Auxiliary heat dissipation structure of central mechanism of composite vulcanizing machine

Abstract

The utility model provides an auxiliary heat dissipation structure of a central mechanism of a composite vulcanizing machine, which comprises the central mechanism, a main seat disc used for mounting and fixing is arranged in the central mechanism, and a central mechanism main column is arranged below the main seat disc. Compared with the prior art, the heat dissipation device has the advantages that the center mechanism, the first auxiliary heat dissipation assembly and the second auxiliary heat dissipation assembly are additionally arranged, the first auxiliary heat dissipation assembly and the second auxiliary heat dissipation assembly are symmetrically installed on the outer side of the center mechanism main column, and heat generated by the center mechanism is guided into the heat exchange heat dissipation cavity; cold air is introduced through the heat exchange heat dissipation pipe to achieve cold and heat exchange, the contact area between the heat dissipation fins and the outside is increased, the heat dissipation effect is improved, heat dissipation disturbance is conducted on the outer portions of the heat dissipation fins through the disturbance base, heat dissipation can be assisted, and the heat dissipation effect can be improved; the two sets of heat exchange radiating pipes are communicated in a sealed mode and connected through the first butt-joint plate and the second butt-joint plate, and disassembly and assembly can be assisted for use.

Description

Technical Field

[0001] This utility model belongs to the field of vulcanizing machine technology, and specifically relates to an auxiliary heat dissipation structure for the central mechanism of a composite vulcanizing machine. Background Technology

[0002] A compound vulcanizing machine is a specialized piece of equipment used for molding and vulcanizing rubber or plastic products. It combines the molding and vulcanization processes to improve production efficiency and ensure consistent product quality. The central mechanism of a compound vulcanizing machine is a crucial component, and its specific structure varies between different machines. The central mechanism houses numerous actuators, generating heat during operation. Heat accumulation can affect the performance of the central mechanism, consequently impacting the quality of the final molded product. In commonly used compound vulcanizing machines, the central mechanism typically relies on natural heat dissipation, external fans for airflow disturbance, or water cooling and complex piping systems for heat dissipation. However, these methods are not highly effective at heat dissipation. Furthermore, water leakage, for example, can wet the equipment, potentially leading to malfunctions.

[0003] In summary, we hope to propose a new structure to solve the aforementioned technical problems. Utility Model Content

[0004] To address the shortcomings of existing technologies, the purpose of this utility model is to provide an auxiliary heat dissipation structure for the central mechanism of a composite vulcanizing machine, thereby solving the problems mentioned in the background art.

[0005] This utility model is achieved through the following technical solution: an auxiliary heat dissipation structure for the central mechanism of a composite vulcanizing machine, comprising: a central mechanism, wherein a main base plate for mounting and fixing is provided in the central mechanism, a main column of the central mechanism is provided below the main base plate, an auxiliary heat dissipation component one for assisting the heat dissipation of the central mechanism is provided on the right side of the main column of the central mechanism, an auxiliary heat dissipation component two is provided on the left side of the auxiliary heat dissipation component one, a heat dissipation main ring seat is provided in the auxiliary heat dissipation component one, a heat exchange heat dissipation cavity is opened on the side of the heat dissipation main ring seat near the center, a heat exchange heat dissipation pipe for achieving heat exchange and auxiliary heat dissipation is fixedly connected to the inner side of the heat exchange heat dissipation cavity, a number of sets of heat dissipation fins are fixedly connected to the outer side of the heat dissipation main ring seat, and two sets of disturbance seats for disturbing the air are fixedly connected to the outer side of the heat dissipation fins in a vertically symmetrical arrangement.

[0006] In a preferred embodiment, a mounting ring seat 1 is fixedly connected above the main heat dissipation ring seat, and a mounting ring seat 2 is provided in the auxiliary heat dissipation component 2. A main heat dissipation ring seat 2 is fixedly connected below the mounting ring seat 2. The auxiliary heat dissipation component 1 and the auxiliary heat dissipation component 2 are connected to the central mechanism through the mounting ring seat 1 and the mounting ring seat 2.

[0007] In a preferred embodiment, the second heat dissipation main ring seat has the same structure as the heat dissipation main ring seat and is also provided with a heat exchange heat dissipation cavity, a heat exchange heat dissipation pipe, heat dissipation fins and a disturbance seat. The disturbance seat has several sets of disturbance airflow holes on both the upper and lower sides.

[0008] In a preferred embodiment, a disturbance connecting pipe is fixedly connected to the upper starting position of the disturbance seat in the first auxiliary heat dissipation component. The disturbance connecting pipe is connected to an external air pipe. The disturbance seats of the first auxiliary heat dissipation component and the second auxiliary heat dissipation component are interconnected. The disturbance connecting pipe introduces external gas into the disturbance seat and sprays it out through a number of disturbance airflow holes, which disturbs the heat dissipation fins and prevents the heat from accumulating and affecting the heat dissipation effect.

[0009] In a preferred embodiment, the heat exchange heat dissipation pipes of the auxiliary heat dissipation component one and the auxiliary heat dissipation component two form a connected structure and are arranged in a spiral structure. A cooling inlet pipe is fixedly connected to the upper starting position of the heat exchange heat dissipation pipe of the auxiliary heat dissipation component one.

[0010] In a preferred embodiment, a cooling outlet pipe is fixedly connected to the lower end of the heat exchange heat dissipation pipe of the auxiliary heat dissipation component. The cooling inlet pipe is connected to an external refrigeration device. The outer surface of the heat dissipation fins is coated with a nano-alumina coating to enhance the heat dissipation effect. External cold air is introduced into the heat exchange heat dissipation pipe through the cooling inlet pipe and flows out through the cooling outlet pipe to achieve cold air circulation. The heat in the heat exchange heat dissipation cavity is cooled down through heat exchange.

[0011] In a preferred embodiment, a connecting groove is provided on the left side of the heat dissipation main ring seat at the heat exchange heat dissipation pipe connection point, and a sealing ring is fixedly connected to the left side of the heat dissipation main ring seat at the connecting groove.

[0012] The second heat dissipation main ring seat is provided with a sealing groove at the connection of the heat exchange heat dissipation pipe, and the sealing ring and the sealing groove are mutually sealed and fitted.

[0013] In a preferred embodiment, a set of docking plates is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat, and a docking block is fixedly connected to the left side of the docking plate. A set of docking plates is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat.

[0014] The right side of the second docking plate is provided with a docking groove, and the upper surface of the second docking plate and the docking block are provided with docking thread holes. The docking block and the docking groove are interlocked. The heat exchange heat dissipation pipes in the first auxiliary heat dissipation component and the second auxiliary heat dissipation component are sealed and connected. The two components are connected by bolts to complete the symmetrical installation and can assist in disassembly and assembly.

[0015] After adopting the above technical solution, the beneficial effects of this utility model are:

[0016] 1. By adding a central mechanism, auxiliary heat dissipation component one and auxiliary heat dissipation component two, the auxiliary heat dissipation component one and auxiliary heat dissipation component two are installed in a symmetrical structure on the outside of the main column of the central mechanism. The heat generated by the central mechanism is introduced into the heat exchange heat dissipation cavity, and the cold air introduced through the heat exchange heat dissipation pipe achieves heat exchange. The heat dissipation fins increase the contact area with the outside to improve the heat dissipation effect. The disturbance seat can disturb the heat dissipation outside the heat dissipation fins to assist in heat dissipation and improve the heat dissipation effect.

[0017] 2. By adding auxiliary heat dissipation component one and auxiliary heat dissipation component two, the heat exchange heat dissipation pipes in auxiliary heat dissipation component one and auxiliary heat dissipation component two are sealed and connected, and the splicing is symmetrically installed by bolt connection between docking plate one and docking plate two, which can assist in disassembly and assembly. Attached Figure Description

[0018] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a schematic diagram of the overall structure of the auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine according to the present invention.

[0020] Figure 2 This is a schematic diagram of the central mechanism in the auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine according to the present invention.

[0021] Figure 3 This is a schematic diagram of the left side of the auxiliary heat dissipation component one in the auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine according to the present invention.

[0022] Figure 4 This is a schematic diagram of the right side of the auxiliary heat dissipation component one in the auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine according to the present invention.

[0023] Figure 5 This is a schematic diagram of the auxiliary heat dissipation component two in the auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine according to the present invention.

[0024] In the diagram, 100 is the central mechanism, 101 is the main support plate, and 102 is the main column of the central mechanism.

[0025] 200-Auxiliary heat dissipation component one, 201-Mounting ring seat one, 202-Main heat dissipation ring seat, 203-Heat exchange heat dissipation cavity, 204-Heat exchange heat dissipation pipe, 205-Connecting groove, 206-Sealing ring, 207-Heat dissipation fins, 208-Disturbance seat, 209-Disturbance airflow hole, 210-Disturbance connecting pipe, 211-Cooling inlet pipe, 212-Cooling outlet pipe, 213-Matching plate one, 214-Matching block;

[0026] 300-Auxiliary heat dissipation component II, 301-Mounting ring seat II, 302-Main heat dissipation ring seat II, 303-Sealing groove, 304-Matching plate II, 305-Matching groove, 306-Matching threaded hole. Detailed Implementation

[0027] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0028] Please see Figures 1-5 As the first embodiment of this utility model:

[0029] An auxiliary heat dissipation structure for the central mechanism of a composite vulcanizing machine includes: a central mechanism 100, a main base plate 101 for mounting and fixing is provided in the central mechanism 100, and a central mechanism main column 102 is provided below the main base plate 101.

[0030] An auxiliary heat dissipation component 200 for assisting the heat dissipation of the central mechanism 100 is provided on the right side of the main column 102 of the central mechanism. An auxiliary heat dissipation component 200 is provided on the left side of the auxiliary heat dissipation component 200. A heat dissipation main ring seat 202 is provided in the auxiliary heat dissipation component 200. A heat exchange heat dissipation cavity 203 is opened on the side of the end of the heat dissipation main ring seat 202 near the center.

[0031] A heat exchange heat dissipation pipe 204 for auxiliary heat dissipation to achieve heat exchange is fixedly connected to the inner side of the heat exchange heat dissipation cavity 203. Several sets of heat dissipation fins 207 are fixedly connected to the outer side of the heat dissipation main ring seat 202. Two sets of disturbance seats 208 for disturbing the air are fixedly connected to the outer side of the heat dissipation fins 207 in an up-down symmetrical arrangement.

[0032] A mounting ring seat 201 is fixedly connected above the main heat dissipation ring seat 202. An auxiliary heat dissipation component 200 is provided with a mounting ring seat 301. The main heat dissipation ring seat 202 is fixedly connected below the mounting ring seat 201. The auxiliary heat dissipation component 200 and the auxiliary heat dissipation component 200 are connected to the central mechanism 100 through the mounting ring seat 201 and the mounting ring seat 201.

[0033] The heat dissipation main ring seat 202 has the same structure as the heat dissipation main ring seat 202 and is also provided with a heat exchange heat dissipation cavity 203, a heat exchange heat dissipation pipe 204, heat dissipation fins 207 and a disturbance seat 208. The disturbance seat 208 has several sets of disturbance airflow holes 209 on both the upper and lower sides.

[0034] A disturbance connecting pipe 210 is fixedly connected to the upper starting position of the disturbance seat 208 in the auxiliary heat dissipation component 1 200. The disturbance connecting pipe 210 is connected to the external air pipe. The disturbance seats 208 of the auxiliary heat dissipation component 1 200 and the auxiliary heat dissipation component 2 300 are interconnected. The disturbance connecting pipe 210 introduces the external gas into the disturbance seat 208 and sprays it out through a number of disturbance airflow holes 209, which disturbs the heat dissipation fins 207 and prevents the heat from accumulating and affecting the heat dissipation effect.

[0035] The heat exchange heat dissipation pipes 204 of the auxiliary heat dissipation component 1 200 and the auxiliary heat dissipation component 2 300 form a connected structure and are arranged in a spiral structure. A cooling inlet pipe 211 is fixedly connected to the upper starting position of the heat exchange heat dissipation pipe 204 of the auxiliary heat dissipation component 1 200.

[0036] The lower end of the heat exchange heat dissipation pipe 204 of the auxiliary heat dissipation component 200 is fixedly connected to a cooling outlet pipe 212. The cooling inlet pipe 211 is connected to an external refrigeration device. The outer surface of the heat dissipation fins 207 is coated with a nano-alumina coating to enhance the heat dissipation effect. External cold air is introduced into the heat exchange heat dissipation pipe 204 through the cooling inlet pipe 211 and then discharged through the cooling outlet pipe 212 to achieve cold air circulation. The heat in the heat exchange heat dissipation cavity 203 is cooled down through heat exchange.

[0037] Specifically, auxiliary heat dissipation components 200 and 300 are connected to the central mechanism 100 via mounting ring seat 1 201 and mounting ring seat 2 301, and are arranged in a symmetrical structure. The heat generated by the operation of the central mechanism 100 is dissipated into the heat exchange heat dissipation cavity 203. External cold air is introduced into the heat exchange heat dissipation pipe 204 through the cooling inlet pipe 211, and after flowing, it is discharged through the cooling outlet pipe 212 to achieve cold air circulation. The heat in the heat exchange heat dissipation cavity 203 is cooled by heat exchange. Heat dissipation fins 207 are fixedly installed on the outer side of the heat dissipation main ring seat 202 and the heat dissipation main ring seat 2 302, and their outer surfaces are coated with nano-alumina coating to enhance heat dissipation.

[0038] Secondly, a disturbance seat 208 is fixedly installed on the outside of the heat dissipation fins 207. The disturbance connecting pipe 210 introduces external gas into the disturbance seat 208 and sprays it out through a number of disturbance airflow holes 209. This disturbs the heat dissipation lost on the outside of the heat dissipation fins 207 to prevent it from accumulating and affecting the heat dissipation effect, thereby assisting in heat dissipation and improving the heat dissipation effect.

[0039] Please see Figure 1 and Figures 3-5 As a second embodiment of this utility model:

[0040] A connecting groove 205 is provided on the left side of the heat dissipation main ring seat 202 at the connection point of the heat exchange heat dissipation pipe 204, and a sealing ring 206 is fixedly connected to the connecting groove 205 on the left side of the heat dissipation main ring seat 202.

[0041] The heat dissipation main ring seat 302 is provided with a sealing groove 303 at the connection of the heat exchange heat dissipation pipe 204, and the sealing ring 206 and the sealing groove 303 are mutually sealed and fitted.

[0042] A set of docking plates 213 is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat 202. A docking block 214 is fixedly connected to the left side of the docking plate 213. A set of docking plates 304 is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat 202.

[0043] A docking groove 305 is provided on the right side of the docking plate 204. A docking threaded hole 306 is provided on the upper surface of both the docking plate 204 and the docking block 214. The docking block 214 and the docking groove 305 are fitted together. The heat exchange heat dissipation pipe 204 in the auxiliary heat dissipation component 1 200 and the auxiliary heat dissipation component 2 300 are sealed and connected. The symmetrical installation is completed by bolt connection between the docking plate 1 213 and the docking plate 204.

[0044] Based on the first embodiment described above, further, in use, the auxiliary heat dissipation component 200 and the auxiliary heat dissipation component 300 can be symmetrically installed, and at the joint, the sealing ring 206 and the sealing groove 303 are sealed and fitted together, so that the heat exchange heat dissipation pipes 204 of the auxiliary heat dissipation component 200 and the auxiliary heat dissipation component 300 can be sealed and connected. In the docking installation, the docking plate 213 and the docking plate 304 are attached together, and the docking block 214 is embedded in the docking recess 305 and bolts are screwed into the stacked thread hole 306 for connection and fixation, thereby assisting in disassembly and assembly.

[0045] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. An auxiliary heat dissipation structure for the central mechanism of a composite vulcanizing machine, comprising: The central mechanism (100) is characterized in that: the central mechanism (100) is provided with a main base plate (101) for installation and fixing, and a central mechanism main column (102) is provided below the main base plate (101). The outer right end of the main column (102) of the central mechanism is provided with an auxiliary heat dissipation component 1 (200) for assisting the central mechanism (100) in heat dissipation. The left side of the auxiliary heat dissipation component 1 (200) is provided with an auxiliary heat dissipation component 2 (300). The auxiliary heat dissipation component 1 (200) is provided with a heat dissipation main ring seat (202). The side of the heat dissipation main ring seat (202) near the center is provided with a heat exchange heat dissipation cavity (203). The heat exchange heat dissipation cavity (203) is fixedly connected to a heat exchange heat dissipation pipe (204) for achieving auxiliary heat dissipation of heat exchange. The heat dissipation main ring seat (202) is fixedly connected to a number of heat dissipation fins (207) on its outer side. The heat dissipation fins (207) are fixedly connected to two sets of disturbance seats (208) that are symmetrically distributed vertically on their outer sides for disturbing the air.

2. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 1, characterized in that: A mounting ring seat (201) is fixedly connected above the main heat dissipation ring seat (202), and a mounting ring seat (301) is provided in the auxiliary heat dissipation component (300). A main heat dissipation ring seat (302) is fixedly connected below the mounting ring seat (301).

3. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 2, characterized in that: The second heat dissipation main ring seat (302) has the same structure as the heat dissipation main ring seat (202) and is also provided with a heat exchange heat dissipation cavity (203), a heat exchange heat dissipation pipe (204), heat dissipation fins (207) and a disturbance seat (208). The disturbance seat (208) has several sets of disturbance airflow holes (209) on both the upper and lower sides.

4. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 3, characterized in that: The disturbance seat (208) in the first auxiliary heat dissipation component (200) is fixedly connected to the starting position of the disturbance connecting pipe (210), which is connected to the external air pipe. The disturbance seats (208) of the first auxiliary heat dissipation component (200) and the second auxiliary heat dissipation component (300) are interconnected.

5. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 4, characterized in that: The heat exchange heat dissipation pipes (204) of the auxiliary heat dissipation component one (200) and the auxiliary heat dissipation component two (300) form a connected structure and are arranged in a spiral structure. A cooling inlet pipe (211) is fixedly connected to the upper starting position of the heat exchange heat dissipation pipe (204) of the auxiliary heat dissipation component one (200).

6. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 5, characterized in that: The lower end of the heat exchange heat dissipation pipe (204) of the auxiliary heat dissipation component (200) is fixedly connected to a cooling outlet pipe (212), the cooling inlet pipe (211) is connected to an external refrigeration device, and the outer surface of the heat dissipation fins (207) is coated with a nano-alumina coating to enhance the heat dissipation effect.

7. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 2, characterized in that: The left side of the heat dissipation main ring seat (202) is provided with a connecting groove (205) at the connection point of the heat exchange heat dissipation pipe (204), and a sealing ring (206) is fixedly connected to the left side of the heat dissipation main ring seat (202) at the connecting groove (205). The second heat dissipation main ring seat (302) is provided with a sealing groove (303) at the connection of the heat exchange heat dissipation pipe (204), and the sealing ring (206) and the sealing groove (303) are mutually sealed and fitted.

8. The auxiliary heat dissipation structure of the central mechanism of a composite vulcanizing machine as described in claim 7, characterized in that: A set of docking plates (213) is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat (202). A docking block (214) is fixedly connected to the left side of the docking plate (213). A set of docking plates (304) is fixedly connected to both the front and rear ends of the outer side of the heat dissipation main ring seat (302). The right side of the second docking plate (304) is provided with a docking groove (305), and the upper surface of the second docking plate (304) and the docking block (214) are provided with docking thread holes (306). The docking block (214) and the docking groove (305) are fitted together.

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