Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberCN102245894 B
Publication typeGrant
Application numberCN 200980149666
PCT numberPCT/EP2009/064084
Publication date4 Jun 2014
Filing date26 Oct 2009
Priority date12 Dec 2008
Also published asCN102245894A, EP2138714A1, EP2368034A1, EP2368034B1, US8944776, US20110243753, WO2010066500A1
Publication number200980149666.0, CN 102245894 B, CN 102245894B, CN 200980149666, CN-B-102245894, CN102245894 B, CN102245894B, CN200980149666, CN200980149666.0, PCT/2009/64084, PCT/EP/2009/064084, PCT/EP/2009/64084, PCT/EP/9/064084, PCT/EP/9/64084, PCT/EP2009/064084, PCT/EP2009/64084, PCT/EP2009064084, PCT/EP200964084, PCT/EP9/064084, PCT/EP9/64084, PCT/EP9064084, PCT/EP964084
InventorsK.伦茨, P.富格尔桑格, S.皮拉加拉塔尔沃
ApplicantLm 玻璃纤维制品有限公司
Export CitationBiBTeX, EndNote, RefMan
External Links: SIPO, Espacenet
Wind turbine blade having a flow guiding device with optimised height
CN 102245894 B
Abstract  translated from Chinese
本发明公开了一种风力涡轮机叶片(10),其具有在叶片的压力侧(52)被附连到成形轮廓(40、42、50)的流动引导装置(70)。 The present invention discloses a wind turbine blade (10), having a pressure side of the blade (52) is attached to flow shaping profile (40,42,50) of the guide means (70). 所述流动引导装置沿叶片的过渡区域(32)的至少纵向部分延伸并且被设置成当叶片被入射气流冲击时在所述流动引导装置和所述叶片的后缘(20)之间的点处产生沿所述流动引导装置的至少中心纵向部分(71)从所述叶片的所述压力侧的气流分离。 At least a longitudinal portion of said flow directing means along the blade of the transition region (32) extends and is arranged at a point between said flow directing means and said blade trailing edge (20) of the air flow when the blades are incident shock generating said flow directing means along at least the central longitudinal portion (71) is separated from the gas stream the pressure side of the blade. 从叶片的前缘观察,流动引导装置被设置在位于40%至92%之间的区间内的相对弦位置。 Viewed from the blade leading edge, the flow guide means is arranged in the relative chord position located between 40 to 92% of the interval. 针对每个横向截面,流动引导装置到成形轮廓的高度是成形轮廓的最大厚度的至少10%。 For each of the transverse cross-section, the flow directing means to the shaping profile height is at least 10% of the maximum thickness of the shaping profile.
Claims(16)  translated from Chinese
1.一种用于风力涡轮机(2)的转子的叶片(10),该转子具有基本水平的转子轴,所述转子包括毂(8),当被安装于所述毂(8)时所述叶片(10)从所述毂(8)基本沿径向方向延伸,所述叶片具有带尖端(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: 成形轮廓(40、42、50),其包括压力侧和吸力侧以及前缘(18)和后缘(20),具有其弦长在所述前缘和所述后缘之间延伸的弦,当被入射气流冲击时所述成形轮廓产生升力,其中所述成形轮廓被划分为: 最靠近所述毂、具有基本圆形或椭圆形外形的根部区域(30), 最远离所述毂、具有升力生成外形的翼型区域(34),以及在所述根部区域(30)和所述翼型区域(34)之间的过渡区域(32),所述过渡区域(32)具有沿所述径向方向从所述根部区域的所述圆形或椭圆形外形逐渐变化到所述翼型区域的所述升力生成外形的外形,并且其中所述叶片在所述叶片(10)的所述压力侧(52)设有被附加到所述叶片的所述成形轮廓(40、42、50)的流动引导装置(70),所述流动引导装置(70)具有入流表面(72),该入流表面(72)具有附连到所述成形轮廓(40、42、50)的起点(74)以及位于距所述叶片的所述成形轮廓(40、42、50) —定距离的终点(76),所述终点(76)具有到所述叶片的所述成形轮廓(40、42,50)的最小距离(dep),其特征在于所述流动引导装置(70)沿所述过渡区域(32)的至少纵向部分延伸并且被设置成当所述叶片(10)被所述入射气流冲击时在所述流动引导装置(70)和所述叶片(10)的后缘(20)之间的点处产生沿所述流动引导装置(70)的至少中心纵向部分(71)从所述叶片(10)的压力侧(52)的气流分离,所述流动引导装置的中心纵向部分沿所述流动引导装置的纵向尺度的至少80%延伸,其中在至少所述中心纵向部分内的所述流动引导装置(70)被设置成使得所述终点(76)具有从所述叶片的所述前缘观察时位于40%至92%的区间内的相对弦位置,所述相对弦位置对应由所述成形轮廓的具体截面的弦长沿弦所划分的距前缘的距离,所述相对弦位置与所述流动引导装置投影到所述成形轮廓的具体截面的弦上的点相关,并且在至少所述中心纵向部分(71)内的所述入流表面(72)被成形为针对每个横向截面,从所述终点(76)到所述成形轮廓的所述最小距离(dep)是所述成形轮廓的最大厚度的至少10%。 A wind turbine (2) for a rotor blade (10), the rotor having a substantially horizontal rotor shaft, said rotor comprising a hub (8), when mounted on the hub (8) when the vanes (10) extending substantially in a radial direction from the hub (8), said blade tip having a belt (14) and a root end (16) in the longitudinal direction (r) and a transverse direction, said blade further comprising: forming profile (40,42,50), which comprises a pressure side and a suction side and a leading edge (18) and a trailing edge (20), with the chord at the leading edge and the trailing edge extending between the chord, when is incident on the air impact molding contour to generate lift, wherein the shaped profile is divided into: the closest to the hub, having a substantially circular or elliptical shape of the root region (30), farthest from the hub, having a lift generating profile of the airfoil region (34), and a transition region at the root region (30) and the airfoil region (34) between (32), said transition region (32) having said radial direction direction from the circular or elliptical shape of the root region to the airfoil region gradually changes the lift generating profile shape, and wherein the pressure of the blade in the blade (10) of the side ( 52) has been attached to the shaping of the blade profile (40,42,50) of the flow guide means (70), said flow directing means (70) having inflow surface (72), the inflow surface (72 ) having attached to the shaping contour starting point (40,42,50) of (74) and located at a distance of the blade of the shaping profile (40,42,50) - the end point of a given distance (76), the The minimum distance (dep) the end (76) to said blade having a shaped profile (40,42,50), characterized in that said flow directing means (70) along the transition zone (32) of at least lengthwise generating points along the extending portion and is arranged such that when the blade (10) when the incident air impact in the flow directing means (70) and the blade (10) of the trailing edge (20) between the said flow directing means (70) is at least the central longitudinal portion (71) from said blade (10) of the pressure side (52) of the flow separation, the flow directing means of the longitudinal center portion along the longitudinal dimension of the flow guide means extending at least 80%, wherein the flow within at least a portion of the central longitudinal guide means (70) is arranged such that the end (76) having, when viewed from the leading edge of the blade between 40% to Relative chord locations within the interval of 92%, the relative position of the chord formed by the profile chord length along the cross section of the divided specific chord distance from the leading edge, the relative chord position with the flow directing means projection chord point related to the contour of the forming section of the concrete, and at least the central longitudinal portion of said inflow surface (71) inside (72) is shaped for each of the transverse cross-section, from the end point (76 ) to the contour of the smallest distance (dep) is at least 10% of the forming of the maximum thickness of the shaping profile.
2.根据权利要求1所述的叶片,其中在至少所述中心纵向部分(71)内的所述入流表面(72)被成形为使得针对每个横向截面,在所述终点(76)处与所述入流表面(72)相切的终点切线(80)在交叉点(82)处与所述成形轮廓(40、42、50)相交,在该交叉点处所述成形轮廓(40、42、50 )具有与所述成形轮廓(40、42、50 )相切的外形切线(78 ),并且其中在所述外形切线(78)和所述终点切线(80)之间的角度(a)是至少45度。 2. The blade of claim 1, wherein at least said central portion of said longitudinal inflow surface (71) inside (72) is shaped such that for each transverse section (76) and at the end the inflow surface (72) tangent to the end point tangent (80) at the intersection (82) at the shaping profile (40,42,50) intersect, the intersection of said shaped profile (40, 42, 50) having the shaping profile (40,42,50) tangent shape tangent (78), and wherein the angle of the contour tangent at (78) and the end point tangent (80) between (a) is at least 45 degrees.
3.根据权利要求2所述的叶片,其中在所述外形切线(78)和所述终点切线(80)之间的角度是至少50度,或至少55度,或至少60度。 3. The blade according to claim 2, wherein the angle of the contour tangent at (78) and the end point tangent (80) between at least 50 degrees, or at least 55 degrees, or at least 60 degrees.
4.根据权利要求1所述的叶片,其中所述流动引导装置的入流表面(72)的中线(86)与所述成形轮廓的弦(44)形成第二角度(Θ ),所述第二角度是至少25度,或至少30度,或至少35度。 4. The blade according to claim 1, wherein said flow directing means of the inflow surface (72) of the center line (86) with the shaped profile chord (44) forming a second angle (Θ), the second the angle is at least 25 degrees, or at least 30 degrees, or at least 35 degrees.
5.根据权利要求1所述的叶片,其中从所述叶片的所述前缘观察,所述终点的相对弦位置位于75%至92%之间的区间内,并且其中对于所述中心纵向部分的设计点而言攻角位于15至25度之间的区间内,或在15至20度之间的区间内。 5. The blade according to claim 1, wherein the leading edge of the blade from the observation, the relative position of the end point of the chord is located in the interval between 75 to 92%, and wherein the center longitudinal portion The design point in terms of the angle of attack is located within the range 15-25 degrees, or within a range of between 15-20 degrees.
6.根据权利要求1所述的叶片,其中从所述叶片的所述前缘观察,所述终点的相对弦位置位于40%至80%之间的区间内,或者位于40%至70%之间的区间内,或者位于40%至60%之间的区间内。 6. A blade according to claim 1, wherein viewed from the leading edge of the blade, the relative position of the end point of the chord is located in the interval from 40 to 80%, or between 40-70% is located between the interval between, or in the range of 40-60% between.
7.根据权利要求1所述的叶片,其中所述流动引导装置(70)基本沿所述过渡区域(32)的整个纵向长度延伸。 7. A blade according to claim 1, wherein said flow directing means (70) substantially along said transition region (32) extends the entire longitudinal length.
8.根据权利要求7所述的叶片,其中所述中心纵向部分(71)是所述流动引导装置(70)的纵向尺度的至少50%、60%、70%、80%或90%。 8. A blade according to claim 7, wherein said central longitudinal portion (71) is the flow directing means (70) of the longitudinal dimension of at least 50%, 60%, 70%, 80% or 90%.
9.根据权利要求1所述的叶片,其中所述流动引导装置(70)延伸到所述根部区域(30)内。 9. A blade according to claim 1, wherein said flow directing means (70) extending into the root region (30).
10.根据权利要求1所述的叶片,其中从所述叶片的所述前缘观察,所述终点的相对弦位置沿所述叶片的纵向方向减小。 10. A blade according to claim 1, wherein the leading edge of the blade from the observation, the longitudinal direction of the relative position of the end point along the chord of the blade is reduced.
11.根据权利要求10所述的叶片,其中从所述叶片的所述前缘观察,在所述流动引导装置的内侧部分处所述终点的相对弦位置位于75%至92%之间的区间内,并且在所述流动引导装置的外侧部分处所述终点的相对弦位置位于40%至60%之间的区间内。 11. A blade according to claim 10, wherein the leading edge of the blade from the observation, the inside portion of the flow directing means of the relative position of the end point of the chord in the interval from 75 to 92% between within, and is located within the range of 40-60% between the relative position of the chord of said flow guiding means at the end of the outer portion.
12.根据权利要求1所述的叶片,其中在所述流动引导装置(70)的至少所述中心纵向部分(71)内,从所述终点(76)到所述成形轮廓的最小距离(dep)沿纵向方向朝向所述尖端(14)减小。 At least said central longitudinal portion (71), from the end (76) to said contoured minimum distance (dep 12. blade according to claim 1, wherein said flow directing means (70) ) toward the longitudinal direction of the tip (14) is reduced.
13.根据权利要求1所述的叶片,其中所述流动引导装置(70)被形成为从所述叶片的所述成形轮廓突出的肋,基本正交于所述叶片的所述成形轮廓的肋。 13. A blade according to claim 1, wherein said flow directing means (70) is formed as a shaped rib projecting from the contour of the blade, substantially orthogonal to the contour of the rib forming the blade .
14.根据权利要求1所述的叶片,其中所述流动引导装置(70)与所述叶片(10)—体成形。 14. A blade according to claim 1, wherein said flow directing means (70) with the blade (10) - is molded.
15.根据权利要求1所述的叶片,其中所述流动引导装置(70)被装配到所述叶片(10)的表面上。 15. A blade according to claim 1, wherein said flow directing means (70) is fitted to the upper surface of the blade (10).
16.一种包括多个如前述权利要求中任一项所述的叶片的风力涡轮机。 16. A method comprising a plurality of the preceding claims, wherein the blades of a wind turbine.
Description  translated from Chinese

具有优化高度的流动引导装置的风力涡轮机叶片 Having a high degree of optimization of the flow guide means of the wind turbine blade

技术领域 FIELD

[0001] 本发明涉及用于风力涡轮机转子的叶片,该转子具有基本水平的转子轴,所述转子包括毂,当被安装于该毂时叶片基本沿径向方向从该毂延伸,所述叶片具有纵向方向和横向方向且纵向方向上带有尖端和根部端,其中所述叶片还包括:成形轮廓,该成形轮廓包括压力侧和吸力侧以及前缘和后缘,具有在前缘和后缘之间延伸的弦长的弦,当被入射气流冲击时成形轮廓产生升力,其中成形轮廓被划分为:最接近毂的具有基本圆形或椭圆形外形的根部区域、具有最远离毂的具有升力生成外形的翼型区域以及在根部区域和翼型区域之间的过渡区域,所述过渡区域具有沿径向方向逐渐从根部区域的圆形或椭圆形外形变化到翼型区域的升力生成外形的外形。 [0001] The present invention relates to a rotor for a wind turbine blade, the rotor having a substantially horizontal rotor shaft, said rotor comprising a hub, when the blade is mounted on the hub extending from the hub substantially in a radial direction, the blade having a longitudinal direction and a transverse direction and with the tip and the root end of the longitudinal direction, wherein the blade further comprises: shaping profile, the shaped contour comprising a pressure side and a suction side as well as leading and trailing edges, with the leading and trailing edges chord length chord extending between, forming air impact incident when the outline is to generate lift, wherein the shaped contour is divided into: a root region closest to the hub having a substantially circular or elliptical shape, with most having a lift away from the hub and generating the shape of the airfoil region in a transition region between the root region and the airfoil region, said transition region having a gradual change in the radial direction from the circular or elliptical shape of the root region to the lift generating profile of the airfoil region shape.

背景技术 BACKGROUND

[0002] 理论上,翼型类型的风力涡轮机叶片被成形为类似于典型飞机机翼,其中叶片的弦平面宽度及其一阶导数随着距毂距离的减小而连续增加。 [0002] In theory, the airfoil type of wind turbine blade is shaped like a typical airplane wing, where the chord plane width of the blade and the first derivative of the hub distance decreases as the distance increases continuously. 这导致了,在毂的附近,理论上叶片相当宽。 This led, in the vicinity of the hub, in theory, a relatively wide blade. 这又导致了当必须将叶片安装于毂时的问题,并且此外,由于叶片具有大的表面面积,从而这导致了在叶片工作期间具有较大载荷,例如暴风载荷。 This has led to problems when it is necessary to install the hub when the blades are in, and furthermore, since the blade has a large surface area, which thereby results in the blade working with a large load during, e.g., storm loads.

[0003] 因此,多年间,叶片的构造朝向形状方面发展,其中叶片由最靠近毂的根部区域、最远离毂的包括升力生成外形的翼型区域以及在根部区域和翼型区域之间的过渡区域构成。 [0003] Thus, among many years, build up a blade shape toward the development, by which the blade root area closest to the hub, the hub comprising farthest from the lift generating profile of the airfoil region and a transition region between the root region and the airfoil Regional composition. 关于生成升力,翼型区域具有理论或几乎理论的叶片形状,而根部区域具有基本圆形截面,这减小了暴风载荷并且使得更容易且安全地将叶片安装到毂。 About generate lift, airfoil or blade shape region having almost theoretical theory, whereas the root region has a substantially circular cross-section, which reduces storm loads and makes it easier to install and secure the blade to the hub. 根部区域直径优选地沿整个根部区域是恒定的。 Root area diameter is preferably constant along the entire root area is. 由于圆形截面的原因,根部区域不对风力涡轮机的能量生产作出贡献,并且实际上由于阻力而使其少量减少。 Due to the circular cross-section, the energy production of the wind turbine root region does not contribute to, and in fact, due to the resistance and make it small reduction. 如名称所示,过渡区域具有从根部区域的圆形形状向翼型区域的翼型外形逐渐变化的形状。 As shown in the name, the transition area has a circular shape from the root region to the airfoil shape of the airfoil region of gradually varying shape. 通常,在过渡区域中叶片的宽度随着距毂的距离增大而基本线性增大。 Typically, in the transition region of the blade width increases with distance from the hub and substantially linear increase.

[0004] 因为,例如,随着时间的推移,风力涡轮机的叶片变得越来越大并且现在可能已经超过60米长,因此对于优化空气动力学性能的需求逐渐增加。 [0004] Because, for example, over time, blades of the wind turbine becomes larger and may now be more than 60 meters long, thus increasing demand for optimizing aerodynamic performance. 风力涡轮机叶片被设计成具有至少20年的工作寿命。 Wind turbine blades are designed to have at least 20 years of working life. 因此,即使对于叶片总体性能的小的改变也会随风力叶片的工作寿命而累积成经济收益的大幅增加,其超过与这种改变相关的额外制造成本。 Thus, even for a small change in the overall performance of the blade of the wind force of the blade will accumulate into the working life of a substantial increase in the economic benefits, which exceeds the change associated with such additional manufacturing costs. 许多年间研究的关注领域针对改进叶片的翼型区域,不过在近几年,也越来越多地关注改进叶片的根部区域和过渡区域的空气动力学性能。 Research areas of concern for many years to improve the blade airfoil region, but in recent years, more and more attention to improve the aerodynamic performance of the blade root area and the transition area.

[0005] W02007/065434公开了一种叶片,其中根部区域具有凹口和/或突起以便减少来自叶片这个部分的阻力。 [0005] W02007 / 065434 discloses a blade, wherein the root area has a notch and / or projections in order to reduce resistance from this part of the blade.

[0006] W02007/045244公开了一种叶片,其中根部区域和过渡区域被设计成具有至少两个单独的翼型外形以便增加这些区域的升力。 [0006] W02007 / 045244 discloses a blade, wherein the root area and the transition area are designed to have at least two separate lift airfoil shape in order to increase these areas.

[0007] W02007/118581公开了一种叶片,其中叶片的内侧部分在叶片的压力侧上具有流动引导装置以便延迟气流的分离并且增加叶片的空气动力学性能。 [0007] W02007 / 118581 discloses a blade, wherein the inner portion of the blade has a flow directing means in order to delay separation of the air flow on the pressure side of the blade and to increase the aerodynamic performance of the blade.

[0008] W002/08600公开了一种叶片,其包括用于连接风力涡轮机的毂的连接部分,其中所述连接部分具有从连接部分突出的肋,从而增加了风力涡轮机的整体效率。 [0008] W002 / 08600 discloses a blade comprising a connection portion for connecting a wind turbine hub used, wherein the connecting portion has ribs projecting from the connecting portion, thereby increasing the overall efficiency of the wind turbine.

发明内容 SUMMARY

[0009] 本发明的目标是获得一种新型叶片,并且其克服或改善了现有技术的至少一个缺点或者其提供了有用的替代品。 [0009] The object of the present invention is to obtain a new blade, and which overcomes or ameliorate at least one of the disadvantages of the prior art or which provides a useful alternative.

[0010] 根据本发明的第一方面,叶片具有在叶片的压力侧被附加于叶片的成形轮廓的流动引导装置,所述流动引导装置具有入流表面,该入流表面具有附连到成形轮廓的起点以及位于距叶片的成形轮廓一段距离处的终点,该终点具有到叶片的成形轮廓的最小距离,其中所述流动引导装置沿过渡区域的至少纵向部分延伸并且被设置成当叶片被入射气流冲击时在流动引导装置和叶片的后缘之间的点处产生沿流动引导装置的至少中心纵向部分从叶片的压力侧的气流分离,其中在至少所述中心纵向部分内的流动引导装置被设置成使得终点具有从叶片的前缘观察的位于40%至92%的区间内的相对弦位置,并且处于至少所述中心纵向部分内的入流表面被成形为针对每个横向截面,从终点到成形轮廓的最小距离是在该截面内成形轮廓的最大厚度的至少10%。 [0010] According to a first aspect of the present invention, the blade having a pressure side of the blade is attached to the blade profile forming flow directing means, said guide means having a flow surface inflow, the inflow surface has a shaping profile attached to the starting point and is located at a distance from the end of the shaping profile from the blade, the end with the smallest distance to the forming of the profile of the blade, wherein said flow directing means in the transition region at least partially longitudinally extending blades and is arranged such that when the airflow is incident shock generating at the point along the flow guide means and the trailing edge of the blade flow guide means between at least the central longitudinal portion of the airflow from the pressure side of the blade of the separation, wherein at least a portion of said central longitudinal flow guide means is arranged such that From the end of the blade having a leading edge chord seen at opposite positions from 40 to 92% of the interval, and in the central longitudinal surface of at least the inflow portion is shaped within the transverse cross-section for each, from the end to the shaping profile The minimum distance is at least 10% of the shaped profile in cross-section the maximum thickness.

[0011] 因此,可以看出,针对流动引导装置的中心纵向部分内的所有横向截面,流动引导装置的相对高度是局部最大外形厚度的至少10%,这显著大于常规流动引导装置。 [0011] Thus, it can be seen, for all transverse cross-sectional center of the flow guide means inside the longitudinal portion, the relative height of the flow guide means is at least 10% of the local maximum thickness shape, which is significantly larger than the conventional flow directing means. 流动引导装置被安装到叶片的内侧部分,即最靠近毂的部分,并且具体地安装到叶片的过渡区域。 Flow directing means is mounted to the inner portion of the blade, i.e. the part closest to the hub, and in particular the installation into the transition zone of the blade. 从叶片的这个部分产生的动力是非常贫乏的,不过在管理这个部段的入流角度方面,根据本发明附连流动引导装置显著增加了叶片的这个部段上的寿命。 Power generation from this portion of the blade is very poor, but in the management of this section of the inflow angle, the apparatus significantly increases the lifetime of the segment on the blade attachment according to the present invention the flow guide. 流动引导装置用于阻碍在外形的压力侧上的流动。 Flow directing means for obstruction in the shape of the pressure side of the flow. 这种阻碍导致了由于流动的脱离而在流动引导装置之后(即在流动引导装置和风力涡轮机叶片的后缘之间)具有更大压力。 This leads to obstruction (i.e., between the flow guide means and the trailing edge of a wind turbine blade) because of the flow from and after the flow guide means having a greater pressure. 在流动引导装置之后,即在流动引导装置和风力涡轮机叶片的后缘之间,气流产生分离。 After the flow guide means, i.e. between the flow guide means and the trailing edge of the wind turbine blade, the airflow separation generated. 因此,流动引导装置高度的增加也显著增加了具体叶片节段的阻力。 Therefore, the height of the guide means the flow increases also significantly increased the resistance to specific blade segments. 不过,实验惊人地证明,与相对高度基本小于10%的常规流动引导装置相比,根据本发明的流动引导装置尽管增加了阻力不过仍将整体升力-阻力比提高了高达10%或更多。 However, experiments surprisingly show that compared with the conventional apparatus of the flow relative height substantially less than 10% of the guide, the flow guide means according to the present invention, despite the increase in resistance, but still the overall lift - drag ratio improved up to 10% or more. 与没有这种流动引导装置的常规风力涡轮机叶片相比,对潜在性能提高的实际估算是年度能量产量的1-1.5%。 Compared with a conventional flow without such a wind turbine blade guiding means, the actual estimate of the potential performance improvement is 1-1.5% of the annual energy production. 当考虑风力涡轮机转子的使用寿命时,相比于与制造具有这种流动引导装置的叶片有关的额外制造成本,这提供了显著的经济效益。 When considering the service life of the wind turbine rotor, compared with the manufacturing costs associated with the additional manufacturing such flow guide vane apparatus, which provides significant economic benefits.

[0012] 最小距离被定义为沿成形轮廓的法线从入流表面的终点到成形轮廓的距离。 [0012] is defined as the minimum distance along the normal to the contour formed from the inflow end to the contoured surface of the distance. 因此,最小距离对应于中心在入流表面的终点处且仅触及叶片的成形轮廓的单个点的圆的半径。 Therefore, the minimum radius of the circle from the center at the end of the inflow surface and contoured blade touches only a single point corresponding to.

[0013] 相对弦位置对应由成形轮廓的具体截面的弦长所划分的(沿弦)距前缘的距离。 [0013] The relative position of the chord length of the chord formed by the specific cross-sectional profile of the distance from the leading edge of the divided (along the chord). 因此,相对弦位置与流动引导装置投影到该弦上的点相关。 Therefore, the relative position of the flow guiding means chord is projected onto a point on the associated chord.

[0014] 根据有利实施例,从终点到成形轮廓的最小距离是成形轮廓的最大厚度的至少11%、12%、13%、14%、15%、16%、17%、18%、19%、20%、21%、22%、23%、24% 或25%。 At least 11% [0014] According to an advantageous embodiment, the end contoured to the minimum distance is the maximum thickness of the shaping profile, 12%, 13%, 14%, 15%, 16%, 17%, 18%, 19% 20%, 21%, 22%, 23%, 24% or 25%. 在此方面,已经惊人地发现,根据这些高度增加流动引导装置的相对高度,则进一步增加了叶片的能量产量。 In this regard, it has been surprisingly found that, depending on the relative height of these highly increase the flow guide means, further increasing the energy yield of the blades.

[0015] 由于制造考量的因素,从终点到成形轮廓的最小距离有利地小于或等于成形轮廓的最大厚度的50%、45%、40%、35%或30%。 Minimum distance [0015] Since the factors of manufacturing considerations, from the end to the shaping profile is advantageously less than or equal to 50% of the profile forming the maximum thickness, 45%, 40%, 35% or 30%.

[0016] 根据优选实施例,在流动引导装置的至少中心纵向部分内的入流表面被成形为使得针对每个横向截面,在终点与入流表面相切的终点切线在交叉点处与成形轮廓交叉,在该交叉点处成形轮廓具有与成形轮廓相切的外形切线,并且其中在外形切线和终点切线之间的角度(a)是至少45度。 [0016] According to the inflow surface of at least the center of the preferred embodiment, the flow directing means within the longitudinal portion is shaped such that for each transverse section, at the end of the inflow end surface tangent to the tangent at the intersection with the cross-shaped contour, shaping profile has a contoured shape tangent to the tangent at the intersection point, and wherein the angle between the tangent and the end point of the tangent of the shape (a) is at least 45 degrees. 不过,明显的是,气流的“释放角度”的增加使得具体叶片节段的阻力也显著增加。 However, obviously, increasing airflow "release angle" is such that the specific resistance of the blade segment also significantly increased. 不过,实验已惊人地证明根据该实施例的流动引导装置虽然使得阻力增加,不过与所述角度基本小于45度的常规流动引导装置相比,在流动引导装置的纵向尺度内仍将整体升力-阻力比提高了至少5%。 However, experiments have proved surprisingly although the guide means such that the flow resistance increases in accordance with this embodiment, but substantially less than with the conventional flow angle of 45 degrees compared to the guide means, the guide means within the flow of the overall longitudinal dimension will lift - resistance ratio increased by at least 5%. 因此,升力-阻力比的增加甚至进一步提高了风力涡轮机转子的整体性能,并且仅升力的增加减少了局部入流角度,从而稍稍限制了在吸力侧被分离的流动区域的尺寸。 Thus, the lift - drag ratio is increased even further improves the overall performance of the wind turbine rotor and increases only partially reduced lift inflow angle, thereby slightly limiting the size of the separated flow area on the suction side. 应该注意到,终点切线和外形切线形成了多于一个角度。 It should be noted, the end point tangent and shape is formed more than one tangent angle. 从下述详细描述中,明显的是,提到的角度是在终点切线的外部和外形切线朝向叶片的后缘延伸的部分之间的角度。 From the following detailed description, it is apparent, the angle is referred to at the end of the angle portion and the tangent of the external shape of the tangent extending toward the trailing edge of the blade between. 换言之,提到的角度位于最靠近叶片的后缘的在叶片外形外侧的象限(四分之一圆)。 In other words, the angle referred to is located closest to the trailing edge of the blade in the blade shape of the outer quadrant (quarter circle). 两条切线形成了锐角和钝角(除非它们相互垂直)。 Two tangents form the acute and obtuse angles (unless they are perpendicular to each other). 因此,明显的是这是至少45度的锐角。 Thus, it is apparent that an acute angle of at least 45 degrees.

[0017] 根据有利实施例,外形切线和终点切线之间的角度是至少50度,或者至少55度,或者至少60度。 [0017] According to an advantageous embodiment, the angle between the tangent and the end point tangent shape is at least 50 degrees, or at least 55 degrees, or at least 60 degrees. 角度可以高达90度。 Angle may be up to 90 degrees. 优选地,角度位于60至90度的区间内,惊人地发现这种角度提供了最佳的效率,即使具有高度分离和增加的阻力也是如此。 Preferably, the angle is located within the range of 60 to 90 degrees, surprisingly found that this angle provides the optimum efficiency, even though having a high degree of separation and increased resistance as well. 已经发现,升力-阻力比在所述区间内基本恒定。 It has been found, the lift - drag substantially constant ratio within the range.

[0018] 根据又一有利实施例,入流表面的中线与弦形成第二角度,该第二角度是至少25度,或至少30度,或至少35度。 [0018] According to a further advantageous embodiment, the center line and the chord of the inflow surface forming a second angle, the second angle is at least 25 degrees, or at least 30 degrees, or at least 35 degrees. 第二角度可以是对于终点切线和外形切线之间的角度的补充设计参数,或者其可以是替代性设计参数。 The second angle may be the end point tangent angle between the tangent and shape supplementary design parameters, or it may be an alternative design parameters. 根据有利实施例,入流表面沿与弦形成一角度的线基本对齐,该角度是至少25度,或至少30度,或至少35度。 According to an advantageous embodiment, the inflow surface and the chord along a line forming an angle of substantially aligned, the angle is at least 25 degrees, or at least 30 degrees, or at least 35 degrees. 因此,如果入流表面是直的,则终点切线与弦形成的角度也可以是至少25度,或至少30度,或至少35度。 Therefore, if the inflow surface is straight, the angle of the tangent to the chord end may also be formed by at least 25 degrees, or at least 30 degrees, or at least 35 degrees. 中线对应入流表面的线性拟合线或者入流表面的平均切线。 Middle line corresponds to the linear fit inflow surface or the surface of the average tangential inflow. 因此,可以看出,入流表面平均上与弦形成至少25度的第二角度。 Thus, it can be seen, the average inflow surface is formed on the second chord angle of at least 25 degrees. 而且,应该注意,第二角度指代的是在中线和弦之间形成的锐角。 Moreover, it should be noted that the second angle refers to the acute angle formed between the centerline of the chord.

[0019] 根据另一有利实施例,从叶片前缘观察,终点的相对弦位置位于75%至92%之间的区间内,并且其中对于中心纵向部分的设计点而言攻角位于15至25度之间的区间内,或者在15至20度之间的区间内。 [0019] According to another advantageous embodiment, as viewed from the blade leading edge, the relative position of the end point of the chord is located in the interval between 75 to 92%, and wherein the central longitudinal portion of the design point for the purposes of the angle of attack is located 15-25 within the range of degrees, or interval between 15-20 degrees. 当流动引导装置的终点位于向后位置(即叶片后缘附近的位置)时,已经发现随着攻角增加到近似25度的攻角,升力系数增加,而在该区间内的升力-阻力比基本恒定。 When the end of the flow guide means is located at a rearward position (i.e., close to the blade edge position), it has been found that as the angle of attack increases to approximately 25 degrees angle of attack, the lift coefficient increases, and the lift in the interval - drag ratio substantially constant.

[0020] 根据又一实施例,从叶片的前缘观察,终点的相对弦位置位于40%至80%之间的区间内,或在40%至70%之间的区间内,或在40%至60%之间的区间内。 [0020] According to yet another embodiment 40%, as seen from the leading edge of the blade, the relative position of the end point of the chord is located in the interval from 40 to 80% between, or within the range between 40% to 70%, or at within the range of 60% to between. 当流动弓I导装置的终点位于向前位置(即朝向最大厚度的截面点和叶片的后缘的位置)时,已经令人惊讶地发现升力系数和升力-阻力比基本独立于进入气流的攻角。 When the end of the flow guide means located at the bow I forward position (i.e. the position of the trailing edge toward the point of the maximum cross-sectional thickness and the blade), the case has been surprisingly found that the lift coefficient and the lift - drag ratio substantially independent of the air flow entering the attack angle. 因此,入流角度的工作范围可以被扩展并且同时保持来自叶片的增加的工作生产产量。 Therefore, the scope of work can be extended inflow angle and keep working while production output increased from leaves of. 此外,叶片对于风速的波动更不敏感,因此减小了叶片上的载荷。 In addition, the blades for wind speed is less sensitive to fluctuations, thereby reducing the load on the blades.

[0021] 根据又一有利实施例,流动引导装置基本沿过渡区域的整个纵向长度延伸。 [0021] According to a further advantageous embodiment, the flow directing entire longitudinal length of the transition region extends substantially along the apparatus. 因而,对于基本整个空气动力学上非理论的过渡区域而言,提高了升力和升力-阻力比。 Thus, for substantially the entire transition region on a non-aerodynamic theory, raising the lift and the lift - drag ratio.

[0022] 在根据本发明的优选实施例中,中心纵向部分是流动引导装置的纵向尺度的至少50%、60%、70%、80% 或90%。 [0022] In a preferred embodiment of the present invention, the central longitudinal portion is at least 50% of the flow directing means of the longitudinal dimension, 60%, 70%, 80% or 90%.

[0023] 实验已经惊人地证明,针对小攻角,流动引导装置或阻流板可以有利地朝向截面外形的最大厚度的点运动,而针对大攻角,流动引导装置可以有利地朝向叶片的后缘运动。 After the [0023] Experiments have proved surprisingly for a small angle of attack, the flow directing device or spoilers may advantageously point toward cross-sectional profile of the maximum thickness of the movement, but for the high angle of attack, the flow guide means toward the blade can be advantageously edge movement. 不过,在转子叶片上,随着叶片半径的增加,由于局部旋转速度的增加,流动角度将减小。 However, on the rotor blades, with increasing blade radius, due to the increased local rotation speed, the flow angle decreases. 因此,当沿外侧方向观察,即朝向叶片的翼型区域观察时,在根部区域附近,流动引导装置应该朝向叶片的后缘运动,并且之后其应该逼近前缘。 Thus, when viewed in the direction along the outer side, i.e., toward the blade airfoil area observed in the vicinity of the root region, the flow guiding means should movement of the blade towards the trailing edge, and thereafter it should approach the leading edge. 因此,根据本发明的有利实施例,从叶片的前缘观察,终点的相对弦位置沿叶片的纵向方向减小。 Thus, according to an advantageous embodiment of the present invention, viewed from the leading edge of the blade, the relative position of the end point of the chord decreases in the longitudinal direction of the blade. 根据有利实施例,从叶片的前缘观察,在流动引导装置的内侧部分处终点的相对弦位置位于75%至92%之间的区间内,并且在流动引导装置的外侧部分处终点的相对弦位置位于40%至60%之间的区间内。 According to an advantageous embodiment, observed from the blade leading edge, at the end of the relative chord locations inside portion of the flow guide means is located within the range between 75 to 92%, and the relative chord at the end of the outer portion of the flow guide means located in the interval from 40 to 60% between. 内侧部分被限定为流动引导装置最靠近叶片的根部端或者等价地最靠近毂的部分。 The inner portion is defined as the flow guide means closest to the root end of the blade closest to the hub or equivalently portion. 外侧部分被限定为流动引导装置最靠近叶片的尖端或者等价地最远离毂的部分。 Farthest from the outer portion of the hub is defined portion of the device closest to the tip of the blade or equivalently as the mobile guide.

[0024] 根据叶片的一种具体简单实施例,流动引导装置被形成为从叶片的成形轮廓突出的肋,例如基本正交于叶片的成形轮廓的肋。 [0024] According to one particularly simple embodiment of the blade, the flow guide means is formed to protrude from the profile of the blade shaped ribs, e.g., substantially orthogonal to the ribs forming the contour of the blade. 因此,流动引导装置可以例如被成形为被安装在叶片的表面上的角杆。 Thus, the flow guiding means can for example be shaped as angle lever is mounted on the surface of the blade.

[0025] 可替代地,流动引导装置可以基本是楔形的。 [0025] Alternatively, the flow guiding means may be substantially wedge. 入流表面可以基本是直的。 Inflow surface may be substantially straight. 根据另一实施例,入流表面是凹的。 According to another embodiment, the inflow surface is concave.

[0026] 根据一种实施例,在起点处入流表面的起点切线基本平行于起点处外形的切线。 [0026] According to one embodiment, at the start of the starting point of tangential inflow surface substantially parallel to the contour tangent at the starting point. 因而,外形具有向流动引导装置的入流表面的平滑表面过渡。 Thus, the shape having a smooth surface to the flow directing means of the inflow surface of the transition.

[0027] 根据一种有利实施例,流动引导装置具有一宽度,其中宽度和弦长之间的比沿纵向方向朝向尖端减小。 [0027] According to an advantageous embodiment, the flow guide means having a width, wherein the ratio between the width of the chord length in the longitudinal direction toward the tip decreases. 这能够例如通过使得宽度沿叶片的纵向方向基本恒定来实现,因为弦长在过渡区域内增加。 This can, for example such that the longitudinal direction by a substantially constant width along the blade to achieve, because the chord length increased within the transition zone. 不过,宽度也可以沿叶片的纵向方向减小。 However, the width can be reduced in the longitudinal direction of the blade.

[0028] 在根据本发明的一种实施例中,从叶片的前缘观察,在至少中心纵向部分内的起点被设置在弦长的55%至88%之间的区域内,或者在57%至87%之间的区域内,或者在60%至85%之间的区域内。 [0028] In accordance with one embodiment of the present invention, observed from the blade leading edge, at least at the starting point of the central longitudinal section is disposed in the region of 55 to 88% of the chord length between, or 57% to 87% in the region between, or in the region between 60 to 85 percent of the. 在根据本发明的另一实施例中,从叶片的前缘观察,在至少中心纵向部分内的终点被设置在弦长的70%至90%之间的区域内,或者在75%至88%之间的区域内,或者在80%至87%之间的区域内。 In accordance with another embodiment of the present invention, observed from the blade leading edge, at least the central longitudinal end portions are disposed in the region of 70 to 90% of the chord length between, or from 75 to 88% in the region between or within the region from 80 to 87% between.

[0029] 在根据本发明的又一实施例中,在终点和叶片的后缘之间的距离沿纵向长度朝向叶片的尖端增加。 [0029] In accordance with still another embodiment of the present invention, the end point of the trailing edge and the distance between the blades increases along the longitudinal length toward the tip of the blade.

[0030] 根据优选实施例,叶片被部分制造为由纤维增强聚合物材料制成的外壳构造。 [0030] According to a preferred embodiment, the blade is manufactured by fiber reinforced shell portion-forming polymer material.

[0031] 在一种有利实施例中,流动引导装置与叶片整体成形。 [0031] In an advantageous embodiment, the flow guide means formed integrally with the blade. 因此,流动引导装置可以与叶片一同制造,例如通过如VARTM工艺的模制工艺被制造。 Thus, the flow guiding means can be manufactured together with the blade, for example, is produced by a process such as VARTM molding process. 在这种情况下,成形轮廓被认为是从入流表面的起点向入流表面的终点附近的第二点延伸的假想平滑连续表面。 In this case, the shaped contour is considered to be an imaginary smooth continuous surface extending from the second end point to the starting point of the inflow surface near the inflow surface. 在另一有利实施例中,流动引导装置被装配在叶片的表面上。 In another advantageous embodiment, the flow guide means is mounted on the surface of the blade. 因此,叶片和流动引导装置可以被分别制造,并且之后流动引导装置被装配到叶片的表面。 Thus, the blades and the flow guiding means can be manufactured separately, and thereafter the flow directing means is fitted to the surface of the blade. 从而,用于制造叶片的模具的模制表面可以具有更加简单的形式而不需要有任何间断。 Thus, the molding surface of a mold for manufacturing a blade may have a more simple form without any interruption. 这减少了当叶片在固化后要从模具被移除时叶片表面粘附于模制表面且因而被毁坏的可能性。 This reduces the likelihood of when the blade is removed from the mold after curing, the molding surface of the blade is adhered to the surface and thus being destroyed. 根据又一有利实施例,流动引导装置可以主动地从成形轮廓显现或缩回到成形轮廓。 According to a further advantageous embodiment, the flow directing means may actively contoured apparent from or retracted into the shaping profile. 流动引导装置可以被主动控制,以便根据工况,叶片可以使用或不使用从叶片的成形轮廓突出的流动引导装置来工作。 Flow directing means can be actively controlled so as to work in accordance with working conditions, the blades can be used with or without the blade from protruding contoured flow directing means.

[0032] 如上所述,流动引导装置优选地基本沿叶片的过渡区域的整个纵向尺度延伸。 [0032] As described above, the flow directing means preferably extends substantially along the entire longitudinal dimension of the blade of the transition region. 不过,流动引导装置还可以延伸到根部区域内。 However, the flow guiding means may also extend into the root region.

[0033] 根据一种实施例,流动引导装置具有带一定后方边缘高度的后方边缘,并且其中在流动引导装置的至少中心纵向部分内该后方边缘高度沿纵向方向朝向尖端减小。 [0033] According to one embodiment, the flow guide means having a certain height of the rear edge with the rear edge, and wherein at least the central longitudinal portion of the flow guide means toward the tip of the back edge to reduce the height in the longitudinal direction. 因而,获得了具有从叶片的过渡区域到翼型区域的平滑过渡的特别简单的形状,并且其中后方边缘高度和外形厚度之间的比任选地可以保持基本恒定。 Thus, to obtain a particularly simple shape with a smooth transition from the transition region to the blade airfoil region, and wherein the ratio between the height and shape of the rear edge thickness optionally can be kept substantially constant.

[0034] 根据另一实施例,流动引导装置具有带一定后方边缘高度的后方边缘,并且其中在流动引导装置的至少中心纵向部分内该后方边缘高度基本恒定。 [0034] According to the rear edge of the inner center of the at least another embodiment, the flow guide means having a certain height of the rear edge with the rear edge, and wherein the longitudinal portion of the flow guide means substantially constant height. 后方边缘高度可以从中心纵向部分向流动引导装置的纵向端部减小,以便获得向流动引导装置的纵向端部附近的成形轮廓的平滑过渡。 Height of the longitudinal ends of the rear edge of the can to flow guiding means is reduced from the central longitudinal portion, so as to obtain a smooth transition to the vicinity of the flow guide means forming longitudinal ends of the profile. 当然,所描述的后两种实施例也涉及终点到成形轮廓的最小距离。 Of course, after the described two embodiments may also relate to the contoured end of the minimum distance.

[0035] 流动引导装置的后方边缘可以向后指向叶片的后缘或者向前指向叶片的前缘。 Rear edge [0035] The flow guiding means can be directed rearwardly or forwardly the trailing edge of the blade leading edge of the blade point. 后方边缘可以是凹的、直的或凸的。 The rear edge may be concave, straight or convex.

[0036] 根据叶片的有利实施例,叶片被设计用于工作于在过渡区域的中心纵向部分内具有15-20度的攻角的情况。 [0036] According to an advantageous embodiment of the blade, the blade is designed to operate in the case of having the angle of attack of 15-20 degrees in the central longitudinal portion of the transition region.

[0037] 流动引导装置能够以不同方式来设计。 [0037] The flow guiding means can be designed in different ways. 例如,其可以被形成作为肋、三角形或稍弯曲的形状。 For example, it may be formed as ribs, triangular or slightly curved shape. 沿纵向方向,流动引导装置的形状和弦位置可以变化。 In the longitudinal direction, the shape of the flow guide means is variable chord position. 根据有利实施例,流动引导装置是阻流板装置。 According to an advantageous embodiment, the flow directing means is a baffle plate arrangement.

[0038] 根据另一有利实施例,叶片还具有在叶片的过渡区域和/或根部区域处的涡流发生器。 [0038] According to another advantageous embodiment, the blade also having a blade in the transition region and / or at the root region of the vortex generator. 当涡流发生器与流动引导装置被优化地放置在一起时,使得特别是叶片根部区具有甚至更好的性能。 When the vortex generator and the flow guiding means are placed together optimally, so that in particular the blade root region with even better performance.

附图说明 Brief Description

[0039] 在下文中参考附图中所示的实施例具体解释了本发明,附图中: [0039] In an embodiment shown in the drawings with reference to the following detailed explanation of the present invention, the drawings:

[0040] 图1示出了风力涡轮机, [0040] Figure 1 shows a wind turbine,

[0041] 图2示出了具有根据本发明的流动引导装置的风力涡轮机叶片的第一实施例的示意图, [0041] Figure 2 shows a schematic view of a first embodiment of a guiding device according to the present invention, the flow of wind turbine blades,

[0042] 图3示出了翼型外形的示意图, [0042] Figure 3 shows a schematic view of the airfoil shape,

[0043] 图4示出了根据本发明的风力涡轮机叶片的截面; [0043] Figure 4 shows a wind turbine blade of the present invention is a cross-sectional;

[0044] 图5示出了具有根据本发明的流动引导装置的风力涡轮机叶片的第二实施例的示意图, [0044] FIG. 5 shows a schematic view of a guiding device according to the present invention, the flow of the wind turbine blade of the second embodiment,

[0045] 图6示出了作为距毂的径向距离的函数的、根据本发明的第一流动引导装置的后方边缘高度, [0045] Figure 6 shows, as a function of radial distance from the hub, according to the first flow guide device of the present invention the height of the rear edge,

[0046] 图7示出了作为距毂的径向距离的函数的、根据本发明的第二流动引导装置的后方边缘高度, [0046] FIG. 7 shows as a function of radial distance from the hub, according to the present invention, the second flow guide means of the rear edge height,

[0047] 图8示出了用于根据本发明的流动引导装置的第一后方边缘形状, [0047] Figure 8 shows a first rear edge shape for directing the flow of the present apparatus according to the invention,

[0048] 图9示出了用于根据本发明的流动引导装置的第二后方边缘形状, [0048] Figure 9 shows a second means for guiding the rear edge of the shape of the flow according to the present invention,

[0049] 图10示出了用于根据本发明的流动引导装置的第三后方边缘形状, [0049] Figure 10 shows a third apparatus for guiding the rear edge of the shape of the flow according to the present invention,

[0050] 图11示出了作为入射气流的攻角的函数的升力系数的图示, [0050] FIG. 11 shows, as an illustration of the incident airflow lift coefficient of a function of angle of attack,

[0051] 图12示出了作为入射气流的攻角的函数的升力-阻力比的图示, [0051] Figure 12 shows a stream of lift as the incident angle of attack as a function of - the resistance ratio of illustration,

[0052] 图13示出了用于设计根据本发明的风力涡轮机叶片的其他参数, [0052] FIG. 13 shows a design of the other parameters of the wind turbine blade according to the invention,

[0053] 图14示出了具有根据本发明的流动引导装置的叶片的截面, [0053] Figure 14 shows a cross-section having a blade according to the flow guide means of the present invention,

[0054] 图15示出了作为流动引导装置的高度的函数的升力系数的图示,以及 [0054] FIG. 15 shows an illustration of the height of the lift coefficient as a function of the flow guide means, and

[0055] 图16示出了作为流动引导装置的高度的函数的升力-阻力比的图示,[0056] 图17示出了作为入射气流的攻角的函数的升力系数的图示,以及 [0055] Figure 16 shows a flow directing means of the lift as a function of height - resistance than the illustration, [0056] FIG. 17 shows, as an illustration of the incident airflow lift coefficient of a function of angle of attack, as well as

[0057] 图18示出了作为入射气流的攻角的函数的升力-阻力比的图示。 [0057] Figure 18 shows the flow as the incident angle of attack as a function of the lift - drag ratio of the icon.

具体实施方式 DETAILED DESCRIPTION

[0058] 图1示出了根据所谓的“Danish概念”的常规现代逆风风力涡轮机,其具有塔4、机舱6和具有基本水平转子轴的转子。 [0058] Figure 1 shows a so-called "Danish concept" conventional modern upwind wind turbine having a tower 4, a nacelle 6 and a rotor having a substantially horizontal rotor shaft. 转子包括毂8和从毂8径向延伸的三个叶片10,每个叶片10均具有最靠近毂的叶片根部16和最远离毂8的叶片尖端14。 The rotor includes a hub 8 and a blade root 16 from the hub 8 three blades 10 extending radially, each blade 10 have closest to farthest from the hub and the hub 8 of the blade tip (14).

[0059] 图3示出了使用各种参数描述的风力涡轮机的典型叶片的翼型外形50的示意图,所述参数通常用于限定翼型的几何形状。 [0059] Figure 3 shows a schematic view of an airfoil shape is described using various parameters of a typical wind turbine blade 50, the parameter generally used to define the geometry of the airfoil. 翼型外形50具有压力侧52和吸力侧54,在使用期间,即在转子旋转期间,所述压力侧52和所述吸力侧54通常分别面向迎风侧和背风侧。 50 airfoil shape having a pressure side 52 and suction side 54, during use, i.e. during rotation of the rotor, the pressure side of the suction side 52 and 54 respectively, for the windward side and generally leeward side. 翼型50具有弦60,该弦60具有在叶片的前缘56和后缘58之间延伸的弦长C。 Airfoil 50 has a chord 60, the chord between the blade 60 has a leading edge 56 and a trailing edge 58 extending in chord length C. 翼型50具有厚度t,该厚度t被定义为压力侧52和吸力侧54之间的距离。 Airfoil 50 has a thickness t, the thickness t is defined as the distance the pressure side 52 and suction side 54 between. 翼型的厚度t沿弦60变化。 The thickness t of the airfoil 60 along a chord change. 通过拱弧线62来得到距对称外形的偏移,该拱弧线62是穿过翼型外形50的中线。 By 62 to get away from the arch arc symmetrical shape shift, the arch is 62 arc airfoil shape through the middle 50's. 可以通过从前缘56向后缘58画内切圆来找到该中线。 Through from the front edge of the rear edge 58 56 to find the painting inscribed circle midline. 中线遵循这些内切圆的中心,并且距弦60的偏移或距离被称作拱度f。 Follow these midline inscribed circle in the center, and 60 from the string offset or distance is called camber f. 可以通过使用所谓的上拱度和下拱度的参数来定义不对称性,所述上拱度和所述下拱度被定义为分别从弦60到吸力侧54和压力侧52的距离。 Asymmetry can be defined by using the so-called upper camber and camber parameters, the lower the upper camber camber and is defined as the distance from the strings were 60 to 54 and the pressure side of the suction side 52.

[0060] 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图。 [0060] Figure 2 shows a schematic view of a first embodiment of the wind turbine blade 10 of the present invention. 风力涡轮机10具有常规风力涡轮机叶片的形状并且包括最靠近毂的根部区域30、最远离毂的成形或翼型区域34以及在根部区域30和翼型区域34之间的过渡区域32。 Wind turbine 10 has the shape of a conventional wind turbine blade and comprises a root region 30 closest to the hub, the hub most remote from the molding area or airfoil 34 and a transition region between the root region 30 and the region 34 of the airfoil 32. 叶片10包括当叶片被安装在毂上时面向叶片10的旋转方向的前缘18以及面向前缘18的相反方向的后缘20。 When the blade 10 includes a blade is mounted on the hub 10 when facing the direction of rotation of the blade leading edge 18 and a trailing edge 18 facing in the opposite direction of the leading edge 20.

[0061] 关于产生升力,翼型区域34 (也被称为成形区域)具有理论上或几乎理论上的叶片形状,而由于结构性考虑的原因,根部区域30具有基本圆形或椭圆形截面,这例如使得更容易且更安全地将叶片10安装于毂。 [0061] With regard to generate lift, the airfoil region 34 (also referred to as the forming region) having a theoretical or nearly theoretical blade shape, and due to structural considerations, the root region 30 having a substantially circular or oval cross-section, This example makes it easier and safer to the blade 10 is attached to the hub. 根部区域30的直径(或弦)通常沿整个根部区30是恒定的。 Diameter (or chord) of the root region 30 is typically along the entire root area 30 is constant. 过渡区域32具有从根部区域30的圆形或椭圆形形状40向翼型区域34的翼型外形50逐渐变化的过渡外形42。 The transition region from the base region 32 having a circular or elliptical shape of the airfoil region 30 of the airfoil shape 40 34 50 42 shape changes gradually transition. 过渡区域32的宽度通常随着距毂的距离r的增加而基本线性增加。 The width of the transition region 32 typically increases as the distance r from the hub and substantially linear increase.

[0062] 翼型区域34具有翼型外形50,且翼型外形50具有在叶片10的前缘18和后缘20之间延伸的弦。 [0062] airfoil region 34 has an airfoil shape 50, and the shape of the airfoil 50 having a leading edge in the chord of the blade 10 extending between 20 18 and a trailing edge. 弦的宽度随距毂的距离r的增加而减小。 The width of the chord with increasing distance r from the hub increases.

[0063] 应该注意到,叶片的不同段的弦通常不位于公共平面内,因为叶片会扭曲和/或弯曲(即,预弯曲),因此提供了具有相应扭曲和/或弯曲过程的弦平面,这种情况是常见的,以便补偿取决于距毂的半径的叶片的局部速度。 [0063] It is noted that the different sections of the blade chord is usually not located in a common plane, since the blade will distort and / or curved (i.e. pre-bent), thus providing the chord plane with a corresponding twisting and / or bending process, This situation is common to compensate for the local velocity of the blade depends on the pitch radius of the hub.

[0064] 根据本发明的风力涡轮机叶片10具有流动引导装置70,该装置70在叶片的过渡区域32内从叶片的压力侧突出。 [0064] A wind turbine blade 10 of the invention having a flow directing means 70, the apparatus 70 within the transition zone of the blade 32 protruding from the pressure side of the blade.

[0065] 图4示出了在过渡区域32内的风力涡轮机叶片10的截面。 [0065] Figure 4 shows a cross-section in the transition region 32 of the wind turbine blade (10). 在这个区域内的风力涡轮机包括具有过渡外形42的成形轮廓,该过渡外形42从根部区域32的圆形外形40逐级变化成翼型区域的翼型外形50。 In this region of the wind turbine comprises a contoured shape having a transition 42, 42 shape the transition from the circular shape of the root region 32 of the airfoil 40 is changed to the stepwise shape of the airfoil region 50. 过渡外形是来自于非理想状态的空气动力学观点。 Shape is aerodynamic viewpoint transition from non-ideal conditions. 可以看出外形具有平滑形状,流动引导装置70在叶片的压力侧上从其突出。 Shape having a smooth shape can be seen, the flow guide means 70 on the pressure side of the blade protruding therefrom. 流动引导装置70包括具有起点74和终点76的入流表面72,在起点74处入流表面72连续地延展到叶片的成形轮廓42,在终点76处流动从外形脱离。 Flow directing device 70 includes a starting point and an end point inflow surface 76 74 72, 74 at the start of the inflow surface 72 is continuously extended to the contoured blade 42, at the end of 76 from flowing out of shape. 如果流动引导装置被改装到叶片10的表面,则起点74也可以被看作是流动引导装置70的连接点。 If the flow guide means is adapted to the surface of the blade 10, the starting point 74 can also be seen as a flow directing means 70 of the connection point. 流动引导装置70还包括后方边缘84,该后方边缘84从终点76延伸到叶片10的成形轮廓42。 Flow directing means 70 further includes a rear edge 84, the rear edge 84 extends from the end 76 to the shaping profile 42 of the blade 10. 流动引导装置70的入流表面72和成形轮廓42之间的距离朝向叶片的后缘增加,以便流动引导装置具有楔形形状。 The distance between the flow guide 72 and the inflow surface of the forming device 70 of the contour 42 facing the blade trailing edge increases, so that the flow guide means having a wedge-like shape. 入流表面72可以是基本直的或者可以如图4所示是稍弯曲的。 Inflow surface 72 may be substantially straight or may be shown in Figure 4 is slightly curved.

[0066] 入流表面72被成形为,针对过渡区域32的至少中心纵向部分71中的各横向截面,在终点76处入流表面72的终点切线80在交叉点82处相交于成形轮廓42,在该交叉点82处成形轮廓42具有与成形轮廓相切的外形切线78。 [0066] inflow surface 72 is shaped, at least against the transition region 32 of the longitudinal center portion 71 of each transverse section, the end point 76 at the end 72 of the inflow surface 80 at tangent point 82 intersects the cross-shaped contour 42, in which intersection 82 forming contour 42 has contoured shape tangent to tangent 78. 终点切线80和外形切线78形成彼此间的交叉角度a。 End point tangent 80 and 78 form a cross shape tangent angle between them a. 应该注意到,终点切线和外形切线形成多于一个角。 It should be noted, the end tangents and shape tangent to form more than one angle. 从下述具体描述中可以显而易见,角度a是在终点切线的外部和外形切线的朝向叶片的后缘延伸的部分之间的角。 From the following detailed description may be apparent, the angle of a tangent at the end of the external tangent orientation and shape of the corner portion of the trailing edge of the blade extends between. 换言之,角度a位于叶片外形外部最靠近叶片的后缘的象限内。 In other words, the angle of a trailing edge of the blade is located in the external shape of the quadrant closest to the blade. 两条切线78、80形成锐角和钝角(除非它们彼此垂直)。 Two tangents 78, 80 forms an acute angle and an obtuse angle (unless they are perpendicular to each other). 因此,从说明书中显而易见到这是锐角,是至少45度。 Therefore, from the description it is apparent to the acute angle, is at least 45 degrees.

[0067] 此外,另一设计参数可以用于流动引导装置70的设计,并且具体地是,入流表面72的形状,即第二角度Θ,其是流动引导装置70的入流表面72的中线86与成形轮廓42的弦44之间的角度。 [0067] Further, another design parameters may be used to design the flow guide means 70, and specifically, the shape of the inflow surface 72, i.e., the second angle Θ, which is a flow directing means 70 of the inflow surface 72 and the center line 86 42 forming an angle profile chord 44 between.

[0068] 入流引导装置70用于阻碍在外形的压力侧上的流动。 [0068] inflow guide device 70 for obstruction in the shape of the pressure side of the flow. 这种阻碍导致了,由于流动从表面脱离,在流动引导装置70之后,即在流动引导装置70和风力涡轮机叶片的后缘之间具有更大压力。 This obstruction leads, since the flow detachment from the surface, after the flow directing means 70, i.e. between the flow guide 70 having a larger pressure and wind turbine blade trailing edge device. 在流动引导装置70之后,即在流动引导装置70和风力涡轮机叶片的后缘之间,产生气流分离。 After the flow directing means 70, i.e. between the flow guide 70 and the trailing edge of the wind turbine blade means for generating flow separation.

[0069] 当角度a是至少45度时,实验已经证明相比于具有简单流动引导装置的现有技术叶片,过渡区域32的截面的升力-阻力比能够显著增加。 [0069] When the angle a is at least 45 degrees, has been found that compared to the prior art blade having a simple flow directing means, the lift section of the transition region (32) - than can significantly increase the resistance. 这是不希望的,因为由于来自流动引导装置的气流具有更大的“释放角”,分离度且因而外形上引起的阻力会显著增加。 This is undesirable, because the air flow from the flow directing means due to greater "release angle", and thus the separation resistance due to the shape will increase significantly. 实验已经证明大于60度且高达90度的更大角度对于升力-阻力比提供了进一步的改善。 Experiments have shown that greater than 60 degrees and an angle up to 90 degrees for greater lift - drag ratio provides a further improvement.

[0070] 在第一实施例中,在图2和图7中可见,流动引导装置的后方边缘84的高度h沿纵向方向(或距毂的径向方向)朝向叶片的尖端r减小。 [0070] In the first embodiment, in FIG. 2 and FIG. 7 shows that the rear edge of the flow directing means of the height h 84 of the longitudinal direction (or from the hub in a radial direction) decreases toward the blade tip r. 后方边缘84的高度被示作是距离毂的径向距离r的函数,如图7所示。 The height of the rear edge 84 is shown as a function of the radial distance r from the hub, as shown in Fig. 在流动引导装置70最靠近毂的纵向端部处,流动引导装置70被倒圆角或呈锥形以便获得向叶片的成形轮廓的平滑过渡。 At the longitudinal ends of the flow guide means 70 closest to the hub, the flow guide means 70 is rounded or tapered so as to obtain a smooth transition to the forming of the profile of the blade. 后方边缘高度h对应沿与弦垂直的方向在流动引导装置的终点与成形轮廓之间的距离。 The height h corresponding to the rear edge along a chord direction perpendicular to the end of the flow guide means and the forming distance between the profiles.

[0071] 图5示出了根据本发明的叶片110的第二实施例,其中类似附图标记指代图2所示第一实施例中的类似部件。 [0071] FIG. 5 shows a second embodiment of the present invention, the blade 110, wherein the first embodiment shown in similar parts similar reference numerals in FIG. 因此,仅描述两种实施例间的区别。 Therefore, only differences between the two embodiments embodiment. 第二实施例的不同之处在于流动引导装置170的后方边缘184的高度至少在中心部分171内沿叶片的纵向方向基本恒定。 Differs from the second embodiment in that the flow guide means 170 of the rear edge height 184 is at least in the central portion 171 along the longitudinal direction of the blade is substantially constant. 这也在图6中被示出。 This is also shown in Fig. 6 is shown. 如图6所示,流动引导装置170在流动引导装置170的纵向端部附近能够被倒圆角或呈锥形以便获得向叶片的成形轮廓的平滑过渡。 As shown in Figure 6, the flow directing device 170 can be rounded or near tapered shaped contour so as to obtain a smooth transition to the blade longitudinal end portion of the guide means 170 in the flow.

[0072] 流动引导装置70、170的后方边缘84、184的形状可以具有各种形状。 [0072] the flow directing means of the shape of the rear edge 70, 170 84, 184 may have various shapes. 后方边缘可以例如如图8所示向后指向叶片的后缘,如图4所示被定向为基本横于弦,或者向前指向叶片的前缘(未示出)。 The rear edge 8 can, for example as shown in FIG rearwardly directed rear edge of the blade, as shown in Figure 4 is oriented substantially transverse to the string, or the leading edge of the forwardly directed blade (not shown). 后方边缘可以如图8所示是直的,如图9所示是凹的,或者如图10所示是凸的。 The rear edge may be straight as shown in FIG. 8, shown in Figure 9 is concave, or convex as shown in Fig.

[0073] 根据两种实施例的流动引导装置70、170必须被设计成使得针对流动引导装置70、170的中心部分71、171内的每个横向截面而言角度a是至少45度。 [0073] According to an embodiment of the two flow guide means 70, 170 must be designed such that the center of the flow directing means 70, 170 for each transversal cross-section in terms of an angle within a portion 71,171 is at least 45 degrees. 此外,流动引导装置70、170被设置在某一位置,以便当叶片10、110被入射气流冲击时,在流动引导装置70、170和叶片10、110的后缘20、120之间的点处沿流动引导装置70、170的至少中心纵向部分71、171从叶片的压力侧产生气流分离。 In addition, the flow guide means 70, 170 is provided at a certain position, so that when the blade 10, 110 is incident air impact, at a point between the flow guiding means 70, 170 20, 120 and the trailing edge of the blade 10, 110 flow directing means 70, 170 along the central longitudinal portion of at least 71,171 from the pressure side of the blade to produce flow separation. 在流动引导装置70、170的纵向端部附近,设计多样性可以落在这些设计参数的范围之外。 Flow directing means in the vicinity of the longitudinal end portions, design diversity 70,170 may fall outside the scope of these design parameters. 优选地,流动引导装置的中心部分71、171沿流动引导装置70、170的纵向尺度的至少80%延伸。 Center Preferably, the flow guide means along a portion 71,171 70,170 flow guiding means of the longitudinal dimension of at least 80% elongation.

[0074] 图11和图12分别示出了在变化角度a和流动引导装置的恒定后方边缘高度的情况下作为攻角AOA的函数的升力系数C1和升力-阻力比Cl/Cd的图示。 [0074] Figures 11 and 12 illustrate the rear edge at a constant height of the change in the angle a and the flow guiding means as a function of angle of attack AOA the lift coefficient C1 and lift - drag ratio Cl / Cd illustration. 在这些测量中已经被测试的具体外形被设计为在落入近似15至20度范围内的攻角AOA的情况下工作。 Concrete shape in these measurements have been tested in the fall is designed to approximate the conditions under AOA angle of attack within the range of 15-20 degrees to work. 此外,入流表面是基本直的。 In addition, the inflow surface is substantially straight.

[0075] 在图11中,第一图示210示出了a=25度情况下作为攻角AOA的函数的升力系数C1,第二图示220示出了a=65度情况下作为攻角AOA的函数的升力系数C1,并且第三图示230示出了a=85度情况下作为攻角AOA的函数的升力系数Cl。 [0075] In Figure 11, the first diagram 210 shows the case of a = 25 degrees as a function of angle of attack AOA the lift coefficient C1, the second diagram 220 shows the case of a = 65 degrees as the angle of attack AOA function of the lift coefficient C1, and the third diagram 230 illustrates the case of a = 85 degrees AOA as a function of the angle of attack of the lift coefficient Cl. 可以看出,在设计AOA的范围内升力系数显著增加。 As can be seen, a significant increase in the design lift coefficient AOA range. a=85度情况下的升力系数比a=25度情况下的升力系数例如大10-12%。 a = lift coefficient than 85 degrees in case of a = lift coefficient, e.g., 25 degrees in case of a large 10-12%.

[0076] 在图12中,第一图示240示出了a=25度的情况下作为攻角AOA的函数的升力-阻力比Cl/Cd,第二图示250示出了a=65度的情况下作为攻角AOA的函数的升力-阻力比C1/cd,并且第三图示260示出了a=85度的情况下作为攻角AOA的函数的升力_阻力比Cl/Cd。 [0076] In Figure 12, the first diagram 240 illustrates a case where a = 25 degrees of lift as a function of the angle of attack AOA - drag ratio Cl / Cd, the second diagram 250 illustrates a = 65 degrees The case of lift as a function of the angle of attack of the AOA - next resistance ratio C1 / cd, and the third diagram 260 illustrates the case of a = 85 degrees AOA as a function of the angle of attack of the lift-drag ratio _ Cl / Cd. 可以看出,在设计AOA的范围内升力-阻力比显著增加。 It can be seen in the design AOA lift range - significantly more than the resistance. a=85度情况下的升力系数比a=25度情况下的例如大近似5%。 a = lift coefficient than 85 degrees in case of a = 5%, for example approximately 25 degrees large case.

[0077] 应该注意到,第二角度Θ可以用作设计流动引导装置的补充或替代参数。 [0077] It should be noted, the second angle Θ can be used as supplemental or alternative flow guide design parameters of the device. 在这种情况下,根据本发明,第二角度Θ应该是至少25度。 In this case, according to the present invention, the second angle Θ should be at least 25 degrees. 图11和图12示出的图示分别对应于 11 and FIG. 12 shows an illustration corresponding to FIG.

0、45和60度的第二角度Θ。 0,45 and the second angle 60 degrees Θ. 因为入流表面是直的,所以第二角度Θ也对应于终点切线和弦之间的角度。 Because the inflow surface is straight, so a second end tangent angle Θ angle between chords also corresponds.

[0078] 还已发现,流动引导装置的高度以及流动引导装置的弦位置与叶片的性能相关。 [0078] It has also been found that the height of the flow guide means and the flow guide performance associated with the blade chord position of the device. 因此,当设计流动引导装置时必须引入另一设计参数,即流动引导装置的高度(或等价地终点到叶片的成形轮廓的最小距离dep)以及终点的相对弦位置cep。 Thus, when designing the flow guiding means is necessary to introduce the other design parameters, i.e., the height of the flow guide device (or equivalently to the minimum distance from the end of contoured blade dep) and the relative chord locations cep end. 这些参数在图13中被示出。 These parameters are illustrated in Figure 13. 因此,可以看出,设计参数dep被给定为沿成形轮廓的法线从入流表面的终点到成形轮廓的距离。 Thus, it can be seen, the design parameters are given as dep contoured along the normal to the inflow from the end surface to the contoured distance. 因此,最小距离对应于中心在入流表面的终点处且仅接触叶片的成形轮廓的单个点的圆的半径。 Therefore, the minimum radius of the circle from the center of a single point at the end point of the inflow surface and only contact blade shaped profile corresponding to. 流动引导装置的高度在下文中被描述为相对高度,其针对给定截面被给定为终点到成形轮廓的最小距离与成形轮廓在该截面内的最大厚度之间的比dep/t_。 Highly liquid guiding means is hereinafter described as relative height, which for a given cross-section is given by the end of the shaping profile contoured in the minimum distance within the section ratio dep / t_ between the maximum thickness.

[0079] 流动引导装置高度的增加也显著增加了具体叶片段的阻力。 Increasing the height of the apparatus [0079] flow guide also significantly increased the resistance of concrete blade sections. 不过,实验已经惊人地证明了与相对高度基本小于10%的常规流动引导装置相比,根据本发明的流动引导装置虽然阻力增加但是仍显著提高了整体升力和/或整体升力-阻力比。 However, experiments have surprisingly demonstrated compared with the conventional flow directing means relative height substantially less than 10%, the flow guide means according to the present invention, although the increase in resistance but still significantly improved the overall lift and / or the overall lift - drag ratio.

[0080] 从图11和图12绘制的实施例可以看出,在60至90度的释放角度范围内,升力-阻力比基本恒定。 [0080] 12 drawn from FIG. 11 and FIG embodiments can be seen, the release angle within the range of 60 to 90 degrees, lift - drag ratio substantially constant. 因此,实验证明,使用从叶片的成形轮廓基本法向地突出的流动引导装置是足够的。 Thus, experiments show that the use of the contoured Basic blade radially protruding flow guiding means is sufficient. 这样的实施例在图14中被示出,其中类似附图标记对应图4所示的实施例中的类似部件,并且其中可以看出基本肋型的流动引导装置270在叶片的吸力侧上从表面突出。 Such an embodiment is shown in Figure 14, wherein like reference numerals correspond to the embodiment shown in Figure 4 is similar parts, and in which it is substantially rib-type flow guide means 270 on the suction side of the blade from surface prominent. 在这个实施例中的入流表面272面向进入的流动或者朝向叶片的前缘。 Example In this embodiment of the inflow surface 272 facing the incoming flow or toward the blade leading edge. 能够通过使用第一附连装置294和第二附连装置296将流动引导装置270安装到叶片的表面,其可以以任意常规方式被连接到叶片,例如通过胶粘或通过使用螺母和螺栓装置。 294 and can be for example by gluing or by using a nut and bolt means to the second attachment means 296 the flow guide means 270 mounted to the surface of the blade, which can be connected in any conventional manner to the blade, by using the first attachment means. 可替代地,使用仅具有单个附连装置的角杆是足够的。 Alternatively, using only a single attachment angle lever connected device is sufficient.

[0081] 图15-18分别示出了升力系数C1和升力-阻力比Cl/Cd的图示,并且其中可以看出流动引导装置的高度变化的影响。 [0081] Figures 15-18 show the lift coefficient and the lift C1 - resistance ratio Cl / Cd illustration, and in which it is highly variable flow directing means of the impact. 在过渡外形上进行试验,该过渡外形具有450mm的弦长和280_的最大厚度。 Tested in the transition form factor, the transition has a 450mm chord shape and a maximum thickness of 280_. 所用的流动引导装置是被安装到外形的压力侧的肋。 Flow directing means is used in the shape of a rib is mounted to the pressure side. 在两个安装点处测试流动引导装置,其中第一安装点距叶片的前缘210mm、对应47%的相对弦位置,第二安装点距叶片的前缘410mm、对应91%的相对弦位置。 Testing at the two mounting points flow guiding means, wherein the first mounting pitch of the blade leading edge 210mm, corresponding to 47% of the relative chord location, the second mounting pitch of the blade leading edge 410mm, corresponding to 91% of the relative chord position. 使用的三个不同的肋分别具有20mm、30mm和40mm高度,分别对应7.1%、10.7%和14.3%的相对高度。 The use of three different ribs each having 20mm, 30mm and 40mm height, respectively 7.1%, 10.7% and 14.3% relative height.

[0082] 在图15中,第一图示310示出了9度攻角且被安装在47%的相对弦位置处的情况下作为肋高度的函数的升力系数Cl。 [0082] In Figure 15, the first diagram 310 shows a 9-degree angle of attack and is mounted in the case at a relative position of 47% chord as a function of the height of the rib lift coefficient Cl. 第二图示315示出了27度攻角且被安装在47%的相对弦位置处的情况下作为肋高度的函数的升力系数Cl。 The second diagram 315 shows the angle of attack of 27 degrees in the case and is installed at a position of 47% of the relative chord rib height as a function of the lift coefficient Cl. 第三图示320示出了9度攻角且被安装在91%的相对弦位置处的情况下作为肋高度的函数的升力系数Cl。 The third diagram 320 shows a 9-degree angle of attack and is mounted in the case at a relative position of 91% chord as a function of the height of the rib lift coefficient Cl. 第四图示325示出了27度攻角且被安装在91%的相对弦位置处的情况下作为肋高度的函数的升力系数Cl。 The fourth diagram 325 shows a 27-degree angle of attack and is mounted in the case at a relative position of 91% chord as a function of the height of the rib lift coefficient Cl.

[0083] 图16示出了升力-阻力比Cl/Cd的对应图示。 [0083] Figure 16 shows a lift - drag ratio Cl / Cd corresponding icon. 第一图示330示出了9度攻角且被安装在47%的相对弦位置处的情况下作为肋高度的函数的升力-阻力比Cl/Cd。 The first diagram 330 shows a 9-degree angle of attack and is mounted in the case at a relative position of 47% chord as a function of the height of the ribs of the lift - drag ratio Cl / Cd. 第二图示335示出了27度攻角且被安装在47%的相对弦位置处的情况下作为肋高度的函数的升力-阻力比Cl/Cd。 The second diagram 335 shows the angle of attack of 27 degrees in the case and is installed at a position of 47% of the relative chord rib height as a function of the lift - drag ratio Cl / Cd. 第三图示340示出了9度攻角且被安装在91%的相对弦位置处的情况下作为肋高度的函数的升力-阻力比Cl/cd。 The third diagram 340 shows a 9-degree angle of attack and is mounted in the case at a relative position of 91% chord as a function of the height of the ribs of the lift - drag ratio Cl / cd. 第四图示345示出了27度攻角且被安装在91%的相对弦位置处的情况下作为肋高度的函数的升力-阻力比Cl/Cd。 The fourth diagram 345 shows a 27-degree angle of attack and is mounted in the case at a relative position of 91% chord as a function of the height of the ribs of the lift - drag ratio Cl / Cd.

[0084] 在图17中,第一图示350示出了流动引导装置被安装在47%的相对弦位置处且具有7.1%的相对高度的情况下作为攻角的函数的升力系数Cl。 [0084] In FIG. 17, the first diagram 350 shows the flow guide means is mounted range as a function of the angle of attack of the relative height of the lift coefficient Cl of 7.1 percent at a position of 47% relative to the chord. 第二图示355示出了流动引导装置被安装在47%的相对弦位置处且具有14.3%的相对高度的情况下作为攻角的函数的升力系数Cl。 The second diagram 355 shows the flow guide means is mounted range as a function of the angle of attack of the lift coefficient Cl relative height of the 14.3% of the chord at a position relative to 47%. 第三图示360示出了流动引导装置被安装在91%的相对弦位置处且具有7.1%的相对高度的情况下作为攻角的函数的升力系数Cl。 The third diagram 360 shows the flow guide means is mounted at a position of 91% relative to the chord and having as a function of the angle of attack of the relative height of the lift coefficient Cl of 7.1 percent. 第四图示365示出了流动引导装置被安装在91%的相对弦位置处且具有14.3%的相对高度的情况下作为攻角的函数的升力系数 The fourth diagram 365 illustrates a case where a relatively high degree of 14.3% as a function of angle of attack of the lift coefficient and the flow guiding means is mounted at a position having a 91% relative to the chord

Ci ο Ci ο

[0085] 图18示出了升力-阻力比C1Ad的对应图示。 [0085] Figure 18 shows the lift - drag ratio C1Ad corresponding icon. 第一图示370示出了流动弓丨导装置被安装在47%的相对弦位置处且具有7.1%的相对高度的情况下作为攻角的函数的升力-阻力比Cl/cd。 The first diagram 370 shows the relative position of the flow of the bow string 丨 guide means is mounted in 47% and having a relatively high level of 7.1 percent as a function of the angle of attack of the lift - drag ratio Cl / cd. 第二图示375示出了流动引导装置被安装在47%的相对弦位置处且具有14.3%的相对高度的情况下作为攻角的函数的升力-阻力比Cl/cd。 The second diagram 375 shows the relative position of the chord flow guide means is mounted in 47% and having a relative height of the 14.3% as a function of the angle of attack of the lift - drag ratio Cl / cd. 第三图示380示出了流动引导装置被安装在91%的相对弦位置处且具有7.1%的相对高度的情况下作为攻角的函数的升力-阻力比Cl/Cd。 The third diagram 380 shows the flow guide means is mounted at a position of 91% relative to the chord and has a relatively high level of 7.1% of the lift as a function of angle of attack - the resistance ratio Cl / Cd. 第四图示385示出了流动引导装置被安装在91%的相对弦位置处且具有14.3%的相对高度的情况下作为攻角的函数的升力-阻力比C1A^ The fourth diagram 385 illustrates a flow guide means is mounted and a case having a relatively high degree of 14.3% as a function of angle of attack at a position opposite the lift 91% of the chord - drag ratio C1A ^

[0086] 从图15中可以看出,当流动引导装置的高度增加时,升力系数增加;这与流动引导装置的位置和入流的攻角无关。 [0086] As can be seen from Figure 15, when the height of the flow directing means increases the lift coefficient increases; nothing to do with the flow directing means of the position and angle of attack inflow. 通过将流动引导装置的相对高度从7.1%增加到14.3%,根据装置的位置和攻角,升力增加15%_50%。 By the relative height of the flow guide means increased 14.3 percent from 7.1 percent, according to the position and angle of attack of the device, lift 15% _50%. 对于所有装置位置和工作攻角而言,趋势是,流动引导装置的高度越高,则升力系数越大。 For all devices and operating position angle of attack, the trend is that the higher the altitude the flow guiding device, the lift coefficient increases. 这也被图17所支持,并且申请人进行了额外的实验(未示出)。 This is also supported by Fig. 17, and the applicant carried out an additional experiment (not shown).

[0087] 从图15中还可以看出,在入流攻角较小的工况下应该朝向叶片的前缘移动流动引导装置。 [0087] can also be seen from Figure 15, the angle of attack smaller inflow conditions should move toward the leading edge of the blade flow guide means. 相反地,当攻角较大时应该朝向叶片的后缘移动流动引导装置。 Conversely, when the angle of attack is large trailing edge of the blade should move towards the flow guide means. 在转子叶片上,由于局部旋转速度增大的原因,随着叶片半径的增加,流动角度将减小。 On the rotor blades, the rotational speed is increased due to local reasons, with increasing blade radius, the flow angle decreases. 因此,当沿外侧方向朝向翼型区域观察时,在根部区域附近,应该朝向叶片的后缘,例如90%的相对弦位置附近,来移动流动引导装置,并且之后流动引导装置应该接近前缘,例如50%的相对弦位置附近。 Accordingly, when the direction toward the airfoil along the outside observation area, in the vicinity of the root region, should be facing the rear edge of the blade, for example, near 90% chord position relative to move the flow guide means, and thereafter the flow guiding means should be close to the leading edge, near 50% relative chord location, for example.

[0088] 图16示出了独立于流动引导装置的高度,当朝向叶片的后缘移动流动引导装置时升力-阻力比增加。 [0088] FIG. 16 shows the flow guiding means is independent of the height, when moving towards the trailing edge of the blade flow guide means lift - drag ratio increases.

[0089] 如图17所示,当流动引导装置被置于叶片的后缘附近时,随着攻角的增大,升力系数将增加,而针对流动引导装置的前向位置,升力系数将开始减小。 [0089] As shown in Figure 17, when the flow guide means is disposed near the trailing edge of the blade, with the angle of attack increases, the lift coefficient will increase, while the forward position against the flow guide means, will begin to lift coefficient decreases. 因此,根据给定截面处的准确入流角度,对于流动引导装置而言具有产生最大可能升力系数的一个优化部位。 Thus, according to an accurate inflow angle at a given cross-section, for purposes of generating flow guide means having a maximum possible lift coefficient optimization portion.

[0090] 图18示出了与改变流动引导装置的高度的影响相比,作为攻角函数的升力-阻力比的变化是不显著的。 [0090] Figure 18 shows a high degree of influence and alter the flow guiding means compared to the angle of attack as a function of the lift - drag ratio change is not significant. 还可以看出,当流动引导装置运动到前向位置,即朝向叶片的前缘运动时,流动引导装置的高度变化的效果减小。 Can also be seen that, when the flow guide means is moved to the forward position, i.e., movement toward the leading edge of the blade, the effect of the flow guide means of the height variation is reduced. 因此,入流角度的工作范围可以被扩展。 Therefore, the scope of work inflow angle can be extended.

[0091] 已经参考优选实施例描述了本发明。 [0091] have been described with reference to preferred embodiments of the present invention. 不过本发明的范围不限于所示实施例,并且在不偏离本发明范围的情况下能够实现替代方式和改型。 However, the scope of the present invention is not limited to the illustrated embodiments, and without departing from the scope of the present invention can realize alternative ways and variations.

[0092] 附图标记列表 [0092] List of reference numerals

[0093] 2风力涡轮机 [0093] 2 of the wind turbine

[0094] 4 塔 [0094] 4 tower

[0095] 6 机舱 [0095] 6 cabin

[0096] 8 毂 [0096] 8 hub

[0097] 10 叶片 [0097] 10 blades

[0098] 14叶片尖端 [0098] 14 blade tip

[0099] 16叶片根部 [0099] 16 of the blade root

[0100] 18 前缘 [0100] 18 leading edge

[0101] 20 后缘 [0101] 20 trailing edge

[0102] 30根部区域 [0102] 30 root area

[0103] 32过渡区域 [0103] 32 transition area

[0104] 34翼型区域 [0104] 34 airfoil area

[0105] 40,42,50成形轮廓/外形 [0105] 40,42,50 shaping profile / shape

[0106] 44 弦 [0106] 44 chord

[0107] 52压力侧 [0107] 52 pressure side

[0108] 54吸力侧 [0108] 54 suction side

[0109] 56 前缘 [0109] 56 leading edge

[0110] 58 后缘 [0110] 58 trailing edge

[0111] 60 弦 [0111] 60 chord

[0112] 62拱弧线/中线 [0112] 62 arc arch / midline

[0113] 70流动引导装置/阻流板 [0113] flow guiding means 70 / spoiler

[0114] 71中心纵向部分 [0114] 71 central longitudinal section

[0115] 72入流表面[0116] 74 起点 [0115] 72 inflow surface [0116] 74 starting

[0117] 76 终点 [0117] 76 end

[0118] 78外形切线 [0118] 78 appearance tangent

[0119] 80终点切线 [0119] 80 end tangent

[0120] 82交叉点 [0120] 82 intersection

[0121] 84流动引导装置的后方边缘 [0121] 84 of the flow guide means rear edge

[0122] 86入流表面的中线 [0122] 86 surface inflow midline

[0123] 210-260 图示 [0123] 210-260 icon

[0124] 294第一附连装置 [0124] The first attachment means 294

[0125] 296第二附连装置 [0125] The second attachment means 296

[0126] 310-385 图示 [0126] 310-385 icon

[0127] a在外形切线和终点切线之间的角度 [0127] a tangent angle between the shape and the end point tangent

[0128] c 弦长 [0128] c chord length

[0129] C1升力系数 [0129] C1 lift coefficient

[0130] C1Ad升力-阻力比 [0130] C1Ad lift - drag ratio

[0131] dt最大厚度的位置 [0131] The position dt of the maximum thickness

[0132]七最大拱度的位置 [0132] The position of the seven largest camber

[0133] f 拱度 [0133] f camber

[0134] t 厚度 [0134] t Thickness

[0135] tmax截面外形的最大厚度 [0135] The maximum thickness tmax sectional shape

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
EP1845258A110 Apr 200617 Oct 2007Siemens AktiengesellschaftWind turbine rotor blade
WO2002/08600A1 Title not available
WO2002/38442A2 Title not available
WO2007/118581A1 Title not available
WO2008113349A213 Mar 200825 Sep 2008Vestas Wind Systems A/SSlow rotating wind turbine rotor with slender blades
Classifications
International ClassificationF03D1/06
Cooperative ClassificationF05B2240/301, Y02E10/721, F03D1/0641
Legal Events
DateCodeEventDescription
16 Nov 2011C06Publication
8 Feb 2012C10Request of examination as to substance
4 Jun 2014C14Granted