CN219213793U - Aviation tire manufacturing mold - Google Patents

Abstract

The utility model provides an aviation tire manufacturing mould, which belongs to the technical field of tires and comprises; a placement table; the lower die box is fixedly connected to the upper end of the placing table; the moulding-die mechanism, moulding-die mechanism includes: the two hydraulic cylinders are fixedly connected to the upper end of the placing table; four sliding rods fixedly connected to the upper end of the placing table; four springs slidably connected to the circumferential surfaces of the four sliding bars, respectively; the movable plate is fixedly connected to the thin rods of the two hydraulic cylinders; and go up the mould box, fixed connection in the lower extreme of movable plate, this facility can be through setting up the spring on the slide bar surface, and collide slowly to last mould box to avoid last mould box to cause the effect of damage, set up the buffer block under last mould box, reducible cause the collision.

Description

Aviation tire manufacturing mold

Technical Field

The utility model belongs to the technical field of tires, and particularly relates to a mold for manufacturing an aviation tire.

Background

Tires are ground-engaging rolling, annular elastomeric rubber articles assembled on a variety of vehicles or machines. The automobile body is usually arranged on a metal rim, can support the automobile body, buffer external impact, realize contact with a road surface and ensure the running performance of the automobile. Tires are often used under complex and severe conditions, and they are subjected to various deformations, loads, forces and high and low temperatures during running, and therefore must have high load-bearing, traction and cushioning properties.

The patent publication No. CN213797590U describes a tire mold with self-vulcanizing narrow slit exhaust, and relates to the technical field of tire molds. This tire mould with from vulcanization slot exhaust, including the mould, the mould includes mould and lower mould, go up the mould lock in the lower mould top, it all is provided with the guide wing board to go up mould and lower mould outside, the guide wing board outside is provided with the guide part, the lower mould front side is provided with the handle, the inside first inflation hole that is provided with of guide wing board, the inside second inflation hole that is provided with of handle, the lower mould rear side is provided with the baffle. This tire mould with from vulcanizing narrow slit exhaust can drive its relative motion when exerting certain pressure to the guide, and then fix last mould and lower mould fast, and this device has increased guide wing plate and guide through improving traditional mould, can make things convenient for quick mould assembly to the precision is high, is favorable to automated production. "

The above patent is when carrying out the compound die, leads to causing the collision between the mould easily to cause the mould to damage, reduced life.

Disclosure of Invention

The utility model aims to provide an aviation tire manufacturing mold, which aims to solve the problems that in the prior art, when aviation tires are rapidly assembled, the molds are easy to collide with each other, so that the molds are damaged, and the service life is reduced.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

an aircraft tire manufacturing mold comprising:

a placement table;

the lower die box is fixedly connected to the upper end of the placing table;

a die mechanism, the die mechanism comprising:

the two hydraulic cylinders are fixedly connected to the upper end of the placing table;

the four sliding rods are fixedly connected to the upper end of the placing table;

four springs slidably connected to the circumferential surfaces of the four slide bars, respectively;

the movable plate is fixedly connected to the thin rods of the two hydraulic cylinders; and

and the upper die box is fixedly connected to the lower end of the moving plate.

As a preferable scheme of the utility model, the lower end of the upper die box is fixedly connected with four buffer blocks, and the upper end of the lower die box is provided with four supporting grooves.

As a preferable scheme of the utility model, the upper end of the movable plate is fixedly connected with a delivery pipe, and the upper end of the delivery pipe is fixedly connected with a wear-resistant pipe.

As a preferable scheme of the utility model, the lower end of the placing table is fixedly connected with a wear-resisting plate, and the upper end of the wear-resisting plate is provided with four positioning holes.

As a preferable scheme of the utility model, the upper end of the placing table is fixedly connected with two mounting frames, and one side ends of the two mounting frames are fixedly connected with infrared sensors.

As a preferable scheme of the utility model, one side end of the placing table is fixedly connected with a mounting plate, the upper end of the mounting plate is fixedly connected with a mounting column, and the upper end of the mounting column is fixedly connected with a mounting box.

As a preferable scheme of the utility model, one side end of the upper die box is fixedly connected with a mounting block, and the lower end of the mounting block is fixedly connected with a positioning strip.

As a preferable scheme of the utility model, one side end of the wear-resistant plate is fixedly connected with a placing pad, and the upper end of the placing pad is fixedly connected with two guard bars.

Compared with the prior art, the utility model has the beneficial effects that:

in this scheme, through the pneumatic cylinder that sets up on placing the bench, can drive the mould box and remove to make the effect of carrying out the compound die to aircraft tire good, through the slide bar that sets up on placing the bench, can support the mould box and slide and remove and reach such effect.

In this scheme, through setting up the infrared inductor of placing the bench, but external equipment is connected and is controlled the pneumatic cylinder, can stop the operation of pneumatic cylinder when the staff is around equipment to reduce the potential safety hazard, through setting up the antifriction plate of placing under the bench, reduced ground and placed the bench and caused wearing and tearing.

Drawings

The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:

FIG. 1 is a perspective view of a first view of the present utility model;

FIG. 2 is an exploded view of the present utility model;

FIG. 3 is an enlarged view of the upper mold box of FIG. 2 in accordance with the present utility model;

fig. 4 is a perspective view of a second view of the present utility model.

In the figure: 1. a moving plate; 2. a wear resistant tube; 3. an upper mold box; 4. a slide bar; 5. a placement table; 6. a hydraulic cylinder; 7. a spring; 8. a buffer block; 9. a mounting frame; 10. an infrared sensor; 11. a groove is propped against; 12. a lower mold box; 13. positioning holes; 14. a delivery tube; 15. a mounting plate; 16. a wear plate; 17. a mounting column; 18. a mounting box; 19. a positioning strip; 20. a mounting block; 21. placing a pad; 22. and (5) protecting the strip.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Example 1

Referring to fig. 1-4, the present utility model provides the following technical solutions:

an aircraft tire manufacturing mold comprising:

a placement table 5;

the lower die box 12 is fixedly connected to the upper end of the placing table 5;

the moulding-die mechanism, moulding-die mechanism includes:

two hydraulic cylinders 6 fixedly connected to the upper end of the placement table 5;

four sliding rods 4 fixedly connected to the upper end of the placement table 5;

four springs 7 slidably connected to the circumferential surfaces of the four slide bars 4, respectively;

the movable plate 1 is fixedly connected to the thin rods of the two hydraulic cylinders 6; and

the upper die box 3 is fixedly connected to the lower end of the movable plate 1.

In the specific embodiment of the utility model, the hydraulic cylinder 6 arranged on the placing table 5 drives the upper die box 3 to move, so that the upper die box 3 performs the die closing function on the lower die box 12, the sliding rod 4 arranged on the placing table 5 performs the function of stably moving the upper die box 3, the buffer block 8 arranged below the upper die box 3 performs the function of buffering the upper die box 3, the wear-resisting plate 16 arranged below the placing table 5 performs the function of fixing equipment, the external equipment can be connected through the infrared sensor 10 arranged on the placing table 5, the hydraulic cylinder 6 is controlled, the hydraulic cylinder 6 can be stopped when workers are around the equipment, the potential safety hazards of the workers are reduced, the installation box 18 arranged on the placing table 5 performs the function of installing equipment control equipment, the buffer block 3 can perform the function of buffering the upper die box 3 through the spring 7 arranged on the surface of the sliding rod 4, the installation box 17 is supported by the support column 18, and the installation box 17 is required to be installed. The specific type of hydraulic cylinder 6 and infrared sensor 10 used is selected by those skilled in the art, and the hydraulic cylinder 6 and infrared sensor 10 can be connected by external power source.

Referring to fig. 2 specifically, four buffer blocks 8 are fixedly connected to the lower end of the upper mold box 3, and four supporting grooves 11 are formed in the upper end of the lower mold box 12.

In this embodiment: the buffer block 8 provided below the upper die box 3 plays a role of buffering the upper die box 3.

Referring to fig. 2 specifically, an upper end of the moving plate 1 is fixedly connected with a delivery tube 14, and an upper end of the delivery tube 14 is fixedly connected with a wear-resistant tube 2.

In this embodiment: the guide pipe 14 provided in the moving plate 1 serves to guide the raw material of the aircraft tire into the lower mold box 12.

Referring to fig. 2 specifically, the lower end of the placement table 5 is fixedly connected with a wear-resistant plate 16, and four positioning holes 13 are formed in the upper end of the wear-resistant plate 16.

In this embodiment: the function of fixing the device is achieved by means of the wear plate 16 arranged under the placement table 5.

Referring to fig. 2 specifically, the upper end of the placement table 5 is fixedly connected with two mounting frames 9, and one side ends of the two mounting frames 9 are fixedly connected with an infrared sensor 10.

In this embodiment: through the infrared sensor 10 that sets up on placing the platform 5, can connect external equipment, control pneumatic cylinder 6, can stop the operation of pneumatic cylinder 6 when the staff is around equipment to the effect of reduction staff potential safety hazard has been played.

Referring to fig. 4 specifically, a mounting plate 15 is fixedly connected to one side end of the placement table 5, a mounting column 17 is fixedly connected to an upper end of the mounting plate 15, and a mounting box 18 is fixedly connected to an upper end of the mounting column 17.

In this embodiment: the mounting box 18 provided on the placement table 5 plays a role in mounting and fixing the device control board.

Referring to fig. 2 specifically, a mounting block 20 is fixedly connected to one side end of the upper mold box 3, and a positioning strip 19 is fixedly connected to the lower end of the mounting block 20.

In this embodiment: the mounting block 20 on one side of the upper die box 3 is arranged to play a role in mounting and fixing the positioning strip 19, and the positioning strip 19 arranged under the mounting block 20 plays a role in positioning the upper die box 3.

Referring to fig. 2 specifically, a placement pad 21 is fixedly connected to one side end of the wear plate 16, and two guard bars 22 are fixedly connected to the upper end of the placement pad 21.

In this embodiment: the pad 21 arranged on one side of the wear plate 16 plays a role in placing the tire when occupied, and the protection strip 22 arranged on the pad 21 plays a role in protecting the tire.

The working principle and the using flow of the utility model are as follows: this facility is through setting up pneumatic cylinder 6, drives mould box 3 and removes, and rethread is led the tire material into the lower mould box 12 through delivery tube 14 in, and the last mould box 3 of rethread pneumatic cylinder 6 drive removes to can take out the tire, this facility can drive mould box 3 and remove through setting up the pneumatic cylinder 6 on placing the platform 5, thereby makes the effectual of carrying out the compound die to the aviation tire, through setting up the slide bar 4 on placing the platform 5, thereby support mould box 3 and slide and remove and reach such effect.

The above is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that the present utility model is described in detail with reference to the foregoing embodiments, and modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims (8)

1. An aircraft tire manufacturing mold, comprising:

a placement table (5);

the lower die box (12) is fixedly connected to the upper end of the placing table (5);

a die mechanism, the die mechanism comprising:

the two hydraulic cylinders (6) are fixedly connected to the upper end of the placing table (5);

four sliding rods (4) fixedly connected to the upper end of the placing table (5);

four springs (7) slidably connected to the circumferential surfaces of the four slide bars (4), respectively;

the moving plate (1) is fixedly connected to the thin rods of the two hydraulic cylinders (6); and

and the upper die box (3) is fixedly connected to the lower end of the moving plate (1).

2. An aircraft tire manufacturing mold according to claim 1, wherein: the lower end of the upper die box (3) is fixedly connected with four buffer blocks (8), and the upper end of the lower die box (12) is provided with four supporting grooves (11).

3. An aircraft tire manufacturing mold according to claim 2, wherein: the upper end of the movable plate (1) is fixedly connected with a delivery pipe (14), and the upper end of the delivery pipe (14) is fixedly connected with a wear-resistant pipe (2).

4. An aircraft tire manufacturing mold according to claim 3, wherein: the lower extreme fixedly connected with antifriction plate (16) of placing platform (5), four locating holes (13) have been seted up to the upper end of antifriction plate (16).

5. An aircraft tire manufacturing mold according to claim 4, wherein: the upper end fixedly connected with two mounting brackets (9) of placing platform (5), two the one side end of mounting bracket (9) is all fixedly connected with infrared inductor (10).

6. An aircraft tire manufacturing mold according to claim 5, wherein: one side end fixedly connected with mounting panel (15) of placing platform (5), the upper end fixedly connected with erection column (17) of mounting panel (15), the upper end fixedly connected with installation box (18) of erection column (17).

7. An aircraft tire manufacturing mold according to claim 6, wherein: one side end of the upper die box (3) is fixedly connected with a mounting block (20), and the lower end of the mounting block (20) is fixedly connected with a positioning strip (19).

8. An aircraft tire manufacturing mold according to claim 7, wherein: one side end of the wear-resisting plate (16) is fixedly connected with a placing pad (21), and the upper end of the placing pad (21) is fixedly connected with two protection strips (22).

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