Compaction device for assembling EDI (Electronic Data Interchange) membrane block

Abstract

The utility model relates to the technical field of EDI (Electronic Data Interchange) membrane blocks, discloses a compaction device for assembling an EDI membrane block, and solves the problems that when the existing EDI membrane block is assembled and compacted, because the environment temperature does not reach a proper range, when the EDI membrane block is installed, the change of the environment temperature can possibly cause the shrinkage or expansion of a material, and the compaction effect is poor. The size and the structure of the membrane block are influenced, so that the compaction effect is influenced. A compaction device for EDI film block assembling comprises a machine body, a moving assembly is movably installed in the machine body, a compaction assembly is fixedly installed at the top of the machine body and comprises an electric telescopic rod and a compaction plate, and the compaction plate comprises a round hole, a temperature adjusting plate, an air outlet, a rectangular plate, a heating plate, a wind wheel, an L-shaped pipe groove, a connecting opening and a motor box. The compaction effect of the EDI film block during assembly is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of EDI modules, and specifically relates to a compaction device for assembling EDI modules. Background Technique

[0002] EDI modules are an advanced technology used for water treatment and purification, usually used to remove ions in water, especially electrolytes and dissolved inorganic salts. EDI modules combine ion exchange and electrochemical desalination technologies and can efficiently remove ions in water to produce high-purity water. However, when assembling existing EDI modules, the templates are directly installed layer by layer and then all are fixed with bolts to complete the installation. However, when the EDI modules are installed when the ambient temperature does not reach the appropriate range, the change in ambient temperature may cause the material to contract or expand, resulting in the problem of affecting the size and structure of the module and further affecting the compaction effect. Content of the Utility Model

[0003] The purpose of the utility model is to provide a compaction device for assembling EDI modules. By using this device to work, the problem that when assembling and compacting existing EDI modules, when the ambient temperature does not reach the appropriate range for installing the EDI modules, the change in ambient temperature may cause the material to contract or expand, resulting in affecting the size and structure of the module and further affecting the compaction effect is solved.

[0004] To achieve the above purpose, the utility model provides the following technical solution: A compaction device for assembling EDI modules, including a fuselage, a moving component for taking out EDI modules is movably installed inside the fuselage, and a compaction component for compacting EDI modules is fixedly installed on the top of the fuselage;

[0005] The compaction component includes an electric telescopic rod fixedly installed on the top of the fuselage, a compaction plate fixedly installed on the lower surface of the electric telescopic rod, a round hole penetrating through the upper surface of the compaction plate, a temperature adjustment plate fixedly installed on one side of the compaction plate, air outlets opened at both ends of the temperature adjustment plate, a rectangular plate opened at the bottom of the air outlet, a heating plate fixedly installed at the bottom of the rectangular plate, a motor box fixedly installed inside the rectangular plate, a wind wheel fixedly installed on one side of the motor box, an L-shaped pipe groove opened on the inner wall of the rectangular plate, and a connection port opened on the upper surface of the L-shaped pipe groove.

[0006] Preferably, an exhaust port is opened on the lower surface of the compaction plate, the connection port penetrates through the inside of the compaction plate, the exhaust port is communicated with the connection port, a motor slot is opened on one side of the compaction plate, a motor is fixedly installed inside the motor slot, a rotating shaft is fixedly installed on one side of the motor, and one end of the rotating shaft is fixedly installed with one side of the temperature adjustment plate.

[0007] Preferably, the moving component includes a moving plate movably arranged inside the fuselage. An EDI membrane module housing is arranged on the upper surface of the moving plate, and a vertical rod is movably installed on the upper surface of the moving plate.

[0008] Preferably, a storage groove is formed on the upper surface of the moving plate. A pulling groove is formed on the upper surface of the storage groove. A vertical plate and a T-shaped block are fixedly installed on the lower surface of the moving plate. Rollers are movably installed inside the vertical plate and the T-shaped block. The T-shaped block is arranged at one end of the lower surface of the moving plate. An installation groove is formed on the upper surface of the storage groove. A sliding groove is formed on the inner wall of the installation groove. A clamping groove is formed on the inner wall of the sliding groove. A guiding block is fixedly installed on the inner wall of the sliding groove. An arc-shaped plate is fixedly installed on one side of the guiding block.

[0009] Preferably, a plate groove is formed on the outer surface of the vertical rod. A rectangular groove is formed on the inner wall of the plate groove. A sliding plate is movably arranged inside the rectangular groove. A tension spring is fixedly installed on the inner wall of the plate groove. One end of the tension spring is fixedly installed with a clamping block. An arc surface is arranged on one side of the clamping block. The clamping block is adapted to the clamping groove. The installation groove is adapted to the vertical rod.

[0010] Preferably, a chamber is formed on one side of the fuselage. A moving groove is formed at the bottom of the chamber. A T-shaped groove is formed at the bottom of the moving groove. The T-shaped block is slidably connected with the T-shaped groove. The moving groove is adapted to the moving plate.

[0011] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0012] For a compaction device for EDI membrane module assembly proposed by the present utility model, when assembling the EDI membrane module, after installing the vertical rod into the installation groove and then rotating the vertical rod to fix it inside the moving plate, then pulling out the moving component and placing the EDI membrane module housing into the storage groove through the vertical rod. Then, the membrane sheets can be sequentially placed into the EDI membrane module housing. Then, the electric telescopic rod can be started to make the compaction plate flatten the resin of the membrane sheets. When the external environment is relatively low, the heating plate is started to make the hot air of the heating plate heat the module, so that the environmental temperature during compaction is within a suitable range, realizing the improvement of the compaction effect during the assembly of the EDI membrane module. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 is a schematic diagram of the overall structure of the present utility model;

[0014] Figure 2 is a schematic diagram of the overall cross-section of the present utility model;

[0015] Figure 3 is a schematic diagram of the cross-section of the fuselage of the present utility model;

[0016] Figure 4 is a schematic diagram of the cross-section of the moving plate of the present utility model;

[0017] Figure 5Schematic diagram of the guiding block and arc-shaped plate of the present utility model;

[0018] Figure 6 Partial sectional view schematic diagram of the vertical rod of the present utility model;

[0019] Figure 7 Sectional view schematic diagram of the compaction plate of the present utility model;

[0020] Figure 8 Schematic diagram of the compaction plate of the present utility model.

[0021] In the figure: 1, fuselage; 11, chamber; 12, moving groove; 13, T-shaped groove; 2, compaction assembly; 21, electric telescopic rod; 22, compaction plate; 221, round hole; 222, temperature regulating plate; 2221, air outlet; 2222, rectangular plate; 2223, heating plate; 2224, wind wheel; 2225, L-shaped pipe groove; 2226, connection port; 2227, motor box; 223, exhaust port; 224, motor slot; 225, motor; 226, rotating shaft; 3, moving assembly; 31, moving plate; 311, storage groove; 312, pulling groove; 313, vertical plate; 314, roller; 315, installation groove; 316, sliding groove; 317, clamping groove; 318, guiding block; 319, arc-shaped plate; 32, vertical rod; 321, plate groove; 322, rectangular groove; 323, sliding plate; 324, clamping block; 325, arc surface; 326, tension spring; 33, EDI membrane module housing. Detailed implementation manners

[0022] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments in the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0023] To further understand the content of the present utility model, the present utility model will be described in detail in conjunction with the accompanying drawings.

[0024] Combined with Figure 1 , a compaction device for EDI membrane module assembly includes a fuselage 1, a moving assembly 3 for taking out the EDI membrane module is movably installed inside the fuselage 1, and a compaction assembly 2 for compacting the EDI membrane module is fixedly installed on the top of the fuselage 1.

[0025] The present utility model will be further described below in conjunction with the embodiments.

[0026] Please refer to Figures 1-8, the compaction component 2 includes an electric telescopic rod 21 fixedly installed on the top of the fuselage 1, a compaction plate 22 fixedly installed on the lower surface of the electric telescopic rod 21, a circular hole 221 penetrating through the upper surface of the compaction plate 22, a temperature adjustment plate 222 fixedly installed on one side of the compaction plate 22, air outlets 2221 opened at both ends of the temperature adjustment plate 222, a rectangular plate 2222 opened at the bottom of the air outlet 2221, a heating plate 2223 fixedly installed at the bottom of the rectangular plate 2222, a motor box 2227 fixedly installed inside the rectangular plate 2222, a wind wheel 2224 fixedly installed on one side of the motor box 2227, an L-shaped pipe groove 2225 opened on the inner wall of the rectangular plate 2222, a connection port 2226 opened on the upper surface of the L-shaped pipe groove 2225. By means of the heating plate 2223 and the wind wheel 2224, the temperature for compaction can be adjusted when compacting the EDI membrane module, so as to better compact the membrane module and improve its density.

[0027] An exhaust port 223 is opened on the lower surface of the compaction plate 22. The connection port 2226 penetrates through the inside of the compaction plate 22, and the exhaust port 223 is communicated with the connection port 2226. A motor slot 224 is opened on one side of the compaction plate 22. A motor 225 is fixedly installed inside the motor slot 224. A rotating shaft 226 is fixedly installed on one side of the motor 225. One end of the rotating shaft 226 is fixedly installed with the temperature adjustment plate 222 on one side. By means of the rotating shaft 226, the temperature adjustment plate 222 can be flipped, so as to select when compacting the EDI membrane module.

[0028] The moving component 3 includes a moving plate 31 movably arranged inside the fuselage 1. An EDI membrane module housing 33 is arranged on the upper surface of the moving plate 31. A vertical rod 32 is movably installed on the upper surface of the moving plate 31. By means of the vertical rod 32, the EDI membrane module can be assembled inside the moving plate 31.

[0029] A storage groove 311 is opened on the upper surface of the moving plate 31. A pulling groove 312 is opened on the upper surface of the storage groove 311. A vertical plate 313 and a T-shaped block are fixedly installed on the lower surface of the moving plate 31. A roller 314 is movably installed inside the vertical plate 313 and the T-shaped block. The T-shaped block is arranged at one end of the lower surface of the moving plate 31. An installation groove 315 is opened on the upper surface of the storage groove 311. A chute 316 is opened on the inner wall of the installation groove 315. A clamping groove 317 is opened on the inner wall of the chute 316. A guiding block 318 is fixedly installed on the inner wall of the chute 316. An arc-shaped plate 319 is fixedly installed on one side of the guiding block 318. The vertical rod 32 can be fixed by means of the chute 316 and the clamping groove 317, and the EDI membrane module can be stored through the storage groove 311.

[0030] The outer surface of the vertical rod 32 is provided with a plate groove 321, the inner wall of the plate groove 321 is provided with a rectangular groove 322, a sliding plate 323 is movably arranged inside the rectangular groove 322, a tension spring 326 is fixedly installed on the inner wall of the plate groove 321, one end of the tension spring 326 is fixedly installed with a clamping block 324, an arc surface 325 is arranged on one side of the clamping block 324, the clamping block 324 is adapted to the clamping groove 317, the installation groove 315 is adapted to the vertical rod 32, and the vertical rod 32 can be installed inside the installation groove 315 through the clamping block 324, and then the vertical rod 32 can be fixed through the clamping groove 317.

[0031] A chamber 11 is provided on one side of the fuselage 1, a moving groove 12 is provided at the bottom of the chamber 11, a T-shaped groove 13 is provided at the bottom of the moving groove 12, the T-shaped block is slidably connected to the T-shaped groove 13, the moving groove 12 is adapted to the moving plate 31, and the moving plate 31 can be moved through the T-shaped groove 13.

[0032] Working principle: When assembling the EDI membrane module, it is necessary to choose whether to cool down or heat up according to the ambient temperature. Then, the motor 225 can be started to drive the rotating shaft 226 to flip the temperature regulating plate 222 so that the required side faces downward. Then, the moving plate 31 is pulled, and the vertical rod 32 is aligned with the installation groove 315 for installation. When installing the vertical rod 32, the clamping block 324 is squeezed into the plate groove 321. Then, the vertical rod 32 is inserted into the installation groove 315. As the vertical rod 32 enters, the clamping block 324 will move the column guiding block 318 to the bottommost position. Then, the vertical rod 32 can be rotated so that the clamping block 324 enters the clamping groove 317 along the arc-shaped plate 319. At this time, the installation of the vertical rod 32 is completed. Then, the EDI membrane module housing 33 can be placed into the storage groove 311, and then the membrane sheets can be installed. When the resin on the surface of the membrane sheet needs to be compacted, the moving plate 31 is pushed directly below the compaction plate 22, and the electric telescopic rod 21 is started to move the compaction plate 22 downward, thereby compacting the membrane sheet. At this time, because the required temperature has been adjusted in advance, the sealing performance between the membrane modules can be improved during compaction. After all the membrane sheets are installed, the moving plate 31 can be pulled out, and then the vertical rod 32 is rotated to disassemble the vertical rod 32. Finally, the compacted EDI membrane module can be bolt-fixed, and the speed of taking out the EDI membrane module after installation is also increased, realizing the effect of improving the compaction during the assembly of the EDI membrane module.

[0033] It should be noted that in this text, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprising", "including" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device comprising a series of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article or device.

[0034] Although the embodiments of the present invention have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A compacting device for EDI membrane block assembly, comprising a body (1), characterized in that: A moving assembly (3) for taking out the EDI membrane block is movably installed inside the body (1), and a compacting assembly (2) for compacting the EDI membrane block is fixedly installed on the top of the body (1); The compacting assembly (2) comprises an electric telescopic rod (21) fixedly mounted on the top of the machine body (1), a compacting plate (22) fixedly mounted on the lower surface of the electric telescopic rod (21), a circular hole (221) penetrating the upper surface of the compacting plate (22), a temperature regulating plate (222) fixedly mounted on one side of the compacting plate (22), air outlets (2221) provided at both ends of the temperature regulating plate (222), a rectangular plate (2222) provided at the bottom of the air outlet (2221), a heating plate (2223) fixedly mounted on the bottom of the rectangular plate (2222), a motor box (2227) fixedly mounted inside the rectangular plate (2222), a wind wheel (2224) fixedly mounted on one side of the motor box (2227), an L-shaped pipe groove (2225) provided on the inner wall of the rectangular plate (2222), and a connection port (2226) provided on the upper surface of the L-shaped pipe groove (2225).

2. The compacting device for EDI membrane block assembly according to claim 1, characterized in that: The lower surface of the compacting plate (22) is provided with an exhaust port (223), a connecting port (2226) passes through the interior of the compacting plate (22), the exhaust port (223) is communicated with the connecting port (2226), a motor slot (224) is provided on one side of the compacting plate (22), a motor (225) is fixedly installed inside the motor slot (224), a rotating shaft (226) is fixedly installed on one side of the motor (225), and one end of the rotating shaft (226) is fixedly installed on one side of the temperature regulating plate (222).

3. The compacting device for EDI membrane block assembly according to claim 1, characterized in that: The moving assembly (3) comprises a moving plate (31) movably arranged inside the fuselage (1), an EDI membrane block housing (33) being arranged on the upper surface of the moving plate (31), and a vertical rod (32) being movably mounted on the upper surface of the moving plate (31).

4. The compacting device for EDI membrane block assembly according to claim 3, characterized in that: The upper surface of the movable plate (31) is provided with a receiving groove (311), the upper surface of the receiving groove (311) is provided with a pulling groove (312), the lower surface of the movable plate (31) is fixedly installed with a vertical plate (313) and a T-shaped block, the vertical plate (313) and the T-shaped block are movably installed with rollers (314), the T-shaped block is arranged at one end of the lower surface of the movable plate (31), the upper surface of the receiving groove (311) is provided with a mounting groove (315), the inner wall of the mounting groove (315) is provided with a sliding groove (316), the inner wall of the sliding groove (316) is provided with a clamping groove (317), the inner wall of the sliding groove (316) is fixedly installed with a guide block (318), and one side of the guide block (318) is fixedly installed with an arc plate (319).

5. The compacting device for EDI membrane block assembly according to claim 4, characterized in that: The outer surface of the vertical pole (32) is provided with a plate groove (321), the inner wall of the plate groove (321) is provided with a rectangular groove (322), a slide plate (323) is movably arranged inside the rectangular groove (322), a tension spring (326) is fixedly installed on the inner wall of the plate groove (321), a clamping block (324) is fixedly installed on one end of the tension spring (326), a curved surface (325) is arranged on one side of the clamping block (324), the clamping block (324) is matched with the clamping groove (317), and the installation groove (315) is matched with the vertical pole (32).

6. The compacting device for EDI membrane block assembly according to claim 4, characterized in that: A chamber (11) is provided on one side of the body (1), a movable groove (12) is provided at the bottom of the chamber (11), a T-shaped groove (13) is provided at the bottom of the movable groove (12), a T-shaped block is slidably connected to the T-shaped groove (13), and the movable groove (12) is adapted to the movable plate (31).

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