CN114844270A - A stator assembly and motor - Google Patents
A stator assembly and motor Download PDFInfo
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- CN114844270A CN114844270A CN202210521873.1A CN202210521873A CN114844270A CN 114844270 A CN114844270 A CN 114844270A CN 202210521873 A CN202210521873 A CN 202210521873A CN 114844270 A CN114844270 A CN 114844270A
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 68
- 238000004804 winding Methods 0.000 claims abstract description 32
- 239000004519 grease Substances 0.000 claims abstract description 12
- 229920001296 polysiloxane Polymers 0.000 claims abstract description 9
- 238000012546 transfer Methods 0.000 claims description 14
- 239000012790 adhesive layer Substances 0.000 claims description 11
- 239000010410 layer Substances 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 238000005452 bending Methods 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 5
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 238000010292 electrical insulation Methods 0.000 claims description 3
- 238000009413 insulation Methods 0.000 abstract description 2
- 230000001737 promoting effect Effects 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000005347 demagnetization Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000007596 consolidation process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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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
- H02K3/24—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors with channels or ducts for cooling medium between the conductors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/12—Stationary parts of the magnetic circuit
- H02K1/20—Stationary parts of the magnetic circuit with channels or ducts for flow of cooling medium
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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
- H02K3/12—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors arranged in slots
- H02K3/14—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors arranged in slots with transposed conductors, e.g. twisted conductors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/22—Arrangements for cooling or ventilating by solid heat conducting material embedded in, or arranged in contact with, the stator or rotor, e.g. heat bridges
- H02K9/225—Heat pipes
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/22—Arrangements for cooling or ventilating by solid heat conducting material embedded in, or arranged in contact with, the stator or rotor, e.g. heat bridges
- H02K9/227—Heat sinks
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Motor Or Generator Cooling System (AREA)
Abstract
Description
技术领域technical field
本发明涉及电机技术领域,具体而言,涉及一种定子组件及电机。The present invention relates to the technical field of motors, and in particular, to a stator assembly and a motor.
背景技术Background technique
大型重载无人机的发展趋势对电机的功率密度、转矩密度和可靠性提出了更高的要求。而现阶段限制电机性能提高的主要瓶颈就是电机的热管理系统,因此改善电机的散热条件对于提高电机的性能和促进行业发展具有重要意义。The development trend of large and heavy-duty UAVs puts forward higher requirements on the power density, torque density and reliability of the motors. At this stage, the main bottleneck restricting the improvement of motor performance is the thermal management system of the motor. Therefore, improving the heat dissipation conditions of the motor is of great significance for improving the performance of the motor and promoting the development of the industry.
高功率密度电机的电流密度和热负荷通常比较大,因此电机在运行过程中产生大量热量,电机温升较高。无人机驱动电机对功重比和可靠性要求较高,因此通常采用风冷散热方式。但是在不增加额外散热结构的情况下,由于散热路径较长且路径上热阻较大,电机内部的热量无法快速有效地传导至机壳并及时消散到空气中,这会导致电机的温升过高,进而影响电机性能和可靠性。The current density and thermal load of high power density motors are usually relatively large, so the motor generates a lot of heat during operation, and the temperature rise of the motor is relatively high. The UAV drive motor has high requirements on power-to-weight ratio and reliability, so air-cooled heat dissipation is usually adopted. However, without adding an additional heat dissipation structure, due to the long heat dissipation path and the large thermal resistance on the path, the heat inside the motor cannot be quickly and effectively conducted to the casing and dissipated into the air in time, which will cause the temperature of the motor to rise. If it is too high, it will affect the performance and reliability of the motor.
永磁电机中的永磁体随着温度升高而性能会大幅下降,出现退磁现象并影响电机的电磁性能;严重者可发生永久性退磁并使得电机彻底无法工作,严重威胁飞行器的安全运行。The performance of the permanent magnets in the permanent magnet motor will drop significantly with the increase of temperature, and demagnetization will occur and affect the electromagnetic performance of the motor; in severe cases, permanent demagnetization may occur and the motor will be completely unable to work, which seriously threatens the safe operation of the aircraft.
因此,研究和开发具有先进散热系统的定子组件及其电机对于提升无人机性能和可靠性具有重要意义。Therefore, research and development of stator components and their motors with advanced cooling systems is of great significance for improving the performance and reliability of UAVs.
发明内容SUMMARY OF THE INVENTION
本发明主要目的是提供一种具有散热效果的定子组件,使应用该技术方案的电机在运行时稳定温升有较大幅度的降低,且功率密度和可靠性得到大幅提升,用以解决现有技术下该类电机运行温升过高和电机功率密度低导致的无人机有效载荷不足的问题,从而提高无人机的有效载荷、续航时间和可靠性。The main purpose of the present invention is to provide a stator assembly with heat dissipation effect, so that the stable temperature rise of the motor using the technical solution is greatly reduced during operation, and the power density and reliability are greatly improved, so as to solve the problem of existing Under the technology, the operating temperature of this type of motor is too high and the power density of the motor is low, resulting in insufficient payload of the UAV, thereby improving the payload, endurance and reliability of the UAV.
本发明的上述目的,通过以下技术方案来实现:The above-mentioned purpose of the present invention is realized by the following technical solutions:
一种定子组件,包括具有多个定子槽的定子铁芯,每个所述定子槽内均设有两层绕组,两层所述绕组之间设有间隙,所述定子组件还包括有用于供绕组散热的散热部,所述散热部包括导热管和散热元件,所述导热管一端与散热元件连接,所述导热管另一端插接在所述间隙内且与所述绕组通过接触热传导,所述间隙内填充有具有电性绝缘的导热硅脂,所述导热硅脂用于将绕组产生的热量传递至导热管。A stator assembly includes a stator core with a plurality of stator slots, two layers of windings are arranged in each of the stator slots, and a gap is arranged between the two layers of the windings, and the stator assembly further includes a The heat dissipation part for the heat dissipation of the winding, the heat dissipation part includes a heat pipe and a heat dissipation element, one end of the heat pipe is connected with the heat dissipation element, and the other end of the heat pipe is inserted into the gap and conducts heat conduction with the winding through contact, so The gap is filled with thermally conductive silicone grease with electrical insulation, and the thermally conductive silicone grease is used to transfer the heat generated by the winding to the heat conduction pipe.
上述技术方案的有益效果为:通过设置导热管和散热元件,使绕组产生的热量部分导入导热管,通过导热管再将热量导入散热元件,通过散热元件使热量扩散至外界大气,有利于绕组的散热,其中导热管端部能插接在间隙内,使得散热元件能通过导热管得到支撑,提高散热元件的稳定性,且间隙内填充的导热硅脂能增大导热管与绕组接触面积,进一步提高导热管与绕组热传递的效率,同时导热硅脂具有电性绝缘,能电性隔离导热管与绕组,防止绕组漏电发生。The beneficial effects of the above technical solutions are: by arranging the heat pipe and the heat dissipation element, the heat generated by the winding is partially introduced into the heat pipe, and then the heat is introduced into the heat dissipation element through the heat pipe, and the heat is diffused to the outside atmosphere through the heat dissipation element, which is beneficial to the heat dissipation of the winding. Heat dissipation, in which the end of the heat pipe can be inserted into the gap, so that the heat dissipation element can be supported by the heat pipe, and the stability of the heat dissipation element is improved, and the thermal grease filled in the gap can increase the contact area between the heat pipe and the winding, further Improve the efficiency of heat transfer between the heat pipe and the winding, and at the same time, the heat conductive silicone grease has electrical insulation, which can electrically isolate the heat pipe and the winding to prevent the leakage of the winding.
优选的,所述导热管包括第一热管,所述散热元件包括散热板组,所述散热板组包括若干个间隔设置的散热片,若干个所述散热片上设有用于连接所述第一热管的第一连接部。通过间隔设置的多个散热片,使散热板组与外界大气的接触面大大增加,利于散热板组的快速散热,同时设置第一连接部,方便散热板组与导热管的第一热管连接,便于热量传递。Preferably, the heat pipe includes a first heat pipe, the heat dissipation element includes a heat dissipation plate group, and the heat dissipation plate group includes a plurality of heat dissipation fins arranged at intervals, and a plurality of the heat dissipation fins are provided for connecting the first heat pipe. the first connection part. A plurality of radiating fins arranged at intervals greatly increase the contact surface between the radiating plate group and the outside atmosphere, which is beneficial to the rapid heat dissipation of the radiating plate group. Facilitates heat transfer.
优选的,所述第一连接部包括穿设在若干个所述散热片上的连接管,所述连接管上设有通孔,所述通孔供所述第一热管插接,所述连接管与第一热管通过接触热传导。通过连接管插入到多个散热片上,增加连接管与多个散热片接触,使多个散热片的连接更稳定,同时连接管上的通孔供第一热管插接,实现多个散热片与第一热管的有效连接,且能提高连接稳定性和热传递效率。Preferably, the first connecting portion includes a connecting pipe that penetrates through a plurality of the heat sinks, the connecting pipe is provided with a through hole, the through hole is used for the first heat pipe to be inserted, and the connecting pipe Conduct heat conduction through contact with the first heat pipe. The connecting tube is inserted into multiple heat sinks, increasing the contact between the connecting tube and multiple heat sinks, so that the connection of multiple heat sinks is more stable. The first heat pipe is effectively connected, and the connection stability and heat transfer efficiency can be improved.
优选的,所述第一连接部包括连接板,若干个所述散热片设置在所述连接板的一侧面,所述连接板的另一侧面设有用于粘接第一热管的第一粘接层,所述第一粘接层具有将第一热管的热量传递至连接板上。通过设置连接板能有效连接多个散热片,同时连接板上的第一粘胶层能粘接第一热管增加两者接触面,实现多个散热片与第一热管的有效连接,使两者连接方便,且第一粘接层的热传导,有利于提高第一热管与连接板的热传递效率。Preferably, the first connecting part includes a connecting plate, a plurality of the cooling fins are arranged on one side of the connecting plate, and the other side of the connecting plate is provided with a first adhesive for bonding the first heat pipe layer, the first adhesive layer has the function of transferring the heat of the first heat pipe to the connecting plate. By setting the connecting plate, a plurality of heat sinks can be effectively connected, and at the same time, the first adhesive layer on the connecting plate can bond the first heat pipe to increase the contact surface between the two, so as to realize the effective connection between the plurality of heat sinks and the first heat pipe, so that the two The connection is convenient, and the heat conduction of the first adhesive layer is beneficial to improve the heat transfer efficiency between the first heat pipe and the connecting plate.
优选的,所述导热管还包括第二热管,所述散热元件包括用于支撑所述定子铁芯的支架,所述支架过盈配合在所述定子铁芯的安装通槽内,所述支架与所述第二热管通过第二连接部连接。通过采用上述结构,使支架能为绕组提供散热,同时通过第二连接部,能提高第二热管的安装稳定性。Preferably, the heat transfer pipe further includes a second heat pipe, the heat dissipation element includes a bracket for supporting the stator iron core, the bracket is interference fit in the installation through groove of the stator iron core, and the bracket connected with the second heat pipe through a second connection part. By adopting the above structure, the bracket can provide heat dissipation for the winding, and at the same time, through the second connection portion, the installation stability of the second heat pipe can be improved.
优选的,所述第二连接部包括设置在支架上的肋条,所述肋条上设有用于粘接第二热管的第二粘接层,所述第二粘接层具有将第二热管的热量传递至肋条上。通过设置肋条,一方面能增加支架的结构强度,另一方面能为第二热管与支架的连接提供有效位置,便于通过第二粘接层的连接,增加两者接触面,同时第二粘接层的热传导,有利于提高第二热管与支架的热传递效率。Preferably, the second connecting part includes ribs arranged on the bracket, the ribs are provided with a second adhesive layer for bonding the second heat pipe, and the second adhesive layer has the ability to reduce the heat of the second heat pipe Transfer to the ribs. By arranging the ribs, on the one hand, the structural strength of the bracket can be increased, and on the other hand, it can provide an effective position for the connection between the second heat pipe and the bracket, which facilitates the connection through the second adhesive layer, increases the contact surface between the two, and at the same time the second adhesive layer The heat conduction of the layer is beneficial to improve the heat transfer efficiency between the second heat pipe and the bracket.
优选的,所述散热部包括多个第一热管和第二热管,多个所述第一热管和第二热管沿周向均匀分布在定子铁芯上。通过采用上述结构,能增加散热元件,提高散热效果。Preferably, the heat dissipation part includes a plurality of first heat pipes and a plurality of second heat pipes, and the plurality of the first heat pipes and the second heat pipes are uniformly distributed on the stator iron core along the circumferential direction. By adopting the above structure, heat dissipation elements can be added, and the heat dissipation effect can be improved.
优选的,所述第一热管呈向外弯折结构,所述第一热管连接的散热板组远离绕组设置,所述第二热管朝支架弯折,所述第一热管和第二热管的弯折角度为80-100度。通过采用上述结构,弯折后的导热管能撑开散热元件,利于散热。Preferably, the first heat pipe is in an outwardly bent structure, the heat dissipation plate group connected to the first heat pipe is disposed away from the winding, the second heat pipe is bent toward the bracket, and the bending of the first heat pipe and the second heat pipe is The folding angle is 80-100 degrees. By adopting the above structure, the bent heat-conducting pipe can spread the heat-dissipating element, which is beneficial to heat dissipation.
优选的,所述导热管的材质为铜合金,所述散热元件的材质为铝合金。通过采用铜合金的导热管和铝合金的散热元件,在兼顾成本的同时能提高导热性能,利于绕组的热量传导,便于散热。Preferably, the material of the heat transfer pipe is copper alloy, and the material of the heat dissipation element is aluminum alloy. By using a copper alloy heat pipe and an aluminum alloy heat dissipation element, the heat conduction performance can be improved while taking into account the cost, which is beneficial to the heat conduction of the winding and the heat dissipation.
本发明还公开一种电机,包括如上所述的定子组件,具有该定子组件的电机在运行时稳定温升有较大幅度的降低,且功率密度和可靠性得到大幅提升,用以解决现有技术下该类电机运行温升过高和电机功率密度低导致的无人机有效载荷不足的问题,从而提高无人机的有效载荷、续航时间和可靠性。The present invention also discloses a motor, including the above stator assembly, the motor with the stator assembly has a relatively large reduction in the stable temperature rise during operation, and the power density and reliability are greatly improved, so as to solve the problem of existing problems. Under the technology, the operating temperature of this type of motor is too high and the power density of the motor is low, resulting in insufficient payload of the UAV, thereby improving the payload, endurance and reliability of the UAV.
附图说明Description of drawings
图1是实施例一的定子组件的爆炸结构示意图;Fig. 1 is the exploded structure schematic diagram of the stator assembly of
图2是实施例一的定子组件的整体结构示意图;2 is a schematic diagram of the overall structure of the stator assembly of the first embodiment;
图3是实施例一的电机的整体结构示意图;3 is a schematic diagram of the overall structure of the motor of the first embodiment;
图4是实施例一的散热板组的结构示意图;FIG. 4 is a schematic structural diagram of the heat dissipation plate set according to the first embodiment;
图5是第一热管的结构示意图;5 is a schematic structural diagram of a first heat pipe;
图6是实施例二的散热板组的结构示意图;6 is a schematic structural diagram of the heat dissipation plate group of the second embodiment;
附图标记说明:Description of reference numbers:
1、定子铁芯;11、安装通槽;2、绕组;3、间隙;4、散热部;41、导热管;411、第一热管;412、第二热管;413、弯折角度;42、散热板组;421、散热片;422、连接管;4221、通孔;423、连接板;5、支架;51、肋条。1. Stator iron core; 11. Installation slot; 2. Winding; 3. Gap; 4. Heat dissipation part; 41. Heat conduction pipe; 411, First heat pipe; 412, Second heat pipe; 421, heat sink; 422, connecting pipe; 4221, through hole; 423, connecting plate; 5, bracket; 51, rib.
具体实施方式Detailed ways
为使本发明的上述目的、特征和优点能够更为明显易懂,下面结合附图对本发明的具体实施例做详细的说明。In order to make the above objects, features and advantages of the present invention more clearly understood, the specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
在本发明的描述中,需要说明的是,术语“上”、“下”、“左”、“右”、“前”、“后”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制。In the description of the present invention, it should be noted that the orientations or positional relationships indicated by the terms "upper", "lower", "left", "right", "front", "rear", etc. are based on those shown in the accompanying drawings. The orientation or positional relationship is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of the present invention.
实施例一Example 1
如图1-5所示,本发明提供一种定子组件,包括具有24个定子槽的定子铁芯1,所述定子铁芯1上设有用于支撑定子铁芯1的支架5,所述支架5过盈配合在所述定子铁芯1的安装通槽11内,所述支架5上设有肋条51,每个所述定子槽内均设有两层绕组2,两层所述绕组2之间设有间隙3,所述定子组件还包括有用于供绕组2散热的散热部4,所述散热部4包括有24个导热管41,24个导热管41包括18个第一热管411和6个第二热管412,其中18个第一热管411的一端连接有一散热板组42其另一端插接在相应定子槽的间隙3内,所述散热板组42沿周向均匀分布在定子铁芯1上,剩下的6个第二热管412的一端与所述支架5的肋条51连接其另一端插接在相应定子槽的间隙3内,所述间隙3内设有用于填充间隙3的导热硅脂,所述导热硅脂固结后具有粘接性、高导热性和良好绝缘性,以使得24个导热管41分别稳定插接在定子槽的间隙3内,所述导热硅脂用于将绕组2产生的热量传递至导热管41。As shown in FIGS. 1-5 , the present invention provides a stator assembly including a
具体的,所述散热板组42包括若干个间隔设置的散热片421,若干个所述散热片421上设有用于连接所述第一热管411的第一连接部,所述第一连接部包括穿设在若干个所述散热片421上的连接管422,所述连接管422上设有通孔4221,所述通孔4221供所述第一热管411插接,所述连接管422与第一热管411通过接触热传导,所述连接管422与第一热管411之间设有用于传递热量的导热硅脂。Specifically, the heat dissipation plate set 42 includes a plurality of
为了提高定子组件的散热效果,所述导热管41的材质为铜合金,所述导热管41的内腔设有导热介质,所述导热介质为水,所述散热板组42的材质为铝合金,所述支架5的材质为铝合金,由此在兼顾成本的同时能提高导热性能,利于绕组2的热量传导,便于散热。In order to improve the heat dissipation effect of the stator assembly, the material of the
所述第一热管411呈向外弯折结构,所述第一热管411连接的散热板组42远离绕组2设置,所述第二热管412朝支架5弯折,所述第一热管411和第二热管412的弯折角度413为90度,由此限定弯折角度413,使散热元件最大程度的撑开,提高散热效果。The
所述散热部4的6个第二热管412通过导热硅脂与所述支架5的肋条51连接。The six
本发明还公开了一种电机,包括上述的定子组件,所述电机为外转子电机,具有该定子组件的电机在运行时稳定温升有较大幅度的降低,且功率密度和可靠性得到大幅提升,用以解决现有技术下该类电机运行温升过高和电机功率密度低导致的无人机有效载荷不足的问题,从而提高无人机的有效载荷、续航时间和可靠性。The invention also discloses a motor including the above stator assembly, the motor is an outer rotor motor, the stable temperature rise of the motor with the stator assembly is greatly reduced during operation, and the power density and reliability are greatly improved The improvement is used to solve the problem of insufficient payload of the UAV caused by the high temperature rise of the motor and the low power density of the motor under the existing technology, thereby improving the payload, endurance and reliability of the UAV.
实施例二
如图6所示,本实施例与实施例一的不同之处在于,所述散热板组42的第一连接部包括连接板423,若干个所述散热片421设置在所述连接板423的一侧面,所述连接板423的另一侧面通过导热硅脂与所述第一热管411粘接。As shown in FIG. 6 , the difference between this embodiment and the first embodiment is that the first connecting portion of the heat
实施例三
本实施例与实施例一的不同之处在于,所述定子组件的散热部4的24个导热管41均为第一热管411,所述第一热管411远离绕组2的一端均连接一所述散热板组42。The difference between this embodiment and the first embodiment is that the 24
虽然本公开披露如上,但本公开的保护范围并非仅限于此。本领域技术人员,在不脱离本公开的精神和范围的前提下,可进行各种变更与修改,这些变更与修改均将落入本发明的保护范围。Although the present disclosure is disclosed above, the scope of protection of the present disclosure is not limited thereto. Those skilled in the art can make various changes and modifications without departing from the spirit and scope of the present disclosure, and these changes and modifications will fall within the protection scope of the present invention.
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CN116094199A (en) * | 2023-04-10 | 2023-05-09 | 湖南大学 | Multiplexing type modularized permanent magnet wind driven generator stator structure |
CN116111748A (en) * | 2023-04-10 | 2023-05-12 | 湖南大学 | A reinforced synchronous cooling stator structure |
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CN113489221A (en) * | 2021-08-03 | 2021-10-08 | 珠海格力电器股份有限公司 | Motor cooling structure, motor and compressor |
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CN113937957A (en) * | 2020-06-29 | 2022-01-14 | 上海海立电器有限公司 | Stator assembly and rotary compressor |
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CN116111748A (en) * | 2023-04-10 | 2023-05-12 | 湖南大学 | A reinforced synchronous cooling stator structure |
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