CN115492721A - Wind driven generator with wind resistance reducing blades - Google Patents
Wind driven generator with wind resistance reducing blades Download PDFInfo
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- CN115492721A CN115492721A CN202211033405.6A CN202211033405A CN115492721A CN 115492721 A CN115492721 A CN 115492721A CN 202211033405 A CN202211033405 A CN 202211033405A CN 115492721 A CN115492721 A CN 115492721A
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- 230000000979 retarding effect Effects 0.000 claims description 14
- 238000009434 installation Methods 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 6
- 230000000903 blocking effect Effects 0.000 claims description 5
- 230000017525 heat dissipation Effects 0.000 claims description 3
- 230000002401 inhibitory effect Effects 0.000 claims 1
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- 238000013461 design Methods 0.000 abstract description 2
- 238000010248 power generation Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
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- 238000013021 overheating Methods 0.000 description 1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
- F03D1/06495—Aerodynamic elements attached to or formed with the blade, e.g. flaps, vortex generators or noise reducers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/20—Wind motors characterised by the driven apparatus
- F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D7/00—Controlling wind motors
- F03D7/02—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor
- F03D7/022—Adjusting aerodynamic properties of the blades
- F03D7/0236—Adjusting aerodynamic properties of the blades by changing the active surface of the wind engaging parts, e.g. reefing or furling
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D7/00—Controlling wind motors
- F03D7/02—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor
- F03D7/022—Adjusting aerodynamic properties of the blades
- F03D7/0236—Adjusting aerodynamic properties of the blades by changing the active surface of the wind engaging parts, e.g. reefing or furling
- F03D7/0239—Adjusting aerodynamic properties of the blades by changing the active surface of the wind engaging parts, e.g. reefing or furling by means of teetering or coning blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D7/00—Controlling wind motors
- F03D7/02—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor
- F03D7/0264—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor for stopping; controlling in emergency situations
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/306—Surface measures
- F05B2240/3062—Vortex generators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2270/00—Control
- F05B2270/60—Control system actuates through
- F05B2270/606—Control system actuates through mechanical actuators
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
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- Sustainable Development (AREA)
- Sustainable Energy (AREA)
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- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Power Engineering (AREA)
- Wind Motors (AREA)
Abstract
本发明涉及一种带有降风阻叶片的风力发电机,包括:塔架、机舱、发电机、限速停止装置、电动折叠装置、翼型叶片、涡流发生器;所述塔架垂直固定在地面,所述机舱固定在所述塔架上;所述发电机设置在所述机舱内,并且发电机转轴贯穿所述机舱,所述限速停止装置与所述发电机转轴相连,所述翼型叶片通过所述电动折叠装置固定在所述发电机转轴上,翼型叶片尾部固定连接有所述涡流发生器。本发明能够通过翼型叶片以及涡流发生器,减小叶片阻力,增加叶片在低风速下的转速,还可以通过限速停止装置,使得风叶转速超过设计转速时,对其进行限定、刹车,通过所述电动折叠装置,在风速较大时对叶片进行折叠,对风力发电机起到保护作用。
The invention relates to a wind power generator with blades for reducing wind resistance, comprising: a tower, a nacelle, a generator, a speed limit stop device, an electric folding device, airfoil blades, and a vortex generator; the tower is vertically fixed on the ground , the nacelle is fixed on the tower; the generator is arranged in the nacelle, and the shaft of the generator runs through the nacelle, the speed limiting stop device is connected with the shaft of the generator, and the airfoil The blade is fixed on the rotating shaft of the generator through the electric folding device, and the tail of the airfoil blade is fixedly connected with the vortex generator. The invention can reduce the blade resistance through the airfoil blade and the vortex generator, increase the speed of the blade at low wind speed, and can also use the speed limit stop device to limit and brake the speed of the wind blade when the speed exceeds the design speed. Through the electric folding device, the blades are folded when the wind speed is high, so as to protect the wind power generator.
Description
技术领域technical field
本发明涉及风力发电技术领域,更具体的说是涉及一种带有降风阻叶片的风力发电机。The invention relates to the technical field of wind power generation, in particular to a wind power generator with blades for reducing wind resistance.
背景技术Background technique
风力发电是一种将风能转换为机械能的动力机械,而风力发电机则是通过利用风能带动叶片旋转,最终输出交流电的电力设备,具有很好的应用前景。Wind power generation is a power machine that converts wind energy into mechanical energy, while wind power generators are electrical equipment that use wind energy to drive blades to rotate and finally output alternating current, which has a good application prospect.
风力发电机的发功功率与风轮扫掠面积成正比,而在相同的扫掠面积情况下,叶片的旋转速度越快,发电量就越大,因此三叶片式风力发电机被普遍使用,但是三叶片式风力发电机目前存在的风阻问题以及如何在有限风速的情况下,使得叶片转动速度更快仍未得到很好的解决,因此如何在现有风力发电机叶片的基础上,减小叶片风阻,增加叶片转动速度是本领域技术人员亟需解决的问题。The power generated by the wind turbine is proportional to the swept area of the wind rotor, and in the case of the same swept area, the faster the blade rotates, the greater the power generation, so the three-bladed wind turbine is widely used. However, the current wind resistance problem of the three-bladed wind turbine and how to make the blades rotate faster under the condition of limited wind speed have not been well resolved. Therefore, on the basis of the existing wind turbine blades, how to reduce the Wind resistance of the blades and increasing the rotational speed of the blades are urgent problems to be solved by those skilled in the art.
发明内容Contents of the invention
有鉴于此,本发明提供了一种带有降风阻叶片的风力发电机。In view of this, the present invention provides a wind generator with blades for reducing wind resistance.
本发明提供的一种带有降风阻叶片的风力发电机,包括:塔架、机舱、发电机、翼型叶片、涡流发生器,其中:The invention provides a wind power generator with a blade for reducing wind resistance, comprising: a tower, a nacelle, a generator, an airfoil blade, and a vortex generator, wherein:
所述塔架垂直固定在地面,所述机舱固定在所述塔架的顶端,所述发电机固定在所述机舱内,其发电机转轴的前端沿所述机舱的前端穿出,多片所述翼型叶片沿所述发电机转轴的轴线呈圆周阵列并安装在其穿出端的轴壁上,所述涡流发生器固定在所述翼型叶片的后缘位置。The tower is vertically fixed on the ground, the nacelle is fixed on the top of the tower, the generator is fixed in the nacelle, and the front end of the generator rotating shaft passes through the front end of the nacelle, and the multi-piece The airfoil blades form a circular array along the axis of the generator shaft and are installed on the shaft wall at the exit end thereof, and the vortex generator is fixed at the trailing edge of the airfoil blades.
本发明的一些实施例中,还包括限速停止装置,其中包括:温度感应器、电磁缓速机构、电磁摩擦机构和控制器;In some embodiments of the present invention, a speed limit stop device is also included, including: a temperature sensor, an electromagnetic retarding mechanism, an electromagnetic friction mechanism and a controller;
优选的,所述发电机为双轴发电机,其两个发电机转轴分为发电机转轴前轴与发电机转轴后轴;并分别沿所述机舱的前端和后端穿出,所述翼型叶片安装在所述发电机转轴前轴的轴壁上;Preferably, the generator is a two-shaft generator, and the two generator shafts are divided into the front shaft of the generator shaft and the rear shaft of the generator shaft; Type blades are installed on the shaft wall of the front shaft of the generator shaft;
优选的,所述温度感应器固定设置在所述机舱内壁靠近所述发电机的位置;Preferably, the temperature sensor is fixedly arranged on the inner wall of the nacelle close to the generator;
优选的,所述电磁缓速机构固定设置在所述机舱尾部内壁,所述控制器能够根据所述温度感应器数据控制所述电磁缓速机构工作,所述控制器还与所述电磁摩擦机构电连接,所述控制器能够根据所述电磁缓速机构工作时长控制所述电磁摩擦机构工作;Preferably, the electromagnetic retarding mechanism is fixedly arranged on the inner wall of the tail of the nacelle, the controller can control the operation of the electromagnetic retarding mechanism according to the temperature sensor data, and the controller is also connected with the electromagnetic friction mechanism Electrically connected, the controller can control the electromagnetic friction mechanism to work according to the working time of the electromagnetic retarding mechanism;
本发明的一些实施例中,所述电磁缓速机构包括固定支架、定子线圈和转子,所述固定支架的中部设有转子孔,通过所述转子孔套设在所述发电机转轴后轴的外部,且端部与所述机舱的内壁上固定,其侧壁内部设有线圈腔,所述定子线圈安装在所述线圈腔内,所述转子套设固定连接在所述发电机转轴后轴上,能够在所述发电机转轴后轴的带动下在所述转子孔内转动;In some embodiments of the present invention, the electromagnetic retarding mechanism includes a fixed bracket, a stator coil, and a rotor. A rotor hole is provided in the middle of the fixed bracket, and is sleeved on the rear shaft of the generator shaft through the rotor hole. outside, and the end is fixed on the inner wall of the nacelle, and a coil cavity is provided inside the side wall, the stator coil is installed in the coil cavity, and the rotor is sheathed and fixedly connected to the rear shaft of the generator shaft above, it can rotate in the rotor hole driven by the rear shaft of the generator shaft;
本发明的一些实施例中,所述电磁摩擦机构包括:电磁块、刹停片、复位弹簧、挡片;所述电磁块中部开有避让孔,并套设于所述发电机转轴后轴的穿出端,与所述发电机转轴后轴的轴壁之间留有间隙,并固定在所述机舱的外壁上,所述刹停片通过滑轨滑动连接在所述发电机转轴后轴上,与所述电磁块相对,所述刹停片沿所述发电机转轴后轴做轴向滑动,所述复位弹簧套设在所述发电机转轴后轴上,且处于所述电磁块和所述刹停片之间,与所述避让孔对应,能够通过所述复位弹簧对所述刹停片进行复位,所述挡片固定在所述发电机转轴后轴的穿出端,限制所述刹停片与所述电磁块之间的滑动距离;所述控制器固定在所述机舱内,且分别与所述温度感应器,所述定子线圈和所述电磁块电连接,当风速较大,所述发电机产生的热量过高时,所述温度感应器会将信号传递至所述控制器,所述控制器控制所述定子线圈通电产生磁场,此时所述转子旋转切割磁场,产生抑制所述发电机转轴后轴转动的电磁力,降低所述发电机转轴后轴的转动速度;当所述定子线圈工作一定时间时,所述控制器将信号传递至所述电磁块,所述电磁块产生磁力,所述刹停片在磁力的作用下向所述电磁块方向移动,并与之贴合,两者相互摩擦,使所述发电机转轴停止运转;当温度降低到一定数值时,所述温度传感器将信号传递至控制器,控制器控制所述定子线圈和所述电磁块停止工作,所述发电机转轴后轴恢复转动;In some embodiments of the present invention, the electromagnetic friction mechanism includes: an electromagnetic block, a brake plate, a return spring, and a blocking plate; an escape hole is opened in the middle of the electromagnetic block, and it is sleeved on the rear shaft of the generator shaft. There is a gap between the penetrating end and the shaft wall of the rear shaft of the generator shaft, and is fixed on the outer wall of the nacelle, and the brake plate is slidably connected to the rear shaft of the generator shaft through slide rails , opposite to the electromagnetic block, the brake piece slides axially along the rear shaft of the generator shaft, the return spring is sleeved on the rear shaft of the generator shaft, and is located between the electromagnetic block and the Between the brake stop pieces, corresponding to the avoidance hole, the brake stop pieces can be reset by the return spring, and the blocking piece is fixed on the passing end of the rear shaft of the generator shaft to limit the The sliding distance between the brake plate and the electromagnetic block; the controller is fixed in the nacelle and is electrically connected to the temperature sensor, the stator coil and the electromagnetic block respectively. , when the heat generated by the generator is too high, the temperature sensor will transmit a signal to the controller, and the controller controls the stator coil to be energized to generate a magnetic field. At this time, the rotor rotates and cuts the magnetic field to generate Inhibit the electromagnetic force of the rotation of the rear shaft of the generator shaft and reduce the rotation speed of the rear shaft of the generator shaft; when the stator coil works for a certain period of time, the controller transmits the signal to the electromagnetic block, and the The electromagnetic block generates magnetic force, and the brake piece moves to the direction of the electromagnetic block under the action of the magnetic force, and sticks to it, and the two rub against each other to stop the rotation of the generator shaft; when the temperature drops to a certain value , the temperature sensor transmits the signal to the controller, the controller controls the stator coil and the electromagnetic block to stop working, and the rear shaft of the generator shaft resumes rotation;
在本发明的实施例中,还包括电动开合装置,所述电动开合装置包括电动液压推杆、铰接接头、折叠器;In an embodiment of the present invention, an electric opening and closing device is also included, and the electric opening and closing device includes an electro-hydraulic push rod, an articulated joint, and a folder;
优选的,所述折叠器的两活动页分别与所述发电机转轴后轴的穿出端和所述所述翼型叶片的内壁固定;Preferably, the two movable leaves of the folder are respectively fixed to the exit end of the rear shaft of the generator shaft and the inner wall of the airfoil blade;
优选的,所述电动液压推杆的两端均连接有铰接接头,且与所述控制器电连接,两个所述铰接接头分别固定在所述发电机转轴后轴的穿出端和对应的所述翼型叶片的内壁上,所述电动液压推杆进行伸缩时,能够带动所述翼型叶片随所述所述折叠器摆动;Preferably, both ends of the electro-hydraulic push rod are connected with articulated joints, and are electrically connected with the controller, and the two articulated joints are respectively fixed on the exit end of the rear shaft of the generator shaft and the corresponding On the inner wall of the airfoil blade, when the electro-hydraulic push rod is stretched, it can drive the airfoil blade to swing with the folder;
优选的,当翼型叶片停止工作时,所述控制器将会控制所述电动液压推杆进行收缩,使得所述翼型叶片向所述机舱方向折叠,当所述翼型叶片开始工作时,所述控制器控制所述电动液压推杆伸长,使得所述翼型叶片恢复原位;Preferably, when the airfoil blades stop working, the controller will control the electro-hydraulic push rod to shrink, so that the airfoil blades are folded toward the cabin, and when the airfoil blades start working, The controller controls the extension of the electro-hydraulic push rod so that the airfoil blade returns to its original position;
优选的,刹停片与电磁块的对应工作面上分别设有摩擦面;Preferably, friction surfaces are respectively provided on the corresponding working surfaces of the brake plate and the electromagnetic block;
优选的,在所述翼型叶片的连接处,靠近所述发电机转轴处设有一切角,且切角形状与所述机舱前端外壁壁形状吻合,所述切角上开有与所述电动液压推杆对应的避让开口;Preferably, at the connection of the airfoil blades, a cut corner is provided near the rotating shaft of the generator, and the shape of the cut corner matches the shape of the outer wall of the front end of the nacelle. The avoidance opening corresponding to the hydraulic push rod;
优选的,所述翼型叶片对切角与所述机舱贴合时,所述电动液压推杆停止工作,此时为翼型叶片收合的最大角度;Preferably, when the tangent angle of the airfoil blade fits the nacelle, the electro-hydraulic push rod stops working, which is the maximum angle of the airfoil blade retraction at this time;
优选的,所述翼型叶片通过螺栓固定连接在所述折叠器活动页上;Preferably, the airfoil blade is fixedly connected to the movable leaf of the folder by bolts;
优选的,所述电磁块的摩擦面与所述电磁块表面之间设有隔热层;Preferably, a heat insulating layer is provided between the friction surface of the electromagnetic block and the surface of the electromagnetic block;
优选的,所述机舱对应所述发电机安装位置上方处设有散热口;Preferably, the engine room is provided with a heat dissipation port above the installation position of the generator;
本发明提供的一种带有降风阻叶片的风力发电机,翼型形状选择为飞机翼型,可有效降低叶片风的阻力,通过在翼型叶片尾部安装涡流发生器,可避免气流过早发生分离,影响翼型叶片升力,进而使得翼型叶片转速降低,安装涡流发生器还会进一步减小翼型叶片的阻力,解决了目前风力发电机叶片的风阻问题,还提高了在有限风速的情况下,使得叶片转动速度更快。The present invention provides a wind generator with blades for reducing wind resistance. The airfoil shape is selected as an aircraft airfoil, which can effectively reduce the wind resistance of the blades. By installing a vortex generator at the tail of the airfoil blades, the premature occurrence of airflow can be avoided. Separation affects the lift force of the airfoil blades, which in turn reduces the speed of the airfoil blades. The installation of vortex generators will further reduce the resistance of the airfoil blades, which solves the wind resistance problem of the current wind turbine blades and also improves the airfoil in the case of limited wind speed. down, making the blades turn faster.
本发明的其它特征和优点将在随后的说明书中阐述,并且,部分地从说明书中变得显而易见,或者通过实施本发明而了解。本发明的目的和其他优点可通过在所写的说明书、权利要求书、以及附图中所特别指出的结构来实现和获得。Additional features and advantages of the invention will be set forth in the description which follows, and in part will be apparent from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention may be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
下面通过附图和实施例,对本发明的技术方案做进一步的详细描述。The technical solution of the present invention will be described in further detail below with reference to the drawings and embodiments.
附图说明Description of drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据提供的附图获得其他的附图。In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only It is an embodiment of the present invention, and those skilled in the art can also obtain other drawings according to the provided drawings without creative work.
图1为本发明的结构示意图。Fig. 1 is a structural schematic diagram of the present invention.
图2为限速停止装置示意图。Figure 2 is a schematic diagram of the speed limiting stop device.
图3为电动开合装置结构示意图。Fig. 3 is a schematic structural diagram of the electric opening and closing device.
图中:1、塔架;2、机舱;3、发电机;4、发电机转轴;5、翼型叶片; 6、涡流发生器;7、温度感应器;8、控制器;9、电磁缓速机构;10、电磁摩擦机构;11、电动开合装置;15、限速停止装置;16、散热口;18、螺栓; 41、发电机转轴前轴;42、发电机转轴后轴;91、固定支架;92、定子线圈; 93、转子;101、电磁块;102、刹停片;103、复位弹簧;104、挡片;112、电动液压推杆;113、铰接接头;115、折叠器。In the figure: 1. Tower; 2. Engine room; 3. Generator; 4. Generator shaft; 5. Airfoil blade; 6. Vortex generator; 7. Temperature sensor; 8. Controller; 9. Electromagnetic buffer 10. Electromagnetic friction mechanism; 11. Electric opening and closing device; 15. Speed limit stop device; 16. Cooling port; 18. Bolt; 41. Front shaft of generator shaft; 42. Rear shaft of generator shaft; Fixed bracket; 92, stator coil; 93, rotor; 101, electromagnetic block; 102, brake stop piece; 103, return spring; 104, stop piece; 112, electrohydraulic push rod;
具体实施方式detailed description
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
在本申请的描述中,需要理解的是,术语“中心”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本申请和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本申请的限制。In the description of this application, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", The orientations or positional relationships indicated by "top", "bottom", "inner", "outer", etc. are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the application and simplifying the description, rather than indicating or implying References to devices or elements must have a particular orientation, be constructed, and operate in a particular orientation and therefore should not be construed as limiting the application.
术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个该特征。在本申请的描述中,除非另有说明,“多个”的含义是两个或两个以上。The terms "first" and "second" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance or implicitly specifying the quantity of indicated technical features. Thus, a feature defined as "first" and "second" may explicitly or implicitly include one or more of these features. In the description of the present application, unless otherwise specified, "plurality" means two or more.
在本申请的描述中,需要说明的是,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通。对于本领域的普通技术人员而言,可以具体情况理解上述术语在本申请中的具体含义。In the description of this application, it should be noted that unless otherwise specified and limited, the terms "installation", "connection", and "connection" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection. Connected, or integrally connected; it can be mechanically connected or electrically connected; it can be directly connected or indirectly connected through an intermediary, and it can be the internal communication of two components. Those of ordinary skill in the art can understand the specific meanings of the above terms in this application in specific situations.
本发明实施例公开了一种带有降风阻叶片的风力发电机,包括:塔架1、机舱2、发电机3、翼型叶片5、涡流发生器6,其中:The embodiment of the present invention discloses a wind power generator with windage-reducing blades, including: a tower 1, a
塔架1垂直固定在地面,机舱2固定在塔架1的顶端,发电机3固定在机舱2内,其发电机转轴4的前端沿机舱2的前端穿出,多片翼型叶片5沿发电机转轴4的轴线呈圆周阵列并安装在其穿出端的轴壁上,涡流发生器6 固定在翼型叶片5的后缘位置。The tower 1 is vertically fixed on the ground, the
本实施例翼型形状选择为飞机翼型,可有效降低叶片风的阻力,通过在翼型叶片5尾部安装涡流发生器6,可避免气流过早发生分离,影响翼型叶片 5的升力,进而使得翼型叶片5转速降低,安装涡流发生器6还会进一步减小翼型叶片5的阻力,解决了目前风力发电机叶片的风阻问题,还提高了在有限风速的情况下,使得叶片转动速度更快。The airfoil shape of this embodiment is selected as an aircraft airfoil, which can effectively reduce the resistance of the blade wind. By installing a
为了防止因风速过大,发电机3转速过快,引起发电机3内部过热,进而影响发电机3使用寿命,在实施例1的基础上,还包括实施例2,在实施例 2中,还包括限速停止装置15,其中包括:温度感应器7、电磁缓速机构9、电磁摩擦机构10和控制器8;In order to prevent the generator 3 from overheating due to excessive wind speed and causing the generator 3 to overheat, thereby affecting the service life of the generator 3, on the basis of embodiment 1,
其中,发电机3为双轴发电机,其两个发电机转轴4分为发电机转轴前轴41与发电机转轴后轴42;并分别沿机舱2的前端和后端穿出,翼型叶片5 安装在发电机转轴前轴41的轴壁上;Wherein, the generator 3 is a biaxial generator, and its two generator shafts 4 are divided into a
在机舱2对应发电机3安装位置上方处设有散热口16,温度感应器7固定设置在机舱2内壁靠近发电机3的位置;A heat dissipation port 16 is provided above the installation position of the
电磁缓速机构9固定设置在机舱2尾部内壁,控制器8能够根据温度感应器7数据控制电磁缓速机构9工作,控制器8还与电磁摩擦机构10电连接, 8控制器能够根据电磁缓速机构9工作时长控制电磁摩擦机构10工作;The electromagnetic retarding mechanism 9 is fixedly arranged on the inner wall of the tail of the
电磁缓速机构9包括固定支架91、定子线圈92和转子93,固定支架91 的中部设有转子孔,通过转子孔套设在发电机转轴后轴42的外部,且端部与机舱2的内壁上固定,其侧壁内部设有线圈腔,定子线圈92安装在线圈腔内,转子93套设固定连接在发电机转轴后轴42上,能够在发电机转轴后轴42的带动下在转子孔内转动;The electromagnetic retarding mechanism 9 comprises a fixed
电磁摩擦机构10包括:电磁块101、刹停片102、复位弹簧103、挡片 104;电磁块101中部开有避让孔,并套设于发电机转轴后轴42的穿出端,与发电机转轴后轴42的轴壁之间留有间隙,并固定在机舱2的外壁上,刹停片402通过滑轨滑动连接在发电机转轴后轴42上,与电磁块101相对,刹停片102沿发电机转轴后轴42做轴向滑动,复位弹簧103套设在发电机转轴后轴42上,且处于电磁块101和刹停片102之间,与避让孔对应,能够通过复位弹簧103对刹停片102进行复位,挡片104固定在发电机转轴后轴42的穿出端,限制刹停片102与电磁块101之间的滑动距离;控制器8固定在机舱2 内,且分别与温度感应器7,定子线圈92和电磁块101电连接;The electromagnetic friction mechanism 10 comprises: an
当风速较小,发电机3工作时,产生的少量的热可以通过发电机3上方的散热口16排出,当风速过大,发电机3上方的散热口16不能够及时排除大量的热时,温度感应器7将会发挥作用,温度感应器7内的微处理器设置一个最高温度,当发电机3温度高于最高温度时,温度感应器7会将信号传递至控制器8,控制器8控制定子线圈92通电产生磁场,此时转子93旋转切割磁场,产生抑制发电机转轴后轴42转动的电磁力,降低发电机转轴后轴42 的转动速度;当定子线圈92工作一定时间时,控制器8将信号传递至电磁块 101,电磁块101产生磁力,刹停片102在磁力的作用下向电磁块101方向移动,并与之贴合,刹停片102与电磁块101的对应工作面上分别设有摩擦面,两者相互摩擦,使发电机转轴4停止运转;当温度降低到微处理器设置的正常温度数值时,温度传感器7将信号传递至控制器8,控制器8控制定子线圈 92和电磁块101停止工作,发电机转轴后轴42恢复转动。When the wind speed is low and the generator 3 is working, a small amount of heat generated can be discharged through the cooling vent 16 above the generator 3; when the wind speed is too high, the cooling vent 16 above the generator 3 cannot remove a large amount of heat in time The temperature sensor 7 will play a role, the microprocessor in the temperature sensor 7 sets a maximum temperature, when the temperature of the generator 3 is higher than the maximum temperature, the temperature sensor 7 will transmit the signal to the
此实施例的限速停止装置15可有效对发电机转轴4进行减速,防止因发电机转轴4转速过快,产生大量的热,而降低风力发电机的使用寿命。The speed-limiting
当风力发电机停止转动时,风力发电机翼型叶片5仍在进行迎风,因此会产生使得风力发电机旋转的力,而且此时风力发电机翼型叶片5承受很大的力,对风力发电机寿命有很大的影响,因此为了使风力发电机翼型叶片5 在风力发电机停止工作时,承受尽可能小的力,在实施例1的基础上,增加实施例3,在本实施例中设置了电动开合装置11,电动开合装置11包括电动液压推杆112、铰接接头113、折叠器115;When the wind-driven generator stops rotating, the wind-driven
折叠器115的两活动页分别与发电机转轴后轴42的穿出端和翼型叶片5 的内壁固定,折叠器115一活动页与翼型叶片5通过螺栓18进行固定,可实现翼型叶片5的折叠;The two movable pages of the
电动液压推杆112的两端均连接有铰接接头113,且与控制器8电连接,两个铰接接头113分别固定在发电机转轴后轴42的穿出端和对应的翼型叶片 5的内壁上,电动液压推杆112进行伸缩时,能够带动翼型叶片5随折叠器 115摆动。Both ends of the electro-
当翼型叶片5停止工作时,控制器8将会控制电动液压推杆112进行收缩,使得翼型叶片5向机舱2方向折叠,当翼型叶片5开始工作时,控制器8 控制电动液压推杆112伸长,使得翼型叶片5恢复原位。When the
为了使翼型叶片5收合角度最大,在翼型叶片5的连接处,靠近发电机转轴4处设有一切角,且切角形状与机舱2前端外壁壁形状吻合,切角上开有与电动液压推杆112对应的避让开口,此口大小仅允许电动液压推杆112 活动,此设计可防止因开口过大,而在翼型叶片5后方产生涡流,增加风阻。In order to make the folding angle of the
通过在实施例1的基础上,增加了实施例3,实施例3能够实现翼型叶片 5的开合,在发电机转轴停止旋转时,可实现向机舱2方向收合,尽可能减小翼型叶片5的迎风面积,减小限速停止装置的负担,当发电机转轴重新旋转时,翼型叶片5又可以恢复原位,以最大面积迎风,实现了风力发电机翼型叶片5的自动开合。By adding Embodiment 3 on the basis of Embodiment 1, Embodiment 3 can realize the opening and closing of the
本说明书中各个实施例采用递进的方式描述,每个实施例重点说明的都是与其他实施例的不同之处,各个实施例之间相同相似部分互相参见即可。对于实施例公开的装置而言,由于其与实施例公开的方法相对应,所以描述的比较简单,相关之处参见方法部分说明即可。Each embodiment in this specification is described in a progressive manner, each embodiment focuses on the difference from other embodiments, and the same and similar parts of each embodiment can be referred to each other. As for the device disclosed in the embodiment, since it corresponds to the method disclosed in the embodiment, the description is relatively simple, and for the related information, please refer to the description of the method part.
对所公开的实施例的上述说明,使本领域专业技术人员能够实现或使用本发明。对这些实施例的多种修改对本领域的专业技术人员来说将是显而易见的,本文中所定义的一般原理可以在不脱离本发明的精神或范围的情况下,在其它实施例中实现。因此,本发明将不会被限制于本文所示的这些实施例,而是要符合与本文所公开的原理和新颖特点相一致的最宽的范围。The above description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the invention. Therefore, the present invention will not be limited to the embodiments shown herein, but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
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CN101534090A (en) * | 2008-03-11 | 2009-09-16 | 扬州神州风力发电机有限公司 | Speed limiting and braking device of wind driven generator |
CN105065195A (en) * | 2014-05-01 | 2015-11-18 | 西门子能量股份有限公司 | Aerodynamic device for a rotor blade of a wind turbine |
CN105992870A (en) * | 2013-12-20 | 2016-10-05 | Lm Wp 专利控股有限公司 | Wind turbine blade with deployable aerodynamic device |
CN107387309A (en) * | 2017-08-08 | 2017-11-24 | 上海交通大学 | A kind of Anti-Typhoon blower fan of folding-jib |
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CN101534090A (en) * | 2008-03-11 | 2009-09-16 | 扬州神州风力发电机有限公司 | Speed limiting and braking device of wind driven generator |
CN105992870A (en) * | 2013-12-20 | 2016-10-05 | Lm Wp 专利控股有限公司 | Wind turbine blade with deployable aerodynamic device |
CN105065195A (en) * | 2014-05-01 | 2015-11-18 | 西门子能量股份有限公司 | Aerodynamic device for a rotor blade of a wind turbine |
CN107387309A (en) * | 2017-08-08 | 2017-11-24 | 上海交通大学 | A kind of Anti-Typhoon blower fan of folding-jib |
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