Aviation radial tire vulcanizing machine

Abstract

The utility model relates to the technical field of aviation radial tire vulcanization, in particular to an aviation radial tire vulcanizing machine, which is provided with a supporting mechanism and a rotating mechanism, so that materials can be internally supported in the vulcanization process of an aviation radial tire, the deformation of the materials in the vulcanization process is reduced, and the processing quality is improved. Comprising a heating mechanism; the device further comprises a pressurizing mechanism, a rotating mechanism, a supporting mechanism and a cooling mechanism, the pressurizing mechanism is installed at the upper end of the heating mechanism, the rotating mechanism is installed in the heating mechanism, the supporting mechanism is installed on the rotating mechanism, and the cooling mechanism is installed at the lower end of the heating mechanism; the heating mechanism is used for heating, the pressurizing mechanism is used for pressurizing, the rotating mechanism is used for rotating, the supporting mechanism is used for supporting, and the cooling mechanism is used for cooling.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of aviation meridian tire vulcanization, in particular to an aviation meridian tire vulcanization machine. BACKGROUND

[0002] Tire is the round annular elastic rubber product that rolls on the ground and is equipped on various vehicles or machines.

[0003] In the existing aviation meridian tire vulcanization machine, for example, the aviation meridian tire vulcanization machine disclosed in the Chinese utility model patent with the application number CN201921171194.6, a reduction motor is connected with the tire placing frame, so that the reduction motor can drive the rubber tire on the tire placing frame to rotate slowly, ensuring uniform heating and vulcanization of the rubber tire; an infrared heating plate and a temperature controller are arranged, so that the temperature controller can control the infrared heating plate to perform constant temperature heating on the rubber tire in the heating barrel, ensuring the balance of the heating temperature in the heating barrel; a small air compressor, a gas supply pipeline and a pressure gauge are arranged, so that the small air compressor can fill compressed air into the heating barrel through the gas supply pipeline, maintaining a high pressure state in the heating barrel, thereby ensuring the constant temperature heating and high pressure state in the heating barrel, and ensuring the vulcanization effect of the rubber tire.

[0004] However, during the vulcanization process of the aviation meridian tire, the rubber will deform under high temperature and high pressure, resulting in softening and deformation of the material after vulcanization, and reducing the processing quality. UTILITY MODEL CONTENTS

[0005] To solve the above technical problems, the utility model provides an aviation meridian tire vulcanization machine by arranging a supporting mechanism and a rotating mechanism, so that the material can be internally supported during the vulcanization process of the aviation meridian tire, thereby reducing the deformation of the material during the vulcanization process and improving the processing quality.

[0006] The aviation meridian tire vulcanization machine of the utility model comprises a heating mechanism; further comprises a pressurizing mechanism, a rotating mechanism, a supporting mechanism and a cooling mechanism, the pressurizing mechanism is installed on the upper end of the heating mechanism, the rotating mechanism is installed in the heating mechanism, the supporting mechanism is installed on the rotating mechanism, and the cooling mechanism is installed on the lower end of the heating mechanism;

[0007] The heating mechanism is heated, the pressurizing mechanism is pressurized, the rotating mechanism is rotated, the supporting mechanism is supported, and the cooling mechanism is cooled; the material is supported by opening the supporting mechanism, the material is sealed and pressurized by opening the pressurizing mechanism, the material is heated by opening the heating mechanism, and the material is rotated by opening the rotating mechanism at the same time, and the material is rapidly cooled by opening the cooling mechanism after vulcanization, so that the material can be internally supported during the vulcanization process of the aviation meridian tire, thereby reducing the deformation of the material during the vulcanization process and improving the processing quality.

[0008] Preferably, the heating mechanism comprises a heating bin and a microwave heating plate, the microwave heating plate is installed in the heating bin; the material is heated by the microwave heating plate.

[0009] Preferably, the pressurizing mechanism comprises a sealing cover and a booster pump, the sealing cover is hinged to the upper end of the heating bin, and the booster pump is installed at the upper end of the sealing cover; the heating bin is sealed by the sealing cover, and the material is pressurized by opening the booster pump.

[0010] Preferably, the rotating mechanism comprises a rotating table, a slave gear, a main gear and a motor one, the rotating table is rotatably installed in the heating bin, the slave gear is installed on the rotating table, the main gear is rotatably installed in the heating bin and is engaged with the slave gear, and the motor one is installed in the heating bin and is connected with the input end of the main gear; the main gear is driven to rotate by opening the motor one, and the slave gear is driven to rotate by the engagement of the main gear and the slave gear.

[0011] Preferably, the supporting mechanism comprises eight groups of supporting plates, sixteen groups of connecting rods, top plates, lead screws, worm gears, a motor two and a worm, each of the eight groups of supporting plates is rotatably connected with two groups of connecting rods, the eight groups of connecting rods are rotatably installed at the upper end of the rotating table, the top plates are rotatably connected with the other eight groups of connecting rods, the lead screws are installed at the lower end of the top plates, the worm gears are rotatably installed in the heating bin and are threadedly matched with the lead screws, the motor two is installed in the heating bin, the input end of the worm is connected with the output end of the motor two, and the worm is threadedly matched with the worm gears; the worm is driven to rotate by opening the motor two, the worm gears are driven to rotate by the thread matching between the worm and the worm gears, and the lead screws are driven to move by the thread matching between the worm gears and the lead screws to support the top plates, so that the top plates support the supporting plates through the connecting rods to support the material.

[0012] Preferably, the cooling mechanism comprises a water bin, a water pump, a spray head and a water pipe, the water bin is installed at the lower end of the heating bin, the water pump is installed at the left end of the water bin, the spray head is installed in the heating bin, and the output end of the water pump is connected with the input end of the spray head through the water pipe; the material is sprayed and cooled by opening the water pump, the water pipe and the spray head.

[0013] Compared with the prior art, the beneficial effects of the utility model are that: the material is supported by opening the supporting mechanism, the material is sealed and pressurized by opening the pressurizing mechanism, the material is heated by opening the heating mechanism, and the material is rotated by opening the rotating mechanism, and the material is rapidly cooled by opening the cooling mechanism after vulcanization, so that the material can be internally supported during the vulcanization process of the aviation meridian tire, the deformation of the material during the vulcanization process is reduced, and the processing quality is improved. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1Is the axial measurement structure schematic diagram of the utility model;

[0015] Figure 2 Is the front view cross section axial measurement structure schematic diagram of the utility model;

[0016] Figure 3 Is the upper view cross section axial measurement structure schematic diagram of the utility model;

[0017] Figure 4 Is the lower view cross section axial measurement structure schematic diagram of the utility model;

[0018] Marked in the drawing: 1, heating mechanism;11, heating bin;12, microwave heating plate;2, pressurizing mechanism;21, sealing cover;22, booster pump;3, rotating mechanism;31, rotary table;32, from gear;33, main gear;34, motor one;4, supporting mechanism;41, support plate;42, connecting rod;43, top plate;44, lead screw;45, worm wheel;46, motor two;47, worm;5, cooling mechanism;51, water bin;52, water pump;53, spray head;54, water pipe. DETAILED DESCRIPTION

[0019] In order to facilitate understanding the utility model, below will be with reference to relevant drawings more comprehensive description of the utility model. The utility model can be realized in many different forms, and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the utility model more thorough and comprehensive.

[0020] Embodiment 1

[0021] As Figures 1 to 4 Indicated, an aviation meridian tire vulcanizing machine, including heating mechanism 1, still including pressurizing mechanism 2, rotating mechanism 3, supporting mechanism 4 and cooling mechanism 5, pressurizing mechanism 2 installs on heating mechanism 1 upper end, rotating mechanism 3 installs in heating mechanism 1, supporting mechanism 4 installs on rotating mechanism 3, cooling mechanism 5 installs on heating mechanism 1 lower end;

[0022] Heating mechanism 1 carries out heating, pressurizing mechanism 2 carries out pressurizing, rotating mechanism 3 carries out rotation, supporting mechanism 4 carries out support, cooling mechanism 5 carries out cooling;

[0023] Heating mechanism 1 includes heating bin 11 and microwave heating plate 12, and microwave heating plate 12 is installed in heating bin 11;

[0024] Pressurizing mechanism 2 includes sealing cover 21 and booster pump 22, and sealing cover 21 is hinged to the upper end of heating bin 11, and booster pump 22 is installed on the upper end of sealing cover 21;

[0025] The rotating mechanism 3 comprises a rotating table 31, a slave gear 32, a main gear 33 and a first motor 34, the rotating table 31 is rotatably installed in the heating bin 11, the slave gear 32 is installed on the rotating table 31, the main gear 33 is rotatably installed in the heating bin 11 and is in mesh with the slave gear 32, and the first motor 34 is installed in the heating bin 11 and is connected with the input end of the main gear 33;

[0026] The supporting mechanism 4 comprises eight sets of supporting plates 41, sixteen sets of connecting rods 42, a top plate 43, a lead screw 44, a worm gear 45, a second motor 46 and a worm 47, each set of the supporting plates 41 is rotatably connected with two sets of the connecting rods 42, the eight sets of the connecting rods 42 are rotatably installed on the upper end of the rotating table 31, the top plate 43 is rotatably connected with the other eight sets of the connecting rods 42, the lead screw 44 is installed on the lower end of the top plate 43, the worm gear 45 is rotatably installed in the heating bin 11 and is in screw thread cooperation with the lead screw 44, the second motor 46 is installed in the heating bin 11, the input end of the worm 47 is connected with the output end of the second motor 46, and the worm 47 is in screw thread cooperation with the worm gear 45;

[0027] The cooling mechanism 5 comprises a water bin 51, a water pump 52, a spray head 53 and a water pipe 54, the water bin 51 is installed on the lower end of the heating bin 11, the water pump 52 is installed on the left end of the water bin 51, the spray head 53 is installed in the heating bin 11 and is connected with the output end of the water pump 52 through the water pipe 54;

[0028] When the second motor 46 is turned on to drive the worm 47 to rotate, the worm 47 is in screw thread cooperation with the worm gear 45 to drive the worm gear 45 to rotate, and the worm gear 45 is in screw thread cooperation with the lead screw 44 to drive the lead screw 44 to move to support the top plate 43, so that the top plate 43 supports the supporting plates 41 through the connecting rods 42 to support the material, the heating bin 11 is sealed by the sealing cover 21, the material is pressurized by turning on the booster pump 22, the material is heated by the microwave heating plate 12, and the main gear 33 is driven to rotate by turning on the first motor 34, the main gear 33 is in mesh with the slave gear 32 to drive the rotating table 31 to rotate, and the material is cooled by turning on the water pump 52 to spray water through the water pipe 54 and the spray head 53 after vulcanization, so that the material can be internally supported during the vulcanization of the aviation radial tire, the deformation of the material during the vulcanization is reduced, and the processing quality is improved.

[0029] As Figures 1 to 4As shown, the aviation meridian tire vulcanizing machine of the utility model, when working, through the transmission of opening motor two 46 to worm 47 to make worm 47 rotate, worm 47 rotates simultaneously with worm gear 45 to make worm gear 45 rotate, worm gear 45 rotates simultaneously with lead screw 44 to make lead screw 44 move to support top plate 43, so that top plate 43 cooperates with connecting rod 42 to support support plate 41 and support the material, the heating bin 11 is sealed through the sealing cover 21, the material is pressurized through the opening of the booster pump 22, the material is heated through the microwave heating plate 12, and at the same time, the main gear 33 is rotated through the transmission of opening motor one 34 to the main gear 33, the main gear 33 is rotated simultaneously with the gear 32 to make the turntable 31 rotate, and the material is cooled through the opening of the water pump 52 through the water pipe 54 cooperates with the nozzle 53 after vulcanization.

[0030] The microwave heating plate 12, the booster pump 22, the motor one 34, the motor two 46 and the water pump 52 of the utility model are purchased on the market, and the technical personnel in the industry only need to install and operate according to the attached instruction manual, and the technical personnel in the field do not need to pay creative labor.

[0031] The main function realized by the utility model is that: in the aviation meridian tire vulcanization working process, the support mechanism and the rotating mechanism are arranged, so that the material can be internally supported in the aviation meridian tire vulcanization process, so that the deformation of the material in the vulcanization process is reduced, and the processing quality is improved.

[0032] The above only is the preferred implementation mode of the utility model, and it should be pointed out that, for ordinary technical personnel in the technical field, on the premise of not departing from the technical principle of the utility model, a plurality of improvements and modifications can be made, and the improvements and modifications should be regarded as the protection range of the utility model.

Claims

1. An aviation radial tire vulcanizer, comprising a heating mechanism (1); characterized in that: The heating device further comprises a pressurizing mechanism (2), a rotating mechanism (3), a supporting mechanism (4) and a cooling mechanism (5), wherein the pressurizing mechanism (2) is mounted on the upper end of the heating mechanism (1), the rotating mechanism (3) is mounted inside the heating mechanism (1), the supporting mechanism (4) is mounted on the rotating mechanism (3), and the cooling mechanism (5) is mounted on the lower end of the heating mechanism (1); The heating mechanism (1) performs heating, the pressurizing mechanism (2) performs pressurizing, the rotating mechanism (3) performs rotation, the supporting mechanism (4) performs support, and the cooling mechanism (5) performs cooling.

2. The aviation radial tire vulcanizer according to claim 1, characterized in that: The heating mechanism (1) comprises a heating chamber (11) and a microwave heating plate (12), wherein the microwave heating plate (12) is installed in the heating chamber (11).

3. The aviation radial tire vulcanizer according to claim 2, characterized in that: The pressurizing mechanism (2) comprises a sealing cover (21) and a booster pump (22). The sealing cover (21) is hinged to the upper end of the heating chamber (11), and the booster pump (22) is installed on the upper end of the sealing cover (21).

4. The aviation radial tire vulcanizer according to claim 2, characterized in that: The rotating mechanism (3) includes a turntable (31), a slave gear (32), a main gear (33) and a motor (34). The turntable (31) is rotatably mounted in the heating chamber (11), the slave gear (32) is mounted on the turntable (31), the main gear (33) is rotatably mounted in the heating chamber (11), and the main gear (33) is meshed with the slave gear (32). The motor (34) is mounted in the heating chamber (11), and the output end of the motor (34) is connected to the input end of the main gear (33).

5. The aviation radial tire vulcanizer according to claim 4, characterized in that: The supporting mechanism (4) comprises eight groups of supporting plates (41), sixteen groups of connecting rods (42), a top plate (43), a lead screw (44), a worm gear (45), a second motor (46) and a worm (47). The eight groups of supporting plates (41) are rotatably connected to two groups of connecting rods (42), and the eight groups of connecting rods (42) are rotatably mounted on the upper end of the turntable (31). The top plate (43) is rotatably connected to the other eight groups of connecting rods (42). The lead screw (44) is mounted on the lower end of the top plate (43). The worm gear (45) is rotatably mounted in the heating chamber (11), and the worm gear (45) and the lead screw (44) are threadedly matched. The second motor (46) is mounted in the heating chamber (11). The input end of the worm gear (47) is connected to the output end of the second motor (46), and the worm gear (47) and the worm gear (45) are threadedly matched.

6. The aviation radial tire vulcanizer according to claim 2, characterized in that: The cooling mechanism (5) comprises a water tank (51), a water pump (52), a nozzle (53) and a water pipe (54). The water tank (51) is installed at the lower end of the heating tank (11), the water pump (52) is installed at the left end of the water tank (51), the nozzle (53) is installed in the heating tank (11), and the output end of the water pump (52) is connected to the input end of the nozzle (53) through the water pipe (54).

Images