Gas cooling tube array structure
By employing staggered flow-guiding modules and brazing technology in the gas-cooled tube structure, cooling efficiency has been improved and costs have been reduced, solving the problems of limited cooling efficiency and high production costs in existing technologies.
Patent Information
- Application Number
- CN202423160685.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-20
- Publication Date
- 2025-12-09
- Estimated Expiration
- 2034-12-20
AI Technical Summary
The cooling efficiency of existing gas-cooled tube structures is limited, and the production cost of fins is high.
The system employs a first and second flow guiding module that are positioned opposite each other, connected by a tube array to allow gas to flow back and forth between the modules, increasing the cooling path length, and uses brazing technology to reduce production costs.
It improves cooling efficiency and reduces production costs.
Smart Images
Figure CN223649746U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to gas cooling field, especially a kind of gas cooling pipe arrangement structure. BACKGROUND
[0002] Common gas cooling mode includes letting gas pass through grid cooler or be cooled after being introduced into multiple pipes.The grid cooler is high in cooling efficiency, but the production process of its fins increases manufacturing cost.In the existing pipe arrangement cooling structure, gas is directly introduced into multiple pipes for cooling, which is large in cooling capacity, but the length of pipe is short, so that the cooling effect is limited. SUMMARY
[0003] In order to overcome the above-mentioned defects of the prior art, the purpose of the utility model is to provide a gas cooling pipe arrangement structure to improve the cooling efficiency in limited space.
[0004] In order to achieve the above-mentioned purpose, the utility model adopts the following technical scheme:
[0005] A gas cooling pipe arrangement structure comprises a first flow guide module and a second flow guide module arranged opposite to each other, and the first flow guide module and the second flow guide module are connected by a pipe group so that gas flows back and forth between the first flow guide module and the second flow guide module.
[0006] In a preferred embodiment of the utility model, the pipe group comprises a first pipe group, a second pipe group and a third pipe group, the first flow guide module has a first through-hole groove for communicating with an outer air channel and a first flow guide groove for connecting adjacent pipe groups to realize the back-and-forth flow of the gas, and the second flow guide module is similar to the first flow guide module and also has a second through-hole groove and a second flow guide groove.
[0007] In a preferred embodiment of the utility model, the first flow guide module and the second flow guide module are circumferentially staggered.
[0008] In a preferred embodiment of the utility model, the circumferential staggering means that the first flow guide module and the second flow guide module have an included angle of 36° in the circumferential direction.
[0009] In a preferred embodiment of the utility model, the two ends of the first pipe group are connected with the first through-hole groove and the second flow guide groove respectively, the two ends of the second pipe group are connected with the second flow guide groove and the first flow guide groove respectively, and the two ends of the third pipe group are connected with the first flow guide groove and the second through-hole groove respectively, so that the gas flows back and forth through the first pipe group, the second pipe group and the third pipe group.
[0010] In one preferred embodiment of the utility model, the first flow guide module is placed in the gas inlet end head, a gas inlet is formed in the gas inlet end head and connected with the outer air channel, and the first through hole groove is communicated with the gas inlet; the second flow guide module is placed in the gas outlet end head, a gas outlet is formed in the gas outlet end head and connected with the outer air channel, and the second through hole groove is communicated with the gas outlet.
[0011] The utility model has the advantages of:
[0012] The gas cooling column pipe structure has the advantages of: on the one hand, the reciprocating movement of the gas between the column pipe groups is realized by the opposing and staggered flow guide modules, so that the length of the cold pipe is increased and the cooling efficiency is improved; and on the other hand, the production cost is further reduced by using the flow guide modules with the same structure. BRIEF DESCRIPTION OF DRAWINGS
[0013] In order to more clearly illustrate the technical scheme in the embodiments of the utility model or the prior art, the drawings needed to be used in the embodiment or the prior art description will be briefly introduced.
[0014] Figure 1 It is the overall schematic view of the utility model.
[0015] Figure 2 It is the schematic view of the column pipe structure.
[0016] Figure 3 It is the structural schematic view of the gas inlet end head.
[0017] Figure 4 It is the structural schematic view of the gas outlet end head.
[0018] Figure 5 It is the projection schematic view of the gas inlet and outlet end heads. DETAILED DESCRIPTION
[0019] In the description of the utility model, it should be explained that the terms "upper", "lower", "left", "right", "inner", "outer" and the like indicate the orientation or position relationship based on the orientation or position relationship shown in the drawings, and the above description is simplified for the convenience of describing the utility model, and does not indicate or imply that the indicated device or element must have a specific orientation, a specific orientation and operation, so it cannot be understood as a limitation on the utility model.
[0020] The singular forms "a", "said" and "the" used in the specification contain plural forms unless it is clear that the singular forms are used. The terms "include", "contain" and "have" used in the specification indicate the existence of the claimed features, but do not exclude the existence of one or more other features.
[0021] In the specification, when it is stated that an element is "on", "fixed" to, "connected" to, "joined" to another element, etc., the element can be directly on, fixed to, connected to, joined to or in contact with the other element, or there may be an intermediate element. In the specification, when a feature is arranged "adjacent" to another feature, it may mean that the feature has a part overlapping with the adjacent feature or a part located above or below the adjacent feature.
[0022] It can be understood that although terms such as "first", "second", etc. may be used herein to describe different elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. Thus, a first element can be referred to as a second element without departing from the teachings of the concept of the present application.
[0023] Exemplary embodiments of the present application will be described hereinafter with reference to the accompanying drawings. However, it should be understood that the present application can be presented in many different ways and is not limited to the embodiments described below. It should also be understood that the embodiments disclosed herein can be combined in various ways to provide more additional embodiments. In all the drawings, the same reference numerals denote the same or functionally identical elements.
[0024] Figure 1 and Figure 2 The overall structure of such a gas-cooled tube bundle is shown. This tube bundle mechanism is arranged in the cooler box body 1, and the box body 1 is filled with a coolant. The gas enters from the inlet end head 10, is cooled in the box body 1, and then flows out from the exhaust end head 20. A tube bundle group is connected between the inlet end head 10 and the exhaust end head 20. The gas reciprocates between the inlet end head 10 and the exhaust end head 20 through the tube bundle group, so as to achieve the maximum cooling effect.
[0025] With reference to Figures 3 to 5 , the tube bundle group is composed of a first tube group 31, a second tube group 32 and a third tube group 33. A first flow guiding module 13 for guiding the gas into the tube bundle group is arranged on the inlet end head 10. Similarly, a second flow guiding module 23 for guiding the gas out of the tube bundle group is arranged on the exhaust end head 20. Specifically, an air inlet passage 12 connected to the air inlet end 11 is arranged in the inlet end head 10, and an exhaust passage 22 connected to the exhaust end 21 is arranged in the exhaust end head 20. A first through-hole groove 15 and a first flow guiding groove 14 are respectively formed on the first flow guiding module 13. The first through-hole groove 15 enables the air inlet passage 12 to pass through the first flow guiding module 13 and be connected to the tube bundle group. The first flow guiding groove 14 is in a "U" shape so as to simultaneously accommodate and connect a pair of tube groups. Similarly, a second through-hole groove 25 and a second flow guiding groove 24 are also formed on the second flow guiding module 23.
[0026] Specifically, the first guide channel 14 connects the second pipe group 32 and the third pipe group 33, while the second guide channel 24 connects the first pipe group 31 and the second pipe group 32. The first pipe group 31 allows air to flow from the intake end 11 into the pipe group through the first through-hole groove 15, and finally flows out through the third pipe group 33 via the second through-hole groove 15 and the exhaust passage 22. Furthermore, the first guide module 13 and the second guide module 23 have essentially the same structure, but are offset circumferentially by overlapping their side profile projections, thus creating a deflection angle. In a preferred embodiment, the deflection angle is 36°. The first pipe group 31, the second pipe group 32, and the third pipe group 33 are all fixed to the first guide module 13 and the second guide module 23 using brazing. Due to the small space at the welding point, conventional welding is difficult, and fusion welding might damage the sealing structure. Therefore, brazing is used. During brazing, only the filler metal melts, not the base material, thus avoiding damage to the connection structure.
Claims
1. A gas-cooled tube structure, characterized in that, include: A first flow guiding module and a second flow guiding module are arranged opposite to each other. The first flow guiding module and the second flow guiding module are connected by a tube array so that the gas flows back and forth between the first flow guiding module and the second flow guiding module.
2. The gas-cooled tube structure as described in claim 1, characterized in that, The tube array includes a first tube array, a second tube array, and a third tube array. The first flow guiding module has a first through-hole groove for communicating with an external air passage and a first flow guiding groove for connecting adjacent tube arrays to realize the reciprocating flow of the gas. The second flow guiding module is similar to the first flow guiding module and also has a second through-hole groove and a second flow guiding groove.
3. The gas-cooled tube structure as described in claim 2, characterized in that, The first flow guiding module and the second flow guiding module are circumferentially offset.
4. The gas-cooled tube structure as described in claim 3, characterized in that, The term "circumferentially offset" means that the first flow guiding module and the second flow guiding module have an included angle of 36° in the circumferential direction.
5. A gas-cooled tube structure as described in claim 3, characterized in that, The first pipe group is connected to the first through hole groove and the second guide groove at both ends, the second pipe group is connected to the second guide groove and the first guide groove at both ends, and the third pipe group is connected to the first guide groove and the second through hole groove at both ends, so that the gas flows back and forth through the first pipe group, the second pipe group and the third pipe group.
6. The gas-cooled tube structure as described in claim 5, characterized in that, The first flow guide module is placed inside the air inlet end cap, and an air inlet channel connected to an external air channel is provided inside the air inlet end cap. The first through hole groove is connected to the air inlet channel. The second flow guide module is placed inside the exhaust end cap, and an exhaust channel connected to an external air channel is provided inside the exhaust end cap. The second through hole groove is connected to the exhaust channel.