Aviation tire wear-resistant layer curing equipment

Abstract

The utility model relates to the technical field of curing of wear-resistant layers of aviation tires, in particular to curing equipment for wear-resistant layers of aviation tires, which is provided with a limiting mechanism and a rotating mechanism, so that materials can be rotated in the curing process of the wear-resistant layers of the aviation tires, the materials are distributed more uniformly under the centrifugal action, and the processing quality is improved. Comprising a vulcanizing mechanism; the device further comprises a heating mechanism, a limiting mechanism, two locking mechanisms and a rotating mechanism, the heating mechanism is installed at the lower end of the vulcanizing mechanism, the limiting mechanism is installed at the upper end of the vulcanizing mechanism, the two locking mechanisms are installed on the limiting mechanism, and the rotating mechanism is installed at the upper end of the vulcanizing mechanism; the vulcanizing mechanism is used for vulcanizing, the heating mechanism is used for heating, the limiting mechanism is used for limiting, the locking mechanism is used for locking, and the rotating mechanism is used for rotating.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of aviation tire wear -resistant layer curing, in particular to an aviation tire wear -resistant layer curing equipment. BACKGROUND

[0002] The curing of the wear -resistant layer of the aviation tire is an important link in the tire manufacturing process, which is directly related to the wear resistance, service life and flight safety of the tire.

[0003] In the existing aviation tire wear -resistant layer curing equipment, for example, the utility model patent no. 201910255835.4 discloses an aviation tire wear -resistant layer curing equipment, the vulcanization device of the vibrating curing rubber tire of the invention is more beneficial to the curing process of the thermal expansion rubber mixed with the foaming agent compared with the traditional rubber tire vulcanization device, even if the air bubble is generated in the contact surface between the tread and the inner surface of the mold, the above-mentioned air bubble can be discharged through eccentric vibration, therefore, the air bubble rate of the produced tire is low, and the yield is high.

[0004] But in the aviation tire wear -resistant layer curing process, the material is relatively soft in the material curing, which can cause uneven material accumulation and reduce the processing quality. UTILITY MODEL CONTENT

[0005] To solve the above technical problems, the utility model provides an aviation tire wear -resistant layer curing equipment through the setting of the limiting mechanism and the rotating mechanism, so that the material can be rotated in the aviation tire wear -resistant layer curing process, the material is more evenly distributed under the centrifugal action, and the processing quality is improved.

[0006] The utility model discloses an aviation tire wear -resistant layer curing equipment, including vulcanization mechanism, still including heating mechanism, limiting mechanism, two groups of locking mechanism and rotating mechanism, heating mechanism installs in the lower extreme of vulcanization mechanism, limiting mechanism installs in the upper extreme of vulcanization mechanism, two groups of locking mechanism install on limiting mechanism, and rotating mechanism installs in the upper extreme of vulcanization mechanism.

[0007] The vulcanization mechanism carries out vulcanization, the heating mechanism carries out heating, the limiting mechanism carries out limiting, the locking mechanism carries out locking, and the rotating mechanism carries out rotation, the limiting mechanism is positioned to the material, the locking mechanism is locked to the limiting mechanism, the heating mechanism is heated to the vulcanization mechanism, the material is vulcanized to the vulcanization mechanism, and the material is rotated by opening the rotating mechanism, so that the material can be rotated in the aviation tire wear -resistant layer curing process, the material is more evenly distributed under the centrifugal action, and the processing quality is improved.

[0008] Preferably, the vulcanization mechanism includes a water tank, a steam network and a stirring blade, the steam network is installed on the upper end of the water tank, and the stirring blade is installed on the upper end of the steam network, the steam network releases steam to form vulcanization in the high temperature and high pressure of the material inside.

[0009] Preferably, the heating mechanism comprises a heating bin and a heating wire, the heating bin is installed at the lower end of the water tank, and the heating wire is installed in the heating bin; the heating wire heats the water tank by being electrified.

[0010] Preferably, the limiting mechanism comprises a rotating frame, a limiting bin and a cover plate, the rotating frame is rotatably installed at the upper end of the water tank, the limiting bin is installed at the upper end of the rotating frame, and the cover plate is installed at the upper end of the limiting bin; the limiting bin cooperates with the cover plate to limit the material.

[0011] Preferably, the locking mechanism comprises six groups of screw rods, a locking frame and six groups of nuts, the six groups of screw rods are installed on the limiting bin, the locking frame is sleeved on the six groups of screw rods, and each group of screw rod is threadedly connected with a group of nuts to fix the locking frame; the locking frame locks the limiting mechanism by threadedly connecting the nuts with the screw rods.

[0012] Preferably, the rotating mechanism comprises a gear ring, a motor and a gear, the gear ring is installed on the rotating frame, the motor is installed at the upper end of the water tank, the gear is connected with the output end of the motor, and the gear is engaged with the gear ring; the motor rotates by driving the gear, and the gear ring drives the rotating frame to rotate by being engaged with the gear ring.

[0013] Compared with the prior art, the beneficial effects of the utility model are as follows: the limiting mechanism limits the material, the locking mechanism locks the limiting mechanism, the heating mechanism heats the vulcanization mechanism, the vulcanization mechanism vulcanizes the material, and the rotating mechanism rotates the material, so that the material can rotate in the aviation tire wear-resistant layer curing process, the material is more evenly distributed under the centrifugal force, and the processing quality is improved. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 is the first axonometric structural schematic view of the utility model;

[0015] Figure 2 is the second axonometric structural schematic view of the utility model;

[0016] Figure 3 is the front view cross-sectional axonometric structural schematic view of the utility model;

[0017] Figure 4 is the top view cross-sectional axonometric structural schematic view of the utility model;

[0018] Figure 5 is the locking mechanism in the utility model A part front view cross-sectional axonometric enlarged structural schematic view; Figure 3

[0019] ​Markings in the accompanying drawings: 1. Vulcanizing mechanism; 11. Water tank; 12. Steam network; 13. Stirring blade; 2. Heating mechanism; 21. Heating chamber; 22. Heating wire; 3. Limiting mechanism; 31. Rotating frame; 32. Limiting chamber; 33. Cover plate; 4. Locking mechanism; 41. Screw; 42. Locking frame; 43. Nut; 5. Rotating mechanism; 51. Gear ring; 52. Motor; 53. Gear. DETAILED DESCRIPTION

[0020] To facilitate understanding of the present invention, a more comprehensive description of the present invention will be provided below with reference to the accompanying drawings. The present invention can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to provide a more thorough and comprehensive understanding of the present invention.

[0021] Example 1

[0022] like Figures 1 to 5 As shown, an aircraft tire wear-resistant layer curing device includes a vulcanizing mechanism 1, a heating mechanism 2, a limiting mechanism 3, two sets of locking mechanisms 4, and a rotating mechanism 5. The heating mechanism 2 is mounted on the lower end of the vulcanizing mechanism 1, the limiting mechanism 3 is mounted on the upper end of the vulcanizing mechanism 1, the two sets of locking mechanisms 4 are mounted on the limiting mechanism 3, and the rotating mechanism 5 is mounted on the upper end of the vulcanizing mechanism 1;

[0023] The vulcanizing mechanism 1 performs vulcanization, the heating mechanism 2 performs heating, the limiting mechanism 3 performs limiting, the locking mechanism 4 performs locking, and the rotating mechanism 5 performs rotation;

[0024] The vulcanizing mechanism 1 includes a water tank 11, a steam screen 12 and a stirring blade 13. The steam screen 12 is installed at the upper end of the water tank 11, and the stirring blade 13 is installed at the upper end of the steam screen 12.

[0025] The heating mechanism 2 includes a heating chamber 21 and a heating wire 22. The heating chamber 21 is installed at the lower end of the water tank 11, and the heating wire 22 is installed in the heating chamber 21.

[0026] The limiting mechanism 3 includes a rotating frame 31, a limiting bin 32 and a cover plate 33. The rotating frame 31 is rotatably mounted on the upper end of the water tank 11, the limiting bin 32 is mounted on the upper end of the rotating frame 31, and the cover plate 33 is mounted on the upper end of the limiting bin 32.

[0027] The locking mechanism 4 includes six sets of screws 41, a locking frame 42 and six sets of nuts 43. The six sets of screws 41 are installed on the limit bin 32, and the locking frame 42 is sleeved on the six sets of screws 41. A set of nuts 43 are installed on each set of screws 41 through threaded engagement to fix the locking frame 42.

[0028] The rotating mechanism 5 comprises a gear ring 51, a motor 52 and a gear 53, the gear ring 51 is installed on the rotating frame 31, the motor 52 is installed on the upper end of the water tank 11, the gear 53 is connected with the output end of the motor 52, and the gear 53 is engaged with the gear ring 51;

[0029] The material is limited by the limiting bin 32 and the cover plate 33, the limiting mechanism 3 is locked by the locking frame 42 through the threaded cooperation of the nut 43 and the screw rod 41, the water tank 11 is heated by the heating wire 22 through the electrification of the heating wire 22, the material is vulcanized through the release of steam by the steam net 12, the motor 52 is rotated through the transmission of the gear 53, the rotating frame 31 is rotated through the engagement of the gear ring 51 and the motor 52, so that the material can be rotated in the curing process of the wear-resistant layer of the aviation tire, and the material is more uniformly distributed under the centrifugal effect, and the processing quality is improved.

[0030] As shown in Figures 1 to 5 The utility model discloses a kind of aviation tire wear-resistant layer curing equipment, when working, material is limited by limiting bin 32 and cover plate 33, limiting mechanism 3 is locked by locking frame 42 through the threaded cooperation of nut 43 and screw rod 41, water tank 11 is heated by heating wire 22 through the electrification of heating wire 22, material is vulcanized through the release of steam by steam net 12, motor 52 is rotated through the transmission of gear 53, rotating frame 31 is rotated through the engagement of gear ring 51 and motor 52 simultaneously with the rotation of motor 52.

[0031] The motor 52 of the utility model is purchased on the market, and the technical personnel in the industry only needs to install and operate according to the attached instruction manual, without the creative labor of the technical personnel in the field.

[0032] The utility model realizes the main function: in the curing work process of the wear-resistant layer of the aviation tire, limiting mechanism and rotating mechanism are set, so that the material can be rotated in the curing process of the wear-resistant layer of the aviation tire, the material is more uniformly distributed under the centrifugal effect, and the processing quality is improved.

[0033] The above is only preferred embodiment of the utility model, and it should be pointed out that, for ordinary technical personnel in the technical field, without departing from the technical principle of the utility model, a plurality of improvements and modifications can be made, and these improvements and modifications should be regarded as the protection range of the utility model.

Claims

1. An aircraft tire wear-resistant layer curing device, comprising a vulcanizing mechanism (1); characterized in that: The device further comprises a heating mechanism (2), a limiting mechanism (3), two sets of locking mechanisms (4) and a rotating mechanism (5), wherein the heating mechanism (2) is mounted on the lower end of the vulcanizing mechanism (1), the limiting mechanism (3) is mounted on the upper end of the vulcanizing mechanism (1), the two sets of locking mechanisms (4) are mounted on the limiting mechanism (3), and the rotating mechanism (5) is mounted on the upper end of the vulcanizing mechanism (1); The vulcanizing mechanism (1) performs vulcanization, the heating mechanism (2) performs heating, the limiting mechanism (3) performs limiting, the locking mechanism (4) performs locking, and the rotating mechanism (5) performs rotation.

2. The aircraft tire wear-resistant layer curing device according to claim 1, characterized in that: The vulcanizing mechanism (1) comprises a water tank (11), a steam net (12) and a stirring blade (13). The steam net (12) is installed on the upper end of the water tank (11), and the stirring blade (13) is installed on the upper end of the steam net (12).

3. The aircraft tire wear-resistant layer curing device according to claim 2, characterized in that: The heating mechanism (2) comprises a heating chamber (21) and a heating wire (22). The heating chamber (21) is installed at the lower end of the water tank (11), and the heating wire (22) is installed in the heating chamber (21).

4. The aircraft tire wear-resistant layer curing device according to claim 2, characterized in that: The limiting mechanism (3) comprises a rotating frame (31), a limiting bin (32) and a cover plate (33); the rotating frame (31) is rotatably mounted on the upper end of the water tank (11); the limiting bin (32) is mounted on the upper end of the rotating frame (31); and the cover plate (33) is mounted on the upper end of the limiting bin (32).

5. The aircraft tire wear-resistant layer curing device according to claim 4, characterized in that: The locking mechanism (4) comprises six groups of screw rods (41), a locking frame (42) and six groups of nuts (43). The six groups of screw rods (41) are installed on the limit bin (32). The locking frame (42) is sleeved on the six groups of screw rods (41). Each group of screw rods (41) is equipped with a group of nuts (43) through threaded engagement to fix the locking frame (42).

6. The aircraft tire wear-resistant layer curing device according to claim 4, characterized in that: The rotating mechanism (5) comprises a gear ring (51), a motor (52) and a gear (53). The gear ring (51) is mounted on the rotating frame (31), the motor (52) is mounted on the upper end of the water tank (11), the gear (53) is connected to the output end of the motor (52), and the gear (53) is meshed with the gear ring (51).

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