CN202094716U - Stator heat radiation structure of flywheel energy storage system and flywheel energy storage system - Google Patents

Stator heat radiation structure of flywheel energy storage system and flywheel energy storage system Download PDF

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CN202094716U
CN202094716U CN201120155638.4U CN201120155638U CN202094716U CN 202094716 U CN202094716 U CN 202094716U CN 201120155638 U CN201120155638 U CN 201120155638U CN 202094716 U CN202094716 U CN 202094716U
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stator
cooling
energy storage
storage system
flywheel energy
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方曼荻
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SHENZHEN FEINENG POWER CO Ltd
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y02E60/16Mechanical energy storage, e.g. flywheels or pressurised fluids

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Abstract

一种飞轮储能系统定子散热结构及飞轮储能系统,该散热结构包括环形扁平状定子、冷却腔、位于冷却腔中的冷却液和热传输装置,热传输装置设置在冷却腔上或设置在冷却腔中并引出冷却腔,冷却腔的侧壁包括定子的圆周面,定子位于定子圆周上的导线裸露于圆周面,与散热结构连接的结构与导线绝缘;该系统包括盘状定子、转子和壳体,定子连接在壳体内侧,转子、定子侧表面邻近,转子转动支承在壳体上。本实用新型通过设置冷却腔,通过流经冷却腔的冷却液使定子环形圆周面的裸露导线实现冷却,定子内部导线热量经导线传导至定子圆周面实现冷却,提高定子冷却效果,满足大功率飞轮储能系统定子的冷却要求;结构简单,冷却效率高。

Figure 201120155638

A flywheel energy storage system stator heat dissipation structure and a flywheel energy storage system, the heat dissipation structure includes an annular flat stator, a cooling cavity, a cooling liquid located in the cooling cavity and a heat transfer device, the heat transfer device is arranged on the cooling cavity or on the The side wall of the cooling chamber includes the circumferential surface of the stator, the wires of the stator located on the circumference of the stator are exposed on the circumferential surface, and the structure connected to the heat dissipation structure is insulated from the wires; the system includes a disc-shaped stator, a rotor and The casing and the stator are connected inside the casing, the rotor and the side surfaces of the stator are adjacent, and the rotor is rotatably supported on the casing. The utility model is provided with a cooling cavity, through which the cooling liquid flowing through the cooling cavity realizes cooling of the exposed wires on the annular peripheral surface of the stator, and the heat of the internal wires of the stator is conducted to the peripheral surface of the stator to realize cooling, thereby improving the cooling effect of the stator and satisfying the requirements of high-power flywheels. The cooling requirements of the stator of the energy storage system; the structure is simple and the cooling efficiency is high.

Figure 201120155638

Description

一种飞轮储能系统定子散热结构及飞轮储能系统A stator heat dissipation structure of a flywheel energy storage system and a flywheel energy storage system

技术领域 technical field

本实用新型涉及一种储能系统定子散热结构,还涉及一种储能系统,具体涉及一种飞轮储能系统定子散热结构及应用此结构的飞轮储能系统。The utility model relates to a stator heat dissipation structure of an energy storage system, and also relates to an energy storage system, in particular to a stator heat dissipation structure of a flywheel energy storage system and a flywheel energy storage system using the structure.

背景技术 Background technique

飞轮储能系统是采用飞轮电机对机械能和电能自由转换的特点、对系统能量进行储存的常用系统。如单转子单定子盘式永磁电机、双转子单定子盘式永磁电机等,具有定子无铁芯、无铁磁损耗、效率高等优点。The flywheel energy storage system is a common system that uses the characteristics of the flywheel motor to freely convert mechanical energy and electrical energy to store system energy. Such as single-rotor single-stator disc permanent magnet motor, double-rotor single-stator disc permanent magnet motor, etc., which have the advantages of no iron core in the stator, no ferromagnetic loss, and high efficiency.

但是,在一些飞轮储能系统如双转子单定子盘式永磁电机结构中,由于定子盘紧紧夹在两个转子盘中间,间隙很小,对流传热极不方便,特别是在盘式飞轮电池中,由于通常将电池壳体内抽成真空,完全没有对流散热,定子散热条件更加困难。However, in some flywheel energy storage systems such as double-rotor single-stator disc permanent magnet motor structure, since the stator disc is tightly clamped between the two rotor discs, the gap is very small, and the convective heat transfer is extremely inconvenient, especially in the disc type In the flywheel battery, since the inside of the battery case is usually evacuated, there is no convection heat dissipation at all, and the heat dissipation conditions of the stator are more difficult.

如图1所示,定子盘10的中部9是电磁作用区域,该区域除铜导线外,不能放置其他任何导电物质。所以,定子盘10通常是用环氧树脂作为基体,将铜导线全部封死固定,形成一个薄盘。由于环氧树脂热导率极低,只有0.2W/(m*K),所以其传热能力极低。As shown in FIG. 1 , the middle part 9 of the stator disk 10 is an electromagnetic action area, and no other conductive substances can be placed in this area except copper wires. Therefore, the stator disk 10 is usually made of epoxy resin as a matrix, and all the copper wires are sealed and fixed to form a thin disk. Due to the extremely low thermal conductivity of epoxy resin, only 0.2W/(m*K), its heat transfer capacity is extremely low.

为了提高飞轮储能系统定子的散热能力,一般采用往环氧树脂中加入氮化铝等导热绝缘粉末的办法,提高环氧树脂基体的热导率。In order to improve the heat dissipation capacity of the stator of the flywheel energy storage system, the method of adding heat-conducting insulating powder such as aluminum nitride to the epoxy resin is generally used to improve the thermal conductivity of the epoxy resin matrix.

但是,现有飞轮储能系统的定子散热结构仍存在如下缺陷:However, the stator heat dissipation structure of the existing flywheel energy storage system still has the following defects:

1、环氧树脂添加氮化铝等导热绝缘粉末后,热导率提高有限,只能从0.2W/(m*K)提高到2W/(m*K)左右,仍然不能满足大功率飞轮储能系统定子的散热要求;1. After the epoxy resin is added with aluminum nitride and other heat-conducting insulating powders, the thermal conductivity can only be increased from 0.2W/(m*K) to about 2W/(m*K), which still cannot meet the needs of high-power flywheel storage. Heat dissipation requirements of the energy system stator;

2、环氧树脂添加导热绝缘粉工艺比较复杂,很难混合均匀,导致环氧树脂热传导能力不均匀,难以保证飞轮储能系统定子可靠散热。2. The process of adding thermally conductive insulating powder to epoxy resin is relatively complicated, and it is difficult to mix evenly, resulting in uneven thermal conductivity of epoxy resin, and it is difficult to ensure reliable heat dissipation of the stator of the flywheel energy storage system.

实用新型内容 Utility model content

本实用新型要解决的技术问题之一是,提供一种飞轮储能系统定子散热结构,解决现有飞轮储能系统定子散热困难、不能满足大功率飞轮储能系统定子散热要求的缺陷。One of the technical problems to be solved by the utility model is to provide a stator heat dissipation structure of the flywheel energy storage system, which solves the defects that the stator heat dissipation of the existing flywheel energy storage system is difficult and cannot meet the stator heat dissipation requirements of the high-power flywheel energy storage system.

本实用新型要解决的技术问题之二是,提供一种飞轮储能系统,解决现有飞轮储能系统定子散热困难、不能满足大功率飞轮储能系统定子散热要求的缺陷。The second technical problem to be solved by the utility model is to provide a flywheel energy storage system, which solves the defects that the stator of the existing flywheel energy storage system is difficult to dissipate heat and cannot meet the heat dissipation requirements of the stator of the high-power flywheel energy storage system.

本实用新型解决其技术问题之一所采用的技术方案是:构造一种飞轮储能系统定子散热结构,其特征在于,包括环形扁平状定子、冷却腔、位于该冷却腔中的冷却液和热传输装置,该热传输装置设置在该冷却腔上或设置在该冷却腔中并引出该冷却腔,所述冷却腔的侧壁包括所述定子的圆周面,所述定子位于定子圆周上的导线裸露于该圆周面,与所述散热结构连接的结构与所述导线绝缘。The technical solution adopted by the utility model to solve one of its technical problems is to construct a stator heat dissipation structure of the flywheel energy storage system, which is characterized in that it includes an annular flat stator, a cooling cavity, a cooling liquid and a heat sink located in the cooling cavity A transmission device, the heat transmission device is arranged on or in the cooling cavity and leads out of the cooling cavity, the side wall of the cooling cavity includes the circumferential surface of the stator, and the stator is located on the wire on the circumference of the stator Exposed on the circumferential surface, the structure connected to the heat dissipation structure is insulated from the wire.

在本实用新型的飞轮储能系统定子散热结构中,所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的冷却管和位于该冷却管中的流动的冷却液A;In the stator heat dissipation structure of the flywheel energy storage system of the present invention, the heat transfer device includes a cooling pipe arranged in the cooling cavity and leading out of the cooling cavity, and a flowing cooling liquid A located in the cooling tube;

或所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的导热体。Or the heat transfer device includes a heat conductor arranged in the cooling cavity and leading out of the cooling cavity.

在本实用新型的飞轮储能系统定子散热结构中,所述热传输装置包括连接在所述冷却腔上的进液管和出液管,所述冷却液为绝缘冷却液。In the heat dissipation structure of the stator of the flywheel energy storage system of the present utility model, the heat transfer device includes a liquid inlet pipe and a liquid outlet pipe connected to the cooling cavity, and the cooling liquid is an insulating cooling liquid.

在本实用新型的飞轮储能系统定子散热结构中,所述冷却腔按如下结构构成:所述散热结构包括设置在飞轮储能系统壳体内表面对应于所述定子安装位置并与所述定子的圆周顶面相间隔的环形凸台、对应于该环形凸台和所述定子的环形板A和环形板B,所述环形板A和环形板B对应密封连接在所述环形凸台和所述定子的两侧表面构成冷却腔,所述环形凸台与所述定子之间绝缘。In the heat dissipation structure of the stator of the flywheel energy storage system of the present invention, the cooling cavity is constituted according to the following structure: the heat dissipation structure includes an inner surface of the housing of the flywheel energy storage system corresponding to the installation position of the stator and connected to the stator. An annular boss at intervals on the top surface of the circumference, an annular plate A and an annular plate B corresponding to the annular boss and the stator, and the annular plate A and the annular plate B are correspondingly sealed and connected between the annular boss and the stator The two side surfaces of the ring form a cooling cavity, and the annular boss is insulated from the stator.

在本实用新型的飞轮储能系统定子散热结构中,所述进液管和出液管设置在所述飞轮储能系统壳体侧壁对应于所述环形凸台的位置或者经所属定子的环形板由系统壳体的上下端盖引出。In the heat dissipation structure of the stator of the flywheel energy storage system of the present invention, the liquid inlet pipe and the liquid outlet pipe are arranged on the side wall of the flywheel energy storage system shell corresponding to the position of the annular boss or pass through the ring of the stator. The board is led out from the upper and lower end covers of the system housing.

本实用新型解决其技术问题之二所采用的技术方案是:构造一种飞轮储能系统,包括环形扁平状定子、盘状转子和壳体,所述定子连接在所述壳体内侧,所述转子侧表面与所述定子侧表面邻近,所述转子转动支承在所述壳体上,其特征在于,包括定子散热结构,该定子散热结构包括环形扁平状定子、冷却腔、位于该冷却腔中的冷却液和热传输装置,该热传输装置设置在该冷却腔上或设置在该冷却腔中的并引出该冷却腔,所述冷却腔的侧壁包括所述定子的圆周面,所述定子位于定子圆周上的导线裸露于该圆周面,与所述散热结构连接的结构与所述导线绝缘,所述定子经所述冷却腔构件连接在所述壳体上,该定子与所述壳体之间绝缘。The technical solution adopted by the utility model to solve the second technical problem is: to construct a flywheel energy storage system, including an annular flat stator, a disk-shaped rotor and a housing, the stator is connected to the inside of the housing, and the The side surface of the rotor is adjacent to the side surface of the stator, the rotor is rotatably supported on the housing, and it is characterized in that it includes a stator heat dissipation structure, and the stator heat dissipation structure includes an annular flat stator, a cooling cavity, and is located in the cooling cavity The cooling liquid and the heat transmission device, the heat transmission device is arranged on or in the cooling cavity and leads out of the cooling cavity, the side wall of the cooling cavity includes the circumferential surface of the stator, and the stator The wires located on the circumference of the stator are exposed on the circumference, and the structure connected to the heat dissipation structure is insulated from the wires. The stator is connected to the housing through the cooling chamber component, and the stator is connected to the housing. insulated.

在本实用新型的飞轮储能系统中,所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的冷却管和位于该冷却管中的流动冷却液;In the flywheel energy storage system of the present utility model, the heat transfer device includes a cooling pipe arranged in the cooling chamber and leading out of the cooling chamber and a flowing cooling liquid located in the cooling pipe;

或所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的导热体。Or the heat transfer device includes a heat conductor arranged in the cooling cavity and leading out of the cooling cavity.

在本实用新型的飞轮储能系统中,所述热传输装置包括连接在所述冷却腔上的进液管和出液管,所述冷却液为绝缘冷却液。In the flywheel energy storage system of the present invention, the heat transfer device includes a liquid inlet pipe and a liquid outlet pipe connected to the cooling chamber, and the cooling liquid is insulating cooling liquid.

在本实用新型的飞轮储能系统中,所述冷却腔按如下结构构成:所述散热结构包括设置在壳体内表面对应于所述定子安装位置并与所述定子的圆周顶面相间隔的环形凸台、对应于该环形凸台和所述定子的环形板A和环形板B,所述环形板A和环形板B对应密封连接在所述环形凸台和所述定子的两侧表面构成冷却腔,所述环形凸台与所述定子之间绝缘。In the flywheel energy storage system of the present utility model, the cooling cavity is structured as follows: the heat dissipation structure includes an annular protrusion arranged on the inner surface of the housing corresponding to the installation position of the stator and spaced from the circumferential top surface of the stator. Platform, corresponding to the annular boss and the annular plate A and the annular plate B of the stator, the annular plate A and the annular plate B are correspondingly sealed and connected to the two side surfaces of the annular boss and the stator to form a cooling chamber , there is insulation between the annular boss and the stator.

在本实用新型的飞轮储能系统中,所述进液管和出液管设置在所述壳体侧壁对应于所述环形凸台的位置或者经所属定子的环形板由系统壳体的上下端盖引出。In the flywheel energy storage system of the present utility model, the liquid inlet pipe and the liquid outlet pipe are arranged on the side wall of the housing corresponding to the position of the annular boss or from the upper and lower sides of the system housing through the annular plate of the stator. end cap out.

实施本实用新型的飞轮储能系统定子散热结构及飞轮储能系统,与现有技术比较,其有益效果是:Compared with the prior art, the stator cooling structure of the flywheel energy storage system and the flywheel energy storage system implementing the utility model have beneficial effects as follows:

1.通过设置冷却腔使冷却液与定子圆周面的裸露导线表面接触实现导热,再通过冷却装置使冷却腔内的液体冷却液实现对定子圆周面的裸露导线的冷却,定子内部导线的热量经导线传导与冷却液热交换实现冷却,大大提高定子的冷却效果,满足大功率飞轮储能系统定子的冷却要求;1. By setting the cooling chamber to make the cooling liquid contact with the surface of the exposed wires on the circumferential surface of the stator to conduct heat conduction, and then through the cooling device, the liquid cooling liquid in the cooling chamber can cool the exposed wires on the circumferential surface of the stator. The heat of the internal wires of the stator is passed through Wire conduction and coolant heat exchange to achieve cooling, greatly improving the cooling effect of the stator, and meeting the cooling requirements of the stator of the high-power flywheel energy storage system;

2.结构简单,冷却效率高;2. Simple structure and high cooling efficiency;

3.安装简单,成本低。3. Simple installation and low cost.

附图说明Description of drawings

下面将结合附图及实施例对本实用新型作进一步说明,附图中:The utility model will be further described below in conjunction with accompanying drawing and embodiment, in the accompanying drawing:

图1是本实用新型飞轮储能系统定子散热结构中定子的结构剖面图。Fig. 1 is a structural sectional view of the stator in the stator cooling structure of the flywheel energy storage system of the present invention.

图2是本实用新型飞轮储能系统一种实施例的剖视图。Fig. 2 is a sectional view of an embodiment of the flywheel energy storage system of the present invention.

图3是图2中A部放大图。Fig. 3 is an enlarged view of part A in Fig. 2 .

图4是本实用新型飞轮储能系统另一种实施例的剖视图。Fig. 4 is a cross-sectional view of another embodiment of the flywheel energy storage system of the present invention.

图5是本实用新型飞轮储能系统另一种实施例的剖视图。Fig. 5 is a cross-sectional view of another embodiment of the flywheel energy storage system of the present invention.

图6是本实用新型飞轮储能系统另一种实施例的剖视图。Fig. 6 is a cross-sectional view of another embodiment of the flywheel energy storage system of the present invention.

具体实施方式 Detailed ways

如图1、图2、图3所示,本实用新型的飞轮储能系统定子散热结构包括环形扁平状定子10、冷却腔40、位于该冷却腔中的冷却液(图中未示出)和热传输装置,热传输装置设置在冷却腔40上或设置在冷却腔40中的并引出该冷却腔40。冷却腔40的侧壁包括定子10的圆周面11(冷却腔40可以包括定子10的全部圆周面11,也可以仅包括定子10的部分圆周定子圆周面的裸露导线11),定子10在定子圆周上的导线裸露于该圆周面11。与飞轮储能系统定子散热结构连接的结构与定子的导线绝缘。As shown in Fig. 1, Fig. 2 and Fig. 3, the stator heat dissipation structure of the flywheel energy storage system of the present invention includes an annular flat stator 10, a cooling chamber 40, a cooling liquid (not shown in the figure) located in the cooling chamber and The heat transport device is arranged on or in the cooling cavity 40 and leads out of the cooling cavity 40 . The sidewall of cooling cavity 40 comprises the circumferential surface 11 of stator 10 (cooling cavity 40 can comprise the whole circumferential surface 11 of stator 10, also can only comprise the exposed wire 11 of stator circumferential surface of partial circumference of stator 10), and stator 10 is in stator circumferential surface The wires above are exposed on the peripheral surface 11. The structure connected with the heat dissipation structure of the stator of the flywheel energy storage system is insulated from the wires of the stator.

在本实施例中,热传输装置采用如下结构,并实现与飞轮储能系统定子散热结构连接的结构与定子的导线绝缘:热传输装置包括连接在冷却腔40上的进液管70和出液管80(如图4所示),冷却液采用绝缘冷却液。In this embodiment, the heat transmission device adopts the following structure, and the structure connected to the heat dissipation structure of the stator of the flywheel energy storage system is insulated from the wires of the stator: the heat transmission device includes a liquid inlet pipe 70 connected to the cooling cavity 40 and a liquid outlet pipe Pipe 80 (as shown in FIG. 4 ), the cooling liquid adopts insulating cooling liquid.

在其他实施例中,热传输装置可以采用包括但不限于如下结构,并实现与飞轮储能系统定子散热结构连接的结构与定子的导线绝缘:In other embodiments, the heat transmission device may adopt a structure including but not limited to the following, and realize the insulation between the structure connected to the heat dissipation structure of the stator of the flywheel energy storage system and the wires of the stator:

1、如图5所示,热传输装置包括设置在冷却腔中并引出冷却腔的冷却管90和位于该冷却管90中的流动的第二冷却液。实现与飞轮储能系统定子散热结构连接的结构与定子的导线绝缘可采用:冷却腔中的冷却液采用绝缘冷却液,冷却管90与导线相绝缘;或冷却管90采用导热绝缘材料制成;或第二冷却液采用绝缘冷却液,冷却管90与外部结构绝缘连接等。1. As shown in FIG. 5 , the heat transfer device includes a cooling pipe 90 arranged in the cooling chamber and leading out of the cooling chamber, and a second cooling liquid flowing in the cooling pipe 90 . The insulation between the structure connected to the heat dissipation structure of the stator of the flywheel energy storage system and the wires of the stator can be insulated: the cooling liquid in the cooling chamber is an insulating cooling liquid, and the cooling pipe 90 is insulated from the wires; or the cooling pipe 90 is made of thermally conductive insulating material; Or the second cooling liquid is an insulating cooling liquid, and the cooling pipe 90 is insulated and connected to the external structure.

2、热传输装置包括设置在冷却腔中并引出该冷却腔的导热体,实现与飞轮储能系统定子散热结构连接的结构与定子的导线绝缘可采用:导热体与定子的导线相绝缘,冷却腔中的冷却液采用绝缘冷却液;或导热体采用导热绝缘材料制成等。2. The heat transmission device includes a heat conductor arranged in the cooling chamber and leading out of the cooling chamber. The structure connected to the heat dissipation structure of the stator of the flywheel energy storage system and the wire insulation of the stator can be used: the heat conductor is insulated from the wires of the stator, and the cooling The cooling liquid in the cavity is made of insulating cooling liquid; or the heat conductor is made of heat-conducting insulating material, etc.

在本实施例中,冷却腔40采用如下结构构成:散热结构包括设置在飞轮储能系统壳体30内表面的环形凸台31、环形板50和环形板60,该环形凸台31对应于定子10的安装位置并与定子10的圆周顶面11相间隔(为了增大冷却腔40的容积,提高散热效率,在环形凸台31上设置凹槽),环形板50和环形板60对应与环形凸台31和定子10的侧表面配合,通过密封槽51、61内的密封材料密封连接在环形凸台31和定子10的两侧表面构成冷却腔40,环形凸台31与定子10之间绝缘(可采用绝缘材料制作环形板50和环形板60实现绝缘,也可以采用通过密封槽51、61内的绝缘密封材料实现绝缘)。In the present embodiment, the cooling cavity 40 adopts the following structure: the heat dissipation structure includes an annular boss 31, an annular plate 50 and an annular plate 60 arranged on the inner surface of the flywheel energy storage system housing 30, and the annular boss 31 corresponds to the stator 10 and spaced from the circumferential top surface 11 of the stator 10 (in order to increase the volume of the cooling cavity 40 and improve the heat dissipation efficiency, a groove is provided on the annular boss 31), the annular plate 50 and the annular plate 60 correspond to the annular The boss 31 cooperates with the side surface of the stator 10, and the sealing material in the sealing groove 51, 61 is sealed and connected to form a cooling chamber 40 on both sides of the annular boss 31 and the stator 10, and the annular boss 31 is insulated from the stator 10. (The annular plate 50 and the annular plate 60 can be made of insulating material to realize insulation, and the insulating sealing material in the sealing grooves 51, 61 can also be used to realize insulation).

在其他实施例中,冷却腔40可以采用其他结构构成,如采用两侧与定子10的两侧表面密封连接的环形密封套,定子10与密封套密封连接后,再经密封套绝缘连接在飞轮储能系统壳体30的内表面等。In other embodiments, the cooling chamber 40 can be constructed with other structures, such as an annular sealing sleeve whose two sides are sealed with the surfaces of both sides of the stator 10. After the stator 10 is sealed with the sealing sleeve, it is then insulated and connected to the flywheel The inner surface of the energy storage system casing 30 and the like.

进液管和出液管可以设置在飞轮储能系统壳体侧壁上对应于环形凸台31的位置,也可以根据结构需要设置在飞轮储能系统壳体的其他位置,如将进液管和出液管设置在环形板50和环形板60上,由飞轮储能系统壳体的上下侧壁引出,也能够实现本发明目的。The liquid inlet pipe and the liquid outlet pipe can be arranged on the side wall of the flywheel energy storage system shell corresponding to the position of the annular boss 31, and can also be arranged at other positions of the flywheel energy storage system shell according to the structural requirements, such as the liquid inlet pipe And the liquid outlet pipe is arranged on the annular plate 50 and the annular plate 60, and is led out from the upper and lower side walls of the housing of the flywheel energy storage system, which can also achieve the purpose of the present invention.

本实用新型的飞轮储能系统包括环形扁平状定子、盘状转子和壳体,定子连接在壳体内侧,转子侧表面与定子侧表面邻近安装,转子转动支承在壳体上。定子采用上述散热结构进行散热,结构如上述。定子经散热结构的冷却腔构件连接在壳体上,且保证定子与壳体之间绝缘。The flywheel energy storage system of the utility model includes an annular flat stator, a disk-shaped rotor and a casing, the stator is connected inside the casing, the side surface of the rotor is installed adjacent to the side surface of the stator, and the rotor is rotatably supported on the casing. The stator adopts the above heat dissipation structure for heat dissipation, and the structure is as above. The stator is connected to the casing through the cooling cavity component of the heat dissipation structure, and the insulation between the stator and the casing is ensured.

如图2所示,本实施例的飞轮储能系统包括一个环形扁平状定子10、两个盘状转子20和电机壳体30,定子10经散热结构的冷却腔构件连接在该电机壳体30的内侧,转子20位于定子10的两侧转动支承在壳体30上。As shown in Figure 2, the flywheel energy storage system of this embodiment includes an annular flat stator 10, two disc rotors 20 and a motor housing 30, the stator 10 is connected to the motor housing through a cooling cavity member of a heat dissipation structure Inside the body 30 , the rotor 20 is located on both sides of the stator 10 and rotatably supported on the housing 30 .

在其他实施例中,定子和转子的数量可以根据需要设置,如可以采用一个环形扁平状定子、一个盘状转子的结构,也可以采用两个环形扁平状定子、三个盘状转子的结构等,均能够实现本发明目的。In other embodiments, the number of stators and rotors can be set according to needs, such as the structure of one annular flat stator and one disc rotor, or the structure of two annular flat stators and three disc rotors, etc. , can realize the object of the present invention.

图6是运用本实用新型的飞轮储能系统定子散热结构的飞轮电机的一种实施方式。Fig. 6 is an embodiment of the flywheel motor using the stator cooling structure of the flywheel energy storage system of the present invention.

Claims (10)

1.一种飞轮储能系统定子散热结构,其特征在于,包括环形扁平状定子、冷却腔、位于该冷却腔中的冷却液和热传输装置,该热传输装置设置在该冷却腔上或设置在该冷却腔中并引出该冷却腔,所述冷却腔的侧壁包括所述定子的圆周面,所述定子位于定子圆周上的导线裸露于该圆周面,与所述散热结构连接的结构与所述导线绝缘。1. A heat dissipation structure for a stator of a flywheel energy storage system, characterized in that it comprises an annular flat stator, a cooling chamber, a cooling liquid located in the cooling chamber and a heat transfer device, and the heat transfer device is arranged on the cooling chamber or provided In the cooling cavity and leading out of the cooling cavity, the side wall of the cooling cavity includes the circumferential surface of the stator, the wires of the stator located on the circumference of the stator are exposed on the circumferential surface, and the structure connected to the heat dissipation structure and The wires are insulated. 2.如权利要求1所述的飞轮储能系统定子散热结构,其特征在于,所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的冷却管和位于该冷却管中的流动的冷却液A;2. The heat dissipation structure of the stator of the flywheel energy storage system according to claim 1, wherein the heat transfer device includes a cooling pipe arranged in the cooling cavity and leading out of the cooling cavity, and a flow in the cooling tube coolant A; 或所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的导热体。Or the heat transfer device includes a heat conductor arranged in the cooling cavity and leading out of the cooling cavity. 3.如权利要求1所述的飞轮储能系统定子散热结构,其特征在于,所述热传输装置包括连接在所述冷却腔上的进液管和出液管,所述冷却液为绝缘冷却液。3. The stator heat dissipation structure of the flywheel energy storage system according to claim 1, wherein the heat transfer device includes a liquid inlet pipe and a liquid outlet pipe connected to the cooling cavity, and the cooling liquid is an insulating cooling liquid. 4.如权利要求3所述的飞轮储能系统定子散热结构,其特征在于,所述冷却腔按如下结构构成:所述散热结构包括设置在飞轮储能系统壳体内表面对应于所述定子安装位置并与所述定子的圆周顶面相间隔的环形凸台、对应于该环形凸台和所述定子的环形板A和环形板B,所述环形板A和环形板B对应密封连接在所述环形凸台和所述定子的两侧表面构成冷却腔,所述环形凸台与所述定子之间绝缘。4. The heat dissipation structure of the stator of the flywheel energy storage system according to claim 3, wherein the cooling cavity is configured as follows: the heat dissipation structure includes a cooling chamber arranged on the inner surface of the flywheel energy storage system housing corresponding to the installation of the stator. An annular boss at a position and spaced from the circumferential top surface of the stator, an annular plate A and an annular plate B corresponding to the annular boss and the stator, and the annular plate A and the annular plate B are correspondingly sealed and connected to the The annular boss and the two side surfaces of the stator form a cooling cavity, and the annular boss is insulated from the stator. 5.如权利要求4所述的飞轮储能系统定子散热结构,其特征在于,所述进液管和出液管设置在所述飞轮储能系统壳体侧壁对应于所述环形凸台的位置或者经所属定子的环形板由系统壳体的上下端盖引出。5. The stator heat dissipation structure of the flywheel energy storage system according to claim 4, wherein the liquid inlet pipe and the liquid outlet pipe are arranged on the side wall of the flywheel energy storage system housing corresponding to the annular boss. The position or via the ring plate of the associated stator leads from the upper and lower end shields of the system housing. 6.一种飞轮储能系统,包括环形扁平状定子、盘状转子和壳体,所述定子连接在所述壳体内侧,所述转子侧表面与所述定子侧表面邻近,所述转子转动支承在所述壳体上,其特征在于,包括定子散热结构,该定子散热结构包括环形扁平状定子、冷却腔、位于该冷却腔中的冷却液和热传输装置,该热传输装置设置在该冷却腔上或设置在该冷却腔中的并引出该冷却腔,所述冷却腔的侧壁包括所述定子的圆周面,所述定子位于定子圆周上的导线裸露于该圆周面,与所述散热结构连接的结构与所述导线绝缘,所述定子经所述冷却腔构件连接在所述壳体上,该定子与所述壳体之间绝缘。6. A flywheel energy storage system, comprising an annular flat stator, a disc-shaped rotor and a casing, the stator is connected inside the casing, the side surface of the rotor is adjacent to the side surface of the stator, and the rotor rotates Supported on the housing, it is characterized in that it includes a stator heat dissipation structure, and the stator heat dissipation structure includes an annular flat stator, a cooling cavity, a cooling liquid located in the cooling cavity, and a heat transfer device, and the heat transfer device is arranged on the The cooling cavity is provided on or in the cooling cavity and leads out of the cooling cavity, the side wall of the cooling cavity includes the circumferential surface of the stator, the wires of the stator located on the circumference of the stator are exposed on the circumferential surface, and the The structure connected to the heat dissipation structure is insulated from the wires, the stator is connected to the casing through the cooling chamber component, and the stator is insulated from the casing. 7.如权利要求6所述的飞轮储能系统,其特征在于,所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的冷却管和位于该冷却管中的流动冷却液;7. The flywheel energy storage system according to claim 6, wherein the heat transfer device comprises a cooling pipe arranged in the cooling chamber and leading out of the cooling chamber, and a flowing cooling liquid located in the cooling pipe; 或所述热传输装置包括设置在所述冷却腔中并引出该冷却腔的导热体。Or the heat transfer device includes a heat conductor arranged in the cooling cavity and leading out of the cooling cavity. 8.如权利要求6所述的飞轮储能系统,其特征在于,所述热传输装置包括连接在所述冷却腔上的进液管和出液管,所述冷却液为绝缘冷却液。8. The flywheel energy storage system according to claim 6, wherein the heat transfer device comprises a liquid inlet pipe and a liquid outlet pipe connected to the cooling cavity, and the cooling liquid is insulating cooling liquid. 9.如权利要求8所述的飞轮储能系统,其特征在于,所述冷却腔按如下结构构成:所述散热结构包括设置在壳体内表面对应于所述定子安装位置并与所述定子的圆周顶面相间隔的环形凸台、对应于该环形凸台和所述定子的环形板A和环形板B,所述环形板A和环形板B对应密封连接在所述环形凸台和所述定子的两侧表面构成冷却腔,所述环形凸台与所述定子之间绝缘。9. The flywheel energy storage system according to claim 8, characterized in that, the cooling cavity is configured as follows: the heat dissipation structure includes a motor that is arranged on the inner surface of the housing corresponding to the installation position of the stator and is connected to the stator. An annular boss at intervals on the top surface of the circumference, an annular plate A and an annular plate B corresponding to the annular boss and the stator, and the annular plate A and the annular plate B are correspondingly sealed and connected between the annular boss and the stator The two side surfaces of the ring form a cooling cavity, and the annular boss is insulated from the stator. 10.如权利要求9所述的飞轮储能系统,其特征在于,所述进液管和出液管设置在所述壳体侧壁对应于所述环形凸台的位置或者经所属定子的环形板由系统壳体的上下端盖引出。10. The flywheel energy storage system according to claim 9, characterized in that, the liquid inlet pipe and the liquid outlet pipe are arranged on the side wall of the housing corresponding to the position of the annular boss or pass through the ring of the associated stator. The board is led out from the upper and lower end covers of the system housing.
CN201120155638.4U 2011-05-16 2011-05-16 Stator heat radiation structure of flywheel energy storage system and flywheel energy storage system Expired - Fee Related CN202094716U (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107196452A (en) * 2012-04-03 2017-09-22 波音公司 Open-core flywheel construction
CN111835153A (en) * 2019-04-23 2020-10-27 擎声自动化科技(上海)有限公司 Motor with PCB stator
CN113497517A (en) * 2021-09-08 2021-10-12 沈阳微控新能源技术有限公司 Flywheel energy storage system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107196452A (en) * 2012-04-03 2017-09-22 波音公司 Open-core flywheel construction
CN107196452B (en) * 2012-04-03 2019-05-21 波音公司 Open-core flywheel construction
US10826348B2 (en) 2012-04-03 2020-11-03 The Boeing Company Open-core flywheel architecture
US11070107B2 (en) 2012-04-03 2021-07-20 The Boeing Company Open-core flywheel architecture
CN111835153A (en) * 2019-04-23 2020-10-27 擎声自动化科技(上海)有限公司 Motor with PCB stator
CN111835153B (en) * 2019-04-23 2023-05-26 擎声自动化科技(上海)有限公司 Motor with PCB stator
CN113497517A (en) * 2021-09-08 2021-10-12 沈阳微控新能源技术有限公司 Flywheel energy storage system
CN113497517B (en) * 2021-09-08 2021-12-17 沈阳微控新能源技术有限公司 Flywheel energy storage system

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