Carbon fiber construction tool

Abstract

The utility model discloses a carbon fiber construction tool which comprises a machine body, an adhesive storage cavity, a carbon fiber material containing cavity and a feeding channel are formed in the machine body, and one end of the feeding channel is communicated with the carbon fiber material containing cavity. The carbon fiber construction tool has the beneficial effects that a group of carbon fiber construction tools consisting of the machine body, the adhesive storage cavity, the adhesive outlet, the leakage net, the carbon fiber material accommodating cavity, the fixed bearing, the carbon fiber material disc, the feeding channel and the rotating shaft assembly are arranged, so that a worker can utilize the construction tools; the gluing work and the attaching work in the carbon fiber pasting work are completed together, so that the pasting work of the carbon fiber material can be rapidly completed, it can be guaranteed that bonding glue is fully utilized, waste is avoided, meanwhile, the covering completion degree of attaching of the bonding glue and the carbon fiber material can be guaranteed, and the pasting efficiency of the carbon fiber material is improved. Pollution of exposed colloid to the concrete surface is avoided, and the environment-friendly effect is improved.

Description

Technical Field

[0001] The utility model relates to the field of carbon fibers, in particular to a carbon fiber construction tool. Background Art

[0002] Carbon fiber, a high-strength, high-modulus fiber with a carbon content of over 90%, boasts high-temperature resistance, anti-friction, thermal conductivity, and corrosion resistance. Its fibrous, flexible appearance allows it to be processed into a variety of fabrics. Its high-temperature resistance is the highest among all chemical fibers. It is made from acrylic and viscose fibers through high-temperature oxidation and carbonization.

[0003] The existing traditional carbon fiber pasting construction process is to manually apply glue and then manually paste the carbon fiber. This operation method is time-consuming and labor-intensive. In the process of applying glue, if the width of the glue is not increased, manual precise pasting is required, resulting in low operation efficiency. Although increasing the width of the glue improves the pasting efficiency, it not only wastes the adhesive, but the exposed glue also pollutes the concrete surface. Therefore, it is necessary to propose a carbon fiber construction tool that can simultaneously complete the gluing and pasting operations. Utility Model Content

[0004] The technical problem to be solved by the utility model is to provide a carbon fiber construction tool capable of completing gluing and pasting operations simultaneously in response to the current status of the existing technology.

[0005] The present invention is achieved through the following technical solution: The present invention proposes a carbon fiber construction tool, including a fuselage, wherein the fuselage is respectively provided with an adhesive storage chamber, a carbon fiber material accommodating chamber and a feeding channel, one end of the feeding channel is connected with the carbon fiber material accommodating chamber, and the other end passes through the fuselage to form a discharge port, a glue outlet is provided at the lower end of the adhesive storage chamber adjacent to the feeding channel, a permeation net is fixedly installed in the glue outlet, a carbon fiber material disk is rotatably connected to the carbon fiber material accommodating chamber through a fixed bearing, the carbon fiber material disk extends out of the discharge port through the feeding channel, and a rotating shaft assembly is arranged in the feeding channel.

[0006] By adopting the above technical solution, the carbon fiber material disc can be rotated and discharged in the carbon fiber material accommodating cavity under the action of the fixed bearing, and the released carbon fiber material strip will be discharged from the fuselage through the feeding channel. When the carbon fiber material strip passes through the glue outlet, a layer of glue can be adhered to its surface for the pasting operation after being discharged from the fuselage.

[0007] Furthermore, the shaft assembly consists of the guide shaft, the gluing shaft and the rolling shaft. The guide shaft is located at the junction of the feeding channel and the carbon fiber material accommodating cavity, the gluing shaft is located below the glue outlet, and the rolling shaft is located outside the outlet. The guide shaft and the gluing shaft are both rotatably connected to the fuselage, and the rolling shaft is connected to the fuselage through a top pressure assembly.

[0008] By adopting the above technical solution, the guide shaft can provide a guiding effect for the discharge of the carbon fiber material disc, and the glue coating shaft can provide a top pressure effect for the discharge of the carbon fiber material disc, so that it can be close to the glue outlet, so that the glue in the adhesive glue storage cavity can be coated on the surface of the carbon fiber material disc through the permeable net, and the rolling shaft can roll the carbon fiber material disc discharged from the fuselage to the surface of the target object.

[0009] Furthermore, the pressing assembly is composed of a spring sheet and a fixing seat. The spring sheet is sleeved on both ends of the rolling shaft, and the spring sheet is fixedly mounted on both side walls of the fuselage through the fixing seat.

[0010] By adopting the above technical solution, the spring sheet can make the rolling shaft have appropriate deformation elasticity, so that the rolling shaft can be used flexibly and can be applied to uneven surfaces of objects.

[0011] Furthermore, a sealing plate is detachably connected to one side wall of the fuselage through a slot, and the sealing plate can cover the carbon fiber material accommodating cavity.

[0012] By adopting the above technical solution, the sealing plate can be disassembled and assembled, so that the staff can use and replace the carbon fiber material disk.

[0013] Furthermore, an observation window is embedded on one side wall of the fuselage, the observation window is made of a transparent material, and scale markings are coated on the observation window.

[0014] By adopting the above technical solution, it is convenient for staff to observe the remaining glue in the adhesive storage cavity.

[0015] Furthermore, a handle is fixedly installed at the lower end of the fuselage.

[0016] By adopting the above technical solution, it is convenient for workers to grasp.

[0017] Furthermore, a glue injection valve is installed on the body above the adhesive storage cavity through a card slot.

[0018] By adopting the above technical solution, the glue liquid in the adhesive glue storage cavity can be replenished when the remaining amount is insufficient.

[0019] Compared with the prior art, the present invention has the following beneficial effects:

[0020] The utility model provides a carbon fiber construction tool consisting of a body, an adhesive storage cavity, an adhesive outlet, a leakage net, a carbon fiber material accommodating cavity, a fixed bearing, a carbon fiber material disc, a feeding channel and a rotating shaft assembly. The utility model can use the construction tool to complete the gluing work and the attachment work in the carbon fiber pasting operation at the same time, so that the pasting operation of the carbon fiber material can be completed quickly, which not only ensures the full utilization of the adhesive and avoids waste, but also ensures the coverage completion of the adhesive and the carbon fiber material attachment, avoids the exposed colloid from polluting the concrete surface, and improves the environmental protection effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 This is a schematic structural diagram of the carbon fiber construction tool of the present invention;

[0022] Figure 2 This is a left side view of the carbon fiber construction tool of the present invention;

[0023] Figure 3 This is a schematic structural diagram of the separation and sealing plate in the carbon fiber construction tool of the present invention;

[0024] Figure 4 This is a cross-sectional view of the carbon fiber construction tool of the present invention;

[0025] Figure 5 It is a carbon fiber construction tool described in the utility model Figure 5 Schematic diagram of the independent structure of the mid-fuselage.

[0026] The following are the descriptions of the reference numerals:

[0027] 1. Body; 2. Adhesive storage chamber; 201. Glue injection valve; 202. Glue outlet; 203. Leakage net; 3. Carbon fiber material accommodating chamber; 301. Fixed bearing; 302. Carbon fiber material disc; 4. Feeding channel; 401. Discharge port; 402. Guide shaft; 403. Gluing shaft; 404. Rolling shaft; 5. Pressing assembly; 501. Spring sheet; 502. Fixed seat; 6. Sealing plate; 7. Observation window; 8. Handle. DETAILED DESCRIPTION

[0028] In order to make the purpose, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.

[0029] like Figure 1 、 Figure 3 and Figure 4 As shown, the carbon fiber construction tool in this embodiment includes a fuselage 1, which is respectively provided with an adhesive storage chamber 2, a carbon fiber material accommodating chamber 3 and a feeding channel 4. One end of the feeding channel 4 is connected to the carbon fiber material accommodating chamber 3, and the other end passes through the fuselage 1 to form a discharge port 401. A glue discharge port 202 is provided at the lower end of the adhesive storage chamber 2 adjacent to the feeding channel 4, and a permeation net is fixedly installed in the glue discharge port 202. A carbon fiber material disk 302 is rotatably connected to the carbon fiber material accommodating chamber 3 through a fixed bearing 301. The carbon fiber material disk 302 extends out of the discharge port 401 through the feeding channel 4. A rotating shaft assembly is arranged in the feeding channel 4. The carbon fiber material disk 302 can be discharged outward through the feeding channel 4. The rotating shaft assembly can provide a guiding effect for the discharge of the carbon fiber material disk 302, and enables the carbon fiber material disk 302 to pass through the glue discharge port 202 during the discharge process, so that a layer of adhesive is coated on its surface. When the carbon fiber material disk 302 is discharged from the fuselage 1, the pasting operation can be carried out.

[0030] like Figure 3-Figure 5 As shown, the shaft assembly consists of a guide shaft 402, a glue coating shaft 403 and a rolling shaft 404. The guide shaft 402 is located at the junction of the feeding channel 4 and the carbon fiber material accommodating chamber 3. The glue coating shaft 403 is located below the glue outlet 202. The rolling shaft 404 is located outside the discharge port 401. The guide shaft 402 and the glue coating shaft 403 are both rotatably connected to the fuselage 1. The rolling shaft 404 is connected to the fuselage 1 through the top pressure component 5. The guide shaft 402 can provide a space for the carbon fiber material disc 302 to enter the feeding channel 4. The material channel 4 provides a guiding function, and the glue coating shaft 403 can press the carbon fiber material disc 302 to make it close to the glue outlet 202, and under the action of the permeable net 203, a layer of glue is adhered to its surface. The permeable net 203 can prevent the glue from overflowing too quickly or too much, ensuring the uniformity of the glue adhering to the surface of the carbon fiber material disc 302. The rolling shaft 404 can provide a rolling effect for the carbon fiber material disc 302 discharged from the fuselage 1 during pasting, so that the pasted carbon fiber material disc 302 can be adhered to the target object flatly.

[0031] like Figure 3 and Figure 4 As shown, the pressing assembly 5 is composed of a spring sheet 501 and a fixing seat 502. The spring sheet 501 is sleeved on both ends of the rolling shaft 404. The spring sheet 501 is fixedly mounted on the two side walls of the fuselage 1 through the fixing seat 502. The spring sheet 501 can provide an elastic support effect for the rolling shaft 404, so that the carbon fiber material disk 302 can smoothly complete the adhesion and rolling operation when encountering uneven places during the pasting process.

[0032] like Figure 1 and Figure 2As shown, a sealing plate 6 is detachably connected to one side wall of the fuselage 1 through a card slot, and the sealing plate 6 can cover the carbon fiber material accommodating chamber 3, so that the user can open the carbon fiber material accommodating chamber 3 to replace the carbon fiber material disk 302; an observation window 7 is embedded on one side wall of the fuselage 1, and the observation window 7 is made of transparent material. The observation window 7 is coated with scale markings, and the user can observe the remaining glue in the adhesive storage chamber 2 through the observation window 7; a handle 8 is fixedly installed at the lower end of the fuselage 1 to facilitate the user's grip on the fuselage 1; a glue injection valve 201 is installed on the fuselage 1 above the adhesive storage chamber 2 through a card slot, and the user can add glue to the adhesive storage chamber 2 through the glue injection valve 201.

[0033] The above description of the disclosed embodiments will enable one skilled in the art to implement or use the present invention. Various modifications to these embodiments will be readily apparent to one skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention is not limited to the embodiments shown herein but is intended to conform to the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. Carbon fiber construction tool, characterized by: The invention comprises a fuselage (1), wherein the fuselage (1) is respectively provided with an adhesive storage chamber (2), a carbon fiber material accommodating chamber (3) and a feeding channel (4), one end of the feeding channel (4) is communicated with the carbon fiber material accommodating chamber (3), and the other end thereof penetrates the fuselage (1) and is formed with a discharge port (401), a glue discharge port (202) is provided at the lower end of the adhesive storage chamber (2) adjacent to the feeding channel (4), a permeation net is fixedly installed in the glue discharge port (202), a carbon fiber material disk (302) is rotatably connected in the carbon fiber material accommodating chamber (3) via a fixed bearing (301), the carbon fiber material disk (302) extends out of the discharge port (401) through the feeding channel (4), and a rotating shaft assembly is arranged in the feeding channel (4).

2. The carbon fiber construction tool according to claim 1, characterized in that: The rotating shaft assembly consists of a guide rotating shaft (402), a glue coating rotating shaft (403) and a rolling rotating shaft (404); the guide rotating shaft (402) is located at the junction of the feeding channel (4) and the carbon fiber material accommodating chamber (3); the glue coating rotating shaft (403) is located below the glue outlet (202); and the rolling rotating shaft (404) is located outside the discharge outlet (401); the guide rotating shaft (402) and the glue coating rotating shaft (403) are both rotatably connected to the fuselage (1); and the rolling rotating shaft (404) is connected to the fuselage (1) via a top pressing assembly (5).

3. The carbon fiber construction tool according to claim 2, characterized in that: The pressing assembly (5) is composed of a spring sheet (501) and a fixing seat (502), wherein the spring sheet (501) is sleeved on both ends of the rolling shaft (404), and the spring sheet (501) is fixedly mounted on both side walls of the body (1) via the fixing seat (502).

4. The carbon fiber construction tool according to claim 1, characterized in that: A sealing plate (6) is detachably connected to one side wall of the fuselage (1) via a slot, and the sealing plate (6) can cover the carbon fiber material accommodating cavity (3).

5. The carbon fiber construction tool according to claim 1, characterized in that: An observation window (7) is embedded on one side wall of the fuselage (1); the observation window (7) is made of a transparent material, and a scale mark is coated on the observation window (7).

6. The carbon fiber construction tool according to claim 1, characterized in that: A handle (8) is fixedly mounted on the lower end of the body (1).

7. The carbon fiber construction tool according to claim 1, characterized in that: The body (1) is provided with a glue injection valve (201) above the adhesive glue storage cavity (2) via a slot.

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