CN113996217B - High-speed dispersion machine - Google Patents

High-speed dispersion machine Download PDF

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Publication number
CN113996217B
CN113996217B CN202111653805.2A CN202111653805A CN113996217B CN 113996217 B CN113996217 B CN 113996217B CN 202111653805 A CN202111653805 A CN 202111653805A CN 113996217 B CN113996217 B CN 113996217B
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space
cooling
flow
barrel
liquid
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CN113996217A (en
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卞慧民
郑邵雍
文旭峰
陈积瑜
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Zhejiang Hansure Technology Co ltd
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Zhejiang Hansure Technology Co ltd
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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/20Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
    • H02K5/203Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium specially adapted for liquids, e.g. cooling jackets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • 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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Abstract

The application discloses a high-speed dispersion machine, which comprises a dispersion barrel; a dispersing wheel; a drive motor; driving the main shaft; a bearing seat; the dispersion barrel is provided with a first interlayer space configured to have: a first liquid inlet; a first liquid outlet; the first cooling flow channel extends from the first liquid inlet to the first liquid outlet so that a liquid flow formed by the cooling liquid in the first cooling flow channel at least has motion components in a first direction, a second direction and a third direction which are perpendicular to each other; wherein, first cooling channel includes: a plurality of circulation flow channels formed at different axial positions of the first interlayer space and extending in a surrounding manner; and the plurality of communicating flow passages are formed between two adjacent circulating flow passages in the axial direction to communicate the two circulating flow passages. The application has the advantages that: a high-speed disperser is provided for cooling a dispersing barrel by constructing a first cooling flow passage having a circulation flow passage and a communicating flow passage in a first sandwiched space of the dispersing barrel.

Description

High-speed dispersion machine
Technical Field
The application relates to the field of dispersion machines, in particular to a high-speed dispersion machine.
Background
Generally, the high-speed dispersion machine is widely applied to the new energy industry, the coating industry, the cosmetic industry, the food industry, the LED coating industry, the flexible circuit manufacturing and the like. In particular to the dispersion pulping of the positive and negative materials of the lithium ion battery and the dispersion of various nano materials (such as nano aluminum oxide, nano lithium titanate) and the like, and has higher dispersion efficiency and excellent dispersion quality.
After the thick liquids got into the dispersion bucket that scatters the machine, the main shaft drives dispersion wheel high-speed rotatory can produce a large amount of heats, and thick liquids also can produce the heat in bumping when the dispersion simultaneously, and these heats need be in time distributed out in case form the heat pile up not only to the thick liquids quality production huge influence but also can produce very big damage to equipment.
Disclosure of Invention
This summary is provided to introduce a selection of concepts in a simplified form that are further described below in the detailed description. This summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter.
Some embodiments of the present application provide a high-speed disperser, comprising: a dispersing barrel for containing the slurry to be subjected to the dispersing treatment; the dispersing wheel is rotatably arranged in the barrel inner space of the dispersing barrel; the driving motor is used for driving the dispersion wheel to rotate around a central axis; the driving main shaft is used for forming transmission between the driving motor and the dispersing wheel; the bearing block is used for installing a plurality of bearings for the driving main shaft to pass through, and a seat inner space for accommodating the bearings is formed in the bearing block; the dispersion barrel is provided with a first interlayer space surrounding the barrel inner space, the first interlayer space being configured to have: the first liquid inlet is used for allowing cooling liquid to flow into the first interlayer space; the first liquid outlet is used for allowing cooling liquid to flow out of the first interlayer space; the first cooling flow channel extends from the first liquid inlet to the first liquid outlet so that a liquid flow formed by the cooling liquid in the first cooling flow channel at least has motion components in a first direction, a second direction and a third direction which are perpendicular to each other; wherein, first cooling channel includes: a plurality of circulation flow passages formed at different axial positions of the first interlayer space and extending in a manner of surrounding the space in the tub; and the plurality of communicating flow passages are formed between two adjacent circulating flow passages in the axial direction to communicate the two circulating flow passages.
Further, the two communication flow passages are arranged at different circumferential positions.
Further, the first liquid inlet and the first liquid outlet are arranged at different axial positions.
Further, two adjacent communication flow passages in the axial direction are provided at two opposite circumferential positions.
Furthermore, the flow passage section of the circulation flow passage has at least one straight-line section profile, and the section profile is parallel to the central axis and is positioned on one side of the flow passage section close to the central axis.
Furthermore, a plurality of flow guide pieces are arranged in the interlayer space of the dispersing barrel, and the flow guide pieces are at least arranged in the circulation flow channel.
Further, the dispersion barrel includes: the feeding barrel body is provided with a feeding hole of the dispersing barrel; the discharging barrel body is provided with a discharging port of the dispersing barrel; the separator is arranged between the feeding barrel body and the discharging barrel body and is provided with a central hole at least for the driving main shaft to pass through; the dispersion wheel is arranged in a barrel space formed by the feeding barrel body and is positioned on one side of the separator close to the feeding hole.
Further, the feed barrel body forms a first interlayer space
Further, the discharge barrel body is provided with a second interlayer space surrounding the barrel space, the second interlayer space being configured to have: the second liquid inlet is used for allowing cooling liquid to flow into the second interlayer space; the second liquid outlet is used for allowing cooling liquid to flow out of the second interlayer space; the second cooling flow channel extends from the second liquid inlet to the second liquid outlet so that a liquid flow formed by the cooling liquid in the second cooling flow channel at least has motion components in a first direction, a second direction and a third direction which are perpendicular to each other; wherein the second cooling flow passage includes: a plurality of circulation flow passages formed at different axial positions of the second interlayer space and extending in a manner of surrounding the space in the tub; and the plurality of communicating flow passages are formed between two adjacent circulating flow passages in the axial direction to communicate the two circulating flow passages.
Further, the bearing housing is provided with a third interlayer space surrounding the housing space, the third interlayer space being configured to have: a third liquid inlet for allowing the cooling liquid to flow into the third interlayer space; a third liquid outlet for the cooling liquid to flow out of the third interlayer space; a third cooling flow passage extending from the third liquid inlet to the third liquid outlet so that a liquid flow formed by the cooling liquid in the third cooling flow passage has at least motion components in a first direction, a second direction and a third direction which are perpendicular to each other; wherein the third cooling flow passage includes: a plurality of circulation flow passages formed at different axial positions of the third interlayer space and extending in a manner of surrounding the space in the tub; and the plurality of communicating flow passages are formed between two adjacent circulating flow passages in the axial direction to communicate the two circulating flow passages.
The beneficial effect of this application lies in: a high-speed disperser is provided for cooling a dispersing barrel by constructing a first cooling flow passage having a circulation flow passage and a communicating flow passage in a first sandwiched space of the dispersing barrel.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, serve to provide a further understanding of the application and to enable other features, objects, and advantages of the application to be more apparent. The drawings and their description illustrate the embodiments of the invention and do not limit it.
Further, throughout the drawings, the same or similar reference numerals denote the same or similar elements. It should be understood that the drawings are schematic and that elements and elements are not necessarily drawn to scale.
In the drawings:
fig. 1 is an overall schematic view of a high-speed disperser according to an embodiment of the present application;
FIG. 2 is a schematic perspective view of a portion of the high speed disperser shown in FIG. 1;
fig. 3 is an internal structural view of a part of the structure in the high-speed disperser shown in fig. 1;
FIG. 4 is a schematic view showing the internal structure of the first cooling system in the high-speed disperser shown in FIG. 1;
FIG. 5 is a schematic perspective view of a first cooling system in the high-speed disperser shown in FIG. 1;
FIG. 6 is a schematic perspective view of a second perspective view of the first cooling system of the high-speed disperser shown in FIG. 1;
FIG. 7 is a schematic top view of a first type of baffle in the high-speed disperser of FIG. 1;
FIG. 8 is a schematic top view of another first type of baffle in the high speed disperser of FIG. 1;
FIG. 9 is a schematic side view of the high speed disperser shown in FIG. 1;
FIG. 10 is a schematic perspective view of the portion of FIG. 9 taken along line A-A of FIG. 9;
FIG. 11 is a schematic view showing the internal structure of a second cooling system in the high-speed disperser shown in FIG. 1;
FIG. 12 is a schematic perspective view of a portion of a second cooling system of the high-speed disperser shown in FIG. 1;
FIG. 13 is a schematic top view of a second type of baffle in the high speed disperser of FIG. 1;
FIG. 14 is a schematic view showing the internal structure of a third cooling system in the high-speed disperser shown in FIG. 1;
FIG. 15 is a schematic perspective view of a portion of a third cooling system of the high-speed disperser shown in FIG. 1;
fig. 16 is a schematic structural view of a third partition plate in the high-speed disperser according to an embodiment of the present application;
FIG. 17 is a schematic top view of another third type of baffle in the high speed disperser of FIG. 1;
FIG. 18 is a schematic perspective view of a portion of a third cooling system according to a second embodiment of the present application;
FIG. 19 is a schematic perspective view of a third cooling system according to a third embodiment of the present application, partially cut away;
FIG. 20 is a schematic perspective view of the portion of FIG. 19 shown in another cutaway configuration;
FIG. 21 is a schematic perspective view of a third cooling system according to a fourth embodiment of the present application, partially cut away;
FIG. 22 is an enlarged fragmentary schematic view of a portion of FIG. 21;
FIG. 23 is a schematic perspective view of a portion of a third cooling system according to a fourth embodiment of the present application taken in another cross-section;
FIG. 24 is an enlarged fragmentary schematic view of a portion of FIG. 23;
fig. 25 is a schematic perspective view of a third cooling system according to a fourth embodiment of the present application, with a portion cut away.
Detailed Description
Embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While certain embodiments of the present disclosure are shown in the drawings, it is to be understood that the disclosure may be embodied in various forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided for a more thorough and complete understanding of the present disclosure. It should be understood that the drawings and embodiments of the disclosure are for illustration purposes only and are not intended to limit the scope of the disclosure.
It should be noted that, for convenience of description, only the portions related to the related invention are shown in the drawings. The embodiments and features of the embodiments in the present disclosure may be combined with each other without conflict.
It should be noted that the terms "first", "second", and the like in the present disclosure are only used for distinguishing different devices, modules or units, and are not used for limiting the order or interdependence relationship of the functions performed by the devices, modules or units.
It is noted that references to "a", "an", and "the" modifications in this disclosure are intended to be illustrative rather than limiting, and that those skilled in the art will recognize that "one or more" may be used unless the context clearly dictates otherwise.
The present disclosure will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Referring to fig. 1 to 3, a high-speed disperser 100 of the present application includes: a dispersing barrel 101, a dispersing wheel 102, a driving motor 103, a driving main shaft 104 and a bearing seat 105.
Wherein the dispersing barrel 101 has a barrel inner space 1010 for containing the slurry to be dispersion-treated. The dispersing wheel 102 is rotatably arranged in the barrel inner space 1010, and the dispersing wheel 102 is driven by the driving motor 103 to rotate around a central axis S at a high speed, so that the slurry in the dispersing barrel 101 is dispersed; the central axis S here corresponds to the axis of the dispersing wheel 102 or the barrel space 1010. The driving spindle 104 is used for transmission between the driving motor 103 and the dispersing wheel 102, and specifically, one end of the driving spindle 104 is connected to the dispersing wheel 102 in a rotation-stopping manner, and the other end is connected to an output shaft of the driving motor 103 through a coupling. The bearing housing 105 is used to mount a plurality of bearings 106 through which the drive shaft 104 passes, and the bearing housing 105 is formed with a housing space 1050 that accommodates the bearings 106.
The high-speed rotation of the dispersing wheel 102 generates a large amount of heat, and the slurry collides during dispersion to generate heat, which needs to be dissipated in time, so that once the heat is accumulated, the heat has great influence on the quality of the slurry and great damage to equipment.
Referring to fig. 4 to 8, the high-speed disperser 100 preferably further includes a first cooling system 20 for cooling the dispersing barrel 101, and the first cooling system 20 includes a first interlayer space formed or disposed on the dispersing barrel 101. Wherein the first interlayer space is distributed around the barrel space 1010, the first interlayer space being configured to have: a first liquid inlet 21, a first liquid outlet 22 and a first cooling channel 23. Wherein, the first liquid inlet 21 is formed or arranged outside the dispersion barrel 101 and is used for allowing the cooling liquid to flow into the first interlayer space; a first liquid outlet 22 is formed or arranged outside the dispersion barrel 101 and used for allowing the cooling liquid to flow out of the first interlayer space; the first cooling flow passage 23 extends from the first liquid inlet 21 to the first liquid outlet 22 so that the flow of the cooling liquid in the first cooling flow passage 23 has at least motion components in a first direction, a second direction and a third direction perpendicular to each other. Specifically, the first direction may be defined as a direction parallel to the central axis S, and the second direction and the third direction are configured as two mutually perpendicular directions on a plane perpendicular to the central axis S.
As shown in fig. 4 to 8, as a concrete scheme, the first cooling flow passage 23 includes a circulation flow passage 231 and a communication flow passage 232. The plurality of circulation flow paths 231 are provided, and the plurality of circulation flow paths 231 are formed at different axial positions (the axial positions are in a direction parallel to the central axis S) of the first interlayer space and extend so as to surround the barrel space 1010. Specifically, the plurality of circulation flow channels 231 are partitioned by a plurality of first partition plates 24 axially spaced apart in the sandwiched space. The number of the communication flow passages 232 is plural, and the plural communication flow passages 232 are formed between two adjacent circulation flow passages 231 in the axial direction to communicate the two circulation flow passages 231. Specifically, the communication flow passage 232 is formed in the first partition plate 24 in the axial direction. By providing the circulation flow channel 231 and the communication flow channel 232 so that the cooling liquid flows in the cooling flow channel in a spatially folded manner, heat generated when the slurry in the dispersing barrel 101 is dispersed is absorbed.
Referring to fig. 5 and 6, as a preferable mode, the two communication flow passages 232 are provided at different circumferential positions (the circumferential positions are in a direction around the central axis S).
As a further alternative, as shown in fig. 5 and 6, two opposing circumferential positions are provided in two communication flow passages 232 adjacent in the axial direction, so that the circulation flow passage 231 has the longest stroke in the circumferential direction through which the cooling liquid can flow, whereby the cooling liquid absorbs the heat in the dispersion barrel 101 to the greatest extent. Wherein "relative position" is specifically interpreted as: with a plane perpendicular to the central axis S as a reference plane, an included angle between the center of the projection of the two axially adjacent communicating flow channels 232 on the reference plane and a connecting line of the projection points of the central axis S on the reference plane is 180 °.
As shown in fig. 7 and 8, the communication flow passage 232 may preferably be formed in one of a circular hole shape and a kidney-shaped hole shape according to a design flow rate of the coolant.
As shown in fig. 5 and 6, the first inlet port 21 and the first outlet port 22 are preferably provided at different axial positions.
Preferably, the flow path cross section of the annular flow path 231 has at least one linear cross sectional profile, where the "flow path cross section" is a cross section formed by cutting the annular flow path 231 in a plane passing through and coinciding with the central axis S. The cross-sectional profile is parallel to the central axis S and is located on the side of the flow passage cross section close to the central axis S, so that the maximum area surrounding the barrel inner space 1010 is provided in the circumferential direction of the annular flow passage while the safe wall thickness of the dispersion barrel 101 is ensured, and the cooling area is large, so that the heat generated in the barrel inner space 1010 can be sufficiently absorbed by the cooling liquid in the annular flow passage.
As a further alternative, as shown in fig. 4, the cross-sectional profiles of the flow passage sections of the circulation flow passage 231 in the axial direction are all straight lines parallel to the central axis S, and the cross-sectional profiles of the flow passage sections of the circulation flow passage 231 in the radial positions (in any direction perpendicular to the central axis S) are all straight lines perpendicular to the central axis S, and at this time, the cross-sectional shape of the annular flow passage is rectangular, so as to ensure the flow rate of the cooling liquid in the annular flow passage.
Referring to fig. 4, 9 and 10, as a preferable scheme, a plurality of flow guiding members 25 are further disposed in the interlayer space of the dispersing barrel 101, the flow guiding members 25 are disposed at least in the circulation flow channel 231, and the flow guiding members 25 guide the passing cooling liquid to prolong the heat absorption time of the flow in the circulation flow channel 231. Specifically, one circulation flow channel (defined as a sub-flow channel 233) axially distant from the first liquid outlet 22 is located at one end of the barrel space 1010, a communication flow channel 232a close to the first liquid inlet 21 and a communication flow channel 232b distant from the first liquid inlet 21 are formed in the first partition plate 24 adjacent to the sub-flow channel 233, and the cooling liquid flowing from the first liquid outlet 22 first enters the sub-flow channel 233 through the communication flow channel 232a and then enters the next circulation flow channel 231 through the communication flow channel 232b to cool the end region of the barrel space 1010.
The flow guiding elements 25 are formed in the secondary flow channel 233, a connecting line between the center of the communicating flow channel 232a and the center of the communicating flow channel 232b is perpendicular to at least one flow guiding element 25, and the extension lines of the plurality of flow guiding elements 25 are sequentially intersected end to form a polygon. The cooling liquid is fully diffused in the auxiliary flow channel 233 by the guiding function of the flow guide 25, and the heat absorption effect is improved.
As a further alternative, as shown in fig. 11 to 13, the dispersing barrel 101 includes a feeding barrel body 1011, a discharging barrel body 1012, and a partition 1013; wherein the feeding barrel body 1011 is provided with a feeding port 1014 of the dispersing barrel 101, and the feeding barrel body 1011 forms a first interlayer space, so that the first cooling system 20 mainly cools the feeding barrel body 1011; the discharging barrel body 1012 is provided with a discharging hole 1015 of the dispersing barrel 101. The partition 1013 is provided between the feed barrel 1011 and the discharge barrel 1012 and is provided with a central hole through which at least the driving main shaft 104 passes. The dispersing wheel 102 is disposed at the inter-barrel space formed by the feeding barrel body 1011 and at a side of the partition 1013 near the feed port 1014. The inner diameter of the central hole is larger than the outer diameter of the driving main shaft 104, so that the dispersed slurry can enter the discharging barrel body 1012 from the feeding barrel body 1011 through the space between the driving main shaft 104 and the central hole.
Referring to fig. 11 to 13, the high-speed disperser 100 preferably further includes a second cooling system 30 for cooling the discharging barrel body 1012, and the second cooling system 30 includes a second interlayer space formed or disposed on the discharging barrel body 1012. Wherein the second interlayer space is distributed around the space inside the tub, the second interlayer space being configured to have: a second inlet port 31, a second outlet port 32, and a second cooling channel 33. The second liquid inlet 31 is formed on or arranged outside the material storage barrel body and is used for allowing cooling liquid to flow into the second interlayer space; the second liquid outlet 32 is formed or arranged outside the discharging barrel body 1012 and is used for allowing the cooling liquid to flow out of the second interlayer space; the second cooling flow passage 33 extends from the second inlet port 31 to the second outlet port 32 so that the flow of the cooling liquid in the second cooling flow passage 33 has at least motion components in a first direction, a second direction and a third direction perpendicular to each other. Specifically, the first direction may be a direction parallel to the central axis S, and the second direction and the third direction may be configured as two mutually perpendicular directions on a plane perpendicular to the central axis S.
As shown in fig. 11 to 13, as a concrete configuration, the second cooling flow passage 33 includes a circulation flow passage 331 and a communication flow passage 332. The number of the circulation flow paths 331 is plural, and the plural circulation flow paths 331 are formed at different axial positions (the axial positions are directions parallel to the central axis S) of the second interlayer space and extend so as to surround the space in the tub. Specifically, the plurality of circulation flow paths 331 are partitioned by a plurality of second partition plates 34 axially spaced apart in the sandwiched space. The communication flow path 332 is provided with a plurality of communication flow paths 332, and the plurality of communication flow paths 332 are formed between two adjacent circulation flow paths 331 in the axial direction to communicate the two circulation flow paths 331. Specifically, the communication flow passage 332 is formed in the second partition plate 34 in the axial direction. By providing the circulation flow path 331 and the communication flow path 332, the cooling liquid flows in the second cooling flow path in a spatially returning manner, thereby absorbing the heat of the slurry in the discharge bucket and preventing the slurry from being overheated to affect the characteristics of the slurry.
Referring to fig. 11 to 13, an axis of the discharge hole 1015 of the dispersing barrel 101 is disposed perpendicular to the central axis S, and the discharge hole 1015 passes through the second cooling flow passage 33 so that the slurry passing through the discharge hole 1015 may be further cooled. One of the second partitions 34 at least partially overlaps the outlet 1015 in the axial direction, so that the outlet 1015 is in contact with the cooling fluid in at least two adjacent circulation channels, thereby prolonging the cooling time. The second partition 34 has a notch for the discharge opening 1015 to pass through, and a partially circular communication flow passage 332 is formed at the notch.
Referring to fig. 14 to 17, the high speed disperser 100 preferably further includes a third cooling system 40 for cooling the bearing housing 105, and the third cooling system 40 includes a third sandwiched space formed or provided on the bearing housing 105. Wherein the third interlayer space is distributed around the seat space 1050, the third interlayer space being configured to have: a third liquid inlet 41, a third liquid outlet 42 and a third cooling channel 43. The third liquid inlet 41 is formed on or arranged outside the bearing seat 105 and is used for allowing cooling liquid to flow into the third interlayer space; a third liquid outlet 42 is formed on or arranged outside the bearing seat 105, and is used for allowing the cooling liquid to flow out of the third interlayer space; the third cooling flow channel 43 extends from the third liquid inlet 41 to the third liquid outlet 42 so that the flow of the cooling liquid in the third cooling flow channel 43 has at least motion components in a first direction, a second direction and a third direction perpendicular to each other. Specifically, the first direction may be a direction parallel to the central axis S, and the second direction and the third direction are configured as two mutually perpendicular directions on a plane perpendicular to the central axis S.
As shown in fig. 14 to 17, as a concrete configuration, the third cooling flow passage 43 includes a circulation flow passage 431 and a communication flow passage 432. The circulation flow passages 431 are provided in plural, and the plural circulation flow passages 431 are formed at different axial positions (the axial positions are directions parallel to the central axis S, which is equivalent to the axis of the drive spindle 104 or the seat space 1050) of the third sandwiched space and extend so as to surround the seat space 1050. Specifically, the plurality of circulation flow passages 431 are partitioned by a plurality of third partition plates 44 axially spaced apart in the sandwiched space. The plurality of communication flow passages 432 are provided, and the plurality of communication flow passages 432 are formed between two adjacent circulation flow passages 431 in the axial direction to communicate the two circulation flow passages 431. Specifically, the communication flow passage 432 is formed in the axial direction on the third partition plate 44. By providing the circulation flow passage 431 and the communication flow passage 432, the cooling liquid flows in the third cooling flow passage in a spatially returning manner, and heat generated in the seat space 1050 is absorbed, thereby achieving rapid heat dissipation of the bearing 106.
As shown in fig. 16 and 17, the communication flow path 432 may be preferably formed in one of a circular hole shape and a kidney-shaped hole shape according to a designed flow rate of the coolant.
Referring to fig. 18, as an alternative, a longitudinal partition plate 45 is formed in the third sandwiched space in a direction parallel to the central axis S, and the communication flow passages 432a of the axially adjacent third partition plates 44 are located on both sides of the longitudinal partition plate 45, so that the path taken by the cooling liquid on one circulation passage is almost a full circle, and the heat of the seat space 1050 can be diffused into the cooling liquid for a long time.
In the scheme, the cooling flow channel is formed into the circulation flow channel and the communication flow channel, so that the flowing time of the cooling liquid in the cooling flow channel is prolonged to improve the heat dissipation effect, however, compared with the traditional cooling mode, the radial multilayer circulation flow channel has the advantage that the residence time of the cooling liquid absorbed in the cooling flow channel under the same cooling liquid flow speed is not particularly obvious.
As a further alternative, as shown in fig. 19 and 20, a plurality of layers of circulation passages 433a are provided in the radial direction of the central axis S, the circulation passages of two radially adjacent layers are connected by the transfer passages 434, and the two radially adjacent transfer passages 434 are provided at different axial positions. For example, in one embodiment of the present application, the interlayer space is formed with an inner flow path 4331, a middle flow path 4332 and an outer flow path 4333. By arranging the multilayer circulation channels, the flowing time of the cooling liquid in the cooling flow channel is further prolonged, and the heat dissipation effect is improved.
An inter-wall space 46 which is through in the axial direction and the circumferential direction is arranged between the two adjacent layers of circulation channels, and the inter-wall space 46 is filled with phase change materials. By utilizing the characteristics of the phase-change material, when the temperature of the circulation channel reaches the phase-change temperature, the phase-change material absorbs heat without increasing the temperature, and the temperature of the heat-generating part of the dispersion machine is ensured not to be increased too much in a short time. Meanwhile, when the high-speed dispersion machine stops, heat absorbed by the phase-change material is diffused to cooling liquid in the circulation channel, and quick heat dissipation to room temperature is achieved.
In order to adapt to the temperature of the cooling liquid in each layer of the circulation flow passage 431 in the radial direction, the phase transition temperature of the phase change material in the inner-layer wall space 46 is higher than that of the phase change material in the outer-layer wall space 46.
Referring to fig. 21 to 24, when a heat generating portion of the high speed disperser is overheated, and the coolant may reach the highest temperature through the inner layer flow channel 4331, the outer layer flow channel cannot achieve the effect of auxiliary heat dissipation, and the coolant needs to be rapidly discharged. As a further proposal, a temporary water outlet point 436 is further provided between the inner layer flow channel 4331 and the liquid outlet 42a, the temporary water outlet point 436 is provided with a flexible bag 51 near one side of the inner layer flow channel 4331, the inner space of the flexible bag 51 is communicated with an in-wall space 46 near the central axis S, the phase change material in the in-wall space is partially filled into the flexible bag 51, and the temporary water outlet point 436 is blocked when the flexible bag 51 is filled with the phase change material. An arc-shaped limiting part 437 is formed on the inner wall of the middle flow channel 4332 close to the central flexible bag 51, so as to limit the shape of the flexible bag 51 filled with the phase change material. The phase change temperature of the inner layer phase change material is designed to be the safe temperature of the heat generating part of the dispersion machine (when the temperature is higher than the safe temperature, the temperature is regarded as overheating), when the temperature of the inner layer circulation flow channel 431 reaches the safe temperature, the phase change material of the inner layer is changed from a solid phase to a liquid phase, the flexible bag 51 is extruded into the inner wall space under the action of the cooling hydraulic pressure in the inner layer flow channel 4331, so that the temporary water outlet point 436 is opened, and the overheated cooling liquid in the inner layer flow channel 4331 directly flows out through the temporary water outlet point 436 and the liquid outlet 42 a.
Referring to fig. 25, as an alternative, a plurality of circulation passages 433b are provided in the radial direction of the central axis S, an inter-wall space 46 that penetrates in the circumferential direction is provided between the circulation passages 433b of adjacent two layers, and the inter-wall space 46 is filled with a phase change material. The phase transition temperature of the phase change material in the in-wall space 46 gradually decreases from the inlet 41 toward the outlet 42.
The foregoing description is only exemplary of the preferred embodiments of the disclosure and is illustrative of the principles of the technology employed. It will be appreciated by those skilled in the art that the scope of the invention in the embodiments of the present disclosure is not limited to the specific combination of the above-mentioned features, but also encompasses other embodiments in which any combination of the above-mentioned features or their equivalents is made without departing from the inventive concept as defined above. For example, the above features and (but not limited to) technical features with similar functions disclosed in the embodiments of the present disclosure are mutually replaced to form the technical solution.

Claims (8)

1. A high-speed disperser, comprising:
a dispersing barrel for containing the slurry to be subjected to the dispersing treatment;
the dispersing wheel is rotatably arranged in the barrel inner space of the dispersing barrel;
the driving motor is used for driving the dispersion wheel to rotate around a central axis;
the driving main shaft is used for forming transmission between the driving motor and the dispersing wheel;
the bearing seat is used for mounting a plurality of bearings for the driving main shaft to pass through, and a seat inner space for accommodating the bearings is formed in the bearing seat;
the method is characterized in that:
the dispersion barrel is provided with a first interlayer space surrounding the barrel inner space, the first interlayer space being configured to have:
the first liquid inlet is used for allowing cooling liquid to flow into the first interlayer space;
the first liquid outlet is used for allowing cooling liquid to flow out of the first interlayer space;
a first cooling flow passage extending from the first liquid inlet to the first liquid outlet so that a flow of the cooling liquid formed in the first cooling flow passage has at least motion components in a first direction, a second direction and a third direction which are perpendicular to each other;
wherein, first cooling channel includes:
a plurality of circulation flow passages formed at different axial positions of the first interlayer space and extending in a manner of surrounding the space in the tub;
a plurality of communicating flow passages formed between two adjacent circulating flow passages in the axial direction to communicate the two circulating flow passages;
two adjacent communication flow passages in the axial direction are arranged at opposite circumferential positions;
a plurality of layers of circulation channels are arranged in the radial direction of the central axis, two adjacent layers of circulation channels in the radial direction are connected through the overflowing channels, and two overflowing channels adjacent in the radial direction are arranged at different axial positions;
an inner wall space which is through in the axial direction and the circumferential direction is arranged between the two adjacent layers of circulation channels, and phase change materials are filled in the inner wall space; the phase-change temperature of the phase-change material in the inner space of the inner wall is higher than that of the phase-change material in the outer wall.
2. The high-speed disperser according to claim 1, characterized in that:
the first liquid inlet and the first liquid outlet are arranged at different axial positions.
3. The high-speed disperser according to claim 1, characterized in that:
the flow passage section of the circular flow passage has at least one straight-line section contour, and the section contour is parallel to the central axis and is positioned on one side of the flow passage section close to the central axis.
4. The high-speed disperser according to claim 1, characterized in that:
and a plurality of flow guide pieces are also arranged in the interlayer space of the dispersion barrel, and the flow guide pieces are at least arranged in the circulation flow channel.
5. The high-speed disperser according to claim 1, characterized in that:
the dispersion barrel includes:
the feeding barrel body is provided with a feeding hole of the dispersing barrel;
the discharging barrel body is provided with a discharging port of the dispersing barrel;
the separator is arranged between the feeding barrel body and the discharging barrel body and is provided with a central hole at least for the driving main shaft to pass through;
the dispersion wheel is arranged in the barrel space formed by the feeding barrel body and is positioned on one side of the separator close to the feeding hole.
6. The high-speed disperser according to claim 5, characterized in that:
the feed barrel body forms the first interlayer space.
7. The high-speed disperser according to claim 5, characterized in that:
the discharge barrel body is provided with a second interlayer space surrounding the barrel inner space, the second interlayer space being configured to have:
the second liquid inlet is used for allowing cooling liquid to flow into the second interlayer space;
a second liquid outlet for flowing cooling liquid out of the second interlayer space;
a second cooling flow passage extending from the second liquid inlet to the second liquid outlet so that a flow of the cooling liquid formed in the second cooling flow passage has at least motion components in a first direction, a second direction and a third direction which are perpendicular to each other;
wherein the second cooling flow passage includes:
a plurality of circulation flow passages formed at different axial positions of the second interlayer space and extending in a manner of surrounding the space in the tub;
and the plurality of communication flow passages are formed between two adjacent circulation flow passages in the axial direction so as to communicate the two circulation flow passages.
8. The high-speed disperser according to claim 1, characterized in that:
the bearing housing is provided with a third interlayer space surrounding the housing space, the third interlayer space being configured to have:
a third liquid inlet for allowing cooling liquid to flow into the third interlayer space;
a third liquid outlet for flowing cooling liquid out of the third interlayer space;
a third cooling flow passage extending from the third liquid inlet to the third liquid outlet so that a flow of the cooling liquid formed in the third cooling flow passage has at least motion components in a first direction, a second direction and a third direction which are perpendicular to each other;
wherein the third cooling flow passage includes:
a plurality of circulation flow passages formed at different axial positions of the third interlayer space and extending in a manner of surrounding the space in the tub;
and the plurality of communication flow passages are formed between two adjacent circulation flow passages in the axial direction so as to communicate the two circulation flow passages.
CN202111653805.2A 2021-12-31 2021-12-31 High-speed dispersion machine Active CN113996217B (en)

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Publication number Priority date Publication date Assignee Title
CN114682149B (en) * 2022-02-28 2023-01-31 浙江汉信科技有限公司 Stirring device and stirring paddle thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105148766A (en) * 2015-09-09 2015-12-16 深圳市尚水智能设备有限公司 High-speed dispersing device, high-speed dispersing equipment and high-speed dispersing method
CN107774224A (en) * 2016-08-31 2018-03-09 天津市津冠润滑脂有限公司 Lubricating grease mediation kettle
CN208627081U (en) * 2018-06-12 2019-03-22 北京北方华创新能源锂电装备技术有限公司 A kind of cooling device and high speed disperser of high speed disperser
CN111629559A (en) * 2020-04-29 2020-09-04 上海航天科工电器研究院有限公司 Liquid cooling heat dissipation plate based on three-dimensional cooling flow channel and machining method thereof
CN212588185U (en) * 2020-08-03 2021-02-23 安徽威灵汽车部件有限公司 Motor casing, motor and vehicle with motor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102394230B (en) * 2011-11-11 2013-07-17 电子科技大学 Multi-start spiral flow channel liquid cooler used for heat radiation of electronic component
DE102012008209A1 (en) * 2012-04-21 2013-10-24 Volkswagen Aktiengesellschaft Electric machine
US20140246931A1 (en) * 2013-03-04 2014-09-04 Remy Technologies, Llc Liquid-cooled rotary electric machine having fluid channel with auxiliary coolant groove
TWM517473U (en) * 2015-06-16 2016-02-11 Univ Nat Cheng Kung Liquid cooling type casing with dual helical coolant flow passages
CN108574365A (en) * 2017-03-10 2018-09-25 郑州宇通客车股份有限公司 A kind of fluid-cooled electrical machine shell and the fluid-cooled electrical machine using the fluid-cooled electrical machine shell
CN206577429U (en) * 2017-03-21 2017-10-24 洛阳隆中重工机械有限公司 A kind of simple efficient dense mechanism
CN109285821A (en) * 2017-07-19 2019-01-29 刘梅 A kind of Multi-start spiral flow channel liquid cooler used for heat radiation of electronic component
NL2019306B1 (en) * 2017-07-20 2019-02-12 E Traction Europe Bv Cooling jacket and in-wheel motor with a cooling jacket
CN109474119A (en) * 2018-12-19 2019-03-15 江苏金彭车业有限公司 A kind of machine shaft with forced cooling device
CN214205187U (en) * 2020-12-25 2021-09-14 珠海格力电器股份有限公司 Cooling structure, motor and air compressor machine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105148766A (en) * 2015-09-09 2015-12-16 深圳市尚水智能设备有限公司 High-speed dispersing device, high-speed dispersing equipment and high-speed dispersing method
CN107774224A (en) * 2016-08-31 2018-03-09 天津市津冠润滑脂有限公司 Lubricating grease mediation kettle
CN208627081U (en) * 2018-06-12 2019-03-22 北京北方华创新能源锂电装备技术有限公司 A kind of cooling device and high speed disperser of high speed disperser
CN111629559A (en) * 2020-04-29 2020-09-04 上海航天科工电器研究院有限公司 Liquid cooling heat dissipation plate based on three-dimensional cooling flow channel and machining method thereof
CN212588185U (en) * 2020-08-03 2021-02-23 安徽威灵汽车部件有限公司 Motor casing, motor and vehicle with motor

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