CN218687064U - Diaphragm coating slurry recovery device - Google Patents
Diaphragm coating slurry recovery device Download PDFInfo
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- CN218687064U CN218687064U CN202222960231.XU CN202222960231U CN218687064U CN 218687064 U CN218687064 U CN 218687064U CN 202222960231 U CN202222960231 U CN 202222960231U CN 218687064 U CN218687064 U CN 218687064U
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Abstract
The utility model relates to a lithium cell technical field just discloses a diaphragm coating thick liquids recovery unit, which comprises a bod, the left side fixed mounting of fuselage has the shell, the first motor of top fixedly connected with of shell, the output fixedly connected with one end of first motor extends to the inboard stirring rake of shell, the one end of first motor and the inner chamber diapire fixed connection of shell are kept away from to the stirring rake, the top fixedly connected with of shell is located first motor left side and one end and extends to the inboard inlet pipe of shell, the right side fixedly connected with one end of shell extends to the inboard first solenoid valve of fuselage. This diaphragm coating thick liquids recovery unit possesses advantages such as the filter effect is good, has solved most only possesses the recovery function of current diaphragm coating thick liquids recovery unit, can not be fine filter thick liquids, and possess filter function's thick liquids recovery unit, because of the easy caking of thick liquids after the use, leads to the not good problem of filter effect.
Description
Technical Field
The utility model relates to a lithium cell technical field specifically is a diaphragm coating thick liquids recovery unit.
Background
The lithium ion battery is widely applied to the fields of electronic products, power drive, energy storage and the like due to a series of advantages of excellent electrical property, long service life, environmental protection and the like, the diaphragm is an important component of the lithium battery, the traditional lithium battery diaphragm mainly adopts a polyethylene or polypropylene diaphragm, but the heat resistance and the wettability to electrolyte limit the application range, so that the ceramic coating diaphragm is produced at the same time, the heat resistance and the wettability to electrolyte of the polyethylene or polypropylene diaphragm can be greatly improved through ceramic coating, the ceramic coating diaphragm replaces a common diaphragm, is an inevitable choice of a large battery with high energy and high power and is also an integrated requirement of market and science and technology, and in order to avoid waste, the used revolutionary coating slurry is often required to be recycled.
Most of existing membrane coating slurry recovery devices only have a recovery function, the slurry cannot be well filtered, and the slurry recovery devices with the filtering function are poor in filtering effect due to the fact that the used slurry is easy to agglomerate, so that the membrane coating slurry recovery devices are provided to solve the problems.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a not enough to prior art, the utility model provides a diaphragm coating thick liquids recovery unit possesses advantages such as the filter effect is good, has solved most recovery function that only possesses of current diaphragm coating thick liquids recovery unit, can not be fine filter thick liquids, and possess filter function's thick liquids recovery unit, because of the thick liquids after the use caking easily, leads to the not good problem of filter effect.
(II) technical scheme
The utility model provides an above-mentioned technical problem's technical scheme as follows: the utility model provides a diaphragm coating thick liquids recovery unit, includes the fuselage, the left side fixed mounting of fuselage has the shell, the first motor of top fixedly connected with of shell, the output fixedly connected with one end of first motor extends to the inboard stirring rake of shell, the one end that first motor was kept away from to the stirring rake and the inner chamber diapire fixed connection of shell, the top fixedly connected with of shell is located first motor left side and one end and extends to the inboard inlet pipe of shell, the right side fixedly connected with one end of shell extends to the inboard first solenoid valve of fuselage, the inboard fixed mounting of fuselage has quantity for two and be the spacing frame of upper and lower symmetric distribution, two the relative one side sliding connection of spacing frame has the filter cartridge, the inner chamber diapire of filter cartridge is equipped with the filter screen, the inner chamber left side wall fixed mounting of fuselage has the second motor, the output fixedly connected with first motor, the inboard rotation of fuselage is connected with and is located the filter cartridge left side and the dwang is located first helical gear right side, the outside fixedly connected with of fuselage and the second helical gear engaged with second eccentric wheel, the right side fixed connection of the helical gear is located the right side wall of the filter cartridge, the right side of the helical gear fixed connection has the filter cartridge and the right side of the solenoid valve communicates with the second helical gear.
The utility model has the advantages that: in will retrieving filterable coating slurry through the inlet pipe and drop into the shell, start first motor, make it drive the stirring rake and stir thick liquids, after the stirring, open first solenoid valve and make thick liquids flow in the filter cartridge, start that the second motor drives the filter cartridge and rock about, improve the filter effect.
This diaphragm coating thick liquids recovery unit has possessed the good advantage of filter effect.
On the basis of the technical scheme, the utility model discloses can also do following improvement.
Further, the front side fixed mounting of fuselage has the socket, the inboard of socket is equipped with the bolt, the front side fixedly connected with joint seat of filter cartridge, the slot with bolt looks adaptation is seted up to joint seat's inboard.
Adopt above-mentioned further scheme's beneficial effect be, the bolt is spacing to the filter cartridge with the slot suits for the filter cartridge can not remove forward from the inboard roll-off of fuselage.
Further, the inlet pipe is funnel dress setting, the slot is rectangular form setting.
Adopt the beneficial effect of above-mentioned further scheme to be, it makes the inboard that thick liquids can be more convenient get into the shell through the inlet pipe to leak hopper-shaped setting.
Further, the front side fixed mounting of filter cartridge has the handle that is located joint seat below, the antiskid groove has been seted up in the outside of handle.
Adopt above-mentioned further scheme's beneficial effect to be, can conveniently take out the filter cartridge and clear up through holding the handle.
Furthermore, the number of the springs is two, and the two springs are distributed up and down symmetrically.
Adopt above-mentioned further scheme's beneficial effect be, quantity is two and makes the elasticity of spring bigger, has improved the fly leaf and to the thrust of filter cartridge, makes it rock and feels stronger, and then has improved the filter effect.
Furthermore, the bottom fixed mounting of fuselage has the supporting legs, the quantity of supporting legs is four and is the distribution of rectangle array.
The beneficial effect who adopts above-mentioned further scheme is that, the supporting legs makes the fuselage keep away from ground, has protected the interior part of fuselage not easily to wet.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the connection structure of the filter cartridge and the clamping seat of the present invention;
FIG. 3 is a side view of the connection structure of the filter cartridge and the frame of the present invention;
FIG. 4 is an enlarged view of the structure A of the present invention;
fig. 5 is a top view of the connection structure of the eccentric wheel and the rotating rod of the present invention.
In the figure: 1. a body; 2. a housing; 3. a first motor; 4. a stirring paddle; 5. a feed pipe; 6. a first solenoid valve; 7. a limiting frame; 8. a filter cartridge; 9. a filter screen; 10. a second motor; 11. a first helical gear; 12. rotating the rod; 13. a second helical gear; 14. an eccentric wheel; 15. a spring; 16. a movable plate; 17. a second solenoid valve; 18. a socket; 19. a bolt; 20. a clamping seat; 21. and (4) a slot.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the embodiment, as shown in fig. 1-5, a separator coating slurry recycling device, the utility model discloses a fuselage 1, there is a shell 2 fixedly installed on the left side of fuselage 1, the top of shell 2 is fixedly connected with a first motor 3, the output end of first motor 3 is fixedly connected with a stirring paddle 4 with one end extending to the inner side of shell 2, one end of stirring paddle 4 far away from first motor 3 is fixedly connected with the inner cavity bottom wall of shell 2, the top of shell 2 is fixedly connected with an inlet pipe 5 located on the left side of first motor 3 and one end extending to the inner side of shell 2, the right side of shell 2 is fixedly connected with a first electromagnetic valve 6 with one end extending to the inner side of fuselage 1, the inner side of fuselage 1 is fixedly installed with two spacing frames 7 which are symmetrically distributed up and down, one side opposite to two spacing frames 7 is slidably connected with a filter box 8, the inner cavity bottom wall of filter box 8 is provided with a filter screen 9, the left side wall of the inner cavity of fuselage 1 is fixedly installed with a second motor 10, the output end of second motor 10 is fixedly connected with a first helical gear 11, the inner side wall of fuselage 1 is fixedly connected with a first helical gear 13, the inner side of fuselage 1 is fixedly connected with a right side of helical gear 13, the right side of helical gear is fixedly connected with a helical gear 13, the eccentric gear 13, the right side of fuselage 1 is fixedly connected with a helical gear 13, the right side of helical gear 13, the eccentric gear 13, the right side of helical gear is fixedly connected with a helical gear 13, the right side of the eccentric gear, the eccentric gear 13 of the fuselage 1;
a socket 18 is fixedly arranged on the front side of the machine body 1, a plug pin 19 is arranged on the inner side of the socket 18, a clamping seat 20 is fixedly connected on the front side of the filter box 8, and a slot 21 matched with the plug pin 19 is formed in the inner side of the clamping seat 20;
the plug pin 19 is matched with the slot 21 to limit the filter box 8, so that the filter box 8 cannot move forwards and slide out of the inner side of the machine body 1;
the feeding pipe 5 is arranged in a funnel shape, and the slot 21 is arranged in a strip shape;
the funnel-shaped arrangement enables the slurry to more conveniently enter the inner side of the shell 2 through the feeding pipe 5, and the slot 21 is arranged in a strip shape so that the left and right movement of the filter box 8 is not influenced;
a handle positioned below the clamping seat 20 is fixedly arranged at the front side of the filter box 8, and an anti-slip groove is formed in the outer side of the handle;
the filter box 8 can be conveniently taken out for cleaning by holding the handle, and the friction force between the hand and the handle is increased by the anti-slip groove, so that the handle is held more stably;
the number of the springs 15 is two, and the two springs 15 are distributed up and down symmetrically;
the number of the springs 15 is two, so that the elasticity of the springs 15 is larger, the thrust of the movable plate 16 to the filter box 8 is improved, the shaking feeling of the filter box is stronger, the filtering effect is further improved, and the springs 15 are distributed in a vertically symmetrical manner and are more stable;
the bottom of the machine body 1 is fixedly provided with four supporting legs which are distributed in a rectangular array;
the supporting legs make fuselage 1 keep away from ground, has protected 1 internals of fuselage not easily to wet, and quantity is four and be the distribution of rectangle array and make it more stable.
The working principle is as follows:
the first step is as follows: pouring coating slurry needing to be recycled and filtered into a feeding pipe 5, enabling the coating slurry to enter the inner side of the shell 2, starting a first motor 3, and driving a stirring paddle 4 to rotate by the first motor 3 to stir the slurry;
the second step is that: after the slurry is uniformly stirred, the first electromagnetic valve 6 is opened to enable the slurry to enter the inner side of the machine body 1 and fall into the filter box 8, and then filtering can be carried out;
the third step: the second motor 10 is started, the second motor 10 drives the first bevel gear 11 to rotate, the first bevel gear 11 drives the second bevel gear 13 to rotate, the second bevel gear 13 drives the rotating rod 12 to rotate, the rotating rod 12 drives the eccentric wheel 14 to rotate, when one end, far away from the circle center, of the eccentric wheel 14 rotates to the right side and contacts with the filter box 8, the filter box 8 is driven to move rightwards, the filter box 8 contacts with the right side movable plate 16 and then extrudes the spring 15 to shrink, when one end, far away from the circle center, of the eccentric wheel 14 rotates to the left side, the spring 15 rebounds due to tension and drives the filter box 8 to move leftwards, the second motor 10 continuously rotates to enable the filter box 8 to continuously move leftwards and rightwards in a reciprocating mode, and therefore the filtering effect is improved.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrases "comprising a," "8230," "8230," or "comprising" does not exclude the presence of additional like elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. A membrane coating slurry recovery device, includes fuselage (1), its characterized in that: left side fixed mounting of fuselage (1) has shell (2), the first motor (3) of top fixedly connected with of shell (2), the output fixedly connected with one end of first motor (3) extends to stirring rake (4) of shell (2) inboard, the one end of first motor (3) and the inner chamber diapire fixed connection of shell (2) are kept away from to stirring rake (4), the top fixedly connected with of shell (2) is located first motor (3) left side and one end extends to inlet pipe (5) of shell (2) inboard, the right side fixedly connected with one end of shell (2) extends to fuselage (1) inboard first solenoid valve (6), the inboard fixed mounting of fuselage (1) has quantity to be two and be upper and lower symmetric distribution's spacing frame (7), two the relative one side sliding connection of spacing frame (7) has filter cartridge (8), the inner chamber diapire of filter cartridge (8) is equipped with filter screen (9), the inner chamber left side wall fixed mounting of fuselage (1) has second motor (10), the output fixedly connected with of second motor (10) has first bevel gear (11) the first bevel gear (11) and bevel gear (11) inboard be located the first bevel gear (11) and first bevel gear (12) inboard mesh (12), the fuselage (11) inboard side of dwang (11), the inner chamber (11) is connected with the dwang (11) is located the fuselage (12) inboard Second helical gear (13) that closes, the outside fixedly connected with of dwang (12) is located eccentric wheel (14) of second helical gear (13) top, the inner chamber right side wall fixedly connected with spring (15) of fuselage (1), the left side fixedly connected with of spring (15) is located fly leaf (16) on filter cartridge (8) right side, the right side fixed mounting of fuselage (1) has second solenoid valve (17) with fuselage (1) inboard intercommunication.
2. The separator coating slurry recovery device according to claim 1, wherein: the front side fixed mounting of fuselage (1) has socket (18), the inboard of socket (18) is equipped with bolt (19), the front side fixedly connected with joint seat (20) of filter cartridge (8), slot (21) with bolt (19) looks adaptation are seted up to the inboard of joint seat (20).
3. The separator coating slurry recovery device according to claim 2, wherein: the feeding pipe (5) is arranged in a funnel mode, and the inserting grooves (21) are arranged in a long strip mode.
4. The separator coating slurry recovery device according to claim 1, wherein: the front side of the filter box (8) is fixedly provided with a handle positioned below the clamping seat (20), and the outer side of the handle is provided with an anti-skidding groove.
5. The separator coating slurry recovery device according to claim 1, wherein: the number of the springs (15) is two, and the two springs (15) are symmetrically distributed up and down.
6. The separator coating slurry recovery device according to claim 1, wherein: the bottom fixed mounting of fuselage (1) has the supporting legs, the quantity of supporting legs is four and is the distribution of rectangle array.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222960231.XU CN218687064U (en) | 2022-11-08 | 2022-11-08 | Diaphragm coating slurry recovery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222960231.XU CN218687064U (en) | 2022-11-08 | 2022-11-08 | Diaphragm coating slurry recovery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218687064U true CN218687064U (en) | 2023-03-24 |
Family
ID=85607961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222960231.XU Active CN218687064U (en) | 2022-11-08 | 2022-11-08 | Diaphragm coating slurry recovery device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218687064U (en) |
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2022
- 2022-11-08 CN CN202222960231.XU patent/CN218687064U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A diaphragm coating slurry recovery device Effective date of registration: 20230808 Granted publication date: 20230324 Pledgee: Hubei Bank Co.,Ltd. Zhushan Branch Pledgor: Hubei Dinghao New Energy Technology Co.,Ltd. Registration number: Y2023980051231 |