Aircraft tire tread pattern press cooling and setting device

Abstract

The utility model relates to the technical field of aviation tire tread pattern press fit cooling and shaping, particularly relates to an aviation tire tread pattern press fit cooling and shaping device, which is characterized in that a supporting mechanism and a sealing mechanism are arranged, so that the material can be cooled simultaneously from inside and outside during the aviation tire tread pattern press fit cooling and shaping process, the material is evenly cooled, and the processing efficiency is improved, the utility model discloses a supporting mechanism, and further includes a sealing mechanism, a filtering mechanism, a cooling mechanism and a discharging mechanism, the sealing mechanism is installed on the upper end of the supporting mechanism, the filtering mechanism is installed on the upper end of the supporting mechanism, the cooling mechanism is installed on the left end of the filtering mechanism, and the discharging mechanism is installed on the upper end of the supporting mechanism, the supporting mechanism supports, the sealing mechanism seals, the filtering mechanism filters, the cooling mechanism cools, and the discharging mechanism discharges.

Description

Technical Field

[0001] This utility model relates to the technical field of pressing, cooling and shaping of aircraft tire tread patterns, and in particular to an aircraft tire tread pattern pressing, cooling and shaping device. Background Technology

[0002] Tires are rubber parts used on various vehicles or machinery. They are essential for vehicle operation because they can roll on the ground. Tires have a strong load-bearing capacity and cushioning properties. They can support the entire weight of the vehicle and ensure adhesion between the wheels and the ground.

[0003] In existing aviation tire tread pattern pressing, cooling, and shaping devices, such as the shaping mold for rubber tire production disclosed in utility model patent application number 202322933523.9, the lifting and demolding mechanism of this utility model uses a starter motor as a power source to drive a screw to rotate. The screw drives a lifting sleeve structure to move up and down. When the lifting sleeve structure rises, it removes the tire from the lower shaping mold. Subsequently, the left and right electric push rods in the secondary lifting and demolding structure are controlled to rise synchronously. The upper extension of the electric push rods lifts the tire again, so that the bottom surface of the tire is separated from the demolding top plate on the lifting sleeve structure. This reduces the contact area between the bottom surface of the tire and the support, reduces adhesion, makes it easier to remove the tire, and reduces the difficulty of operation for workers.

[0004] However, during the pressing, cooling and shaping process of aircraft tire tread patterns, it is impossible to cool the material evenly, resulting in uneven temperature inside and outside the material and reducing processing quality. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides an aircraft tire tread pattern pressing, cooling and shaping device that, by setting a support mechanism and a closing mechanism, allows for simultaneous cooling of the material inside and outside during the pressing, cooling and shaping process of aircraft tire tread patterns, resulting in uniform cooling of the material and improved processing efficiency.

[0006] This utility model discloses an aircraft tire tread pattern pressing, cooling and shaping device, which includes a support mechanism; it also includes a sealing mechanism, a filtering mechanism, a cooling mechanism and a discharge mechanism. The sealing mechanism is installed on the upper end of the support mechanism, the filtering mechanism is installed on the upper end of the support mechanism, the cooling mechanism is installed on the left end of the filtering mechanism, and the discharge mechanism is installed on the upper end of the support mechanism. The supporting mechanism performs supporting, the closing mechanism performs closing, the filtering mechanism performs filtering, the cooling mechanism performs cooling, and the discharging mechanism performs discharging; the material is supported and placed by the supporting mechanism, the material is closed by the closing mechanism, cooling is performed by turning on the cooling mechanism, filtering is performed by the filtering mechanism, and discharging is performed by turning on the discharging mechanism, so that in the press-fit cooling and shaping process of the tread pattern of an aviation tire, the inside and outside of the material can be cooled simultaneously, so that the material is cooled uniformly, and the processing efficiency is improved.

[0007] Preferably, the supporting mechanism comprises a bottom plate, a bottom mold and a ventilation cover, the bottom mold is mounted at an upper end of the bottom plate, and the ventilation cover is mounted at a lower end of the bottom mold; the material is supported by the bottom mold, and ventilation and temperature reduction are performed through the ventilation cover.

[0008] Preferably, the closing mechanism comprises an upper mold, an exhaust hood and four sets of screws, the upper mold is mounted on the bottom mold through the four sets of screws, and the exhaust hood is mounted at an upper end of the upper mold; the material is closed by the upper mold, and exhaust is performed through the exhaust hood.

[0009] Preferably, the filtering mechanism comprises an air inlet box and a filter screen, the air inlet box is mounted at an upper end of the bottom plate, and the filter screen is slidably mounted on the air inlet box; air is fed through the air inlet box, and the entering air is filtered through the filter screen.

[0010] Preferably, the cooling mechanism comprises a fan and an air inlet pipe, the fan is mounted at a left end of the air inlet box, an input end of the air inlet pipe is connected with an output end of the fan, and an output end of the air inlet box extends into the ventilation cover; the fan is turned on to blow air into the ventilation cover through the air inlet pipe so as to cool the material.

[0011] Preferably, the discharging mechanism comprises a lifting cylinder and a supporting plate, the lifting cylinder is mounted at an upper end of the bottom plate, and the supporting plate is mounted at an upper end of the lifting cylinder; the lifting cylinder is turned on to drive the supporting plate, so that the supporting plate lifts to discharge the material.

[0012] Compared with the prior art, the beneficial effects of the present utility model are as follows: the material is supported and placed by the supporting mechanism, the material is closed by the closing mechanism, cooling is performed by turning on the cooling mechanism, filtering is performed by the filtering mechanism, and discharging is performed by turning on the discharging mechanism, so that in the press-fit cooling and shaping process of the tread pattern of an aviation tire, the inside and outside of the material can be cooled simultaneously, so that the material is cooled uniformly, and the processing efficiency is improved. Description of Drawings

[0013] Figure 1 is an axonometric structural schematic diagram of the present utility model; Figure 2 is a left-view sectional axonometric structural schematic diagram of the present utility model; Figure 3 is a front-view sectional axonometric structural schematic diagram of the present utility model; The following are labels in the attached diagram: 1. Support mechanism; 11. Base plate; 12. Bottom mold; 13. Ventilation hood; 2. Sealing mechanism; 21. Upper mold; 22. Exhaust hood; 23. Screw; 3. Filtering mechanism; 31. Air inlet box; 32. Filter screen; 4. Cooling mechanism; 41. Fan; 42. Air inlet pipe; 5. Discharge mechanism; 51. Lifting cylinder; 52. Pallet. Detailed Implementation

[0014] 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. Example 1

[0015] like Figures 1 to 3 As shown, an aircraft tire tread pattern pressing, cooling and shaping device includes a support mechanism 1, a sealing mechanism 2, a filtering mechanism 3, a cooling mechanism 4 and a discharge mechanism 5. The sealing mechanism 2 is installed on the upper end of the support mechanism 1, the filtering mechanism 3 is installed on the upper end of the support mechanism 1, the cooling mechanism 4 is installed on the left end of the filtering mechanism 3, and the discharge mechanism 5 is installed on the upper end of the support mechanism 1. The supporting mechanism 1 provides support, the sealing mechanism 2 provides sealing, the filtering mechanism 3 provides filtration, the cooling mechanism 4 provides cooling, and the discharging mechanism 5 discharges materials. The support mechanism 1 includes a base plate 11, a bottom mold 12, and a ventilation hood 13. The bottom mold 12 is installed on the upper end of the base plate 11, and the ventilation hood 13 is installed on the lower end of the bottom mold 12. The closing mechanism 2 includes an upper mold 21, an exhaust hood 22 and four sets of screws 23. The upper mold 21 is installed on the bottom mold 12 by the four sets of screws 23, and the exhaust hood 22 is installed on the upper end of the upper mold 21. The filtration mechanism 3 includes an air inlet box 31 and a filter screen 32. The air inlet box 31 is installed on the upper end of the base plate 11, and the filter screen 32 is slidably installed on the air inlet box 31. The cooling mechanism 4 includes a fan 41 and an air inlet pipe 42. The fan 41 is installed at the left end of the air inlet box 31. The input end of the air inlet pipe 42 is connected to the output end of the fan 41, and the output end of the air inlet pipe 42 extends into the ventilation hood 13. The material discharge mechanism 5 includes a lifting cylinder 51 and a pallet 52. The lifting cylinder 51 is installed on the upper end of the base plate 11, and the pallet 52 is installed on the upper end of the lifting cylinder 51. The material is supported by the bottom mold 12, ventilated and cooled by the vent hood 13, sealed by the upper mold 21, and vented by the exhaust hood 22. The material is cooled by blowing air into the vent hood 13 through the air inlet pipe 42 by the fan 41, and air is introduced through the air inlet box 31 and filtered by the filter screen 32. The material is discharged by driving the pallet 52 to move up and down by opening the lifting cylinder 51. Thus, during the pressing, cooling and shaping process of the aircraft tire tread pattern, the material can be cooled both inside and out at the same time, so that the material is cooled evenly and the processing efficiency is improved.

[0016] like Figures 1 to 3 As shown, this utility model discloses an aircraft tire tread pattern pressing, cooling and shaping device. During operation, the bottom mold 12 supports the material, the ventilation hood 13 vents and cools the material, the upper mold 21 seals the material, the exhaust hood 22 exhausts the material, the fan 41 blows air into the ventilation hood 13 through the air inlet pipe 42 to cool the material, the air inlet box 31 introduces air, the filter screen 32 filters the incoming air, and the lifting cylinder 51 drives the pallet 52 to lift and discharge the material.

[0017] The fan 41 and lifting cylinder 51 of this utility model are 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.

[0018] The main function achieved by this utility model is: during the pressing, cooling and shaping process of aircraft tire tread patterns, by setting up a support mechanism and a closing mechanism, the material can be cooled both inside and out at the same time, so that the material is cooled evenly and the processing efficiency is improved.

[0019] 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 aviation tire tread pattern press cooling setting device comprising a support mechanism (1); characterized in that, It also includes a sealing mechanism (2), a filtering mechanism (3), a cooling mechanism (4) and a discharge mechanism (5). The sealing mechanism (2) is installed on the upper end of the support mechanism (1), the filtering mechanism (3) is installed on the upper end of the support mechanism (1), the cooling mechanism (4) is installed on the left end of the filtering mechanism (3), and the discharge mechanism (5) is installed on the upper end of the support mechanism (1). The supporting mechanism (1) provides support, the sealing mechanism (2) provides sealing, the filtering mechanism (3) provides filtering, the cooling mechanism (4) provides cooling, and the discharging mechanism (5) discharges materials.

2. An aircraft tire tread pattern press cooling and setting device as claimed in claim 1 wherein, The support mechanism (1) includes a base plate (11), a bottom mold (12) and a ventilation hood (13). The bottom mold (12) is installed on the upper end of the base plate (11), and the ventilation hood (13) is installed on the lower end of the bottom mold (12).

3. The aircraft tire tread pattern pressing, cooling, and shaping device as described in claim 2, characterized in that, The closing mechanism (2) includes an upper mold (21), an exhaust hood (22) and four sets of screws (23). The upper mold (21) is installed on the bottom mold (12) by the four sets of screws (23), and the exhaust hood (22) is installed on the upper end of the upper mold (21).

4. An aircraft tire tread pattern press cooling and setting device as claimed in claim 2 wherein, The filtration mechanism (3) includes an air inlet box (31) and a filter screen (32). The air inlet box (31) is installed on the upper end of the base plate (11), and the filter screen (32) is slidably installed on the air inlet box (31).

5. An aircraft tire tread pattern press cooling and setting device as claimed in claim 4 wherein, The cooling mechanism (4) includes a fan (41) and an air intake pipe (42). The fan (41) is installed at the left end of the air intake box (31). The input end of the air intake pipe (42) is connected to the output end of the fan (41), and the output end of the air intake pipe (42) extends into the ventilation hood (13).

6. An aircraft tire tread pattern press cooling and setting device as claimed in claim 2 wherein, The material discharge mechanism (5) includes a lifting cylinder (51) and a pallet (52). The lifting cylinder (51) is installed on the upper end of the base plate (11), and the pallet (52) is installed on the upper end of the lifting cylinder (51).

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