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CN116317302A - A cooling structure for magnetic levitation centrifugal compressor motor - Google Patents

A cooling structure for magnetic levitation centrifugal compressor motor Download PDF

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Publication number
CN116317302A
CN116317302A CN202310183178.3A CN202310183178A CN116317302A CN 116317302 A CN116317302 A CN 116317302A CN 202310183178 A CN202310183178 A CN 202310183178A CN 116317302 A CN116317302 A CN 116317302A
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heat dissipation
cooling
motor
stator
cooling structure
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CN116317302B (en
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钟仁志
袁军
项懂欣
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Xinlei Compressor Co Ltd
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Xinlei Compressor Co Ltd
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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/20Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
    • H02K5/207Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium with openings in the casing specially adapted for ambient air
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/16Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
    • H02K5/163Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields radially supporting the rotary shaft at only one end of the rotor
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/20Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
    • H02K5/203Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium specially adapted for liquids, e.g. cooling jackets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/08Structural association with bearings
    • H02K7/09Structural association with bearings with magnetic bearings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K9/00Arrangements for cooling or ventilating
    • H02K9/02Arrangements for cooling or ventilating by ambient air flowing through the machine
    • H02K9/04Arrangements for cooling or ventilating by ambient air flowing through the machine having means for generating a flow of cooling medium
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K9/00Arrangements for cooling or ventilating
    • H02K9/19Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil
    • 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
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K2205/00Specific aspects not provided for in the other groups of this subclass relating to casings, enclosures, supports
    • H02K2205/03Machines characterised by thrust bearings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K2205/00Specific aspects not provided for in the other groups of this subclass relating to casings, enclosures, supports
    • H02K2205/09Machines characterised by drain passages or by venting, breathing or pressure compensating means
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/64Electric machine technologies in electromobility

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Motor Or Generator Cooling System (AREA)

Abstract

本发明公开了一种磁悬浮离心式压缩机电机的冷却结构,电机包括依次套设的转子、定子和外壳,转子和定子之间分隔设有散热间隙;定子固定在外壳的内壁上,定子两端均设有连通散热间隙的散热区,外壳上固定设有连通散热区的进风口和出风口;外壳内设有水冷流道,外壳上固定设有连通水冷流道的进水口和出水口。本发明的好处是风冷和水冷两种冷却方式结合共同散热,提高磁悬浮电机的冷却效率;能够完成电机内部推力轴承和磁悬浮轴承的散热,散热效率强。

Figure 202310183178

The invention discloses a cooling structure for a magnetic levitation centrifugal compressor motor. The motor includes a rotor, a stator, and a casing that are sheathed in sequence. A heat dissipation gap is arranged between the rotor and the stator; the stator is fixed on the inner wall of the casing, and the All are provided with a heat dissipation area connected to the heat dissipation gap, and an air inlet and an air outlet connected to the heat dissipation area are fixedly provided on the casing; a water cooling flow channel is provided inside the casing, and a water inlet and a water outlet connected to the water cooling flow path are fixedly provided on the casing. The advantage of the present invention is that the two cooling modes of air cooling and water cooling are combined to dissipate heat together to improve the cooling efficiency of the magnetic levitation motor; the heat dissipation of the thrust bearing and the magnetic levitation bearing inside the motor can be completed, and the heat dissipation efficiency is strong.

Figure 202310183178

Description

一种磁悬浮离心式压缩机电机的冷却结构A cooling structure for magnetic levitation centrifugal compressor motor

技术领域technical field

本发明涉及磁悬浮电机技术领域,尤其是一种磁悬浮离心式压缩机电机的冷却结构。The invention relates to the technical field of magnetic levitation motors, in particular to a cooling structure for a magnetic levitation centrifugal compressor motor.

背景技术Background technique

磁悬浮高速电机已成为国际电工领域研究的热点之一,主要结构是鼓风机叶轮直接安装在点击轴延伸端上,而转子被垂直悬浮于主动式磁性轴承上,实现由高速电机直接驱动。使用磁悬浮电机驱动压缩机-膨胀机机组可有效提升系统性能,而磁悬浮电机的冷却方式直接决定电机是否能够稳定安全运行。由于磁悬浮电机的转速非常高,在运行过程中,需要通过冷却带走电机损耗产生的热量,否则容易影响电机的正常运行。The magnetic levitation high-speed motor has become one of the hotspots in the field of international electrotechnical research. The main structure is that the blower impeller is directly installed on the extension end of the click shaft, and the rotor is vertically suspended on the active magnetic bearing to be directly driven by the high-speed motor. Using the magnetic levitation motor to drive the compressor-expander unit can effectively improve the system performance, and the cooling method of the magnetic levitation motor directly determines whether the motor can run stably and safely. Because the speed of the magnetic levitation motor is very high, it is necessary to take away the heat generated by the loss of the motor through cooling during operation, otherwise it will easily affect the normal operation of the motor.

现有技术中通常至采用风冷或水冷的一种来实现磁悬浮离心式压缩机电机的冷却。对于风冷和水冷模式的选择,我司进行了如下的研究。In the prior art, one of air cooling or water cooling is usually used to realize the cooling of the magnetic levitation centrifugal compressor motor. For the selection of air-cooled and water-cooled modes, our company has conducted the following research.

中国专利文献中,专利号为CN202121792227.6于2022年2月18日授权公告的一种兼容水冷和风冷系统的磁悬浮电机外壳和电机,该申请在机壳上设置水冷通道,在第一轴承座和第二轴承座上设置风冷用的盲孔气孔,该申请的目的是做风冷应用时,盲孔气孔打通,能够导入冷却风,在进行水冷应用时,盲孔气孔不打通,呈封闭状态,配合水冷通道完成电机水冷。In the Chinese patent literature, the patent number is CN202121792227.6, which was authorized and announced on February 18, 2022. It is a magnetic levitation motor shell and motor compatible with water-cooling and air-cooling systems. Blind holes for air cooling are set on the bearing seat and the second bearing seat. The purpose of this application is that the air holes in the blind holes can be opened for the introduction of cooling air in the application of air cooling. In the closed state, the water cooling of the motor is completed with the water cooling channel.

现有技术虽然实现了水冷或风冷的应用,但是实际冷却过程中只能应用一种冷却方式,冷却效率还是较为不足。Although the prior art realizes the application of water cooling or air cooling, only one cooling method can be used in the actual cooling process, and the cooling efficiency is still relatively insufficient.

发明内容Contents of the invention

基于现有技术中的上述不足,本申请提供了一种磁悬浮离心式压缩机电机的冷却结构,风冷和水冷两种冷却方式结合共同散热,提高磁悬浮电机的冷却效率。Based on the above-mentioned deficiencies in the prior art, the present application provides a cooling structure for a magnetic levitation centrifugal compressor motor. Air cooling and water cooling are combined to dissipate heat together to improve the cooling efficiency of the magnetic levitation motor.

为实现上述目的,本发明提出以下技术方案。In order to achieve the above object, the present invention proposes the following technical solutions.

一种磁悬浮离心式压缩机电机的冷却结构,电机包括依次套设的转子、定子和外壳,转子和定子之间分隔设有散热间隙;定子固定在外壳的内壁上,定子两端均设有连通散热间隙的散热区,外壳上固定设有连通散热区的进风口和出风口;外壳内设有水冷流道,外壳上固定设有连通水冷流道的进水口和出水口。A cooling structure for a magnetic levitation centrifugal compressor motor. The motor includes a rotor, a stator, and a casing that are sheathed in sequence, and a heat dissipation gap is provided between the rotor and the stator; In the heat dissipation area of the heat dissipation gap, an air inlet and an air outlet connected to the heat dissipation area are fixedly provided on the shell; a water cooling flow channel is provided inside the shell, and a water inlet and a water outlet connected to the water cooling flow channel are fixedly provided on the shell.

采用水冷加风冷相结合的冷却方式,电机定子外表面采用水冷,电机转子、线包及电机定子内圈采用风冷结构,两种冷却方式同时作用在电机上进行冷却,虽然转子、线包和定子内圈是采用的风冷,但冷却气流在进风口经过水冷的电机外壳后被进一步降温,比一般风冷具有更高的降温效率,从而确保电机运行时极低的运行温度。The cooling method combining water cooling and air cooling is adopted. The outer surface of the motor stator is water-cooled, and the motor rotor, wire package and inner ring of the motor stator are air-cooled. The two cooling methods act on the motor at the same time for cooling. Although the rotor, wire package And the inner ring of the stator is air-cooled, but the cooling airflow is further cooled after passing through the water-cooled motor casing at the air inlet, which has a higher cooling efficiency than ordinary air-cooled, thus ensuring an extremely low operating temperature when the motor is running.

作为优选,转子的一端设有推力轴承,推力轴承的隔圈上设有连通散热区的散热孔。在磁悬浮电机工作时,推力盘被悬浮在前后推力轴承的中心位置,两边均有0.5mm的间隙。此时由于推力盘高速旋转,会产生离心力,推力轴承隔圈上开有一圈散热孔,推力轴承产生的热量会从散热孔中带出,实现推力轴承的冷却。Preferably, one end of the rotor is provided with a thrust bearing, and the spacer ring of the thrust bearing is provided with cooling holes communicating with the cooling area. When the magnetic levitation motor is working, the thrust plate is suspended at the center of the front and rear thrust bearings, with a gap of 0.5 mm on both sides. At this time, due to the high-speed rotation of the thrust disc, centrifugal force will be generated. There is a circle of cooling holes on the spacer ring of the thrust bearing. The heat generated by the thrust bearing will be taken out from the cooling holes to realize the cooling of the thrust bearing.

作为优选,外壳的前端设有前端磁轴承座,前端磁轴承座内设有前端径向磁轴承,前端磁轴承座内设有连通散热区的散热风口,散热风口连通散热区。在前端磁轴承座上开有散热风口作为风道,通过热传导方式,保证前端径向磁轴承被完全冷却;散热区和散热风口的设计增加了散热面积,将磁轴承产生的热量也通过水冷带走。Preferably, the front end of the casing is provided with a front-end magnetic bearing seat, and a front-end radial magnetic bearing is provided in the front-end magnetic bearing seat, and a heat dissipation air port connected to the heat dissipation area is provided in the front end magnetic bearing seat, and the heat dissipation air port is connected to the heat dissipation area. There is a heat dissipation air outlet on the front magnetic bearing seat as an air channel, and the front radial magnetic bearing is guaranteed to be completely cooled through heat conduction; the design of the heat dissipation area and the heat dissipation air outlet increases the heat dissipation area, and the heat generated by the magnetic bearing is also passed through the water cooling belt. Walk.

作为优选,外壳采用铝拉伸型材电机筒,外壳两端通过摩擦搅拌焊密封。电机外壳采用铝拉伸型材制成,导热性高;通过摩擦搅拌焊使外壳两端密封,并在内部形成循环的轴向水道,保证外壳的散热能力。Preferably, the casing is made of an aluminum stretched profile motor barrel, and the two ends of the casing are sealed by friction stir welding. The motor casing is made of aluminum stretched profile, which has high thermal conductivity; the two ends of the casing are sealed by friction stir welding, and a circulating axial water channel is formed inside to ensure the heat dissipation capacity of the casing.

作为优选,进风口的位置与定子上的线包正对。进风口通过外部散热风机冷却散热向内鼓风,进风位置与线包相对,确保线包被完全充分冷却。Preferably, the position of the air inlet is directly opposite to the wire package on the stator. The air inlet is cooled and dissipated by an external heat dissipation fan, and blows air inwardly. The position of the air inlet is opposite to the wire package to ensure that the wire package is completely and fully cooled.

作为优选,水冷流道包括平行外壳轴线设置的若干根轴向流道,轴向流道彼此串联。通过轴向走水,加长流道及水冷散热面积。Preferably, the water-cooling flow channel includes several axial flow channels arranged parallel to the axis of the casing, and the axial flow channels are connected in series. Through the axial water flow, the flow channel and water cooling heat dissipation area are lengthened.

作为优选,轴向流道设有绕外壳轴线圆周阵列设置的十二根,轴向流道的径向横截面形状为圆弧形,轴向流道的径向横截面的圆心角在20到27度之间。轴向流道对应至外壳的大部分面积,散热区域大,保证外壳和定子的冷却效率,并且轴向流道的横向尺寸大,能够有效减小水阻,提高散热效率。As a preference, there are twelve axial flow passages arranged in a circular array around the axis of the housing, the radial cross-sectional shape of the axial flow passage is arc-shaped, and the central angle of the radial cross-section of the axial flow passage is between 20 and Between 27 degrees. The axial flow channel corresponds to most of the area of the shell, and the heat dissipation area is large to ensure the cooling efficiency of the shell and the stator. The lateral dimension of the axial flow channel is large, which can effectively reduce the water resistance and improve the heat dissipation efficiency.

作为优选,进风口设置在电机的外壳的前端,推力轴承设置在前端磁轴承座的端部内,散热孔连通散热风口。工作时,散热风将从前端进入,通过电机定子与电机转子之间间隙流出,最终从后端线包处流出,保证了推力轴承和磁悬浮轴承的散热能力。Preferably, the air inlet is arranged at the front end of the casing of the motor, the thrust bearing is arranged in the end of the magnetic bearing seat at the front end, and the cooling holes communicate with the cooling air outlets. When working, the cooling air will enter from the front end, flow out through the gap between the motor stator and the motor rotor, and finally flow out from the rear end wire wrap, which ensures the heat dissipation capacity of the thrust bearing and magnetic suspension bearing.

作为优选,进风口在电机轴向上的长度的范围在定子轴向长度的1/4到2/5之间。确保进风口处进风对电机定子的冷却效率。Preferably, the length of the air inlet in the axial direction of the motor ranges from 1/4 to 2/5 of the axial length of the stator. Ensure the cooling efficiency of the motor stator by the air intake at the air inlet.

本发明的有益效果是:风冷和水冷两种冷却方式结合共同散热,提高磁悬浮电机的冷却效率;能够完成电机内部推力轴承和磁悬浮轴承的散热,散热效率强。The beneficial effects of the present invention are: air cooling and water cooling are combined to jointly dissipate heat to improve the cooling efficiency of the magnetic levitation motor; the heat dissipation of the thrust bearing and the magnetic levitation bearing inside the motor can be completed, and the heat dissipation efficiency is strong.

附图说明Description of drawings

图1是本发明的结构示意图。Fig. 1 is a structural schematic diagram of the present invention.

图2是本发明中外壳的结构示意图。Fig. 2 is a structural schematic diagram of the casing in the present invention.

图3是图2中A-A处的剖视图。Fig. 3 is a cross-sectional view at A-A in Fig. 2 .

图4是图2中B-B处的剖视图。Fig. 4 is a cross-sectional view at B-B in Fig. 2 .

图5是轴向流道一端连通相邻轴向流道位置的剖视图。Fig. 5 is a cross-sectional view where one end of the axial flow channel is connected to adjacent axial flow channels.

图6是图5中C-C处的剖视图。Fig. 6 is a cross-sectional view at C-C in Fig. 5 .

图中:转子1 推力盘101 定子2 线包201 散热间隙202 外壳3 进风口301 出风口302 进水口303 出水口304 推力轴承4 隔圈401 散热孔402 前端磁轴承座5 前端径向磁轴承501 散热风口502 前散热区503 后端磁轴承座6 后散热区601 水冷流道7 轴向流道701。In the figure: rotor 1 thrust disc 101 stator 2 wire package 201 heat dissipation gap 202 shell 3 air inlet 301 air outlet 302 water inlet 303 water outlet 304 thrust bearing 4 spacer 401 cooling hole 402 front end magnetic bearing seat 5 front radial magnetic bearing 501 Cooling air outlet 502 Front heat dissipation area 503 Rear end magnetic bearing seat 6 Rear heat dissipation area 601 Water cooling flow channel 7 Axial flow channel 701.

具体实施方式Detailed ways

下面结合附图与具体实施例对本发明进行进一步的描述。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

实施例1,Example 1,

一种磁悬浮离心式压缩机电机的冷却结构,如图1和图2所示,电机包括依次套设的转子1、定子2和外壳3,定子2固定在外壳3的内壁上,转子1是与转轴集成的一体结构;转子1和定子2之间分隔设有散热间隙202。定子2两端均设有连通散热间隙202的散热区,定子2的前端和推力轴承4、前端磁轴承座5间隙相对,形成前散热区503;定子2的后端和后端磁轴承座6间隙相对,形成后散热区601。外壳3上固定设有连通散热区的进风口301和出风口302;进风口301和出风口302的位置与定子2上的线包201正对。进风口301设置在电机的外壳3的前端,进风口301在电机轴向上的位置与前散热区503相邻,进风口301进气时经过定子2上的线包201外侧分流向前端磁轴承座5和散热间隙202。进风口301在电机轴向上的长度时电机定子2轴向长度的8/25。转子1的一端设有推力轴承4,两推力轴承4之间的隔圈401上设有连通散热区的散热孔402。外壳3的前端设有前端磁轴承座5,前端磁轴承座5内设有前端径向磁轴承501,前端磁轴承座5内设有连通散热区的散热风口502,推力轴承4设置在前端磁轴承座5的端部内,散热孔402连通散热风口502。散热风口502连通散热区。转子1上设置凸肩形成与推力轴承4配合的推力盘101,电机工作时,推力盘101被悬浮到推力轴承4的中间位置,推力盘101与其两边的推力轴承4形成间隙,推力盘101旋转产生离心力将内部空气和热量一起甩出,经过散热孔402进入散热风口502后一起被向散热风口502流出的气流带出,实现推力轴承4的散热。外壳3内设有水冷流道7,如图3到图6所示,水冷流道7包括平行外壳3轴线设置的若干根轴向流道701,轴向流道701彼此串联,具体为,轴向流道701的一端连通相邻一侧的轴向流道701的一端,轴向流道701的另一端连通相邻另一侧的轴向流道701的另一端,相邻轴向流道701连通的水道沿外壳3径向设置。轴向流道701设有绕外壳3轴线圆周阵列设置的十二根,轴向流道701的径向横截面形状为圆弧形,轴向流道701的径向横截面两端为直线形,轴向流道701的径向横截面两端的直线呈30度夹角,轴线流道的径向横截面两端和轴向流道701的弧形侧面之间设有圆角过渡。轴向流道701的径向横截面的圆心角采用二十四度。外壳3采用铝拉伸型材电机筒,外壳3两端通过摩擦搅拌焊密封。外壳3上固定设有连通水冷流道7的进水口303和出水口304。进水口303和出水口304通过管道连通外部的冷却水路。进气口和出气口连通外部的冷却气路。由于进风口301和出风口302穿过外壳3设置,因此进风口301进入的冷却气流会被水冷的外壳3降温,实现整体的快速散热。电机的外壳3两端分别设置泵壳,电机的转子1轴两端在对应的泵壳内分别设置叶轮。A cooling structure of a magnetic levitation centrifugal compressor motor, as shown in Figure 1 and Figure 2, the motor includes a rotor 1, a stator 2 and a casing 3 that are sequentially sleeved, the stator 2 is fixed on the inner wall of the casing 3, and the rotor 1 is connected to the An integral structure with integrated rotating shafts; a cooling gap 202 is provided between the rotor 1 and the stator 2 . Both ends of the stator 2 are provided with heat dissipation areas connected to the heat dissipation gap 202. The front end of the stator 2 is opposite to the thrust bearing 4 and the front end magnetic bearing seat 5 to form a front heat dissipation area 503; the rear end of the stator 2 and the rear end magnetic bearing seat 6 The gaps are opposite to form a rear heat dissipation area 601 . The housing 3 is fixed with an air inlet 301 and an air outlet 302 connected to the heat dissipation area; The air inlet 301 is arranged at the front end of the housing 3 of the motor. The position of the air inlet 301 in the axial direction of the motor is adjacent to the front cooling area 503. When the air inlet 301 takes in air, the air flows through the outer side of the wire package 201 on the stator 2 to the front magnetic bearing. Seat 5 and cooling gap 202. The length of the air inlet 301 in the axial direction of the motor is 8/25 of the axial length of the motor stator 2 . One end of the rotor 1 is provided with a thrust bearing 4 , and a spacer 401 between the two thrust bearings 4 is provided with a cooling hole 402 communicating with the cooling area. The front end of the housing 3 is provided with a front-end magnetic bearing seat 5, and the front-end magnetic bearing seat 5 is provided with a front-end radial magnetic bearing 501, and the front-end magnetic bearing seat 5 is provided with a cooling air outlet 502 connected to the heat dissipation area, and the thrust bearing 4 is arranged on the front-end magnetic bearing seat 5. In the end portion of the bearing housing 5 , the heat dissipation holes 402 communicate with the heat dissipation air outlets 502 . The heat dissipation air outlet 502 communicates with the heat dissipation area. A shoulder is set on the rotor 1 to form a thrust disc 101 that cooperates with the thrust bearing 4. When the motor is in operation, the thrust disc 101 is suspended to the middle position of the thrust bearing 4, and a gap is formed between the thrust disc 101 and the thrust bearings 4 on both sides, and the thrust disc 101 rotates. Centrifugal force is generated to throw out the internal air and heat together, and then enter the heat dissipation air outlet 502 through the heat dissipation hole 402 and be taken out together by the airflow flowing out to the heat dissipation air outlet 502 to realize the heat dissipation of the thrust bearing 4 . The housing 3 is provided with a water-cooling channel 7, as shown in Figure 3 to Figure 6, the water-cooling channel 7 includes several axial channels 701 arranged parallel to the axis of the housing 3, and the axial channels 701 are connected in series, specifically, the shaft One end of the flow channel 701 is connected to one end of the axial flow channel 701 on the adjacent side, and the other end of the axial flow channel 701 is connected to the other end of the axial flow channel 701 on the other side. The water channels communicated with 701 are arranged radially along the casing 3 . The axial flow channel 701 is provided with twelve circumferential arrays arranged around the axis of the housing 3. The radial cross-sectional shape of the axial flow channel 701 is arc-shaped, and the two ends of the radial cross-section of the axial flow channel 701 are linear. , the straight lines at both ends of the radial cross-section of the axial flow channel 701 form an included angle of 30 degrees, and there is a rounded transition between the two ends of the radial cross-section of the axial flow channel and the arc-shaped side of the axial flow channel 701 . The central angle of the radial cross section of the axial channel 701 is 24 degrees. The casing 3 is made of an aluminum stretch profile motor barrel, and both ends of the casing 3 are sealed by friction stir welding. The casing 3 is fixedly provided with a water inlet 303 and a water outlet 304 communicating with the water-cooling channel 7 . The water inlet 303 and the water outlet 304 communicate with the external cooling water circuit through pipes. The air inlet and the air outlet are connected to the external cooling air path. Since the air inlet 301 and the air outlet 302 are provided through the casing 3, the cooling airflow entering the air inlet 301 will be cooled by the water-cooled casing 3, so as to realize rapid overall heat dissipation. The two ends of the casing 3 of the motor are respectively provided with pump casings, and the two ends of the rotor 1 shaft of the motor are respectively provided with impellers in the corresponding pump casings.

本申请采用水冷加风冷相结合的冷却方式,电机定子2外表面采用水冷,电机转子1、线包201及电机定子2内圈采用风冷结构,两种冷却方式同时作用在电机上进行冷却,虽然转子1、线包201和定子2内圈是采用的风冷,但冷却气流在进风口301经过水冷的电机外壳3后被进一步降温,比一般风冷具有更高的降温效率,从而确保电机运行时极低的运行温度。此外,本申请不仅具有水冷和风冷结合的散热方式来提高电机散热效率,而且还优化了电机外壳3上的水冷流道7和电机内的冷却风道,从结构上进一步提高电机整体的散热效率,还能完成推力轴承4的热传导散热,散热效率高。This application adopts a combination of water cooling and air cooling. The outer surface of the motor stator 2 is water-cooled, and the motor rotor 1, wire package 201 and the inner ring of the motor stator 2 are air-cooled. The two cooling methods act on the motor at the same time for cooling , although the rotor 1, the wire package 201 and the inner ring of the stator 2 are air-cooled, the cooling air flow is further cooled after passing through the water-cooled motor casing 3 at the air inlet 301, which has a higher cooling efficiency than the general air-cooled, thus ensuring Extremely low operating temperature when the motor is running. In addition, this application not only has a combination of water cooling and air cooling to improve the heat dissipation efficiency of the motor, but also optimizes the water cooling flow channel 7 on the motor casing 3 and the cooling air channel in the motor, further improving the overall heat dissipation of the motor from the structure efficiency, and can also complete the heat conduction and heat dissipation of the thrust bearing 4, and the heat dissipation efficiency is high.

Claims (9)

1. The cooling structure of the magnetic suspension centrifugal compressor motor is characterized in that the motor comprises a rotor, a stator and a shell which are sleeved in sequence, and a heat dissipation gap is arranged between the rotor and the stator in a separation mode; the stator is fixed on the inner wall of the shell, the two ends of the stator are respectively provided with a heat dissipation area communicated with the heat dissipation gap, and the shell is fixedly provided with an air inlet and an air outlet communicated with the heat dissipation area; the shell is internally provided with a water cooling flow passage, and the shell is fixedly provided with a water inlet and a water outlet which are communicated with the water cooling flow passage.
2. The cooling structure of claim 1, wherein a thrust bearing is disposed at one end of the rotor, and a heat dissipation hole communicating with the heat dissipation area is disposed on a spacer of the thrust bearing.
3. The cooling structure of claim 2, wherein the front end of the housing is provided with a front end magnetic bearing seat, a front end radial magnetic bearing is arranged in the front end magnetic bearing seat, and a heat dissipation air port communicated with the heat dissipation area is arranged in the front end magnetic bearing seat and communicated with the heat dissipation area.
4. The cooling structure of a magnetic levitation centrifugal compressor motor according to claim 1, wherein the housing is an aluminum stretching profile motor cylinder, and both ends of the housing are sealed by friction stir welding.
5. The cooling structure of claim 1, wherein the air inlet is located opposite to the coil on the stator.
6. A cooling structure of a magnetic levitation centrifugal compressor motor according to claim 1 or 4, wherein the water-cooling flow passage comprises a plurality of axial flow passages arranged parallel to the axis of the housing, the axial flow passages being connected in series with each other.
7. The cooling structure of claim 6, wherein the axial flow channels are twelve arranged in a circumferential array around the axis of the casing, the radial cross section of the axial flow channels is circular arc, and the central angle of the radial cross section of the axial flow channels is 20 to 27 degrees.
8. A cooling structure of a magnetic suspension centrifugal compressor motor according to claim 3, wherein the air inlet is arranged at the front end of the motor housing, the thrust bearing is arranged in the end part of the front magnetic bearing seat, and the heat dissipation hole is communicated with the heat dissipation air inlet.
9. A cooling structure of a magnetic levitation centrifugal compressor motor according to claim 1 or 2 or 3 or 5 or 8, wherein the length of the air inlet in the axial direction of the motor ranges from 1/4 to 2/5 of the axial length of the stator.
CN202310183178.3A 2023-02-21 2023-02-21 Cooling structure of magnetic suspension centrifugal compressor motor Active CN116317302B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118499254A (en) * 2024-04-01 2024-08-16 雷茨智能装备(广东)有限公司 Magnetic suspension air compressor

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3683464A1 (en) * 2019-01-21 2020-07-22 Ingersoll-Rand Industrial U.S., Inc. Active magnetic bearing apparatus
CN112460056A (en) * 2020-11-26 2021-03-09 广州市昊志机电股份有限公司 Centrifugal air compressor and hydrogen fuel cell
CN212935650U (en) * 2020-07-15 2021-04-09 稳力(广东)科技有限公司 Cooling structure of fuel cell centrifugal air compressor
CN113394906A (en) * 2021-06-18 2021-09-14 河南通宇新源动力有限公司 Welding-free water-cooling motor shell and motor thereof
CN113746253A (en) * 2021-08-03 2021-12-03 鑫磊压缩机股份有限公司 Magnetic suspension motor shell and motor compatible with water cooling and air cooling system
CN115030784A (en) * 2022-06-13 2022-09-09 康跃科技(山东)有限公司 Bearing cooling device of air bearing turbocharger

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3683464A1 (en) * 2019-01-21 2020-07-22 Ingersoll-Rand Industrial U.S., Inc. Active magnetic bearing apparatus
CN212935650U (en) * 2020-07-15 2021-04-09 稳力(广东)科技有限公司 Cooling structure of fuel cell centrifugal air compressor
CN112460056A (en) * 2020-11-26 2021-03-09 广州市昊志机电股份有限公司 Centrifugal air compressor and hydrogen fuel cell
CN113394906A (en) * 2021-06-18 2021-09-14 河南通宇新源动力有限公司 Welding-free water-cooling motor shell and motor thereof
CN113746253A (en) * 2021-08-03 2021-12-03 鑫磊压缩机股份有限公司 Magnetic suspension motor shell and motor compatible with water cooling and air cooling system
WO2023010697A1 (en) * 2021-08-03 2023-02-09 鑫磊压缩机股份有限公司 Magnetic levitation motor housing compatible with water cooling and air cooling system, and motor
CN115030784A (en) * 2022-06-13 2022-09-09 康跃科技(山东)有限公司 Bearing cooling device of air bearing turbocharger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN118499254A (en) * 2024-04-01 2024-08-16 雷茨智能装备(广东)有限公司 Magnetic suspension air compressor

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