An assembly spot welding system for H-beam
By designing the assembly spot welding system of H-shaped steel, the automated feeding mechanism and roof plate mechanism of web and wing plate are used to realize welding assembly and welding, which solves the problems of low welding efficiency, high labor cost and welding environment pollution in the existing technology, and achieves an efficient and safe welding process.
Patent Information
- Application Number
- CN202420359902.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-02-27
- Publication Date
- 2025-04-04
- Estimated Expiration
- 2034-02-27
AI Technical Summary
The assembly welding method of existing H-shaped steel is inefficient and has high labor costs. There are problems such as welding smoke and light pollution affecting the health of welding personnel during welding.
A H-shaped steel assembly spot welding system is designed, including a web feeding mechanism, a wing feeding mechanism and a top plate mechanism. Through these mechanisms, the automatic assembly and welding of webs and wings is realized, and manual spot welding is avoided.
It improves the efficiency of H-shaped steel welding, reduces labor costs, and reduces the harm to the health of welding personnel during the welding process.
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Figure CN222711168U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of steel structure processing equipment, in particular to an assembly spot welding system for H-shaped steel. Background Art
[0002] Steel structure support frames made of I-beams are widely used in various large-scale construction projects. Steel structure support frames are usually manufactured in the factory in advance and then transported to the construction site for use. In the manufacturing process of steel structure support frames, they are usually welded from small angle steels and I-beams or I-beams.
[0003] For large-scale construction projects such as steel structure support frames of large factories, the overall size is relatively large, and the size of the I-beams or H-shaped steels of the steel structure support frames is also relatively large. In the process of producing I-beams and H-shaped steels, multiple steel plates are assembled and welded. At present, it is usually done manually by spot welding the assembled multiple steel plates to finalize the shape, and then the welds are welded by a welding machine. However, when spot welding is done manually, one of the wing plates is usually welded first, and then the other wing plate is assembled and spot welded after the welding of the wing plate is completed. As a result, the current H-beam assembly welding method is inefficient. In particular, when welding the wing plates, two welders are required to weld from both sides of the web, which has high labor costs. In addition, there are problems such as welding smoke and light pollution during welding that affect the health of welders.
[0004] In view of the above background, the inventor has designed an assembly spot welding system for H-beams to solve at least one of the above problems, and thus proposed the present application. Utility Model Content
[0005] The purpose of this application is to provide an assembly spot welding system for H-beam to solve the above problems.
[0006] In order to solve the above technical problems, the utility model adopts the following solutions:
[0007] The present application provides an assembly spot welding system for H-shaped steel, comprising a web feeding mechanism and a wing feeding mechanism, and a top plate mechanism for placing a web on top, wherein the top plate mechanism and the wing feeding mechanism are arranged alternately with the web feeding mechanism along a feeding direction;
[0008] It also includes a spot welding structure arranged on the wing plate feeding mechanism and a guide rail arranged perpendicular to the feeding direction. The welding end of the spot welding structure is arranged toward the middle of the wing plate close to the web side, and the wing plate feeding structure is slidably connected to the guide rail.
[0009] Preferably, the web feeding mechanism comprises a plurality of feeding rollers arranged in parallel, and a transmission mechanism and a driving structure for driving the plurality of feeding rollers to rotate synchronously;
[0010] The wing plate feeding mechanism and the top plate mechanism are arranged between the feeding rollers, and the guide rails are arranged parallel to the feeding rollers.
[0011] Preferably, the fender feeding mechanism comprises a fender bracket and at least two fender support wheels rotatably connected to the fender bracket, and a drive motor, wherein:
[0012] The two fender support wheels are arranged up and down, and the two fender support wheel brackets have space for accommodating the fenders. The drive motor is fixed on the fender brackets, and the output end of the drive motor is fixedly connected to the fender support wheel located below. The height of the fender support wheel located below is higher than the height of the belly plate feeding mechanism.
[0013] Preferably, a wing plate placement groove for placing the wing plate is provided in the middle of the wing plate support wheel;
[0014] The wing support wheel comprises a support wheel part A and a support wheel part B which are detachably connected, and the wing placement groove is located between the support wheel part A and the support wheel part B.
[0015] Preferably, the wing support is further provided with two transverse support rods for installing the spot welding structure, and the two transverse support rods are respectively located above and below the two wing support wheels;
[0016] The spot welding structure is arranged at one end of the transverse support rod away from the wing plate bracket.
[0017] Preferably, wing plate feeding mechanisms are provided on both sides of the feeding channel of the web feeding mechanism, and the wing plate feeding mechanisms on both sides of the feeding channel of the web feeding mechanism are arranged opposite to each other.
[0018] Preferably, the bracket is provided with a vertical strip hole, and a horizontal connecting rod is detachably provided on the strip hole;
[0019] The wing support wheel located above is rotatably connected to the bracket through a connecting rod.
[0020] Preferably, the top plate mechanism is located below the feeding channel of the web feeding mechanism, and the top plate mechanism includes a vertically arranged telescopic rod, a roller bracket arranged at the output end of the telescopic rod, and a supporting roller arranged on the roller bracket.
[0021] Preferably, two top plate mechanisms are provided, and the structures of the two top plate mechanisms are the same;
[0022] The top plate mechanism also includes a first sliding block slidably connected to the guide rail, and the telescopic rod is arranged on the first sliding block.
[0023] Beneficial effects of the utility model:
[0024] The present application sets up a web feeding mechanism, a wing plate feeding mechanism, and a top plate mechanism. After the web and wing plates are transported to the predetermined positions, the top plate mechanism is used to push the web to a predetermined height to complete the assembly. Subsequently, the spot welding mechanism is used to perform spot welding to complete the welding and shaping of the H-shaped steel. Compared with the prior art, manual spot welding is not required, which can solve the problems of low welding efficiency and high labor cost in the prior art. In addition, there are problems such as welding smoke and light pollution that affect the health of welders during welding. BRIEF DESCRIPTION OF THE DRAWINGS
[0025] Figure 1 It is a schematic diagram of the structure of an embodiment of the present application.
[0026] Figure 2 This is a schematic diagram of the structure of the embodiment of the present application when in use.
[0027] Explanation of the accompanying drawings: 1-feeding roller, 2-guide rail, 31-first slider, 32-telescopic rod, 33-roller bracket, 34-support roller, 41-wing plate bracket, 411-second slider, 412-lateral support rod, 42-driving motor, 421-output shaft, 43-connecting rod, 44-wing plate support wheel, 441-support wheel part A, 442-support wheel part B, 443-wing plate placement groove, 45-spot welding structure. DETAILED DESCRIPTION
[0028] The present invention will be further described in detail below in conjunction with the embodiments and drawings, but the implementation manner of the present invention is not limited thereto.
[0029] In the description of the present utility model, it should be noted that the terms "center", "up", "down", "left", "right", "vertical", "longitudinal", "lateral", "horizontal", "inside", "outside", "front", "back", "top", "bottom", etc. indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings, or are the directions or positional relationships in which the utility model product is usually placed when in use. They are only for the convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore cannot be understood as a limitation on the present utility model.
[0030] In the description of the present invention, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "set", "open", "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0031] The present invention will be described in detail below with reference to the accompanying drawings and in combination with embodiments.
[0032] like Figure 1 and Figure 2 As shown, this embodiment provides an assembly spot welding system for H-beams, including a web feeding mechanism and a wing feeding mechanism, and a top plate mechanism for placing a web on top, wherein the top plate mechanism and the wing feeding mechanism are arranged alternately with the web feeding mechanism along a feeding direction;
[0033] It also includes a spot welding structure 45 arranged on the wing plate feeding mechanism, and a guide rail 2 arranged perpendicular to the feeding direction. The welding end of the spot welding structure 45 is arranged toward the middle part of the wing plate close to the web side, and the wing plate feeding structure is slidably connected to the guide rail 2.
[0034] In this embodiment, a web feeding mechanism, a wing plate feeding mechanism, and a top plate mechanism are provided. After the web and the wing plates are transported to predetermined positions, the top plate mechanism is used to push the web to a predetermined height to complete the assembly. Subsequently, the spot welding mechanism is used to perform spot welding to complete the welding and shaping of the H-shaped steel. Compared with the prior art, manual spot welding is not required, which can solve the problems of low welding efficiency and high labor cost in the prior art. In addition, there are problems such as welding smoke and light pollution that affect the health of welders during welding.
[0035] The spot welding structure 45 in this embodiment can adopt a common welding device, which will not be described in detail here. The core concept of this application is to combine the web feeding mechanism and the wing feeding mechanism, as well as the top plate mechanism, the guide rail 2, etc., so as to complete the automatic assembly and welding according to the shape characteristics of the H-shaped steel, and solve the problem of existing manual welding.
[0036] In some preferred embodiments, the web feeding mechanism comprises a plurality of feeding rollers 1 arranged in parallel, and a transmission mechanism and a driving structure for driving the plurality of feeding rollers 1 to rotate synchronously;
[0037] The wing plate feeding mechanism and the top plate mechanism are arranged between the feeding rollers 1, and the guide rail 2 is arranged parallel to the feeding rollers 1. The feeding rollers, transmission mechanism and driving structure in this embodiment are all common components and will not be described in detail here.
[0038] In some preferred embodiments, the flap feeding mechanism includes a flap bracket 41 and at least two flap support wheels 44 rotatably connected to the flap bracket 41, and a drive motor 42, wherein:
[0039] Two flap support wheels 44 are arranged up and down, and the two flap support wheel 44 brackets have a space for accommodating the flaps, and the drive motor 42 is fixed on the flap bracket 41. The output end of the drive motor 42 is fixedly connected to the flap support wheel 44 located below, and the height of the flap support wheel 44 located below is higher than the height of the web feeding mechanism. By setting the drive motor 42, the flap support wheel 44 located below can be driven to rotate, thereby driving the flap to move.
[0040] In some preferred embodiments, a wing plate placement groove 443 for placing the wing plate is provided in the middle of the wing plate support wheel 44;
[0041] The wing support wheel 44 includes a detachably connected support wheel A portion 441 and a support wheel B portion 442, and the wing placement groove 443 is located between the support wheel A portion 441 and the support wheel B portion 442. By providing the detachable support wheel A portion 441 and the support wheel B portion 442, the shape of the support wheel A portion 441 can be set as needed, and the width of the wing placement groove 443 can be controlled to improve the adaptability to wing panels of different thicknesses.
[0042] In some preferred embodiments, the wing support 41 is further provided with two transverse support rods 412 for mounting the spot welding structure 45, and the two transverse support rods 412 are respectively located above and below the two wing support wheels 44;
[0043] The spot welding structure 45 is arranged at one end of the transverse support rod 412 away from the wing support 41. By providing two transverse support rods 412 and the spot welding structure 45 on the transverse support rods 412, welding can be performed from both sides of the web at one time to complete welding shaping.
[0044] In some preferred embodiments, wing plate feeding mechanisms are provided on both sides of the feeding channel of the web feeding mechanism, and the wing plate feeding mechanisms on both sides of the feeding channel of the web feeding mechanism are arranged opposite to each other. In this embodiment, wing plate feeding mechanisms are provided on both sides of the feeding channel of the web feeding mechanism, so that the wing plates on both sides of the web can be welded at one time, thereby improving welding efficiency.
[0045] In some preferred embodiments, the bracket is provided with a vertical strip hole, and a horizontal connecting rod 43 is detachably provided on the strip hole;
[0046] The wing support wheel 44 located above is rotatably connected with the bracket through a connecting rod 43. By arranging the strip hole and the connecting rod 43, the height difference of the two wing support wheels 44 can be adjusted, and wing plates of different widths can be used.
[0047] In some preferred embodiments, the top plate mechanism is located below the feeding channel of the web feeding mechanism, and the top plate mechanism includes a telescopic rod 32 arranged vertically, a roller bracket 33 arranged at the output end of the telescopic rod 32, and a supporting roller 34 arranged on the roller bracket 33. The supporting roller can avoid affecting the movement of the H-beam during welding.
[0048] In some preferred embodiments, two top plate mechanisms are provided, and the structures of the two top plate mechanisms are the same;
[0049] The top plate mechanism also includes a first slider 31 slidably connected to the guide rail 2, and the telescopic rod 32 is arranged on the first slider 31. By arranging two top plate mechanisms, the web is lifted more stably and the stability is improved.
[0050] The working principle of this embodiment:
[0051] When this embodiment is in use, the web and wing plates are first transported to the specified position by the web transport mechanism and the wing plate transport mechanism, and then the web is lifted up by the top plate mechanism. When the web is pushed to the middle of the wing plate, it stops and the height is stabilized. Then the two wing plate transport mechanisms are close to each other, so that the end faces of the two wing plates and the web plate are in contact and pressed against each other. At this time, the H-shaped steel is assembled, and then it can be fixed by spot welding using the spot welding structure 45.
[0052] It is understood that the above embodiments are merely exemplary embodiments used to illustrate the principles of the present invention, but the present invention is not limited thereto. For those skilled in the art, various modifications and improvements can be made without departing from the spirit and essence of the present invention, and these modifications and improvements are also considered to be within the scope of protection of the present invention.
Claims
1. An assembly spot welding system for H-beam, characterized in that: It includes a web feeding mechanism and a wing feeding mechanism, and a top plate mechanism for pushing the web, and the top plate mechanism and the wing feeding mechanism are arranged alternately with the web feeding mechanism along the feeding direction; It also includes a spot welding structure (45) arranged on the wing plate feeding mechanism and a guide rail (2) arranged perpendicular to the feeding direction, the welding end of the spot welding structure (45) is arranged toward the middle of the wing plate near the web, and the wing plate feeding structure is slidably connected to the guide rail (2); The web feeding mechanism comprises a plurality of feeding rollers (1) arranged in parallel, and a transmission mechanism and a driving structure for driving the plurality of feeding rollers (1) to rotate synchronously; The wing plate feeding mechanism and the top plate mechanism are arranged between the feeding rollers (1), and the guide rail (2) is arranged parallel to the feeding rollers (1); The wing plate feeding mechanism comprises a wing plate bracket (41), at least two wing plate support wheels (44) rotatably connected to the wing plate bracket (41), and a driving motor (42), wherein: Two wing support wheels (44) are arranged up and down, and the two wing support wheel (44) brackets have a space for accommodating the wing, and the drive motor (42) is fixed to the wing bracket (41), and the output end of the drive motor (42) is fixedly connected to the wing support wheel (44) located below, and the height of the wing support wheel (44) located below is higher than the height of the web feeding mechanism.
2. The H-beam assembly spot welding system according to claim 1, characterized in that: A wing plate placement groove (443) for placing the wing plate is provided in the middle of the wing plate support wheel (44); The wing plate support wheel (44) comprises a support wheel portion A (441) and a support wheel portion B (442) which are detachably connected, and the wing plate placement groove (443) is located between the support wheel portion A (441) and the support wheel portion B (442).
3. The H-beam assembly spot welding system according to claim 1, characterized in that: The wing support (41) is further provided with two transverse support rods (412) for mounting the spot welding structure (45), and the two transverse support rods (412) are respectively located above and below the two wing support wheels (44); The spot welding structure (45) is arranged at one end of the transverse support rod (412) away from the wing plate bracket (41).
4. The H-beam assembly spot welding system according to claim 1, characterized in that: Wing plate feeding mechanisms are arranged on both sides of the feeding channel of the web feeding mechanism, and the wing plate feeding mechanisms on both sides of the feeding channel of the web feeding mechanism are arranged opposite to each other.
5. The H-beam assembly spot welding system according to claim 1, characterized in that: The bracket is provided with a vertical strip hole, and a horizontal connecting rod (43) is detachably provided on the strip hole; The wing support wheel (44) located above is rotatably connected to the bracket via a connecting rod (43).
6. The H-beam assembly spot welding system according to claim 1, characterized in that: The top plate mechanism is located below the feeding channel of the web feeding mechanism, and comprises a telescopic rod (32) arranged vertically, a roller bracket (33) arranged at the output end of the telescopic rod (32), and a supporting roller (34) arranged on the roller bracket (33).
7. The H-beam assembly spot welding system according to claim 6, characterized in that: The top plate mechanisms are provided with two, and the structures of the two top plate mechanisms are the same; The top plate mechanism also includes a first sliding block (31) slidably connected to the guide rail (2), and the telescopic rod (32) is arranged on the first sliding block (31).