Automatic processing equipment for brim fixing iron ring

By designing the automatic processing equipment of the iron rim fixed iron rings, the automatic circle, cutting, and welding of the iron rings are used to achieve the use of wires, cut welding, circle wire and raw institutions, and solve the problem of low traditional production process and poor quality. , Improve production efficiency and product quality.

CN222386336UActive Publication Date: 2025-01-24CIXI HANGZHOU BAY SECONDARY VOCATIONAL SCHOOL (CIXI TECH SCHOOL)
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Patent Information

Application Number
CN202420220620.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-01-30
Publication Date
2025-01-24
Estimated Expiration
2034-01-30

AI Technical Summary

Technical Problem

The production process of traditional cap brim fixed iron rings is low in efficiency, poor in quality, high in cost, and high labor intensity, and lacks automation equipment to improve production efficiency and product quality.

Method used

Design an automatic processing equipment for iron rings fixed on the brim, including a wire feeding mechanism, a cutting and spot welding mechanism, a wire looping mechanism and a discharging mechanism on the fuselage. Through these mechanisms, automatic looping, cutting and welding of the iron hoops can be realized.

Benefits of technology

Improve the production efficiency and product quality of the fixed iron rim of the hats, reduce production costs and labor intensity, and achieve automated production of iron rings.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses automatic processing equipment for a brim fixing iron ring, which comprises a machine body and is reasonable in structural design. The machine body is provided with a wire feeding mechanism located on the side face of the machine body, a material cutting and spot welding mechanism located above the machine body, a wire coiling mechanism located below the material cutting and spot welding mechanism and a discharging mechanism located on the side edge of the material cutting and spot welding mechanism. An iron ring is sequentially conveyed to the wire coiling mechanism through the wire feeding mechanism to be coiled and formed, is cut off and welded through the material cutting and spot welding mechanism and is discharged through the discharging structure. An iron ring is conveyed to the wire coiling mechanism through the wire feeding mechanism, the iron ring is coiled and formed through the wire coiling mechanism, the iron ring is welded and formed after being cut off through the material cutting and spot welding mechanism, and the formed iron ring is pushed out through the discharging structure. According to the automatic processing equipment for the brim fixing iron ring, the production efficiency and the product quality of the brim fixing iron ring are improved, and the production cost and the labor intensity are reduced.
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Description

Technical Field

[0001] The utility model relates to the field of metal processing equipment, in particular to automatic processing equipment for fixing a hat brim iron ring. Background Art

[0002] The brim is an important part of a hat, which can protect the head from sunlight, rain and dust. The brim is usually made of plastic, cloth or other materials. In order to increase the strength and stability of the brim, a circle of iron ring is usually fixed on the edge of the brim. The function of the iron ring is to provide a support frame so that the brim is not easily deformed or damaged. The traditional production process of the brim fixing iron ring is to first bend the iron wire into a circle, and then weld the two ends of the iron wire together to form a complete iron ring. This production process has problems such as low efficiency, poor quality, high cost, and high labor intensity. In order to improve the production efficiency and product quality of the brim fixing iron ring, and reduce production costs and labor intensity, an integrated equipment that can automatically complete the three processes of circling, cutting and welding is needed. Utility Model Content

[0003] The technical problem to be solved by the utility model is to provide an automatic processing device for fixing a hat brim iron ring in view of the current status of the prior art.

[0004] The technical solution adopted by the utility model to solve the above technical problems is:

[0005] An automatic processing equipment for fixing an iron ring for a brim of a hat comprises a fuselage, and is characterized in that: a wire feeding mechanism located on the side of the fuselage, a cutting and spot welding mechanism located above the fuselage, a wire coiling mechanism located below the cutting and spot welding mechanism, and a discharging mechanism located on the side of the cutting and spot welding mechanism are respectively arranged on the fuselage; the iron ring is sequentially transported to the wire coiling mechanism through the wire feeding mechanism to be coiled and formed, cut and welded through the cutting and spot welding mechanism, and discharged through the discharging structure; the iron ring is transported to the wire coiling mechanism through the wire feeding mechanism, the wire coiling mechanism coils the iron ring into shape, cuts and welds through the cutting and spot welding mechanism, and is discharged through the discharging structure. The iron ring is transported to the wire coiling mechanism through the wire feeding mechanism, the wire coiling mechanism coils the iron ring into shape, is cut and welded through the cutting and spot welding mechanism, and is pushed out through the discharging structure.

[0006] Preferably, the cutting spot welding mechanism comprises:

[0007] The cutting and spot welding cylinder assembly comprises a first cylinder arranged above the cutting and spot welding mechanism and a second cylinder arranged at the side of the cutting and spot welding mechanism;

[0008] The clamp cylinder assembly includes a third cylinder and a fourth cylinder arranged on both sides of the first cylinder, a third pressing block bracket connected to the third cylinder is provided below the third cylinder, and a fourth pressing block bracket connected to the fourth cylinder is provided below the fourth cylinder;

[0009] A base is arranged below the cutting and spot welding mechanism, a guide copper seat is arranged above the base, a guide base is arranged on the side of the base, and the guide base is connected with the third pressing block bracket in cooperation;

[0010] A spot welding assembly is arranged below the first cylinder, comprising a spot welding bracket connected to each other below the first cylinder and a spot welding copper rod above the guide copper seat, wherein the spot welding copper rod is connected to the spot welding bracket;

[0011] The cutter is arranged inside the spot welding assembly and connected with the first cylinder.

[0012] Preferably, the wire loop mechanism comprises:

[0013] A push cylinder assembly is arranged outside the wire coiling mechanism, comprising a first push cylinder arranged on the left side of the wire coiling mechanism, a second push cylinder arranged on the right side of the wire coiling mechanism, a third push cylinder arranged below the wire coiling mechanism, and a fourth push cylinder and a fifth push cylinder arranged above the first push cylinder and the second push cylinder;

[0014] An arc-shaped push plate assembly is arranged on the push cylinder assembly, and the arc-shaped push plate assembly is connected to the push cylinder assembly;

[0015] The guide plate assembly is arranged in the middle of the wire loop mechanism, and comprises a first guide plate arranged on the left side of the guide plate, a second guide plate arranged on the right side of the guide plate, and a lower guide plate arranged below the guide plate.

[0016] Preferably, the discharging mechanism comprises a discharging cylinder arranged on the discharging mechanism and a discharging claw arranged on the discharging cylinder, and the discharging claw is connected to the discharging cylinder.

[0017] Preferably, the wire feeding mechanism includes a driving motor, a feeding roller group and a correction round tube arranged on the right side of the spot welding structure, and the correction round tube is fixedly connected by a fixing frame.

[0018] Preferably, the wire feeding mechanism, the material cutting spot welding mechanism, the wire coiling mechanism and the wire coiling mechanism are all arranged on a fixed plate above the fuselage and fixedly connected.

[0019] Preferably, a button box is provided on the side of the fuselage.

[0020] Compared with the prior art, the utility model has the advantages that when the automatic processing equipment is started, the iron ring is transmitted to the wire coiling mechanism through the driving motor of the wire feeding mechanism to control the feeding roller group, the wire coiling mechanism drives the arc push plate through the push cylinder to cooperate with the guide plate assembly arranged in the middle to form a circular contour, and the iron ring is circled in the circular contour. At this time, the cutting spot welding mechanism drives the fourth pressure block bracket to fix the iron ring through the fourth cylinder, the first cylinder drives the cutter to press down and cut the iron ring, the third cylinder drives the third pressure block bracket to fix the cut iron ring, the second cylinder drives the guide base to move the iron ring fixed by the third pressure block bracket to the guide copper seat, the first cylinder drives the spot welding bracket and the connected spot welding copper rod to move downward, the spot welding copper rod generates a strong current to weld the iron ring into shape, and the discharging mechanism drives the discharging claw to push out the formed iron ring through the discharging cylinder. Improve the production efficiency and product quality of the brim iron ring, and reduce production costs and labor intensity. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a structural schematic diagram of the utility model;

[0022] Figure 2 It is a schematic diagram of the overall structure on the fixed plate of the utility model;

[0023] Figure 3 It is an exploded schematic diagram of the cutting spot welding mechanism of the utility model;

[0024] Figure 4 It is a schematic diagram of the exploded structure of the wire coiling mechanism of the utility model.

[0025] Figure numerals: 1, fuselage; 2, cutting spot welding mechanism; 3, wire coiling mechanism; 4, wire feeding mechanism; 5, discharging mechanism; 6, fixed plate; 7, discharging cylinder; 8, discharging claw; 9, driving motor; 10, feeding roller group; 11, correction round tube; 12, fixing frame; 13, first cylinder; 14, second cylinder; 15, third cylinder; 16, fourth cylinder; 17, base; 18, guide base; 19, guide copper seat; 20, third pressure block bracket; 21, fourth pressure block bracket; 22, spot welding bracket; 23, spot welding copper rod; 24, cutter; 25, first push cylinder; 26, second push cylinder; 27, third push cylinder; 28, fourth push cylinder; 29, fifth push cylinder; 30, first arc push plate; 31, second arc push plate; 32, third arc push plate; 33, fourth arc push plate; 34, fifth arc push plate; 35, first guide plate; 36, second guide plate; 37, lower guide plate; 38, button box; 39, arc push plate assembly; 40, push cylinder assembly; 41, guide plate assembly; 42, connecting parts. DETAILED DESCRIPTION

[0026] The following will disclose multiple embodiments of the present invention with drawings. For the purpose of clear description, many practical details will be described together in the following description. However, it should be understood that these practical details should not be used to limit the present invention. In other words, in some embodiments of the present invention, these practical details are not necessary. In addition, in order to simplify the drawings, some conventional structures and components will be depicted in a simple schematic manner in the drawings.

[0027] It should be noted that all directional indications in the embodiments of the present invention, such as up, down, left, right, front, back... are only used to explain the relative position relationship, movement status, etc. between the components under a certain specific posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication will also change accordingly.

[0028] Moreover, some of the above-mentioned terms may be used to express other meanings besides indicating orientation or positional relationships. For example, the term "on" may also be used to indicate a certain dependency or connection relationship in certain circumstances. A person skilled in the art may understand the specific meanings of these terms in the present utility model according to the specific circumstances.

[0029] In addition, the terms "install", "set", "provided with", "connect", "connected", and "socketed" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral structure; it can be a mechanical connection, or an electrical connection; it can be a direct connection, or an indirect connection through an intermediate medium, or it can be an internal connection between two devices, elements, or components. The connection methods involved in this article are prior arts, without any improvement, and are all common knowledge of those skilled in the art. For those skilled in the art, the specific meanings of the above terms in this utility model can be understood according to specific circumstances.

[0030] In addition, in the present utility model, the descriptions of "first", "second", etc. are only used for descriptive purposes, and do not specifically refer to the order or sequence, nor are they used to limit the present utility model. They are only used to distinguish components or operations described with the same technical terms, and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the technical solutions between the various embodiments can be combined with each other, but they must be based on the ability of ordinary technicians in this field to implement them. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by the present utility model.

[0031] like Figures 1 to 4As shown, the utility model provides an automatic processing equipment for fixing an iron ring of a hat brim, comprising a fuselage 1, characterized in that: the fuselage 1 is respectively provided with a wire feeding mechanism 4 located on the side of the fuselage 1, a cutting and spot welding mechanism 2 located above the fuselage 1, a wire coiling mechanism 3 located below the cutting and spot welding mechanism 2, and a discharging mechanism 5 located on the side of the cutting and spot welding mechanism 2; the iron ring is sequentially transported to the wire coiling mechanism 3 through the wire feeding mechanism 4 to be coiled and formed, cut and welded through the cutting and spot welding mechanism 2, and discharged through the discharging structure, the iron ring is transported to the wire coiling mechanism 3 through the wire feeding mechanism 4, the wire coiling mechanism 3 coils the iron ring into shape, cuts through the cutting and spot welding mechanism 2, and is welded into shape, and the formed iron ring is pushed out through the discharging structure.

[0032] The cutting spot welding mechanism 2 comprises:

[0033] The cutting spot welding cylinder assembly includes a first cylinder 13 disposed above the cutting spot welding mechanism 2 and a second cylinder 14 disposed on the side of the cutting spot welding mechanism 2;

[0034] The clamp cylinder assembly includes a third cylinder 15 and a fourth cylinder 16 disposed on both sides of the first cylinder 13, wherein a third pressing block bracket 20 connected thereto is disposed below the third cylinder 15, and a fourth pressing block bracket 21 connected thereto is disposed below the fourth cylinder 16;

[0035] A base 17 is disposed below the cutting and spot welding mechanism 2, a guide copper seat 19 is disposed above the base 17, a guide base 1817 is disposed on the side of the base 17, and the guide base 1817 is connected with the third pressing block bracket 20;

[0036] A spot welding assembly is arranged below the first cylinder 13, comprising a spot welding bracket 22 arranged below the first cylinder 13 and connected to a spot welding copper rod 23 above the guide copper seat 19, wherein the spot welding copper rod 23 is connected to the spot welding bracket 22;

[0037] The cutter 24 is arranged inside the spot welding assembly and connected to the first cylinder 13;

[0038] The iron ring is fixed by the fourth pressure block bracket 21 driven by the fourth cylinder 16; the first cylinder 13 drives the cutter 24 to press down and cut the iron ring; the third cylinder 15 drives the third pressure block bracket 20 to fix the cut iron ring; the second cylinder 14 drives the guide base 1817 to move the iron ring fixed by the third pressure block bracket 20 to the guide copper seat 19; the first cylinder 13 drives the spot welding bracket 22 and the connected spot welding copper rod 23 to move downward; the spot welding copper rod 23 generates a strong current to weld the iron ring; a connecting part 42 is provided between the spot welding copper rod 23 and the spot welding bracket 22 to be connected and fixed.

[0039] The wire coil mechanism 3 comprises:

[0040] The push cylinder assembly 40 is arranged outside the wire coiling mechanism 3, and includes a first push cylinder 25 arranged on the left side of the wire coiling mechanism 3, a second push cylinder 26 arranged on the right side of the wire coiling mechanism 3, a third push cylinder 27 arranged below the wire coiling mechanism 3, and a fourth push cylinder 28 and a fifth push cylinder 29 arranged above the first push cylinder 25 and the second push cylinder 26;

[0041] The arc-shaped push plate assembly 39 is arranged on the push cylinder assembly 40, and the arc-shaped push plate is connected to the push cylinder assembly 40;

[0042] The guide plate assembly 41 is disposed in the middle of the wire coiling mechanism 3, and includes a first guide plate 35 disposed on the left side of the guide plate, a second guide plate 36 disposed on the right side of the guide plate, and a lower guide plate 37 disposed below the guide plate;

[0043] The first pushing cylinder 25 is connected to the first arc-shaped push plate 30, the second pushing cylinder 26 is connected to the second arc-shaped push plate 31, the third pushing cylinder 27 is connected to the third arc-shaped push plate 32, the fourth pushing cylinder 28 is connected to the fourth arc-shaped push plate 33, and the fifth pushing cylinder 29 is connected to the fifth arc-shaped push plate 34. The iron ring drives the arc-shaped push plate assembly 39 through the pushing cylinder assembly 40, and cooperates with the guide plate assembly 41 arranged in the middle to form a circular contour so that the iron ring forms a circle within the circular contour.

[0044] The discharging mechanism 5 comprises a discharging cylinder 7 arranged on the discharging mechanism 5 and a discharging claw 8 arranged on the discharging cylinder 7, and the discharging claw 8 is connected to the discharging cylinder 7; the formed iron ring is pushed out by the discharging cylinder 7 driving the discharging claw 8.

[0045] The wire feeding mechanism 4 includes a driving motor 9, a feeding roller group 10 and a correction tube 11 on the right side of the spot welding structure, and the correction tube 11 is fixedly connected by a fixing frame 12; the iron ring is driven by the driving motor 9 to drive the feeding roller group 10 to transport the iron ring through the correction tube 11 to the next process; the driving motor 9 controls the length of the iron ring and the wire feeding speed.

[0046] The wire feeding mechanism 4, the cutting and spot welding mechanism 2, the wire coiling mechanism 3 and the wire coiling mechanism 3 are all arranged on the fixed plate 6 above the fuselage 1 and fixedly connected; the wire feeding mechanism 4 is arranged on the side of the fixed plate 6 and fixedly connected; the cutting and spot welding mechanism 2, the wire coiling mechanism 3 and the wire coiling mechanism 3 are all arranged on the front of the fixed plate 6 and fixedly connected.

[0047] The button box 38 is arranged on the side of the body 1; the button box 38 controls the start and stop of the device.

[0048] In this embodiment, when the automatic processing equipment is started, the iron ring is transmitted to the wire coiling mechanism 3 through the driving motor 9 of the wire feeding mechanism 4 to control the feeding roller group 10. The wire coiling mechanism 3 drives the arc push plate assembly 39 to cooperate with the guide plate assembly 41 arranged in the middle to present a circular contour by pushing the cylinder assembly 40, and the iron ring is circled and formed within the circular contour. At this time, the cutting and spot welding mechanism 2 drives the fourth pressure block bracket 21 to fix the iron ring through the fourth cylinder 16, and the first cylinder 13 drives the cutter 24 to press down and cut the iron ring. The third cylinder 15 drives the third pressure block bracket 20 to fix the cut iron ring, and the second cylinder 14 drives the guide base 18 to move the iron ring fixed by the third pressure block bracket 20 to the guide copper seat 19. The first cylinder 13 drives the spot welding bracket 22 and the connected spot welding copper rod 23 to move downward, and the spot welding copper rod 23 generates a strong current to weld the iron ring into shape, and the discharging mechanism 5 drives the discharging claw 8 through the discharging cylinder 7 to push out the formed iron ring.

[0049] As described in the specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example" or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art can combine and combine different embodiments or examples described in this specification and the features of different embodiments or examples without contradiction.

[0050] The standard parts used in the present invention can all be purchased from the market, and special-shaped parts can be customized according to the description in the specification and drawings. The specific connection methods of each part adopt conventional means such as mature bolts, rivets, welding, and bonding in the prior art, which will not be described in detail here.

[0051] The above contents are only preferred embodiments of the present invention. For ordinary technicians in this field, various changes and variations can be made in the specific implementation methods and application scopes based on the ideas of the present invention. The content of this specification should not be understood as a limitation on the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of the claims of the present invention.

Claims

1. An automatic processing device for fixing a hat brim iron ring, comprising a machine body, characterized in that: The fuselage is respectively provided with a wire feeding mechanism located on the side of the fuselage, a cutting and spot welding mechanism located above the fuselage, a wire coiling mechanism located below the cutting and spot welding mechanism, and a discharging mechanism located on the side of the cutting and spot welding mechanism; the iron ring is sequentially transported to the wire coiling mechanism through the wire feeding mechanism to be coiled and formed, cut and welded through the cutting and spot welding mechanism, and discharged through the discharging structure; the iron ring is transported to the wire coiling mechanism through the wire feeding mechanism, the wire coiling mechanism coils the iron ring into shape, cuts and welds through the cutting and spot welding mechanism, and the formed iron ring is pushed out through the discharging structure.

2. The automatic processing equipment for fixing the brim iron ring according to claim 1 is characterized by: The cutting spot welding mechanism comprises: The cutting and spot welding cylinder assembly comprises a first cylinder arranged above the cutting and spot welding mechanism and a second cylinder arranged at the side of the cutting and spot welding mechanism; The clamp cylinder assembly includes a third cylinder and a fourth cylinder arranged on both sides of the first cylinder, a third pressing block bracket connected to the third cylinder is provided below the third cylinder, and a fourth pressing block bracket connected to the fourth cylinder is provided below the fourth cylinder; A base is arranged below the cutting and spot welding mechanism, a guide copper seat is arranged above the base, a guide base is arranged on the side of the base, and the guide base is connected with the third pressing block bracket in cooperation; A spot welding assembly is arranged below the first cylinder, comprising a spot welding bracket connected to each other below the first cylinder and a spot welding copper rod above the guide copper seat, wherein the spot welding copper rod is connected to the spot welding bracket; The cutter is arranged inside the spot welding assembly and connected with the first cylinder.

3. The automatic processing equipment for fixing the brim iron ring according to claim 1 is characterized by: The wire coil mechanism comprises: A push cylinder assembly is arranged outside the wire coiling mechanism, comprising a first push cylinder arranged on the left side of the wire coiling mechanism, a second push cylinder arranged on the right side of the wire coiling mechanism, a third push cylinder arranged below the wire coiling mechanism, and a fourth push cylinder and a fifth push cylinder arranged above the first push cylinder and the second push cylinder; An arc-shaped push plate assembly is arranged on the push cylinder assembly, and the arc-shaped push plate assembly is connected to the push cylinder assembly; The guide plate assembly is arranged in the middle of the wire loop mechanism, and comprises a first guide plate arranged on the left side of the guide plate, a second guide plate arranged on the right side of the guide plate, and a lower guide plate arranged below the guide plate.

4. The automatic processing equipment for fixing the brim iron ring according to claim 1 is characterized by: The discharging mechanism comprises a discharging cylinder arranged on the discharging mechanism and a discharging claw arranged on the discharging cylinder, and the discharging claw is connected to the discharging cylinder.

5. The automatic processing equipment for fixing the brim iron ring according to claim 1 is characterized by: The wire feeding mechanism comprises a driving motor, a feeding roller group and a correction round tube on the right side of the spot welding structure, and the correction round tube is fixedly connected via a fixing frame.

6. The automatic processing equipment for fixing the brim iron ring according to claim 1, characterized in that: The wire feeding mechanism, the material cutting spot welding mechanism, the wire coiling mechanism and the wire coiling mechanism are all arranged on a fixed plate above the machine body and are fixedly connected.

7. The automatic processing equipment for hat brim fixing iron ring according to claim 1, characterized in that: A button box is arranged on the side of the fuselage.