Dedusting and moisture-proof treatment device for electrical automation element

Abstract

The invention discloses an electrical automation element dedusting and moisture-proof processing device, and relates to the technical field of electrical automation elements, the electrical automation element dedusting and moisture-proof processing device comprises a machine body, a machine door is movably installed on the machine body through hinges, two placing tables are arranged in the machine body, a first separation net is embedded in the placing tables, a base is installed below the machine body, and an air blowing pump is installed on the base; a first air blowing pipe is installed at the output end of the air blowing pump, the top of the first air blowing pipe is fixedly connected with the top of the machine body, a second air blowing pipe communicated with the first air blowing pipe is installed in the machine body, a first air blowing hole is formed in the second air blowing pipe, a moving mechanism is arranged on the machine body, and an auxiliary air blowing mechanism is further arranged in the machine body. The auxiliary blowing mechanism comprises a mounting block and a telescopic frame, the mounting block is slidably mounted on the placement table and the machine body, and the telescopic frame is mounted on the mounting block. The multi-angle blowing device achieves the effect of blowing electrical elements from multiple angles, reduces blowing dead angles, and improves the dust removal and damp-proof effects.

Description

Technical Field

[0001] The present invention relates to the technical field of electrical automation components, and in particular to a dust removal and moisture-proof treatment device for electrical automation components. Background Art

[0002] Electrical automation components are components of small machines and instruments, which are usually composed of several parts. During the use of electrical automation components, a dust removal and moisture-proof treatment device is required to ensure their normal operation.

[0003] After retrieval, a Chinese patent with the publication number CN117858404A discloses a dust removal and moisture-proof treatment device for electrical automation components, including a treatment box. A placement component is provided inside the treatment box. The treatment box is provided with a jet plate. The treatment box is fixed with a mounting plate. The mounting plate is provided with an air extraction box. The mounting plate is provided with a water tank. The mounting plate is installed with a motor. A rotating rod is provided inside the air extraction box. Blades are distributed outside the rotating rod. The rotating rod is provided with helical teeth. An air suction pipe is connected between the air extraction box and the treatment box. An air outlet pipe is connected between the air extraction box and the water tank. The mounting plate is provided with an electric heating box. A gas transmission pipe is connected between the water tank and the air extraction box. A guide pipe is connected between the air extraction box and the jet plate. A cooling component is provided outside the guide pipe. By starting the motor, the rotating rod and the blades are driven to rotate, so that the air inside the treatment box flows. During the flowing process, the air is dust-removed by the water tank, and the air is heated by the electric heating box. Thus, during the internal circulation of the air, the dust removal and moisture-proof treatment of the electrical automation components is completed.

[0004] Based on the above retrieval and in combination with the prior art, it is found that: When the existing equipment removes dust from electrical components, it generally blows the dust on the electrical components by blowing air. However, in the existing equipment, the electrical components are generally fixed in position, and at the same time, the blowing angle is also fixed and unchanged. This results in a small blowing range for the electrical components, thereby affecting the dust removal and moisture-proof effects. Summary of the Invention

[0005] The purpose of the present invention is to provide a dust removal and moisture-proof treatment device for electrical automation components to solve the problems raised in the above background art.

[0006] The technical solution of the present invention is: A dust removal and moisture-proof treatment device for electrical automation components, including a body. A machine door is movably installed on the body through a hinge. Two placement platforms are arranged inside the body. A first partition net is inlaid and installed on the placement platforms. A base is installed below the body. A blowing pump is installed on the base. A first blowing pipe is installed at the output end of the blowing pump. The top of the first blowing pipe is fixedly connected to the top of the body. A second blowing pipe communicated with the first blowing pipe is installed inside the body. A first blowing hole is opened on the second blowing pipe. A moving mechanism is arranged on the body. An auxiliary blowing mechanism is also arranged inside the body; The auxiliary blowing mechanism includes: An installation block and a telescopic frame, the installation block is slidably installed on the placement table and the fuselage, and the telescopic frame is installed on the installation block; An airbag and a pressing plate, the airbag is installed on the inner wall of the fuselage corresponding to the position of the upper telescopic frame, and the pressing plate is fixedly installed on the outer side wall of the airbag; A connecting plate, a telescopic rod and a first connecting shaft, the connecting plate is arranged below the side wall of the pressing plate, both ends of the telescopic rod are respectively connected with the connecting plate and the telescopic frame, and the first connecting shaft is movably installed on the telescopic frame; A corrugated pipe and a check valve, the corrugated pipe is arranged between the fuselage and the placement table, the other end of the corrugated pipe is communicated with the inside of the airbag, and the check valve is installed at the position corresponding to the placement table on the corrugated pipe; An inner cavity and a second air blowing hole, the inner cavity is arranged inside the placement table, there are multiple second air blowing holes, and the multiple second air blowing holes are evenly distributed on the inner wall of the placement table, and the second air blowing holes are communicated with the inside of the inner cavity.

[0007] Preferably, the telescopic frame is movably installed between the placement table and the fuselage through the installation block, the airbag is a telescopic structure with a spring inside, a one-way valve tube communicated with the outside is installed on the airbag, one end of the telescopic rod is movably sleeved on the first connecting shaft, and the telescopic rod is movably connected with the telescopic frame through the first connecting shaft.

[0008] Preferably, the moving mechanism includes a driving roller, a driving belt and a driving block. There are two driving rollers in total, and both driving rollers are movably installed on both sides inside the fuselage through motors. The driving belt is movably sleeved between the two driving rollers. There are two driving blocks in total, and the two driving blocks are respectively fixedly installed on the driving belt at the positions corresponding to the two placement tables, and the two driving blocks are respectively fixedly connected with the two placement tables.

[0009] Preferably, two moving seats are fixedly installed inside the fuselage, sliders are movably installed inside the two moving seats, and the two sliders are fixedly connected with the side walls of the placement table.

[0010] Preferably, an installation groove is opened inside the fuselage corresponding to the position of the second air blowing pipe, an installation seat is fixedly installed inside the installation groove, a movable seat is movably installed inside the installation seat through a torsion spring shaft, the second air blowing pipe is fixedly installed on the movable seat, and a link mechanism is arranged on the fuselage.

[0011] Preferably, the linkage mechanism includes a movable groove, a pressing rod, a lever, a reset rod, a connecting rod I, and a reset spring. The movable groove is formed in the upper movable seat and the machine body. The pressing rod is movably installed inside the movable groove and is fixedly connected to the upper slider. The lever is fixedly installed at one end of the movable seat away from the second air blowing pipe. The movable groove is formed between the machine body and the movable seat. The pressing rod is movably installed inside the movable groove and is fixedly connected to the slider. The connecting rod I is fixedly installed on the bottom wall surface of the lever. The reset rod is a rod with a rectangular structure, and the bottom wall surface of the reset rod has two inclined surfaces. The top of the connecting rod I is located inside the reset rod. The reset spring is movably installed inside the connecting rod I and is movably connected to the reset rod.

[0012] Preferably, a connecting rod II is movably installed between the two levers. Connecting shafts II are fixedly installed at the tops of the two levers. The connecting rod II is movably sleeved between the two connecting shafts II. Two maintenance openings are formed in the side wall of the machine body. A baffle is movably installed inside the maintenance openings.

[0013] Preferably, a dust collection groove is arranged below the interior of the machine body. A second partition net is installed inside the dust collection groove. A drying filter box is installed below the interior of the machine body. A return air pipe is installed on the drying filter box. The return air pipe corresponds to the position of the second partition net. An air suction pipe is installed on the input end of the air blowing pump. The air suction pipe is communicated with the interior of the drying filter box.

[0014] Preferably, a plurality of connecting pipes are installed on the corrugated pipe. The connecting pipes are communicated with the interior of the corrugated pipe. A positioning shaft is installed on the connecting pipe. The positioning shaft is movably connected to the telescopic frame. A first nozzle is installed below the side wall of the upper connecting pipe. A second nozzle is installed at the position corresponding to the connecting pipe on the lower telescopic frame. The second nozzle is communicated with the interior of the connecting pipe through the positioning shaft.

[0015] Preferably, a transmission gear ring is fixedly installed at the bottom of the first partition net. A rotating shaft is movably installed at the bottom of the placing table. A transmission gear is movably sleeved on the rotating shaft. The transmission gear meshes with the transmission gear ring for transmission. A transmission rack is installed at the position corresponding to the transmission gear at the bottom of the movable seat. The transmission gear meshes with the transmission rack for transmission.

[0016] The present invention provides an electrical automation component dust removal and moisture-proof treatment device through improvement. Compared with the prior art, it has the following improvements and advantages: First: Through the setting of the auxiliary air blowing structure in the present invention, when the placement table moves inside the fuselage, the movement of the upper placement table will squeeze the telescopic frame. After being squeezed, the telescopic frame will drive the telescopic rod and the connecting plate to move towards the pressing plate, thereby squeezing the pressing plate. Then, the pressing plate squeezes the airbag. At this time, the air inside the airbag will be discharged into the bellows and then enter the inner cavity, and then be blown onto the electrical components on the first partition net through the second air blowing hole, thus achieving the effect of blowing air on the electrical components from multiple angles, reducing the dead angle of air blowing, and improving the dust removal and moisture-proof effects.

[0017] Second: In the present invention, the driving roller is rotated by the motor, so that the driving roller can drive the driving belt to rotate. By controlling the back-and-forth rotation of the motor, the driving belt can be driven to move back and forth, and thus the two placement tables can be driven to move alternately and reciprocally through the transmission block. At this time, the electrical components will also move back and forth, thereby improving the air blowing effect on the electrical components.

[0018] Third: Through the setting of the transmission link mechanism in the present invention, the reciprocating movement of the placement table can be driven by the driving belt, and the slider will also move inside the moving seat. At this time, the slider drives the extrusion rod to move. When the extrusion rod moves to the bottom of the reset rod, the extrusion rod squeezes the reset rod. At this time, the squeezing force of the extrusion rod on the reset rod is less than the pressure of the reset rod on the reset spring. Subsequently, the reset rod can drive the lever to move to one side, thereby driving the movable seat and the second air blowing pipe to swing. At this time, the second air blowing pipe flips inside the fuselage, thus increasing the air blowing range. When the movable seat and the second air blowing pipe swing to the point where they cannot swing anymore, at this time, the squeezing force of the extrusion rod on the reset rod is greater than the pressure of the reset rod on the reset spring, and the reset spring will be compressed. At this time, the reset rod can move upward, the extrusion rod and the reset rod are separated, and then the extrusion rod is driven to move back to its original position, and the extrusion rod can squeeze the reset rod again. The reset rod will drive the second air blowing pipe to swing inside the fuselage again to blow air at other positions, thereby further improving the air blowing effect on the electrical components.

[0019] Fourth: In the present invention, when the placement table and the first partition net move, the transmission gear will move on the transmission rack, causing the transmission gear to rotate. The transmission gear meshes with the transmission gear ring for transmission, and the transmission gear can drive the transmission gear ring to rotate, thereby driving the first partition net to rotate. At this time, while the electrical components move back and forth and reciprocally on the first partition net, they will also rotate, further increasing the air blowing range for the electrical components and improving the dust removal and moisture-proof effects. Description of the Drawings

[0020] To more clearly illustrate the specific embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings required for the description of the specific embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0021] Figure 1 Schematic diagram of the overall front structure in the present invention; Figure 2 Cross-sectional view of the internal structure of the fuselage in the present invention; Figure 3 In the present invention Figure 2 Enlarged view of part A in; Figure 4 In the present invention Figure 2 Enlarged view of part B in; Figure 5 Schematic diagram of the internal partial structure in the present invention; Figure 6 In the present invention Figure 2 Enlarged view of part C in; Figure 7 Schematic diagram of the back structure of the fuselage in the present invention; Figure 8 In the present invention Figure 7 Enlarged view of part D in; Figure 9 Schematic diagram of the partial structure of the link mechanism in the present invention; Figure 10 Schematic diagram of the main structure of the placement table in the present invention.

[0022] Reference numerals: 1. Body; 2. Door; 3. Placing table; 4. First partition net; 5. Blowing pump; 6. First blowing pipe; 7. Second blowing pipe; 8. First blowing hole; 9. Base; 10. Mounting block; 11. Telescopic frame; 12. Airbag; 13. Pressing plate; 14. Connecting plate; 15. Telescopic rod; 16. First connecting shaft; 17. Bellows; 18. Check valve; 19. Inner cavity; 20. Second blowing hole; 21. Driving roller; 22. Driving belt; 23. Driving block; 24. Moving seat; 25. Slide block; 26. Mounting groove; 27. Mounting seat; 28. Movable seat; 29. Movable groove; 30. Extrusion rod; 31. Poking rod; 32. Reset rod; 33. First connecting rod; 34. Reset spring; 35. Second connecting rod; 36. Second connecting shaft; 37. Maintenance opening; 38. Baffle; 39. Dust collection groove; 40. Second partition net; 41. Dry filter box; 42. Return air pipe; 43. Suction pipe; 44. Driving gear ring; 45. Rotating shaft; 46. Driving gear; 47. Driving rack; 48. Connecting pipe; 49. Positioning shaft; 50. First nozzle; 51. Second nozzle. Detailed implementation manner

[0023] The present invention will be described in detail below. The technical solutions in the embodiments of the present invention are clearly and completely described. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0024] The present invention provides a dust removal and moisture-proof treatment device for electrical automation components by improvement. The technical solution of the present invention is as follows: As Figures 1 to 10 shown, the embodiment of the present invention provides a dust removal and moisture-proof treatment device for electrical automation components, including a body 1. The body 1 is of a hollow structure. A door 2 is movably installed on the body 1 through a hinge. The door 2 seals the inside of the body 1. Two placing tables 3 are arranged inside the body 1. A first partition net 4 is inlaid and installed on the placing table 3. Electrical components are placed on the first partition net 4 and are dust-removed and moisture-proofed inside the body 1. A base 9 is installed below the body 1. A blowing pump 5 is installed on the base 9. A first blowing pipe 6 is installed at the output end of the blowing pump 5. The first blowing pipe 6 is of a tubular structure. The top of the first blowing pipe 6 is fixedly connected to the top of the body 1. Two second blowing pipes 7 are movably installed inside the body 1. Both of the two second blowing pipes 7 are communicated with the inside of the first blowing pipe 6. A first blowing hole 8 is opened on the second blowing pipe 7. A moving mechanism is arranged on the body 1. An auxiliary blowing mechanism is also arranged inside the body 1; The auxiliary air blowing mechanism includes a mounting block 10, a telescopic frame 11, an airbag 12, a pressing plate 13, a connecting plate 14, a telescopic rod 15, a first connecting shaft 16, a corrugated pipe 17, a check valve 18, an inner cavity 19, and a second air blowing hole 20. The mounting block 10 is a rectangular block. The mounting block 10 is slidably mounted on the side wall of the placing table 3 and the inner wall of the fuselage 1. The telescopic frame 11 is mounted on the mounting block 10. The telescopic frame 11 is movably mounted between the placing table 3 and the fuselage 1 through the mounting block 10. The airbag 12 is mounted on the inner wall of the fuselage 1 corresponding to the position of the upper telescopic frame 11. The airbag 12 is a telescopic structure with a spring inside. A one-way valve pipe communicating with the inside of the fuselage 1 is mounted on the airbag 12, and a dust-proof net is provided at the nozzle of the one-way valve pipe. The pressing plate 13 is a rectangular plate. The pressing plate 13 is fixedly mounted on the outer side wall of the airbag 12. The connecting plate 14 is a rectangular structure. The connecting plate 14 is arranged below the side wall of the pressing plate 13. The telescopic rod 15 is a telescopic structure with a spring inside. Two ends of the telescopic rod 15 are respectively connected to the connecting plate 14 and the telescopic frame 11. The first connecting shaft 16 is movably mounted on the telescopic frame 11. One end of the telescopic rod 15 is movably sleeved on the first connecting shaft 16. The telescopic rod 15 is movably connected to the telescopic frame 11 through the first connecting shaft 16. The corrugated pipe 17 is a telescopic tubular structure. The corrugated pipe 17 is arranged between the fuselage 1 and the placing table 3. The other end of the corrugated pipe 17 communicates with the inside of the airbag 12. The check valve 18 is mounted on the corrugated pipe 17 corresponding to the position of the placing table 3. The inner cavity 19 is a rectangular structure. The inner cavity 19 is arranged inside the placing table 3. The second air blowing hole 20 is a circular hole. There are multiple second air blowing holes 20. The multiple second air blowing holes 20 are evenly distributed on the inner wall of the placing table 3. The second air blowing hole 20 communicates with the inside of the inner cavity 19. Through the setting of the auxiliary air blowing structure, when the placing table 3 moves inside the fuselage 1, the movement of the upper placing table 3 will squeeze the telescopic frame 11. After being squeezed, the telescopic frame 11 will drive the telescopic rod 15 and the connecting plate 14 to move towards the pressing plate 13, and then the pressing plate 13 can be squeezed. Thus, the pressing plate 13 squeezes the airbag 12. At this time, the air inside the airbag 12 will be discharged into the inside of the corrugated pipe 17, then enter the inside of the inner cavity 19, and then be blown onto the electrical components on the first partition net 4 through the second air blowing holes 20. Thus, the effect of blowing the electrical components from multiple angles is achieved, the dead angle of blowing is reduced, and the dust removal and moisture-proof effects are improved.

[0025] The moving mechanism includes a driving roller 21, a driving belt 22 and a driving block 23. There are two driving rollers 21 in total. Both driving rollers 21 are movably installed on both sides inside the fuselage 1 through motors. The driving belt 22 is movably sleeved between the two driving rollers 21. There are two driving blocks 23 in total. The two driving blocks 23 are respectively fixedly installed on the driving belt 22 at positions corresponding to the two placing platforms 3. The two driving blocks 23 are respectively fixedly connected to the two placing platforms 3. By driving the driving roller 21 to rotate through the motor, the driving roller 21 can drive the driving belt 22 to rotate. By controlling the back-and-forth rotation of the motor, the driving belt 22 can be driven to move back and forth, so that the two placing platforms 3 can be driven by the driving block 23 to move alternately and reciprocally. At this time, the electrical components will also move back and forth, thereby improving the blowing effect on the electrical components; An installation groove 26 is opened inside the fuselage 1 at the position corresponding to the second blowing pipe 7. The installation groove 26 is a groove with a rectangular structure. An installation seat 27 is fixedly installed inside the installation groove 26. A movable seat 28 is movably installed inside the installation seat 27 through a torsion spring shaft. The second blowing pipe 7 is fixedly installed on the movable seat 28. A link mechanism is arranged on the fuselage 1; Two moving seats 24 are fixedly installed inside the fuselage 1. The moving seats 24 are of rectangular structure. Sliders 25 are movably installed inside both moving seats 24. The sliders 25 are blocks with a rectangular structure. Both sliders 25 are fixedly connected to the side walls of the placing platform 3; The linkage mechanism includes a movable groove 29, a pressing rod 30, a shifting rod 31, a reset rod 32, a first connecting rod 33 and a reset spring 34. The movable groove 29 is formed in the upper movable seat 24 and the fuselage 1. The pressing rod 30 is movably installed inside the movable groove 29 and is fixedly connected to the upper slider 25. The shifting rod 31 is an "L"-shaped rod and is fixedly installed at one end of the movable seat 28 away from the second blowing pipe 7. The movable groove 29 is a rectangular groove and is formed between the fuselage 1 and the movable seat 24. The pressing rod 30 is a long rectangular rod and is movably installed inside the movable groove 29 and is fixedly connected to the slider 25. The first connecting rod 33 is a hollow rectangular structure and is fixedly installed on the bottom wall surface of the shifting rod 31. The reset rod 32 is a rectangular rod and the bottom wall surface of the reset rod 32 has two inclined surfaces. The top of the first connecting rod 33 is located inside the reset rod 32. The reset spring 34 is movably installed inside the first connecting rod 33 and is movably connected to the reset rod 32. The reciprocating movement of the placing table 3 can be driven by the transmission belt 22, and the slider 25 will also move inside the movable seat 24. At this time, the slider 25 can drive the pressing rod 30 to move. When the pressing rod 30 moves to the bottom of the reset rod 32, the pressing rod 30 presses the reset rod 32. At this time, the pressing force of the pressing rod 30 on the reset rod 32 is less than the pressure of the reset rod 32 on the reset spring 34. Subsequently, the reset rod 32 can drive the shifting rod 31 to move to one side, and then drive the movable seat 28 and the second blowing pipe 7 to swing. At this time, the second blowing pipe 7 flips inside the fuselage 1, thereby improving the blowing range. When the movable seat 28 and the second blowing pipe 7 swing to the point where they cannot swing, at this time, the pressing force of the pressing rod 30 on the reset rod 32 is greater than the pressure of the reset rod 32 on the reset spring 34, and the reset spring 34 will be compressed. At this time, the reset rod 32 can move upward, and the pressing rod 30 and the reset rod 32 are separated. Subsequently, the pressing rod 30 is driven to move back to its original position, and the pressing rod 30 can press the reset rod 32 again. The reset rod 32 will drive the second blowing pipe 7 to swing inside the fuselage 1 again and blow air to other positions, thereby further improving the blowing effect on the electrical components.

[0026] A second connecting rod 35 is movably installed between the two shifting rods 31. The second connecting rod 35 is a long rectangular structure. Connecting shafts two 36 are fixedly installed at the tops of the two shifting rods 31. The second connecting rod 35 is movably sleeved between the two connecting shafts two 36. Thus, when the pressing rod 30 presses one of the reset rods 32 and causes the shifting rod 31 to move, the other shifting rod 31 will also be driven to move, and then the two second blowing pipes 7 can swing together inside the fuselage 1.

[0027] Below the interior of the fuselage 1, there is a dust collection tank 39. Inside the dust collection tank 39, a second partition net 40 is installed. Below the interior of the fuselage 1, a drying and filtering box 41 is installed. The drying and filtering box 41 is a hollow rectangular structure. An air return pipe 42 is installed on the drying and filtering box 41. The air return pipe 42 corresponds to the position of the second partition net 40. An air suction pipe 43 is installed on the input end of the air blowing pump 5. The air suction pipe 43 is communicated with the interior of the drying and filtering box 41. Through the setting of the drying and filtering box 41, when the air with a certain amount of dust moves downward and is guided by the dust collection tank 39, the air can be filtered inside the drying and filtering box 41, and then the air blowing pump 5 can send the filtered air into the interior of the fuselage 1 again through the first air blowing pipe 6 through the air suction pipe 43. A filter plate and a desiccant are arranged inside the drying and filtering box 41 to achieve dust removal and moisture-proof of the air.

[0028] There are two maintenance openings 37 on the side wall of the fuselage 1. A baffle 38 is movably installed inside the maintenance opening 37. By controlling the stroke of the motor driving the transmission belt 22, the placement table 3 can drive the electrical components to move away from the interior of the fuselage 1 through the maintenance opening 37 to the greatest extent, thus facilitating the maintenance of the electrical components.

[0029] A transmission gear ring 44 is fixedly installed at the bottom of the first partition net 4. The transmission gear ring 44 is a circular ring structure. A rotating shaft 45 is rotatably installed at the bottom of the placement table 3. A transmission gear 46 is fixed on the rotating shaft 45. The transmission gear 46 is in meshing transmission with the transmission gear ring 44. A transmission rack 47 is fixedly installed at the bottom of the moving seat 24 corresponding to the position of the transmission gear 46. The transmission gear 46 is in meshing transmission with the transmission rack 47. When the placement table 3 and the first partition net 4 move, the transmission gear 46 will move on the transmission rack 47, causing the transmission gear 46 to rotate. Since the transmission gear 46 is in meshing transmission with the transmission gear ring 44, the transmission gear 46 can drive the transmission gear ring 44 to rotate, thereby driving the first partition net 4 to rotate. At this time, while the electrical components move back and forth on the first partition net 4, they will also rotate, further increasing the air blowing range for the electrical components and improving the dust removal and moisture-proof effects.

[0030] A plurality of connecting pipes 48 are installed on the corrugated pipe 17. The connecting pipes 48 communicate with the inside of the corrugated pipe 17. A positioning shaft 49 is installed on the connecting pipe 48. The positioning shaft 49 is of a hollow cylindrical structure. The positioning shaft 49 is movably connected with the telescopic frame 11. Below the side wall of the connecting pipe 48 located above, a first nozzle 50 is installed. At the position corresponding to the connecting pipe 48 on the telescopic frame 11 located below, a second nozzle 51 is installed. The second nozzle 51 communicates with the inside of the connecting pipe 48 through the positioning shaft 49. When the placing table 3 moves to drive the body 1 to contract, the air inside the corrugated pipe 17 will be squeezed. At this time, the air can be ejected through the connecting pipe 48, the first nozzle 50 and the second nozzle 51 installed on the corrugated pipe 17. The first nozzle 50 ejects the air downward onto the electrical components on the lower partition net 4, and the second nozzle 51 ejects the air upward onto the electrical components on the upper partition net 4, so as to further blow air on the electrical components and enhance the dust removal and moisture-proof effects.

[0031] Specific implementation steps: Drive the driving roller 21 to rotate through the motor, so that the driving roller 21 can drive the driving belt 22 to rotate. By controlling the back-and-forth rotation of the motor, the driving belt 22 can be driven to move back and forth, so that the two placing tables 3 can be driven to move alternately and reciprocally through the transmission block 23; Meanwhile, an auxiliary air blowing mechanism is provided. When the placing table 3 moves inside the body 1, the movement of the upper placing table 3 will squeeze the telescopic frame 11. After being squeezed, the telescopic frame 11 will drive the telescopic rod 15 and the connecting plate 14 to move towards the pressing plate 13, and then the pressing plate 13 can be squeezed. The pressing plate 13 thus squeezes the airbag 12. At this time, the air inside the airbag 12 will be discharged into the inside of the corrugated pipe 17, then enter the inside of the inner cavity 19, and then be blown onto the electrical components on the partition net 4 through the second air blowing hole 20, thus achieving the effect of blowing air on the electrical components from multiple angles, reducing the blowing dead angle, and improving the dust removal and moisture-proof effects.

[0032] The above description enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be obvious to those skilled in the art. The general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to these embodiments shown herein, but will be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. An electrical automation component dust removal and moisture-proof treatment device, including a fuselage (1), and a machine door (2) is installed on the fuselage (1), characterized in that: Inside the fuselage (1), there are two placement platforms (3). A first partition net (4) is installed on the placement platform (3). A base (9) is installed below the fuselage (1). An air blowing pump (5) is installed on the base (9). A first air blowing pipe (6) is installed at the output end of the air blowing pump (5). A second air blowing pipe (7) is installed inside the fuselage (1). A first air blowing hole (8) is formed on the second air blowing pipe (7). A moving mechanism is arranged on the fuselage (1), and an auxiliary air blowing mechanism is also arranged inside the fuselage (1). The auxiliary air blowing mechanism includes: A mounting block (10) and a telescopic frame (11). The mounting block (10) is slidably installed on the placement platform (3) and the fuselage (1), and the telescopic frame (11) is installed on the mounting block (10). An airbag (12) and a pressing plate (13). The airbag (12) is installed on the inner wall of the fuselage (1) at the position corresponding to the upper telescopic frame (11), and the pressing plate (13) is fixedly installed on the outer side wall of the airbag (12). A connecting plate (14), a telescopic rod (15), and a first connecting shaft (16). The connecting plate (14) is arranged below the side wall of the pressing plate (13). The two ends of the telescopic rod (15) are respectively connected to the connecting plate (14) and the adjacent telescopic frame (11). The first connecting shaft (16) is movably installed on the telescopic frame (11). A corrugated pipe (17) and a check valve (18). The corrugated pipe (17) is arranged between the fuselage (1) and the placement platform (3), and the check valve (18) is installed on the corrugated pipe (17) at the position corresponding to the placement platform (3). An inner cavity (19) and a second air blowing hole (20). The inner cavity (19) is arranged inside the placement platform (3), and the second air blowing hole (20) is formed on the inner wall of the placement platform (3).

2. The dust removal and moisture-proof treatment device for an electrical automation component according to claim 1, wherein: The telescopic frame (11) is slidably installed between the placement platform (3) and the fuselage (1) through the mounting block (10). The airbag (12) is a telescopic structure with a spring inside. A one-way valve pipe communicating with the inside of the fuselage (1) is installed on the airbag (12), and a dust-proof net is arranged at the pipe orifice of the one-way valve pipe. One end of the telescopic rod (15) is movably sleeved on the first connecting shaft (16), and the telescopic rod (15) is movably connected to the telescopic frame (11) through the first connecting shaft (16). The other end of the corrugated pipe (17) is communicated with the inside of the airbag (12), and the second air blowing hole (20) is communicated with the inside of the inner cavity (19).

3. The dust removal and moisture-proof treatment device for an electrical automation component according to claim 2, wherein: The moving mechanism includes a driving roller (21), a driving belt (22), and a driving block (23). There are two driving rollers (21) in total, and both driving rollers (21) are movably installed on both sides inside the fuselage (1) through motors. The driving belt (22) is movably sleeved between the two driving rollers (21). There are two driving blocks (23) in total, and the two driving blocks (23) are respectively fixedly installed on the driving belt (22) at the positions corresponding to the two placement platforms (3), and the two driving blocks (23) are respectively fixedly connected to the two placement platforms (3).

4. An electrical automation component dust removal and moisture-proof treatment device according to claim 1, characterized in that: Two moving seats (24) are fixedly installed inside the fuselage (1). Sliders (25) are movably installed inside the two moving seats (24), and the two sliders (25) are respectively fixedly connected to the side walls of the placement platform (3).

5. The dust removal and moisture-proof treatment device for an electrical automation component according to claim 1, characterized in that: An installation groove (26) is formed inside the fuselage (1) corresponding to the position of the second blowing pipe (7). An installation seat (27) is fixedly installed inside the installation groove (26). A movable seat (28) is movably installed inside the installation seat (27) through a torsion spring shaft. The second blowing pipe (7) is fixedly installed on the movable seat (28). A link mechanism is arranged on the fuselage (1).

6. The dust removal and moisture-proof treatment device for an electrical automation component according to claim 5, characterized in that: The link mechanism includes a movable groove (29), a pressing rod (30), a dial rod (31), a reset rod (32), a first connecting rod (33) and a reset spring (34). The movable groove (29) is formed in the upper movable seat (24) and the fuselage (1). The pressing rod (30) is movably installed inside the movable groove (29). The pressing rod (30) is fixedly connected to the upper slider (25). The dial rod (31) is fixedly installed at one end of the movable seat (28) away from the second blowing pipe (7). The movable groove (29) is formed between the fuselage (1) and the movable seat (24). The pressing rod (30) is movably installed inside the movable groove (29) and is fixedly connected to the slider (25). The first connecting rod (33) is fixedly installed on the bottom wall surface of the dial rod (31). The reset rod (32) is a rod with a rectangular structure, and the bottom wall surface of the reset rod (32) is two inclined surfaces. The top of the first connecting rod (33) is located inside the reset rod (32). The reset spring (34) is movably installed inside the first connecting rod (33) and is movably connected to the reset rod (32).

7. An electrical automation component dust removal and moisture-proof treatment device according to claim 6, characterized in that: A second connecting rod (35) is movably installed between the two dial rods (31). Two connecting shafts II (36) are fixedly installed at the tops of the two dial rods (31). The second connecting rod (35) is movably sleeved between the two connecting shafts II (36). Two maintenance openings (37) are formed in the side wall of the fuselage (1). A baffle (38) is movably installed inside the maintenance opening (37).

8. An electrical automation component dust removal and moisture-proof treatment device according to claim 7, characterized in that: A dust collection groove (39) is arranged below the interior of the fuselage (1). A second partition net (40) is installed inside the dust collection groove (39). A drying and filtering box (41) is installed below the interior of the fuselage (1). A return air pipe (42) is installed on the drying and filtering box (41). The return air pipe (42) corresponds to the position of the second partition net (40). An air suction pipe (43) is installed on the input end of the air blowing pump (5). The air suction pipe (43) is communicated with the interior of the drying and filtering box (41).

9. An electrical automation component dust removal and moisture-proof treatment device according to any one of claims 1-8, characterized in that: A plurality of connecting pipes (48) are installed on the corrugated pipe (17). The connecting pipes (48) are communicated with the interior of the corrugated pipe (17). A positioning shaft (49) is installed on the connecting pipe (48). The positioning shaft (49) is movably connected to the telescopic frame (11). A first nozzle (50) is installed below the side wall of the upper connecting pipe (48). A second nozzle (51) is installed at the position corresponding to the connecting pipe (48) on the lower telescopic frame (11). The second nozzle (51) is communicated with the interior of the connecting pipe (48) through the positioning shaft (49).

10. A dust removal and moisture-proof treatment device for an electrical automation component according to any one of claims 1-8, characterized in that: A transmission gear ring (44) is fixedly installed at the bottom of the partition net one (4), a rotating shaft (45) is rotatably installed at the bottom of the placing table (3), a transmission gear (46) is fixed on the rotating shaft (45), the transmission gear (46) and the transmission gear ring (44) are meshed and transmitted, a transmission rack (47) is fixed at the position corresponding to the transmission gear (46) at the bottom of the moving seat (24), and the transmission gear (46) and the transmission rack (47) are meshed and transmitted.

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