Aircraft tire carcass steel wire winding device

Abstract

The utility model relates to the technical field of aviation tire production especially is aviation tire body steel wire winding device, it can be through cleaning mechanism in advance with the dust of steel wire surface clean when winding and sticking steel wire to aviation tire surface, so guarantee the firmness of steel wire in aviation tire surface sticking winding, convenient to use, reliability and practicality are high, including bottom plate, still including support board, guide roller, gumming mechanism, moving mechanism, winding mechanism and cleaning mechanism, support board fixed mounting is in bottom plate, guide roller rotary installation is in support board, gumming mechanism installs in bottom plate, gumming mechanism has the function that glues, moving mechanism installs in bottom plate, winding mechanism and cleaning mechanism all install in bottom plate, cleaning mechanism is used for with tire cleaning, winding mechanism is used for to tire rotation.

Description

Technical Field

[0001] This utility model relates to the technical field of aircraft tire production, and in particular to an aircraft tire carcass steel wire winding device. Background Technology

[0002] To meet the high-strength load requirements of aircraft takeoff and landing, steel wires are wound around the tire carcass during the manufacturing process of aircraft tires, improving the carcass's performance. In the prior art, utility model patent application number 201120384666.3 discloses a steel wire winding device for tire retreading, which uses adhesive padding to fix and bond the steel wires to the tire during winding. However, this device has the following problems in use: due to the inevitable accumulation of dust on the tire carcass surface during production and manufacturing, this dust affects the adhesion of the steel wires to the tire surface, resulting in inconvenience and poor reliability. Utility Model Content

[0003] To solve the above-mentioned technical problems, this utility model provides an aircraft tire carcass steel wire winding device that can clean the dust on the surface of the steel wire in advance by a cleaning mechanism when winding and bonding steel wire to the surface of the aircraft tire, thus ensuring the firmness of the steel wire bonding and winding on the surface of the aircraft tire. It is convenient to use, reliable and practical.

[0004] This utility model discloses a steel wire winding device for aircraft tires, comprising a base plate, a support plate, a guide roller, a glue application mechanism, a moving mechanism, a winding mechanism, and a cleaning mechanism. The support plate is fixedly mounted on the base plate, the guide roller is rotatably mounted on the support plate, the glue application mechanism is mounted on the base plate and has a glue application function, the moving mechanism is mounted on the base plate, and both the winding mechanism and the cleaning mechanism are mounted on the base plate. The cleaning mechanism is used for cleaning the tire, and the winding mechanism is used for rotating the tire. When steel wire needs to be wound onto the surface of an aircraft tire, the aircraft tire is first clamped and fixed by the winding mechanism, then the dust on the surface of the aircraft tire is cleaned by the cleaning mechanism, and the steel wire is sequentially passed through the guide roller, the glue application mechanism, and the moving mechanism before being fixed to the aircraft tire wheel. The process involves rotating the aircraft tire via a winding mechanism, causing steel wires to wrap around its surface. As the wires pass through an adhesive applicator, adhesive is applied to their surface. Then, a moving mechanism moves the wires back and forth, ensuring they are evenly wrapped around the tire. Once the wires are wrapped, they are cut, and the aircraft tire can be removed. Because a cleaning mechanism removes dust from the wires before wrapping, the adhesion and wrapping are strong, making the process convenient, reliable, and practical.

[0005] Preferably, the glue application mechanism includes a glue storage tank, a vertical plate, a motor A, and a glue application roller. The glue storage tank is fixedly installed on the base plate and has a chamber inside. The upper end of the glue storage tank is open. The vertical plate is fixedly installed on the base plate, and the motor A is fixedly installed on the vertical plate. The glue application roller is rotatably installed on the vertical plate, and the power output end of the motor A is connected to the front end of the glue application roller. When the motor A is turned on, the motor A drives the glue application roller to rotate. Since the glue storage tank contains glue, the glue application roller transfers the glue from the storage tank to its surface during rotation. When the steel wire passes over the surface of the glue application roller, the glue on the surface of the roller is transferred to the surface of the steel wire, which facilitates the bonding and fixing of the steel wire to the aircraft tire and improves convenience.

[0006] Preferably, the moving mechanism includes an electric slide rail, a sliding plate, a first fixed plate, and a roller. The electric slide rail is mounted on the base plate, and the sliding plate is provided on the electric slide rail. The electric slide rail is used to move the sliding plate back and forth. The first fixed plate is fixedly mounted on the upper end of the sliding plate, and the roller is rotatably mounted on the first fixed plate. Baffles are provided at the front and rear ends of the roller. After the steel wire is coated with glue, the steel wire passes through the roller and is wound around the aircraft tire. When the electric slide rail is opened, the electric slide rail drives the sliding plate to move back and forth. The sliding plate, through the first fixed plate, causes the roller to drive the steel wire to move back and forth, so that the steel wire is wound around the surface of the aircraft tire during the back and forth movement, and the steel wire can be evenly wound around the front and rear ends of the aircraft tire.

[0007] Preferably, the winding mechanism includes a second fixed plate, a drive motor, and an inner support chuck. The drive motor is fixedly mounted on the second fixed plate, and a rotating shaft is provided at the output end of the drive motor. The rotating shaft is rotatably mounted on the second fixed plate, and the inner support chuck is fixedly mounted on the rotating shaft. The aircraft tire is fixed by the inner support chuck, so that one end of the steel wire is fixedly bonded to the aircraft tire. Then, the drive motor is turned on, and the drive motor winds the steel wire around the surface of the aircraft tire through the inner support chuck. This facilitates the winding of steel wire on the surface of the aircraft tire.

[0008] Preferably, the cleaning mechanism includes a support plate, a hydraulic cylinder, a push rod, a fixed frame, and a dust-adhesive roller. The support plate is fixedly mounted on the base plate, the hydraulic cylinder is fixedly mounted on the support plate, the push rod is slidably mounted on the support plate, the right end of the push rod is connected to the output end of the hydraulic cylinder, the fixed frame is fixedly mounted on the left end of the push rod, and the dust-adhesive roller is rotatably mounted on the fixed frame. Before wrapping steel wire around the surface of the aircraft tire, the hydraulic cylinder is first opened. The hydraulic cylinder, through the push rod, causes the fixed frame to move the dust-adhesive roller to the left, so that the dust-adhesive roller contacts the surface of the aircraft tire. Then, the aircraft tire is rotated. During the rotation of the aircraft tire, the dust-adhesive roller evenly adheres the dust off the surface of the aircraft tire, which facilitates the cleaning of the aircraft tire surface.

[0009] Preferably, the assembly also includes a lifting frame, a servo cylinder, a lifting rod, a mounting frame, and a pressure roller. The servo cylinder is fixedly installed on the upper end of the lifting frame, the lifting rod is slidably installed on the lifting frame, the upper end of the lifting rod is connected to the output end of the servo cylinder, the mounting frame is fixedly installed on the lower end of the lifting rod, and the pressure roller is rotatably installed on the mounting frame. The lifting frame is fixedly suspended on a support in the workshop. When bonding and winding the steel wire onto the aircraft tire, the servo cylinder is activated. The servo cylinder, through the lifting rod, causes the mounting frame to drive the pressure roller to descend, making the pressure roller contact the steel wire on the aircraft tire. The pressure roller presses the steel wire tightly onto the aircraft tire, making the bond between the steel wire and the aircraft tire more secure.

[0010] Preferably, the surface of the roller is provided with a rubber layer; this arrangement reduces the scratches on the steel wire by the roller and improves reliability.

[0011] Compared with the prior art, the beneficial effects of this utility model are as follows: when wrapping and bonding steel wires to the surface of aircraft tires, the dust on the surface of the steel wires can be cleaned in advance by the cleaning mechanism, thus ensuring the firmness of the steel wires on the surface of aircraft tires. It is convenient to use and has high reliability and practicality. Attached Figure Description

[0012] Figure 1 This is a schematic diagram of the first isometric structure of this utility model;

[0013] Figure 2 This is a schematic diagram of the second isometric structure of this utility model;

[0014] Figure 3 It is a structural diagram of the internal support chuck, lifting frame, and pressure roller, etc.

[0015] Figure 4 It is a structural diagram of electric slide rails, sliding plates, and rollers, etc.

[0016] Figure 5 It is a structural diagram of the glue storage tank, glue application roller, and vertical plate, etc.

[0017] Figure 6 This is a structural diagram of the cleaning system.

[0018] The following components are labeled in the attached diagram: 1. Base plate; 2. Support plate; 3. Guide roller; 4. Glue storage tank; 5. Vertical plate; 6. Motor A; 7. Glue application roller; 8. Electric slide rail; 9. Sliding plate; 10. First fixed plate; 11. Roller; 12. Second fixed plate; 13. Drive motor; 14. Inner support chuck; 15. Support plate; 16. Hydraulic cylinder; 17. Push rod; 18. Fixed frame; 19. Adhesive roller; 20. Lifting frame; 21. Servo electric cylinder; 22. Lifting rod; 23. Mounting frame; 24. Pressure roller; 25. Aviation tire; 26. Steel wire. Detailed Implementation

[0019] To facilitate understanding of this utility model, a more complete description will be given below with reference to the accompanying drawings. This utility model can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to make the disclosure of this utility model more thorough and complete.

[0020] Example 1

[0021] like Figures 1 to 6 The aircraft tire carcass steel wire winding device of this utility model includes a base plate 1, a support plate 2, a guide roller 3, an adhesive application mechanism, a moving mechanism, a winding mechanism, and a cleaning mechanism. The support plate 2 is fixedly installed on the base plate 1, the guide roller 3 is rotatably installed on the support plate 2, the adhesive application mechanism is installed on the base plate 1, and the adhesive application mechanism has the function of applying adhesive. The moving mechanism is installed on the base plate 1, and the winding mechanism and the cleaning mechanism are both installed on the base plate 1. The cleaning mechanism is used for cleaning the tire, and the winding mechanism is used for rotating the tire. When it is necessary to wind steel wire onto the surface of the aircraft tire 25, the aircraft tire 25 is first clamped and fixed by the winding mechanism, and then the dust on the surface of the aircraft tire 25 is cleaned by the cleaning mechanism. The steel wire 26 is then passed through the guide roller 3, the adhesive application mechanism, and the moving mechanism in sequence onto the aircraft tire 25 fixed thereon, while the winding mechanism... The aircraft tire 25 is rotated, causing the steel wire 26 to wrap around its surface. As the steel wire 26 passes through the adhesive applicator, adhesive is applied to its surface. Then, as the steel wire 26 passes through the moving mechanism, it is moved back and forth, ensuring it wraps evenly around the aircraft tire 25. Once the steel wire is wrapped around the aircraft tire 25, it is cut, and the aircraft tire 25 can be removed. Because the cleaning mechanism cleans the surface of the steel wire 26 beforehand, the adhesion and wrapping of the steel wire 26 to the aircraft tire 25 is ensured, resulting in a strong bond. This method is convenient, reliable, and practical.

[0022] like Figure 1 , Figure 2 and Figure 5The glue application mechanism includes a glue storage tank 4, a vertical plate 5, a motor A6, and a glue application roller 7. The glue storage tank 4 is fixedly installed on the base plate 1 and has a chamber inside. The upper end of the glue storage tank 4 is open. The vertical plate 5 is fixedly installed on the base plate 1, the motor A6 is fixedly installed on the vertical plate 5, and the glue application roller 7 is rotatably installed on the vertical plate 5. The power output end of the motor A6 is connected to the front end of the glue application roller 7. When the motor A6 is turned on, the motor A6 drives the glue application roller 7 to rotate. Since the glue storage tank 4 stores glue, the glue application roller 7 transfers the glue from the glue storage tank 4 to the glue application roller 7 during rotation. When the steel wire 26 passes over the surface of the glue application roller 7, the glue on the surface of the glue application roller 7 is transferred to the surface of the steel wire 26, which facilitates the bonding and fixing of the steel wire 26 to the aircraft tire 25 and improves convenience.

[0023] like Figure 1 and Figure 4 The moving mechanism includes an electric slide rail 8, a sliding plate 9, a first fixed plate 10, and a roller 11. The electric slide rail 8 is mounted on the base plate 1, and the sliding plate 9 is provided on the electric slide rail 8. The electric slide rail 8 is used to move the sliding plate 9 back and forth. The first fixed plate 10 is fixedly mounted on the upper end of the sliding plate 9, and the roller 11 is rotatably mounted on the first fixed plate 10. Baffles are provided at the front and rear ends of the roller 11. After the steel wire 26 is coated with glue, the steel wire 26 passes through the roller 11 and is wound around the aircraft tire 25. When the electric slide rail 8 is opened, the electric slide rail 8 drives the sliding plate 9 to move back and forth. The sliding plate 9, through the first fixed plate 10, causes the roller 11 to drive the steel wire 26 to move back and forth, so that the steel wire 26 is wound around the surface of the aircraft tire 25 during the back and forth movement, so that the steel wire 26 can be evenly wound around the front and rear ends of the aircraft tire 25.

[0024] like Figure 1 and Figure 3 The winding mechanism includes a second fixed plate 12, a drive motor 13, and an inner support chuck 14. The drive motor 13 is fixedly mounted on the second fixed plate 12, and a rotating shaft is provided at the output end of the drive motor 13. The rotating shaft is rotatably mounted on the second fixed plate 12, and the inner support chuck 14 is fixedly mounted on the rotating shaft. The aircraft tire 25 is fixed by the inner support chuck 14, so that one end of the steel wire 26 is fixedly bonded to the aircraft tire 25. Then, the drive motor 13 is turned on, and the drive motor 13 winds the steel wire 26 around the surface of the aircraft tire 25 through the inner support chuck 14. This facilitates the winding of steel wire on the surface of the aircraft tire 25.

[0025] like Figure 1 , Figure 3 and Figure 6The cleaning mechanism includes a support plate 15, a hydraulic cylinder 16, a push rod 17, a fixed frame 18, and a dust-adhesive roller 19. The support plate 15 is fixedly installed on the base plate 1, the hydraulic cylinder 16 is fixedly installed on the support plate 15, the push rod 17 is slidably installed on the support plate 15, the right end of the push rod 17 is connected to the output end of the hydraulic cylinder 16, the fixed frame 18 is fixedly installed on the left end of the push rod 17, and the dust-adhesive roller 19 is rotatably installed on the fixed frame 18. Before wrapping steel wire around the surface of the aircraft tire 25, the hydraulic cylinder 16 is first opened. The hydraulic cylinder 16, through the push rod 17, causes the fixed frame 18 to move the dust-adhesive roller 19 to the left, so that the dust-adhesive roller 19 contacts the surface of the aircraft tire 25. Then, the aircraft tire 25 is rotated. During the rotation, the dust-adhesive roller 19 evenly adheres the dust off the surface of the aircraft tire 25, which facilitates the cleaning of the surface of the aircraft tire 25.

[0026] like Figure 1 and Figure 3 It also includes a hoisting frame 20, a servo cylinder 21, a lifting rod 22, a mounting frame 23, and a pressure roller 24. The servo cylinder 21 is fixedly installed on the upper end of the hoisting frame 20. The lifting rod 22 is slidably installed on the hoisting frame 20, and the upper end of the lifting rod 22 is connected to the output end of the servo cylinder 21. The mounting frame 23 is fixedly installed on the lower end of the lifting rod 22, and the pressure roller 24 is rotatably installed on the mounting frame 23. The hoisting frame 20 is fixedly hoisted on the workshop support frame. When bonding and winding the steel wire 26 onto the aircraft tire 25, the servo cylinder 21 is opened. The servo cylinder 21 causes the mounting frame 23 to drive the pressure roller 24 to descend through the lifting rod 22, so that the pressure roller 24 contacts the steel wire 26 on the aircraft tire 25. The pressure roller 24 presses the steel wire 26 tightly onto the aircraft tire 25, making the bond between the steel wire 26 and the aircraft tire 25 more secure.

[0027] Example 2

[0028] Based on Embodiment 1, a rubber layer is provided on the surface of the roller 11; through the above provision, the scratches on the steel wire 26 by the roller 11 are reduced, and the reliability is improved.

[0029] The coating roller 7, electric slide rail 8, drive motor 13, inner support chuck 14, dust sticking roller 19, and servo electric cylinder 21 of the aviation tire carcass steel wire winding device of this utility model are all purchased from the market. Technical personnel in this industry only need to install and operate them according to the accompanying instruction manual, without requiring any creative work from those skilled in the art.

[0030] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.

Claims

1. An aircraft tire carcass steel wire winding device, comprising a base plate (1); characterized in that, It also includes a support plate (2), a guide roller (3), an adhesive application mechanism, a moving mechanism, a winding mechanism, and a cleaning mechanism. The support plate (2) is fixedly installed on the base plate (1), the guide roller (3) is rotatably installed on the support plate (2), the adhesive application mechanism is installed on the base plate (1), the adhesive application mechanism has the function of applying adhesive, the moving mechanism is installed on the base plate (1), and the winding mechanism and the cleaning mechanism are both installed on the base plate (1). The cleaning mechanism is used to clean the tire, and the winding mechanism is used to rotate the tire.

2. The aircraft tire carcass steel wire winding device as described in claim 1, characterized in that, The glue application mechanism includes a glue storage tank (4), a vertical plate (5), a motor A (6), and a glue application roller (7). The glue storage tank (4) is fixedly installed on the base plate (1). The glue storage tank (4) has a chamber inside and the upper end of the glue storage tank (4) is open. The vertical plate (5) is fixedly installed on the base plate (1). The motor A (6) is fixedly installed on the vertical plate (5). The glue application roller (7) is rotatably installed on the vertical plate (5). The power output end of the motor A (6) is connected to the front end of the glue application roller (7).

3. The aircraft tire carcass steel wire winding device as described in claim 1, characterized in that, The moving mechanism includes an electric slide rail (8), a sliding plate (9), a first fixed plate (10), and a roller (11). The electric slide rail (8) is mounted on the base plate (1), and the sliding plate (9) is provided on the electric slide rail (8). The electric slide rail (8) is used to move the sliding plate (9) back and forth. The first fixed plate (10) is fixedly mounted on the upper end of the sliding plate (9), and the roller (11) is rotatably mounted on the first fixed plate (10). Baffles are provided on the front and rear parts of the roller (11).

4. The aircraft tire carcass steel wire winding device as described in claim 1, characterized in that, The winding mechanism includes a second fixed plate (12), a drive motor (13) and an inner support chuck (14). The drive motor (13) is fixedly installed on the second fixed plate (12). The output end of the drive motor (13) is provided with a rotating shaft, which is rotatably installed on the second fixed plate (12). The inner support chuck (14) is fixedly installed on the rotating shaft.

5. The aircraft tire carcass steel wire winding device as described in claim 1, characterized in that, The cleaning mechanism includes a support plate (15), a hydraulic cylinder (16), a push rod (17), a fixed frame (18), and a dust roller (19). The support plate (15) is fixedly installed on the base plate (1), the hydraulic cylinder (16) is fixedly installed on the support plate (15), the push rod (17) is slidably installed on the support plate (15), the right end of the push rod (17) is connected to the output end of the hydraulic cylinder (16), the fixed frame (18) is fixedly installed on the left end of the push rod (17), and the dust roller (19) is rotatably installed on the fixed frame (18).

6. The aircraft tire carcass steel wire winding device as described in claim 1, characterized in that, It also includes a hoisting frame (20), a servo electric cylinder (21), a lifting rod (22), a mounting frame (23), and a pressure roller (24). The servo electric cylinder (21) is fixedly installed on the upper end of the hoisting frame (20). The lifting rod (22) slides up and down on the hoisting frame (20). The upper end of the lifting rod (22) is connected to the output end of the servo electric cylinder (21). The mounting frame (23) is fixedly installed on the lower end of the lifting rod (22). The pressure roller (24) is rotatably installed on the mounting frame (23).

7. The aircraft tire carcass steel wire winding device as described in claim 3, characterized in that, The surface of the roller (11) is provided with a rubber layer.

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