Cable copper ring assembling equipment
Through the integrated cable copper ring assembly equipment of drive components, clamping components and fixing components, the problems of low production efficiency and high cost in the prior art are solved, and efficient insertion and fixation of copper rings are achieved.
Patent Information
- Application Number
- CN202422026463.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-20
- Publication Date
- 2025-07-01
- Estimated Expiration
- 2034-08-20
AI Technical Summary
During the existing cable processing process, two equipment is required to use for sleeve copper rings and fixed copper rings, resulting in low production efficiency and high cost.
Design a cable copper ring assembly equipment, integrating drive components, clamping components and fixing components, and implementing copper ring insertion and fixation through a single device, simplifying the production process.
Improve production efficiency, reduce processing costs, and efficient insertion and fixation of copper rings through integrated mechanical structure.
Smart Images

Figure CN223052553U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of cable automatic assembly, and particularly relates to a cable copper ring assembly device. Background Art
[0002] As a signal transmission medium, cables play an important role in the fields of electric power, communication, data transmission, etc. However, with the development of modern technology, the problem of electromagnetic wave interference has become increasingly prominent and has seriously affected the normal operation of equipment. In order to reduce the impact of electromagnetic waves on equipment, a copper ring is usually sleeved at the end of the cable, and the grounding function is realized by connecting the metal braid layer of the cable with the ground through the copper ring, so as to reduce electromagnetic interference. At the same time, the setting of the copper ring can enhance the shielding performance of the cable and reduce the impact of external electromagnetic interference on signal transmission.
[0003] In the existing cable processing procedure, it is necessary to first use a copper ring sleeving device to sleeve the copper ring onto the end of the cable, and then use a copper ring fixing device to press the copper ring onto the end of the cable. Two devices are required for processing during the processing, resulting in low production efficiency and high processing costs. Summary of the Utility Model
[0004] The main object of the utility model is to propose a cable copper ring assembly device, aiming to solve the problems of low production efficiency and high processing costs of the existing copper ring sleeving device and copper ring fixing device.
[0005] To achieve the above object, a cable copper ring assembly device proposed by the utility model includes: a fuselage, a driving component, a clamping component and a fixing component. The driving component is installed on the fuselage. The driving component at least includes a first driving member and a second driving member. The clamping component is movably installed on the fuselage. The clamping component is drivingly connected to the first driving member. The clamping component is used for clamping the copper ring. And the fixing component is movably installed on the fuselage. The fixing component is drivingly connected to the second driving member. The fixing component is used for fixing the copper ring.
[0006] The first driving member drives the clamping component to clamp the copper ring and sleave the copper ring onto the end of the cable along a first direction. The second driving member drives the fixing component to press the copper ring onto the cable.
[0007] In an embodiment of the utility model, the clamping component includes two clamping jaws and a support seat. There are two first driving members. The two clamping jaws are movably installed on the support seat. The support seat is slidably connected to the fuselage along the first direction. Both of the two clamping jaws are drivingly connected to one of the first driving members. The support seat is drivingly connected to the other first driving member.
[0008] One of the first driving members drives the two jaws to approach each other and clamp the copper ring, and the other first driving member drives the support base to slide along the first direction so as to sleave the copper ring onto the end of the cable.
[0009] In an embodiment of the present invention, clamping grooves are formed on one side of each of the two jaws facing each other, and the clamping grooves extend along the first direction. One of the first driving members drives the two jaws to approach each other so that the groove walls of the two clamping grooves press against the surface of the copper ring.
[0010] In an embodiment of the present invention, there are two second driving members, and the fixing assembly includes a fixing table and a stamping member. The fixing table and the stamping member are arranged at intervals perpendicular to the first direction;
[0011] One of the second driving members is drivingly connected to the fixing table and drives the fixing table to move towards the stamping member and abut against the copper ring so as to support the copper ring and the cable;
[0012] The other second driving member is drivingly connected to the stamping member and drives the stamping member to move towards the fixing table and press against the copper ring so as to press the copper ring tightly against the cable.
[0013] In an embodiment of the present invention, a support groove is recessed on the end face of the fixing table facing the stamping member. The cross-sectional shape of the support groove is semi-circular and is adapted to the copper ring.
[0014] In an embodiment of the present invention, the end of the stamping member facing the fixing table is conical.
[0015] In an embodiment of the present invention, the cable copper ring assembling device further includes a cable straightening assembly. The cable straightening assembly is installed on the fuselage and is located on the moving path of the clamping assembly along the first direction;
[0016] The driving member further includes a third driving member. The third driving member is drivingly connected to the cable straightening assembly and drives the cable straightening assembly to clamp the end of the cable so as to straighten the end of the cable.
[0017] In an embodiment of the present invention, the cable straightening assembly includes two clamping blocks. Guide grooves are formed on the surfaces of the two clamping blocks. The guide grooves extend along the first direction. The third driving member is drivingly connected to both of the clamping blocks and drives the two clamping blocks to approach each other so that the two guide grooves are aligned to clamp the end of the cable so as to straighten the end of the cable.
[0018] In an embodiment of the present utility model, the cable copper ring assembling device further includes a feeding mechanism, which is installed on the machine body and located on the moving path of the clamping assembly along the first direction. The feeding mechanism is provided with a feeding groove for placing the copper rings.
[0019] In an embodiment of the present utility model, the feeding mechanism includes a storage table and a lifting table. The storage table and the lifting table are arranged adjacent to each other along the first direction. Both the storage table and the lifting table are provided with feeding grooves. The feeding groove of the storage table is used for placing a plurality of copper rings;
[0020] The driving assembly further includes a fourth driving member. There are two fourth driving members. One fourth driving member drives the copper rings in the feeding groove of the storage table to move along the first direction into the feeding groove of the lifting table. The other fourth driving member is drivingly connected to the lifting table and drives the lifting table to move in a direction perpendicular to the first direction, so that the lifting table moves to the clamping height of the clamping assembly.
[0021] The technical solution of the present utility model provides a cable copper ring assembling device, which includes a machine body, a driving assembly, a clamping assembly and a fixing assembly. The driving assembly, the clamping assembly and the fixing assembly are all installed on the machine body to form an integrated and stable mechanical structure. The driving assembly at least includes a first driving member and a second driving member. The clamping assembly is drivingly connected to the first driving member, and the clamping assembly is used for clamping the copper rings. The fixing assembly is drivingly connected to the second driving member, and the fixing assembly is used for fixing the copper rings. The first driving member and the second driving member respectively drive the clamping assembly and the fixing assembly to sleave and fix the copper rings on the end of the cable. This cable copper ring assembling device integrates the clamping assembly and the fixing assembly together, realizes the coordination of production steps, simplifies the production process, improves the production efficiency, and also reduces the production cost. BRIEF DESCRIPTION OF THE DRAWINGS
[0022] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the following drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, other drawings can be obtained based on the structures shown in these drawings without creative efforts.
[0023] Figure 1 is a schematic structural diagram of the cable copper ring assembling device provided by the present utility model;
[0024] Figure 2 is Figure 1 the left view of
[0025] Figure 3 isFigure 2 Cross-sectional view along A-A;
[0026] Figure 4 is Figure 3 the enlarged partial view at B in;
[0027] Figure 5 the main internal view of the fuselage from another perspective of the cable copper ring assembly device provided by the present utility model;
[0028] Figure 6 is Figure 5 the enlarged partial view at C in.
[0029] Explanation of the reference numerals in the drawings:
[0030] 10, fuselage; 20, driving assembly; 21, first driving member; 22, second driving member; 30, clamping assembly; 31, clamping jaw; 311, clamping groove; 32, support base; 40, fixing assembly; 41, fixing table; 411, support groove; 42, stamping part; 50, cable straightening assembly; 51, clamping block; 511, guiding groove; 60, feeding mechanism; 61, material placing groove; 62, storage table; 63, lifting table.
[0031] The realization, functional features and advantages of the purpose of the present utility model will be further described with reference to the embodiments and the accompanying drawings. Specific embodiments
[0032] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described with reference to 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 of the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without making creative efforts shall fall within the protection scope of the present utility model.
[0033] It should be noted that if there are directional indications (such as up, down, left, right, front, back...) in the embodiments of the present utility model, the directional indications are only used to explain the relative position relationship and movement conditions between components in a specific posture. If the specific posture changes, the directional indications will also change accordingly.
[0034] In addition, if the descriptions such as "first", "second", etc. are involved in the embodiments of the present utility model, the descriptions of "first", "second", etc. are only for descriptive purposes and cannot be construed as indicating or implying their relative importance or implicitly specifying the quantity of the indicated technical features. Thus, the features defined with "first", "second" may explicitly or implicitly include at least one such feature. In addition, if "and / or" or "and / or" appears throughout the text, its meaning includes three parallel solutions. Taking "A and / or B" as an example, it includes solution A, or solution B, or the solution where A and B are satisfied simultaneously. In addition, the technical solutions between various embodiments can be combined with each other, but it must be based on the ability of those of ordinary skill in the art to implement. When the combination of technical solutions results in contradictions or cannot be implemented, it should be considered that such a combination of technical solutions does not exist and is not within the scope of protection required by the present utility model.
[0035] A cable copper ring assembly device proposed by the present utility model.
[0036] Combined Figure 1 and Figure 3 As shown, in an embodiment of the present utility model, the cable copper ring assembly device includes: a fuselage 10, a driving assembly 20, a clamping assembly 30, and a fixing assembly 40. The driving assembly 20 is installed on the fuselage 10. The driving assembly 20 at least includes a first driving member 21 and a second driving member 22. The clamping assembly 30 is movably installed on the fuselage 10. The clamping assembly 30 is drivingly connected to the first driving member 21. The clamping assembly 30 is used for clamping the copper ring. And the fixing assembly 40 is movably installed on the fuselage 10. The fixing assembly 40 is drivingly connected to the second driving member 22. The fixing assembly 40 is used for fixing the copper ring.
[0037] The first driving member 21 drives the clamping assembly 30 to clamp the copper ring and slews the copper ring onto the end of the cable along the first direction. The second driving member 22 drives the fixing assembly 40 to press the copper ring onto the cable.
[0038] In this embodiment, the fuselage 10 is made of materials such as steel castings and cast iron, and has high strength and hardness, providing support and connection for various components of the cable copper ring assembly device.
[0039] The first driving member 21 and the second driving member 22 can be driving structures such as cylinders, hydraulic presses, and motors.
[0040] The clamping assembly 30 can be a clamping pliers, a clamping block, or a jaw 31. For example, when using the jaw 31 for clamping, the clamping assembly 30 includes two oppositely arranged jaws 31, and the two jaws 31 are on the same horizontal line. The first driving member 21 is drivingly connected to the two jaws 31. The first driving member 21 drives the two jaws 31 to approach each other to clamp the copper ring, and drives the two jaws 31 to drive the copper ring to move in the first direction until the copper ring moves to a preset position to sleeve the copper ring onto the end of the cable. The first direction in this application is Figure 1 the positive direction of the y-axis in
[0041] In other embodiments of this application, the first driving member 21 can also drive the two jaws 31 to rotate along the axial direction of the jaws 31 to clamp the copper ring. As long as the effect of fixed clamping can be achieved, it is within the protection scope of this utility model.
[0042] The fixing assembly 40 includes a fixing table 41 and a stamping member 42. The fixing table 41 and the stamping member 42 are movably arranged on the fuselage 10. The end face of the fixing table 41 facing the stamping member 42 is a supporting surface. The second driving member 22 drives the fixing table 41 to move towards the cable, so that the supporting surface abuts against the copper ring to support the copper ring and the cable. The second driving member 22 drives the stamping member 42 to move towards the cable and abuts against the copper ring to press the copper ring tightly against the cable.
[0043] Compared with the existing solution of using two devices to separately complete sleeving the copper ring and fixing the copper ring, this application simplifies the production process to a certain extent, improves the production efficiency, and reduces the processing cost.
[0044] In this application, the cable copper ring assembly device includes two sets of clamping assemblies 30 and fixing assemblies 40. The two sets of clamping assemblies 30 and fixing assemblies 40 are arranged at intervals along the X-axis direction and are installed on the same fuselage 10. Each clamping assembly 30 and fixing assembly 40 cooperate to sleeve and fix the copper ring on the end of the cable. The two sets of clamping assemblies 30 and fixing assemblies 40 can be processed simultaneously, further improving the production efficiency and reducing the processing cost.
[0045] Combined with Figure 1 and Figure 2 As shown, in an embodiment of this utility model, the clamping assembly 30 includes two jaws 31 and a support seat 32. There are two first driving members 21. The two jaws 31 are movably installed on the support seat 32. The support seat 32 is slidably connected to the fuselage 10 in the first direction. Both of the two jaws 31 are drivingly connected to one first driving member 21, and the support seat 32 is drivingly connected to the other first driving member 21;
[0046] One first driving member 21 drives the two jaws 31 to approach each other and clamp the copper ring, and the other first driving member 21 drives the support seat 32 to slide in the first direction to sleeve the copper ring onto the end of the cable.
[0047] In this embodiment, one end of the jaw 31 close to the support base 32 is rotationally or swingably connected to the support base 32, and a first driving member 21 drives the two jaws 31 to move relative to the support base 32 in a direction perpendicular to the first direction and approach each other to clamp the copper ring.
[0048] One end of the support base 32 facing the fuselage 10 is provided with a slider, and the end face of the fuselage 10 facing the support base 32 is provided with a chute. The chute extends along the first direction, and the slider is embedded in the chute so that another first driving member 21 drives the support base 32 to slide along the first direction.
[0049] Combined Figure 1 and Figure 4 As shown in, in an embodiment of the present utility model, clamping grooves 311 are formed on the opposite sides of the two jaws 31. The clamping grooves 311 extend along the first direction. A first driving member 21 drives the two jaws 31 to approach each other so that the groove walls of the two clamping grooves 311 press against the surface of the copper ring.
[0050] In this embodiment, the two clamping grooves 311 are symmetrically arranged, and the longitudinal cross-section formed by their alignment is circular, and the shape of this longitudinal cross-section is adapted to the shape of the longitudinal cross-section of the copper ring, so that the groove walls of the clamping grooves 311 are in contact with the copper ring, so that the jaws 31 clamp the copper ring. By clamping the copper ring in the clamping groove 311, a surface contact is formed between the clamping groove 311 and the copper ring. Compared with the scheme where the jaw 31 forms a line contact with the copper ring, the scheme of the present application increases the acting area of the jaw 31 on the copper ring, makes the force on the contact surface between the jaw 31 and the copper ring uniform, and avoids breakage of the copper ring due to excessive local force.
[0051] Furthermore, the clamping groove 311 extends along the first direction, so that the clamping groove 311 has a certain length, thereby further increasing the contact area between the jaw 31 and the copper ring and improving the clamping stability.
[0052] Of course, the sizes of the two clamping grooves 311 of the two jaws 31 may also be different. As long as the shape or structure that realizes the surface contact between the jaw 31 and the copper ring belongs to the protection scope of the present utility model.
[0053] Combined Figure 1 and Figure 3 As shown in, in an embodiment of the present utility model, there are two second driving members 22. The fixing assembly 40 includes a fixing table 41 and a stamping member 42. The fixing table 41 and the stamping member 42 are arranged at intervals in a direction perpendicular to the first direction;
[0054] A second driving member 22 is drivingly connected to the fixing table 41 and drives the fixing table 41 to move towards the stamping member 42 and abut against the copper ring to support the copper ring and the cable;
[0055] Another second driving member 22 is drivingly connected to the stamping member 42, and drives the stamping member 42 to move towards the fixed table 41 and abut against the copper ring, so as to press the copper ring against the cable.
[0056] In this embodiment, when the two jaws 31 sleeved the copper ring to the preset position of the cable, the fixed table 41, the jaws 31 and the stamping member 42 are arranged at intervals in sequence along the positive direction of the Z axis and are on the same axis, so that when fixing the copper ring, the fixed table 41 and the stamping member 42 can be accurately aligned with the position of the copper ring.
[0057] Then, a first driving member 21 drives the two jaws 31 to move away from each other to loosen the copper ring, and another first driving member 21 drives the support base 32 to drive the two jaws 31 to move in a direction opposite to the first direction. The two second driving members 22 respectively drive the fixed table 41 and the stamping member 42 to approach each other and respectively abut against both sides of the cable.
[0058] In other embodiments of the present application, the fixing assembly 40 may also be two clamping blocks 51 that are rotatably connected. The two clamping blocks 51 are both arranged on the side of the cable away from the clamping assembly 30, and the two clamping blocks 51 are arranged at intervals relative to the cable. A punch is provided at the end of the clamping block 51 facing the cable, and the second driving member 22 drives the punches of the two clamping blocks 51 to approach each other towards the cable to press the copper ring against the cable.
[0059] Combined with Figure 1 、 Figure 3 and Figure 4 As shown, in an embodiment of the present utility model, a support groove 411 is recessed on the end face of the fixed table 41 facing the stamping member 42. The cross-sectional shape of the support groove 411 is semi-circular and is adapted to the copper ring.
[0060] In this embodiment, the groove wall of the support groove 411 abuts against the copper ring. Compared with the scheme in which the end face of the fixed table 41 is set as a plane to support the copper ring, the scheme of the present application increases the contact area between the fixed table 41 and the copper ring, thereby improving the stability of the support.
[0061] Combined with Figure 2 and Figure 3 As shown, in an embodiment of the present utility model, the end of the stamping member 42 facing the fixed table 41 is conical.
[0062] In this embodiment, the end of the stamping member 42 facing the fixed table 41 is a punch. Designing the shape of the punch as conical can reduce the acting area of the punch on the copper ring, thereby increasing the acting force of the punch on the copper ring, so that the copper ring can be pressed against the end of the cable.
[0063] The material of the punch can be made of high-strength alloy steel to ensure that its shape and performance are maintained during long-term use.
[0064] Combined withFigure 1 and Figure 4 As shown in Figure 4 , in an embodiment of the present utility model, the cable copper ring assembly device further includes a cable straightening assembly 50. The cable straightening assembly 50 is installed on the fuselage 10 and is located on the moving path of the clamping assembly 30 along the first direction;
[0065] The driving member further includes a third driving member. The third driving member is drivingly connected to the cable straightening assembly 50 and drives the cable straightening assembly 50 to clamp the end of the cable, so as to straighten the end of the cable.
[0066] In this embodiment, the end of the cable penetrates into the cable straightening assembly 50. The third driving member drives the cable straightening assembly 50 to clamp the end of the cable, so that the extending direction of the cable is aligned with the first direction. Thus, when the clamping assembly 30 moves, it can accurately position the end of the cable and clamp the copper ring to penetrate from the end of the cable.
[0067] Combined with Figure 1 、 Figures 4 to 6 As shown in Figures 4 to 6 , in an embodiment of the present utility model, the cable straightening assembly 50 includes two clamping blocks 51. Guide grooves 511 are formed on the surfaces of the two clamping blocks 51. The guide grooves 511 extend along the first direction. The third driving member is drivingly connected to both clamping blocks 51 and drives the two clamping blocks 51 to approach each other, so that the two guide grooves 511 are aligned to clamp the end of the cable, so as to straighten the end of the cable.
[0068] In this embodiment, the clamping block 51 is composed of a plurality of clamping teeth. The number and shape of the clamping teeth of the two opposite clamping blocks 51 are the same and are arranged in a staggered manner, and can be meshed with each other after being aligned. The clamping block 51 has a certain length in the direction extending towards the cable, so as to increase the contact area between the clamping teeth and the cable and improve the straightening efficiency.
[0069] The cable straightening assembly 50 further includes a transmission shaft. The transmission shaft is drivingly connected to the third driving member, and the clamping block 51 is rotatably connected to the transmission shaft. The third driving member drives the transmission shaft to drive the clamping block 51 to rotate. When the two clamping blocks 51 are meshed, the shape of the alignment of the two guide grooves 511 is cylindrical. The groove wall of the guide groove 511 abuts against the cable, and the extending direction of the guide groove 511 is the same as the extending direction of the cable, so as to improve the cable straightening effect.
[0070] Combined with Figure 1 、 Figure 4 and Figure 6 As shown in Figure 6 , in an embodiment of the present utility model, the cable copper ring assembly device further includes a feeding mechanism 60. The feeding mechanism 60 is installed on the fuselage 10 and is located on the moving path of the clamping assembly 30 along the first direction. The feeding mechanism 60 is provided with a material placing groove 61 for placing copper rings.
[0071] In this embodiment, by arranging the feeding mechanism 60 on the moving path of the clamping assembly 30, the procedure of the clamping assembly 30 for picking up materials is simplified, the speed of picking up materials is increased, and the stability of picking up materials is improved.
[0072] Combined with Figure 1 、 Figures 4 to 6 As shown in the figure, in an embodiment of the present utility model, the feeding mechanism 60 includes a storage table 62 and a lifting table 63. The storage table 62 and the lifting table 63 are arranged adjacent to each other along a first direction. Both the storage table 62 and the lifting table 63 are provided with a material discharging groove 61. The material discharging groove 61 of the storage table 62 is used for placing a plurality of copper rings.
[0073] The driving assembly 20 further includes a fourth driving member. There are two fourth driving members. One fourth driving member drives the copper ring in the material discharging groove 61 of the storage table 62 to move along the first direction into the material discharging groove 61 of the lifting table 63. The other fourth driving member is drivingly connected to the lifting table 63 and drives the lifting table 63 to move in a direction perpendicular to the first direction, so that the lifting table 63 moves to the clamping height of the clamping assembly 30.
[0074] In this embodiment, openings are provided on both sides of the groove wall of the material discharging groove 61 of the lifting table 63. The openings communicate with the material discharging groove 61 to avoid the clamping jaws 31, improving the convenience of the clamping jaws 31 for picking up materials.
[0075] The material discharging groove 61 of the storage table 62 extends in the reverse direction of the Y-axis with a certain length to place a plurality of copper rings. When the clamping assembly 30 picks up the copper ring in the material discharging groove 61 of the lifting table 63, one fourth driving member drives the storage table 62 to replenish the copper ring to the lifting table 63. Thus, the feeding and picking up of materials are continuously cyclic, ensuring that the lifting table 63 is in a full-material state, avoiding time waiting, and further improving the production efficiency.
[0076] The above are only exemplary embodiments of the present utility model, and do not limit the patent scope of the present utility model accordingly. Any equivalent structural transformation made under the technical concept of the present utility model by using the content of the specification and drawings of the present utility model, or directly / indirectly applied in other related technical fields, is included in the patent protection scope of the present utility model.
Claims
1. A cable copper ring assembly device, used to insert and fix the copper ring on the end of the cable, characterized in that: The cable copper ring assembly equipment comprises: body; A driving assembly, the driving assembly is mounted on the fuselage, and the driving assembly at least comprises a first driving member and a second driving member; A clamping assembly, wherein the clamping assembly is movably mounted on the fuselage, the clamping assembly is drivingly connected to the first driving member, and the clamping assembly is used to clamp the copper ring; and A fixing assembly, the fixing assembly is movably mounted on the fuselage, the fixing assembly is drivingly connected to the second driving member, and the fixing assembly is used to fix the copper ring; The first driving member drives the clamping assembly to clamp the copper ring and insert the copper ring into the end of the cable along the first direction, and the second driving member drives the fixing assembly to crimp the copper ring onto the cable.
2. The cable copper ring assembly device according to claim 1, characterized in that: The clamping assembly comprises two clamping jaws and a support seat, the first driving member is provided with two, the two clamping jaws are movably mounted on the support seat, the support seat is slidably connected with the body along the first direction, the two clamping jaws are both drivingly connected with one of the first driving members, and the support seat is drivingly connected with another of the first driving members; One of the first driving members drives the two clamping jaws to approach each other and clamp the copper ring, and another of the first driving members drives the supporting seat to slide along the first direction to insert the copper ring into the end of the cable.
3. The cable copper ring assembly device according to claim 2, characterized in that: A clamping groove is formed on one side opposite to the two clamping jaws, and the clamping groove is extended along the first direction. The first driving member drives the two clamping jaws to approach each other so that the groove walls of the two clamping grooves are pressed against the surface of the copper ring.
4. The cable copper ring assembly device according to claim 3, characterized in that: The second driving members are provided with two, the fixing assembly comprises a fixing platform and a stamping member, and the fixing platform and the stamping member are spaced apart and arranged perpendicular to the first direction; The second driving member is drivingly connected to the fixing platform, and drives the fixing platform to move toward the stamping part and abut against the copper ring to support the copper ring and the cable; Another of the second driving members is drivingly connected to the stamping member, and drives the stamping member to move toward the fixing platform and press against the copper ring to press the copper ring tightly against the cable.
5. The cable copper ring assembly device according to claim 4, characterized in that: The end surface of the fixing platform facing the stamping part is concavely provided with a supporting groove, the cross-section of the supporting groove is semicircular and is matched with the copper ring.
6. The cable copper ring assembly device according to claim 5, characterized in that: The end of the stamping part facing the fixing platform is conical.
7. The cable copper ring assembly device according to any one of claims 1 to 6, characterized in that: The cable copper ring assembly device further comprises a cable straightening assembly, which is mounted on the body and located on a moving path of the clamping assembly along the first direction; The driving member further includes a third driving member, which is drivingly connected to the cable straightening assembly and drives the cable straightening assembly to clamp the cable end to straighten the cable end.
8. The cable copper ring assembly device according to claim 7, characterized in that: The cable straightening assembly includes two clamping blocks, and guide grooves are provided on the surfaces of the two clamping blocks. The guide grooves are extended along the first direction. The third driving member is drivingly connected to the two clamping blocks and drives the two clamping blocks to approach each other so that the two guide grooves are aligned to clamp the cable ends to straighten the cable ends.
9. The cable copper ring assembly device according to any one of claims 1 to 6, characterized in that: The cable copper ring assembly equipment also includes a feeding mechanism, which is installed on the body and located on the moving path of the clamping assembly along the first direction. The feeding mechanism is provided with a feeding trough for placing the copper ring.
10. The cable copper ring assembly device according to claim 9, characterized in that: The feeding mechanism comprises a material storage platform and a lifting platform, wherein the material storage platform and the lifting platform are arranged adjacent to each other along the first direction, and both the material storage platform and the lifting platform are provided with a material discharge trough, and the material discharge trough of the material storage platform is used to place a plurality of copper rings; The driving assembly also includes a fourth driving member, and two fourth driving members are provided. One of the fourth driving members drives the copper ring in the discharge trough of the storage table to move along the first direction to the discharge trough of the lifting platform, and the other fourth driving member is connected to the lifting platform and drives the lifting platform to move in a direction perpendicular to the first direction, so that the lifting platform moves to the clamping height of the clamping assembly.