CN116155002A - Double-fed wind generator rotor connecting wire structure, wound rotor and its generator - Google Patents
Double-fed wind generator rotor connecting wire structure, wound rotor and its generator Download PDFInfo
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- CN116155002A CN116155002A CN202211609527.5A CN202211609527A CN116155002A CN 116155002 A CN116155002 A CN 116155002A CN 202211609527 A CN202211609527 A CN 202211609527A CN 116155002 A CN116155002 A CN 116155002A
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
- H02K3/50—Fastening of winding heads, equalising connectors, or connections thereto
- H02K3/51—Fastening of winding heads, equalising connectors, or connections thereto applicable to rotors only
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/04—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors
- H02K3/28—Layout of windings or of connections between windings
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/03—Machines characterised by numerical values, ranges, mathematical expressions or similar information
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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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Abstract
本发明属于风力发电机技术领域,涉及一种双馈风力发电机转子连接线结构、绕线式转子及其发电机。该绕线式转子,通过对转子连接线固定架、转子零环、补强支撑架、转子连接线圆弧折弯结构改进,形成具有一体化转子连接线结构的绕线式转子,在装机后进行严苛工况下的寿命测试,该绕线式转子具有更高地可靠性和更好地机械性能;同时,通过改进后转子风扇的紧凑型结构,使转子风扇到转子铁心和转子绕组的轴向距离被缩短,从而提高了发电机内部的空间利用率,同时对发电机转子的温升表现也有一定的改善作用。
The invention belongs to the technical field of wind power generators, and relates to a doubly-fed wind power generator rotor connection wire structure, a wound rotor and a generator thereof. The wound rotor, through the improvement of the rotor connecting wire fixing frame, rotor zero ring, reinforcing support frame, and rotor connecting wire arc bending structure, forms a wound rotor with an integrated rotor connecting wire structure. After installation The wound rotor has higher reliability and better mechanical performance for life testing under severe working conditions; at the same time, by improving the compact structure of the rear rotor fan, the shaft of the rotor fan to the rotor core and rotor winding The vertical distance is shortened, thereby improving the space utilization rate inside the generator, and at the same time, it also has a certain improvement effect on the temperature rise performance of the generator rotor.
Description
技术领域technical field
本发明属于风力发电机技术领域,涉及绕线式发电机转子,具体涉及一种双馈风力发电机转子连接线结构、绕线式转子及其发电机。The invention belongs to the technical field of wind power generators, and relates to a wound generator rotor, in particular to a doubly-fed wind power generator rotor connecting wire structure, a wound rotor and a generator thereof.
背景技术Background technique
随着风力发电机功率等级和风电行业成本压力的不断增大,风力发电机舱内的空间可谓是“寸土寸金”,提升发电机整机可靠性、提高发电机内部空间利用率、降低风力发电成本是必须要解决的技术难题。因此,如何在有限的机舱及发电机空间内尽可能充分地利用空间,同时提高发电机及部件的可靠性,就成为了风力发电机设计的关键。As the power level of wind turbines and the cost pressure of the wind power industry continue to increase, the space in the cabin of wind turbines can be described as "every inch of land" to improve the reliability of the generator, improve the utilization of the internal space of the generator, and reduce the cost of wind power generation. Cost is a technical problem that must be solved. Therefore, how to make full use of the space in the limited space of the nacelle and the generator while improving the reliability of the generator and its components has become the key to the design of the wind turbine.
目前,国内外主流绕线式转子的连接线和零环的固定结构如图3所示。转子铁心10、转子绕组支架2和转子连接线固定架3通过各自内圆与转轴11采用过盈配合的连接方式固定;转子绕组1通过转子连接线5(其结构参见图1)与转子引出线9或转子零环13相连,转子连接线5通过绝缘绑扎带6与转子连接线固定架3(其截面带有凹槽,用于绑扎定位,但非封闭式结构)进行绑扎固定;转子零环13通过外圈的绝缘绑扎带6固定在转轴11表面;转子连接线5和转子引出线9是变流器与转子绕组4之间双向能量流动的重要部件,它们的可靠性设计直接关系到风力发电机组的运行稳定性。At present, the fixed structure of the connecting wire and the zero ring of the mainstream wound rotor at home and abroad is shown in Figure 3. The
而现有绕线式转子仍存在如下不足:第一、转子连接线固定架功能单一且此固定结构在严苛工况下的可靠性存在风险;第二、转子连接线90°折弯处的R角通常按照国标执行,在严苛工况下存在应力集中风险;第三、转子零环的固定结构在严苛工况下的可靠性存在风险;第四、转子连接线、转子零环、转子绕组支架的结构一体性不佳;第五、转子连接线和风扇之间(无风扇则为与端盖之间)的轴向空间利用不够充分。However, the existing wound rotor still has the following deficiencies: first, the function of the rotor connecting wire fixing frame is single, and the reliability of this fixing structure under severe working conditions is at risk; second, the 90° bend of the rotor connecting wire The R angle is usually implemented in accordance with the national standard, and there is a risk of stress concentration under severe working conditions; third, the reliability of the fixed structure of the rotor zero ring is at risk under severe working conditions; fourth, the rotor connection line, rotor zero ring, The structural integrity of the rotor winding support is not good; fifth, the axial space between the rotor connection line and the fan (or between the end cover and the end cover if there is no fan) is not fully utilized.
发明内容Contents of the invention
本发明的目的在于克服上述现有技术的缺点,提供一种双馈风力发电机转子连接线结构、绕线式转子及其发电机。该绕线式转子,提供了可靠性更高的转子连接线和转子零环的固定结构,同时降低了转子整体的轴向空间占用率(含风扇),提升了双馈风力发电机转子结构在严苛工况下的可靠性。The purpose of the present invention is to overcome the above-mentioned shortcomings of the prior art, and provide a doubly-fed wind power generator rotor connecting wire structure, a wound rotor and a generator thereof. The wound rotor provides a more reliable fixed structure for the rotor connection line and the rotor zero ring, and at the same time reduces the overall axial space occupancy of the rotor (including the fan), and improves the rotor structure of the doubly-fed wind turbine. Reliability under harsh conditions.
为实现上述目的,本发明提供了如下技术方案:To achieve the above object, the present invention provides the following technical solutions:
第一方面,本发明提供了一种双馈风力发电机转子连接线结构,包括一体成型的转子连接线本体,所述转子连接线本体包括与转子绕组相接的第一连接部,所述第一连接部的下方依次分布扭转连接部、与转子绕组支架端面相接的第二连接部以及用于减弱转子连接线本体折弯处应力的圆弧状连接部,所述圆弧状连接部与水平状的第三连接部相接;所述第二连接部与圆弧状连接部的连接处形成第一过渡圆弧,所述圆弧状连接部与水平状的第三连接部的连接处形成第二过渡圆弧,所述第一过渡圆弧和第二过渡圆弧之间为第三过渡圆弧。In the first aspect, the present invention provides a doubly-fed wind power generator rotor connection wire structure, which includes an integrally formed rotor connection wire body, the rotor connection wire body includes a first connecting portion connected to the rotor winding, and the first Below the first connecting part, there are sequentially distributed a twisted connecting part, a second connecting part connected to the end face of the rotor winding support, and an arc-shaped connecting part for reducing the stress at the bending part of the rotor connecting wire body. The horizontal third connection part is connected; the connection between the second connection part and the arc-shaped connection part forms a first transitional arc, and the connection between the arc-shaped connection part and the horizontal third connection part A second transitional arc is formed, and a third transitional arc is formed between the first transitional arc and the second transitional arc.
进一步,所述第一过渡圆弧、第二过渡圆弧各自对应的圆心角的度数均介于135°和180°之间。Further, the degrees of the central angles corresponding to the first transitional arc and the second transitional arc are both between 135° and 180°.
进一步,所述第一过渡圆弧、第二过渡圆弧、第三过渡圆弧各自对应的弧半径均介于X和2X之间,所述X为转子连接线本体的厚度。Further, the respective arc radii of the first transitional arc, the second transitional arc and the third transitional arc are all between X and 2X, where X is the thickness of the main body of the connecting wire of the rotor.
进一步,所述第三过渡圆弧的圆心角为90°。Further, the central angle of the third transition arc is 90°.
第二方面,本发明提供了一种绕线式转子,包括转轴、转子铁心、转子绕组、转子绕组支架、转子连接线、转子零环、转子引出线和转子连接线固定架;其中,所述转子连接线采用如上部分或全部所述的转子连接线结构;In the second aspect, the present invention provides a wound rotor, including a rotating shaft, a rotor core, a rotor winding, a rotor winding support, a rotor connection wire, a rotor zero ring, a rotor lead wire, and a rotor connection wire fixing frame; wherein, the The rotor connection line adopts the structure of the rotor connection line described in part or all above;
所述转子绕组嵌放在转子铁心内,并沿转轴的轴向伸出转子铁心端面,且伸出部分由转子绕组支架支撑,伸出部分通过转子连接线与转子零环、转子引出线连接;The rotor winding is embedded in the rotor core, and protrudes from the end face of the rotor core along the axial direction of the rotating shaft, and the protruding part is supported by the rotor winding bracket, and the protruding part is connected with the rotor zero ring and the rotor lead wire through the rotor connecting wire;
所述转子连接线固定架的截面呈“D”型,其竖直侧与转子绕组支架连接,弧形侧通过绝缘绑扎带与转子连接线绑扎固定;The section of the rotor connecting wire fixing frame is "D" shape, its vertical side is connected with the rotor winding support, and the arc side is bound and fixed with the rotor connecting wire by insulating binding tape;
所述转轴上套设有转子零环限位环,所述转子零环沿轴向嵌入转子零环限位环和转轴之间的间隙内,所述间隙内填充有绝缘块;A rotor zero-ring limiting ring is sleeved on the rotating shaft, and the rotor zero-ring is axially embedded in the gap between the rotor zero-ring limiting ring and the rotating shaft, and the gap is filled with insulating blocks;
所述转轴上还安装有转子风扇,所述转子风扇位于转子引出线的右侧;所述转子风扇的内圆开设有用以避让转子连接线和转轴表面固定结构的缺口。A rotor fan is also installed on the rotating shaft, and the rotor fan is located on the right side of the rotor lead-out line; the inner circle of the rotor fan is provided with a gap for avoiding the rotor connection line and the fixed structure on the surface of the rotating shaft.
进一步,所述转子连接线中的三支与转子零环连接,另外三支与转子引出线连接,且两者的轴向引出方向相反。Further, three of the rotor connection lines are connected to the rotor zero ring, and the other three are connected to the rotor lead-out lines, and the axial lead-out directions of the two are opposite.
进一步,所述转子零环限位环采用整圆环或整圆槽,或者采用由分段圆弧形成的圆环或圆槽。具体地,所述转子零环限位环可以是额外安装在转子绕组支架上的圆环,也可以是由转子绕组支架加工而成的槽。Further, the rotor zero ring limit ring adopts a full circle or a full circle groove, or adopts a circle or a circle formed by segmented arcs. Specifically, the rotor zero-ring limiting ring may be a circular ring additionally installed on the rotor winding support, or may be a groove processed by the rotor winding support.
进一步,所述转子连接线固定架焊接固定在转子绕组支架的端面,且转子连接线固定架采用圆钢或扁钢制成。Further, the rotor connecting wire fixing frame is welded and fixed on the end surface of the rotor winding support, and the rotor connecting wire fixing frame is made of round steel or flat steel.
进一步,所述转子连接线固定架内还设置有异型补强支撑架,用以增强转子连接线固定架的刚性,使发电机在运转过程中,在转子连接线受到大小相同的离心力时产生更小的变形或位移。Further, the fixed frame of the rotor connecting wire is also provided with a special-shaped reinforcing support frame, which is used to enhance the rigidity of the fixing frame of the rotor connecting wire, so that during the operation of the generator, when the rotor connecting wire is subjected to the same centrifugal force, a stronger Small deformation or displacement.
更进一步,为了实现转子绕组支架整体的轻量化设计,使用有限元仿真软件对传统的“类直角三角形”补强支撑架进行分析、减重,将其受力较小的部分移除,最终形成一个类似斜向的“工”字型结构的异型补强支撑结构,且该异型补强支撑结构的重量相比于轻量化之前,减重50%,但支撑强度完全能够满足支撑强度的需求。Furthermore, in order to realize the overall lightweight design of the rotor winding support, finite element simulation software was used to analyze and reduce the weight of the traditional "right-angled triangle-like" reinforcing support frame, and remove the part with less force, and finally formed A special-shaped reinforced support structure similar to an oblique "I"-shaped structure, and the weight of the special-shaped reinforced support structure is reduced by 50% compared with that before lightening, but the supporting strength can fully meet the needs of supporting strength.
第三方面,本发明还提供了一种风力发电机,包括如上部分或全部所述的绕线式转子。该风力发电机由于转子风扇到转子铁心和转子绕组的轴向距离被缩短,在提高发电机内部空间利用率的同时对发电机转子的温升表现也有一定的改善作用。In a third aspect, the present invention also provides a wind power generator, comprising the wound rotor described in part or all above. Since the axial distance from the rotor fan to the rotor core and the rotor winding is shortened in the wind generator, the temperature rise performance of the generator rotor is also improved to a certain extent while improving the utilization rate of the inner space of the generator.
与现有技术相比,本发明提供的技术方案包括以下有益效果:通过对转子连接线固定架、转子零环、补强支撑架、转子连接线圆弧折弯结构改进,形成具有一体化转子连接线结构的绕线式转子,在装机后进行严苛工况下的寿命测试,该绕线式转子具有更高地可靠性和更好地机械性能。Compared with the prior art, the technical solution provided by the present invention includes the following beneficial effects: by improving the structure of the rotor connecting line fixing frame, the rotor zero ring, the reinforcing support frame, and the arc bending structure of the rotor connecting line, an integrated rotor is formed. The wound rotor with connecting wire structure is tested for life under severe working conditions after installation. The wound rotor has higher reliability and better mechanical performance.
就该风力发电机而言,由于改进后转子风扇的紧凑型结构,使转子风扇到转子铁心和转子绕组的轴向距离被缩短,从而提高发电机内部的空间利用率,同时对发电机转子的温升表现也有一定的改善作用。As far as the wind generator is concerned, due to the improved compact structure of the rotor fan, the axial distance from the rotor fan to the rotor core and rotor winding is shortened, thereby improving the space utilization ratio inside the generator, and improving the generator rotor The temperature rise performance also has a certain improvement effect.
附图说明Description of drawings
此处的附图被并入说明书中并构成本说明书的一部分,与说明书一起用于解释本发明的原理。The accompanying drawings are incorporated in and constitute a part of this specification, and together with the description, serve to explain the principles of the invention.
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,对于本领域普通技术人员而言,在不付出创造性劳动性的前提下,还可以根据这些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, for those of ordinary skill in the art, In other words, other drawings can also be obtained from these drawings without paying creative labor.
图1为现有转子连接线结构的示意图;Fig. 1 is a schematic diagram of the existing rotor connection line structure;
图2为本发明提供的转子连接线结构的示意图;Fig. 2 is a schematic diagram of the structure of the rotor connecting wire provided by the present invention;
图3为现有绕线式转子的结构图;Fig. 3 is a structural diagram of an existing wound rotor;
图4为本发明提供的绕线式转子的结构图;Fig. 4 is a structural diagram of a wound rotor provided by the present invention;
图5为本发明提供的转子绕组支架的结构图;Fig. 5 is a structural diagram of the rotor winding support provided by the present invention;
图6为本发明提供的异型补强支撑架轻量化前后的结构示意图;Fig. 6 is a schematic diagram of the structure of the special-shaped reinforcing support frame before and after lightening provided by the present invention;
图7为本发明提供的转子风扇的结构图。Fig. 7 is a structural diagram of the rotor fan provided by the present invention.
其中:1、转子绕组;2、转子绕组支架;3、转子连接线固定架;4、异型补强支撑架;5、转子连接线;6、绝缘绑扎带;7、转子连接线折弯处;8、转子风扇;9、转子引出线;10、转子铁心;11、转轴;12、转子零环限位环;13、转子零环;14、第一连接部;15、扭转连接部;16、第二连接部;17、圆弧状连接部;18、第三连接部;19、缺口。Among them: 1. Rotor winding; 2. Rotor winding support; 3. Rotor connecting wire fixing frame; 4. Special-shaped reinforcing support frame; 5. Rotor connecting wire; 6. Insulation binding tape; 8. Rotor fan; 9. Rotor lead wire; 10. Rotor core; 11. Rotating shaft; 12. Rotor zero ring limit ring; 13. Rotor zero ring; 14. First connection part; 15. Torsion connection part; 16. The second connecting part; 17, the arc-shaped connecting part; 18, the third connecting part; 19, the notch.
具体实施方式Detailed ways
这里将详细地对示例性实施例进行说明,其示例表示在附图中。下面的描述涉及附图时,除非另有表示,不同附图中的相同数字表示相同或相似的要素。以下示例性实施例中所描述的实施方式并不代表与本发明相一致的所有实施方式。相反,它们仅是与所附权利要求书中所详述的、本发明的一些方面相一致的结构的例子。Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numerals in different drawings refer to the same or similar elements unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the present invention. Rather, they are merely examples of structures consistent with aspects of the invention as recited in the appended claims.
为了使本领域的技术人员更好地理解本发明的技术方案,下面结合附图及实施例对本发明作进一步详细描述。In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
实施例1Example 1
参见图2所示,本实施例提供了一种双馈风力发电机转子连接线结构,包括一体成型的转子连接线本体,所述转子连接线本体包括与转子绕组1相接的第一连接部14,所述第一连接部14的下方依次分布扭转连接部15、与转子绕组支架2端面相接的第二连接部16以及用于减弱转子连接线本体折弯处应力的圆弧状连接部17,所述圆弧状连接部17与水平状的第三连接部18相接;所述第二连接部16与圆弧状连接17的连接处形成第一过渡圆弧,所述圆弧状连接部17与水平状的第三连接部18的连接处形成第二过渡圆弧,所述第一过渡圆弧和第二过渡圆弧之间为第三过渡圆弧。As shown in FIG. 2 , this embodiment provides a doubly-fed wind turbine rotor connecting wire structure, which includes an integrally formed rotor connecting wire body, and the rotor connecting wire body includes a first connecting portion connected to the rotor winding 1 14. Below the first connecting
进一步,所述扭转连接部15之所以进行扭转,是为了更好地配合转子连接线本体与转子绕组1和转子引出线9的连接。具体地讲,如果不进行“麻花状”扭转,转子连接线本体按照和转子绕组1的端部连接的方向直接下来折弯的话,折弯处的厚度必然远大于其宽度;一方面,会在径向方向和轴向方向占用更多的空间,另一方面,如果以上述截面(不扭转时的截面)折弯过去的话,转子连接线本体和转子引出线9的焊接面积也会减小,绝缘也更难做。而如果为了保证焊接面积和绝缘工艺,把转子引出线9截面也竖起来的话,他就会在轴孔内部占用更多空间,同时还会降低绝缘可靠性。Further, the reason why the twisted connecting
进一步,所述第一过渡圆弧对应的圆心角α、第二过渡圆弧对应的圆心角β的度数均介于135°和180°之间。其中,圆心角α的度数取决于转子连接线本体左侧边距离铁心侧转子支架的距离,圆心角β的度数取决于转子连接线本体下方距离转轴11的距离。Further, the degrees of the central angle α corresponding to the first transitional arc and the central angle β corresponding to the second transitional arc are both between 135° and 180°. Wherein, the degree of the central angle α depends on the distance from the left side of the rotor connecting line body to the rotor support on the core side, and the degree of the central angle β depends on the distance from the bottom of the rotor connecting line body to the
进一步,所述第一过渡圆弧、第二过渡圆弧、第三过渡圆弧各自对应的弧半径均介于X和2X之间,所述X为转子连接线本体的厚度。Further, the respective arc radii of the first transitional arc, the second transitional arc and the third transitional arc are all between X and 2X, where X is the thickness of the main body of the connecting wire of the rotor.
优选地,所述第一过渡圆弧、第二过渡圆弧、第三过渡圆弧各自对应的弧半径均为1.5X,X为转子连接线本体的厚度。Preferably, the arc radii corresponding to the first transition arc, the second transition arc, and the third transition arc are all 1.5X, and X is the thickness of the rotor connecting wire body.
进一步,所述第三过渡圆弧的圆心角为90°。Further, the central angle of the third transition arc is 90°.
具体地,转子连接线本体优化了折弯处的大圆弧结构,由原本的一次折弯更改为“反向折弯-大圆弧折弯-正向折弯”的三次折弯结构,在不额外占用空间的前提下最大限度地避免了转子连接线5折弯处的应力集中,提升了它在发电机转子中的受力表现,提高了它和转子的整体可靠性。Specifically, the body of the rotor connection line optimizes the large arc structure at the bend, changing from the original one-time bend to the three-fold bend structure of "reverse bend-large arc bend-forward bend". Under the premise of not occupying additional space, the stress concentration at the bend of the
该转子连接线结构,通过“反向折弯-大圆弧折弯-正向折弯”的三次折弯设计,可以在折弯半径相同的情况下,使转子连接线折弯处7的长度变长,转子连接线折弯处7的长度越长,受到相同应力的情况下会产生相对更小的应变。将现有结构(图1)中折弯的圆弧长度和本发明结构(图2)中折弯的圆弧长度进行比对,两者圆弧长度的比值为23.5/38,可知相对于现有结构折弯处的应变,本发明中转子连接线折弯处7的折弯处的应变减小。The rotor connecting line structure, through the three-fold bending design of "reverse bending-big arc bending-forward bending", can make the length of the rotor connecting
实施例2Example 2
在实施例1的基础上,本实施例提供了一种绕线式转子,参见图4,包括转轴11、转子铁心10、转子绕组1、转子绕组支架2、转子连接线5、转子零环13、转子引出线9和转子连接线固定架3;所述转子连接线5采用如前所述的转子连接线结构;On the basis of Embodiment 1, this embodiment provides a wound rotor, as shown in FIG. 4 , including a
所述转子绕组1嵌放在转子铁心10内,并沿转轴11的轴向伸出转子铁心10的端面,且伸出部分由转子绕组支架2支撑,伸出部分通过转子连接线5与转子零环13、转子引出线9连接;所述转子绕组支架2通过其内圆与转轴11过盈配合连接,所述转子连接线固定架3及其异型补偿支撑架4均为转子绕组支架2的一部分;The rotor winding 1 is embedded in the
所述转子连接线固定架3的截面呈“D”型,其竖直侧与转子绕组支架2连接,弧形侧(靠近转子连接线侧)通过绝缘绑扎带6与转子连接线5的竖直部分绑扎固定;其中,圆弧部分有利于绝缘绑扎带6的绑扎固定,由于“D”型结构的封闭截面,避免了绝缘绑扎带6在转子连接线5受到强离心力作用时脱离转子连接线固定架3的风险;The cross-section of the rotor connecting
所述转轴11上套设有转子零环限位环12,所述转子零环13沿轴向嵌入转子零环限位环12和转轴11之间的间隙内,所述间隙内填充有绝缘块;The rotor zero ring limiting ring 12 is sleeved on the
所述转轴11上还安装有转子风扇8,所述转子风扇8位于转子引出线9的右侧;所述转子风扇8的内圆开设有用以避让转子连接线5和转轴11表面固定结构的缺口19(参见图7)。A
进一步,所述转子连接线5中的三支与转子零环13连接,另外三支与转子引出线9连接,且两者的轴向引出方向相反。Further, three of the
进一步,所述转子零环限位环12采用整圆环或整圆槽,或者采用由分段圆弧形成的圆环或圆槽。Further, the rotor zero-ring limiting ring 12 adopts a full circle or a full circle groove, or adopts a circle or a circle formed by segmented arcs.
具体地,在现有的转子结构中,转子零环13和转子引出线9相对于转子连接线5的引出方向是相同的,具体的讲:三支转子连接线5与转子零环13连接,转子零环13在轴向上靠近转子连接线5,另外三支转子连接线5与转子引出线9连接,其连接位置在轴向上位于转子零环13外侧。但在发明提供的转子结构中,转子零环13和转子引出线9相对于转子连接线5的引出方向是相反的;具体地讲:转子零环13沿轴向嵌入转子零环限位环12(或转子零环限位槽)和转轴11之间的空隙,转子零环13与转子零环限位环12(或转子零环限位槽)与转子连接线5产生的空隙由绝缘块填充,经过真空压力浸漆并烘干后的转子零环13固定结构,能获得相较于现有绕线式转子零环固定结构更高的可靠性和运行稳定性。即使转子零环13在极限工况下受到离心力作用发生形变,在转子零环限位环12(或转子零环限位槽)的限制下,转子零环13的形变也会非常有限,不至于产生裂纹甚至导致断裂等故障。Specifically, in the existing rotor structure, the rotor zero
进一步,所述转子连接线固定架3内还设置有异型补强支撑架4。Further, a special-shaped reinforcing
具体地讲,为提高转子连接线固定架3在与转子连接线5绑扎紧固并浸漆固化后,转子绕组1(线圈)和转子连接线5在转子高速旋转和转速急速变化时受到强离心力作用下的机械性能表现(包括其刚性),使其不至于被转子连接线5反复拉扯变形,能够更好地固定转子连接线5,确保转子连接线5不会因为离心力的变化而变形或断裂。为此,通过在转子连接线固定架3的外侧或内侧设有异型补强支撑架4,避免在受到强离心力及周向力时产生形变甚至断裂故障。Specifically, in order to improve the rotor connection
可选地,结合图5-6所示,异型补强支撑架4截面的基础形状近似于直角三角形,其可以被设置在转子连接线固定架3的封闭截面(有一定深度)的内侧或外侧。其结构特征为两直角边分别与转子绕组支架2、转子连接线固定架3连接,其厚度与转子连接线固定架3近似,由于三角形具有稳定性,该结构设计可有效地对转子连接线固定架3进行补强,更好地应对离心力及周向力。Optionally, as shown in FIGS. 5-6 , the basic shape of the section of the special-shaped reinforcing
优选地,为实现转子绕组支架2轻量化的设计要求,本发明的相关研发人员使用有限元仿真软件对异型补强支撑架4的受力情况进行分析、减重,将其受力较小的部分移除,最终得到的结构一个类似斜向的“工”字型的异型补强支撑架4,且该异型补强支撑架4的重量相比于轻量化之前,减重50%,但支撑强度完全能够满足支撑强度的需求。Preferably, in order to realize the lightweight design requirements of the
进一步,转子连接线固定架3的材质包括但不限于金属材料,其制造方式包括但不限于焊接、切削加工、铸造及3D打印。优选地,转子连接线固定架3的材质选用圆钢或者扁钢,折弯后焊接固定在转子绕组支架2的端面,具有制造简单、成本低、工艺性好等优点。Further, the material of the rotor connecting
进一步,结合图7所示,为实现转子风扇8的内圆靠近转子连接线5和转子引出线9部分的直角部分对转子引出线9所在的轴孔延伸出的空间进行避让,转子风扇8的内圆开设有用以避让转子连接线5和转轴11表面固定结构的缺口19。上述设计在不降低转子风扇8可靠性的前提下充分利用了发电机内部空间,关于转子风扇8的避让部分可以是整圆进行避让,也可以是仅在三处转子引出线9影响的部分进行避让。Further, as shown in FIG. 7 , in order to realize that the right-angled part of the inner circle of the
此外,本实施例还提供了风力发电机,尤其是双馈风力发电机,包括如上部分或全部所述的绕线式转子。In addition, the present embodiment also provides a wind power generator, especially a doubly-fed wind power generator, including the wound rotor described in part or all above.
在装机后对某双馈风力发电机(装有上述绕线式转子结构)严苛工况下的寿命测试,该绕线式转子具有更高地可靠性和更好地机械性能;同时,通过改进后转子风扇8的紧凑型结构,使转子风扇8到转子铁心10和转子绕组1的轴向距离被缩短,从而提高了发电机内部的空间利用率,同时对发电机转子的温升表现也有一定的改善作用。After installation, the life test of a double-fed wind turbine (equipped with the above-mentioned wound rotor structure) under severe working conditions shows that the wound rotor has higher reliability and better mechanical properties; at the same time, through the improvement The compact structure of the
以上所述仅是本发明的具体实施方式,使本领域技术人员能够理解或实现本发明。对这些实施例的多种修改对本领域的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。The above descriptions are only specific embodiments of the present invention, so that those skilled in the art can understand or implement the present 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.
应当理解的是,本发明并不局限于上述已经描述的内容,并且可以在不脱离其范围进行各种修改和改变。本发明的范围仅由所附的权利要求来限制。It should be understood that the present invention is not limited to what has been described above, and various modifications and changes can be made without departing from the scope thereof. The scope of the invention is limited only by the appended claims.
Claims (10)
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| JPH06203896A (en) * | 1992-12-29 | 1994-07-22 | Funai Electric Co Ltd | Pin structure for connector |
| CN208369344U (en) * | 2018-07-19 | 2019-01-11 | 宜兴华永电机有限公司 | A kind of leading-out wire structure of double-fed wind power generator rotor busbar |
| CN114499000A (en) * | 2021-12-30 | 2022-05-13 | 西安中车永电捷力风能有限公司 | Rotor outgoing line fixing structure of wound-rotor asynchronous motor |
| CN217769667U (en) * | 2022-06-09 | 2022-11-08 | 西安辰安电气有限公司 | Double-fed rotor lead structure device |
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2022
- 2022-12-14 CN CN202211609527.5A patent/CN116155002A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06203896A (en) * | 1992-12-29 | 1994-07-22 | Funai Electric Co Ltd | Pin structure for connector |
| CN208369344U (en) * | 2018-07-19 | 2019-01-11 | 宜兴华永电机有限公司 | A kind of leading-out wire structure of double-fed wind power generator rotor busbar |
| CN114499000A (en) * | 2021-12-30 | 2022-05-13 | 西安中车永电捷力风能有限公司 | Rotor outgoing line fixing structure of wound-rotor asynchronous motor |
| CN217769667U (en) * | 2022-06-09 | 2022-11-08 | 西安辰安电气有限公司 | Double-fed rotor lead structure device |
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