Automatic pressing device for rubber aviation tire belt layer

By combining heating and driving mechanisms, the problems of deviation and stress concentration in the automatic belt layer pressing device during the pressing process were solved, achieving a stable and efficient pressing effect.

CN224335141UActive Publication Date: 2026-06-09QINGDAO SENTURY TIRE CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
QINGDAO SENTURY TIRE CO LTD
Filing Date
2025-05-16
Publication Date
2026-06-09

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  • Figure CN224335141U_ABST
    Figure CN224335141U_ABST
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Abstract

This utility model relates to the technical field of aircraft tires, and in particular to an automatic pressing device for the belt layer of a rubber aircraft tire. It not only prevents the belt layer from deviating during movement and ensures the pressing effect, but also heats the belt layer and gradually increases the pressure to avoid stress concentration. The device includes a heating mechanism, a feeding mechanism, a discharging mechanism, a driving mechanism, and a pressing mechanism. The feeding mechanism is mounted on the heating mechanism and feeds the belt layer; the discharging mechanism is mounted on the heating mechanism and drives the belt layer to discharge; the driving mechanism is mounted on the discharging mechanism and drives the feeding and discharging mechanisms to rotate synchronously; and the pressing mechanism is mounted on the heating mechanism and presses the belt layer.
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Description

Technical Field

[0001] This utility model relates to the technical field of aircraft tires, and in particular to an automatic pressing device for the belt layer of a rubber aircraft tire. Background Technology

[0002] Aircraft tires are the core component of aircraft landing gear, and their design and performance are directly related to flight safety. Aircraft tires are usually made of high-strength rubber, nylon or aramid fiber, and the tire carcass structure contains multiple layers of cord to withstand high pressure and impact.

[0003] Existing automatic belt layer pressing devices, such as the one disclosed in utility model patent application number 202122622390.4, mainly include a worktable. Rotatable pressure rollers are evenly arranged inside the worktable. A telescopic rod is positioned opposite each other at the upper end of the worktable, and a support plate is positioned opposite each other at the lower end of the connecting plate. Each of the two opposing support plates has a rotatably connected adjustment device. A drive motor is mounted on the horizontal plate. In use, the belt layer pressure rollers of different sizes are first adjusted and replaced according to the width of the tire belt layer. Then, the screws rotate within the threaded holes. During rotation, both screws rotate simultaneously, driving the tire shoulder pressure roller to move closer to the tire shoulder pressure roller. A locking block is installed in a slot, and then a fixing nut is used to rotate the device closer to the rotating shaft for fixation.

[0004] However, most existing pressing devices do not position the two sides of the belt layer, making it easy for the belt layer to deviate during the pressing process. Moreover, most existing pressing devices use a single roller to press, resulting in poor pressing effect and easy stress concentration in the belt layer. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides an automatic pressing device for rubber aircraft tire belt layers that not only prevents the belt layer from deviating during movement and ensures the pressing effect of the belt layer, but also heats the belt layer and gradually increases the pressure to avoid stress concentration in the belt layer.

[0006] This utility model discloses an automatic pressing device for rubber aircraft tire belt layers, including a heating mechanism; it also includes a feeding mechanism, a discharging mechanism, a driving mechanism, and a pressing mechanism. The feeding mechanism is mounted on the heating mechanism and conveys the belt layer for feeding; the discharging mechanism is mounted on the heating mechanism and drives the belt layer for discharging; the driving mechanism is mounted on the discharging mechanism and drives the feeding and discharging mechanisms to rotate synchronously; the pressing mechanism is mounted on the heating mechanism and presses the belt layer. When the driving mechanism is activated, it drives the feeding and discharging mechanisms to rotate synchronously. The feeding and discharging mechanisms cooperate to feed the belt layer and prevent the belt layer from deviating during movement. The heating mechanism heats the belt layer and cooperates with the pressing mechanism to press the rubber aircraft tire belt layer.

[0007] Preferably, the heating mechanism includes a workbench, an insulation box, a heat-conducting plate, and a heater. The bottom end of the workbench is connected to the ground, the bottom end of the insulation box is connected to the top end of the workbench, the bottom end of the heat-conducting plate is connected to the top end of the workbench, and the heater is installed on the heat-conducting plate. The feeding mechanism, in conjunction with the unloading mechanism, transports the belt layer into the insulation box. The heater heats the pressing mechanism, and the pressing mechanism, in conjunction with the heat-conducting plate, heats and presses the belt layer to enhance the pressing effect. The insulation box reduces heat loss.

[0008] Preferably, the feeding mechanism includes two sets of feeding rollers, a first synchronous wheel, a connecting rod, two sets of sliders, two sets of fixing bolts, and two sets of first side baffles. Both sets of feeding rollers are rotatably mounted on the worktable, the first synchronous wheel is mounted on the first set of feeding rollers, the connecting rod is mounted on the worktable, both sets of sliders are slidably mounted on the connecting rod, the two sets of fixing bolts are respectively mounted on the two sets of sliders, and the two sets of first side baffles are respectively mounted on the two sets of sliders. The operator slides the two sets of sliders so that the distance between the two sets of first side baffles matches the width of the belt layer, and then rotates the two sets of fixing bolts to fix the two sets of sliders. The drive mechanism drives the first synchronous wheel to rotate, and the two sets of first synchronous wheels drive the belt layer forward.

[0009] Preferably, the feeding mechanism includes two sets of feeding rollers, a second synchronous wheel, two sets of gears, two sets of electric cylinders, and two sets of second side baffles. Both sets of feeding rollers are rotatably mounted on the worktable. The second synchronous wheel is mounted on the feeding roller located on the lower layer. The two sets of gears are respectively mounted on the two sets of feeding rollers. Both sets of electric cylinders are mounted on the heat preservation box. The two sets of second side baffles are respectively mounted on the two sets of electric cylinders. The operator slides the two sets of sliders so that the distance between the two sets of first side baffles matches the width of the belt layer. Then, the operator rotates the two sets of fixing bolts to fix the two sets of sliders. The drive mechanism drives the first synchronous wheel to rotate, and the two sets of first synchronous wheels drive the belt layer forward.

[0010] Preferably, the drive mechanism includes a motor, a reducer, a drive shaft, two sets of third synchronous pulleys, and two sets of synchronous belts. The motor and the reducer are mounted on the worktable, the drive shaft is rotatably mounted on the worktable, and both sets of third synchronous pulleys are mounted on the drive shaft. The first set of synchronous belts is tensioned between the third synchronous pulley and the first synchronous pulley, and the second set of synchronous belts is tensioned between the third synchronous pulley and the second synchronous pulley. When the motor is started, the motor drives the drive shaft to rotate through the reducer, the drive shaft drives the two sets of third synchronous pulleys to rotate, and the two sets of third synchronous pulleys drive the first synchronous pulley and the second synchronous pulley to rotate through the two sets of synchronous belts.

[0011] Preferably, the pressing mechanism includes two sets of guide columns, four sets of hydraulic cylinders, two sets of positioning sliders, four sets of belt layer pressing rollers, and four sets of tire shoulder pressing rollers. The insulation box has two sets of positioning slots, and the two sets of guide columns are respectively installed in the two sets of positioning slots. All four sets of hydraulic cylinders are installed on the insulation box. The two sets of positioning sliders are slidably installed on the two sets of positioning slots and the two sets of guide columns of the insulation box, and the top of the positioning sliders is connected to the bottom of the two sets of hydraulic cylinders on the same side. All four sets of belt layer pressing rollers are rotatably installed between the two sets of positioning sliders, and the four sets of tire shoulder pressing rollers are respectively installed on the four sets of belt layer pressing rollers. Based on the thickness of the tire belt layer, the four sets of hydraulic cylinders are activated to push the two sets of positioning sliders downwards. The two sets of guide columns ensure the smoothness of the lifting and lowering of the two sets of positioning sliders, allowing the four sets of belt layer pressing rollers and the four sets of tire shoulder pressing rollers to press the belt layer.

[0012] Preferably, it also includes four sets of belt lamination rollers with progressively larger diameters from front to back; by setting four sets of belt lamination rollers with progressively larger diameters, it is convenient to squeeze out the air bubbles in the middle, while the pressure on the belt layer gradually increases, avoiding stress concentration in the belt layer and ensuring the lamination effect.

[0013] Compared with the prior art, the beneficial effects of this utility model are as follows: the drive mechanism is started, which drives the feeding mechanism and the unloading mechanism to rotate synchronously. The feeding mechanism and the unloading mechanism work together to feed the belt layer and prevent the belt layer from deviating during movement. The heating mechanism heats the belt layer and works with the pressing mechanism to press the rubber aviation tire belt layer. Attached Figure Description

[0014] Figure 1 This is a cross-sectional axonometric structural schematic diagram of this utility model;

[0015] Figure 2 This is a cross-sectional isometric structural diagram of the heating mechanism and pressing mechanism of this utility model;

[0016] Figure 3 This is a partially enlarged isometric structural diagram of the feeding mechanism of this utility model;

[0017] Figure 4 This is an isometric structural diagram of the drive mechanism of this utility model;

[0018] Figure 5 This is a partially enlarged isometric structural diagram of the feeding mechanism of this utility model.

[0019] The attached diagram is labeled as follows: 01, heating mechanism; 11, workbench; 12, heat preservation box; 13, heat conduction plate; 14, heater; 02, feeding mechanism; 21, feeding roller; 22, first synchronous pulley; 23, connecting rod; 24, slider; 25, fixing bolt; 26, first side baffle; 03, unloading mechanism; 31, unloading roller; 32, second synchronous pulley; 33, gear; 34, electric cylinder; 35, second side baffle; 04, drive mechanism; 41, electric motor; 42, reducer; 43, transmission shaft; 44, third synchronous pulley; 45, synchronous belt; 05, pressing mechanism; 51, guide column; 52, hydraulic cylinder; 53, positioning slider; 54, belt lamination pressing roller; 55, tire shoulder pressing roller. Detailed Implementation

[0020] 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.

[0021] Example 1

[0022] This utility model discloses an automatic pressing device for rubber aircraft tire belt layers, including a heating mechanism 01; it also includes a feeding mechanism 02, a discharging mechanism 03, a driving mechanism 04, and a pressing mechanism 05. The feeding mechanism 02 is mounted on the heating mechanism 01 and conveys the belt layer for feeding; the discharging mechanism 03 is mounted on the heating mechanism 01 and drives the belt layer for discharging; the driving mechanism 04 is mounted on the discharging mechanism 03 and drives the feeding mechanism 02 and the discharging mechanism 03 to rotate synchronously; the pressing mechanism 05 is mounted on the heating mechanism 01 and presses the belt layer. The heating mechanism 01 includes a worktable 11 and a holding device. The workbench 11 has a heat exchange box 12, a heat-conducting plate 13, and a heater 14. The bottom end of the workbench 11 is connected to the ground, the bottom end of the heat exchange box 12 is connected to the top end of the workbench 11, the bottom end of the heat-conducting plate 13 is connected to the top end of the workbench 11, and the heater 14 is mounted on the heat-conducting plate 13. The feeding mechanism 02 includes two sets of feeding rollers 21, a first synchronous wheel 22, a connecting rod 23, two sets of sliders 24, two sets of fixing bolts 25, and two sets of first side baffles 26. Both sets of feeding rollers 21 are rotatably mounted on the workbench 11, the first synchronous wheel 22 is mounted on the first set of feeding rollers 21, and the connecting rod 23 is mounted on the workbench 11. On the worktable 11, two sets of sliders 24 are slidably mounted on the connecting rod 23, two sets of fixing bolts 25 are respectively mounted on the two sets of sliders 24, and two sets of first side baffles 26 are respectively mounted on the two sets of sliders 24; the feeding mechanism 03 includes two sets of feeding rollers 31, a second synchronous wheel 32, two sets of gears 33, two sets of electric cylinders 34, and two sets of second side baffles 35. The two sets of feeding rollers 31 are rotatably mounted on the worktable 11, the second synchronous wheel 32 is mounted on the feeding roller 31 located on the lower layer, the two sets of gears 33 are respectively mounted on the two sets of feeding rollers 31, and the two sets of electric cylinders 34 are both mounted on the heat preservation box 12. The second side baffle 35 is respectively installed on the two sets of electric cylinders 34; the drive mechanism 04 includes a motor 41, a reducer 42, a transmission shaft 43, two sets of third synchronous pulleys 44 and two sets of synchronous belts 45. The motor 41 is installed on the workbench 11, the reducer 42 is installed on the workbench 11, the transmission shaft 43 is rotatably installed on the workbench 11, both sets of third synchronous pulleys 44 are installed on the transmission shaft 43, the first set of synchronous belts 45 is tensioned and installed between the third synchronous pulley 44 and the first synchronous pulley 22, and the second set of synchronous belts 45 is tensioned and installed between the third synchronous pulley 44 and the second synchronous pulley 32.During operation, the operator first slides two sets of sliders 24 to align the spacing of the two sets of first side baffles 26 with the width of the belt layer. Then, the operator rotates two sets of fixing bolts 25 to secure the two sets of sliders 24. The operator then activates two sets of electric cylinders 34 to adjust the spacing of the two sets of second side baffles 35, ensuring the spacing matches the width of the belt layer and preventing it from shifting during transport. The operator then starts the motor 41, which drives the drive shaft 43 to rotate via the reducer 42. The drive shaft 43 drives the two sets of third synchronous pulleys 44 to rotate, and the two sets of third synchronous pulleys 44 drive the first synchronous belts 45 to rotate via the two sets of synchronous belts 45. A synchronous pulley 22 and a second synchronous pulley 32 rotate, and a synchronous belt 45 drives the first synchronous pulley 22 to rotate. The two sets of first synchronous pulleys 22 drive the belt layer forward. A heater 14 heats the pressing mechanism 05, which, in conjunction with a heat-conducting plate 13, heats and presses the belt layer to enhance the pressing effect. A heat preservation box 12 is set to reduce heat loss. The synchronous belt 45 drives the second synchronous pulley 32 to rotate, and the second synchronous pulley 32 drives the lower feed roller 31 to rotate. Two sets of gears 33 mesh and drive the transmission, thereby causing the two sets of feed rollers 31 to rotate synchronously and drive the pressed belt layer forward.

[0023] Example 2

[0024] like Figures 1 to 5As shown, this utility model discloses an automatic pressing device for rubber aircraft tire belt layers, based on Embodiment 1. The pressing mechanism 05 includes two sets of guide columns 51, four sets of hydraulic cylinders 52, two sets of positioning sliders 53, four sets of belt layer pressing rollers 54, and four sets of tire shoulder pressing rollers 55. The insulation box 12 has two sets of positioning grooves, and the two sets of guide columns 51 are respectively installed in the two sets of positioning grooves. All four sets of hydraulic cylinders 52 are installed on the insulation box 12. The two sets of positioning sliders 53 are respectively slidably installed on the two sets of positioning grooves and the two sets of guide columns 51 of the insulation box 12, and the top of the positioning sliders 53 is aligned with the two sets of hydraulic cylinders 54 on the same side. The bottom of the 2 is connected, and four sets of belt laminating rollers 54 are rotatably installed between two sets of positioning sliders 53. Four sets of shoulder laminating rollers 55 are respectively installed on the four sets of belt laminating rollers 54. The diameter of the four sets of belt laminating rollers 54 increases from front to back. When it is working, firstly, the operator slides two sets of sliders 24 so that the distance between the two sets of first side baffles 26 matches the width of the belt layer. Then, the two sets of fixing bolts 25 are rotated to fix the two sets of sliders 24. The two sets of electric cylinders 34 are activated to adjust the distance between the two sets of second side baffles 35 so that the distance between the two sets of second side baffles 35 matches the width of the belt layer, avoiding belt layer If the conveying process deviates, the motor 41 is started. The motor 41 drives the transmission shaft 43 to rotate via the reducer 42. The transmission shaft 43 drives the two sets of third synchronous pulleys 44 to rotate. The two sets of third synchronous pulleys 44 drive the first synchronous pulley 22 and the second synchronous pulley 32 to rotate via the two sets of synchronous belts 45. The synchronous belts 45 drive the first synchronous pulley 22 to rotate. The two sets of first synchronous pulleys 22 drive the belt layer forward. The heater 14 heats the four sets of belt layer pressing rollers 54. According to the thickness of the tire belt layer, the four sets of hydraulic cylinders 52 are activated to push the two sets of positioning sliders 53 downward. The two sets of guide columns 51 are used to ensure that the two sets of positioning sliders 53 are lowered. The smooth lifting and lowering of the positioning slider 53 enables the four sets of belt layer pressing rollers 54 and four sets of tire shoulder pressing rollers 55 to press the belt layer. By setting four sets of belt layer pressing rollers 54 with increasingly larger diameters, it is convenient to squeeze out the air bubbles in the middle. At the same time, the pressure on the belt layer gradually increases to avoid stress concentration in the belt layer and ensure the pressing effect. The heat preservation box 12 reduces heat loss. The synchronous belt 45 drives the second synchronous wheel 32 to rotate, and the second synchronous wheel 32 drives the lower feeding roller 31 to rotate. The two sets of gears 33 mesh and drive, thereby making the two sets of feeding rollers 31 rotate synchronously and drive the pressed belt layer forward.

[0025] The electric motor 41 and the reducer 42 of this utility model are commercially available. 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.

[0026] 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 automatic pressing device for rubber aircraft tire belt layers, comprising a heating mechanism (01); characterized in that, It also includes a feeding mechanism (02), a discharging mechanism (03), a driving mechanism (04), and a pressing mechanism (05). The feeding mechanism (02) is installed on the heating mechanism (01) and feeds the belt layer. The discharging mechanism (03) is installed on the heating mechanism (01) and drives the belt layer to discharge. The driving mechanism (04) is installed on the discharging mechanism (03) and drives the feeding mechanism (02) and the discharging mechanism (03) to rotate synchronously. The pressing mechanism (05) is installed on the heating mechanism (01) and presses the belt layer.

2. The automatic pressing device for rubber aircraft tire belt layers as described in claim 1, characterized in that, The heating mechanism (01) includes a workbench (11), an insulation box (12), a heat-conducting plate (13), and a heater (14). The bottom end of the workbench (11) is connected to the ground, the bottom end of the insulation box (12) is connected to the top end of the workbench (11), the bottom end of the heat-conducting plate (13) is connected to the top end of the workbench (11), and the heater (14) is installed on the heat-conducting plate (13).

3. The automatic pressing device for rubber aircraft tire belt layers as described in claim 2, characterized in that, The feeding mechanism (02) includes two sets of feeding rollers (21), a first synchronous wheel (22), a connecting rod (23), two sets of sliders (24), two sets of fixing bolts (25), and two sets of first side baffles (26). The two sets of feeding rollers (21) are rotatably mounted on the worktable (11). The first synchronous wheel (22) is mounted on the first set of feeding rollers (21). The connecting rod (23) is mounted on the worktable (11). The two sets of sliders (24) are slidably mounted on the connecting rod (23). The two sets of fixing bolts (25) are respectively mounted on the two sets of sliders (24). The two sets of first side baffles (26) are respectively mounted on the two sets of sliders (24).

4. The automatic pressing device for rubber aircraft tire belt layers as described in claim 2, characterized in that, The feeding mechanism (03) includes two sets of feeding rollers (31), a second synchronous wheel (32), two sets of gears (33), two sets of electric cylinders (34) and two sets of second side baffles (35). The two sets of feeding rollers (31) are rotatably mounted on the worktable (11). The second synchronous wheel (32) is mounted on the feeding roller (31) located on the lower layer. The two sets of gears (33) are respectively mounted on the two sets of feeding rollers (31). The two sets of electric cylinders (34) are both mounted on the heat preservation box (12). The two sets of second side baffles (35) are respectively mounted on the two sets of electric cylinders (34).

5. The automatic pressing device for rubber aircraft tire belt layers as described in claim 4, characterized in that, The drive mechanism (04) includes a motor (41), a reducer (42), a transmission shaft (43), two sets of third synchronous pulleys (44) and two sets of synchronous belts (45). The motor (41) is mounted on the workbench (11), the reducer (42) is mounted on the workbench (11), the transmission shaft (43) is rotatably mounted on the workbench (11), both sets of third synchronous pulleys (44) are mounted on the transmission shaft (43), the first set of synchronous belts (45) is tensioned between the third synchronous pulley (44) and the first synchronous pulley (22), and the second set of synchronous belts (45) is tensioned between the third synchronous pulley (44) and the second synchronous pulley (32).

6. The automatic pressing device for rubber aircraft tire belt layers as described in claim 2, characterized in that, The pressing mechanism (05) includes two sets of guide columns (51), four sets of hydraulic cylinders (52), two sets of positioning sliders (53), four sets of belt lamination rollers (54) and four sets of tire shoulder pressing rollers (55). The insulation box (12) has two sets of positioning grooves. The two sets of guide columns (51) are respectively installed in the two sets of positioning grooves. The four sets of hydraulic cylinders (52) are all installed on the insulation box (12). The two sets of positioning sliders (53) are respectively slidably installed on the two sets of positioning grooves and the two sets of guide columns (51) of the insulation box (12). The top of the positioning slider (53) is connected to the bottom of the two sets of hydraulic cylinders (52) on the same side. The four sets of belt lamination rollers (54) are rotatably installed between the two sets of positioning sliders (53). The four sets of tire shoulder pressing rollers (55) are respectively installed on the four sets of belt lamination rollers (54).

7. The automatic pressing device for rubber aircraft tire belt layers as described in claim 6, characterized in that, It also includes four sets of belt laminating rollers (54) with increasing diameter from front to back.