CN209228541U - Structure for Reducing Vortex-Induced Vibration of Fan Tower - Google Patents

Structure for Reducing Vortex-Induced Vibration of Fan Tower Download PDF

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CN209228541U
CN209228541U CN201822103626.1U CN201822103626U CN209228541U CN 209228541 U CN209228541 U CN 209228541U CN 201822103626 U CN201822103626 U CN 201822103626U CN 209228541 U CN209228541 U CN 209228541U
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tower
vortex
induced vibration
air
pipeline structure
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王宁
史伟涛
庞文彦
宋磊建
路绪恒
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Shanghai Electric Wind Power Group Co Ltd
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Shanghai Electric Wind Power Group Co Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/728Onshore wind turbines

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Abstract

本实用新型公开了一种降低风机塔筒涡激振动的结构,该结构可以是塔筒顶部单段整体或部分外围环绕一圈套筒结构,套筒结构包括用于减小涡激振动的尾部;套筒结构设置为柔性套筒结构,包饶在塔筒顶部外围,或者套筒结构设置为刚性套筒结构并包饶在塔筒顶部外围。另,该结构还可以是缠绕在塔筒顶部外周的螺旋管路结构,上风向设有集风口,下风向沿螺旋管路设置泄风口,集风口设置为风流入螺旋管路的入口,泄风口设置为风流出螺旋管路的出口。本实用新型依据涡振的产生机理和特点,改变筒壁流场分布,继而影响筒壁表面泄涡来避免或减轻涡激振动,为减小风压作用下的塔筒振动及避免共振现象发生。

The utility model discloses a structure for reducing vortex-induced vibration of a wind turbine tower. The structure can be a sleeve structure surrounded by a single section on the top of the tower as a whole or part of the periphery. The sleeve structure includes a tail for reducing vortex-induced vibration. ; The sleeve structure is set as a flexible sleeve structure and wraps around the top periphery of the tower, or the sleeve structure is set as a rigid sleeve structure and wraps around the top periphery of the tower. In addition, the structure can also be a spiral pipe structure wound on the outer circumference of the top of the tower. An air collection port is provided in the upwind direction, and an air discharge port is provided along the spiral pipe pipe in the downwind direction. Set as the outlet for the wind to flow out of the helical duct. According to the generation mechanism and characteristics of vortex vibration, the utility model changes the flow field distribution of the cylinder wall, and then affects the vortex discharge on the surface of the cylinder wall to avoid or reduce the vortex-induced vibration, in order to reduce the vibration of the tower under the action of wind pressure and avoid the resonance phenomenon .

Description

降低风机塔筒涡激振动的结构Structure for Reducing Vortex-Induced Vibration of Fan Tower

技术领域technical field

本实用新型涉及风力发电领域,特别涉及一种降低风机塔筒涡激振动的结构。The utility model relates to the field of wind power generation, in particular to a structure for reducing vortex-induced vibration of a wind turbine tower.

背景技术Background technique

近年来空气质量问题成为关乎环境与人类健康的重要问题,作为清洁可再生能源的风能,也越来越多地服务于人类生产和生活。风力发电装置有多种类型,主要为水平轴三叶轮发电机,这类发电机发电功率与叶轮直径大小成正相关关系,因此随着发电功率增大叶轮直径增加,加之高度越大风力越大,风力机高度不断提升。如图1所示,风力发电机主要由叶片、轮毂、机舱、塔筒、过渡部分及底部支撑结构组成。塔筒承担着为顶部结构提供有效支撑的作用。MW级风力机塔筒往往几十上百米,受制造、运输、吊装能力等多方面限制塔筒一般分段建造安装,单段长度20-30m左右,例如图1所示的01段、02段和03段,这里的01段塔筒指顶部单段或整个塔筒上段不超过1/2塔筒高度部分。In recent years, the problem of air quality has become an important issue related to the environment and human health. As a clean and renewable energy, wind energy is increasingly serving human production and life. There are many types of wind power generation devices, mainly horizontal-axis three-blade generators. The power generated by this type of generator is positively correlated with the diameter of the impeller. Therefore, the diameter of the impeller increases with the increase in power generation, and the greater the height, the greater the wind force. The height of wind turbines continues to increase. As shown in Figure 1, the wind turbine is mainly composed of blades, hub, nacelle, tower, transition part and bottom support structure. The tower bears the role of providing effective support for the top structure. MW-level wind turbine towers are often tens to hundreds of meters, limited by many aspects such as manufacturing, transportation, and hoisting capabilities. Towers are generally constructed and installed in sections, and the length of a single section is about 20-30m. For example, sections 01 and 02 shown in Figure 1 section and section 03, where the section 01 tower refers to the top single section or the upper section of the entire tower not exceeding 1/2 the height of the tower.

细长塔筒受风流场作用,流体受塔筒阻挡绕过塔筒继续流动,此时流场受塔筒干扰而改变,受构件尺度、形状、风速、粗糙度、空气粘性等影响流体离开构件时会有不同,在一定条件下会形成周期性不平衡风压作用,从而导致风机发生振动,即风机的涡激振动。当不平衡风压的周期与风机整体某阶固有周期接近时(通常为风机的一阶固有频率),风机的涡激振动会显著增强。涡激振动的发生将对风机运行的可靠性、安全性产生不利影响。随着风机塔架高度的增加,涡激振动已经成为行业内不可避免亟待解决的问题。The slender tower is affected by the wind flow field, and the fluid is blocked by the tower and continues to flow around the tower. At this time, the flow field is changed by the interference of the tower, and the fluid leaves the component due to the influence of the component size, shape, wind speed, roughness, and air viscosity. It will be different from time to time, and under certain conditions, it will form a periodic unbalanced wind pressure effect, which will cause the fan to vibrate, that is, the vortex-induced vibration of the fan. When the period of the unbalanced wind pressure is close to a certain order natural period of the fan as a whole (usually the first-order natural frequency of the fan), the vortex-induced vibration of the fan will be significantly enhanced. The occurrence of vortex-induced vibration will adversely affect the reliability and safety of fan operation. With the increase of wind tower height, vortex-induced vibration has become an inevitable and urgent problem in the industry.

涡振的作用机理及特点如下:The mechanism and characteristics of vortex vibration are as follows:

(1)当风流经塔筒时,会在结构的两侧产生不对称的旋涡脱落,使结构表面受到周期性正负压力,在一定风速下结构所受合力的频率与结构的自振频率一致,此时结构发生涡激振动。(1) When the wind flows through the tower, asymmetrical vortex shedding will occur on both sides of the structure, causing the surface of the structure to be subjected to periodic positive and negative pressures. The frequency of the resultant force on the structure is consistent with the natural frequency of the structure at a certain wind speed , the structure undergoes vortex induced vibration.

(2)涡激振动是一种简谐振动,其振动形式通常表现为横风向振动或扭转振动。结构振幅较大时,结构的运动对气体的绕流形态产生反馈作用,使旋涡脱落频率在一定风速围内和结构固有振动频率相等,即涡激共振的“锁定”现象。“锁定”会增加结构发涡激振动的机率,增强三维结构上的涡激力的相关性。涡激振动是一种限幅振动,对结构的质量和阻尼较为敏感,当结构质量和阻尼均较小时,涡激共振振幅可能很大。在锁定区内,涡脱频率不再服从Strouhal关系式,而是保持在结构固有频率值处。在锁定区,物体振幅可达到结构横风向尺寸的几分之一。(2) Vortex-induced vibration is a kind of simple harmonic vibration, and its vibration form usually manifests as cross-wind vibration or torsional vibration. When the amplitude of the structure is large, the movement of the structure will have a feedback effect on the flow around the gas, so that the frequency of vortex shedding is equal to the natural vibration frequency of the structure within a certain wind speed range, that is, the "locking" phenomenon of vortex induced resonance. "Locking" will increase the probability of vortex-induced vibration of the structure and enhance the correlation of vortex-induced force on the three-dimensional structure. The vortex-induced vibration is a kind of limiting vibration, which is sensitive to the mass and damping of the structure. When the structural mass and damping are small, the vortex-induced resonance amplitude may be large. In the locked region, the vortex shedding frequency no longer obeys the Strouhal relation, but remains at the value of the structural natural frequency. In the locked region, object amplitudes can reach a fraction of the across-wind dimension of the structure.

(3)圆柱涡激振动与Re关系;(3) The relationship between cylindrical vortex induced vibration and Re;

雷诺数Re表示惯性力与粘性力之间关系:Re=惯性力/粘性力=(ρ*U2/L)/(μ*U/L2)=ρ*U*L/μ=U*L/ν,式中,ρ:空气密度;U风速;L结构特征尺度;μ空气粘度;ν空气运动粘性系数=1.5*10-5m2/s;Reynolds number Re represents the relationship between inertial force and viscous force: Re=inertial force/viscous force=(ρ*U 2 /L)/(μ*U/L 2 )=ρ*U*L/μ=U*L /ν, where, ρ: air density; U wind speed; L structural characteristic scale; μ air viscosity; ν air kinematic viscosity coefficient = 1.5*10 -5 m 2 /s;

当Re<5:流动不分离;当5~15<Re<40:尾流出现一对稳定旋涡;当40<Re<3.0×102:旋涡从圆柱后方规则地交替脱落,形成卡门涡街;当3.0×102<Re<3.0×105:亚临界范围旋涡以一个明确的频率周期性地脱落;当3.0×105<Re<3.5×105:在临界范围旋涡被紊流所掩盖,涡脱杂乱无章;当3.5×105<Re:在超临界范围涡重新建立,涡脱重新出现周期性。所以,不同雷诺数情况下的绕流形态不同,因而其旋涡脱落的频率及作用在结构上的气动力也不同。When Re<5: the flow is not separated; when 5~15<Re<40: a pair of stable vortices appear in the wake; when 40<Re<3.0×10 2 : the vortices regularly fall off from the back of the cylinder to form a Karman vortex street; When 3.0×10 2 <Re<3.0×10 5 : the vortex in the subcritical range sheds periodically with a clear frequency; when 3.0×10 5 <Re<3.5×10 5 : the vortex in the critical range is covered by turbulent flow, The vortex shedding is disorderly; when 3.5×10 5 <Re: the vortex is re-established in the supercritical range, and the vortex shedding reappears periodically. Therefore, the shape of the flow around the different Reynolds numbers is different, so the frequency of vortex shedding and the aerodynamic force acting on the structure are also different.

(4)涡振产生条件:St=fv*D/U;式中,St:斯托罗哈数;U:风与塔筒相对速度;fv:涡脱频率;D:塔筒直径。(4) Vortex vibration generation condition: St=f v *D/U; where, St: Storohal number; U: relative velocity between wind and tower; f v : vortex shedding frequency; D: tower diameter.

(5)锁定风速条件:U=fv*D/St。(5) Locking wind speed condition: U=f v *D/St.

(6)涡激振特点:a、是一种一定风速区发生的有限振幅振动;b、只在某一风速区域内发生;c、最大振幅对结构阻尼有很大的依赖;d、断面形状的微小变化对响应很敏感;e、涡激振动可以激起弯曲振动,也可以激振扭转振动。(6) Vortex-induced vibration characteristics: a. It is a limited amplitude vibration that occurs in a certain wind speed area; b. It only occurs in a certain wind speed area; c. The maximum amplitude has a great dependence on structural damping; d. The cross-sectional shape The small change of is very sensitive to the response; e, vortex-induced vibration can excite bending vibration, and can also excite torsional vibration.

涡激振动作为一种周期性动载荷引起的结构振动现象,将对风机塔筒焊接点处的疲劳将产生不利影响。此外,在风机安装或停机等风机控制系统控制策略无法执行的状态下,风机涡激振动的发生将对风机的结构安全产生非常不利的影响。As a structural vibration phenomenon caused by periodic dynamic load, vortex-induced vibration will have an adverse effect on the fatigue of the welding points of the wind turbine tower. In addition, when the control strategy of the fan control system cannot be implemented, such as fan installation or shutdown, the occurrence of vortex-induced vibration of the fan will have a very adverse impact on the structural safety of the fan.

实用新型内容Utility model content

本实用新型的目的是提供一种降低风机塔筒涡激振动的结构,依据涡振产生机理和特点,改变筒壁流场分布,继而影响筒壁表面泄涡来避免或减轻涡激振动,为减小风压作用下的塔筒振动及避免共振现象发生。The purpose of this utility model is to provide a structure to reduce the vortex-induced vibration of the fan tower. According to the mechanism and characteristics of the vortex vibration, the distribution of the flow field on the wall of the tube is changed, and then the vortex discharge on the surface of the tube wall is affected to avoid or reduce the vortex-induced vibration. Reduce tower vibration under wind pressure and avoid resonance phenomenon.

为了达到上述目的,本实用新型一种降低风机塔筒涡激振动的螺旋管路结构,该螺旋管路结构缠绕在塔筒顶部外周,上风向设有集风口,下风向沿螺旋管路设置泄风口,所述集风口设置为风流入螺旋管路的入口,所述泄风口设置为风流出螺旋管路的出口。In order to achieve the above purpose, the utility model provides a spiral pipeline structure for reducing the vortex-induced vibration of the fan tower. The spiral pipeline structure is wound on the outer circumference of the top of the tower. The air outlet, the air collecting opening is set as the inlet of the wind flowing into the spiral pipeline, and the air outlet is set as the outlet of the wind flowing out of the spiral pipeline.

优选地,所述螺旋管路结构中,缠绕管直径范围为50mm至300mm。Preferably, in the spiral pipeline structure, the diameter of the winding tube is in the range of 50 mm to 300 mm.

优选地,所述螺旋管路结构中,导距尺寸设置为塔筒直径的4.5倍到5倍。Preferably, in the spiral pipeline structure, the lead distance is set to be 4.5 to 5 times the diameter of the tower.

优选地,所述螺旋管路结构中,螺距尺寸设置为导距尺寸的三分之一,以使该导距尺寸范围内并置三条缠绕管。Preferably, in the spiral pipeline structure, the pitch size is set to one-third of the lead pitch size, so that three winding pipes are juxtaposed within the lead pitch size range.

优选地,所述缠绕管底部设有用于限定该缠绕管位移的支撑滑槽。Preferably, the bottom of the winding pipe is provided with a support chute for limiting the displacement of the winding pipe.

优选地,所述泄风口小于所述述集风口。Preferably, the air discharge port is smaller than the air collection port.

优选地,所述集风口为喇叭口状。Preferably, the air collecting port is in the shape of a bell mouth.

优选地,所述集风口单独安装,或者与所述缠绕管制成一体。Preferably, the air collecting port is installed separately, or is integrated with the winding pipe.

优选地,所述泄风孔直接开设在集风口背面不大于120度范围之内,或者,所述泄风孔设置在缠绕管上下壁。Preferably, the air discharge hole is directly opened on the back of the air collecting port within a range of not more than 120 degrees, or the air discharge hole is provided on the upper and lower walls of the winding pipe.

优选地,所述泄风孔的直径小于缠绕管的直径,该泄风孔的孔距不小于泄风孔的直径,各个泄风孔的大小相等或者不相等。Preferably, the diameter of the air discharge holes is smaller than the diameter of the winding pipe, the distance between the air discharge holes is not smaller than the diameter of the air discharge holes, and the sizes of the air discharge holes are equal or unequal.

与现有技术相比,本实用新型的有益效果为:(1)本实用新型通过对塔筒顶部单段整体或部分外围环绕一圈套筒,该套筒具有一定尾部形状,可以改善尾部流场,从而减小涡振。套筒上下端设计有具体连接形式,可以使套筒自由滑动,并可以根据机翼理论在风力作用下自动变向,迎接来风。(2)本实用新型套筒可作为柔性包绕,由于流体粘性作用不宜过长,在风力作用下迎风向自动贴合塔筒,背风部分脱离塔筒表面而产生类似翼型的形状,避开紧背部低压区域,改善背部流场,从而减小涡振。(3)本实用新型对塔筒顶部单段外周缠绕螺旋管路,上风向设有集风口,下风向沿管路设置泄风口,以扰乱塔筒下风向的尾流,达到减小涡振目的。Compared with the prior art, the beneficial effects of the utility model are as follows: (1) The utility model surrounds a ring sleeve on the whole or part of the periphery of the top of the tower, and the sleeve has a certain shape of the tail, which can improve the tail flow. field, thereby reducing eddy vibration. The upper and lower ends of the sleeve are designed with a specific connection form, which allows the sleeve to slide freely, and can automatically change direction under the action of the wind according to the wing theory to welcome the incoming wind. (2) The sleeve of the utility model can be used as a flexible wrap. Due to the fluid viscosity, it should not be too long. Under the action of the wind, it will automatically fit the tower in the windward direction. Tight back low-pressure area improves back flow field, thereby reducing eddy vibration. (3) The utility model wraps a single-section outer circumference of a spiral pipeline on the top of the tower. An air collection port is provided in the upwind direction, and an air discharge port is provided along the pipeline in the downwind direction to disturb the wake flow in the downwind direction of the tower tube and reduce vortex vibration. .

附图说明Description of drawings

图1现有技术的塔筒及风力机整体示意图;The overall schematic diagram of the tower tube and wind turbine of Fig. 1 prior art;

图2本实用新型实施例一的塔筒顶段套筒结构示意图;Fig. 2 is a schematic diagram of the structure of the sleeve at the top of the tower in Embodiment 1 of the utility model;

图3本实用新型实施例一的塔筒顶段套筒连接方式示意图;Fig. 3 is a schematic diagram of the connection method of the sleeve at the top section of the tower tube in Embodiment 1 of the utility model;

图4本实用新型实施例一的塔筒顶段套筒的上部连接示意图;Fig. 4 is a schematic diagram of the upper connection of the sleeve at the top section of the tower in Embodiment 1 of the utility model;

图5本实用新型实施例一的塔筒顶段套筒的下部连接示意图;Fig. 5 is a schematic diagram of the connection of the lower part of the sleeve at the top section of the tower in Embodiment 1 of the utility model;

图6本实用新型实施例二的管路结构中上风向示意图;Fig. 6 is a schematic diagram of the upwind direction in the pipeline structure of the second embodiment of the utility model;

图7本实用新型实施例二的管路结构中侧向示意图;Fig. 7 is a lateral schematic diagram of the pipeline structure of Embodiment 2 of the utility model;

图7a本实用新型图7对应的A局部侧向视图;Fig. 7a is a partial side view of A corresponding to Fig. 7 of the present utility model;

图8本实用新型实施例二的管路结构中下风向示意图;Fig. 8 is a schematic diagram of the downwind direction in the pipeline structure of the second embodiment of the utility model;

图8a本实用新型实图8对应的B局部正向视图;Fig. 8a is a partial front view of B corresponding to Fig. 8 of the utility model;

图9本实用新型实施例二的螺距及导程示意图。Fig. 9 is a schematic diagram of the pitch and lead of the second embodiment of the utility model.

具体实施方式Detailed ways

本实用新型公开了一种降低风机塔筒涡激振动的结构,为了使本实用新更加明显易懂,以下结合附图和具体实施方式对本实用新型做进一步说明。The utility model discloses a structure for reducing vortex-induced vibration of a fan tower. In order to make the utility model more obvious and easy to understand, the utility model will be further described below in conjunction with the accompanying drawings and specific implementation methods.

实施例一:Embodiment one:

如图2所示,本实用新型的降低风机塔筒涡激振动的结构设计方法是在塔筒顶部单段整体或部分外围环绕一圈套筒205,该套筒205具有一定尾部形状,可以改善尾部流场,从而减小涡振。套筒上下端设计有具体连接形式,可以使套筒自由滑动,并可以根据机翼理论在风力作用下自动变向,迎接来风。As shown in Figure 2, the structural design method of the utility model for reducing the vortex-induced vibration of the fan tower is to surround a ring of sleeve 205 on the whole or part of the periphery of the top of the tower. The sleeve 205 has a certain tail shape, which can improve Tail flow field, thereby reducing vortex vibration. The upper and lower ends of the sleeve are designed with a specific connection form, which allows the sleeve to slide freely, and can automatically change direction under the action of the wind according to the wing theory to welcome the incoming wind.

套筒可作为柔性包绕(即类似厚牛皮纸等具有一定柔韧度材料),由于流体粘性作用不宜过长,在风力作用下迎风向自动贴合塔筒,背风部分脱离塔筒表面而产生类似翼型的形状,避开紧背部低压区域,改善背部流场,从而减小涡振。The sleeve can be used as a flexible wrap (that is, similar to thick kraft paper and other materials with a certain degree of flexibility). Due to the fluid viscosity, it should not be too long. The shape of the model avoids the low-pressure area at the tight back, improves the flow field at the back, and reduces eddy vibration.

本实施例中,柔性包绕层周长大于其对应包绕部位塔筒周长,而任意挤压形状后其最大纵向延伸长度应小于(1+D)m以保证其任意情况下不与叶轮产生干涉,其中D为塔筒最大直径。包绕层是具有特定柔性韧性的材料,上下端可通过顶段塔筒的上下法兰直接固定。In this embodiment, the perimeter of the flexible wrapping layer is greater than the perimeter of the corresponding wrapping part of the tower, and its maximum longitudinal extension after any extrusion shape should be less than (1+D)m to ensure that it does not interfere with the impeller under any circumstances. Interference occurs, where D is the maximum diameter of the tower. The wrapping layer is a material with specific flexibility and toughness, and the upper and lower ends can be directly fixed by the upper and lower flanges of the top tower.

刚性套筒形式如图2所示,套筒包绕在塔筒顶段的外周。上风向端呈环状,尽量贴近而不接触塔筒筒壁,依据施工精度及材料刚度等条件确定合适的间隔距离。下风向端设有一定翼型或直接棱柱处理。该套筒在高度方向上,任意截面表现为有翼型的剖面形状或圆周与三角形组合。The form of the rigid sleeve is shown in Figure 2, and the sleeve is wrapped around the outer circumference of the top section of the tower. The upwind end is ring-shaped, as close as possible without touching the tower wall, and the appropriate spacing distance is determined according to conditions such as construction accuracy and material stiffness. The downwind end is provided with a certain airfoil or direct prism treatment. In the height direction, any section of the sleeve is shown as an airfoil section shape or a combination of a circle and a triangle.

套筒在周向上最大投影长度应保证不与叶片产生干涉并留有一定安全距离。最大套筒可整体包绕也可分段包绕。刚性套筒的上下端采用一定结构进行固定,该结构可保证刚性套筒可以在风压作用下自由转动以自动对正风向。The maximum projected length of the sleeve in the circumferential direction should ensure that there is no interference with the blade and a certain safety distance should be left. The largest sleeve can be wrapped as a whole or in sections. The upper and lower ends of the rigid sleeve are fixed with a certain structure, which can ensure that the rigid sleeve can rotate freely under the action of wind pressure to automatically align with the wind direction.

(1)套筒端部连接方式一,具体如下:(1) Connection method 1 at the end of the sleeve, as follows:

本实施例中,可采用如图3所示形式固定套筒上下端。In this embodiment, the upper and lower ends of the sleeve can be fixed as shown in FIG. 3 .

如图2和图3结合所示,201为塔筒外壁,202为塔筒连接和外伸部分,203为连接器滑轨部分,205为套筒,206为套筒端部连接段。2 and 3, 201 is the outer wall of the tower, 202 is the connection and extension part of the tower, 203 is the connector slide rail part, 205 is the sleeve, and 206 is the connecting section at the end of the sleeve.

连接器滑轨部分203属于塔筒外伸部分,通过塔筒连接和外伸部分202与塔筒外壁201紧固。连接器滑轨部分203形状可以是球形,也可为其他形状突起。The connector slide rail part 203 belongs to the tower extension part, and is fastened to the tower outer wall 201 through the tower connection and the extension part 202 . The shape of the connector slide rail portion 203 can be spherical, or protruding in other shapes.

本实施例中,塔筒连接和外伸部分202及连接器滑轨部分203环绕塔筒一周形成连续轨道,保证套筒205可以在风压作用下通过滑轨结构自由滑动。具体地,塔筒连接和外伸部分202和连接器滑轨部分203共同构成滑轨,二者通过焊接连接或可制造成一体铸造件。该滑轨通过塔筒连接和外伸部分202与塔筒外壁201焊接,通过连接器滑轨部分203外表面与套筒端部连接段206组成滑道。滑轨仅设置于套筒顶部及底部,顶部及底部的结构形式相同,滑轨位置如图2中的P点所示。In this embodiment, the tower connection and extension part 202 and the connector slide rail part 203 form a continuous track around the tower to ensure that the sleeve 205 can slide freely through the slide rail structure under the action of wind pressure. Specifically, the tower connecting and overhanging portion 202 and the connector sliding rail portion 203 jointly constitute a sliding rail, and the two are connected by welding or can be manufactured as an integral casting. The slide rail is welded to the tower outer wall 201 through the tower connection and the overhanging part 202 , and forms a slideway through the outer surface of the connector slide rail part 203 and the sleeve end connection section 206 . The slide rails are only set on the top and bottom of the sleeve, and the top and bottom have the same structure. The position of the slide rails is shown at point P in Figure 2.

套筒端部连接段206作为套筒连接件可以连续,也可仅沿圆周相对均匀地布置几块,起到有效连接和支撑套筒205重量作用即可。The connecting section 206 at the end of the sleeve can be continuous as the connecting part of the sleeve, or only a few pieces can be arranged relatively evenly along the circumference, so as to effectively connect and support the weight of the sleeve 205 .

套筒和塔筒交接处部分204为连接器滑轨部分203和套筒端部连接段206的接触面,该套筒和塔筒交接处部分204设置为光滑接触,保证套筒和塔筒两者光滑接触。此时,对接触面处加润滑减小接触面间摩擦,保障套筒205通过套筒端部连接段206(即连接件)沿滑道的顺畅滑动,保证套筒205在风力作用下能上风向(圆头部分)迎风,下风向(尖角部分)背风位于尾流区。另,套筒和塔筒交接处部分204也可作磁性连接,使二者不必接触,通过磁极相斥性减小接触面间摩擦,即利用重力和磁场斥力保证滑轨的自由滑动和可靠连接。The junction part 204 of the sleeve and the tower is the contact surface of the connector slide rail part 203 and the connecting section 206 at the end of the sleeve. or smooth contact. At this time, lubricate the contact surface to reduce the friction between the contact surfaces, ensure the smooth sliding of the sleeve 205 along the slideway through the connecting section 206 (ie the connector) at the end of the sleeve, and ensure that the sleeve 205 can go up under the action of wind force. The wind direction (round head part) is upwind, and the leeward direction (sharp part) is located in the wake area. In addition, the junction part 204 of the sleeve and the tower can also be used as a magnetic connection, so that the two do not need to be in contact, and the friction between the contact surfaces is reduced through the repulsion of the magnetic poles, that is, the free sliding and reliable connection of the slide rail are ensured by using gravity and magnetic repulsion. .

本实施例中,应当尽可能减少摩擦阻力及对材料的磨损,可通过一定材料、加工工艺、结构优化等作不断优化改良。In this embodiment, frictional resistance and wear on materials should be reduced as much as possible, and continuous optimization and improvement can be carried out through certain materials, processing techniques, and structural optimization.

(2)套筒端部连接方式二:(2) Sleeve end connection method two:

本实用新型的滑轨可以做磁性导轨,使滑轨摩擦降到最低。如图4和图5所示,此为另一种滑轨设计方法,用于套筒与塔筒的连接,但本实用新型并不限于此截面结构形式。The slide rail of the utility model can be used as a magnetic guide rail to minimize the friction of the slide rail. As shown in Figure 4 and Figure 5, this is another slide rail design method for the connection between the sleeve and the tower, but the utility model is not limited to this cross-sectional structure.

如图4所示的顶端连接处,211为套筒;210为套筒顶端部,用于与滑轨配合的结构;212为滑轨,一端与塔筒连接,另一端为滑轨轨道,底部通过加强件215(扁铁)支撑加强;213为塔筒外壁。211 is the sleeve at the top connection shown in Figure 4; 210 is the top end of the sleeve, which is used to cooperate with the slide rail; 212 is the slide rail, one end is connected with the tower, the other end is the slide rail track, and the bottom It is supported and strengthened by reinforcing member 215 (flat iron); 213 is the outer wall of the tower tube.

滑轨212的轨道凹槽与套筒顶端部210配合的三个表面做成磁力面,即套筒顶端部210与滑轨212接触的内外两个表面及下部端面设为磁力面,并沿塔筒周向连续一周。The track groove of the slide rail 212 and the three surfaces matched with the top end of the sleeve 210 are made into magnetic surfaces, that is, the inner and outer surfaces and the lower end surface of the top end of the sleeve 210 in contact with the slide rail 212 are set as magnetic force surfaces, and along the tower The circumference of the barrel is continuous for one week.

套筒底端部209与套筒顶端部210结构相同。同理,滑轨214的轨道凹槽与套筒底端部209配合的三个表面做成磁力面,即套筒底端部209与滑轨214接触的内外两个表面及上部端面设为磁力面。本实施例中的套筒底部的三个磁力面与套筒顶部的三个磁力面组成三对磁力斥力面,则上下两套导轨与套筒上下端面配合后组成如图4和图5所示的三组斥力:力1与力1’、力2与力2’、力3与力3’。The sleeve bottom end 209 is of the same structure as the sleeve top end 210 . In the same way, the three surfaces where the track groove of the slide rail 214 cooperates with the sleeve bottom end 209 are made into magnetic force surfaces, that is, the inner and outer surfaces and the upper end surface of the sleeve bottom end 209 in contact with the slide rail 214 are set as magnetic force surfaces. noodle. In this embodiment, the three magnetic surfaces at the bottom of the sleeve and the three magnetic surfaces at the top of the sleeve form three pairs of magnetic repulsion surfaces, and then the upper and lower sets of guide rails cooperate with the upper and lower end surfaces of the sleeve to form a composition as shown in Figure 4 and Figure 5 Three groups of repulsive forces: force 1 and force 1', force 2 and force 2', force 3 and force 3'.

其中,力1与力1’组成大小相等方向相反的一对水平方向平衡的斥力;力2与力2’组成大小相等方向相反的一对水平方向平衡斥力。由于磁体间相对距离越近斥力越大,当力1斥力面间距减小时,斥力会使其距离增大,而当力1’斥力面间距减小时同样的,力1’接触面的斥力又会作用更大斥力使其距离增大,最终达到套筒顶端部210两侧距滑轨有一个相对平衡的位置,并始终保持间隙,避免摩擦。Among them, force 1 and force 1' constitute a pair of horizontally balanced repulsive forces of equal magnitude and opposite directions; force 2 and force 2' constitute a pair of horizontally balanced repulsive forces of equal magnitude and opposite directions. Since the closer the relative distance between the magnets, the greater the repulsive force, when the distance between the repulsive force surfaces of force 1 decreases, the repulsive force will increase the distance, and when the distance between the repulsive force surfaces of force 1' decreases, the repulsive force of the contact surface of force 1' will increase The greater the repulsive force, the greater the distance, finally reaching a relatively balanced position between the two sides of the top end of the sleeve 210 and the slide rail, and a gap is always maintained to avoid friction.

力3与力3’为垂直方向一对平衡斥力,但由于重力要大于磁力作用,力3所在的一对接触面往往需要将特殊处理,增加润滑、打磨圆角、或者有条件的话增加力3表面斥力使其大小可平衡重力与力3’面的二力之和,保持整个滑轨在风力作用下可以无摩擦地相对滑动。Force 3 and force 3' are a pair of balanced repulsive forces in the vertical direction, but since gravity is greater than the magnetic force, the pair of contact surfaces where force 3 is located often needs to be specially treated, adding lubrication, grinding rounded corners, or increasing force 3 if conditions permit The surface repulsion force can balance the sum of the two forces of the gravity and the force 3' surface, so that the whole slide rail can slide relative to each other without friction under the action of wind force.

如图3和图4所示,215、216分别为上、下轨道结构支撑加强构件,沿塔筒周向可连续焊接一圈可间断地沿塔筒外周均布。As shown in Fig. 3 and Fig. 4, 215 and 216 are respectively upper and lower rail structure support reinforcement members, which can be continuously welded in one circle along the circumference of the tower and distributed evenly along the outer circumference of the tower intermittently.

综上所述,本实施例一的以上的两种套筒端部连接形式(即图3和图4、5所示)中,轨道设置为沿塔筒一周的环形结构(第一种形式通过塔筒连接和外伸部分202实现;第二种形式中,顶部通过滑轨212和上轨道结构支撑加强构件215一端实现,底部通过轨道214、下轨道结构支撑加强构件216一端实现)可直接与塔筒焊接连接或利用塔筒本身锥度在套筒自重作用下进行紧密套接,或局部点焊连接;也可再优化接触位置结构进行连接。To sum up, in the above two sleeve end connection forms of the first embodiment (as shown in Fig. 3 and Fig. 4, 5), the track is arranged as a circular structure along the circumference of the tower (the first form passes through The tower connection and the overhanging part 202 are realized; in the second form, the top is realized by the slide rail 212 and one end of the upper rail structural support reinforcement member 215, and the bottom is realized by the track 214 and one end of the lower rail structural support reinforcement member 216) can be directly connected with the tower Tube welded connection or use the taper of the tower itself to tightly socket under the action of the sleeve's own weight, or local spot welding connection; it can also be connected by optimizing the contact position structure.

实施例二:Embodiment two:

如图6、图7和图8结合所示,本实施例二中,对塔筒顶部单段外周缠绕螺旋管路,上风向设有集风口,下风向沿管路设置泄风口,以扰乱塔筒下风向的尾流,达到减小涡振目的。As shown in Fig. 6, Fig. 7 and Fig. 8, in the second embodiment, a spiral pipe is wound around the outer circumference of a single section on the top of the tower, and an air collection port is provided in the upwind direction, and an air discharge port is provided along the pipe in the downwind direction to disturb the tower. The wake flow in the downwind direction of the tube can reduce the vortex vibration.

其中,集风口为风流入螺旋管路的入口,应具有大开口形式便于更多气体流入螺旋管内。泄风口为风流出螺旋管路的出口,应较集风口小,以使气流具有较尾流更大流速冲出螺旋管。Among them, the air collecting port is the entrance for wind to flow into the spiral pipe, and should have a large opening to facilitate more air to flow into the spiral pipe. The air discharge port is the outlet for the wind to flow out of the spiral pipe, and should be smaller than the air collection port, so that the air flow has a greater flow rate than the wake to rush out of the spiral pipe.

上述为伯努利方程的一种应用,则根据伯努利方程:The above is an application of the Bernoulli equation, according to the Bernoulli equation:

式中,p为流体中某点压强;v为该点流体流动速度;ρ为流体密度;g为重力加速度;z为该点所在高度;C为一常数。In the formula, p is the pressure of a certain point in the fluid; v is the fluid flow velocity at this point; ρ is the fluid density; g is the acceleration of gravity; z is the height of the point; C is a constant.

基于上述并以最底部一对出入口为例并假定入口在出口之上,可得:Based on the above and taking the bottom pair of entrances and exits as an example and assuming that the entrance is above the exit, it can be obtained:

式中,νin为流体在入口某处的速度;pin为流体入口处压强;ρ为流体密度;g为重力加速度;zin为入口处所在高度;νout为流体在出口某处的速度;pout为流体入口处压强;zout出口处所在高度。In the formula, ν in is the velocity of the fluid at a certain place at the inlet; p in is the pressure at the fluid inlet; ρ is the density of the fluid; g is the acceleration of gravity; z in is the height of the inlet; ν out is the velocity of the fluid at a certain place at the outlet ; p out is the pressure at the fluid inlet; z out is the height of the outlet.

由于风具有粘性,在沿筒壁流动时在塔筒表面形成一边界层,且在与入流成一定夹角位置处边界层分离造成紊流及塔筒背面的粘涡,因此塔筒背风面压力迅速降低,即pin>pout。且对于流体而言向上流动时势能增加动能不足,因此更多风将更容易向低处流动,因此将上部集风口与下部临近泄风口看作一对出入口有Zin>Zout,因此vout>vin冲出气体速度更大可对尾流进行扰动,破坏原始流场。Due to the viscosity of the wind, a boundary layer is formed on the surface of the tower when it flows along the wall of the tower, and the separation of the boundary layer at a position at a certain angle with the inflow causes turbulence and sticky vortices on the back of the tower, so the pressure on the leeward side of the tower Decrease rapidly, that is, p in > p out . And for the fluid, the potential energy increases and the kinetic energy is insufficient when it flows upwards, so more wind will flow to the lower place more easily, so the upper air collection port and the lower adjacent air discharge port are regarded as a pair of inlets and outlets, Z in > Z out , so v out >v in The greater velocity of the gas rushing out can disturb the wake and destroy the original flow field.

本实施例二的具体设计方法如下:The concrete design method of present embodiment two is as follows:

螺旋管路的缠绕管直径50-300mm区间选取。The winding pipe diameter of the spiral pipeline is selected from the range of 50-300mm.

如图9所示,螺旋管路中,导距hw尺寸大小约为塔筒直径的4.5到5倍,导距hw尺寸范围内可并置三条缠绕管,则螺距lw为导距hw的三分之一。As shown in Figure 9, in the spiral pipeline, the size of the lead hw is about 4.5 to 5 times the diameter of the tower, and three winding pipes can be juxtaposed within the size range of the lead hw, so the screw pitch lw is one-third of the lead hw one.

本实施例二中,可使用轻型材料降低重力,管壁与筒壁间有小间距也可采取一定方式做耐磨处理。缠绕管顶部可与顶部机舱相连随叶轮转动而转动,从而使得集风口始终处于上风向,泄风口处于下风向。缠绕管底部可设置支撑滑槽,限定其位移。In the second embodiment, light materials can be used to reduce the gravity, and there is a small distance between the pipe wall and the cylinder wall, and a certain method can also be used for wear-resistant treatment. The top of the winding pipe can be connected with the top cabin and rotate with the rotation of the impeller, so that the air collecting port is always in the upwind direction, and the air discharge port is in the downwind direction. A support chute can be provided at the bottom of the winding pipe to limit its displacement.

集风口主要特点为喇叭口状,喇叭开口大向连接处逐渐缩小,该喇叭口具体形式可多种,(图7a所示为其中一种)。喇叭口内可设置更有效的集风装置,如叶轮,使射入风更有效流入缠绕管。另,集风口可单独安装,也可与缠绕管做成一体。The main characteristic of the air collecting port is the shape of a bell mouth, and the opening of the bell gradually narrows toward the connection. A more effective air collection device, such as an impeller, can be arranged in the bell mouth, so that the injected wind can flow into the winding pipe more effectively. In addition, the air collecting port can be installed separately or integrated with the winding tube.

如图8a所示,泄风孔可直接开于集风口背面不大于120度范围之内,泄风孔直径小于缠绕管直径,泄风孔孔距不小于泄风孔孔直径距离。泄风孔个数不宜过多,大小可相等或者不必相等,也可在缠绕管上下壁设置泄风孔。As shown in Figure 8a, the vent hole can be directly opened within a range of not more than 120 degrees on the back of the air collecting port, the diameter of the vent hole is smaller than the diameter of the winding pipe, and the distance between the vent holes is not less than the diameter of the vent hole. The number of vent holes should not be too many, and the size can be equal or not necessarily equal, and vent holes can also be set on the upper and lower walls of the winding pipe.

尽管本实用新型的内容已经通过上述优选实施例作了详细介绍,但应当认识到上述的描述不应被认为是对本实用新型的限制。在本领域技术人员阅读了上述内容后,对于本实用新型的多种修改和替代都将是显而易见的。因此,本实用新型的保护范围应由所附的权利要求来限定。Although the content of the present invention has been described in detail through the above preferred embodiments, it should be recognized that the above description should not be considered as a limitation of the present invention. Various modifications and substitutions of the present utility model will be obvious to those skilled in the art after reading the above content. Therefore, the protection scope of the present utility model should be defined by the appended claims.

Claims (10)

1.一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,该螺旋管路结构缠绕在塔筒顶部外周,上风向设有集风口,下风向沿所述螺旋管路设置泄风口,所述集风口设置为风流入所述螺旋管路的入口,所述泄风口设置为风流出所述螺旋管路的出口。1. A spiral pipeline structure for reducing vortex-induced vibration of a wind turbine tower, characterized in that the spiral pipeline structure is wound around the outer circumference of the tower top, the upwind direction is provided with an air collection port, and the downwind direction is provided with a discharge outlet along the spiral pipeline. A tuyere, the air collecting opening is set as an inlet for wind to flow into the spiral pipeline, and the air outlet is set as an outlet for wind to flow out of the spiral pipeline. 2.如权利要求1所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,2. A kind of helical pipeline structure that reduces the vortex-induced vibration of the fan tower as claimed in claim 1, characterized in that, 所述螺旋管路结构中,缠绕管直径范围为50mm至300mm。In the spiral pipeline structure, the diameter of the coiled pipe ranges from 50mm to 300mm. 3.如权利要求1或2所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,3. A kind of spiral pipeline structure that reduces the vortex-induced vibration of fan tower as claimed in claim 1 or 2, is characterized in that, 所述螺旋管路结构中,导距(hw)尺寸设置为塔筒直径的4.5倍至5倍。In the spiral pipeline structure, the guide distance (hw) is set to be 4.5 to 5 times the diameter of the tower. 4.如权利要求3所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,4. A kind of helical pipeline structure that reduces the vortex-induced vibration of the fan tower as claimed in claim 3, characterized in that, 所述螺旋管路结构中,螺距(lw)尺寸设置为导距(hw)尺寸的三分之一,以使该导距(hw)尺寸范围内并置三条缠绕管。In the spiral pipeline structure, the pitch (lw) is set to be one-third of the size of the lead (hw), so that three winding pipes are juxtaposed within the size range of the lead (hw). 5.如权利要求2所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,5. A kind of helical pipeline structure that reduces the vortex-induced vibration of the fan tower as claimed in claim 2, characterized in that, 所述缠绕管底部设有用于限定该缠绕管位移的支撑滑槽。A supporting chute for limiting the displacement of the winding pipe is provided at the bottom of the winding pipe. 6.如权利要求1所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,6. A spiral pipeline structure for reducing vortex-induced vibration of a wind turbine tower as claimed in claim 1, characterized in that, 所述泄风口小于所述述集风口。The air discharge port is smaller than the air collection port. 7.如权利要求1或6所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,7. A kind of spiral piping structure for reducing vortex-induced vibration of fan tower as claimed in claim 1 or 6, characterized in that, 所述集风口为喇叭口状。The air collecting port is bell-shaped. 8.如权利要求2所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,8. A kind of helical pipeline structure that reduces the vortex-induced vibration of the fan tower as claimed in claim 2, characterized in that, 所述集风口单独安装,或者与所述缠绕管制成一体。The air collecting port is installed separately, or is integrated with the winding pipe. 9.如权利要求2所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,9. A spiral piping structure for reducing vortex-induced vibration of a wind turbine tower as claimed in claim 2, characterized in that, 所述泄风口直接开设在集风口背面设定范围之内,或者,所述泄风口设置在缠绕管上下壁。The air discharge port is directly set within the setting range on the back of the air collection port, or the air discharge port is arranged on the upper and lower walls of the winding pipe. 10.如权利要求2或9所述的一种降低风机塔筒涡激振动的螺旋管路结构,其特征在于,10. A spiral pipeline structure for reducing vortex-induced vibration of a wind turbine tower as claimed in claim 2 or 9, characterized in that, 所述泄风口的直径小于所述缠绕管的直径,该泄风口的孔距不小于所述泄风口的直径,各所述泄风口的大小相等或者不相等。The diameter of the air outlet is smaller than the diameter of the winding pipe, the hole distance of the air outlet is not smaller than the diameter of the air outlet, and the sizes of the air outlets are equal or unequal.
CN201822103626.1U 2018-12-14 2018-12-14 Structure for Reducing Vortex-Induced Vibration of Fan Tower Expired - Fee Related CN209228541U (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110735767A (en) * 2019-09-18 2020-01-31 浙江运达风电股份有限公司 flexible tower wind-induced vibration flow disturbing device of retractable wind generating set
CN113074086A (en) * 2020-01-06 2021-07-06 周英 Induced air type power generation device and method
CN113819009A (en) * 2021-09-28 2021-12-21 中国华能集团清洁能源技术研究院有限公司 Passive turbulence device, wind turbine generator and passive turbulence method
CN114033634A (en) * 2021-11-22 2022-02-11 南通河海大学海洋与近海工程研究院 A device for suppressing vortex-induced resonance of a wind turbine
CN116025521A (en) * 2023-01-17 2023-04-28 西安交通大学 Wind turbine tower and preparation method thereof

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110735767A (en) * 2019-09-18 2020-01-31 浙江运达风电股份有限公司 flexible tower wind-induced vibration flow disturbing device of retractable wind generating set
CN113074086A (en) * 2020-01-06 2021-07-06 周英 Induced air type power generation device and method
CN113819009A (en) * 2021-09-28 2021-12-21 中国华能集团清洁能源技术研究院有限公司 Passive turbulence device, wind turbine generator and passive turbulence method
CN113819009B (en) * 2021-09-28 2023-03-07 中国华能集团清洁能源技术研究院有限公司 passive spoiler method
CN114033634A (en) * 2021-11-22 2022-02-11 南通河海大学海洋与近海工程研究院 A device for suppressing vortex-induced resonance of a wind turbine
CN114033634B (en) * 2021-11-22 2024-04-09 南通河海大学海洋与近海工程研究院 Device for inhibiting vortex-induced resonance of wind turbine
CN116025521A (en) * 2023-01-17 2023-04-28 西安交通大学 Wind turbine tower and preparation method thereof

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