Electric control structure of winding turret

Abstract

The utility model discloses an electrical control structure of a winding turret. The electrical control structure comprises a winding mechanism and a turret main body arranged in the winding mechanism, a winding needle mechanism is arranged on the outer side of the winding mechanism, a supporting mechanism is arranged at the end, away from the winding mechanism, of the winding needle mechanism, a driven mechanism is arranged at the end, away from the winding needle mechanism, of the winding mechanism, and a motor driver is arranged on the outer side of the driven mechanism. According to the electric control structure of the winding turret, the turret body is arranged in the winding mechanism, controllers of a plurality of motors on the winding turret are installed together, a circuit of an electric slip ring can be reduced by two thirds, wiring is few, the reliability of a series system is met, the failure rate is reduced, installation is easy, and the working time is shortened to at least one fourth of the original working time; through the design of the electrical mechanism, the complexity of the electrical mechanism can be reduced, the working smoothness of the mechanism can be improved, the related abnormal frequency can be greatly reduced, and the equipment reliability can be greatly improved.

Description

Technical Field

[0001] This utility model relates to the field of mango planting technology, specifically to a winding turret electrical control structure. Background Technology

[0002] During the winding process of the lithium battery separator, the winding turret is used to drive the winding needle mechanism to rotate and wind the separator. In this process, the turret needs to be powered by an electric slip ring.

[0003] The turret is located on the outside of the winding structure. During operation, it needs to be powered by electric slip rings and wires. This setup requires a lot of wires for power supply. The power supply structure is located on the outside of the electric slip ring. During the normal operation and wear of the electric slip ring, it needs to be removed along with the power supply structure. After the electric slip ring is replaced, it needs to be reassembled.

[0004] In the current use of electric slip rings, due to the large number of electrical lines involved and the need to complete rotational operations, the internal reliability of the existing electrical structure is low and the failure rate is high. Furthermore, when signals and electrical energy are shared, mutual interference cannot be completely avoided. Moreover, when electric slip rings wear out and need to be replaced or maintained, a long time is required for maintenance and disassembly, which seriously affects the normal operating efficiency of the electrical structure.

[0005] To address the aforementioned issues, there is an urgent need for innovative design based on the existing irrigation device structure. Utility Model Content

[0006] The purpose of this utility model is to provide an electrical control structure for a winding turret, in order to solve the problems mentioned in the background art, such as low internal reliability and high failure rate of the existing electrical structure due to the large number of electrical lines and the need to complete the rotation operation during the use of the electric slip ring, the inability to completely avoid mutual interference when the signal and power are shared, and the long time required for maintenance and disassembly when the electric slip ring is worn and needs to be replaced or maintained, which seriously affects the normal use efficiency of the electrical structure.

[0007] To achieve the above objectives, this utility model provides the following technical solution: an electrical control structure for a winding turret, comprising a winding mechanism and a turret body disposed inside the winding mechanism;

[0008] A needle winding mechanism is provided on the outer side of the winding mechanism, and a support mechanism is provided at the end of the needle winding mechanism away from the winding mechanism. A driven mechanism is provided at the end of the winding mechanism away from the needle winding mechanism, and a motor driver is fixedly installed on the outer side of the driven mechanism. A connecting mechanism is provided at the end of the driven mechanism away from the winding mechanism, and an electric slip ring is provided on the outer side of the connecting mechanism.

[0009] Preferably, the end of the electric slip ring away from the connecting mechanism is provided with a support plate mechanism, and the lower end of the support plate mechanism is provided with a mounting plate, and the end of the mounting plate away from the support plate mechanism is provided with an aviation plug.

[0010] Preferably, the upper end of the support plate mechanism is provided with a support seat, and the support seat is located at the upper end of the mounting plate. A central shaft is rotatably installed inside the support seat. The central shaft passes through the electric slip ring, and the end of the electric slip ring's central shaft away from the support seat is connected to the connecting mechanism.

[0011] Preferably, a limiting block is fixedly installed at the lower end of the support plate mechanism, and the limiting block is engaged with the mounting plate. Furthermore, three sets of limiting blocks are equidistantly arranged at the lower end of the support plate mechanism.

[0012] Preferably, the upper end of the mounting plate is provided with a motion groove, and a sliding block is slidably installed inside the motion groove. A support spring is provided inside the motion groove, and the support spring is located at the upper end of the sliding block.

[0013] Preferably, a snap-fit ​​block is fixedly installed on the outer side of the sliding block, and the snap-fit ​​block is engaged with the limiting block, and a lifting plate is fixedly installed on the upper end of the snap-fit ​​block.

[0014] Preferably, the sliding block, the support spring, and the snap-fit ​​block are arranged in three sets inside the mounting plate, and the mounting plate is in close contact with the support plate mechanism, and the upper end of the support plate mechanism has an inwardly concave arc shape.

[0015] Compared with the prior art, the beneficial effects of this utility model are: by installing the motor driver on the outside of the turret body, the motor driver can control the rotation of the motor, reduce the number of wires used inside the structure, reduce the probability of the structure failing, and provide an easily disassembled slip ring and its docking structure, which reduces the maintenance cost of the structure, improves the ease of use of the structure, and thus improves the production efficiency of the structure.

[0016] 1. By setting the turret body inside the winding mechanism and installing the controllers of multiple motors on the winding turret inside the motor driver, the circuit of the electric slip ring can be reduced by two-thirds, with fewer wires, meeting the reliability requirements of the series system, reducing the failure rate, simplifying installation, and shortening the working time to at least one-quarter of the original.

[0017] 2. Furthermore, the design of this electrical mechanism can reduce its complexity, improve its smooth operation, greatly reduce the number of related anomalies, and significantly improve equipment reliability;

[0018] 3. Furthermore, by changing the settings of the electric slip ring, the original built-in slip ring can be prevented from being easily corroded by electric arc, and the occurrence of abnormalities such as arcing and open circuit can be reduced. This setting method can extend the service life of the electric slip ring and provide conditions for the rapid replacement of the electric slip ring.

[0019] 4. Furthermore, the quick assembly and disassembly of the support plate mechanism and the mounting plate enable rapid maintenance and replacement of aviation plugs, while also facilitating the maintenance and replacement of the slip rings, effectively improving the ease of use of this electrical mechanism. Attached Figure Description

[0020] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0021] Figure 2 This is a three-dimensional structural diagram of the turret body of this utility model;

[0022] Figure 3 This is a top view of the structure of this utility model;

[0023] Figure 4 This is a three-dimensional structural diagram of the electric slip ring of this utility model;

[0024] Figure 5 This is a schematic diagram of the right-side structure of this utility model;

[0025] Figure 6 This is a three-dimensional structural diagram of the support plate mechanism of this utility model;

[0026] Figure 7 This is a schematic diagram of the three-dimensional structure of the snap-fit ​​block of this utility model.

[0027] In the diagram: 1. Winding mechanism; 2. Turret body; 3. Needle winding mechanism; 4. Support mechanism; 5. Driven mechanism; 6. Connecting mechanism; 7. Motor driver; 8. Electric slip ring; 9. Central shaft; 10. Support base; 11. Support plate mechanism; 12. Mounting plate; 13. Aviation plug; 14. Limit block; 15. Motion groove; 16. Sliding block; 17. Support spring; 18. Snap-fit ​​block; 19. Lifting plate. Detailed Implementation

[0028] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0029] In a specific embodiment, such as Figures 1-3 The basic operation process of the winding turret is disclosed as shown; the winding mechanism 1 and the turret body 2 set inside the winding mechanism 1; a winding needle mechanism 3 is set on the outside of the winding mechanism 1, and a support mechanism 4 is set on the end of the winding needle mechanism 3 away from the winding mechanism 1; a driven mechanism 5 is set on the end of the winding mechanism 1 away from the winding needle mechanism 3; a motor driver 7 is fixedly installed on the outside of the driven mechanism 5; a connecting mechanism 6 is set on the end of the driven mechanism 5 away from the winding mechanism 1; and an electric slip ring 8 is set on the outside of the connecting mechanism 6.

[0030] When using the electrical control structure of this winding turret, the electrical mechanism needs to be installed in the working position first. After the electrical mechanism is installed, it can be put into operation and wind the lithium battery separator. During the operation of the electrical mechanism, the turret body 2 drives the winding needle mechanism 3 to rotate. The rotation of the turret body 2 requires power supply through the electric slip ring 8 and the rotation of the turret body 2 needs to be controlled by the motor driver 7 to complete the basic work of the electrical mechanism. By setting the turret body 2 inside the winding mechanism 1, the internal wiring of the electrical mechanism can be greatly reduced, and the probability of failure inside the electrical mechanism can be reduced.

[0031] In one specific embodiment, such as Figures 1-4 and Figures 6-7 As shown, the quick assembly and disassembly process of the support plate mechanism 11 and the mounting plate 12 is disclosed.

[0032] A limiting block 14 is fixedly installed at the lower end of the support plate mechanism 11, and the limiting block 14 is engaged with the mounting plate 12. Three sets of limiting blocks 14 are equidistantly arranged at the lower end of the support plate mechanism 11. A motion groove 15 is opened at the upper end of the mounting plate 12, and a sliding block 16 is slidably installed inside the motion groove 15. A support spring 17 is installed inside the motion groove 15, and the support spring 17 is located at the upper end of the sliding block 16. A snap-fit ​​block 18 is fixedly installed on the outer side of the sliding block 16, and the snap-fit ​​block 18 is engaged with the limiting block 14. A lifting plate 19 is fixedly installed at the upper end of the snap-fit ​​block 18. Three sets of sliding block 16, support spring 17 and snap-fit ​​block 18 are arranged inside the mounting plate 12. The mounting plate 12 is in close contact with the support plate mechanism 11, and the upper end of the support plate mechanism 11 has an inwardly concave arc shape.

[0033] When using this winding turret electrical control structure, it is necessary to install the support plate mechanism 11 and the mounting plate 12 and limit the aviation plug 13. During the process of installing the mounting plate 12 on the outside of the support plate mechanism 11, the mounting plate 12 needs to be engaged with the limiting block 14. Before the mounting plate 12 is engaged with the limiting block 14, the lifting plate 19 needs to be pushed upward. The upward movement of the lifting plate 19 will cause the sliding block 16 to move upward through the locking block 18. The upward movement of the sliding block 16 will compress the support spring 17 and cause the support spring 17 to... When the plate is retracted, the mounting plate 12 can engage with the limiting block 14. After engagement, the lifting plate 19 is released, and the retracted support spring 17 expands and pushes the sliding block 16 downward. At this time, the locking block 18 moves downward and engages with the limiting block 14, thereby installing the mounting plate 12 on the outside of the support plate mechanism 11. Similarly, by reversing the above process, the mounting plate 12 and the support plate mechanism 11 can be disassembled, thus completing the disassembly and assembly process of the support plate mechanism 11 and the mounting plate 12, effectively improving the convenience of disassembly and assembly of the aviation plug 13.

[0034] Based on the above embodiments, such as Figures 1-5 As shown, it has been made public;

[0035] A support plate mechanism 11 is provided at the end of the electric slip ring 8 away from the connecting mechanism 6, and a mounting plate 12 is provided at the lower end of the support plate mechanism 11. An aviation plug 13 is provided at the end of the mounting plate 12 away from the support plate mechanism 11. A support seat 10 is provided at the upper end of the support plate mechanism 11, and the support seat 10 is located at the upper end of the mounting plate 12. A central shaft 9 is rotatably mounted inside the support seat 10. The central shaft 9 passes through the electric slip ring 8, and the end of the central shaft 9 of the electric slip ring 8 away from the support seat 10 is connected to the connecting mechanism 6.

[0036] When using this winding turret electrical control structure, the circuit of the slip ring 8 is reduced from approximately 135 lines to approximately 45 lines. Calculating the reliability of this circuit as a series system, assuming the original reliability of each channel was 99.9%, the total reliability was approximately 87.3%. After adopting this scheme, the total reliability is approximately 95.5%. This represents a significant improvement. Through normal equipment operation, it effectively reduces the number of related anomalies, greatly improving equipment reliability. Simultaneously, it lowers the electricity and wiring costs of the electrical mechanism, reduces the complexity of normal maintenance, and increases overall practicality.

[0037] The contents not described in detail in this specification are existing technologies known to those skilled in the art.

[0038] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A winding turret electrical control structure, comprising a winding mechanism (1) and a turret body (2) arranged inside the winding mechanism (1); characterized in that The outer side of the winding mechanism (1) is provided with a winding needle mechanism (3), and the winding needle mechanism (3) is provided with a supporting mechanism (4) away from the winding mechanism (1). The winding mechanism (1) is provided with a driven mechanism (5) away from the winding needle mechanism (3), and the driven mechanism (5) is fixedly installed with a motor driver (7) on the outer side, and the driven mechanism (5) is provided with a connecting mechanism (6) away from the winding mechanism (1), and the outer side of the connecting mechanism (6) is provided with an electric slip ring (8).

2. A winding turret electrical control structure according to claim 1, characterised in that: The outer side of the electric slip ring (8) is provided with a supporting plate mechanism (11) away from the connecting mechanism (6), and the lower end of the supporting plate mechanism (11) is provided with a mounting plate (12), and the mounting plate (12) is provided with an aviation plug (13) away from the supporting plate mechanism (11).

3. A winding turret electrical control structure according to claim 2, characterised in that: The upper end of the supporting plate mechanism (11) is provided with a supporting seat (10), and the supporting seat (10) is located at the upper end of the mounting plate (12), and the center shaft (9) is rotatably installed in the supporting seat (10). The center shaft (9) penetrates the electric slip ring (8), and the center shaft (9) away from the supporting seat (10) is connected with the connecting mechanism (6).

4. A winding turret electrical control structure according to claim 3, characterised in that: The lower end of the supporting plate mechanism (11) is fixedly installed with a limiting block (14), and the limiting block (14) is connected with the mounting plate (12) in a clamping manner, and the limiting block (14) is provided with three groups equidistantly arranged at the lower end of the supporting plate mechanism (11).

5. A winding turret electrical control structure according to claim 4, characterised in that: The upper end of the mounting plate (12) is provided with a movement groove (15), and the movement groove (15) is provided with a sliding block (16) slidably installed in the movement groove (15), and the movement groove (15) is provided with a supporting spring (17), and the supporting spring (17) is located at the upper end of the sliding block (16).

6. A winding turret electrical control structure according to claim 5, characterised in that: The outer side of the sliding block (16) is fixedly installed with a clamping block (18), and the clamping block (18) is connected with the limiting block (14) in a clamping manner, and the upper end of the clamping block (18) is fixedly installed with a lifting plate (19).

7. A winding turret electrical control structure according to claim 6, characterised in that: The sliding block (16), the supporting spring (17) and the clamping block (18) are provided with three groups in the mounting plate (12), and the mounting plate (12) is in close contact with the supporting plate mechanism (11), and the upper end of the supporting plate mechanism (11) is in a concave arc shape structure.

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