Intercooling pipe structure with cooling fins

Abstract

The utility model relates to an intercooling pipe structure with radiating fins, which belongs to the technical field of radiating of intercooling pipes and comprises an air delivery pipe, a temperature control box is mounted on the outer wall of the air delivery pipe, an air compressor is arranged in the temperature control box, and a cooling structure for cooling the air compressor is arranged at the bottom of the air delivery pipe. The cooling structure comprises two first intercooling pipe rings which are used for movably installing the air compressor and are arranged on the outer circumferential wall, and a communicating pipe is fixedly installed between the two first intercooling pipe rings. According to the intercooling pipe structure with the cooling fins, the loss of the temperature of low-temperature gas in the first intercooling pipe ring is reduced through the effect of the temperature control box body, the low-temperature gas is conveniently input into the second intercooling pipe ring through the effect of the gas conveying auxiliary pipe, and heat dissipation treatment is effectively conducted on an air compressor through the effect of the cooling fins and the second intercooling pipe ring; and the heat preservation sleeve can reduce emission of low-temperature gas, so that the continuous heat dissipation time of the low-temperature gas to the air compressor is prolonged, and the use amount of cooling gas is reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to a middle cooling pipe heat dissipation technical field, concretely to a middle cooling pipe structure with fin. BACKGROUND

[0002] When the middle cooling pipe is used for the air compressor, it refers to the pipeline connected between the compression part of the air compressor and the cooling system, and its function is to transmit the high-temperature air generated in the compression process to the cooling device for temperature reduction. This pipeline ensures that the temperature and humidity of the compressed air are effectively controlled before entering the next stage or being used, thereby improving the efficiency of the air compressor and the quality of the compressed air, and prolonging the service life of the air compressor. The middle cooling pipe is usually made of materials resistant to high temperature and pressure, and the design should minimize air flow resistance, maintain air flow stability and reduce energy consumption.

[0003] The authorized announcement number CN219101531U discloses a novel middle cooling pipe structure with fin, and the technical scheme is: "including first cylinder cover, second cylinder cover and middle cooling pipe, the outer circle of the middle cooling pipe is uniformly and interval provided with a plurality of heat dissipation fins, the first end of the middle cooling pipe is fixed on the first cylinder cover through the first hollow bolt, and the first cylinder cover, the first hollow bolt and the middle cooling pipe are connected in communication". The beneficial effect is that the plurality of heat dissipation fins are uniformly and interval provided on the outer circle of the middle cooling pipe, which can significantly improve the heat dissipation performance of the middle cooling pipe, reduce the heat loss of the air compressor, improve the working efficiency, and thus enhance the application range of the air compressor.

[0004] The above technical scheme has the following defects: the middle cooling pipe and the heat dissipation fins are completely exposed to the air, and the temperature, humidity, wind speed and dust of the external environment can affect the heat dissipation effect, and the low temperature of the middle cooling pipe and the heat dissipation fins will spread to the surrounding, which cannot effectively preserve the low temperature of the middle cooling pipe and the heat dissipation fins, not only increases the use amount of cooling gas, but also reduces the heat dissipation effect of the air compressor, so a middle cooling pipe structure with fin is proposed to solve the above problems. UTILITY MODEL CONTENTS

[0005] In view of the defects of the prior art, the utility model provides a middle cooling pipe structure with fin, which has the advantages of improving the cooling effect of the middle cooling pipe, and solves the problem that the middle cooling pipe and the heat dissipation fins are completely exposed to the air in use, are affected by the surrounding environment, and the low-temperature gas on the middle cooling pipe and the heat dissipation fins is quickly dissipated, thereby reducing the heat dissipation effect of the air compressor.

[0006] To achieve the above purpose, the utility model provides the following technical scheme:

[0007] A cooling pipe structure with fins, comprising a gas conveying pipe, a temperature control box is mounted on the outer wall of the gas conveying pipe, an air compressor is arranged in the temperature control box, and a cooling structure for cooling the air compressor is arranged at the bottom of the gas conveying pipe;

[0008] The cooling structure comprises two first cooling pipe rings with movable mounting air compressors, two first cooling pipe rings are fixedly mounted with a communication pipe, the outer wall of the gas conveying pipe is fixedly mounted with a gas sub-pipe, the inner wall of the temperature control box is fixedly mounted with a heat preservation sleeve, the inner wall of the heat preservation sleeve is fixedly mounted with a second cooling pipe ring, the inner wall of the second cooling pipe ring is fixedly mounted with four heat dissipation fins, the outer wall of the gas conveying pipe is fixedly mounted with a shunt pipe, one end of the shunt pipe away from the gas conveying pipe is fixedly mounted with a control valve, and the outer wall of the shunt pipe is fixedly mounted with two gas flow pipes.

[0009] Further, two first gas discharge pipes are fixedly mounted on the right side of the second cooling pipe ring, the first gas discharge pipes penetrate the right side of the temperature control box, and the first gas discharge pipes extend to the outside of the temperature control box.

[0010] Further, two second gas discharge pipes are fixedly mounted on the right side of the first cooling pipe ring on the right side, and the gas conveying pipe is fixedly mounted on the outer wall of the first cooling pipe ring on the left side.

[0011] Further, six exhaust holes are arranged on the top and bottom of the temperature control box, and the second gas discharge pipes are arranged in the exhaust holes.

[0012] Further, a supporting rod is fixedly mounted on the left side of the temperature control box, and the supporting rod is fixedly mounted on the right side of the control valve away from the temperature control box.

[0013] Further, a supporting bottom plate is fixedly mounted on the inner bottom wall of the temperature control box, the air compressor is arranged on the top of the supporting bottom plate, and three air holes are arranged in the supporting bottom plate.

[0014] Further, the gas flow pipes penetrate the left side of the temperature control box, and the gas flow pipes extend to the inside of the temperature control box.

[0015] Further, the gas conveying pipe penetrates the top of the temperature control box, the gas conveying pipe extends to the inside of the temperature control box, the first cooling pipe ring and the second cooling pipe ring are arranged in the inside of the temperature control box, and the heat dissipation fins are movably mounted on the outer wall of the air compressor.

[0016] Compared with the prior art, the cooling pipe structure with fins has the following beneficial effects:

[0017] 1. The finned intercooler tube structure, through the action of the temperature control box, reduces the loss of low temperature gas temperature in the first intercooler tube ring, through the action of the gas sub pipe, facilitates the input of low temperature gas to the inside of the second intercooler tube ring, through the action of the heat dissipation fin and the second intercooler tube ring, effectively cools the air compressor, and the heat preservation sleeve reduces the emission of low temperature gas, thereby prolonging the time of the low temperature gas for continuously cooling the air compressor and reducing the use amount of cooling gas.

[0018] 2. The finned intercooler tube structure, through the action of the shunt pipe and the gas flow pipe, discharges the gas in the temperature control box, effectively cools the air compressor, prevents the accumulation of heat of the air compressor, and prolongs the service life. BRIEF DESCRIPTION OF DRAWINGS

[0019] Fig. 1 is a structural schematic view of the utility model;

[0020] Fig. 2 is a schematic view of the second intercooler tube ring and the heat dissipation fin connection structure of the utility model;

[0021] Fig. 3 is a schematic view of the support base plate structure of the utility model.

[0022] In the drawing: 1, temperature control box; 2, gas pipe; 3, first intercooler tube ring; 4, communication pipe; 5, gas sub pipe; 6, heat preservation sleeve; 7, second intercooler tube ring; 8, heat dissipation fin; 9, first gas discharge pipe; 10, shunt pipe; 11, control valve; 12, gas flow pipe; 13, second gas discharge pipe; 14, support rod; 15, support base plate. DETAILED DESCRIPTION

[0023] The technical scheme in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0024] Please refer to Figs. 1 to 3 The finned intercooler tube structure in the embodiment comprises a gas pipe 2, the outer wall of the gas pipe 2 is provided with a temperature control box 1, the inside of the temperature control box 1 is provided with an air compressor, and the bottom of the gas pipe 2 is provided with a cooling structure for cooling the air compressor.

[0025] In this embodiment, the cooling structure includes two first intercooling pipe rings 3 movably mounted on the outer peripheral wall of the air compressor, a communication pipe 4 fixedly mounted between the two first intercooling pipe rings 3, a gas delivery auxiliary pipe 5 fixedly mounted on the outer peripheral wall of the gas delivery pipe 2, a heat preservation sleeve 6 fixedly mounted in the interior of the temperature control box 1, a second intercooling pipe ring 7 fixedly mounted on the inner peripheral wall of the heat preservation sleeve 6, four heat dissipation fins 8 fixedly mounted on the inner peripheral wall of the second intercooling pipe ring 7, and two first gas discharge pipes 9 fixedly mounted on the right side of the second intercooling pipe ring 7 and extending through the right side of the temperature control box 1 to the outside of the temperature control box 1.

[0026] It should be noted that the temperature control box 1 and the heat preservation sleeve 6 can perform heat preservation on the cooling gas in the first intercooling pipe ring 3 and the second intercooling pipe ring 7, thereby reducing the influence of external environmental factors on the first intercooling pipe ring 3 and the second intercooling pipe ring 7, and effectively dissipating heat from the air compressor.

[0027] In this embodiment, the gas delivery pipe 2 extends through the top of the temperature control box 1 and extends into the interior of the temperature control box 1, and the first intercooling pipe ring 3 and the second intercooling pipe ring 7 are both located in the interior of the temperature control box 1, and the heat dissipation fins 8 are movably mounted on the outer peripheral wall of the air compressor.

[0028] It should be noted that the cooling gas can be easily input into the interior of the first intercooling pipe ring 3 and the second intercooling pipe ring 7.

[0029] In this embodiment, the outer peripheral wall of the gas delivery pipe 2 is fixedly mounted with a shunt pipe 10, the end of the shunt pipe 10 away from the gas delivery pipe 2 is fixedly mounted with a control valve 11, the outer peripheral wall of the shunt pipe 10 is fixedly mounted with two gas flow pipes 12, the gas flow pipes 12 extend through the left side of the temperature control box 1 to the interior of the temperature control box 1, the right side of the first intercooling pipe ring 3 is fixedly mounted with two second gas discharge pipes 13, the gas delivery pipe 2 is fixedly mounted on the outer peripheral wall of the first intercooling pipe ring 3, the top and the bottom of the temperature control box 1 are both provided with six exhaust holes, and the second gas discharge pipes 13 are located in the interior of the exhaust holes.

[0030] It should be noted that part of the cooling gas is input into the interior of the temperature control box 1 through the shunt pipe 10, the control valve 11 and the gas flow pipes 12, and the heat absorbed and dissipated by the first intercooling pipe ring 3 and the second intercooling pipe ring 7 to the interior of the temperature control box 1 is discharged.

[0031] In this embodiment, the left side of the temperature control box 1 is fixedly mounted with a support rod 14, the side of the support rod 14 away from the temperature control box 1 is fixedly mounted on the right side of the control valve 11, the inner bottom wall of the temperature control box 1 is fixedly mounted with a support bottom plate 15, the air compressor is placed on the top of the support bottom plate 15, and the interior of the support bottom plate 15 is provided with three air holes.

[0032] It should be noted that the heat inside the temperature control box 1 is discharged, thereby effectively cooling the air compressor.

[0033] It should be noted that the gas pipe 2 is connected to the gas pump, and the gas pump inputs cooling gas into the inside of the gas pipe 2.

[0034] The working principle of the above embodiment is as follows:

[0035] First, the cooling gas is input into the inside of the first intercooler pipe ring 3 and the gas sub-pipe 5 through the gas pipe 2. At this time, the cooling gas is input into the inside of the first intercooler pipe ring 3 on the right side through the communication pipe 4. At this time, the first intercooler pipe ring 3 performs heat dissipation treatment on the part close to the left side of the air compressor. At the same time, the gas sub-pipe 5 inputs gas into the inside of the second intercooler pipe ring 7. At this time, the heat dissipation fins 8 are in contact with the air compressor, thereby performing heat dissipation treatment on the part close to the right side of the air compressor. Then, the control valve 11 is opened to input the cooling gas into the inside of the shunt pipe 10. The cooling gas is input into the inside of the temperature control box 1 through the gas flow pipe 12. At this time, the heat inside the temperature control box 1 can be discharged.

[0036] The mounting method, connection method or setting method disclosed in the embodiment are common mechanical connection methods, as long as the beneficial effects can be achieved. In addition, the electrical elements appearing in the embodiment are electrically connected with the master controller and the power supply. The master controller can be a conventional known device such as a computer which plays a control role. The person skilled in the art can control the electrical elements through simple programming. The existing disclosed power connection technology also belongs to the common knowledge in the art. Therefore, the specific structure and working principle of the embodiment will not be described in detail.

[0037] It should be noted that in this document, the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present application and simplifying the description, and does not indicate or imply that the indicated device or element must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the present application.

[0038] It is to be understood that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting; it is not intended to exclude myriad other embodiments of the present application that other inventors can develop based on the same general inventive concepts embodied by the described embodiments. That is, although the present application is described in terms of particular embodiments and implementations, it is to be understood that the terminology used is for the purpose of descriptive clarity and that it is intended to be limited only by the words recited in the appended claims. The scope of the present application shall be limited only by the claims.

[0039] While the embodiments of the present application have been shown and described with respect to particular embodiments thereof, it will be understood by those skilled in the art that various changes in form and details can be made therein without departing from the spirit and scope of the application. Therefore, the scope of the application should not be limited by the embodiments, but should be defined only in accordance with the following claims and their equivalents.

Claims

1. A cooling pipe structure with heat sinks, comprising a gas pipe (2), characterized in that: A temperature control box (1) is installed on the outer wall of the gas transmission pipe (2). An air compressor is installed inside the temperature control box (1). A cooling structure for cooling the air compressor is provided at the bottom of the gas transmission pipe (2). The cooling structure includes two first intercooler pipe rings (3) on the outer periphery of the air compressor, a connecting pipe (4) fixedly installed between the two first intercooler pipe rings (3), an air supply auxiliary pipe (5) fixedly installed on the outer periphery of the air supply pipe (2), an insulation sleeve (6) fixedly installed inside the temperature control box (1), a second intercooler pipe ring (7) fixedly installed on the inner periphery of the insulation sleeve (6), four heat dissipation fins (8) fixedly installed on the inner periphery of the second intercooler pipe ring (7), a diversion pipe (10) fixedly installed on the outer periphery of the air supply pipe (2), a control valve (11) fixedly installed at the end of the diversion pipe (10) away from the air supply pipe (2), and two gas flow pipes (12) fixedly installed on the outer periphery of the diversion pipe (10).

2. The intercooling pipe structure with heat sink according to claim 1, characterized in that: Two first gas discharge pipes (9) are fixedly installed on the right side of the second intercooler pipe ring (7). The first gas discharge pipes (9) penetrate the right side of the temperature control box (1) and extend to the outside of the temperature control box (1).

3. The intercooling pipe structure with heat sink according to claim 1, characterized in that: Two second gas discharge pipes (13) are fixedly installed on the right side of the first intercooler pipe ring (3) on the right side, and the gas transmission pipe (2) is fixedly installed on the outer peripheral wall of the first intercooler pipe ring (3) on the left side.

4. The intercooler pipe structure with heat sink according to claim 3, characterized in that: The temperature control box (1) has six exhaust holes at its top and bottom, and the second gas exhaust pipe (13) is located inside the exhaust holes.

5. The intercooling pipe structure with heat sink according to claim 1, characterized in that: A support rod (14) is fixedly installed on the left side of the temperature control box (1), and the side of the support rod (14) away from the temperature control box (1) is fixedly installed on the right side of the control valve (11).

6. The intercooler pipe structure with heat sink according to claim 1, characterized in that: The temperature control box (1) has a support base plate (15) fixedly installed on its inner bottom wall. The air compressor is placed on top of the support base plate (15). The support base plate (15) has three ventilation holes inside.

7. The intercooling pipe structure with heat sink according to claim 1, characterized in that: The gas flow pipe (12) passes through the left side of the temperature control box (1) and extends into the interior of the temperature control box (1).

8. The intercooling pipe structure with heat sink according to claim 1, characterized in that: The gas supply pipe (2) passes through the top of the temperature control box (1) and extends into the interior of the temperature control box (1). The first intercooler pipe ring (3) and the second intercooler pipe ring (7) are both located inside the temperature control box (1). The heat dissipation fins (8) are movably installed on the outer peripheral wall of the air compressor.

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