thereby increasing the annual energy production. 原则上,其还可延伸到根部区中。 In principle, it may also extend into the root zone. 另外,流动引导装置可单独地布置在根部区中,或单独地布置在翼型区中。 In addition, the flow guide means may be separately disposed in the root zone, or separately arranged in the airfoil region.

[0019] 根据一个有利的实施例,板形元件大致沿底座的整个纵向范围延伸。 [0019] According to an advantageous embodiment, the entire longitudinal extent of the plate-shaped element extends substantially along the base.

[0020] 根据第一实施例,板形元件从底座的第一侧或第二侧突出。 [0020] According to the first embodiment, the plate-shaped member from the first side or second side of the base of the projection. 因此,提供了简单的实施例,其中流动引导装置同样形成为角材。 Accordingly, a simple embodiment, wherein the flow guide means are formed so as Angles. 根据第二实施例,板形元件从底座第一侧与第二侧之间的点突出,例如,中部。 According to the second embodiment, the plate-shaped element from the point between the base of the first side and the second side prominent, for example, the middle. 因此,板形元件可大致从底座的中部延伸。 Thus, the plate-shaped element may extend substantially from the middle of the base.

[0021] 根据一个有利的实施例,板形元件大致为平面。 [0021] According to an advantageous embodiment, the plate-shaped member is substantially planar. 这提供了制造容易且便宜的简单实施例。 This provides a simple and easy to manufacture and inexpensive embodiment. 根据另一有利实施例,板形元件是弯曲的,例如,凸出或凹入。 According to another advantageous embodiment, the plate-shaped member is curved, e.g., convex or concave. 这在某些情形中可能有利,例如,以便获得从叶片表面至板形元件的平滑过渡。 This may be advantageous in some cases, e.g., in order to obtain a smooth transition from the blade to the surface of the plate-shaped member. 板形元件可模制成弯曲形状,或形成为平面元件,其随后弯成所期望的形状。 Plate-shaped member may be molded into a curved shape, or formed as a planar element, which is then bent into the desired shape.

[0022] 在根据本发明的一个实施例中,在附接点处的板形元件与底座形成第一角,第一角为最大80度,有利的是最大70度,更有利的是最大60度。 [0022] In an embodiment of the maximum of 60 degrees in the present invention, the plate-shaped member with the base attachment point at the first angle is formed, the first angle of maximum 80 degrees, advantageously up to 70 degrees, it is based on more favorable . 根据另一实施例,第一角为至少100度,或有利的是至少110度,或更有利的是至少120度。 According to another embodiment, the first angle of at least 100 degrees, or advantageously at least 110 degrees, or more advantageously at least 120 degrees. 如果发现附接点在底座的第一侧或第二侧处,则该实施例是特别相关的。 If it is found at the base of the attachment points of the first side or the second side, the embodiment is particularly relevant. 这些实施例提供了简单的解决方案来使板形向前或向后成角,这还有助于叶片压力侧上的压力累积。 These embodiments provide a simple solution to the plate-shaped forward or backward into the corner, which also helps the blade pressure side pressure accumulation.

[0023] 根据第一有利实施例,板形元件朝叶片后缘成角。 [0023] According to a first advantageous embodiment, the plate-shaped member toward the rear edge of the blade into the corner. 因此,板形元件大致定位后缘与在附接点(或从入流看是在所述表面法线后方)处垂直于底座的表面之间。 Therefore, the plate-shaped elements are generally positioned between the edge of the surface attachment point (or from the inflow to see behind the surface normal) perpendicular to the base at. 在该实施例中,板形元件具有对应于W02007/118581中公开的扰流器入流表面的入流表面。 In this embodiment, the plate-shaped element corresponding to the W02007 / 118581 discloses a spoiler surface inflow inflow surface. 入流表面的角和入流表面远端点的表面高度有利地可对应于分别由本申请人在欧洲专利申请EP08171530.2和EP08171533.6中描述的那些。 Inflow angle and inflow surfaces of the distal end point of the surface height can advantageously correspond to those respectively by the applicant EP08171530.2 and EP08171533.6 described in European patent. 然而,例如,相比于W02007/118581,该设计不是刚性而具有较大的结构优点。 However, for example, compared to W02007 / 118581, the design is not a rigid structure and has a large advantage.

[0024] 根据第二有利实施例,板形元件朝叶片的前缘成角。 [0024] According to a second advantageous embodiment, the plate-shaped member toward the leading edge of the blade into the corner. 因此,板形元件大致定位在前缘与在附接点处垂直于底座的表面(或从入流看是在所述表面法线的前方)之间。 Thus, the plate-shaped elements are generally positioned between (or from the inflow to see in front of the surface normal) in the leading edge and the surface perpendicular to the attachment point at the base. 因此,当叶片的仿形轮廓由入射气流冲击时,流动引导装置在前表面前方产生气穴,这增大了流动引导装置前方的压力,且其围绕流动引导装置引导气流。 Therefore, when the profile contour of the blade from the entrance impact of air flow guide means in front of the front surface of cavitation, which increases the flow directing means of pressure in front, and the flow guiding means to guide airflow around.

[0025] 作为优选,流动引导装置形成为沿纵向延伸的装置。 [0025] Advantageously, the flow guide means is formed as a longitudinally extending means. 根据有利实施例,流动引导装置沿风力涡轮机叶片纵向范围的至少5%延伸。 According to an advantageous embodiment, the flow guide means along the longitudinal extent of wind turbine blade extend at least 5%. 再有,流动引导装置的纵向范围可为叶片纵向范围或长度的至少7%、10%、15%或甚至20%。 Further, the longitudinal extent of the flow guide means may be at least 7% of the blade length or longitudinal extent, 10%, 15% or even 20%.

[0026] 根据另一实施例,沿纵向延伸的流动引导装置沿叶片的至少I米,或风力涡轮机叶片的至少2米,或至少3米,或至少4米,或至少5米,或至少6米,或甚至至少8米,或10米延伸。 [0026] According to another embodiment, the flow direction of the guide means extending longitudinally along the blade of at least I m, 2 m, or at least a wind turbine blade, or at least 3 meters, or at least 4 meters, or at least 5 meters, or at least 6 m, or even at least 8 meters, 10 meters, or extend.

[0027] 在一个实施例中,在流动弓I导装置的至少中心纵向部分中,从远端点至仿形轮廓(或换言之是流动引导装置的高度)的最小距离沿朝末梢端的纵向方向减小。 [0027] In one embodiment, the flow guide means at least I bow central longitudinal section, from the distal end to the profiled contour point (or in other words the height of the flow guide means) is the minimum distance along the longitudinal direction towards the distal end of the Save small. 作为备选,流动弓I导装置的高度可至少在流动弓I导装置的中部大致恒定。 As a highly Alternatively, the flow guide means bow I can at least in the middle of the bow I flow guide means is substantially constant. 该高度可在纵向方向上以高度增大的部分和高度减小的部分交替变化。 The height in the longitudinal direction to increase the height of the reduced height portion and a portion of alternates.

[0028] 在一个有利实施例中,底座由挠性材料形成。 [0028] In an advantageous embodiment, the base is formed of a flexible material. 因此,底座的弯曲刚度可减小,且底座可弯曲来配合叶片表面,而不会在底座与板形元件之间的连结线中弓I入较大应力。 Thus, the bending stiffness of the base can be reduced, and the base can be bent to match the blade surface, but not in the connecting line between the base and the plate-shaped member into the bow I large stress. 例如,这可通过将底座形成为复杂结构而获得,诸如利用玻璃纤维加强的聚合物基材料。 For example, this can be a complex formed by the base structure is obtained, such as the use of a glass fiber reinforced polymer based material. 例如,聚合物基材料可为聚氨基甲酸酯树酯。 For example, the polymer-based material may be a polyurethane resin. 再有,底座可由聚合材料制成,诸如ABS塑料或聚碳酸酯。 Further, the base may be made of a polymeric material, such as ABS plastic or polycarbonate.

[0029] 有利的是,流动引导装置的纵向范围为至少0.5米,或至少I米,或至少2米,或至少3米。 [0029] Advantageously, the longitudinal extent of the flow guide means is at least 0.5 m, or at least I m, or at least 2 meters, or at least three meters. 另外,底座的宽度,即,底座的第一侧与第二侧之间的距离,有利的是在20cm至10cm之间,或20cm至70cm之间。 In addition, the width of the base, i.e., the distance between the first side and the second side of the base, advantageously between between 20cm to 10cm, or 20cm to 70cm.

[0030] 根据一个有利实施例,底座的第一表面是弯曲的,且第一表面的曲率可选为在底座的纵向方向上变化。 [0030] According to an advantageous embodiment, the first surface of the base is curved, and the curvature of the first surface is selected to change in the longitudinal direction of the chassis. 因此,该形状可大致匹配风力涡轮机叶片仿形轮廓的沿纵向变化的表面曲率。 Thus, the shape may substantially match the curvature of the surface of a wind turbine blade profile changes in the contour of the longitudinal direction. 然而,根据一个有利的实施例,底座为平面。 However, according to an advantageous embodiment, the base is flat. 因此,可行的是将流动引导装置制造为压出或挤出的元件。 Therefore, it is feasible flow guide element manufactured as extruded or extruded.

[0031] 风力涡轮机叶片有利的是可由复合结构的材料制成,诸如由纤维材料加强的聚合物基材料。 [0031] Advantageously wind turbine blade is made of a material may be a composite structure, such as a fiber material reinforced polymer based material. 树脂可为热固性树脂,诸如环氧树脂、乙烯基酯、聚酯。 The resin may be a thermosetting resin such as an epoxy, vinylester, polyester. 树脂还可为热塑性塑料,诸如尼龙、PVC、ABS、聚丙烯或聚乙烯。 It may also be a thermoplastic resin, such as nylon, PVC, ABS, polypropylene or polyethylene. 再有,树脂可为热固性热塑性塑料,诸如可循环的PBT或PET。 Further, the resin may be a thermosetting thermoplastic, such as PET or PBT can be recycled. 流动引导装置还可由这样的复合材料制成。 Flow directing means may be made of such a composite material. 聚合物基材料还可为聚氨基甲酸酯树酯。 Polymer-based material may also be a polyurethane resin. 另外,底座可由聚合材料制成,诸如ABS塑料或聚碳酸酯。 In addition, the base may be made of a polymeric material, such as ABS plastic or polycarbonate.

[0032] 流动引导装置(或流动引导装置部分)可通过将其粘附到叶片表面上而附接到叶片表面上。 [0032] The flow guiding means (or flow guide portion) can be adhered to the surface of the blade attached to the blade surface. 其还可螺接或铆接到叶片表面上。 It can also be bolted or riveted to the blade surface. 其还可通过使用螺钉来安装到叶片表面上。 It can also be mounted on the blade surface through the use of screws. 原则上,如果流动引导装置和/或叶片包括可磁化材料,则还有可能的是通过使用磁铁方式将流动引导装置附接到叶片表面上。 In principle, if the flow guide means and / or the blade comprises magnetizable material, it is also possible by way of using a magnet attached to the flow guide means on the blade surface.

[0033] 根据另一方面,本发明提供了一种风力涡轮机,其包括根据任一前述实施例的许多叶片,优选为两个或三个。 [0033] According to another aspect, the present invention provides a wind turbine, comprising a according to any preceding embodiment in many blades, preferably two or three.

附图说明 Brief Description

[0034] 下文将参照附图来详细描述本发明,在附图中: [0034] The present invention will hereinafter be described in detail with reference to the accompanying drawings, in which:

[0035] 图1示出了风力涡轮机, [0035] Figure 1 shows a wind turbine,

[0036] 图2示出了根据本发明的设有流动引导装置部分的风力涡轮机叶片的第一实施例的示意性视图, [0036] FIG. 2 shows a first embodiment of a wind turbine blade part is provided with means for guiding the flow of the present invention, a schematic view,

[0037] 图3示出了翼型轮廓的示意性视图, [0037] FIG. 3 shows a schematic view of the airfoil profile,

[0038] 图4示出了根据本发明的流动引导装置的第一实施例的示意性视图, [0038] FIG. 4 shows a flow guide device according to the present invention, a schematic view of a first embodiment,

[0039] 图5示出了根据本发明的流动引导装置的第二实施例的示意性视图, [0039] FIG. 5 shows a flow guide device according to the present invention, a schematic view of a second embodiment,

[0040] 图6为根据本发明的流动引导装置的各种设计的截面, [0040] FIG. 6 is a cross-sectional design of the various means according to the flow guide of the present invention,

[0041] 图7示出了流动引导装置与风力涡轮机叶片表面的附接, [0041] FIG. 7 shows a flow directing means is attached and a wind turbine blade surface,

[0042] 图8示出了根据本发明的随离桨毂径向距离变化的第一流动引导装置的后缘高度, [0042] FIG. 8 shows a boot with the device according to the change of the radial distance from the hub of the first flow of the present invention the height of the trailing edge,

[0043] 图9a示出了根据本发明的随离桨毂径向距离变化的第二流动引导装置的后缘高度, [0043] FIG. 9a shows a guide device according to the present invention, a hub with radial distance from the change in the height of the trailing edge of the second flow,

[0044] 图9b示出了根据本发明的随离桨毂的径向距离变化的第三流动引导装置的后缘高度, [0044] FIG. 9b shows the guide device according to the hub with the radial distance from the change in the flow of the present invention, a third the height of the trailing edge,

[0045] 图10示出了设有加强部件的流动引导装置的实施例,以及 [0045] FIG. 10 illustrates an embodiment with a reinforcing member of the flow guide means, and

[0046] 图11示出了一个实施例,其中装置的端部设有凹口。 [0046] FIG. 11 shows an embodiment, wherein the apparatus is provided with end notches.

具体实施方式 DETAILED DESCRIPTION

[0047] 图1示出了根据所谓〃丹麦原理〃的常规现代逆风风力涡轮机,其具有塔架4、机舱6和具有大致水平的转子轴的转子。 [0047] Figure 1 shows a principle of the so-called Danish 〃 〃 conventional modern upwind wind turbine having a tower 4, nacelle 6 and a rotor having a substantially horizontal rotor shaft. 转子包括桨毂8和从桨毂8沿径向延伸的三个叶片10,叶片10分别具有最接近桨毂的叶片根部16和最远离桨毂8的叶片末梢14。 The rotor includes a hub 8 and three blades extending radially hub 8 along the paddle 10, the blades 10 are closest to the hub with a blade root 16 and the farthest from the hub 8 of the blade tip 14.

[0048] 图3示出了绘制为具有各种参数的风力涡轮机的典型叶片的翼型轮廓50的示意性视图,参数通常用于限定翼型件的几何形状。 [0048] FIG. 3 shows a drawing of a typical blade having various parameters of the wind turbine airfoil profile 50 is a schematic view, the parameters typically used to define the geometry of the airfoil. 翼型轮廓50具有压力侧52和吸入侧54,在使用期间(即,在转子旋转期间),一般分别面朝迎风侧和背风侧。 Airfoil profile 50 has a pressure side 52 and suction side 54 during use (ie, during the rotation of the rotor), generally were facing the windward side and leeward side. 翼型件50具有翼弦60,翼弦60具有在叶片的前缘56与后缘58之间延伸的弦长C。 Airfoil 50 has 60 chord, chord between the blade 60 has a leading edge 56 and a trailing edge 58 extending chord C. 翼型件50具有厚度t,其限定为压力侧52与吸入侧54之间的距离。 Airfoil 50 has a thickness t, which is defined as the distance between the pressure side 54 and suction side 52. 翼型件的厚度t沿翼弦60变化。 The thickness t of the airfoil 60 along the chord changes. 与对称轮廓背离是由脊线62给予的,脊线62为穿过翼型轮廓50的中线。 And symmetric contour ridge line 62 departing is given, the ridge line 62 to pass through the center line 50 of the airfoil profile. 中线通过从前缘56到后缘58绘制内切圆来发现。 Midline cut through the inner edge of the circle 58 drawn from the leading edge 56 to the rear to find. 中线沿着这些内切圆的中心,且与翼弦60的偏离或距离称为弧f。 Along the midline of the center of the inscribed circle, and with deviation from the chord or 60 is called arc f. 还可通过使用称为上弧和下弧的参数来限定不对称,参数分别限定为离翼弦60和压力侧52及吸入侧54的距离。 Asymmetry is defined on the arc and arc parameters can also be called by using the parameters are defined as from the chord 60 and the pressure side 52 and suction side 54 of the distance.

[0049] 图2示出了根据本发明的风力涡轮机叶片10的第一实施例的示意性视图。 [0049] FIG. 2 shows a first embodiment of a wind turbine blade 10 of the invention schematic view. 风力涡轮机叶片10具有常规风力涡轮机叶片的形状,且包括最接近桨毂的根部区30、最远离桨毂的仿形或翼型区34,以及根部区30与翼型区34之间的过渡区32。 The transition zone of the wind turbine blade 10 has the shape of a conventional wind turbine blade and comprises a root area closest to the hub 30, farthest from the hub or contoured airfoil region 34, and between the root 30 and the airfoil region 34 region 32. 叶片10包括在叶片安装到桨毂上时面对叶片10旋转方向的前缘18,以及面对前缘18相对方向的后缘20。 Blade 10 includes a face 10 in the direction of rotating blades mounted on the hub the blade leading edge 18, and face the opposite direction of the leading edge 18 trailing edge 20.

[0050] 翼型区34(也称为仿形区)具有相对于产生升力理想的或几乎理想的叶片形状,而根部区30由于结构考虑而具有大致圆形或椭圆形的截面,例如,这使得将叶片10安装至桨毂更容易和安全。 [0050] airfoil region 34 (also referred to as profiling zone) with respect to generating lift ideal or almost ideal blade shape, whereas the root region 30 due to structural considerations having a substantially circular or elliptical cross-section, for example, which so that the blade 10 is mounted to the hub easier and safer. 根部区30的直径(或翼弦)通常沿整个根部区域30是恒定的。 Root zone diameter (or chord) generally along the entire root area 30 is a constant 30's. 过渡区32具有从根部区30的圆形或椭圆形状40逐渐变成翼型区34的翼型轮廓50的过渡轮廓42。 The transition zone from the base region 32 has a circular or oval shape 30 airfoil region 40 becoming airfoil profile of the transition profile 34 42 50. 过渡区32的宽度通常随离桨毂的距离r增大而大致线性地增大。 The width of the transition zone 32 generally increases substantially linearly increases the distance r from the hub increases.

[0051] 翼型区34具有翼型轮廓50,其中翼弦在叶片10的前缘18与后缘20之间延伸。 [0051] airfoil region 34 has an airfoil profile 50, wherein the leading edge chord 18 extending between the blade 10 and the trailing edge 20. 翼弦的宽度随离桨毂的距离r增大而减小。 The width of the chord with the distance r from the hub increases.

[0052] 应当注意的是,叶片不同区段的翼弦一般不会处于公共平面内,因为叶片可能扭曲和/或弯曲(即,预弯曲),因此向翼弦平面提供了对应的扭曲和/或弯曲路线,这是最普遍的情况,以便补偿取决于距离桨毂的半径的叶片局部速度。 [0052] It should be noted that different sections of the blade chord is generally not in a common plane, because the leaves may distort and / or curved (ie, pre-curved), therefore the chord plane to provide a corresponding distortion and / or curved line, which is the most common situation, in order to compensate for the local velocity depends on the blade radius from the hub.

[0053] 根据本发明的风力涡轮机叶片10设有流动引导装置70,其至少在叶片的过渡区32中从叶片压力侧突出。 [0053] 10 is provided with a wind turbine blade according to the present invention, the flow guide means 70, which at least in the transition region 32 of the blade protruding from the blade pressure side. 但是,元件还可布置在叶片10的其它部分中。 However, elements may also be disposed in other portions of the blade 10. 在特别有利的实施例中,流动引导装置70延伸到根部区30中。 In a particularly advantageous embodiment, the flow guide means 70 extends to 30 in the root zone.

[0054] 图4示出了根据本发明的流动引导装置70的第一实施例。 [0054] FIG. 4 shows a first embodiment of the guide device 70 according to the flow of the present invention. 流动引导装置形成为具有底座90的沿纵向延伸的装置。 It means forming a flow guide means having a base 90 along a longitudinally extending. 底座90包括第一纵向端91,其在流动引导装置70附接到风力涡轮机叶片10的仿形轮廓上时,布置成最接近叶片的根部端,以及布置成最接近叶片10末梢端的第二纵向端92。 Base 90 includes a first longitudinal end 91, which, when the flow guide means 70 is attached to the profiled contour 10 of the wind turbine blade, the blade is arranged closest to the root end, and arranged to be closest to the distal end 10 of the second longitudinal blade end 92. 底座90还包括布置成最接近叶片10的前缘18的第一侧93,以及布置成最接近叶片的后缘20的第二侧94。 Base 90 also includes a blade 10 disposed closest to the leading edge 18 of the first side 93, and arranged closest to the blade trailing edge 20 of the second side 94. 底座90还包括附接到叶片10的表面上的第一表面95,以及背对叶片10的表面的第二表面。 The base 90 also includes a first surface 95 attached on the surface of the blade 10, the blade 10 and the surface facing away from the second surface. 板形元件97从底座90的第二表面96,从大致在第一侧93与第二侧94中间的部分突出。 Plate-shaped element 97 from the second surface 96 of the base 90, protruding from the first side roughly 93 and 94 in the middle portion of the second side. 板形元件97沿底座90的整个纵向程度沿纵向延伸。 Plate-shaped member 97 along the entire longitudinal extent of the base 90 extends longitudinally. 板形元件包括面朝叶片10的前缘18的前表面98,以及面朝叶片10的后缘20的后表面99。 It comprises a plate-shaped member 10 facing the front surface of the blade leading edge 18 of the 98, and a rear surface 99 facing the rear edge 20 of the blade 10. 在风力涡轮机操作期间,板形元件97的前表面98因此由到来的气流冲击。 During operation of the wind turbine, the front surface 98 of the plate-shaped member 97 and therefore the impact of the incoming air stream. 板形元件97用作为阻塞轮廓的压力侧上的流动。 Plate-shaped element 97 is used as the outline of the flow of the pressure side blocked on. 气流分离出现在流动引导装置之后,即,在流动引导装置与叶片后缘之间。 Flow separation occurs after the flow guide means, i.e., between the rear edge of the blade means in the flow guide. 这种阻塞由于流动分离而在流动引导装置之后,即,流动引导装置与风力涡轮机叶片后缘之间,导致了较高的压力。 Such blockage due to the flow after flow separation guiding means, i.e., after the flow guide means and the wind turbine blade between the edge, resulting in a higher pressure. 这种较高压力有助于流动引导装置70布置于其中的纵截面中的较高升力。 This higher pressure helps the flow guide means 70 disposed therein in a longitudinal section of a high lift.

[0055] 图5示出了根据本发明的流动引导装置170的第二实施例,其中相似的数字表示图4中所示实施例的相似部分。 [0055] FIG. 5 shows a second embodiment of the present invention according to the flow guide means 170, wherein like numerals denote like parts in the embodiment shown in FIG. 因此,仅描述了两个实施例之间的差异。 Therefore, only the differences are described between the two embodiments. 在该实施例中,板形元件197向前成角,以便板形元件197与底座190形成第一角Φ。 In this embodiment, the plate-shaped element 197 forward into a corner, so that the plate-shaped member 197 and the base 190 form a first angle Φ. 因此,前表面198还朝底座190和叶片10的表面略微面向下。 Therefore, also the front surface 198 toward the base 190 and the blade 10 facing downwards slightly. 当在风力涡轮机正常操作期间前表面198由到来的气流冲击时,气穴形成在前表面的前方,这增大了流动引导装置前方的压力,且围绕流动引导装置170引导气流。 When in front of a wind turbine during normal operating surface 198 by the time the impact of the arrival of the air flow, air pockets forming in front of the front surface, which increases the pressure in the flow guide in front of the device and flow guide means around 170 direct airflow. 因此,增大的压力累积在流动引导装置170的前方和后方。 Therefore, increasing the pressure accumulated in the front and rear of the flow guide means 170. 因此,升力沿大部分叶片区段增大。 Therefore, most of the lift along the blade segment increased. 第一角Φ有利的是为至少20度,且大约30至45度的角不但相对于增加升力而且相对于流动引导装置的灵活性都已显出了优异的效果。 Advantageously the first angle Φ is at least 20 degrees, and about 30-45 degree angle relative to not only increase the lift and flexibility with respect to the flow guide means are showing excellent results.

[0056] 然而,板形元件不必如图4中所示那样大致垂直于底座(和叶片的仿形轮廓)突出,或如图5中所示那样向前成角。 [0056] However, the plate-shaped element does not, as shown in Figure 4 is substantially perpendicular to the base (and contoured profile of the blade) is prominent, or as shown in Figure 5 forward into the corner. 另外,板形元件不必从底座的中部突出。 In addition, the plate-shaped element does not protrude from the middle of the base. 图6示出了流动引导装置的截面设计的变型。 Figure 6 shows a cross section of the flow guide means designed variants.

[0057] 图6(a)_(e)示出了流动引导装置的不同实例,其同样定形为角材。 [0057] FIG. 6 (a) _ (e) show different examples of flow directing device, which is also shaped angle material. 在所有实施例中,假定叶片前缘布置在右侧,而后缘在左侧。 In all embodiments, it is assumed disposed at the right side of the blade leading edge, trailing edge on the left side. 因此,在风力涡轮机的正常操作期间,到来的气流从右向左。 Thus, during normal operation of the wind turbine, the gas flow coming from right to left.

[0058] 在实施例(a)中,板形元件向前成角,且从底座的第二侧突出。 [0058] In an embodiment (a), the plate-shaped element angled forward and protrude from the second side of the base. 在实施例(b)中,板形元件向后成角,且从底座的第一侧突出。 In Example (b), the plate-like element back into a corner, and protrudes from the first side of the base. 在这两个实施例中,(a)和(b)的板形元件的角与底座形成45度的角。 In both embodiments, the angle of the base (a) and (b) of the plate-shaped member formed 45 degree angle.

[0059] 在实施例(C)中,板形元件向前成角,且从底座的第二侧突出。 [0059] In an embodiment (C), the plate-shaped element angled forward and protrude from the second side of the base. 在实施例⑷中,板形元件向后成角,且从底座的第二侧突出。 ⑷ In an embodiment, the plate-like element back into a corner, and from the second side of the base of the prominent. 在这两个实施例中,板形元件与底座形成大约135度的角。 In both embodiments, the plate-shaped element and the base form an angle of about 135 degrees.

[0060] 在实施例(e)中,板形元件大致垂直于底座从底座的第一侧突出。 [0060] In an embodiment (e), the plate-shaped member is substantially perpendicular to the base protruding from the first side of the base.

[0061] 实施例(f)-(h)示出了板形元件从底座中部(即,底座的第一侧与第二侧之间)突出的实施例。 [0061] Example (f) - (h) shows a plate-shaped element from the middle of the base (ie, between the first side and the second side of the base) to highlight examples. 板形元件例如可如实施例(f)中所示那样向前成角,如实施例(g)中所示那样向后成角,或如实施例(h)中所示那样从底座垂直地突出。 Plate-shaped element for example as described in Example (f), as shown in angled forward, as in Example (g), as shown back into a corner, or as described in Example (h), as shown vertically from the base outstanding.

[0062] 在所有前述实施例中,板形元件设计为平面元件。 [0062] In all the foregoing embodiments, the plate-shaped element is designed as a planar element. 然而,前述实施例的板形元件可略弯或弯曲,例如,以实施例(i)中所示的凹入形状或实施例(j)中所示的凸出形状。 However, the plate-shaped member in the foregoing embodiments may be slightly bent or curved, e.g., in Example (i) the convex shape or a concave shape as shown in Example (j) as shown. 另夕卜,板形元件可包括不同的平面部分,其相对于底座不同地成角,板形元件因此具有如实施例(k)中所示的不连续设计。 Another Xi Bu, plate-shaped element may include different plane part, with respect to the base differently angled, plate-shaped element and therefore has as Example (k) as shown in discontinuous design.

[0063] 流动弓I导装置通常安装在风力涡轮机叶片的弯曲表面上。 [0063] I bow flow guide device is usually mounted on the curved surface of the wind turbine blade. 因此,底座的侧部可能如图7(a)中所示那样与叶片表面略微分离。 Accordingly, the side portions of the base may be separated slightly as shown in Figure 7 (a) shown in the blade surface. 因此,有利的是流动引导装置的底座由挠性材料制成,以便减少沿整个底座板的应力形成。 Therefore, it is advantageous to base the flow guide means is made of a flexible material, so as to reduce the formation of the stress along the entire base plate. 此外,通过使板形元件具有挠性,就减小了流动引导装置端部处的剥落力。 In addition, the plate-shaped member having flexibility, reduces the flow guide means peeling force at the end. 这可通过使底座形成为相对较薄的板而获得,例如,由复合材料制成,如玻璃纤维加强的聚合物基材料。 This can be achieved by forming a relatively thin base plate is obtained, for example, made of a composite material, such as glass fiber reinforced polymer based material. 作为备选,底座可如图7(b)中所示那样略微弯曲,以便补充风力涡轮机叶片的表面。 As an alternative, the base 7 (b), as shown in FIG. May be slightly curved to complement the wind turbine blade surface. 底座例如可通过将底座第一表面粘附到叶片表面上,或通过将其经由连接装置如螺钉或螺母和螺栓连接到叶片上来附接到叶片表面上。 Base, for example by the base of the first surface adhered to the blade surface, or by being as screws or nuts and bolts to connect up to the blade via a connecting means attached to the blade surface. 还有可能的是将流动引导装置模制到叶片表面上。 It is also possible that the flow guide means molded onto the blade surface. 再有,如果例如底板和/或叶片壳体包括可磁化的材料,则流动引导装置可通过使用磁铁方式来附接到叶片表面上。 Further, if, for example the base plate and / or the blade housing comprising magnetizable material, the flow directing means manner by using a magnet to be attached to the blade surface. 另外,底座第一表面的曲率可沿底座的纵向方向变化,以便适应风力涡轮机叶片变化的形状。 In addition, the curvature of the first surface of the base along the longitudinal direction of the base changes to accommodate changes in the shape of a wind turbine blade.

[0064] 在第一实施例中,流动引导装置的高度h可如图8中所示那样沿纵向方向(或离桨毂的径向距离)朝叶片的末梢端r (至少在流动引导装置的中心纵向部分71内)减小。 [0064] In the first embodiment, the height h of the flow guide means may be as shown in Figure 8 in the longitudinal direction (or the radial distance from the hub) towards the blade tip end r (at least in the flow guide means central longitudinal section 71) is reduced. 流动引导装置的高度在图8中示为随离桨毂的径向距离r而变化。 The height of the flow guide means shown in FIG. 8 with a radial distance r from the hub varies. 在最接近桨毂的流动引导装置70的纵向端处,流动引导装置70成圆形或锥形,以便获得到至叶片仿形轮廓的平滑过渡。 Closest to the hub of the flow guide means 70 at the longitudinal ends of the flow guide means 70 into a round or tapered so as to obtain a smooth contour to the blade contour transitions.

[0065] 在第二实施例中,流动弓丨导装置70的高度在图9a中示出为在叶片纵向方向上,至少在中心纵向部分71内大致恒定。 [0065] In the second embodiment, the height of the flow guide means 70 丨 bow in Figure 9a as shown in the blade longitudinal direction, at least in the longitudinal center of the inner portion 71 is substantially constant. 此外,可以看到的是,流动引导装置70可在流动引导装置70的纵向端附近成圆形或锥形,以便获得到叶片仿形轮廓的平滑过渡。 In addition, we can see that the flow guide means 70 may close the longitudinal ends of the guide device 70 into a rounded or tapered in the flow, so as to obtain a smooth contour to the blade contour transitions.

[0066] 在第三实施例中,流动引导装置70的高度如图9b中所示那样在第一纵向部分中增大,而在第二纵向部分中减小。 [0066] In the third embodiment, the height of the flow guide 70 as shown in FIG. 9b is increased in a first longitudinal portion of the apparatus is reduced in the second longitudinal section.

[0067] 当流动引导装置部分定形为如图5中所示的向前成角的板形元件时,装置部分可有利地设有加强装置1190,其如图10中所示那样布置在板形元件的后表面上。 [0067] As part of the flow guide means shaped plate-shaped element angled forward as shown in FIG. 5, the device portion may advantageously be provided with reinforcement means 1190, which are arranged in a plate shape, as shown in Figure 10 on the rear surface of the element. 加强装置有利的是可形成为后表面与装置底座之间的三角形板。 Strengthen the enabling device is formed into a triangular plate and the rear surface of the base of the unit between. 加强装置有利的是大致布置在叶片的横向方向上,即,大致平行于局部翼弦。 Strengthening means are advantageously arranged substantially in the transverse direction of the blade, i.e., substantially parallel to the local wing chord.

[0068] 如图11中所示,流动引导装置或流动引导装置组合中的单个模块可有利地在装置的一端或两端设有凹口1285、切口等。 [0068] As shown in Figure 11, the flow guide means, or a combination of the flow guide means in a single module may advantageously be at one or both ends of the apparatus is provided with a recess 1285, incisions and the like. 这将减小端部处的应力集中和剥落力。 This will reduce the stress concentration and peel strength at the ends. 凹口可为有用的相关形状,如三角形、圆形、正方形等。 Recesses may be useful related shapes, such as triangles, circles, squares, and the like.

[0069] 虽然已经参照优选实施例描述了本发明。 [0069] Although described with reference to a preferred embodiment of the present invention. 然而,本发明的范围不限于所示的实施例,且备选方案和修改可在不脱离本发明范围的情况下执行。 However, the scope of the present invention is not limited to the embodiments shown, and alternatives and modifications can be performed without departing from the scope of the present invention. 例如,仅提出了流动引导装置布置在叶片过渡区中的叶片压力侧上的实施例。 For example, only the proposed embodiment the flow guide means is arranged in the blade pressure side of the blade in the transition zone on. 然而,有利的是,流动引导装置还延伸至叶片的根部区和/或翼型区。 However, it is advantageous that the flow directing means further region extending to the root of the blade and / or airfoil area. 再有,流动引导装置在其它有利实施例中可布置在叶片的其它部分上,诸如叶片的吸入侧上或在叶片后缘处,如盖尼类装置(Gurney like device)。 Further, the flow guide means in other advantageous embodiments may be disposed on other portions of the blade, or at the edge of the blade on the suction side of the blade, such as, e.g. Gainey class means (Gurney like device).

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Classifications
International ClassificationF03D1/06
Cooperative ClassificationF03D1/0641, F05B2240/301, F05B2260/30, F05B2240/121, Y02E10/721
Legal Events
DateCodeEventDescription
4 Jul 2012C06Publication
5 Sep 2012C10Request of examination as to substance
12 Aug 2015C14Granted