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CN118040992B - A heat dissipation motor system for underwater equipment and a design method thereof - Google Patents

A heat dissipation motor system for underwater equipment and a design method thereof Download PDF

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CN118040992B
CN118040992B CN202410439200.0A CN202410439200A CN118040992B CN 118040992 B CN118040992 B CN 118040992B CN 202410439200 A CN202410439200 A CN 202410439200A CN 118040992 B CN118040992 B CN 118040992B
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motor
rotor shaft
annular jet
heat dissipation
hole
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CN118040992A (en
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田文龙
计四维
毛昭勇
程博
李波
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Northwestern Polytechnical University
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    • 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
    • H02K9/193Arrangements for cooling or ventilating for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil with provision for replenishing the cooling medium; with means for preventing leakage of the cooling medium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/08Propulsion
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/28Design optimisation, verification or simulation using fluid dynamics, e.g. using Navier-Stokes equations or computational fluid dynamics [CFD]
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K1/00Details of the magnetic circuit
    • H02K1/06Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/22Rotating parts of the magnetic circuit
    • H02K1/32Rotating parts of the magnetic circuit with channels or ducts for flow of cooling medium
    • 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
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00Details relating to the application field
    • G06F2113/08Fluids
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2119/00Details relating to the type or aim of the analysis or the optimisation
    • G06F2119/14Force analysis or force optimisation, e.g. static or dynamic forces

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • General Engineering & Computer Science (AREA)
  • Mathematical Optimization (AREA)
  • Power Engineering (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Analysis (AREA)
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  • Aviation & Aerospace Engineering (AREA)
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  • Algebra (AREA)
  • Fluid Mechanics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Mathematical Physics (AREA)
  • Motor Or Generator Cooling System (AREA)

Abstract

The invention provides a heat dissipation motor system of an underwater device and a design method thereof, which belong to the field of motor design of the underwater device. According to the invention, the space resources of the underwater equipment are fully utilized, and no heat dissipation equipment is additionally arranged, so that the cooling system can realize self-adaptive cooling of the motor rotor assembly and the stator assembly under different sailing working conditions under the condition of greatly reducing the weight of the motor cabin section, and the working safety of the motor is ensured.

Description

一种水下装备散热电机系统及其设计方法A heat dissipation motor system for underwater equipment and a design method thereof

技术领域Technical Field

本发明属于水下装备技术领域,具体涉及一种水下装备散热电机系统及其设计方法。The invention belongs to the technical field of underwater equipment, and in particular relates to an underwater equipment heat dissipation motor system and a design method thereof.

背景技术Background technique

基于水下装备高航速和航程的需求,电机需要具备更高的输出功率和效率,电机在大功率、高转速工况下工作时会迅速产生大量热量,而一般水下装备的电机舱段具有密封性,热量若不能及时散去,电机会因过热而无法继续工作,电机过热会影响电机安全运行。Due to the requirements of high speed and range of underwater equipment, the motor needs to have higher output power and efficiency. When the motor works under high power and high speed conditions, it will quickly generate a lot of heat. The motor compartment of general underwater equipment is sealed. If the heat cannot be dissipated in time, the motor will overheat and cannot continue to work. Motor overheating will affect the safe operation of the motor.

公开号为CN208820621U的专利文献,公开一种水下用节能散热电机,该电机的冷却系统需要配备额外的冷却设备来冷却,比如散热器和冷却剂。但是,由于水下装备电机舱段为受限空间,冷却设备会占据水下装备大量内部空间,限制了舱室内其他部件的布置。此外,在水下装备高速航行时,即航速大于30Kn,所需的电机扭矩和功率急剧增大,电机产热量也随之增多,为了确保电机在高速航行时的安全运行,本领域通常会考虑设计优化冷却系统,以提高电机冷却效果,但是往往忽略了设计过程中会增加额外的重量,不利于水下装备的轻量化设计,会导致水下装备航行性能下降,需要更大的推力来维持航行速度。The patent document with publication number CN208820621U discloses an underwater energy-saving heat dissipation motor, the cooling system of which needs to be equipped with additional cooling equipment for cooling, such as a radiator and a coolant. However, since the motor compartment of the underwater equipment is a confined space, the cooling equipment will occupy a large amount of internal space of the underwater equipment, limiting the arrangement of other components in the cabin. In addition, when the underwater equipment is sailing at high speed, that is, the speed is greater than 30Kn, the required motor torque and power increase sharply, and the heat generated by the motor also increases accordingly. In order to ensure the safe operation of the motor when sailing at high speed, the art usually considers designing and optimizing the cooling system to improve the cooling effect of the motor, but often ignores that the design process will add additional weight, which is not conducive to the lightweight design of the underwater equipment, and will lead to a decrease in the navigation performance of the underwater equipment, requiring greater thrust to maintain the navigation speed.

因此,如何兼顾水下装备的航行工况、受限空间、轻量化和电机安全性能进行电机系统设计为亟需解决的问题。Therefore, how to design the motor system while taking into account the navigation conditions, confined space, lightweight and motor safety performance of underwater equipment is an urgent problem that needs to be solved.

发明内容Summary of the invention

本发明的目的在于克服现有技术未兼顾水下装备受限空间、轻量化及航行工况设计电机系统的不足之处,而提供了一种水下装备散热电机系统及其设计方法。The purpose of the present invention is to overcome the shortcomings of the prior art in that the motor system is not designed taking into account the confined space, lightweight and navigation conditions of underwater equipment, and to provide an underwater equipment heat dissipation motor system and a design method thereof.

本发明的发明构思为:The inventive concept of the present invention is:

本发明中水泵采用被动驱动方式,直接由电机转子轴驱动水泵工作,将海水通过转子轴中心孔引入散热流道内对电机进行冷却。由于水泵由电机驱动,在水下装备低速航行阶段,即一般在航速5kn左右时,电机转子轴以较低速度旋转,电机产生热量小,电机冷却系统能够随转子轴转速的提高,实现对电机热量的自适应冷却,以满足电机安全工作需求。而在水下装备高速航行阶段,即航速大于30Kn时,所需的电机扭矩和功率急剧增大,电机转子轴转速提高,电机产热量增大,水泵的压力也随转子轴速度的提高而增大,冷却效果提升,但由于转子轴转速提高后,电机产热量大幅提升,水泵的压力不足以将电机产热量散尽,导致电机温度超出安全工作要求。The water pump in the present invention adopts a passive driving mode, and the water pump is directly driven by the motor rotor shaft to work, and seawater is introduced into the heat dissipation channel through the center hole of the rotor shaft to cool the motor. Since the water pump is driven by the motor, in the low-speed navigation stage of the underwater equipment, that is, generally when the speed is about 5kn, the motor rotor shaft rotates at a relatively low speed, and the motor generates little heat. The motor cooling system can achieve adaptive cooling of the motor heat as the rotor shaft speed increases to meet the motor's safe working requirements. In the high-speed navigation stage of the underwater equipment, that is, when the speed is greater than 30kn, the required motor torque and power increase sharply, the motor rotor shaft speed increases, the motor heat generation increases, and the water pump pressure also increases with the increase of the rotor shaft speed, and the cooling effect is improved. However, after the rotor shaft speed increases, the motor heat generation increases significantly, and the water pump pressure is not enough to dissipate the motor heat generation, resulting in the motor temperature exceeding the safety working requirements.

为了解决水下装备高速航行阶段散热问题,一般对于水下装备电机系统的研究多关注冷却系统的冷却性能,即单纯通过优化冷却系统结构参数来提高散热效果,并未将其与所采用的电机结构及水下装备的总重量需求进行关联。而本发明创新性地从水下装备总重量及空间需求出发,基于水下装备采用被动泵进行冷却的应用场景,对水下装备不同航速下电机产热量和冷却系统的散热性能进行评价,对所配备的电机结构和冷却系统散热流道结构参数进行定量化设计,确保在水下装备高速航行阶段,电机温度在安全工作范围内,同时实现了水下装备电机舱段轻量化设计。In order to solve the heat dissipation problem of underwater equipment during high-speed navigation, the research on the motor system of underwater equipment generally focuses on the cooling performance of the cooling system, that is, simply improving the heat dissipation effect by optimizing the structural parameters of the cooling system, and not associating it with the adopted motor structure and the total weight requirements of the underwater equipment. However, the present invention innovatively starts from the total weight and space requirements of the underwater equipment, based on the application scenario of the underwater equipment using passive pumps for cooling, evaluates the heat generation of the motor and the heat dissipation performance of the cooling system at different speeds of the underwater equipment, and quantitatively designs the structural parameters of the motor structure and the cooling system heat dissipation flow channel to ensure that the motor temperature is within the safe working range during the high-speed navigation stage of the underwater equipment, while achieving the lightweight design of the motor compartment of the underwater equipment.

基于上述发明构思,本发明所提供的技术解决方案是:Based on the above inventive concept, the technical solution provided by the present invention is:

一种水下装备散热电机系统,其特殊之处在于,包括水下装备壳体、电机和冷却系统;所述水下装备壳体包括电机舱段和尾部舱段;An underwater equipment heat dissipation motor system, which is special in that it includes an underwater equipment shell, a motor and a cooling system; the underwater equipment shell includes a motor compartment section and a tail compartment section;

所述电机包括电机前端盖、转子组件、定子组件和电机后端盖;The motor comprises a motor front end cover, a rotor assembly, a stator assembly and a motor rear end cover;

所述电机前端盖和电机后端盖分别径向固设在电机舱段腔体两端,转子组件和定子组件同轴设置在电机前端盖和电机后端盖之间;所述转子组件具有一个转子轴,用于驱动水下装备螺旋桨旋转;The front end cover and the rear end cover of the motor are respectively fixedly arranged at two ends of the motor compartment cavity in a radial direction, and the rotor assembly and the stator assembly are coaxially arranged between the front end cover and the rear end cover of the motor; the rotor assembly has a rotor shaft for driving the propeller of the underwater equipment to rotate;

所述冷却系统为开放式被动型自适应冷却系统,包括散热流道和设置在转子轴前端的水泵;转子轴的后端伸出尾部舱段与海洋连通;The cooling system is an open passive adaptive cooling system, including a heat dissipation channel and a water pump arranged at the front end of the rotor shaft; the rear end of the rotor shaft extends out of the tail compartment and communicates with the ocean;

所述散热流道包括海水吸入孔、第一连接流道、双螺旋流道、第二连接流道和环形射流孔;双螺旋流道为对称开设在电机舱段内壁的螺旋槽;所述海水吸入孔为转子轴的中心孔;环形射流孔同轴开设在转子轴上,且沿转子轴后端开设至所述第二连接流道出口位置处;The heat dissipation channel includes a seawater suction hole, a first connecting channel, a double helical channel, a second connecting channel and an annular jet hole; the double helical channel is a spiral groove symmetrically opened on the inner wall of the motor compartment; the seawater suction hole is the central hole of the rotor shaft; the annular jet hole is coaxially opened on the rotor shaft and opened along the rear end of the rotor shaft to the outlet position of the second connecting channel;

所述水泵上设有两个流道出口,分别通过对称设置的第一连接流道与双螺旋流道的输入口连通,双螺旋流道的输出口分别通过对称设置的第二连接流道与环形射流孔连通;水泵在电机转子轴驱动下将海水从转子轴中心孔吸入,对转子组件冷却,并使海水沿双螺旋流道对定子组件冷却,冷却后从第二连接流道出口流出,通过环形射流孔排入海洋。The water pump is provided with two flow channel outlets, which are respectively connected with the input port of the double helix flow channel through symmetrically arranged first connecting flow channels, and the output ports of the double helix flow channel are respectively connected with the annular jet holes through symmetrically arranged second connecting flow channels; the water pump is driven by the motor rotor shaft to suck seawater from the central hole of the rotor shaft to cool the rotor assembly, and allows the seawater to cool the stator assembly along the double helix flow channel, and after cooling, it flows out from the second connecting flow channel outlet and is discharged into the ocean through the annular jet hole.

所述散热电机系统采用仿真优化确定,以在满足电机舱段重量和强度的要求下,使所述冷却系统在水下装备不同航行工况下对电机进行散热冷却,确保电机安全运行。The heat dissipation motor system is determined by simulation optimization so that the cooling system can dissipate heat and cool the motor under different navigation conditions of the underwater equipment while meeting the weight and strength requirements of the motor compartment, thereby ensuring the safe operation of the motor.

进一步地,所述第二连接流道包括径向开设在电机后端盖上的液流流道、唇形密封舱以及开设在转子轴上的液流孔;Furthermore, the second connecting flow channel includes a liquid flow channel radially opened on the rear end cover of the motor, a lip-shaped sealing chamber, and a liquid flow hole opened on the rotor shaft;

径向开设在电机后端盖上的液流流道两端分别与双螺旋流道的输出口和唇形密封舱连通;Two ends of the liquid flow channel radially opened on the rear end cover of the motor are respectively connected with the output port of the double helix flow channel and the lip-shaped sealing cabin;

所述唇形密封舱设置在电机后端盖中心孔内,唇形密封舱内壁与转子轴外壁过盈配合;The lip-shaped sealing cabin is arranged in the central hole of the rear end cover of the motor, and the inner wall of the lip-shaped sealing cabin is interference-fitted with the outer wall of the rotor shaft;

所述转子轴侧壁上且与唇形密封舱配合位置处径向设有若干液流孔,所述液流孔与环形射流孔连通;A plurality of liquid flow holes are radially arranged on the side wall of the rotor shaft at the position matching with the lip-shaped sealing chamber, and the liquid flow holes are connected with the annular jet hole;

经双螺旋流道排出的冷却废水,依次经过电机后端盖上的液流流道、唇形密封舱、液流孔和环形射流孔排入海洋中。The cooling waste water discharged through the double helix flow channel is discharged into the ocean through the liquid flow channel, lip-shaped sealing cabin, liquid flow hole and annular jet hole on the rear end cover of the motor in sequence.

进一步地,所述转子组件包括所述转子轴、转子铁芯和永磁体;转子轴、转子铁芯和永磁体依次同轴由内向外嵌套固连;Furthermore, the rotor assembly comprises the rotor shaft, the rotor core and the permanent magnet; the rotor shaft, the rotor core and the permanent magnet are coaxially nested and fixedly connected from the inside to the outside in sequence;

所述定子组件套装在所述转子组件外壁上,且定子组件与转子组件之间存在间隙,定子组件包括定子铁芯和定子绕组,所述定子铁芯外壁固定在所述电机舱段内壁上,定子铁芯内绕制有所述定子绕组;在所述永磁体和定子绕组的磁力作用下,所述转子铁芯、永磁体和转子轴一起转动,转子轴带动所述水下装备的螺旋桨旋转。The stator assembly is sleeved on the outer wall of the rotor assembly, and there is a gap between the stator assembly and the rotor assembly. The stator assembly includes a stator core and a stator winding. The outer wall of the stator core is fixed to the inner wall of the motor compartment section, and the stator winding is wound inside the stator core. Under the magnetic force of the permanent magnet and the stator winding, the rotor core, the permanent magnet and the rotor shaft rotate together, and the rotor shaft drives the propeller of the underwater equipment to rotate.

进一步地,所述海水吸入孔与所述环形射流孔的截面积比为3:1。Furthermore, the cross-sectional area ratio of the seawater suction hole to the annular jet hole is 3:1.

进一步地,为确保转子轴的内壁面强度,所述海水吸入孔与所述环形射流孔之间壁厚不小于8毫米。Furthermore, in order to ensure the inner wall strength of the rotor shaft, the wall thickness between the seawater suction hole and the annular jet hole is not less than 8 mm.

进一步地,所述转子轴的后段轴体通过设置在水下装备尾部舱段内的一滑动轴承与尾部舱段连接,该滑动轴承一端面与尾部舱段内端面贴合;Furthermore, the rear shaft of the rotor shaft is connected to the tail compartment through a sliding bearing arranged in the tail compartment of the underwater equipment, and one end face of the sliding bearing is in contact with the inner end face of the tail compartment;

所述尾部舱段腔室内径向设有与尾部舱段本体固定连接的固定支架,所述转子轴的中段轴体与所述固定支架中心孔通过另一滑动轴承连接。A fixing bracket fixedly connected to the tail compartment body is radially provided in the tail compartment chamber, and the middle shaft body of the rotor shaft is connected to the center hole of the fixing bracket through another sliding bearing.

进一步地,所述固定支架整体为圆盘状,固定支架上沿轴线开设中心孔,通过滑动轴承与转子轴外壁连接;Furthermore, the fixing bracket is in the shape of a disk as a whole, a center hole is provided on the fixing bracket along the axis, and the fixing bracket is connected to the outer wall of the rotor shaft through a sliding bearing;

所述固定支架侧壁径向设有若干连接杆,连接杆端部与设置在电机舱段内壁上的凸耳连接。A plurality of connecting rods are radially arranged on the side wall of the fixing bracket, and the ends of the connecting rods are connected to lugs arranged on the inner wall of the motor compartment section.

本发明还提供上述散热电机系统的设计方法,其特殊之处在于,包括以下步骤:The present invention also provides a design method for the above heat dissipation motor system, which is special in that it includes the following steps:

步骤1:根据水下装备电机舱段空间和整体重量要求,为电机舱段配置电机,确定电机的电磁结构;Step 1: According to the space and overall weight requirements of the motor compartment of the underwater equipment, configure the motor for the motor compartment and determine the electromagnetic structure of the motor;

建立电机与水下装备壳体的仿真模型,初始设定所述模型中散热流道的结构参数;所述结构参数包括双螺旋流道的螺距、深度、截面尺寸和螺旋倾角,以及海水吸入孔和环形射流孔的截面尺寸;A simulation model of the motor and the underwater equipment shell is established, and structural parameters of the heat dissipation channel in the model are initially set; the structural parameters include the pitch, depth, cross-sectional dimensions and spiral inclination of the double helical channel, and the cross-sectional dimensions of the seawater intake hole and the annular jet hole;

初始设定所述海水吸入孔与环形射流孔截面积比为1;The cross-sectional area ratio of the seawater suction hole to the annular jet hole is initially set to 1;

步骤2:通过仿真计算,获取电机在水下装备以不同航速Vi高速航行工作时,散热流道的温度场参数,以及定子绕组、定子铁芯和转子铁芯的最高温度Ti;其中i=1,2,3,…,n;Step 2: Through simulation calculation, obtain the temperature field parameters of the heat dissipation channel and the maximum temperature Ti of the stator winding, stator core and rotor core when the motor is working at high speed Vi under water; where i=1, 2, 3, ..., n;

步骤3:基于步骤2得到的温度场参数,判断在不同航速Vi下,定子绕组、定子铁芯和转子铁芯的最高温度Ti是否满足电机设计要求,若满足,则进入步骤5;否则,进入步骤4调整散热流道参数;Step 3: Based on the temperature field parameters obtained in step 2, determine whether the maximum temperatures Ti of the stator winding, stator core, and rotor core meet the motor design requirements at different speeds Vi . If yes, proceed to step 5; otherwise, proceed to step 4 to adjust the heat dissipation channel parameters.

步骤4:以缩小双螺旋流道螺距和/或增大双螺旋流道截面尺寸的方式调整所述散热流道参数,调整后在电机舱段壳体满足强度设计要求的情况下,返回执行步骤2和步骤3,判断定子绕组、定子铁芯和转子铁芯的最高温度Ti是否满足电机设计要求,若满足则进入步骤5;否则,返回步骤1,重新确定电机的电磁结构;Step 4: Adjust the heat dissipation channel parameters by reducing the pitch of the double helix channel and/or increasing the cross-sectional size of the double helix channel. After the adjustment, if the motor compartment shell meets the strength design requirements, return to step 2 and step 3 to determine whether the maximum temperature Ti of the stator winding, the stator core and the rotor core meets the motor design requirements. If so, proceed to step 5; otherwise, return to step 1 and redetermine the electromagnetic structure of the motor.

步骤5:计算获取双螺旋流道的沿程流阻和散热流道弯折处的局部流阻,并判断沿程流阻和局部流阻是否处于水泵的Q-H特性曲线(Q为水泵的流量,H为水泵的扬程)范围之内,若是,则获得所需散热电机系统;否则,调节所述海水吸入孔与环形射流孔的截面尺寸,直至调节后能够使双螺旋流道的沿程流阻及散热流道弯折处的局部流阻处于水泵的Q-H特性曲线范围之内。Step 5: Calculate and obtain the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel, and determine whether the flow resistance along the flow channel and the local flow resistance are within the range of the Q-H characteristic curve of the water pump (Q is the flow rate of the water pump, and H is the head of the water pump). If so, the required heat dissipation motor system is obtained; otherwise, adjust the cross-sectional dimensions of the seawater suction hole and the annular jet hole until the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel are within the range of the Q-H characteristic curve of the water pump after adjustment.

进一步地,步骤5中调节所述海水吸入孔与环形射流孔的截面尺寸的具体过程为:Furthermore, the specific process of adjusting the cross-sectional dimensions of the seawater suction hole and the annular jet hole in step 5 is as follows:

步骤5.1:设定海水吸入孔与环形射流孔截面积比的调节步进,基于调节步进,计算获得海水吸入孔与环形射流孔的截面尺寸;Step 5.1: setting the adjustment step of the cross-sectional area ratio of the seawater intake hole to the annular jet hole, and calculating and obtaining the cross-sectional dimensions of the seawater intake hole and the annular jet hole based on the adjustment step;

步骤5.2:通过仿真计算,获取双螺旋流道的沿程流阻和散热流道弯折处的局部流阻,判断沿程流阻和局部流阻是否处于水泵的Q-H特性曲线范围之内:Step 5.2: Through simulation calculation, obtain the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel, and determine whether the flow resistance along the flow channel and the local flow resistance are within the range of the Q-H characteristic curve of the water pump:

若是,则按照步骤5.1不断增大海水吸入孔与环形射流孔的截面积比,直至沿程流阻和局部流阻大于水泵的Q-H特性曲线范围的最大值;If yes, then continue to increase the cross-sectional area ratio of the seawater suction hole to the annular jet hole according to step 5.1 until the flow resistance along the way and the local flow resistance are greater than the maximum value of the Q-H characteristic curve range of the water pump;

若否,则此时海水吸入孔与环形射流孔的截面积比为极限比例,取处于水泵的Q-H特性曲线范围内的最大海水吸入孔与环形射流孔的截面积比,作为海水吸入孔与环形射流孔的最优截面积比,并以此最优截面积比计算获得所述海水吸入孔与环形射流孔的截面尺寸。If not, then the cross-sectional area ratio of the seawater suction hole to the annular jet hole is a limit ratio. The maximum cross-sectional area ratio of the seawater suction hole to the annular jet hole within the Q-H characteristic curve of the water pump is taken as the optimal cross-sectional area ratio of the seawater suction hole to the annular jet hole, and the cross-sectional dimensions of the seawater suction hole and the annular jet hole are calculated based on this optimal cross-sectional area ratio.

本发明的优点是:The advantages of the present invention are:

1.本发明中水泵设置在电机转子轴上,以转子轴中心孔作为海水吸入孔,水下装备电机舱段壳体内壁上开设双螺旋流道,双螺旋流道与定子组件外壁接触,设置在转子轴端部的水泵在电机驱动下将海洋水通过转子轴中心孔吸入,直接对转子组件进行散热冷却;海洋水通过水泵流道出口与双螺旋流道连通,实现对定子组件散热冷却;双螺旋流道输出口通过设置在电机后端盖上的液流流道与转子轴上的环形射流孔连通,使冷却废水排向海洋。本发明充分利用了水下装备自身空间资源,无需额外配备散热装置,在大大减轻了水下装备电机舱段重量的情况下,使得冷却系统在不同航行工况下对电机转子组件和定子组件实现冷却,确保了电机安全运行。水泵在电机转子轴驱动作用下工作,使得冷却系统被动地根据所述电机的输出功率自适应地对电机进行冷却。此外,由于本发明中双螺旋流道开设在水下装备电机舱段壳体内壁上,水下装备电机舱段壳体替代电机壳体,在通过双螺旋流道内海水冷却的同时,电机舱段外壁直接与海洋接触实现热量交换,大大提高了散热流道的散热效果。1. In the present invention, the water pump is arranged on the motor rotor shaft, and the central hole of the rotor shaft is used as the seawater suction hole. A double helical flow channel is provided on the inner wall of the motor compartment shell of the underwater equipment, and the double helical flow channel contacts the outer wall of the stator assembly. The water pump arranged at the end of the rotor shaft sucks the ocean water through the central hole of the rotor shaft under the drive of the motor, and directly dissipates and cools the rotor assembly; the ocean water is connected with the double helical flow channel through the outlet of the water pump flow channel to achieve heat dissipation and cooling of the stator assembly; the output port of the double helical flow channel is connected with the annular jet hole on the rotor shaft through the liquid flow channel arranged on the rear end cover of the motor, so that the cooling wastewater is discharged to the ocean. The present invention makes full use of the space resources of the underwater equipment itself, and does not need to be equipped with an additional heat dissipation device. While greatly reducing the weight of the motor compartment of the underwater equipment, the cooling system can cool the motor rotor assembly and the stator assembly under different navigation conditions, ensuring the safe operation of the motor. The water pump works under the driving action of the motor rotor shaft, so that the cooling system passively and adaptively cools the motor according to the output power of the motor. In addition, since the double helix flow channel in the present invention is opened on the inner wall of the motor compartment shell of the underwater equipment, the motor compartment shell of the underwater equipment replaces the motor shell. While the seawater in the double helix flow channel is cooled, the outer wall of the motor compartment is in direct contact with the ocean to achieve heat exchange, which greatly improves the heat dissipation effect of the heat dissipation flow channel.

2.本发明中双螺旋流道对称设置,海水通过双螺旋流道对向流动,增加了流体的湍流效应,有利于流体的均匀分布,加快了电机及电机舱段内热量的传递和散发,提高了电机冷却效果,确保了电机的使用安全性。2. The double helix flow channels of the present invention are symmetrically arranged, and seawater flows in opposite directions through the double helix flow channels, which increases the turbulence effect of the fluid, is conducive to the uniform distribution of the fluid, accelerates the transfer and dissipation of heat in the motor and the motor compartment, improves the cooling effect of the motor, and ensures the safety of the motor.

3.本发明中双螺旋流道输出口通过第二连接流道与开设在转子轴上的环形射流孔连通,所述环形射流孔与转子轴的中心孔同轴设计,使得冷却废水在排出的同时能够给水下装备提供轴向的推动力,大大提高了航行器动力系统的工作效率。3. In the present invention, the outlet of the double helical flow channel is connected to the annular jet hole provided on the rotor shaft through the second connecting flow channel. The annular jet hole is coaxially designed with the central hole of the rotor shaft, so that the cooling wastewater can provide axial propulsion to the underwater equipment while being discharged, greatly improving the working efficiency of the vehicle power system.

4.本发明散热电机系统不仅适用于水下航行器,例如AUV、UUV,也适用于鱼雷等其他水下装备。其中,AUV为自主式水下潜器(Autonomous Underwater Vehicle,简称AUV),UUV为无人水下航行器(Unmanned Underwater Vehicle,简称UUV)。4. The heat dissipation motor system of the present invention is not only applicable to underwater vehicles, such as AUV and UUV, but also to other underwater equipment such as torpedoes. AUV is an autonomous underwater vehicle (AUV for short), and UUV is an unmanned underwater vehicle (UUV for short).

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

图1是本发明实施例中航行器外形立体示意图;FIG1 is a perspective schematic diagram of the appearance of an aircraft in an embodiment of the present invention;

图2是本发明实施例中散热电机系统立体结构四分之一剖视图,为体现双螺旋流道结构形式,本图保留了剖切掉的双螺旋流道结构;FIG2 is a quarter cross-sectional view of the three-dimensional structure of the heat dissipation motor system according to an embodiment of the present invention. In order to reflect the double helical flow channel structure, this figure retains the cut-away double helical flow channel structure;

图3是本发明实施例中散热电机系统沿轴向的二维全剖视图;3 is a two-dimensional full cross-sectional view along the axial direction of the heat dissipation motor system according to an embodiment of the present invention;

图4是本发明散热流道内海水流向示意图。FIG. 4 is a schematic diagram of the flow direction of seawater in the heat dissipation channel of the present invention.

附图标记说明:1-水泵;2-转子轴;201-海水吸入孔;202-环形射流孔;3-第一连接流道;4-双螺旋流道;401-上螺旋流道;402-下螺旋流道;5-第二连接流道;6-唇形密封舱;7-电机前端盖;8-转子铁芯;9-定子组件;10-永磁体;11-电机后端盖;12-滑动轴承;13-固定支架;14-电机舱段;15-尾部舱段。Explanation of the reference numerals: 1-water pump; 2-rotor shaft; 201-seawater suction hole; 202-annular jet hole; 3-first connecting flow channel; 4-double helical flow channel; 401-upper spiral flow channel; 402-lower spiral flow channel; 5-second connecting flow channel; 6-lip-shaped sealing cabin; 7-motor front end cover; 8-rotor core; 9-stator assembly; 10-permanent magnet; 11-motor rear end cover; 12-sliding bearing; 13-fixed bracket; 14-motor compartment section; 15-tail compartment section.

具体实施方式Detailed ways

下面以水下航行器为例,详细描述本发明的实施例,所述实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。An embodiment of the present invention is described in detail below by taking an underwater vehicle as an example. The embodiment is exemplary and is intended to be used to explain the present invention, but should not be construed as limiting the present invention.

参照图1-图3,一种水下航行器散热电机系统,包括水下航行器壳体、电机和冷却系统;1-3, an underwater vehicle heat dissipation motor system includes an underwater vehicle housing, a motor and a cooling system;

水下航行器壳体包括电机舱段14和尾部舱段15;The underwater vehicle housing includes a motor compartment section 14 and a tail compartment section 15;

所述电机包括电机前端盖7、转子组件、定子组件9和电机后端盖11;The motor comprises a motor front end cover 7, a rotor assembly, a stator assembly 9 and a motor rear end cover 11;

所述电机前端盖7和电机后端盖11分别径向固设在所述电机舱段14腔体两端,所述转子组件和定子组件9同轴设置在电机前端盖7和电机后端盖11之间;The motor front end cover 7 and the motor rear end cover 11 are radially fixed at both ends of the motor compartment section 14 cavity, and the rotor assembly and the stator assembly 9 are coaxially arranged between the motor front end cover 7 and the motor rear end cover 11;

所述转子组件包括转子轴2、转子铁芯8和永磁体10;所述转子轴2、转子铁芯8和永磁体10依次同轴由内向外嵌套固连为一体;The rotor assembly includes a rotor shaft 2, a rotor core 8 and a permanent magnet 10; the rotor shaft 2, the rotor core 8 and the permanent magnet 10 are coaxially nested and fixedly connected from the inside to the outside in sequence;

所述定子组件9套装在所述转子组件外壁上,且定子组件内壁与转子组件外壁之间存在间隙。定子组件9包括定子铁芯和定子绕组,所述定子铁芯外壁固定在所述电机舱段14内壁上,定子铁芯内绕制有所述定子绕组。在所述永磁体10和定子绕组的磁力作用下,所述转子铁芯8、永磁体10和转子轴2一起转动,转子轴2带动水下航行器的螺旋桨旋转。需要说明的是,图中未示出水下航行器的螺旋桨。The stator assembly 9 is mounted on the outer wall of the rotor assembly, and there is a gap between the inner wall of the stator assembly and the outer wall of the rotor assembly. The stator assembly 9 includes a stator core and a stator winding. The outer wall of the stator core is fixed to the inner wall of the motor compartment section 14, and the stator winding is wound inside the stator core. Under the magnetic force of the permanent magnet 10 and the stator winding, the rotor core 8, the permanent magnet 10 and the rotor shaft 2 rotate together, and the rotor shaft 2 drives the propeller of the underwater vehicle to rotate. It should be noted that the propeller of the underwater vehicle is not shown in the figure.

所述冷却系统采用开放式被动型冷却系统,该冷却系统包括散热流道和水泵1,所述水泵1设置在转子轴2前端,在电机转子轴驱动作用下被动工作。转子轴2后端伸出尾部舱段15壳体外与海洋连通;所述转子轴2尾段轴体通过设置在尾部舱段15内的一滑动轴承12与尾部舱段壳体连接,该滑动轴承12端面与尾部舱段15壳体内端面贴合。尾部舱段15腔室内径向设有与尾部舱段壳体固定连接的固定支架13,所述转子轴2轴体与所述固定支架13中心孔通过另一滑动轴承12连接。The cooling system adopts an open passive cooling system, which includes a heat dissipation channel and a water pump 1. The water pump 1 is arranged at the front end of the rotor shaft 2 and works passively under the driving action of the motor rotor shaft. The rear end of the rotor shaft 2 extends out of the shell of the tail section 15 and communicates with the ocean; the shaft body of the tail section of the rotor shaft 2 is connected to the shell of the tail section through a sliding bearing 12 arranged in the tail section 15, and the end face of the sliding bearing 12 is in contact with the inner end face of the shell of the tail section 15. A fixing bracket 13 fixedly connected to the shell of the tail section is radially arranged in the chamber of the tail section 15, and the shaft body of the rotor shaft 2 is connected to the center hole of the fixing bracket 13 through another sliding bearing 12.

所述固定支架13整体为圆盘状,中部沿轴线开设中心孔,通过滑动轴承与所述转子轴2外壁连接。所述固定支架13侧壁径向设有若干连接杆,连接杆端部与设置在水下航行器壳体内壁上的凸耳连接。The fixing bracket 13 is disc-shaped as a whole, with a central hole in the middle along the axis, and connected to the outer wall of the rotor shaft 2 through a sliding bearing. The side wall of the fixing bracket 13 is radially provided with a plurality of connecting rods, and the ends of the connecting rods are connected to the lugs arranged on the inner wall of the underwater vehicle shell.

所述散热流道包括海水吸入孔201、第一连接流道3、双螺旋流道4、第二连接流道5和环形射流孔202。The heat dissipation channel includes a seawater suction hole 201 , a first connecting channel 3 , a double helical channel 4 , a second connecting channel 5 and an annular jet hole 202 .

所述海水吸入孔201为转子轴2上沿轴线开设的中心孔,海水吸入孔201与水泵1液流入口连接。所述转子轴2上开有环形射流孔202,所述环形射流孔202与所述海水吸入孔201同轴设置,且环形射流孔沿转子轴2后端面开设至电机后端盖11位置处。所述转子轴2侧壁上且位于电机后端盖位置处径向设有若干液流孔,所述液流孔与环形射流孔连通。为了确保转子轴的机械强度,本实施例中,所述海水吸入孔201与环形射流孔的截面积比优选取为3:1。由于海水吸入孔201与环形射流孔之间的壁厚太小,会降低转子轴2壁面强度;壁厚太大,则会造成结构集成度低。因此,海水吸入孔与环形射流孔之间壁厚不小于8毫米。The seawater suction hole 201 is a central hole opened along the axis of the rotor shaft 2, and the seawater suction hole 201 is connected to the liquid flow inlet of the water pump 1. An annular jet hole 202 is opened on the rotor shaft 2, and the annular jet hole 202 is coaxially arranged with the seawater suction hole 201, and the annular jet hole is opened along the rear end face of the rotor shaft 2 to the position of the rear end cover 11 of the motor. A plurality of liquid flow holes are radially arranged on the side wall of the rotor shaft 2 and located at the rear end cover of the motor, and the liquid flow holes are connected to the annular jet hole. In order to ensure the mechanical strength of the rotor shaft, in this embodiment, the cross-sectional area ratio of the seawater suction hole 201 to the annular jet hole is preferably taken as 3:1. If the wall thickness between the seawater suction hole 201 and the annular jet hole is too small, the wall strength of the rotor shaft 2 will be reduced; if the wall thickness is too large, the structural integration will be low. Therefore, the wall thickness between the seawater suction hole and the annular jet hole is not less than 8 mm.

电机舱段14内壁上对称开有两个螺旋槽,所述螺旋槽顶壁与定子组件9外壁贴合固定,形成所述双螺旋流道4,所述双螺旋流道包括上螺旋流道401和下螺旋流道402,两个螺旋流道的螺距、深度、螺旋倾角和截面参数相同。双螺旋流道4的设计,增加了流体的湍流效应,有利于流体的均匀分布,加快了热量的传递和散发,实现电机高效、均衡降温。Two spiral grooves are symmetrically opened on the inner wall of the motor compartment section 14, and the top wall of the spiral groove is fixedly fitted with the outer wall of the stator assembly 9 to form the double spiral flow channel 4, which includes an upper spiral flow channel 401 and a lower spiral flow channel 402. The pitch, depth, spiral inclination and cross-sectional parameters of the two spiral flow channels are the same. The design of the double spiral flow channel 4 increases the turbulent effect of the fluid, is conducive to the uniform distribution of the fluid, accelerates the transfer and dissipation of heat, and realizes efficient and balanced cooling of the motor.

所述水泵1上开有两个流道出口,分别通过两个对称开设在电机舱段14前端内壁的第一连接流道3与上螺旋流道401和下螺旋流道402的输入口连通,上螺旋流道401和下螺旋流道402的输出口分别通过对称设置在电机后端盖11上的第二连接流道5与环形射流孔202连通。工作时,水泵中叶轮转速与电机转子轴的转速相同,当电机输出功率越大时,叶轮转速越大,增大了海水在散热流道内的流速,电机冷却效果也随之提高。The water pump 1 has two flow channel outlets, which are connected to the input ports of the upper spiral flow channel 401 and the lower spiral flow channel 402 through two first connecting flow channels 3 symmetrically opened on the inner wall of the front end of the motor compartment section 14, and the output ports of the upper spiral flow channel 401 and the lower spiral flow channel 402 are connected to the annular jet hole 202 through the second connecting flow channels 5 symmetrically arranged on the rear end cover 11 of the motor. When working, the impeller speed in the water pump is the same as the speed of the motor rotor shaft. When the motor output power is greater, the impeller speed is greater, which increases the flow rate of seawater in the heat dissipation channel, and the motor cooling effect is also improved.

由于转动的转子轴不能直接与固定设置的第二连接流道5连接,因此,在电机后端盖11中心孔内设置唇形密封舱6,所述转子轴2外壁与所述唇形密封舱6中心孔通过过盈配合方式连接。第二连接流道5出口端通过唇形密封舱6的腔室与设置在转子轴上的液流孔连通,使得冷却废水能够经过唇形密封舱和液流孔流入环形射流孔202内,最后排入海洋。Since the rotating rotor shaft cannot be directly connected to the fixed second connecting flow channel 5, a lip seal cabin 6 is provided in the center hole of the motor rear end cover 11, and the outer wall of the rotor shaft 2 is connected to the center hole of the lip seal cabin 6 by interference fit. The outlet end of the second connecting flow channel 5 is connected to the liquid flow hole provided on the rotor shaft through the chamber of the lip seal cabin 6, so that the cooling wastewater can flow into the annular jet hole 202 through the lip seal cabin and the liquid flow hole, and finally discharged into the ocean.

参照图4,工作时,所述水泵1在电机转子轴驱动下被动工作,将海水通过转子轴2上的海水吸入孔201吸入,海水通过海水吸入孔流入过程中对转子组件进行冷却;海水通过水泵1上的两个流道出口,分别通过竖向对称设置的第一连接流道3流入到上螺旋流道401和下螺旋流道402中,对定子组件9进行冷却;冷却废水从双螺旋流道流出,通过设置在电机后端盖11上的第二连接流道5流入到唇形密封舱6内进行液体交换,然后通过转子轴上的液流孔经过环形射流孔202流排入海洋中。同时,由于双螺旋流道开设在水下航行器电机舱段15内壁上,水下航行器壳体直接与海洋水接触,双螺旋流道内海洋水与水下航行器壳体外海洋水存在热量交换,降低了双螺旋流道内海洋水的温度,进一步提高了对电机及电机舱段舱室内热量的散发,提高了冷却效果。本发明冷却系统实现电机均匀散热的同时,由于冷却废水通过设置在转子轴上的环形射流孔排出,提供了航行器前行推力,提高了水下航行器动力系统的效率。Referring to FIG4 , when working, the water pump 1 works passively under the drive of the motor rotor shaft, sucks seawater through the seawater suction hole 201 on the rotor shaft 2, and the seawater cools the rotor assembly during the process of flowing in through the seawater suction hole; the seawater flows into the upper spiral flow channel 401 and the lower spiral flow channel 402 through the two flow channel outlets on the water pump 1, respectively, through the first connecting flow channel 3 arranged vertically symmetrically, to cool the stator assembly 9; the cooling wastewater flows out from the double helical flow channel, flows into the lip seal cabin 6 through the second connecting flow channel 5 arranged on the rear end cover 11 of the motor for liquid exchange, and then flows through the liquid flow hole on the rotor shaft through the annular jet hole 202 and is discharged into the ocean. At the same time, since the double helical flow channel is opened on the inner wall of the motor compartment 15 of the underwater vehicle, the shell of the underwater vehicle is in direct contact with the ocean water, and there is heat exchange between the ocean water in the double helical flow channel and the ocean water outside the shell of the underwater vehicle, which reduces the temperature of the ocean water in the double helical flow channel, further improves the heat dissipation in the motor and the motor compartment, and improves the cooling effect. The cooling system of the present invention realizes uniform heat dissipation of the motor. At the same time, since the cooling waste water is discharged through the annular jet holes arranged on the rotor shaft, it provides forward thrust for the vehicle and improves the efficiency of the underwater vehicle power system.

为了最大限度地减小冷却系统对航行器整体重量的影响,以提高航行器的机动性能和航程性能,需使所设计的电机结构轻小化。另外,由于水下航行器的航行工况不同,实际搭载的电机对散热的要求亦不同。为提高散热效果,可通过缩小螺旋流道的螺距或增大螺旋流道深度和截面尺寸来获得更大的散热表面积,同时根据实际电机性能参数,优化调整双螺旋流道的螺距、螺旋倾角、截面尺寸和深度,来改变海水流动的速度和方向,以提高冷却效果,同时还要使开设在水下航行器壳体内壁上的双螺旋流道不会降低水下航行器壳体强度,以避免水下航行器在航行时因电机的振动产生轻微摆动。In order to minimize the impact of the cooling system on the overall weight of the vehicle and to improve the maneuverability and range performance of the vehicle, the motor structure needs to be designed to be lightweight. In addition, due to the different navigation conditions of underwater vehicles, the actual motors carried have different requirements for heat dissipation. To improve the heat dissipation effect, a larger heat dissipation surface area can be obtained by reducing the pitch of the spiral flow channel or increasing the depth and cross-sectional size of the spiral flow channel. At the same time, according to the actual motor performance parameters, the pitch, spiral inclination, cross-sectional size and depth of the double helix flow channel are optimized and adjusted to change the speed and direction of seawater flow to improve the cooling effect. At the same time, the double helix flow channel opened on the inner wall of the underwater vehicle shell will not reduce the strength of the underwater vehicle shell to avoid slight swinging of the underwater vehicle due to the vibration of the motor during navigation.

另外,由于水流的突然改变会在散热流道内产生瞬时的压力变化,被称为水击力。在其他条件不变的情况下,水流速度增大,水击力也会增大。水击力可能对流道造成损坏,尤其在双螺旋流道与环形射流孔的连接位置,水流以90°的角度射入环形流射孔内,水击力的突然增大会对转子轴造成严重损害。In addition, the sudden change of water flow will produce instantaneous pressure changes in the heat dissipation flow channel, which is called water hammer. When other conditions remain unchanged, the water hammer will increase as the water flow velocity increases. Water hammer may damage the flow channel, especially at the connection position between the double helix flow channel and the annular jet hole, where the water flow enters the annular jet hole at an angle of 90°. The sudden increase of water hammer will cause serious damage to the rotor shaft.

因此,在设计确定环形射流孔的大小时,需要根据实际搭载的电机,考虑流阻和水泵的负荷关系,尽可能扩大进出口压差,以达到使水流推进航行器的作用。本实施例通过设计获得合适的海水吸入孔与环形射流孔的截面尺寸,既使得散热流道的流阻处于水泵Q-H特性曲线(Q为水泵的流量,H为水泵的扬程)范围之内,又使得尽可能对水下航行器提供更大的前行推力。Therefore, when designing and determining the size of the annular jet hole, it is necessary to consider the relationship between the flow resistance and the load of the water pump according to the actual motor carried, and to maximize the inlet and outlet pressure difference to achieve the effect of the water flow propelling the vehicle. This embodiment obtains appropriate cross-sectional dimensions of the seawater intake hole and the annular jet hole by design, so that the flow resistance of the heat dissipation flow channel is within the range of the water pump Q-H characteristic curve (Q is the flow rate of the water pump, and H is the head of the water pump), and provides a greater forward thrust to the underwater vehicle as much as possible.

基于上述考虑,本实施例提供上述水下航行器散热电机系统的设计方法,具体包括以下步骤:Based on the above considerations, this embodiment provides a design method for the above underwater vehicle heat dissipation motor system, which specifically includes the following steps:

步骤1:根据水下航行器电机舱段空间和整体重量要求,为电机舱段配置电机,确定电机的电磁结构;Step 1: According to the space and overall weight requirements of the motor compartment of the underwater vehicle, configure the motor for the motor compartment and determine the electromagnetic structure of the motor;

建立电机与水下航行器壳体的仿真模型;初始设定所述模型中散热流道的结构参数;所述结构参数包括双螺旋流道的螺距、深度、截面尺寸和螺旋倾角,以及海水吸入孔和环形射流孔的截面尺寸;Establishing a simulation model of the motor and the underwater vehicle shell; initially setting the structural parameters of the heat dissipation channel in the model; the structural parameters include the pitch, depth, cross-sectional dimensions and spiral inclination of the double helical channel, and the cross-sectional dimensions of the seawater intake hole and the annular jet hole;

初始设定所述海水吸入孔与环形射流孔截面积比为1;The cross-sectional area ratio of the seawater suction hole to the annular jet hole is initially set to 1;

步骤2,通过仿真计算,获取电机在水下航行器以不同航速Vi航行工作时,散热流道的温度场参数,以及定子绕组、定子铁芯和转子铁芯的最高温度Ti;其中i=1,2,3,…,n。考虑在水下航行器低速航行时定子绕组产热量较大,高速航行时定子铁芯和转子铁芯的产热量较大,因此,我们只关注定子绕组、定子铁芯和转子铁芯的最高温度是否处于电机安全工作温度范围。Step 2, through simulation calculation, obtain the temperature field parameters of the heat dissipation channel and the maximum temperature Ti of the stator winding, stator core and rotor core when the motor is working at different speeds Vi of the underwater vehicle; where i=1, 2, 3, ..., n. Considering that the stator winding generates a large amount of heat when the underwater vehicle is sailing at a low speed, and the stator core and rotor core generate a large amount of heat when the underwater vehicle is sailing at a high speed, therefore, we only focus on whether the maximum temperature of the stator winding, stator core and rotor core is within the safe operating temperature range of the motor.

步骤3,基于步骤2得到的温度场参数,判断在不同航速Vi下,定子绕组、定子铁芯和转子铁芯的最高温度Ti是否满足电机安全工作温度设计要求,若满足,则进入步骤5;否则,进入步骤4调整散热流道参数;Step 3, based on the temperature field parameters obtained in step 2, determine whether the maximum temperatures Ti of the stator winding, stator core, and rotor core meet the design requirements for the safe operating temperature of the motor at different speeds Vi . If yes, proceed to step 5; otherwise, proceed to step 4 to adjust the heat dissipation channel parameters;

步骤4,以缩小双螺旋流道螺距和/或增大双螺旋流道截面尺寸的方式调整所述散热流道参数,调整后在电机舱段壳体满足强度设计要求的情况下,返回执行步骤2和步骤3,判断定子绕组、定子铁芯和转子铁芯的最高温度Ti是否满足电机安全工作温度设计要求,若满足则进入步骤5;否则,返回步骤1,重新确定电机的电磁结构;Step 4, adjusting the heat dissipation channel parameters by reducing the pitch of the double helix channel and/or increasing the cross-sectional size of the double helix channel. After the adjustment, if the motor compartment shell meets the strength design requirements, return to step 2 and step 3 to determine whether the maximum temperature Ti of the stator winding, the stator core and the rotor core meets the motor safe operating temperature design requirements. If so, proceed to step 5; otherwise, return to step 1 and redetermine the electromagnetic structure of the motor;

步骤5,计算获取双螺旋流道的沿程流阻和散热流道弯折处的局部流阻,并判断沿程流阻和局部流阻是否处于水泵的Q-H特性曲线范围之内:若是,则获得所需散热电机系统;否则,调节所述海水吸入孔与环形射流孔的截面尺寸,直至调节后能够使双螺旋流道的沿程流阻及散热流道弯折处的局部流阻处于水泵的Q-H特性曲线范围之内。Step 5, calculate and obtain the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel, and determine whether the flow resistance along the flow channel and the local flow resistance are within the range of the Q-H characteristic curve of the water pump: if so, the required heat dissipation motor system is obtained; otherwise, adjust the cross-sectional dimensions of the seawater suction hole and the annular jet hole until the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel are within the range of the Q-H characteristic curve of the water pump after adjustment.

所述步骤5中,通过调节海水吸入孔与环形射流孔的截面尺寸,使得使双螺旋流道的沿程流阻及散热流道弯折处的局部流阻处于水泵的Q-H特性曲线范围之内的具体过程为:In step 5, the specific process of adjusting the cross-sectional dimensions of the seawater suction hole and the annular jet hole so that the flow resistance along the double helical flow channel and the local flow resistance at the bend of the heat dissipation flow channel are within the range of the Q-H characteristic curve of the water pump is as follows:

步骤5.1,设定海水吸入孔与环形射流孔截面积比的调节步进,基于调节步进,计算获得海水吸入孔与环形射流孔的截面尺寸。本实施例中,比例调节步进取0.5,也可以缩小比例调节步进以获得更精确的设计参数;Step 5.1, set the adjustment step of the cross-sectional area ratio of the seawater intake hole and the annular jet hole, and calculate the cross-sectional dimensions of the seawater intake hole and the annular jet hole based on the adjustment step. In this embodiment, the proportional adjustment step is 0.5, and the proportional adjustment step can also be reduced to obtain more accurate design parameters;

步骤5.2,通过仿真计算,获取双螺旋流道的沿程流阻和散热流道弯折处的局部流阻,判断沿程流阻和局部流阻是否处于水泵的Q-H特性曲线范围之内:Step 5.2, through simulation calculation, obtain the flow resistance along the double helix flow channel and the local flow resistance at the bend of the heat dissipation flow channel, and determine whether the flow resistance along the flow channel and the local flow resistance are within the range of the Q-H characteristic curve of the water pump:

若是,则按照步骤5.1不断增大海水吸入孔与环形射流孔的截面积比,直至沿程流阻和局部流阻大于水泵的Q-H特性曲线范围的最大值;If yes, then continue to increase the cross-sectional area ratio of the seawater suction hole to the annular jet hole according to step 5.1 until the flow resistance along the way and the local flow resistance are greater than the maximum value of the Q-H characteristic curve range of the water pump;

若否,则此时海水吸入孔与环形射流孔的截面积比为极限比例,取处于水泵的Q-H特性曲线范围内的最大海水吸入孔与环形射流孔的截面积比,作为海水吸入孔与环形射流孔的最优截面积比,并以此最优截面尺寸比计算获得所述海水吸入孔与环形射流孔的截面尺寸。If not, then the cross-sectional area ratio of the seawater suction hole to the annular jet hole is a limiting ratio. The maximum cross-sectional area ratio of the seawater suction hole to the annular jet hole within the Q-H characteristic curve of the water pump is taken as the optimal cross-sectional area ratio of the seawater suction hole to the annular jet hole, and the cross-sectional dimensions of the seawater suction hole and the annular jet hole are calculated using this optimal cross-sectional dimension ratio.

以上所述,仅为本发明的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明公开的技术范围内,可轻易想到各种等效的修改或替换,这些修改或替换都应涵盖在本发明的保护范围之内。The above description is only a specific implementation mode of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can easily think of various equivalent modifications or substitutions within the technical scope disclosed in the present invention, and these modifications or substitutions should be included in the protection scope of the present invention.

Claims (8)

1. The underwater equipment heat dissipation motor system is characterized by comprising an underwater equipment shell, a motor and a cooling system; the underwater equipment shell comprises a motor cabin section and a tail cabin section;
the motor comprises a motor front end cover, a rotor assembly, a stator assembly and a motor rear end cover;
The motor front end cover and the motor rear end cover are respectively and radially fixedly arranged at two ends of the motor cabin section cavity, and the rotor assembly and the stator assembly are coaxially arranged between the motor front end cover and the motor rear end cover; the rotor assembly has a rotor shaft for driving the underwater equipment propeller to rotate;
The cooling system is an open type passive self-adaptive cooling system and comprises a heat dissipation flow channel and a water pump arranged at the front end of the rotor shaft; the rear end of the rotor shaft extends out of the tail cabin section and is communicated with the ocean;
the heat dissipation runner comprises a seawater suction hole, a first connecting runner, a double-spiral runner, a second connecting runner and an annular jet hole; the double spiral flow channel is a spiral groove symmetrically arranged on the inner wall of the motor cabin section; the seawater suction hole is a central hole of the rotor shaft; the annular jet hole is coaxially arranged on the rotor shaft and is arranged at the position of the outlet of the second connecting flow passage along the rear end of the rotor shaft;
The water pump is provided with two flow passage outlets which are respectively communicated with the input port of the double-spiral flow passage through first connecting flow passages which are symmetrically arranged, and the output port of the double-spiral flow passage is respectively communicated with the annular jet hole through second connecting flow passages which are symmetrically arranged; the water pump sucks seawater from a central hole of the rotor shaft under the drive of the motor rotor shaft, cools the rotor assembly, cools the stator assembly along the double spiral flow passage, flows out of an outlet of the second connecting flow passage after cooling, and is discharged into the sea through the annular jet hole;
the second connecting flow passage comprises a flow passage radially arranged on the rear end cover of the motor, a lip-shaped seal cabin and a flow hole arranged on the rotor shaft;
two ends of a liquid flow channel radially arranged on a rear end cover of the motor are respectively communicated with an output port of the double-spiral flow channel and the lip-shaped sealing cabin;
The lip seal cabin is arranged in a central hole of the rear end cover of the motor, and the inner wall of the lip seal cabin is in interference fit with the outer wall of the rotor shaft;
A plurality of liquid flow holes are radially formed in the side wall of the rotor shaft and at the position matched with the lip seal cabin, and the liquid flow holes are communicated with the annular jet holes;
the cooling wastewater discharged through the double spiral flow channels is discharged into the ocean through the liquid flow channel, the lip seal cabin, the liquid flow hole and the annular jet hole on the rear end cover of the motor in sequence.
2. The heat-dissipating motor system of claim 1, wherein the rotor assembly comprises the rotor shaft, a rotor core, and a permanent magnet; the rotor shaft, the rotor core and the permanent magnet are nested and fixedly connected from inside to outside coaxially in sequence;
The stator assembly is sleeved on the outer wall of the rotor assembly, a gap exists between the stator assembly and the rotor assembly, the stator assembly comprises a stator core and a stator winding, the outer wall of the stator core is fixed on the inner wall of the motor compartment, and the stator winding is wound in the stator core; under the action of the magnetic force of the permanent magnet and the stator winding, the rotor iron core, the permanent magnet and the rotor shaft rotate together, and the rotor shaft drives the propeller of the underwater equipment to rotate.
3. The heat dissipating motor system of claim 2, wherein a cross-sectional area ratio of said seawater intake port to said annular jet port is 3:1.
4. The heat-dissipating motor system of claim 3, wherein a wall thickness between the seawater intake port and the annular jet port is not less than 8 mm.
5. The heat dissipating motor system of claim 4, wherein the rear shaft body of the rotor shaft is connected to the tail section by a sliding bearing provided in the tail section of the underwater equipment, and an end face of the sliding bearing is fitted to an inner end face of the tail section;
The inner diameter of the chamber of the tail cabin section is provided with a fixed support fixedly connected with the body of the tail cabin section, and the middle section shaft body of the rotor shaft is connected with the central hole of the fixed support through another sliding bearing.
6. The heat dissipation motor system according to claim 5, wherein the fixed support is disc-shaped as a whole, a central hole is formed in the fixed support along the axis, and the fixed support is connected with the outer wall of the rotor shaft through a sliding bearing;
The fixed bolster lateral wall radially is equipped with a plurality of connecting rods, and the connecting rod tip is connected with the lug that sets up on the motor cabinet section inner wall.
7. The method for designing a heat dissipating motor system according to any one of claims 1 to 6, comprising the steps of:
Step 1: according to the space and overall weight requirements of the underwater equipment motor cabin section, configuring a motor for the motor cabin section, and determining the electromagnetic structure of the motor;
Establishing a simulation model of a motor and an underwater equipment shell, and initially setting structural parameters of a heat dissipation runner in the model; the structural parameters comprise the pitch, depth, section size and spiral inclination angle of the double spiral flow channels, and the section sizes of the seawater suction holes and the annular jet holes;
The sectional area ratio of the seawater suction hole to the annular jet hole is initially set to be 1;
Step 2: obtaining temperature field parameters of a heat dissipation runner and the highest temperature T i of a stator winding, a stator core and a rotor core when the motor sails under water with different sailing speeds V i through simulation calculation; wherein i=1, 2,3, …, n;
step 3: judging whether the highest temperatures T i of the stator winding, the stator core and the rotor core meet the motor design requirements under different navigational speeds V i based on the temperature field parameters obtained in the step 2, and if so, entering the step 5; otherwise, enter step 4 and adjust the parameter of the heat dissipation runner;
step 4: adjusting the parameters of the heat dissipation flow channel in a mode of reducing the pitch of the double-spiral flow channel and/or increasing the cross section size of the double-spiral flow channel, returning to the step 2 and the step 3 under the condition that the motor cabin shell meets the strength design requirement after adjustment, judging whether the highest temperature T i of the stator winding, the stator core and the rotor core meets the motor design requirement, and entering the step 5 if the highest temperature T i meets the motor design requirement; otherwise, returning to the step 1, and re-determining the electromagnetic structure of the motor;
Step 5: calculating and obtaining the along-path flow resistance of the double spiral flow channel and the local flow resistance of the bending part of the heat dissipation flow channel, judging whether the along-path flow resistance and the local flow resistance are within the range of the Q-H characteristic curve of the water pump, and if so, obtaining a required heat dissipation motor system; otherwise, the cross section sizes of the seawater suction hole and the annular jet hole are adjusted until the along-distance flow resistance of the double spiral flow channel and the local flow resistance of the bending part of the heat dissipation flow channel can be within the range of the Q-H characteristic curve of the water pump after adjustment.
8. The design method according to claim 7, wherein the specific process of adjusting the cross-sectional dimensions of the seawater intake port and the annular jet port in step 5 is:
step 5.1: setting an adjusting step of the sectional area ratio of the seawater suction hole to the annular jet hole, and calculating to obtain the sectional sizes of the seawater suction hole and the annular jet hole based on the adjusting step;
Step 5.2: obtaining the along-path flow resistance of the double spiral flow channel and the local flow resistance of the bending part of the heat dissipation flow channel through simulation calculation, and judging whether the along-path flow resistance and the local flow resistance are within the range of a Q-H characteristic curve of the water pump;
if yes, continuously increasing the sectional area ratio of the seawater suction hole to the annular jet hole according to the step 5.1 until the along-range flow resistance and the local flow resistance are larger than the maximum value of the Q-H characteristic curve range of the water pump;
If not, the sectional area ratio of the seawater suction hole to the annular jet hole is taken as the limit ratio, the sectional area ratio of the maximum seawater suction hole to the annular jet hole in the Q-H characteristic curve range of the water pump is taken as the optimal sectional area ratio of the seawater suction hole to the annular jet hole, and the sectional size of the seawater suction hole to the annular jet hole is calculated according to the optimal sectional area ratio.
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