Aviation tire mold easy to position

By introducing a mechanism that facilitates positioning in aircraft tire molds and utilizing components such as rotating rods, gears, and threaded rods, the problem of inaccurate mold positioning is solved, thereby improving the accuracy and efficiency of tire injection molding.

CN223431921UActive Publication Date: 2025-10-14QINGDAO SENTURY TIRE CO LTD
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Patent Information

Application Number
CN202421701479.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-18
Publication Date
2025-10-14
Estimated Expiration
2034-07-18

AI Technical Summary

Technical Problem

Existing aircraft tire molds cannot be effectively positioned during the injection molding process, causing the upper and lower mold positions to easily move, affecting the tire shaping.

Method used

A convenient positioning mechanism between the lower mold and the upper mold is designed. The precise positioning and removal of the mold can be achieved through the cooperation of components such as rotating rods, gears, threaded rods and inserts.

Benefits of technology

It effectively prevents the mold from moving, improves the accuracy and work efficiency of tire injection molding, simplifies positioning and removal operations, and improves work efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the field of aircraft tire molds, and particularly relates to an easily-positioned aircraft tire mold which comprises a lower mold, an upper mold is arranged at the top end of the lower mold, and a convenient positioning mechanism is arranged between the lower mold and the upper mold; the convenient positioning mechanism comprises first fixing blocks, the first fixing blocks are arranged on the two sides of the lower mold, the rear ends of the first fixing blocks are fixedly connected with the side ends of the lower mold, and rotating rods are inserted in the positions, close to the front ends, of the first fixing blocks. Through the design of the convenient positioning mechanism, the function of positioning the grinding tools is achieved, and the problem that an existing tire mold is not provided with an assembly convenient to position, the situation that the positions of the upper grinding tool and the lower grinding tool are very prone to moving in the injection molding process, and then shaping of a tire is affected is solved; and the situation that the position of the grinding tool moves is reduced.
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Description

Technical Field

[0001] The utility model relates to the field of aviation tire molds, in particular to an aviation tire mold which is easy to position. Background Art

[0002] Tires are circular elastic rubber products that roll on the ground and are installed on various vehicles or machinery. They are usually installed on metal rims to achieve contact with the road surface and ensure the vehicle's driving performance. Tires are generally made by mold injection.

[0003] Existing aircraft tire molds can be specifically referenced in Application No. CN202221156020.4. The mold comprises an upper mold and a lower mold, which define a tire cavity. The upper mold contains upper tread ribs, and the lower mold contains lower tread ribs. The mold also includes an upper mold ring containing a first tread rib and a lower mold ring containing a second tread rib. The upper mold, upper mold ring, lower mold, and lower mold ring together define a tire cavity. The first and second tread ribs are joined together to form a single, integrated pattern. This mold offers the advantages of high machining precision and a short processing cycle.

[0004] However, the above-mentioned tire mold is not provided with a component that can be easily positioned. When the tire is injection molded, since the tire mold cannot be positioned, the upper and lower mold positions are very likely to move during the shaping process, thereby affecting the shaping of the tire. Therefore, it is urgent to propose an easy-to-position aviation tire mold to address the above problem. Utility Model Content

[0005] In order to make up for the deficiencies of the prior art and solve the problems raised in the background art, the utility model provides an easy-to-position aviation tire mold.

[0006] The technical solution adopted by the utility model to solve the technical problem is as follows: the utility model is an easy-to-position aircraft tire mold, comprising a lower mold; an upper mold is arranged on the top of the lower mold, and a positioning mechanism is arranged between the lower mold and the upper mold;

[0007] The positioning mechanism includes a first fixed block, which is arranged on both sides of the lower mold, and the rear end of the first fixed block is fixedly connected to the side end of the lower mold. A rotating rod is inserted near the front end of the first fixed block, and the bottom end of the rotating rod passes through the top of the first fixed block to reach the inside of the front end of the first fixed block. The rotating rod is rotatably connected to the first fixed block, and the bottom end of the rotating rod is fixedly connected to the top of the first gear, and one side of the first gear is meshed with one side of the second gear.

[0008] Preferably, a second fixed block is sleeved on the outer side of the rotating rod near the top, and the rotating rod is rotatably connected to the second fixed block, the bottom end of the second fixed block is fixedly connected to the top of the fixed rod near the rear position, and the bottom end of the fixed rod is fixedly connected to the top of the first fixed block.

[0009] Preferably, rotation grooves are provided on both sides of the interior of the front end of the first fixed block, the inner wall of the second gear is fixedly connected to the outer side of the threaded rod near the middle position, rotation blocks are provided at both ends of the threaded rod, and the threaded rod is fixedly connected to one side of the rotation block, the rotation groove is sleeved on the outer side of the rotation block, and the rotation groove is rotatably connected to the rotation block.

[0010] Preferably, second plug-in blocks are provided on both sides of the upper mold, and the side end of the upper mold is fixedly connected to the rear end of the second plug-in block, one end of the second plug-in block is inserted into the inside of the first fixed block, and the second plug-in block is slidably connected to the first fixed block.

[0011] Preferably, both ends of the outer side of the threaded rod are sleeved with a first plug-in block, and the threaded rod is threadedly connected to the first plug-in block, and slots are provided on both sides of the first fixed block and the second plug-in block, one end of the first plug-in block is inserted into the slot, and the first plug-in block is slidably connected to the slot.

[0012] Preferably, the front end of the first fixing block is fixedly connected to the rear end of the third fixing block, the inner side of the third fixing block is fixedly connected to both ends of the guide rod, the outer side of the guide rod is sleeved with a first plug block, and the guide rod is slidably connected to the first plug block.

[0013] The utility model is beneficial in that:

[0014] 1. The present invention realizes the function of positioning the mold through the structural design of the convenient positioning mechanism, which solves the problem that the existing tire mold is not equipped with a component that can facilitate positioning. When the tire is injection molded, the tire mold cannot be positioned, and the upper and lower molds are easily moved during the shaping process, thereby affecting the shaping of the tire. The problem of mold position movement is reduced;

[0015] 2. The utility model realizes the function of easy positioning or removal through the structural design of the positioning mechanism, solves the problem that the operation steps of positioning or removing the tire mold are relatively cumbersome, and the mold cannot be positioned or removed conveniently and quickly, which easily leads to a decrease in work efficiency, thereby improving work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0017] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0018] Figure 2 This is a schematic diagram of the first partial cross-sectional structure of the present utility model;

[0019] Figure 3 This is a schematic diagram of a second partial cross-sectional structure of the present invention;

[0020] Figure 4 For the utility model Figure 1 A in the middle is an enlarged schematic diagram of the structure;

[0021] Figure 5 For the utility model Figure 2 Schematic diagram of the structure of the enlarged schematic diagram at point B.

[0022] Figure 6 For the utility model Figure 3 Schematic diagram of the structure of the enlarged diagram at point C in the middle.

[0023] In the figure: 1. Lower mold; 2. Upper mold; 10. First fixed block; 11. Rotating rod; 12. First gear; 13. Rotating groove; 14. Second gear; 15. Second fixed block; 16. Fixed rod; 17. Threaded rod; 18. Rotating block; 19. First plug-in block; 20. Slot; 21. Second plug-in block; 22. Third fixed block; 23. Guide rod. DETAILED DESCRIPTION

[0024] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0025] See also Figures 1-6 As shown, an easy-to-position aircraft tire mold includes a lower mold 1; an upper mold 2 is provided on the top of the lower mold 1, and a positioning mechanism is provided between the lower mold 1 and the upper mold 2;

[0026] The positioning mechanism includes a first fixed block 10, which is arranged on both sides of the lower mold 1, and the rear end of the first fixed block 10 is fixedly connected to the side end of the lower mold 1. A rotating rod 11 is inserted near the front end of the first fixed block 10, and the bottom end of the rotating rod 11 passes through the top of the first fixed block 10 to reach the inside of the front end of the first fixed block 10. The rotating rod 11 is rotatably connected to the first fixed block 10, and the rotating rod 11 is circular in design. The interior of the first fixed block 10 sleeved on the outside of the rotating rod 11 is also circular in design. The bottom end of the rotating rod 11 is fixedly connected to the top of the first gear 12, and one side of the first gear 12 is meshed with one side of the second gear 14;

[0027] During operation, the rotating rod 11 at the top of the first fixed block 10 is rotated. When the rotating rod 11 rotates, the first gear 12 and the second gear 14 are driven to rotate synchronously, so as to position the tire grinding tool.

[0028] Furthermore, a second fixing block 15 is sleeved on the outer side of the rotating rod 11 near the top, and the rotating rod 11 is rotatably connected to the second fixing block 15. The inner wall of the second fixing block 15 is circular in design. The bottom end of the second fixing block 15 is fixedly connected to the top of the fixing rod 16 near the rear position. The bottom end of the fixing rod 16 is fixedly connected to the top of the first fixing block 10. The fixing rod 16 is a circular rod design.

[0029] During operation, the rotating rod 11 rotates, and the outer side of the rotating rod 11 near the top rotates along the inside of the second fixed block 15 at the top of the fixed rod 16.

[0030] Furthermore, a rotation groove 13 is formed on both sides of the front end of the first fixed block 10. The inner wall of the second gear 14 is fixedly connected to the outer side of the threaded rod 17 near the middle position. A rotation block 18 is provided at both ends of the threaded rod 17, and the threaded rod 17 is fixedly connected to one side of the rotation block 18. The threads on both sides of the threaded rod 17 are designed in opposite directions. The rotation groove 13 is sleeved on the outer side of the rotation block 18, and the rotation groove 13 is rotatably connected to the rotation block 18. The rotation block 18 and the rotation groove 13 are both circular in design.

[0031] During operation, the second gear 14 rotates, driving the threaded rod 17 and the rotating block 18 to rotate synchronously, and the rotating block 18 rotates along the inside of the rotating groove 13 to position the tire grinding tool.

[0032] Furthermore, a second plug-in block 21 is provided on both sides of the upper mold 2, and the side end of the upper mold 2 is fixedly connected to the rear end of the second plug-in block 21. One end of the second plug-in block 21 is inserted into the first fixed block 10, and the second plug-in block 21 is slidably connected to the first fixed block 10. One end of the second plug-in block 21 is square in design.

[0033] During operation, the bottom end of the upper mold 2 is first placed on the top end of the lower mold 1, and at the same time, the second inserting block 21 at the side end of the upper mold 2 is driven to be inserted into the first fixing block 10 to position the tire mold.

[0034] Furthermore, first plug-in blocks 19 are sleeved on both ends of the outer side of the threaded rod 17, and the threaded rod 17 is threadedly connected to the first plug-in blocks 19. Slots 20 are formed on both sides of the first fixing block 10 and the second plug-in block 21. One end of the first plug-in block 19 is inserted into the slot 20, and the first plug-in block 19 and the slot 20 are slidably connected. One end of the first plug-in block 19 and the slot 20 are both square in design.

[0035] During operation, the threaded rod 17 rotates, driving the first plugs 19 on both sides to move inward along the surface of the threaded rod 17 until one end of the first plug 19 is completely inserted into the slot 20, thereby positioning the tire grinder.

[0036] Furthermore, the front end of the first fixing block 10 is fixedly connected to the rear end of the third fixing block 22, the inner side of the third fixing block 22 is fixedly connected to both ends of the guide rod 23, the outer side of the guide rod 23 is sleeved with a first plug-in block 19, and the guide rod 23 and the first plug-in block 19 are slidably connected, and the inner walls of the guide rod 23 and the first plug-in block 19 sleeved on the outer side of the guide rod 23 are both circular in design;

[0037] During operation, the first inserting block 19 moves, and the first inserting block 19 also moves along the surface of the guide rod 23 inside the third fixing block 22 to position the tire grinding tool.

[0038] Working principle: When the tire mold needs to be positioned, the bottom end of the upper mold 2 is first placed on the top of the lower mold 1, and at the same time, the second plug-in block 21 at the side end of the upper mold 2 is driven to be inserted into the first fixed block 10, and then the rotating rod 11 at the top of the first fixed block 10 is rotated. When the rotating rod 11 rotates, the first gear 12 and the second gear 14 are driven to rotate synchronously, and when the rotating rod 11 rotates, the outer side of the rotating rod 11 near the top rotates along the second fixed block 15 at the top of the fixed rod 16. At the same time, when the second gear 14 rotates, it drives the threaded rod 17 and the rotating block 18 to rotate synchronously, and the rotating block 18 rotates along the inside of the rotating groove 13. When the threaded rod 17 rotates, it drives the first plug-in blocks 19 on both sides to move inward along the surface of the threaded rod 17 until one end of the first plug-in block 19 is completely inserted into the inside of the slot 20. When the first plug-in block 19 moves, the first plug-in block 19 also moves along the surface of the guide rod 23 inside the third fixed block 22 to position the tire mold.

[0039] The above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or replace some of the technical features therein with equivalents. Any modifications, equivalent replacements, and similar improvements made within the theoretical and principle content of the present invention shall be included in the scope of protection of the present invention.

Claims

1. An easily positionable aircraft tire mold, comprising a lower mold (1); characterized in that: An upper mold (2) is provided at the top of the lower mold (1), and a positioning mechanism is provided between the lower mold (1) and the upper mold (2); The positioning mechanism comprises a first fixed block (10), the first fixed blocks (10) are arranged on both sides of the lower mold (1), and the rear end of the first fixed block (10) is fixedly connected to the side end of the lower mold (1), a rotating rod (11) is inserted near the front end of the first fixed block (10), and the bottom end of the rotating rod (11) passes through the top end of the first fixed block (10) and reaches the inside of the front end of the first fixed block (10), the rotating rod (11) is rotatably connected to the first fixed block (10), the bottom end of the rotating rod (11) is fixedly connected to the top end of the first gear (12), and one side of the first gear (12) is meshed with one side of the second gear (14).

2. The easily positionable aircraft tire mold according to claim 1, characterized in that: A second fixed block (15) is sleeved on the outer side of the rotating rod (11) near the top, and the rotating rod (11) is rotatably connected to the second fixed block (15). The bottom end of the second fixed block (15) is fixedly connected to the top end of the fixed rod (16) near the rear position, and the bottom end of the fixed rod (16) is fixedly connected to the top end of the first fixed block (10).

3. The easily positionable aircraft tire mold according to claim 2, characterized in that: Rotation grooves (13) are provided on both sides of the front end of the first fixed block (10); the inner wall of the second gear (14) is fixedly connected to the outer side of the threaded rod (17) near the middle position; rotation blocks (18) are provided at both ends of the threaded rod (17); the threaded rod (17) is fixedly connected to one side of the rotation block (18); the rotation groove (13) is sleeved on the outer side of the rotation block (18), and the rotation groove (13) is rotationally connected to the rotation block (18).

4. The easily positionable aircraft tire mold according to claim 3, characterized in that: Second plug-in blocks (21) are provided on both sides of the upper mold (2), and the side ends of the upper mold (2) are fixedly connected to the rear ends of the second plug-in blocks (21), one end of the second plug-in block (21) is inserted into the interior of the first fixed block (10), and the second plug-in block (21) is slidably connected to the first fixed block (10).

5. The easily positionable aircraft tire mold according to claim 4, characterized in that: Both ends of the outer side of the threaded rod (17) are sleeved with first plug blocks (19), and the threaded rod (17) is threadedly connected to the first plug block (19). Both sides of the first fixed block (10) and the second plug block (21) are provided with slots (20), one end of the first plug block (19) is inserted into the slot (20), and the first plug block (19) is slidably connected to the slot (20).

6. The easily positionable aircraft tire mold according to claim 5, characterized in that: The front end of the first fixed block (10) is fixedly connected to the rear end of the third fixed block (22), the inner side of the third fixed block (22) is fixedly connected to both ends of the guide rod (23), the outer side of the guide rod (23) is sleeved with a first plug-in block (19), and the guide rod (23) is slidably connected to the first plug-in block (19).

Citation Information

Patent Citations

  • Tire mold

    CN217671225U