CN221705031U - In-service wind power blade wind speed measurement sensor mounting structure - Google Patents
In-service wind power blade wind speed measurement sensor mounting structure Download PDFInfo
- Publication number
- CN221705031U CN221705031U CN202420320451.2U CN202420320451U CN221705031U CN 221705031 U CN221705031 U CN 221705031U CN 202420320451 U CN202420320451 U CN 202420320451U CN 221705031 U CN221705031 U CN 221705031U
- Authority
- CN
- China
- Prior art keywords
- wind speed
- damping
- bearing plate
- measurement sensor
- box body
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000005259 measurement Methods 0.000 title claims abstract description 33
- 230000007246 mechanism Effects 0.000 claims abstract description 50
- 230000004224 protection Effects 0.000 claims abstract description 3
- 238000013016 damping Methods 0.000 claims abstract 21
- 230000035939 shock Effects 0.000 claims description 25
- 238000010521 absorption reaction Methods 0.000 claims 2
- 238000009413 insulation Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 238000009434 installation Methods 0.000 description 12
- 238000001514 detection method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000002955 isolation Methods 0.000 description 3
- 230000009979 protective mechanism Effects 0.000 description 3
- 101001121408 Homo sapiens L-amino-acid oxidase Proteins 0.000 description 2
- 102100026388 L-amino-acid oxidase Human genes 0.000 description 2
- 101100012902 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) FIG2 gene Proteins 0.000 description 2
- 101100233916 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) KAR5 gene Proteins 0.000 description 1
- 239000000443 aerosol Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Wind Motors (AREA)
Abstract
Description
技术领域Technical Field
本实用新型涉及风力发电机领域,具体是一种在役风电叶片风速测量传感器安装结构。The utility model relates to the field of wind turbines, in particular to an installation structure for a wind speed measuring sensor of an in-service wind turbine blade.
背景技术Background Art
风力发电机是将风能转换为机械能,机械能转换为电能的电力设备。风电机组基本结构包括底座基础、塔筒、机舱和叶轮等。目前的风速测量设备普遍安装在风机机舱上方或风电场内架设的测风塔上。Wind turbines are electrical equipment that convert wind energy into mechanical energy and mechanical energy into electrical energy. The basic structure of a wind turbine includes a base foundation, a tower, a nacelle, and an impeller. Currently, wind speed measurement equipment is generally installed above the wind turbine nacelle or on a wind tower erected in a wind farm.
激光测风雷达是用来测量高空风向、风速的雷达。激光雷达测风作为新型的移动测风技术,利用激光的多普勒频移原理,通过测量光波反射在空气中遇到风运动的气溶胶粒子所产生的频率变化得到风速、风向信息,从而计算出相应高度的矢量风速和风向数据。在复杂地形区域,测风塔代表性难以满足风资源评估要求,仅通过测风塔数据模拟得到的结果存在很大差异。而通过激光雷达在风险区域实地测量,结合现有测量结果和软件模拟对比,将有效识别风险区域的真实性,规避潜在风险。Laser wind radar is a radar used to measure high-altitude wind direction and wind speed. As a new type of mobile wind measurement technology, laser radar wind measurement uses the Doppler frequency shift principle of laser to obtain wind speed and direction information by measuring the frequency change caused by the reflection of light waves in the air and aerosol particles moving in the wind, thereby calculating the vector wind speed and direction data at the corresponding height. In complex terrain areas, the representativeness of wind towers is difficult to meet the requirements of wind resource assessment, and the results obtained by simulating wind tower data alone are very different. Through on-site measurements of laser radar in risk areas, combined with existing measurement results and software simulation comparisons, the authenticity of risk areas will be effectively identified and potential risks will be avoided.
CN 218512640 U公开一种测量不同高度风场的机舱式激光测风雷达,其包括机舱式测风激光雷达主体及载板、电机、转动杆、连接座等构件,使得整个机舱式激光测风雷达探测头的测量方向发生变化,从而对不同水平方向的风场进行测量,在机舱式激光测风雷达的底端安装支撑机构,不但能够在电机驱动旋转的同时,始终支撑机舱式激光测风雷达,还能够启动气缸通过升降杆推动机舱式激光测风雷达一端升降,机舱式激光测风雷达另一端保持高度不变,从而调整了机舱式激光测风雷达探测头的测量高度。目前的激光测风雷达是固定设置在风力发电机机舱顶部的,由于风力发电机大多安装在风力大的地方,因而上述现有技术虽然能够实现机舱式激光测风雷达探测头的测量高度的灵活调整,但设备稳固性方面有待提高。CN 218512640 U discloses a nacelle-type laser wind measuring radar for measuring wind fields at different heights, which includes a nacelle-type laser wind measuring radar body and a carrier plate, a motor, a rotating rod, a connecting seat and other components, so that the measuring direction of the entire nacelle-type laser wind measuring radar detection head changes, thereby measuring wind fields in different horizontal directions. A supporting mechanism is installed at the bottom end of the nacelle-type laser wind measuring radar, which can not only always support the nacelle-type laser wind measuring radar while the motor drives the rotation, but also start the cylinder to push one end of the nacelle-type laser wind measuring radar to rise and fall through the lifting rod, and the other end of the nacelle-type laser wind measuring radar keeps the height unchanged, thereby adjusting the measuring height of the nacelle-type laser wind measuring radar detection head. The current laser wind measuring radar is fixedly arranged on the top of the wind turbine nacelle. Since most wind turbines are installed in places with strong wind, although the above-mentioned prior art can realize the flexible adjustment of the measuring height of the nacelle-type laser wind measuring radar detection head, the stability of the equipment needs to be improved.
发明内容Summary of the invention
本实用新型所要解决的技术问题在于针对现有技术存在的上述不足之处,提供一种在役风电叶片风速测量传感器安装结构,用以提高测风设备的安装稳固性,同时实现测风设备高度及水平角度的调节。The technical problem to be solved by the utility model is to provide a wind speed measurement sensor installation structure for in-service wind turbine blades in view of the above-mentioned deficiencies in the prior art, so as to improve the installation stability of the wind measuring equipment and realize the adjustment of the height and horizontal angle of the wind measuring equipment.
为了实现上述目的,本实用新型采用的技术方案是一种在役风电叶片风速测量传感器安装结构,包括:In order to achieve the above-mentioned purpose, the technical solution adopted by the utility model is an installation structure of a wind speed measurement sensor for an in-service wind turbine blade, comprising:
支撑机构,所述支撑机构包括固定支座、调节支座,固定支座中部开设有多个定位孔,固定支座与调节支座之间设有用于带动调节支座进行位置调节的若干个伺服电动缸,伺服电动缸倾斜设置,伺服电动缸上端和下端分别通过虎克铰与调节支座、固定支座铰接;The supporting mechanism comprises a fixed support and an adjustable support, a plurality of positioning holes are opened in the middle of the fixed support, a plurality of servo electric cylinders are arranged between the fixed support and the adjustable support for driving the adjustable support to adjust the position, the servo electric cylinders are arranged obliquely, and the upper and lower ends of the servo electric cylinders are respectively hinged to the adjustable support and the fixed support through a Hook hinge;
减震机构,所述减震机构包括用于安装风速测量传感器主体的减震承载箱,减震承载箱底部安装于调节支座上;A shock absorbing mechanism, wherein the shock absorbing mechanism comprises a shock absorbing bearing box for mounting the wind speed measurement sensor body, and the bottom of the shock absorbing bearing box is mounted on the adjustment support;
防护机构,所述防护机构包括半椭球形的护罩,护罩固定于调节支座上,减震承载箱位于护罩内,护罩上位于风速测量方向的部分开设缺口。The protection mechanism comprises a semi-ellipsoidal shield fixed on an adjustment support, a shock-absorbing bearing box located inside the shield, and a notch is provided on the shield in a part located in a wind speed measurement direction.
进一步地,所述伺服电动缸为六个,分三组周向排列。Furthermore, there are six servo electric cylinders, which are arranged circumferentially in three groups.
进一步地,所述调节支座为圆形,固定支座为六边形,减震承载箱与调节支座之间还设有隔震垫。Furthermore, the adjusting support is circular, the fixed support is hexagonal, and a seismic isolation pad is provided between the shock-absorbing bearing box and the adjusting support.
进一步地,所述减震承载箱包括箱体和用于固定安装风速测量传感器主体的承载板,箱体顶部开设缺口,承载板底面四角对称设置第一减震机构,承载板底面中部设置第二减震机构,承载板、第一减震机构、第二减震机构均位于箱体内,承载板上位于箱体缺口处的区域安装风速测量传感器主体。Furthermore, the shock-absorbing bearing box includes a box body and a bearing plate for fixedly installing the wind speed measurement sensor body, a notch is opened on the top of the box body, a first shock-absorbing mechanism is symmetrically arranged at the four corners of the bottom surface of the bearing plate, and a second shock-absorbing mechanism is arranged in the middle of the bottom surface of the bearing plate, the bearing plate, the first shock-absorbing mechanism, and the second shock-absorbing mechanism are all located in the box body, and the wind speed measurement sensor body is installed in the area of the bearing plate located at the notch of the box body.
进一步地,所述第一减震机构包括套筒、导杆、第一弹簧、下减震块,导杆上端与承载板底面固定连接,导杆下端滑动伸入套筒内,套筒固定与箱体底部,下减震块位于套筒内底部,第一弹簧套在导杆上,且第一弹簧的下端抵触套筒顶面。Furthermore, the first shock absorbing mechanism includes a sleeve, a guide rod, a first spring, and a lower shock absorbing block. The upper end of the guide rod is fixedly connected to the bottom surface of the bearing plate, and the lower end of the guide rod slides into the sleeve. The sleeve is fixed to the bottom of the box body, and the lower shock absorbing block is located at the bottom of the sleeve. The first spring is sleeved on the guide rod, and the lower end of the first spring contacts the top surface of the sleeve.
进一步地,所述第二减震机构包括剪叉杆、滑块、第二弹簧,滑块包括一体成型的滑动部、连接部、铰接部,滑动部滑动设置于承载板底部开设的滑槽内,铰接部与剪叉杆上端转动连接,剪叉杆下端与箱体底部铰接,第二弹簧位于滑槽内,第二弹簧一端与滑槽端部抵触,另一端与滑块的滑动部相抵触。Furthermore, the second shock absorbing mechanism includes a scissor rod, a slider, and a second spring. The slider includes an integrally formed sliding portion, a connecting portion, and a hinged portion. The sliding portion is slidably arranged in a sliding groove opened at the bottom of the supporting plate. The hinged portion is rotatably connected to the upper end of the scissor rod. The lower end of the scissor rod is hinged to the bottom of the box body. The second spring is located in the sliding groove. One end of the second spring is in contact with the end of the sliding groove, and the other end is in contact with the sliding portion of the slider.
进一步地,所述承载板与箱体顶部之间对称设置有多个上减震块,上减震块顶面固定于箱体顶部内壁上。Furthermore, a plurality of upper shock absorbing blocks are symmetrically arranged between the bearing plate and the top of the box body, and the top surfaces of the upper shock absorbing blocks are fixed on the inner wall of the top of the box body.
优选地,所述风速测量传感器主体采用机舱式激光测风雷达。Preferably, the wind speed measurement sensor body adopts a cabin-type laser wind measurement radar.
与现有技术相比,本实用新型的有益技术效果:Compared with the prior art, the beneficial technical effects of the utility model are:
1.本实用新型的在役风电叶片风速测量传感器安装结构设置的支撑机构为六自由度平台结构,不仅能够用于稳固安装和支撑风速测量传感器,提高风速测量传感器高空工作可靠性,还能够灵活调整风速测量传感器位置,便于风速测量传感器测得不同高度的风速、入流角等数据。1. The supporting mechanism of the installation structure of the wind speed measuring sensor for in-service wind turbine blades of the utility model is a six-degree-of-freedom platform structure, which can not only be used to stably install and support the wind speed measuring sensor and improve the reliability of the wind speed measuring sensor working at high altitude, but also can flexibly adjust the position of the wind speed measuring sensor, so that the wind speed measuring sensor can measure the wind speed, inflow angle and other data at different heights.
2.本实用新型的在役风电叶片风速测量传感器安装结构设置的减震机构能够有效减少震动,提高稳定性,与支撑机构配合大大提高了减震效果。2. The shock absorbing mechanism provided in the installation structure of the wind speed measuring sensor for in-service wind turbine blades of the utility model can effectively reduce vibration and improve stability, and cooperates with the supporting mechanism to greatly improve the shock absorbing effect.
附图说明BRIEF DESCRIPTION OF THE DRAWINGS
图1是本实用新型的在役风电叶片风速测量传感器安装结构的结构示意图;FIG1 is a schematic diagram of the structure of the installation structure of the wind speed measurement sensor for in-service wind turbine blades of the utility model;
图2是图1中减震承载箱的内部结构示意图;FIG2 is a schematic diagram of the internal structure of the shock-absorbing bearing box in FIG1 ;
图3是图2中滑块的结构示意图;FIG3 is a schematic structural diagram of the slider in FIG2 ;
附图标记:1-固定支座,101-定位孔,2-调节支座,3-伺服电动缸,4-隔震垫,5-减震承载箱,501-箱体,502-承载板,503-套筒,504-导杆,505-第一弹簧,506-下减震块,507-上减震块、508-滑槽,509-滑块,5091-滑动部,5092-连接部,5093-铰接部,510-第二弹簧,511-剪叉杆,6-护罩,7-风速测量传感器主体。Figure markings: 1-fixed support, 101-positioning hole, 2-adjusting support, 3-servo electric cylinder, 4-seismic isolation pad, 5-shock-absorbing bearing box, 501-box, 502-bearing plate, 503-sleeve, 504-guide rod, 505-first spring, 506-lower shock-absorbing block, 507-upper shock-absorbing block, 508-slide groove, 509-slider, 5091-sliding part, 5092-connecting part, 5093-hinge part, 510-second spring, 511-scissors rod, 6-protective cover, 7-wind speed measurement sensor body.
具体实施方式DETAILED DESCRIPTION
为了使本实用新型的目的、技术方案及优点更加清楚明白,以下通过优选的实施例对本实用新型进行进一步详细说明。In order to make the purpose, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below through preferred embodiments.
如图1-3所示,本实施例提供的一种在役风电叶片风速测量传感器安装结构,包括支撑机构、减震机构和防护机构;所述支撑机构包括固定支座1、调节支座2,固定支座1中部开设有多个定位孔101,固定支座1与调节支座2之间设有用于带动调节支座2进行位置调节的若干个伺服电动缸3,伺服电动缸3倾斜设置,伺服电动缸3上端和下端分别通过虎克铰与调节支座2、固定支座1铰接;所述减震机构包括用于安装风速测量传感器主体7的减震承载箱5,减震承载箱5底部安装于调节支座2上;防护机构,所述防护机构包括半椭球形的护罩6,护罩6固定于调节支座2上,减震承载箱5位于护罩6内,护罩6上位于风速测量方向的部分开设缺口。As shown in FIGS. 1-3, the present embodiment provides an installation structure for an in-service wind turbine blade wind speed measurement sensor, comprising a supporting mechanism, a shock absorbing mechanism and a protective mechanism; the supporting mechanism comprises a fixed support 1 and an adjustable support 2, a plurality of positioning holes 101 are provided in the middle of the fixed support 1, a plurality of servo electric cylinders 3 for driving the adjustable support 2 to adjust the position are provided between the fixed support 1 and the adjustable support 2, the servo electric cylinders 3 are tiltedly arranged, and the upper and lower ends of the servo electric cylinders 3 are respectively hinged to the adjustable support 2 and the fixed support 1 through Hooke's hinges; the shock absorbing mechanism comprises a shock absorbing bearing box 5 for mounting a wind speed measurement sensor body 7, and the bottom of the shock absorbing bearing box 5 is mounted on the adjustable support 2; the protective mechanism comprises a semi-ellipsoidal shield 6, the shield 6 is fixed on the adjustable support 2, the shock absorbing bearing box 5 is located in the shield 6, and a notch is provided on the shield 6 in the wind speed measurement direction.
本实施例的在役风电叶片风速测量传感器安装结构安装于风力发电机机舱顶部,固定支座1通过定位孔101对准定位后采用螺栓固定在机舱顶部。所述伺服电动缸3为六个,分三组周向排列,固定支座1、调节支座2、伺服电动缸3构成的支撑机构形成六自由度平台,能够稳定支撑减震机构和防护机构,并灵活调整减震机构的位置,使减震机构上承载的风速测量传感器主体7所处高度及测量角度得以同时调整,便于风速测量传感器主体7测得不同高度流经叶片的风速、入流角等数据,提高风速测量传感器主体7高空工作可靠性。The installation structure of the wind speed measuring sensor for the in-service wind turbine blades of this embodiment is installed on the top of the nacelle of the wind turbine generator. The fixed support 1 is fixed to the top of the nacelle by bolts after being aligned and positioned through the positioning hole 101. There are six servo electric cylinders 3, which are arranged circumferentially in three groups. The support mechanism composed of the fixed support 1, the adjustment support 2, and the servo electric cylinder 3 forms a six-degree-of-freedom platform, which can stably support the shock absorbing mechanism and the protective mechanism, and flexibly adjust the position of the shock absorbing mechanism, so that the height and measurement angle of the wind speed measuring sensor body 7 carried on the shock absorbing mechanism can be adjusted at the same time, which is convenient for the wind speed measuring sensor body 7 to measure the wind speed, inflow angle and other data flowing through the blades at different heights, and improve the reliability of the wind speed measuring sensor body 7 working at high altitude.
本实施例中,所述风速测量传感器主体7采用机舱式激光测风雷达,所述调节支座2为圆形,固定支座1为六边形,减震承载箱5与调节支座2之间还设有隔震垫4。In this embodiment, the wind speed measurement sensor body 7 adopts a nacelle-type laser wind measurement radar, the adjustment support 2 is circular, the fixed support 1 is hexagonal, and a seismic isolation pad 4 is provided between the shock-absorbing bearing box 5 and the adjustment support 2.
具体的,所述减震承载箱5包括箱体501和用于固定安装风速测量传感器的承载板502,箱体501顶部开设缺口,承载板502底面四角对称设置第一减震机构,承载板502底面中部设置第二减震机构,承载板502、第一减震机构、第二减震机构均位于箱体501内,承载板502上位于箱体501缺口处的区域安装风速测量传感器;其中,所述第一减震机构包括套筒503、导杆504、第一弹簧505、下减震块506剪叉杆,导杆504上端与承载板502底面固定连接,导杆504下端滑动伸入套筒503内,套筒503固定与箱体501底部,下减震块506剪叉杆位于套筒503内底部,第一弹簧505套在导杆504上,且第一弹簧505的下端抵触套筒503顶面;所述第二减震机构包括剪叉杆、滑块、第二弹簧,滑块包括一体成型的滑动部、连接部、铰接部,滑动部滑动设置于承载板502底部开设的滑槽内,铰接部与剪叉杆上端转动连接,剪叉杆下端与箱体501底部铰接,第二弹簧位于滑槽内,第二弹簧一端与滑槽端部抵触,另一端与滑块的滑动部相抵触。所述承载板502与箱体501顶部之间对称设置有多个上减震块,上减震块顶面固定于箱体501顶部内壁上。Specifically, the shock-absorbing bearing box 5 includes a box body 501 and a bearing plate 502 for fixing and installing a wind speed measuring sensor. A notch is provided on the top of the box body 501. A first shock-absorbing mechanism is symmetrically arranged at the four corners of the bottom surface of the bearing plate 502. A second shock-absorbing mechanism is arranged in the middle of the bottom surface of the bearing plate 502. The bearing plate 502, the first shock-absorbing mechanism, and the second shock-absorbing mechanism are all located in the box body 501. The wind speed measuring sensor is installed in the area of the bearing plate 502 located at the notch of the box body 501; wherein the first shock-absorbing mechanism includes a sleeve 503, a guide rod 504, a first spring 505, and a lower shock-absorbing block 506 scissor rod. The upper end of the guide rod 504 is fixedly connected to the bottom surface of the bearing plate 502. The guide rod 50 4 The lower end slides into the sleeve 503, the sleeve 503 is fixed to the bottom of the box 501, the lower shock-absorbing block 506 scissor rod is located at the bottom of the sleeve 503, the first spring 505 is sleeved on the guide rod 504, and the lower end of the first spring 505 abuts against the top surface of the sleeve 503; the second shock-absorbing mechanism includes a scissor rod, a slider, and a second spring. The slider includes an integrally formed sliding part, a connecting part, and a hinged part. The sliding part is slidably arranged in a slide groove opened at the bottom of the bearing plate 502, the hinged part is rotatably connected to the upper end of the scissor rod, the lower end of the scissor rod is hinged to the bottom of the box 501, the second spring is located in the slide groove, one end of the second spring abuts against the end of the slide groove, and the other end abuts against the sliding part of the slider. A plurality of upper shock-absorbing blocks are symmetrically arranged between the bearing plate 502 and the top of the box 501, and the top surface of the upper shock-absorbing blocks is fixed to the inner wall of the top of the box 501.
本实施例中,通过设置减震机构能够有效减少震动,进一步地提高稳定性,与支撑机构配合大大提高了减震效果。In this embodiment, the vibration can be effectively reduced by providing a shock absorbing mechanism, thereby further improving stability, and the shock absorbing effect is greatly improved in cooperation with the supporting mechanism.
本实用新型的在役风电叶片风速测量传感器安装结构用于将风速测量传感器主体7安装于风力发电机机舱顶部。安装时,将风速测量传感器主体7固定于承载板502上,然后将采用螺栓将固定支座1通过定位孔101固定在风力发电机机舱顶部,安装完成后,通过控制伺服电动缸3,实现风速测量传感器主体7高度位置、水平角度、俯仰角度的多姿态调节,便于风速测量传感器主体7测得不同高度流经叶片的风速、入流角等数据。The utility model of the installation structure of the wind speed measuring sensor for in-service wind turbine blades is used to install the wind speed measuring sensor body 7 on the top of the wind turbine nacelle. During installation, the wind speed measuring sensor body 7 is fixed on the bearing plate 502, and then the fixing support 1 is fixed on the top of the wind turbine nacelle through the positioning hole 101 by bolts. After the installation is completed, the height position, horizontal angle, and pitch angle of the wind speed measuring sensor body 7 are adjusted by controlling the servo electric cylinder 3, so that the wind speed measuring sensor body 7 can measure the wind speed, inflow angle and other data flowing through the blades at different heights.
以上所述为本实用新型的较佳实施例,用以解释本实用新型的技术方案,本领域技术人员还可以在本实用新型的精神和原则之内作常规修改、等同替换和改进等。The above description is a preferred embodiment of the present invention, which is used to explain the technical solution of the present invention. Those skilled in the art can also make routine modifications, equivalent substitutions and improvements within the spirit and principles of the present invention.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202420320451.2U CN221705031U (en) | 2024-02-21 | 2024-02-21 | In-service wind power blade wind speed measurement sensor mounting structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202420320451.2U CN221705031U (en) | 2024-02-21 | 2024-02-21 | In-service wind power blade wind speed measurement sensor mounting structure |
Publications (1)
Publication Number | Publication Date |
---|---|
CN221705031U true CN221705031U (en) | 2024-09-13 |
Family
ID=92649617
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202420320451.2U Active CN221705031U (en) | 2024-02-21 | 2024-02-21 | In-service wind power blade wind speed measurement sensor mounting structure |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN221705031U (en) |
-
2024
- 2024-02-21 CN CN202420320451.2U patent/CN221705031U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2004528509A (en) | Collecting wind power generation method and its equipment | |
CN221705031U (en) | In-service wind power blade wind speed measurement sensor mounting structure | |
Zendehbad et al. | Impact of forested fetch on energy yield and maintenance of wind turbines | |
CN111487640A (en) | An offshore scanning lidar wind measurement device and method | |
CN112032000A (en) | Windmill wind-driven generator | |
CN110318955B (en) | Blade shadow influence scope monitoring device for land wind generating set | |
CN204594695U (en) | A kind of small-sized transverse axis wind mill performance testboard bay | |
CN109779851B (en) | Apparatus and method for measuring sound power level of wind turbines | |
McKee et al. | Experimental investigation of the drag of flat plates and cylinders in the slipstream of a hovering rotor | |
Junlai et al. | Analysis of the dynamic response of offshore floating wind power platforms in waves | |
Smith et al. | Mechanisms of amplitude modulation in wind turbine noise | |
CN217233703U (en) | Multi-energy power generation integrated system suitable for shallow water area | |
CN115539296A (en) | Mast type bladeless wind power generation device | |
CN212301892U (en) | An offshore scanning lidar wind measurement device | |
CN115264309A (en) | Virtual reality project construction equipment based on BIM technology | |
CN220913353U (en) | Vehicle-mounted laser radar wind measuring device | |
CN220602506U (en) | Waterproof protection architecture and survey and drawing are with theodolite | |
CN216285362U (en) | Sensor device for moving meteorological observation of wind speed and wind direction | |
CN220772145U (en) | Wind turbine rotor blade test bench | |
Lundsager et al. | The dynamic behaviour of the stall-regulated Nibe A wind turbine. Measurements and a model for stall-induced vibrations | |
CN216042974U (en) | A portable signal tower for wind turbine noise test system | |
CN219159108U (en) | A lightning-resistant wind turbine fixing device | |
CN111862745A (en) | Portable wind driven generator experimental device | |
CN221630783U (en) | Energy power generation monitoring device | |
CN218862781U (en) | Wind wheel of vertical axis wind turbine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |