Waterproof and dustproof high-performance permanent magnet synchronous motor

Abstract

The invention discloses a waterproof and dustproof high-performance permanent magnet synchronous motor, and relates to the technical field of waterproof and dustproof, the waterproof and dustproof high-performance permanent magnet synchronous motor comprises a protection mechanism, a waterproof mechanism and a dust removal mechanism are arranged behind the protection mechanism, and the dust removal mechanism is arranged behind the waterproof mechanism; the protection mechanism comprises a heat insulation protection plate, a set of evaporation heating wires are installed on one side of the outer surface wall of the heat insulation protection plate, a set of first water throwing rolling shafts are arranged on one side of the outer surface wall of the set of evaporation heating wires, and a first wind power system is rotationally connected between the set of water throwing rolling shafts. The first wind power system generates airflow to drive the first water throwing rolling shaft, surface water vapor evaporation is accelerated, and the primary waterproof effect is enhanced. The first water throwing rolling shaft rotates at a high speed to generate centrifugal force, water attached to the surface is rapidly thrown away, the evaporation heating wire is electrified to heat, residual water is evaporated to thoroughly eliminate surface moisture, and the heat insulation protection plate prevents high temperature of the evaporation heating wire from being conducted to the motor body.

Description

Technical Field

[0001] The present invention relates to the technical field of waterproof and dustproof, and in particular to a waterproof and dustproof high-performance permanent magnet synchronous motor. Background Art

[0002] A high-performance permanent magnet synchronous motor is an AC motor that uses rare earth permanent magnets to establish a magnetic field and in which the stator winding rotates synchronously with the rotor magnetic field. Its core advantages lie in high efficiency, high power density and precise control. It is widely used in electric vehicles, industrial robots and other fields.

[0003] When water enters the motor, the winding insulation layer will age and crack, resulting in a decrease in insulation resistance. When water adheres to the motor surface or internal heat dissipation channels, it may hinder heat dissipation, further accelerating insulation aging and permanent magnet demagnetization. When dust enters the motor, it will generate friction with the rotation of components such as the rotor and bearings, causing mechanical wear. Therefore, permanent magnet synchronous motors must be waterproof and dustproof.

[0004] The existing technologies for the above problems are mainly achieved through protective structure design, sealing technology application, material selection and auxiliary protection measures. However, waterproofing mainly relies on passive blocking. Surface moisture is difficult to remove quickly and is easy to penetrate into the interior. After water enters the body, there is a lack of effective collection and discharge mechanism. Water accumulation causes failures. Dust protection is mostly static protection. Internally deposited dust is difficult to remove, and the mixture of dust and residual water will aggravate component corrosion. At the same time, the front and rear end protection is unbalanced, and the gaps at the rear end are prone to water seepage and dust accumulation. There is a lack of a closed-loop design from external protection to internal drainage, resulting in poor waterproof and dustproof effects and shortened motor life.

[0005] Therefore, we propose a waterproof and dustproof high-performance permanent magnet synchronous motor to solve the above problems. Summary of the Invention

[0006] The purpose of the present invention is to provide a high-performance permanent magnet synchronous motor that is waterproof and dustproof. The evaporation heating wire inside the multi-layer waterproof and sealed structure is energized to generate heat to evaporate residual moisture, completely eliminating surface moisture. The first water-removing roller generates centrifugal force through high-speed rotation, quickly throwing off moisture attached to the surface and reducing the risk of infiltration. The annular guide rail provides a sliding track for the brush plate, guiding the brush plate to move in a circular motion, driving the brush plate to drive the brush head to move, thereby cleaning the inner wall of the fuselage shell. The second wind system and the second water-removing roller blow the dust deposited inside to the inside of the fuselage shell, and throw off a small amount of moisture that penetrates from the rear end gap.

[0007] To achieve the above-mentioned object, the present invention provides the following technical solution: a waterproof and dustproof high-performance permanent magnet synchronous motor, comprising a protective mechanism, a waterproof mechanism and a dust removal mechanism provided behind the protective mechanism, and the dust removal mechanism being provided behind the waterproof mechanism; The protective mechanism includes a heat-insulating protective plate, a group of evaporation heating wires are installed on one side of the outer wall of the heat-insulating protective plate, a group of first water-spinning rollers are provided on one side of the outer wall of the group of evaporation heating wires, a first wind system is rotatably connected between the group of water-spinning rollers, the evaporation heating wires are used to evaporate moisture remaining on the outside of the heat-insulating protective plate, the heat-insulating protective plate is used to protect and isolate internal components, and the first water-spinning rollers are used to quickly spin off surface water.

[0008] Preferably, a motor body is installed on one side of the outer wall of the heat insulation protective plate, a power transmission shaft is connected to one side of the outer wall of the motor body, the motor body is installed inside the fuselage shell, a multi-layer waterproof and sealed structure is installed on one side of the outer wall of the fuselage shell, a group of connecting and fixing frames are installed on the inner wall of the waterproof and sealed structure, and the multi-layer waterproof and sealed structure enhances the waterproof sealing performance.

[0009] Preferably, a group of support beams are connected between a group of the connecting and fixing frames, a group of limiting rings are provided on the outer wall ring of a group of the evaporating heating wires, a group of limiting mounting plates are installed on one side of the outer wall of a group of the limiting rings, and a circle of supporting and stabilizing parts are connected on one side of the outer wall of a group of the connecting and fixing frames.

[0010] Preferably, one side of the outer wall of a group of the limiting mounting plates is connected to both sides of the outer wall of a group of connecting fixing frames, a mounting fixture is provided in the middle of a group of the evaporation heating wires, and one side of the outer wall of the mounting fixture is installed on one side of the outer wall of the heat insulation protection plate, and the inner wall of the mounting fixture is sleeved with a rotating shaft mounting sleeve, the evaporation heating wire can remove moisture, and the heat insulation protection plate provides heat insulation protection to ensure the stability of the internal environment of the motor.

[0011] Preferably, the inner surface wall of the rotating shaft mounting sleeve is sleeved with a rotating shaft sealing structure, a group of the connecting fixing frame and the supporting and stabilizing parts are all installed on the inner surface wall of the multi-layer waterproof sealing structure, and a group of first water-repelling rollers are rotatably connected to one side of the outer surface wall of the rotating shaft sealing structure, and a first wind power system is rotatably connected between the group of the first water-repelling rollers, and the first water-repelling rollers and the first blades assist in water removal and cooperate with waterproofing.

[0012] Preferably, a front end cover is connected to one side of the outer wall of the heat insulation protective plate, a group of front end cover ventilation holes are opened on one side of the outer wall of the front end cover, a group of front end cover fixing frames are installed on one side of the outer wall of the front end cover, a group of mounting ears are installed on one side of the outer wall of the front end cover, a group of coupling mounting parts are opened and installed in the middle part of one side of the outer wall of the front end cover fixing frame, and the inner wall of the coupling mounting parts is rotatably connected to the power transmission shaft.

[0013] Preferably, a group of casing heat dissipation plates and casing mounting bolts are respectively installed on the outer wall of the fuselage shell, a group of motor base support frames are installed on the bottom of the outer wall of the fuselage shell, and a motor mounting base is connected to one side of the outer wall of a group of motor base support frames.

[0014] Preferably, a drainage box is installed on the upper part of one side of the outer wall of the motor mounting base, and the drainage box is used to drain moisture from the inside of the fuselage shell. The outer wall of the fuselage shell is also provided with a water collecting box installed on the upper part of the motor mounting base, and the outer wall of the water collecting box and the drainage box are installed with sealed leak-proof fixings on one side.

[0015] Preferably, a group of the sealed and leak-proof fixing parts are connected with a water pipe, a water pump is installed on the outer wall of the water pipe, a power system is installed on one side of the outer wall of the water pump, a limited water collecting trough is installed on the lower part of the inner wall of the fuselage shell, a group of through grooves are opened on the lower part of the inner wall of the limited water collecting trough, the through grooves are connected with the water collecting box, and a group of annular guide rails are opened on the inner wall of the fuselage shell. The drainage box, water pipe, water pump, etc. constitute a drainage system to discharge accumulated water.

[0016] Preferably, the inner surface wall of the annular guide rail is slidably connected to a brush plate, and the outer surface wall of the brush plate is installed with a group of brush heads, one group of the brush heads is used to collect moisture inside the fuselage shell and transport it to the through groove in the lower end limit water collection trough, one side of the outer surface wall of the fuselage shell is connected to a rear end cover, and one side of the outer surface wall of the rear end cover is installed with a rear end cover sealing structure, one side of the outer surface wall of the rear end cover sealing structure is rotatably connected to a group of second water-throwing rollers, and a second wind power system is rotatably connected between a group of second water-throwing rollers, the annular guide rail, the brush plate, and the brush heads can clean the interior to ensure that the interior of the motor is clean and dry, the second water-throwing rollers and the second blades assist in water rejection and dust removal, keep the interior of the motor clean, and prevent dust and moisture from affecting the operation of the motor.

[0017] Compared with the prior art, the present invention has the following beneficial effects: The external protection of the present invention adopts an active defense mechanism. The first wind system cooperates with the first water-removing roller to quickly remove surface moisture through the dual effects of airflow-accelerated evaporation and centrifugal force, solving the problem of moisture adhesion and infiltration caused by passive barrier. The multi-layer waterproof and sealed structure combined with the evaporative heating wire can not only physically block the penetration of residual moisture, but also actively heat and evaporate moisture. It is matched with the heat insulation protection plate and the limiting component to effectively remove moisture while avoiding the impact of high temperature on the motor body, thereby enhancing the deep protection effect. After water enters the interior, the annular guide rail guides the brush plate for circular motion, and the brush head can synchronously collect moisture and dust into the limited water collection trough, which is quickly discharged through the closed-loop drainage system composed of the through trough, water collection box, water pump and water pipe, solving the problems of water accumulation and inefficient drainage. The rear-end protection drives the second water-removing roller through the second wind system, which not only removes water seepage from the gap, but also blows away the deposited dust, and cooperates with the brush head to achieve dynamic dust prevention, avoiding the mixing of dust and water to corrode components, forming a closed-loop protection system with balanced front and rear ends and internal and external linkage, which greatly improves the waterproof and dustproof effect and effectively extends the service life of the motor. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 This is a perspective view of the main structure of a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 2 This is a disassembled three-dimensional diagram of components in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 3 This is a disassembled three-dimensional diagram of components in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 4 This is an exploded perspective view of a protective mechanism in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 5 This is an exploded perspective view of a protective mechanism in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 6 This is an exploded perspective view of a protective mechanism in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 7 This is an exploded perspective view of a waterproof mechanism in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention; Figure 8 This is a disassembled three-dimensional diagram of the waterproof mechanism in a waterproof and dustproof high-performance permanent magnet synchronous motor of the present invention.

[0019] In the figure: 100, protective mechanism; 101, front cover; 102, mounting ear; 103, front cover vent; 104, front cover fixing frame; 105, coupling mounting member; 106, first water-repelling roller; 107, first wind power system; 108, multi-layer waterproof and sealed structure; 109, connecting fixing frame; 110, support beam; 111, supporting and stabilizing member; 112, shaft mounting sleeve; 113, shaft sealing structure; 114, mounting fixing member; 115, limiting ring; 116, limiting mounting plate; 117, evaporation heating wire; 118, thermal insulation protective plate; 200, waterproof mechanism; 201, Body shell; 202, casing heat sink; 203, casing mounting bolts; 204, motor base support beam; 205, motor mounting base; 206, drainage box; 207, sealed leak-proof fixings; 208, water pipe; 209, water pump; 210, power system; 211, water collecting box; 212, limited water collecting trough; 213, through groove; 214, annular guide rail; 215, brush plate; 216, brush head; 300, dust removal mechanism; 301, rear end cover; 302, rear end cover sealing structure; 303, second water-shedding roller; 304, second wind power system; 4, power transmission shaft; 5, motor body. DETAILED DESCRIPTION

[0020] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the implementation regulations described are only part of the embodiments of the present invention, not all of the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments of the present invention without making any creative efforts shall fall within the scope of protection of the present invention.

[0021] Example 1, according to Figures 1-6 As shown, it includes a protection mechanism 100, a waterproof mechanism 200 and a dust removal mechanism 300 are provided behind the protection mechanism 100, and the dust removal mechanism 300 is provided behind the waterproof mechanism 200; The protective mechanism 100 includes a heat-insulating protective plate 118. A group of evaporative heating wires 117 are mounted on one side of the outer wall of the heat-insulating protective plate 118. A group of first water-spinning rollers 106 are mounted on one side of the outer wall of the group of evaporative heating wires 117. A first wind system 107 is rotatably connected between the group of water-spinning rollers 106. The evaporative heating wires 117 are used to evaporate moisture remaining on the outside of the heat-insulating protective plate 118. The heat-insulating protective plate 118 is used to protect and isolate internal components. The first water-spinning rollers 106 are used to quickly remove surface water. The motor body 5 is mounted on one side of the outer wall of the heat-insulating protective plate 118, and the power transmission shaft 4 is connected to one side of the outer wall of the motor body 5. The motor body 5 is mounted inside the fuselage shell 201. A multi-layer waterproof and sealed structure 108 is mounted on one side of the outer wall of the fuselage shell 201, and a set of connecting and fixing frames 109 are mounted on the inner wall of the waterproof and sealed structure 108. The multi-layer waterproof and sealed structure 108 enhances waterproof sealing. A set of support beams 110 are connected between a set of connecting and fixing frames 109. A set of limiting rings 115 are provided around the outer wall of a set of evaporation heating wires 117. A set of limiting mounting plates 116 are installed on one side of the outer wall of the set of limiting rings 115. A set of supporting and stabilizing members 111 are connected around one side of the outer wall of the set of connecting and fixing frames 109. One side of the outer wall of a set of limiting mounting plates 116 is connected to both sides of the outer wall of a set of connecting fixing frames 109. A mounting fixture 114 is provided in the middle of a set of evaporation heating wires 117. One side of the outer wall of the mounting fixture 114 is mounted on one side of the outer wall of the heat insulation protection plate 118. The inner wall of the mounting fixture 114 is sleeved with a rotating shaft mounting sleeve 112. The evaporation heating wires 117 can remove moisture, and the heat insulation protection plate 118 provides heat insulation protection to ensure a stable internal environment of the motor. The inner surface wall of the rotating shaft mounting sleeve 112 is sleeved with a rotating shaft sealing structure 113, a set of connecting fixing frames 109 and supporting and stabilizing members 111 are both installed on the inner surface wall of the multi-layer waterproof sealing structure 108, and one side of the outer surface wall of the rotating shaft sealing structure 113 is rotatably connected to a set of first water-shedding rollers 106, and a first wind power system 107 is rotatably connected between the set of first water-shedding rollers 106. The first water-shedding rollers 106 and the first blades 107 assist in water shedding and cooperate with waterproofing.

[0022] The effect achieved by the entire embodiment 1 is as follows: when external moisture contacts the protective mechanism 100, the first wind system 107 generates airflow to drive the first water-repelling roller 106, accelerating the evaporation of surface water vapor to enhance the primary waterproof effect; the first water-repelling roller 106 rotates at high speed to generate centrifugal force, quickly removing moisture attached to the surface, reducing the risk of infiltration, and the residual moisture that has not been completely removed enters the multi-layer waterproof sealed structure 108 at the rear, and its multi-layer sealing design can prevent moisture penetration and provide installation space for the evaporation heating wire 117; then the evaporation heating wire 117 is powered on and heated, evaporating the residual moisture to completely eliminate surface moisture and enhance the waterproof effect, and the heat insulation protective plate 118 blocks the high temperature of the evaporation heating wire 117 from being transmitted to the motor body 5, and at the same time physically isolates the external environment from the internal components; the limiting ring 115 limits the evaporation heating wire 117 7 radial displacement, preventing it from shaking and contacting other components; the limiting mounting plate 116 fixes the axial position of the heating wire to ensure the stability of the heating area; the mounting fixture 114 rigidly connects the shaft sleeve and the protective plate to enhance the structural stability; the shaft mounting sleeve 112 provides rotation support for the power transmission shaft 4; the shaft sealing structure 113 prevents moisture from penetrating along the shaft, strengthens the sealing of the connection between the power transmission shaft 4 and the heat insulation protective plate 118, and cooperates with the isolation effect of the heat insulation protective plate 118 itself to form a front-end multi-layer protection barrier, which effectively solves the problem of external moisture penetrating into internal components and the high temperature during heating and dehumidification that may cause damage to core components, thereby ensuring the stable operation of each component during operation, and solving the problems of functional failure or malfunction due to component displacement and shaking, as well as the limited effect of a single protection measure and insufficient overall protection capability.

[0023] Example 2, according to Figure 1-Figure 3 and Figure 7-Figure 8 As shown. A front end cover 101 is connected to one side of the outer wall of the heat insulation protection plate 118. A set of front end cover vent holes 103 are formed on one side of the outer wall of the front end cover vent holes 103. A set of front end cover fixing brackets 104 are mounted on one side of the outer wall of the front end cover 101. A set of mounting ears 102 are mounted on one side of the outer wall of the front end cover 101. A coupling mounting member 105 is formed and mounted in the middle of one side of the outer wall of the set of front end cover fixing brackets 104. The inner wall of the coupling mounting member 105 is rotatably connected to the power transmission shaft 4. A set of casing heat dissipation plates 202 and casing mounting bolts 203 are respectively installed on the outer wall of the fuselage shell 201. A set of motor base support frames 204 are installed at the bottom of the outer wall of the fuselage shell 201. One side of the outer wall of the set of motor base support frames 204 is connected to a motor mounting base 205. A drainage box 206 is mounted on the upper portion of one side of the outer wall of the motor mounting base 205. The drainage box 206 is used to drain moisture from the interior of the fuselage shell 201. A water collection box 211 is mounted on the outer wall of the fuselage shell 201 and located above the motor mounting base 205. A sealed, leak-proof fixing member 207 is mounted on one side of the outer wall of the water collection box 211 and the drainage box 206. A water pipe 208 is connected between a set of sealed and leak-proof fixing parts 207. A water pump 209 is installed on the outer wall of the water pipe 208. A power system 210 is installed on one side of the outer wall of the water pump 209. A limited water collection tank 212 is installed at the lower part of the inner wall of the fuselage shell 201. A set of through grooves 213 are opened at the lower part of the inner wall of the limited water collection tank 212. The through grooves 213 are connected to the water collection box 211. A set of annular guide rails 214 are opened on the inner wall of the fuselage shell 201. The drainage box 206, water pipe 208, water pump 209, etc. constitute a drainage system to drain accumulated water. The inner wall of the annular guide rail 214 is slidably connected with a brush plate 215, and the outer wall of the brush plate 215 is installed with a group of brush heads 216. A group of brush heads 216 are used to collect moisture inside the fuselage shell 201 and transport it to the through groove 213 in the lower end limit water collection tank 212. One side of the outer wall of the fuselage shell 201 is connected with a rear end cover 301, and one side of the outer wall of the rear end cover 301 is installed with a rear end cover sealing structure 302. One side of the outer wall of the rear end cover sealing structure 302 is rotatably connected with a group of second water-shedding rollers 303, and a second wind power system 304 is rotatably connected between a group of second water-shedding rollers 303. The annular guide rail 214, the brush plate 215, and the brush heads 216 can clean the interior to ensure that the interior of the motor is clean and dry. The second water-shedding rollers 303 and the second blades 304 assist in water shedding and dust removal, keep the interior of the motor clean, and prevent dust and moisture from affecting the operation of the motor.

[0024] The effect achieved by the entire embodiment 2 is as follows: when moisture penetrates into the interior of the fuselage shell 201, the annular guide rail 214 provides a sliding track for the brush plate, guiding the brush plate 215 to make a circular motion, driving the brush plate 215 to drive the brush head 216 to move, thereby cleaning the inner wall of the fuselage shell 201, and making a circular motion inside the fuselage shell 201, driving the brush head 216 to clean the inner wall of the fuselage shell 201, collecting moisture and dust. Since the fuselage shell 201 is a closed cavity, the directional airflow generated by the operation of the second wind system 304 is from the rear end cover The water diffuses toward the middle of the fuselage, and inevitably acts on the brush plate 215 which is slidably connected to the annular guide rail 214. The brush plate 215 needs to be installed with a brush head 216, which has a sufficient force-bearing area. The airflow thrust directly pushes the brush plate 215 to make a circular motion along the annular guide rail 214, collects it to the designated position to clean the inner wall of the fuselage shell 201, collects the water into the limited water collecting groove 212 to collect the water inside the fuselage, and guides the water to flow into the through groove 213. The water flows into the water collecting box 211 through the through groove 213 inside the limited water collecting groove 212, and passes through the water pipe 20 8 is transported to the drainage box 206, and the water in the water collection box 211 is transported through the water pipe 208 to form a drainage channel. The water leakage is prevented by the sealed leak-proof fixing part 207, and the sealed interface is transported to the drainage box 206 to discharge the water inside the fuselage to the outside of the motor, completing the drainage process, and finally discharged to the outside of the motor to form a closed-loop waterproof system; the second wind system 304 blows up the dust deposited inside, and at the same time drives the second water-removing roller 303 to rotate, assisting in removing the water infiltrated from the rear end and driving the second water-removing roller 303 to remove the water infiltrated from the gap at the rear end. A small amount of moisture is thrown off, and the air is stirred to enhance the dust removal effect. On the one hand, the dust that may be deposited inside is blown to the inside of the fuselage shell 201 through the airflow, and on the other hand, a small amount of moisture that penetrates from the gap at the rear end is thrown off. In the process of collecting moisture, the brush plate 215 and the brush head 216 simultaneously clean the internal dust blown in by the second wind system 304, which effectively solves the problems of the inability to effectively remove the moisture that has penetrated into the fuselage and the easy residual water, the difficulty in thoroughly cleaning the dust deposition, and the weak protection against moisture and dust infiltration at the rear end.

[0025] The entire device operates as follows: After the motor starts, the protective mechanism 100 enters operation. The front cover 101 is secured to the device via mounting ears 102. Ventilation holes 103 on its surface allow for internal and external air circulation, ensuring heat dissipation. The front cover mounting bracket 104, in conjunction with the coupling mounting member 105, provides stable rotational support for the power transmission shaft 4, ensuring efficient power output from the motor body 5.When external moisture contacts the protective mechanism 100, the first wind system 107 starts synchronously, driving a set of first water-removing rollers 106 to rotate at high speed, and using centrifugal force to quickly remove surface water; the residual moisture that has not been completely removed will enter the rear multi-layer waterproof and sealed structure 108, and then the evaporation heating wire 117 inside the multi-layer waterproof and sealed structure 108 is energized and heated to evaporate and remove the residual moisture. In this process, the heat insulation protective plate 118 isolates the evaporation heating wire 117 from the motor body 5, thereby protecting the motor body 5 from the influence of high temperature. The limiting ring 115 and the limiting mounting plate 116 fix the position of the evaporation heating wire 117, and the fixing member 114, the shaft mounting sleeve 112 and the shaft are installed. The sealing structure 113 strengthens the sealing of the connection between the power transmission shaft 4 and the heat insulation protection plate 118, and cooperates with the isolation effect of the heat insulation protection plate 118 itself to form a front-end multi-layer protection barrier; while the protection mechanism 100 is working, the waterproof mechanism 200 enters a continuous operation state, and the fuselage shell 201 serves as the main protective shell of the motor, which is fastened by the shell mounting bolts 203. The shell heat sink 202 on its surface dissipates the heat generated by the motor operation, and the motor base support frame 204 and the motor mounting base 205 jointly support the fuselage to ensure overall stability. The multi-layer waterproof and sealed structure 108 further enhances the sealing of the connection between the fuselage shell 201 and the protection mechanism, and connects the fixing frame 109, the support beam 110 and the support The supporting member 111 strengthens the internal structure to prevent the sealing function from being damaged due to vibration. If water accidentally penetrates into the fuselage shell 201, the annular guide rail 214 drives the brush plate 215 to make a circular motion inside the fuselage shell 201, driving the brush head 216 to clean the inner wall of the fuselage shell 201, and collects the water into the limited water collection groove 212. The water flows into the water collection box 211 through the through groove 213 inside the limited water collection groove 212; then the power system 210 drives the water pump 209 to transport the water in the water collection box 211 through the water pipe 208 and the sealed interface of the sealed leak-proof fixing member 207 to the drainage box 206, and finally discharges it to the outside of the motor body 5, forming a closed-loop waterproof system. During the entire operation of the motor, the dust removal mechanism 300 is synchronized The rear end cover 301 is tightly connected to the fuselage shell 201 through the rear end cover sealing structure 302, blocking the intrusion path of external dust; the second wind system 304 drives the second water-removing roller 303 to rotate, on the one hand, the dust deposited inside is blown to the inside of the fuselage shell 201 through the airflow, and on the other hand, a small amount of water seeping in from the rear end gap is removed. In the process of collecting water, the brush plate 215 and the brush head 216 simultaneously clean the internal dust blown in by the second wind system 304 to prevent dust from adhering to the surface of the motor body 5 and affecting heat dissipation or causing component wear. Through the above-mentioned coordinated operation, the protection, waterproofing and dust removal mechanisms form an all-round protection system to ensure that the motor continues to operate efficiently in a complex environment.

[0026] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A waterproof and dustproof high-performance permanent magnet synchronous motor, comprising a protection mechanism (100), characterized in that: A waterproof mechanism (200) and a dust removal mechanism (300) are provided behind the protection mechanism (100), and the dust removal mechanism (300) is provided behind the waterproof mechanism (200); A protective mechanism (100) includes a heat-insulating protective plate (118), a group of evaporation heating wires (117) is installed on one side of the outer wall of the heat-insulating protective plate (118), a group of first water-spinning rollers (106) are provided on one side of the outer wall of the group of evaporation heating wires (117), a first wind system (107) is rotatably connected between the group of water-spinning rollers (106), the evaporation heating wires (117) are used to evaporate moisture remaining outside the heat-insulating protective plate (118), the heat-insulating protective plate (118) is used to protect and isolate internal components, and the first water-spinning rollers (106) are used to quickly spin off surface water.

2. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 1, characterized in that: A motor body (5) is installed on one side of the outer wall of the heat insulation protection plate (118), a power transmission shaft (4) is connected to one side of the outer wall of the motor body (5), the motor body (5) is installed inside the fuselage shell (201), a multi-layer waterproof sealing structure (108) is installed on one side of the outer wall of the fuselage shell (201), a group of connecting fixing frames (109) are installed on the inner wall of the waterproof sealing structure (108), and the multi-layer waterproof sealing structure (108) enhances waterproof sealing performance.

3. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 2, characterized in that: A group of support beams (110) are connected between a group of the connecting and fixing frames (109), a group of limiting rings (115) are provided around the outer wall of a group of the evaporating heating wires (117), a group of limiting mounting plates (116) are installed on one side of the outer wall of a group of the limiting rings (115), and a circle of supporting and stabilizing members (111) are connected around one side of the outer wall of a group of the connecting and fixing frames (109).

4. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 3, characterized in that: One side of the outer wall of a group of the limiting mounting plates (116) is connected to both sides of the outer wall of a group of the connecting fixing frames (109); a mounting fixture (114) is provided in the middle of a group of the evaporation heating wires (117); and one side of the outer wall of the mounting fixture (114) is mounted on one side of the outer wall of the heat insulation protection plate (118); the inner wall of the mounting fixture (114) is sleeved with a rotating shaft mounting sleeve (112); the evaporation heating wires (117) can remove moisture, and the heat insulation protection plate (118) provides heat insulation protection to ensure the stability of the internal environment of the motor.

5. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 4, characterized in that: The inner surface wall of the rotating shaft mounting sleeve (112) is sleeved with a rotating shaft sealing structure (113), a group of the connecting fixing frame (109) and the supporting and stabilizing member (111) are both installed on the inner surface wall of the multi-layer waterproof sealing structure (108), a group of first water-repelling rollers (106) are rotatably connected to one side of the outer surface wall of the rotating shaft sealing structure (113), a first wind power system (107) is rotatably connected between the group of the first water-repelling rollers (106), and the first water-repelling rollers (106) and the first blades (107) assist in water removal and cooperate with waterproofing.

6. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 5, characterized in that: A front end cover (101) is connected to one side of the outer wall of the heat insulation protection plate (118), a group of front end cover ventilation holes (103) are opened on one side of the outer wall of the front end cover (101), a group of front end cover fixing frames (104) are installed on one side of the outer wall of the front end cover (101), a group of mounting ears (102) are installed on one side of the outer wall of the front end cover (101), and a coupling mounting member (105) is opened and installed in the middle of one side of the outer wall of the front end cover fixing frame (104), and the inner wall of the coupling mounting member (105) is rotatably connected to the power transmission shaft (4).

7. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 2, characterized in that: A set of casing heat dissipation plates (202) and casing mounting bolts (203) are respectively installed on the outer wall of the body shell (201), a set of motor base support frames (204) are installed on the bottom of the outer wall of the body shell (201), and a motor mounting base (205) is connected to one side of the outer wall of the set of motor base support frames (204).

8. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 7, characterized in that: A drainage box (206) is installed on the upper portion of one side of the outer wall of the motor mounting base (205). The drainage box (206) is used to drain moisture from the interior of the fuselage shell (201). A water collecting box (211) is installed on the outer wall of the fuselage shell (201) and is arranged on the upper portion of the motor mounting base (205). A sealed leak-proof fixing member (207) is installed on one side of the outer wall of the water collecting box (211) and the drainage box (206).

9. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 8, characterized in that: A water pipe (208) is connected between a group of the sealed leak-proof fixing members (207), a water pump (209) is installed on the outer wall of the water pipe (208), and a power system (210) is installed on one side of the outer wall of the water pump (209). A limited water collecting trough (212) is installed on the lower part of the inner wall of the fuselage shell (201), and a group of through grooves (213) are opened on the lower part of the inner wall of the limited water collecting trough (212). The through grooves (213) are connected to the water collecting box (211). A group of annular guide rails (214) are opened on the inner wall of the fuselage shell (201). The drainage box (206), the water pipe (208), the water pump (209), etc. constitute a drainage system to discharge accumulated water.

10. The waterproof and dustproof high-performance permanent magnet synchronous motor according to claim 9, characterized in that: The inner surface wall of the annular guide rail (214) is slidably connected to a brush plate (215), and the outer surface wall of the brush plate (215) is installed with a group of brush heads (216). The group of brush heads (216) is used to collect moisture inside the fuselage shell (201) and transport it to the through groove (213) in the lower end limit water collection tank (212). One side of the outer surface wall of the fuselage shell (201) is connected to a rear end cover (301), and one side of the outer surface wall of the rear end cover (301) is installed with a rear end cover sealing structure (302). A group of second water-spinning rollers (303) is rotatably connected to one side of the outer wall of the rear end cover sealing structure (302), and a second wind system (304) is rotatably connected between the group of second water-spinning rollers (303). The annular guide rail (214), the brush plate (215), and the brush head (216) can clean the interior of the motor to ensure that the interior of the motor is clean and dry. The second water-spinning rollers (303) and the second blades (304) assist in water-spinning and dust removal, keeping the interior of the motor clean and preventing dust and moisture from affecting the operation of the motor.

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