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CN115929545A - An electromagnetic force assisted fan sliding yaw device and method - Google Patents

An electromagnetic force assisted fan sliding yaw device and method Download PDF

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Publication number
CN115929545A
CN115929545A CN202310218570.7A CN202310218570A CN115929545A CN 115929545 A CN115929545 A CN 115929545A CN 202310218570 A CN202310218570 A CN 202310218570A CN 115929545 A CN115929545 A CN 115929545A
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yaw
main frame
electromagnet
gear ring
electromagnetic force
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CN115929545B (en
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李阳
宋培龙
刘子哲
张凯
宋健
张荣顺
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CRRC Wind Power Shandong Co Ltd
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CRRC Wind Power Shandong Co Ltd
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Priority to PCT/CN2023/127944 priority patent/WO2024183304A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K11/00Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
    • H02K11/20Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection for measuring, monitoring, testing, protecting or switching
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02NELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR
    • H02N15/00Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Power Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)

Abstract

The invention provides an electromagnetic force assisted fan sliding yaw device and method, relating to the technical field of wind power generation equipment, and adopting the following scheme: the yaw system comprises a yaw gear ring and a main frame, wherein a plurality of yaw motors are installed on the side edge of the main frame and are in transmission connection with the yaw gear ring, one surface, close to the yaw gear ring, of the main frame is a frame yaw surface, an upper electromagnet is arranged on the frame yaw surface, one surface, close to the main frame, of the yaw gear ring is a gear ring yaw surface, a lower electromagnet arranged corresponding to the upper electromagnet is arranged on the gear ring yaw surface, and a piezoelectric sensor and an air gap sensor are further arranged on the gear ring yaw surface. During the yaw, the upper electromagnet and the lower electromagnet are electrified, the same-name magnetic poles are formed under the electrified condition, mutual repulsion force is generated, upward reaction force is given to the main frame, a wire gap is ejected out between the yaw gear ring and the main frame by the upward reaction force, or most of pressure between the yaw bearing and the contact surface is offset through electromagnetic force. Simple structure, high reliability and low cost.

Description

一种电磁力辅助风机滑动偏航装置及方法An electromagnetic force assisted fan sliding yaw device and method

技术领域technical field

本发明涉及风力发电装备技术领域,尤其涉及一种电磁力辅助风机滑动偏航装置及方法。The invention relates to the technical field of wind power generation equipment, in particular to an electromagnetic force assisted sliding yaw device and method for a wind turbine.

背景技术Background technique

偏航为风力发电机组中不可或缺的功能。目前的偏航技术方案多为滚动偏航与滑动偏航。为了降低成本,偏航电机一般选取多个较小扭矩的电机。偏航时多个电机共同输出,进而达到偏航要求的扭矩数。随着当前风力发电机组功率、叶片直径的不断增大,尤其是海上风电的快速发展,主机架尺寸和重量越来越大,其所需要的偏航电机所输出的扭矩也越来越大,而由于空间受限,偏航电机的数量不可能一直增加。且即便是选用多个偏航电机的技术方案,仍具有不小的成本。故,风机在偏航时需要克服的巨大的阻力扭矩为制约风机成本的重要因素。Yawing is an integral function in wind turbines. The current yaw technical solutions are mostly rolling yaw and sliding yaw. In order to reduce the cost, the yaw motor generally selects multiple motors with smaller torque. When yawing, multiple motors output together to achieve the torque required for yawing. With the increasing power and blade diameter of current wind turbines, especially the rapid development of offshore wind power, the size and weight of the main frame are getting larger and larger, and the output torque of the yaw motor required by it is also increasing. However, due to limited space, it is impossible to increase the number of yaw motors all the time. And even if the technical solution of selecting multiple yaw motors, still has a lot of cost. Therefore, the huge resistance torque that the fan needs to overcome when yawing is an important factor that restricts the cost of the fan.

对此,申请号为2017102475494的中国专利提供了一种混合悬浮气隙调整型风机偏航系统,一方面,其方案采用的是行星轮结构,这表明只能有一个大功率电机,成本高,而现在商业化的偏航结构之所以使用较多小功率电机,是因为买多个小功率电机的花费比买一个大功率电机要低,同时,行星轮也挡住了电缆的通路还有人员的移动路径;另一方面,结构复杂,而且永磁体产生的磁力是有限的,其工作时,主机架依托于这个复杂结构一直保持悬浮状态,主机架与其支持结构之间一直存在一个气隙,后期故障率大幅增大。上述便是现有技术目前存在的现状。In this regard, the Chinese patent application number 2017102475494 provides a hybrid suspension air gap adjustment fan yaw system. On the one hand, the solution uses a planetary gear structure, which shows that there can only be one high-power motor, which is expensive. The reason why commercialized yaw structures use more low-power motors is because the cost of buying multiple low-power motors is lower than buying one high-power motor. At the same time, the planetary gears also block the passage of cables and personnel. The moving path; on the other hand, the structure is complex, and the magnetic force generated by the permanent magnet is limited. When it is working, the main frame relies on this complex structure to maintain a suspended state, and there is always an air gap between the main frame and its supporting structure. The failure rate has increased significantly. Above-mentioned is exactly the present situation that prior art exists at present.

因此,针对上述现有技术目前存在的现状,研发一种电磁力辅助风机滑动偏航装置及方法是急需解决的问题。Therefore, in view of the present situation of the above-mentioned prior art, it is an urgent problem to be solved to develop an electromagnetic force assisted fan sliding yaw device and method.

发明内容Contents of the invention

本发明的目的在于,针对现有技术中风机在偏航时需要克服的巨大的阻力扭矩耗费巨大成本、现有偏航装置结构复杂故障率高及成本高的问题,提出并设计一种电磁力辅助风机滑动偏航装置及方法。The purpose of the present invention is to propose and design an electromagnetic force for the problems of the huge resistance torque that the wind turbine needs to overcome when yawing, which consumes huge costs, and the structure of the existing yaw device is complicated, the failure rate is high, and the cost is high. Auxiliary fan sliding yaw device and method.

一方面,本发明为解决上述技术问题所采用的技术方案是:一种电磁力辅助风机滑动偏航装置,包括偏航齿圈和主机架,所述主机架的侧边安装有多个偏航电机(现有技术中方案采用的是行星轮结构,这表明只能有一个大功率电机,一个大功率电机带动行星轮结构运行,行星轮结构复杂,并且行星轮及其辅助电缆挡住了通行通道),所述偏航电机与所述偏航齿圈传动连接,所述主机架上靠近所述偏航齿圈的一面为机架偏航面,所述机架偏航面设置有上电磁铁,所述偏航齿圈上靠近所述主机架的一面为齿圈偏航面,所述齿圈偏航面设置有与所述上电磁铁对应布置的下电磁铁,所述齿圈偏航面还设置有压电传感器与气隙传感器。偏航时,上电磁铁和下电磁铁通电,通电情况下为同名磁极相对,产生相互的斥力,并给予主机架向上的反作用力,向上的反作用力将偏航齿圈与主机架之间顶出一丝缝隙、或通过电磁力抵消掉大部分偏航轴承与接触面之间的压力(现有技术中是工作时主机架一直保持悬浮状态,主机架与其支持结构之间一直存在一个气隙,而且永磁体产生的磁力是有限的,后期故障率大幅增大),从而减小偏航时偏航电机受到的阻力,降低偏航电机的输出功率,降低偏航电机成本。偏航结构更加简易,可靠性高,相对应的成本也会降低。On the one hand, the technical solution adopted by the present invention to solve the above technical problems is: an electromagnetic force assisted fan sliding yaw device, including a yaw ring gear and a main frame, and a plurality of yaw gears are installed on the side of the main frame Motor (the prior art scheme uses a planetary gear structure, which indicates that there can only be one high-power motor, and a high-power motor drives the planetary gear structure to run, and the planetary gear structure is complex, and the planetary gear and its auxiliary cables block the passageway ), the yaw motor is in transmission connection with the yaw ring gear, the side of the main frame close to the yaw ring gear is the frame yaw surface, and the frame yaw surface is provided with an upper electromagnet , the side of the yaw ring gear close to the main frame is the yaw surface of the ring gear, and the yaw surface of the ring gear is provided with a lower electromagnet arranged correspondingly to the upper electromagnet, and the yaw surface of the ring gear The surface is also equipped with piezoelectric sensors and air gap sensors. When yawing, the upper electromagnet and the lower electromagnet are energized. When energized, the magnetic poles of the same name are opposite to each other, generating mutual repulsion, and giving the main frame an upward reaction force. The upward reaction force pushes the gap between the yaw ring gear and the main frame. Create a gap, or offset most of the pressure between the yaw bearing and the contact surface through electromagnetic force (in the prior art, the main frame is always in a suspended state during work, and there is always an air gap between the main frame and its supporting structure. Moreover, the magnetic force generated by the permanent magnet is limited, and the failure rate will increase significantly in the later stage), thereby reducing the resistance of the yaw motor when yawing, reducing the output power of the yaw motor, and reducing the cost of the yaw motor. The yaw structure is simpler, the reliability is higher, and the corresponding cost will be reduced.

进一步的,所述机架偏航面与所述齿圈偏航面之间设置有上衬垫。上衬垫可为铜垫等,通过在主机架与偏航齿圈的接触面放置上衬垫,来减小主机架与偏航齿圈之间的摩擦,当电磁力抵消不足,主机架与偏航齿圈之间无法产生气隙的情况下,也能达到偏航的效果。Further, an upper pad is provided between the yaw surface of the frame and the yaw surface of the ring gear. The upper liner can be a copper pad, etc. By placing the upper liner on the contact surface between the main frame and the yaw ring gear, the friction between the main frame and the yaw ring gear can be reduced. When the electromagnetic force offset is insufficient, the main frame and the yaw ring gear The yaw effect can also be achieved when there is no air gap between the yaw ring gears.

进一步的,所述压电传感器与气隙传感器设置有多个,多个压电传感器与气隙传感器在齿圈偏航面上间隔排布。由于主机架与偏航齿圈接触面间,各处的压力可能均不相同,以及偏航时磁极正对面积变化等原因,所以在偏航齿圈上表面处需设置多个压电传感器与气隙传感器。Further, there are multiple piezoelectric sensors and air gap sensors, and the multiple piezoelectric sensors and air gap sensors are arranged at intervals on the yaw surface of the ring gear. Due to the different pressures on the contact surface between the main frame and the yaw ring gear, and the change in the area of the magnetic poles when yawing, it is necessary to install multiple piezoelectric sensors and sensors on the upper surface of the yaw ring gear Air gap sensor.

进一步的,所述机架偏航面以及齿圈偏航面均设置有磁铁嵌槽,所述上电磁铁和所述下电磁铁均嵌于所述磁铁嵌槽中。因非偏航状态时,电磁极不通电,主机架自然落于偏航齿圈的齿圈偏航面上,上电磁铁和下电磁铁均嵌于磁铁嵌槽中,避免外露影响主机架与偏航齿圈的配合。Further, the yaw surface of the frame and the yaw surface of the ring gear are provided with magnet slots, and the upper electromagnet and the lower electromagnet are both embedded in the magnet slots. Because in the non-yaw state, the electromagnetic pole is not energized, and the main frame naturally falls on the yaw surface of the ring gear of the yaw ring gear. Yaw ring gear fit.

进一步的,所述主机架上固定有制动器,所述制动器与所述偏航齿圈的内侧面配合,所述制动器上与所述偏航齿圈配合的面安装有侧衬垫。主机架在水平方向的位置是由制动器的侧衬垫约束,制动器固定于主机架上,其上的侧衬垫与固定于塔筒上的偏航齿圈保持一定的同心度及间隙。侧衬垫用以保证主机架在水平方向不乱窜。Further, a brake is fixed on the main frame, and the brake cooperates with the inner surface of the yaw ring gear, and a side pad is installed on the surface of the brake that cooperates with the yaw ring gear. The position of the main frame in the horizontal direction is restricted by the side pads of the brake. The brake is fixed on the main frame, and the side pads on it maintain a certain concentricity and clearance with the yaw ring gear fixed on the tower. The side pads are used to ensure that the main frame does not move around in the horizontal direction.

进一步的,所述上电磁铁和所述下电磁铁均为连续式布置。或者,所述上电磁铁和所述下电磁铁均设置有多块,且间隔布置,每相邻两块下电磁铁之间均具有相应的压电传感器与气隙传感器,每个传感器负责控制与自身相邻的两个电磁铁。Further, the upper electromagnet and the lower electromagnet are arranged continuously. Alternatively, the upper electromagnet and the lower electromagnet are provided with multiple pieces, and are arranged at intervals, and there are corresponding piezoelectric sensors and air gap sensors between each adjacent two lower electromagnets, and each sensor is responsible for controlling Two electromagnets adjacent to itself.

进一步的,所述上电磁铁与所述下电磁铁位置正对布置。或者,所述下电磁铁布置有两排,分别位于所述上电磁铁的两侧,呈三角式布置,更加稳定。Further, the upper electromagnet is arranged directly opposite to the lower electromagnet. Alternatively, the lower electromagnets are arranged in two rows, respectively located on both sides of the upper electromagnets, in a triangular arrangement, which is more stable.

另一方面,本发明还提供了一种电磁力辅助风机滑动偏航方法,包括上述电磁力辅助风机滑动偏航装置,还包括以下步骤:偏航时,上电磁铁与下电磁铁通电,通电情况下产生同名磁极,产生相互的斥力,并给予主机架向上的反作用力,向上的反作用力将偏航齿圈与主机架之间顶出一丝缝隙或者通过电磁力抵消掉大部分偏航轴承与接触面之间的压力;在电磁辅助偏航的同时,通过压电传感器检测主机架与偏航齿圈之间的压力,在上电磁铁以及下电磁铁间断式布局情况下,由于在偏航过程中主机架一侧的上电磁铁与偏航齿圈一侧的下电磁铁会由于交错而导致正对面积减小,这便导致了主机架受到的电磁斥力的大小会相应发生波动,此时若压电传感器测得压力较大,则说明其给予的斥力较小、抵消偏航摩擦力不足,则快速加大电流,使其产生较大斥力,快速抵消主机架与偏航齿圈之间的压力,在此过程中,若检测到主机架与偏航齿圈之间的压力已较小,则降低电流的增加速度,缓慢增加主机架与偏航齿圈之间的斥力,直至压力传感器检测到压力近乎为0时,不再增加电流强度。其中,非偏航状态时,上电磁铁和下电磁铁不通电,主机架自然落于偏航齿圈上。On the other hand, the present invention also provides an electromagnetic force assisted fan sliding yaw method, which includes the above electromagnetic force assisted fan sliding yaw device, and also includes the following steps: when yawing, the upper electromagnet and the lower electromagnet are energized, and the energized Under the circumstances, the magnetic poles with the same name are generated, which generate mutual repulsion, and give the main frame an upward reaction force. The upward reaction force will push out a gap between the yaw ring gear and the main frame or offset most of the yaw bearing and the main frame through electromagnetic force. The pressure between the contact surfaces; while the electromagnetic assists the yaw, the piezoelectric sensor detects the pressure between the main frame and the yaw ring gear. In the case of the intermittent layout of the upper electromagnet and the lower electromagnet, due to the During the process, the upper electromagnet on the side of the main frame and the lower electromagnet on the side of the yaw ring gear will reduce the facing area due to interlacing, which will cause the magnitude of the electromagnetic repulsion on the main frame to fluctuate accordingly. If the pressure measured by the piezoelectric sensor is relatively high, it means that the repulsive force given by the piezoelectric sensor is small and the friction force to offset the yaw is insufficient. Then quickly increase the current to make it generate a large repulsive force to quickly offset the gap between the main frame and the yaw ring gear. During this process, if it is detected that the pressure between the main frame and the yaw ring gear is already small, then reduce the increasing speed of the current, and slowly increase the repulsive force between the main frame and the yaw ring gear until the pressure When the sensor detects that the pressure is close to 0, the current intensity is no longer increased. Among them, in the non-yaw state, the upper electromagnet and the lower electromagnet are not powered, and the main frame naturally falls on the yaw ring gear.

从以上技术方案可以看出,本发明具有以下优点:As can be seen from the above technical solutions, the present invention has the following advantages:

本方案提供了一种电磁力辅助风机滑动偏航装置及方法,偏航时,嵌入主机架与偏航齿圈的接触面以内电磁铁通电产生磁力,电磁力将偏航齿圈与主机架之间顶出一丝缝隙、或通过电磁力抵消掉大部分偏航轴承与接触面之间的压力,从而减小偏航时偏航电机受到的阻力。进而在电机选型方面,可降低偏航电机功率及扭矩等输出参数,进一步的在偏航电机选型方面实现降本。This solution provides an electromagnetic force assisted fan sliding yaw device and method. When yawing, the electromagnet embedded in the contact surface of the main frame and the yaw ring gear is energized to generate magnetic force, and the electromagnetic force will move the distance between the yaw ring gear and the main frame. There is a gap between them, or the pressure between most of the yaw bearing and the contact surface is offset by electromagnetic force, so as to reduce the resistance of the yaw motor when yawing. Furthermore, in terms of motor selection, output parameters such as power and torque of the yaw motor can be reduced, and further cost reduction can be achieved in the selection of the yaw motor.

附图说明Description of drawings

为了更清楚地说明本发明的技术方案,下面将对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一些实施例,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,还可以根据这些附图获得其他的附图。In order to illustrate the technical solution of the present invention more clearly, the accompanying drawings that need to be used in the description will be briefly introduced below. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. As far as people are concerned, other drawings can also be obtained based on these drawings on the premise of not paying creative work.

图1为本发明具体实施方式的结构示意图。Fig. 1 is a schematic structural diagram of a specific embodiment of the present invention.

图2为本发明具体实施方式显示上电磁铁与下电磁铁正对位置关系的示意图。Fig. 2 is a schematic diagram showing the positional relationship between the upper electromagnet and the lower electromagnet according to a specific embodiment of the present invention.

图3为本发明具体实施方式显示上电磁铁与下电磁铁三角式位置关系的示意图。Fig. 3 is a schematic diagram showing the triangular positional relationship between the upper electromagnet and the lower electromagnet according to a specific embodiment of the present invention.

图4为本发明具体实施方式显示下电磁铁连续式布置方式的结构示意图。Fig. 4 is a schematic structural view showing the continuous arrangement of lower electromagnets according to a specific embodiment of the present invention.

图5为本发明具体实施方式显示下电磁铁间隔式布置方式的结构示意图。Fig. 5 is a schematic structural diagram showing the spaced arrangement of the lower electromagnets according to a specific embodiment of the present invention.

图6为本发明具体实施方式中压电传感器布置方式的结构示意图。Fig. 6 is a schematic structural diagram of the arrangement of piezoelectric sensors in a specific embodiment of the present invention.

图7为本发明具体实施方式中电磁铁电流变化逻辑图。Fig. 7 is a logic diagram of electromagnet current change in a specific embodiment of the present invention.

图8为本发明具体实施方式中电流与检测到压力大小的关系图。FIG. 8 is a graph showing the relationship between current and detected pressure in a specific embodiment of the present invention.

图9为本发明具体实施方式的电路原理简图。FIG. 9 is a schematic diagram of a circuit principle of a specific embodiment of the present invention.

图10为本发明具体实施方式3中安培力托举方式的结构示意图。Fig. 10 is a schematic structural view of the ampere-force lifting method in Embodiment 3 of the present invention.

图11为本发明具体实施方式整体的结构示意图。Fig. 11 is a schematic diagram of the overall structure of a specific embodiment of the present invention.

图中,1、偏航齿圈,2、主机架,3、偏航电机,4、下电磁铁,5、上电磁铁,6、上衬垫,7、下衬垫,8、侧衬垫,9、制动器,10、压电传感器,11、气隙传感器,12、导线,13、液压制动器,14、机械制动器,15、变速箱,16、塔筒。In the figure, 1. Yaw ring gear, 2. Main frame, 3. Yaw motor, 4. Lower electromagnet, 5. Upper electromagnet, 6. Upper pad, 7. Lower pad, 8. Side pad , 9, brake, 10, piezoelectric sensor, 11, air gap sensor, 12, wire, 13, hydraulic brake, 14, mechanical brake, 15, gearbox, 16, tower.

具体实施方式Detailed ways

为使得本发明的目的、特征、优点能够更加的明显和易懂,下面将结合本具体实施例中的附图,对本发明中的技术方案进行清楚、完整地描述,显然,下面所描述的实施例仅仅是本发明一部分实施例,而非全部的实施例。基于本专利中的实施例,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它实施例,都属于本专利保护的范围。In order to make the purpose, features and advantages of the present invention more obvious and understandable, the technical solutions in the present invention will be clearly and completely described below in conjunction with the accompanying drawings in this specific embodiment. Obviously, the implementation described below Examples are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in this patent, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this patent.

实施例1Example 1

如图1至图9以及图11所示,本具体实施方式提供了一种电磁力辅助风机滑动偏航装置,包括偏航齿圈1和主机架2,偏航齿圈1的下部连接有塔筒16,偏航齿圈1的内侧设置有机械制动器14,主机架2的侧边安装有多个偏航电机3,偏航电机3通过变速箱15与偏航齿圈1传动连接,主机架2上靠近偏航齿圈1的一面为机架偏航面,机架偏航面设置有上电磁铁5,偏航齿圈1上靠近主机架2的一面为齿圈偏航面,齿圈偏航面设置有与上电磁铁5对应布置的下电磁铁4。齿圈偏航面还设置有压电传感器10与气隙传感器11,压电传感器10与气隙传感器11设置有多个,多个压电传感器10与气隙传感器11在齿圈偏航面上间隔排布,由于主机架2与偏航齿圈1接触面间,各处的压力可能均不相同,以及偏航时磁极正对面积变化等原因,所以在偏航齿圈1上表面处需设置多个压电传感器10与气隙传感器11。As shown in Fig. 1 to Fig. 9 and Fig. 11, this specific embodiment provides an electromagnetic force assisted fan sliding yaw device, which includes a yaw ring gear 1 and a main frame 2, and the lower part of the yaw ring gear 1 is connected with a tower cylinder 16, a mechanical brake 14 is provided on the inner side of the yaw ring gear 1, and a plurality of yaw motors 3 are installed on the side of the main frame 2, and the yaw motor 3 is connected to the yaw ring gear 1 through a gearbox 15. 2, the side close to the yaw ring gear 1 is the frame yaw surface, and the upper electromagnet 5 is arranged on the frame yaw surface, and the side of the yaw ring gear 1 close to the main frame 2 is the ring gear yaw surface, and the ring gear The yaw surface is provided with a lower electromagnet 4 arranged corresponding to the upper electromagnet 5 . The yaw surface of the ring gear is also provided with a piezoelectric sensor 10 and an air gap sensor 11. There are multiple piezoelectric sensors 10 and air gap sensors 11, and multiple piezoelectric sensors 10 and air gap sensors 11 are arranged on the yaw surface of the ring gear. Arranged at intervals, due to the different pressures between the main frame 2 and the contact surface of the yaw ring gear 1, and the change in the area of the magnetic poles when yawing, the upper surface of the yaw ring gear 1 needs to be A plurality of piezoelectric sensors 10 and air gap sensors 11 are provided.

其中,机架偏航面以及齿圈偏航面均设置有磁铁嵌槽,上电磁铁5和下电磁铁4均嵌于磁铁嵌槽中。因非偏航状态时,电磁极不通电,主机架2自然落于偏航齿圈1的齿圈偏航面上,上电磁铁5和下电磁铁4均嵌于磁铁嵌槽中,避免外露影响主机架2与偏航齿圈1的配合。具体的,对于磁铁的布置方式,一些方案中,参见图4,上电磁铁5和下电磁铁4均为连续式布置;另一些方案中,参见图5,上电磁铁5和下电磁铁4均设置有多块,且间隔布置,每相邻两块下电磁铁4之间均具有相应的压电传感器10与气隙传感器11,每个传感器负责控制与自身相邻的两个电磁铁。此外,如图2所示,上电磁铁5与下电磁铁4位置正对布置;或者,如图3所示,下电磁铁4布置有两排,分别位于上电磁铁5的两侧,呈三角式布置,更加稳定。Wherein, both the yaw surface of the frame and the yaw surface of the ring gear are provided with magnet slots, and the upper electromagnet 5 and the lower electromagnet 4 are both embedded in the magnet slots. Because in the non-yaw state, the electromagnetic pole is not powered, the main frame 2 naturally falls on the ring gear yaw surface of the yaw ring gear 1, and the upper electromagnet 5 and the lower electromagnet 4 are embedded in the magnet slots to avoid exposure It affects the cooperation between the main frame 2 and the yaw ring gear 1. Specifically, for the layout of the magnets, in some schemes, see Figure 4, the upper electromagnet 5 and the lower electromagnet 4 are arranged continuously; in other schemes, see Figure 5, the upper electromagnet 5 and the lower electromagnet 4 There are multiple pieces arranged at intervals, and there are corresponding piezoelectric sensors 10 and air gap sensors 11 between every two adjacent lower electromagnets 4, and each sensor is responsible for controlling two adjacent electromagnets. In addition, as shown in Figure 2, the upper electromagnet 5 and the lower electromagnet 4 are arranged in direct opposition; or, as shown in Figure 3, the lower electromagnet 4 is arranged in two rows, which are respectively located on both sides of the upper electromagnet 5, forming a Triangular layout, more stable.

实施例2Example 2

本具体实施方式在具体实施方式1的基础上提供了一种偏航主动让步方案,具体的,参见图1,机架偏航面与齿圈偏航面之间设置有上衬垫6,上衬垫6可为铜垫等,通过在主机架2与偏航齿圈1的接触面放置上衬垫6,来减小主机架2与偏航齿圈1之间的摩擦,当电磁力抵消不足,主机架2与偏航齿圈1之间无法产生气隙的情况下,通过电磁力抵消一部分主机架2对偏航齿圈1的压力,也能达到偏航的效果。主机架2上固定有制动器9,制动器9与偏航齿圈1的内侧面配合,制动器9上与偏航齿圈1配合的面安装有侧衬垫8,主机架2在水平方向的位置是由制动器9的侧衬垫8约束,制动器9固定于主机架2上,其上的侧衬垫8与固定于塔筒上的偏航齿圈1保持一定的同心度及间隙,侧衬垫8用以保证主机架2在水平方向不乱窜。This specific embodiment provides a yaw active concession scheme on the basis of specific embodiment 1. Specifically, referring to FIG. 1 , an upper pad 6 is provided between the frame yaw surface and the The liner 6 can be a copper pad, etc. By placing the liner 6 on the contact surface between the main frame 2 and the yaw ring gear 1, the friction between the main frame 2 and the yaw ring gear 1 can be reduced. When the electromagnetic force cancels Insufficient, when there is no air gap between the main frame 2 and the yaw ring gear 1, the yaw effect can also be achieved by offsetting part of the pressure of the main frame 2 on the yaw ring gear 1 by electromagnetic force. A brake 9 is fixed on the main frame 2, and the brake 9 cooperates with the inner surface of the yaw ring gear 1, and a side pad 8 is installed on the surface of the brake 9 that cooperates with the yaw ring gear 1, and the position of the main frame 2 in the horizontal direction is Constrained by the side liner 8 of the brake 9, the brake 9 is fixed on the main frame 2, and the side liner 8 on it maintains a certain concentricity and clearance with the yaw ring gear 1 fixed on the tower. The side liner 8 To ensure that the main frame 2 does not run wild in the horizontal direction.

实施例3Example 3

本具体实施方式提供了一种电磁力辅助风机滑动偏航方法,包括具体实施方式1中的电磁力辅助风机滑动偏航装置,还包括以下步骤:偏航时,上电磁铁5与下电磁铁4通电,通电情况下产生同名磁极,产生相互的斥力,并给予主机架2向上的反作用力,向上的反作用力将偏航齿圈1与主机架2之间顶出一丝缝隙或者通过电磁力抵消掉大部分偏航轴承与接触面之间的压力;在电磁辅助偏航的同时,通过压电传感器10检测主机架2与偏航齿圈1之间的压力,在上电磁铁5以及下电磁铁4间断式布局情况下,由于在偏航过程中主机架2一侧的上电磁铁5与偏航齿圈1一侧的下电磁铁4会由于交错而导致正对面积减小,这便导致了主机架2受到的电磁斥力的大小会相应发生波动,此时若压电传感器10测得压力较大,则说明其给予的斥力较小、抵消偏航摩擦力不足,则快速加大电流,使其产生较大斥力,快速抵消主机架2与偏航齿圈1之间的压力,在此过程中,若检测到主机架2与偏航齿圈1之间的压力已较小,则降低电流的增加速度,缓慢增加主机架2与偏航齿圈1之间的斥力,直至压力传感器检测到压力近乎为0时,不再增加电流强度。其中,非偏航状态时,上电磁铁5和下电磁铁4不通电,主机架2自然落于偏航齿圈1上。This specific embodiment provides an electromagnetic force assisted fan sliding yaw method, including the electromagnetic force assisted fan sliding yaw device in Embodiment 1, and also includes the following steps: when yawing, the upper electromagnet 5 and the lower electromagnet 4. Power on. Under the condition of power on, the magnetic poles with the same name will be generated, which will generate mutual repulsion, and give the main frame 2 an upward reaction force. The upward reaction force will push out a gap between the yaw ring gear 1 and the main frame 2 or offset it by electromagnetic force. The pressure between the main frame 2 and the yaw ring gear 1 is detected by the piezoelectric sensor 10 while the electromagnetic assists the yaw, and the pressure between the upper electromagnet 5 and the lower electromagnetic In the case of iron 4 discontinuous layout, since the upper electromagnet 5 on the side of the main frame 2 and the lower electromagnet 4 on the side of the yaw ring gear 1 will reduce the facing area due to the staggering during the yaw process, this will As a result, the magnitude of the electromagnetic repulsion force received by the main frame 2 will fluctuate accordingly. At this time, if the pressure measured by the piezoelectric sensor 10 is relatively high, it means that the repulsion force given by it is small and the frictional force for offsetting the yaw is insufficient, so the current is quickly increased. , so that it generates a large repulsive force to quickly offset the pressure between the main frame 2 and the yaw ring gear 1. In the process, if it is detected that the pressure between the main frame 2 and the yaw ring gear 1 is already small, then Reduce the increasing speed of the current, slowly increase the repulsive force between the main frame 2 and the yaw ring gear 1, and stop increasing the current intensity until the pressure sensor detects that the pressure is almost zero. Wherein, in the non-yaw state, the upper electromagnet 5 and the lower electromagnet 4 are not energized, and the main frame 2 naturally falls on the yaw ring gear 1 .

实施例4Example 4

如图10所示,本具体实施方式提供了一种不同于具体实施方式1的偏航方式,具体为:将主机架2上方正对处埋入导线12,偏航时导线12通电,使得导线12在磁场中受到向上的安培力,将主机架2托起。结构如图9所示。若磁极N极指向外侧,则从上向下看通以逆时针电流;若N极指向内侧,则从上往下看通以顺时针电流。As shown in Figure 10, this specific embodiment provides a yaw method different from that of specific embodiment 1, specifically: embed a wire 12 directly above the main frame 2, and when yawing, the wire 12 is energized so that the wire 12 12 is subject to the upward ampere force in the magnetic field, and the main frame 2 is lifted up. The structure is shown in Figure 9. If the N pole of the magnetic pole points to the outside, the current flows counterclockwise from top to bottom; if the N pole points to the inside, the current flows clockwise from the top to the bottom.

本发明的说明书和权利要求书及上述附图中的术语“上”、“下”、“外侧”、“内侧”等(如果存在)是用于区别位置上的相对关系,而不必给予定性。应该理解这样使用的数据在适当情况下可以互换,以便这里描述的本发明的实施例能够以除了在这里图示或描述的那些以外的顺序实施。此外,术语“包括”和“具有”以及他们的任何变形,意图在于覆盖不排他的包含。The terms "upper", "lower", "outer side", "inner side" and the like in the description and claims of the present invention and the above drawings (if any) are used to distinguish the relative relationship in position, but not necessarily to be qualitative. It is to be understood that the data so used are interchangeable under appropriate circumstances such that the embodiments of the invention described herein can be practiced in sequences other than those illustrated or described herein. Furthermore, the terms "comprising" and "having", as well as any variations thereof, are intended to cover a non-exclusive inclusion.

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.

Claims (10)

1. The utility model provides a fan slip yaw unit is assisted to electromagnetic force, includes driftage ring gear (1) and main frame (2), a plurality of yaw motors (3) are installed to the side of main frame (2), yaw motors (3) with driftage ring gear (1) transmission is connected, its characterized in that, be close to on main frame (2) the one side of driftage ring gear (1) is the frame yaw face, the frame yaw face is provided with electromagnet (5), be close to on driftage ring gear (1) the one side of main frame (2) is the ring gear yaw face, the ring gear yaw face be provided with lower electro-magnet (4) that upper electro-magnet (5) correspond and arrange, the ring gear yaw face still is provided with piezoelectric sensor (10) and air gap sensor (11).
2. An electromagnetic force assisted fan sliding yaw apparatus according to claim 1, wherein an upper pad (6) is provided between the frame yaw surface and the ring gear yaw surface.
3. An electromagnetic force assisted fan sliding yaw device according to claim 1, wherein a plurality of piezoelectric sensors (10) and air gap sensors (11) are provided, and a plurality of piezoelectric sensors (10) and air gap sensors (11) are arranged on the gear ring yaw surface at intervals.
4. The electromagnetic force assisted fan sliding yaw device according to claim 1, wherein the frame yaw surface and the gear ring yaw surface are provided with magnet slots, and the upper electromagnet (5) and the lower electromagnet (4) are embedded in the magnet slots.
5. An electromagnetic force assisted fan sliding yaw device according to claim 2, characterized in that a brake (9) is fixed on the main frame (2), the brake (9) is matched with the inner side surface of the yaw gear ring (1), and a side gasket (8) is arranged on the surface of the brake (9) matched with the yaw gear ring (1).
6. An electromagnetic force assisted fan slip yaw apparatus according to any of claims 1 to 5, wherein the upper electromagnet (5) and the lower electromagnet (4) are arranged in series.
7. An electromagnetic force assisted fan sliding yaw apparatus according to any one of claims 1 to 5, wherein the upper electromagnet (5) and the lower electromagnet (4) are provided with a plurality of pieces, and are arranged at intervals, and a piezoelectric sensor (10) and an air gap sensor (11) are respectively arranged between every two adjacent lower electromagnets (4).
8. An electromagnetic force assisted fan slide yaw apparatus according to any one of claims 1 to 5, wherein the upper electromagnet (5) is disposed opposite to the lower electromagnet (4).
9. An electromagnetic force assisted fan slip yaw apparatus according to any of claims 1 to 5, wherein the lower electromagnets (4) are arranged in two rows, one on each side of the upper electromagnets (5).
10. An electromagnetic force assisted fan slip yaw method, comprising the electromagnetic force assisted fan slip yaw apparatus of claim 7, further comprising the steps of: during yaw, the upper electromagnet (5) and the lower electromagnet (4) are electrified, the same-name magnetic poles are generated under the electrified condition, mutual repulsion force is generated, upward reaction force is given to the main rack (2), and a wire gap is pushed out between the yaw gear ring (1) and the main rack (2) by the upward reaction force or part of pressure between a yaw bearing and a contact surface is offset through electromagnetic force; when the electromagnetic auxiliary yawing is performed, the pressure between a main frame (2) and a yawing gear ring (1) is detected through a piezoelectric sensor (10), under the condition that an upper electromagnet (5) and a lower electromagnet (4) are arranged in an intermittent manner, because the upper electromagnet (5) on one side of the main frame (2) and the lower electromagnet (4) on one side of the yawing gear ring (1) can reduce the facing area due to staggering in the yawing process, the size of electromagnetic repulsion force borne by the main frame (2) can fluctuate correspondingly, at the moment, if the pressure detected by the piezoelectric sensor (10) is large, the repulsion force given by the piezoelectric sensor is small, and the yawing friction force is not sufficient, the current is increased rapidly, so that the repulsion force is generated, the pressure between the main frame (2) and the yawing gear ring (1) is rapidly counteracted, in the process, if the pressure detected between the main frame (2) and the yawing gear ring (1) is reduced, the increasing speed of the current is reduced, the repulsion force between the main frame (2) and the yawing gear ring (1) is increased, and the current intensity is not increased until the pressure detected by the pressure sensor is nearly 0;
when the main frame is in a non-yawing state, the upper electromagnet (5) and the lower electromagnet (4) are not electrified, and the main frame (2) naturally falls on the yawing gear ring (1).
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