An aviation tire vulcanization processing device

Abstract

The utility model relates to the technical field of aircraft tire processing, and discloses an aircraft tire vulcanization processing device, including a base, a processing mechanism is fixedly arranged on the top surface of the base, and a cooling mechanism is fixedly arranged on the back end surface of the processing mechanism; the processing mechanism includes a processing part and a power part, and the side surface of the power part is fixedly connected to the side surface of the processing part; the processing part includes a fixed mold, and the bottom surface of the fixed mold is fixedly connected to the top surface of the base; the cooling mechanism includes a cooling part and a clamping part, and the side surface of the clamping part is fixedly connected to the side surface of the cooling part; the clamping part includes a fixed block, and the bottom surface of the fixed block is fixedly connected to the bottom surface inside the fixed mold. By providing a cooling mechanism and by providing the cooperation of a spring and a fixed block, when different aircraft tires are placed inside the fixed mold, the clamping block can be quickly adjusted to fix and clamp the aircraft tire, and the scope of application is wide, so that there will be no positional offset during the vulcanization processing of the aircraft tire.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation tire processing, in particular to an aviation tire vulcanization processing device. Background Art

[0002] Tires need to be vulcanized during production. After vulcanization, the tires are in a high temperature state, so they need to be cooled down.

[0003] A Chinese patent discloses a tire vulcanization processing device, with the authorization announcement number CN219855589U, which includes a vulcanization mold, a heat exchange medium storage box and a liquid inlet conduit; the vulcanization mold is provided with a first accommodating chamber and a cooling chamber, the cooling chamber covers the first accommodating chamber, and the first accommodating chamber is used to place the tire blank; the heat exchange medium storage box stores heat exchange medium, the cooling chamber is connected to the heat exchange medium storage box through the liquid inlet conduit, and the heat exchange medium can flow from the heat exchange medium storage box into the cooling chamber, which can effectively improve the cooling efficiency of the tire after vulcanization processing.

[0004] However, there are still the following disadvantages: when the tire vulcanization processing device is performing tire vulcanization processing, it is impossible to adjust and clamp aircraft tires of different sizes accordingly, so it is urgent to design an aircraft tire vulcanization processing device. Utility Model Content

[0005] The utility model aims to provide an aviation tire vulcanization processing device to solve the problems raised in the above background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation tire vulcanization processing device comprises a base, a processing mechanism is fixedly arranged on the top surface of the base, and a cooling mechanism is fixedly arranged on the back end surface of the processing mechanism;

[0007] The processing mechanism comprises a processing part and a power part, and the side surface of the power part and the side surface of the processing part are fixedly connected;

[0008] The processing part comprises a fixed die, the bottom surface of the fixed die is fixedly connected to the top surface of the base;

[0009] The cooling mechanism comprises a cooling portion and a clamping portion, and a side surface of the clamping portion is fixedly connected to a side surface of the cooling portion;

[0010] The clamping part comprises a fixed block, the bottom surface of the fixed block is fixedly connected to the inner bottom surface of the fixed mold, the inner wall of the fixed block is fixedly provided with a spring, the outer side surface of the spring is fixedly provided with a clamping block, and the side surface of the clamping block is in frictional sliding contact with the inner wall of the fixed block.

[0011] Preferably, two support plates are fixedly provided on the top surfaces of the left and right ends of the base respectively, and fixing plates are fixedly provided on the top surfaces of the two support plates. Motor A is fixedly provided on the inner wall of the fixing plate, and a bidirectional threaded rod is fixedly provided on the right end surface of the output rod of motor A.

[0012] Preferably, the right end face of the bidirectional threaded rod and the inner wall of the fixed plate are rotatably connected by a bearing seat, and two moving blocks are threadedly sleeved on the left and right end surfaces of the bidirectional threaded rod respectively, and the side faces of the moving blocks are frictionally and slidably connected to the inner wall of the fixed plate.

[0013] Preferably, a connecting plate A is hingedly provided inside the moving block at the left end, and a connecting plate B is hingedly provided inside the moving block at the right end. A connecting rod is fixedly provided on the inner wall of the bottom end of the connecting plate A, and the surface of the connecting rod and the inner wall of the connecting plate B are hinged.

[0014] Preferably, a movable mold is fixedly provided on the bottom surface of the connecting rod, the bottom surface of the movable mold is in sealing contact with the top surface of the fixed mold, a clamping ring is fixedly provided on the bottom surface of the movable mold, and the surface of the clamping ring is sealingly clamped with the inner wall of the fixed mold.

[0015] Preferably, two fixing rods are fixedly provided on the back sides of the two support plates respectively, a device block is fixedly provided on the inner sides of the two fixing rods, a motor B is fixedly provided on the inner wall of the device block, a fan blade is fixedly provided on the front side of the output rod of the motor B, and a protective net is fixedly provided on the inner wall of the device block.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] 1. The aircraft tire vulcanization processing device is provided with a cooling mechanism, and the cooperation of a spring and a fixing block is provided, so that when different aircraft tires are placed inside a fixed mold, the clamping block can be quickly adjusted to fix and clamp the aircraft tire, and has a wide range of applications, so that there will be no positional deviation during the vulcanization processing of the aircraft tire;

[0018] 2. The aircraft tire vulcanization processing device is provided with a motor B and a fan blade, so that the strong wind generated by the rotation of the fan blade can cool the fixed mold and the movable mold, so that the aircraft tire can be quickly cooled after vulcanization, which improves the efficiency of tire molding and vulcanization on the one hand, and prevents the staff from accidentally touching the tire and causing safety problems on the other hand;

[0019] 3. The aviation tire vulcanization processing device is provided with a processing mechanism, and through the cooperation of the motor A and the bidirectional threaded rod, the two moving blocks move in opposite directions, and the connecting plate A and the connecting plate B move in a folded manner, so that the movable mold can automatically move up and down, and the operation is fully automated, saving time, effort and labor. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a three-dimensional schematic diagram of the front structure of the utility model;

[0021] Figure 2 It is a three-dimensional cross-sectional schematic diagram of the front structure of the utility model;

[0022] Figure 3 It is a three-dimensional schematic diagram of the back structure of the utility model;

[0023] Figure 4 It is a three-dimensional cross-sectional schematic diagram of the right side structure of the utility model;

[0024] Figure 5 For this utility model Figure 4 A three-dimensional enlarged schematic diagram of the structure of area A in the middle.

[0025] In the figure: 1. base; 2. processing mechanism; 201. support plate; 202. fixed plate; 203. motor A; 204. bidirectional threaded rod; 205. moving block; 206. connecting plate A; 207. connecting plate B; 208. connecting rod; 209. moving mold; 210. fixed mold; 211. retaining ring; 3. cooling mechanism; 301. fixed rod; 302. device block; 303. motor B; 304. fan blade; 305. protective net; 306. fixed block; 307. spring; 308. clamping block. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0027] Embodiment 1

[0028] See also Figure 1-Figure 5 As shown, an aircraft tire vulcanization processing device includes a base 1, a processing mechanism 2 is fixedly arranged on the top surface of the base 1, and a cooling mechanism 3 is fixedly arranged on the back end surface of the processing mechanism 2; the processing mechanism 2 includes a processing part and a power part, and the side surface of the power part is fixedly connected to the side surface of the processing part; the processing part includes a fixed mold 210, and the bottom surface of the fixed mold 210 is fixedly connected to the top surface of the base 1; the cooling mechanism 3 includes a cooling part and a clamping part, and the side surface of the clamping part is fixedly connected to the side surface of the cooling part; the clamping part includes a fixed block 306, the bottom surface of the fixed block 306 is fixedly connected to the inner bottom surface of the fixed mold 210, a spring 307 is fixedly arranged on the inner wall of the fixed block 306, and a clamping block 308 is fixedly arranged on the outer side surface of the spring 307, and the clamping block 308 is a round rod with an arc plate arranged on the outer end, and the side surface of the clamping block 308 is in friction and sliding contact with the inner wall of the fixed block 306;

[0029] During operation, the aircraft tire that has completed the molding step is placed inside the fixed mold 210, and the clamping block 308 is repeatedly contracted and rebounded by squeezing the four springs 307, so that the inner tube of the aircraft tire is quickly squeezed and fixed.

[0030] Further, two support plates 201 are fixedly arranged on the top surfaces of the left and right ends of the base 1, and a fixing plate 202 is fixedly arranged on the top surfaces of the two support plates 201. A motor A203 is fixedly arranged on the inner wall of the fixing plate 202. The model of the motor A203 is Y2-112M-6, and a bidirectional threaded rod 204 is fixedly arranged on the right end surface of the output rod of the motor A203.

[0031] During operation, the motor A203 is started to rotate the bidirectional threaded rod 204 .

[0032] Furthermore, the right end surface of the bidirectional threaded rod 204 and the inner wall of the fixed plate 202 are rotatably connected by a bearing seat, and two moving blocks 205 are respectively threadedly sleeved on the left and right end surfaces of the bidirectional threaded rod 204, and the side surfaces of the moving blocks 205 are frictionally and slidably connected with the inner wall of the fixed plate 202;

[0033] During operation, the motor A203 is started to rotate the bidirectional threaded rod 204, and the two moving blocks 205 move in opposite directions through the action of two reverse threads.

[0034] Furthermore, a connecting plate A206 is hingedly provided inside the left end moving block 205, and a connecting plate B207 is hingedly provided inside the right end moving block 205. A connecting rod 208 is fixedly provided on the inner wall of the bottom end of the connecting plate A206, and the surface of the connecting rod 208 is hingedly provided with the inner wall of the connecting plate B207;

[0035] During operation, the bidirectional threaded rod 204 rotates, and through the action of two reverse threads, the two moving blocks 205 move in opposite directions. Through the action of the hinged rod of the moving block 205 and the hinged rod of the connecting plate A206 and the connecting plate B207, the connecting plate A206 and the connecting plate B207 are folded downward.

[0036] Furthermore, a movable mold 209 is fixedly provided on the bottom surface of the connecting rod 208, the bottom surface of the movable mold 209 is in sealing contact with the top surface of the fixed mold 210, a ring groove is fixedly provided on the top surface of the fixed mold 210, a clamping ring 211 is fixedly provided on the bottom surface of the movable mold 209, and the surface of the clamping ring 211 is in sealing connection with the inner wall of the fixed mold 210;

[0037] During operation, the connecting plate A206 and the connecting plate B207 are folded downward, which drives the movable mold 209 to move downward, so that the clamping ring 211 and the clamping groove of the fixed mold 210 are sealed and clamped.

[0038] Further, two fixing rods 301 are fixedly arranged on the back of the two support plates 201, and a device block 302 is fixedly arranged on the inner side of the two fixing rods 301. A motor B303 is fixedly arranged on the inner wall of the device block 302. A fan blade 304 is fixedly arranged on the front of the output rod of the motor B303. A protective net 305 is fixedly arranged on the inner wall of the device block 302;

[0039] During operation, the motor B303 is started to rotate the fan blades 304. The rotation generates strong winds that can quickly cool the surface of the tire. After the vulcanization is completed, the aircraft tire can be taken out.

[0040] Working principle: When in use, first place the aircraft tire that has completed the molding step inside the fixed mold 210, and by squeezing the four springs 307, the clamping block 308 is repeatedly contracted and rebounded, so as to quickly squeeze and fix the inner tube of the aircraft tire, start the motor A203, so that the bidirectional threaded rod 204 rotates, and the two moving blocks 205 move in opposite directions through the action of the two reverse threads, and the connecting plates A206 and B207 are folded downward by the hinge rod of the moving block 205 and the hinge rod of the connecting plate A206 and the connecting plate B207, which drives the moving mold 209 to move downward, so that the retaining ring 211 and the groove of the fixed mold 210 are sealed and clamped, so that the fixed mold 210 and the moving mold 209 are sealed and then subjected to high temperature and high pressure vulcanization treatment, when the vulcanization is completed, start the motor B303, so that the fan blade 304 rotates, and its rotation generates strong wind to quickly cool its surface, and the aircraft tire can be taken out after the vulcanization is completed.

[0041] The above description is only a preferred embodiment of the utility model and is not intended to limit the utility model. Although the utility model is described in detail with reference to the above embodiments, those skilled in the art can still modify the technical solutions recorded in the above embodiments or replace some of the technical features therein by equivalents. Any modification, equivalent replacement, similar improvement, etc. made within the theoretical and principle content of the utility model shall be included in the protection scope of the utility model.

Claims

1. An aircraft tire vulcanization processing device, comprising a base (1), characterized in that: A processing mechanism (2) is fixedly arranged on the top surface of the base (1), and a cooling mechanism (3) is fixedly arranged on the back end surface of the processing mechanism (2); The processing mechanism (2) comprises a processing part and a power part, and the side surface of the power part and the side surface of the processing part are fixedly connected; The processing part comprises a fixed mold (210), the bottom surface of the fixed mold (210) and the top surface of the base (1) being fixedly connected; The cooling mechanism (3) comprises a cooling portion and a clamping portion, and the side surface of the clamping portion and the side surface of the cooling portion are fixedly connected; The clamping portion comprises a fixed block (306), the bottom surface of the fixed block (306) is fixedly connected to the inner bottom surface of the fixed mold (210), a spring (307) is fixedly arranged on the inner wall of the fixed block (306), a clamping block (308) is fixedly arranged on the outer side surface of the spring (307), and the side surface of the clamping block (308) is in frictional sliding contact with the inner wall of the fixed block (306).

2. The aircraft tire vulcanization processing device according to claim 1, characterized in that: Two support plates (201) are fixedly arranged on the top surfaces of the left and right ends of the base (1), respectively; a fixing plate (202) is fixedly arranged on the top surfaces of the two support plates (201); a motor A (203) is fixedly arranged on the inner wall of the fixing plate (202); and a bidirectional threaded rod (204) is fixedly arranged on the right end surface of the output rod of the motor A (203).

3. The aircraft tire vulcanization processing device according to claim 2, characterized in that: The right end surface of the bidirectional threaded rod (204) and the inner wall of the fixed plate (202) are rotatably connected by a bearing seat, and two moving blocks (205) are respectively threadedly sleeved on the left and right end surfaces of the bidirectional threaded rod (204), and the side surfaces of the moving blocks (205) are frictionally and slidably connected to the inner wall of the fixed plate (202).

4. The aircraft tire vulcanization processing device according to claim 3, characterized in that: The movable block (205) at the left end is internally hinged with a connecting plate A (206), and the movable block (205) at the right end is internally hinged with a connecting plate B (207). A connecting rod (208) is fixedly provided on the inner wall of the bottom end of the connecting plate A (206), and the surface of the connecting rod (208) is hinged to the inner wall of the connecting plate B (207).

5. The aircraft tire vulcanization processing device according to claim 4, characterized in that: A movable mold (209) is fixedly arranged on the bottom surface of the connecting rod (208), and the bottom surface of the movable mold (209) is in sealing contact with the top surface of the fixed mold (210). A retaining ring (211) is fixedly arranged on the bottom surface of the movable mold (209), and the surface of the retaining ring (211) is in sealing clamping connection with the inner wall of the fixed mold (210).

6. The aircraft tire vulcanization processing device according to claim 2, characterized in that: Two fixing rods (301) are fixedly arranged on the backs of the two support plates (201), respectively; a device block (302) is fixedly arranged on the inner sides of the two fixing rods (301); a motor B (303) is fixedly arranged on the inner wall of the device block (302); a fan blade (304) is fixedly arranged on the front of the output rod of the motor B (303); and a protective net (305) is fixedly arranged on the inner wall of the device block (302).

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