Intercooler and automobile

By installing reinforced turbulence components at the high and low temperature interface of the intercooler cooling pipes, the structural strength of the cooling pipes is enhanced, the problem of pipe bursting caused by thermal stress is solved, and the service life of the intercooler is extended.

CN223621680UActive Publication Date: 2025-12-02FAWER AUTOMOTIVE PARTS LIMITED COMPARTY
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Patent Information

Application Number
CN202520034290.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-01-07
Publication Date
2025-12-02
Estimated Expiration
2035-01-07

AI Technical Summary

Technical Problem

The cooling tubes of U-shaped flow intercoolers are prone to bursting at the high-low temperature interface due to uneven thermal stress, which reduces the service life of the intercooler.

Method used

Strengthening turbulence components, including fixed parts, redundant parts and bending parts, are set at the high and low temperature junction of the cooling pipe to enhance the structural strength of the cooling pipe and adapt to thermal stress deformation.

Benefits of technology

It improves the strength of the cooling pipes at the high and low temperature interface and extends the service life of the intercooler.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides an intercooler and an automobile. The intercooler comprises an upper air chamber component, a lower air chamber component, a cooling component and a reinforced turbulent flow component; the cooling component comprises a plurality of cooling pipes which are arranged at intervals in the second direction, and the reinforcing turbulent flow components are arranged on the cooling pipes adjacent to a datum plane with the plane where the partition part is located as the datum plane; the reinforced turbulent flow component comprises a fixed part, a redundant part and a bent part; the bent part extends in the third direction, and at least part of the bent part is attached to the side wall, extending in the third direction, of the cooling pipe; the two ends, in the third direction, of the bent part are each provided with a plurality of fixing parts arranged at intervals in the second direction, and a redundancy part is arranged between every two adjacent fixing parts. The reinforcing turbulent flow component is arranged in the cooling pipe adjacent to the datum plane, the strength of the cooling pipe is improved through the reinforcing turbulent flow component, deformation caused by thermal stress is adapted, and therefore the strength of the cooling pipe at the high-temperature and low-temperature junction is improved to a certain degree, and the service life of the intercooler is prolonged.
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Description

Technical Field

[0001] This application relates to the field of equipment technology for automobiles, and more particularly to intercoolers and automobiles. Background Technology

[0002] The working principle of a U-shaped flow intercooler: The hot air with high temperature and high pressure from the engine enters through the air inlet of the intercooler, passes through the cooling pipe assembly (with baffles installed inside the cooling pipes), and after being cooled, the cold air with low temperature and low pressure flows out from the air outlet of the intercooler back to the engine.

[0003] In a U-shaped intercooler, one half contains hot air at high temperature and high pressure, while the other half contains cold air at low temperature and low pressure. The cooling pipes in the middle are located at the interface between high and low temperatures, where they are subjected to uneven thermal stress, which can easily cause the pipes to burst, thereby reducing the service life of the intercooler.

[0004] Therefore, there is an urgent need for an intercooler and a car to address, to some extent, the technical problems existing in the current technology. Utility Model Content

[0005] The purpose of this application is to provide an intercooler and an automobile that improves the strength of the cooling pipe at the high and low temperature interface to a certain extent, thereby increasing the service life of the intercooler.

[0006] This application provides an intercooler, including an upper air chamber component, a lower air chamber component, a cooling component, and a turbulence-enhancing component;

[0007] The cooling component is connected to the upper air chamber component and the lower air chamber component at both ends along the first direction, respectively;

[0008] The upper air chamber component has a partition that divides the upper air chamber component into two non-communicating cavities.

[0009] The cooling component includes a plurality of cooling pipes spaced apart along the second direction. With the plane where the partition is located as the reference plane, the reinforcing turbulence component is respectively disposed on the cooling pipes adjacent to the reference plane.

[0010] The enhanced airflow component includes a fixed part, a redundant part, and a bent part; the bent part extends along a third direction, and at least a portion of the bent part is attached to the side wall of the cooling pipe extending along the third direction; multiple fixed parts are respectively provided at both ends of the bent part along the third direction and spaced apart along the second direction, and the redundant part is provided between adjacent fixed parts.

[0011] In the above technical solution, the fixing part is a fixing plate, the redundant part is a redundant arc plate, and the bending part includes a plurality of first reinforcing plates and a second reinforcing plate.

[0012] Multiple fixing plates arranged at intervals along the second direction are attached to the side wall of the cooling pipe extending along the second direction;

[0013] The redundant arc-shaped plate is disposed between adjacent fixed plates, and the redundant arc-shaped plate is bent toward the outside of the cooling pipe;

[0014] A portion of the first reinforcing plate is affixed at intervals along the third direction to one sidewall of the cooling pipe extending along the third direction, and the remaining portion of the first reinforcing plate is affixed at intervals along the third direction to the other sidewall of the cooling pipe extending along the third direction, with the first reinforcing plates affixed to the two sidewalls of the cooling pipe extending along the third direction arranged alternately; the second reinforcing plate extends along the second direction and its two ends along the second direction are respectively connected to the first reinforcing plates affixed to the two sidewalls of the cooling pipe extending along the third direction.

[0015] In the above technical solution, the first reinforcing plate on one of the side walls of the cooling pipe extending along the third direction and located at the end is connected to the fixing plate.

[0016] In the above technical solution, the first reinforcing plate on one of the side walls of the cooling pipe extending along the third direction and located at the end is connected to the fixing plate through a first arc-shaped portion.

[0017] In the above technical solution, the enhanced turbulence component further includes a tail plate;

[0018] The tail plate extends along the third direction and is connected to the end of the fixing plate away from the first reinforcing plate.

[0019] In the above technical solution, the tail plate and the fixed plate connected thereto are further connected by a second arc-shaped portion.

[0020] In the above technical solution, the corner end of the cooling pipe is connected in a third arc shape, and the first arc shape, the second arc shape and the third arc shape have the same curvature.

[0021] In the above technical solution, the bent portion extends along the first direction and longitudinally traverses the cooling pipe that extends along the first direction.

[0022] In the above technical solution, the upper air chamber component further includes a shell, a main plate, and a partition plate that can serve as the partition portion;

[0023] The shell is fastened to the main piece and surrounds a cavity; the partition is positioned in the cavity at a preset location and divides the cavity into two non-communicating cavities;

[0024] The main plate has through holes starting at the positions corresponding to the cooling pipes, and the cooling pipes can pass through the through holes and communicate with the chamber.

[0025] This application also provides an automobile that includes the aforementioned intercooler.

[0026] Compared with the prior art, this application has the following beneficial effects:

[0027] This application provides an intercooler, including an upper air chamber component, a lower air chamber component, a cooling component, and a turbulence-enhancing component;

[0028] The cooling component is connected to the upper air chamber component and the lower air chamber component at both ends along the first direction, respectively.

[0029] The upper air chamber component has a partition that divides the upper air chamber component into two non-communicating cavities.

[0030] The cooling component includes a plurality of cooling pipes spaced apart along the second direction. With the plane where the partition is located as the reference plane, the reinforcing turbulence component is respectively disposed on the cooling pipes adjacent to the reference plane.

[0031] The enhanced airflow component includes a fixed part, a redundant part, and a bent part; the bent part extends along a third direction, and at least a portion of the bent part is attached to the side wall of the cooling pipe extending along the third direction; multiple fixed parts are respectively provided at both ends of the bent part along the third direction and spaced apart along the second direction, and the redundant part is provided between adjacent fixed parts.

[0032] In summary, this application incorporates a reinforcing turbulence component within the cooling pipe adjacent to the reference plane. This component enhances the strength of the cooling pipe and accommodates deformation caused by thermal stress. Therefore, this application improves the strength of the cooling pipe at the high-low temperature interface to a certain extent, thereby extending the service life of the intercooler.

[0033] This application also provides an automobile that includes the aforementioned intercooler. Therefore, it possesses all the beneficial effects of the aforementioned intercooler, which will not be specifically elaborated upon here. Attached Figure Description

[0034] To more clearly illustrate the technical solutions in the specific embodiments of this application or the prior art, the drawings used in the description of the specific embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are some embodiments of this application. For those skilled in the art, other drawings can be obtained from these drawings without creative effort.

[0035] Figure 1 This is a schematic diagram of the overall structure of the intercooler provided in this application;

[0036] Figure 2 This application provides a structural schematic diagram of the upper air chamber component of the intercooler.

[0037] Figure 3 A structural schematic diagram of the hidden upper and lower air chamber components in the intercooler provided in this application;

[0038] Figure 4 for Figure 3 Enlarged view of point A in the middle;

[0039] Figure 5 for Figure 3 Enlarged view at point B in the middle;

[0040] Figure 6 for Figure 3 Top view;

[0041] Figure 7 for Figure 6 Enlarged view at point C;

[0042] Figure 8 This is a structural schematic diagram of the enhanced turbulence component in the intercooler provided in this application;

[0043] Figure 9 for Figure 8 Enlarged view at point D;

[0044] Figure 10 for Figure 8 Top view;

[0045] Figure 11 A cross-sectional view of the cooling pipes in the intercooler provided in this application.

[0046] Reference numerals: 1-Upper air chamber component; 2-Lower air chamber component; 3-Cooling component; 5-Ordinary turbulence component; 6-First direction; 7-Separation part; 9-First cavity; 10-Second cavity; 11-Cavity; 12-Baffle plate; 14-Second direction; 15-Cooling pipe; 16-Fixing part; 17-Redundancy part; 18-Bending part; 19-Third direction; 20-Fixing plate; 21-Redundant arc plate; 22-First reinforcement 23-Second reinforcing plate; 24-First sidewall; 25-Second sidewall; 26-Third sidewall; 27-Fourth sidewall; 28-First arc-shaped part; 29-Tail plate; 30-Second arc-shaped part; 31-Third arc-shaped part; 32-Shell; 33-Main plate; 35-Reference surface; 36-Air inlet; 37-Air outlet; 38-Fin; 39-First reinforced cooling pipe; 40-Second reinforced cooling pipe; 41-Flow channel. Detailed Implementation

[0047] The following detailed embodiments are provided to help the reader gain a comprehensive understanding of the methods, apparatus, and / or systems described herein. However, various changes, modifications, and equivalents of the methods, apparatus, and / or systems described herein will be apparent after understanding the disclosure of this application. For example, the order of operations described herein is merely illustrative and is not limited to the order set forth herein; changes that will be apparent after understanding the disclosure of this application are possible, except for operations that must occur in a specific order. Furthermore, for clarity and brevity, descriptions of features known in the art may be omitted.

[0048] The features described herein may be implemented in different forms and should not be construed as being limited to the examples described herein. Rather, the examples described herein have been provided merely to illustrate some of the many feasible ways of implementing the methods, apparatus, and / or systems described herein that will be apparent upon understanding the disclosure of this application.

[0049] Throughout the specification, when an element (such as a layer, region, or substrate) is described as being "on" another element, "connected to" another element, "bonded to" another element, "on" another element, or "covering" another element, it may be directly "on" another element, "connected to" another element, "bonded to" another element, "on" another element, or "covering" another element, or there may be one or more other elements in between. In contrast, when an element is described as being "directly on" another element, "directly connected to" another element, "directly bonded to" another element, "directly on" another element, or "directly covering" another element, there may be no other elements in between.

[0050] As used herein, the term “and / or” includes any one of the relevant items listed and any combination of any two or more items.

[0051] Although terms such as “first,” “second,” and “third” may be used herein to describe individual components, assemblies, regions, layers, or parts, these components, assemblies, regions, layers, or parts are not limited by these terms. Rather, these terms are used only to distinguish one component, assembly, region, layer, or part from another. Therefore, without departing from the teachings of the examples described herein, the first component, assembly, region, layer, or part referred to as the second component, assembly, region, layer, or part may also be referred to as the second component, assembly, region, layer, or part.

[0052] For ease of description, spatial relation terms such as “above,” “upper,” “below,” and “lower” are used herein to describe the relationship between one element and another, as shown in the accompanying drawings. Such spatial relation terms are intended to include not only the orientation depicted in the drawings but also different orientations of the device during use or operation. For example, if the device in the drawings is flipped, an element described as being “above” or “upper” relative to another element will subsequently be “below” or “lower” relative to that other element. Therefore, the term “above” includes both “above” and “below” orientations depending on the spatial orientation of the device. The device may also be positioned in other ways (e.g., rotated 90 degrees or in other orientations), and the spatial relation terms used herein will be interpreted accordingly.

[0053] The terminology used herein is for the purpose of describing various examples only and is not intended to limit this disclosure. Unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. The terms “comprising,” “including,” and “having” enumerate the stated features, quantities, operations, components, elements, and / or combinations thereof, but do not exclude the presence or addition of one or more other features, quantities, operations, components, elements, and / or combinations thereof.

[0054] Variations in the shapes shown in the accompanying drawings may occur due to manufacturing techniques and / or tolerances. Therefore, the examples described herein are not limited to the specific shapes shown in the accompanying drawings, but include changes in shape that may occur during manufacturing.

[0055] The features of the examples described herein can be combined in various ways that will be apparent upon understanding the disclosure of this application. Furthermore, although the examples described herein have a wide variety of constructions, other constructions are possible, as will be apparent upon understanding the disclosure of this application.

[0056] Example 1

[0057] The working principle of the U-shaped flow intercooler: The hot air with high temperature and high pressure from the engine enters the intercooler through the air inlet 36, passes through the cooling pipe 15 assembly (the cooling pipe 15 is equipped with baffles), and after being cooled, the cold air with low temperature and low pressure flows out of the intercooler through the air outlet 37 to the engine.

[0058] In a U-shaped intercooler, one half contains high-temperature, high-pressure hot air, and the other half contains low-temperature, low-pressure cold air. The cooling pipe 15 in the middle, located at the high-low temperature interface, is subjected to uneven thermal stress, which can easily lead to pipe rupture, thus reducing the service life of the intercooler. This application addresses this technical problem by providing a new intercooler, which is described below in conjunction with… Figures 1-11 Describe the structure of the intercooler in detail.

[0059] This application provides an intercooler, including an upper air chamber component 1, a lower air chamber component 2, a cooling component 3, and a turbulence-enhancing component;

[0060] Specifically, the cooling component 3 is connected to the upper air chamber component 1 and the lower air chamber component 2 at both ends along the first direction 6, respectively; combined with Figure 1 As shown and with Figure 1 Taking the placement angle as an example, the first direction 6 here refers to the vertical direction; furthermore, the upper air chamber component 1 is located above the cooling component 3 and is connected to the cooling component 3, while the lower air chamber component 2 is located below the cooling component 3 and is connected to the cooling component. The upper air chamber component 1 is connected to the exhaust end of the engine, that is, the high-pressure hot air generated by the engine is first conducted to the upper air chamber component 1.

[0061] Specifically, the upper air chamber component 1 has a partition 7 that divides the upper air chamber component 1 into two non-communicating cavities; further, combined with Figure 1 As shown, the upper air chamber component 1 includes a shell 32, a main plate 33, and a partition 12 that can serve as a partition 7; the shell 32 is fastened to the main plate 33 and surrounds a chamber 11; the partition 12 is positioned in a predetermined location within the chamber 11 and divides the chamber 11 into two non-communicating cavities; combined with Figure 2 As shown, the two unconnected cavities are the first cavity 9 and the second cavity 10.

[0062] Furthermore, combined Figure 6 and Figure 7 As shown, with the surface where the partition 12 is located as the reference surface 35, the air cooling component is also divided into two parts: the left half connected to the first cavity 9 and the right half connected to the second cavity 10. The air inlet 36 is formed in the first cavity 9, and the air outlet 37 is formed in the second cavity 10. That is, the high-pressure hot air generated by the engine is first guided to the first cavity 9 through the air inlet 36, and after passing through the left half cooling component 3, it reaches the lower air chamber component 2. This process achieves the first cooling of the hot air. Then, it is guided from the lower air chamber component 2 to the right half cooling component 3 and then reaches the second cavity 10, and is discharged from the air outlet 37 to the engine. This process achieves the second cooling of the hot air.

[0063] Specifically, in combination Figure 5 As shown, the cooling component 3 includes a plurality of cooling pipes 15 arranged at intervals along the second direction 14. With the surface where the partition 7 is located as the reference surface 35, the airflow strengthening components are respectively disposed on the cooling pipes 15 adjacent to the reference surface 35.

[0064] Furthermore, combined Figure 1 As shown and with Figure 1Taking the placement angle as an example, the second direction 14 refers to the left and right direction, that is, multiple cooling pipes 15 are arranged at intervals along the left and right direction, and fins 38 are provided between adjacent cooling pipes 15.

[0065] Furthermore, in Figure 6 and Figure 7 The reference surface 35 is shown. A flow-enhancing member is provided in the cooling pipe 15 on the left side adjacent to the reference surface 35. Similarly, a flow-enhancing member is provided in the cooling pipe 15 on the right side adjacent to the reference surface 35. The reference surface 35 is located at the junction of high and low temperatures. By providing a flow-enhancing member in the cooling pipe 15 on the left side adjacent to the reference surface 35, this application can increase the strength of the cooling pipe 15 at the junction of high and low temperatures, thereby improving the service life of the intercooler.

[0066] Furthermore, combining Figure 3 and Figure 4 As shown, the enhanced flow-deflecting component includes a fixed portion 16, a redundant portion 17, and a bent portion 18. The bent portion 18 extends along a third direction 19 (here, the third direction 19 refers to the thickness direction of the cooling component 3), and at least a portion of the bent portion 18 is attached to the side wall of the cooling pipe 15 extending along the third direction 19. Multiple fixed portions 16 are provided at both ends of the bent portion 18 along the third direction 19, spaced apart along the second direction 14, and redundant portions 17 are provided between adjacent fixed portions 16. According to the principle of thermal expansion and contraction, when hot air flows to the first enhanced cooling pipe 39 on the left side of the reference plane 35, the enhanced flow-deflecting component expands, and the redundant portion 17 can fully adapt to this expansion, i.e., the redundant portion 17 provides deformation space for thermal expansion. Similarly, the second enhanced cooling pipe 40 on the right side passes through low-temperature air, at which time the enhanced flow-deflecting component contracts, and the redundant portion 17 provides space for cold contraction.

[0067] In addition, the remaining cooling pipes 15 (except for the first reinforced cooling pipe 39 and the second reinforced cooling pipe 40) are equipped with ordinary flow-deflecting components 5. Ordinary flow-deflecting components 5 are currently in use and can be understood by those skilled in the art, so they will not be described in detail here.

[0068] In summary, this application provides a reinforcing turbulence member inside the cooling pipe 15 adjacent to the reference plane 35. The reinforcing turbulence member improves the strength of the cooling pipe 15 and adapts to the deformation caused by thermal stress. Therefore, this application improves the strength of the cooling pipe 15 at the high and low temperature junction to a certain extent, thereby improving the service life of the intercooler.

[0069] In this embodiment, combined with Figure 8 and Figure 9 As shown, the fixing part 16 is a fixing plate 20, the redundant part 17 is a redundant arc plate 21, and the bending part 18 includes multiple first reinforcing plates 22 and multiple second reinforcing plates 23.

[0070] Specifically, in combination Figure 11 As shown, the cooling pipe 15 includes a first sidewall 24, a second sidewall 25, a third sidewall 26, and a fourth sidewall 27, which are connected sequentially. Multiple fixing plates 20 arranged at intervals along the second direction 14 are respectively attached to the first sidewall 24 and the third sidewall 26.

[0071] Specifically, the redundant arc-shaped plate 21 is disposed between adjacent fixed plates 20, and the redundant arc-shaped plate 21 is bent outward toward the cooling pipe 15. Figure 10 As shown, two fixing plates 20 are attached to the first side wall 24, and a redundant arc plate 21 is provided between the two fixing plates 20.

[0072] Specifically, a portion of the first reinforcing plate 22 is spaced along the third direction 19 on one side wall of the cooling pipe 15 extending along the third direction 19, and the remaining portion of the first reinforcing plate 22 is spaced along the third direction 19 on the other side wall of the cooling pipe 15 extending along the third direction 19, and the first reinforcing plates 22 on the two side walls of the cooling pipe 15 extending along the third direction 19 are arranged alternately; the second reinforcing plate 23 extends along the second direction 14 and its two ends along the second direction 14 are respectively connected to the first reinforcing plates 22 on the two side walls of the cooling pipe 15 extending along the third direction 19.

[0073] Furthermore, combined Figure 10 and Figure 11 As shown, both the second sidewall 25 and the fourth sidewall 27 are fitted with first reinforcing plates 22, and the first reinforcing plates 22 on the second sidewall 25 and the fourth sidewall 27 are arranged alternately. Furthermore, the first reinforcing plates 22 on the second sidewall 25 and the fourth sidewall 27 are connected by second reinforcing plates 23. Figure 10 As shown, the connection direction of the first reinforcing plate 22 and the second reinforcing plate 23 ultimately forms a serpentine bend structure, and an airflow channel 41 is formed between adjacent second reinforcing plates 23 for guiding air.

[0074] In summary, taking the first reinforced cooling pipe 39 as an example, when high-pressure hot air passes through the first reinforced cooling pipe 39, the heat of the hot air will be transferred to the first reinforced cooling pipe 39, and the first reinforced cooling pipe 39 will have a slight deformation. Similarly, the reinforced turbulence component will also be slightly deformed due to the heat. The aforementioned redundant arc plate 21 can just adapt to this deformation, so that the fixing plate 20 and the first reinforcing plate 22 are always in contact with the side wall of the first reinforced cooling pipe 39. In this way, it is equivalent to increasing the wall thickness of the first reinforced cooling pipe 39, thus improving the strength of the first reinforced cooling pipe 39 to a certain extent. Therefore, even if the first reinforced cooling pipe 39 is located at the high and low temperature junction and is subjected to uneven thermal stress, it will not cause pipe bursting, thereby improving the service life of the intercooler.

[0075] In this embodiment, a first reinforcing plate 22 located at the end of one of the side walls of the cooling pipe 15 extending along a third direction 19 is connected to a fixing plate 20.

[0076] Specifically, the first reinforcing plate 22 on the second sidewall 25 and located at the end is connected to the fixing plate 20 on the first sidewall 24 and the fixing plate 20 on the third sidewall 26, respectively.

[0077] In this embodiment, combined with Figure 10 As shown, the first reinforcing plate 22 on one of the side walls of the cooling pipe 15 extending along the third direction 19 and located at the end is connected to the fixing plate 20 through the first arc-shaped portion 28.

[0078] In this embodiment, the enhanced turbulence member further includes a tail plate 29; the tail plate 29 extends along a third direction 19 and is connected to the end of the fixed plate 20 away from the first reinforcing plate 22.

[0079] Specifically, in combination Figure 10 As shown, the tail plate 29 is located on the fourth side wall 27. There are two tail plates 29. One tail plate 29 is connected to the fixing plate 20 on the first side wall 24, and the other tail plate 29 is connected to the fixing plate 20 on the third side wall 26.

[0080] Furthermore, combined Figure 10 As shown, the tail plate 29 is connected to the fixed plate 20 connected thereto by a second arc-shaped portion 30.

[0081] Furthermore, the corner of the cooling pipe 15 is connected by a third arc-shaped section 31. The first arc-shaped section 28, the second arc-shaped section 30, and the third arc-shaped section 31 have the same curvature, thereby ensuring that when the reinforcing turbulence component is installed inside the cooling pipe 15, the tail plate 29, the fixing plate 20, and the first reinforcing plate 22 are all attached to the side wall of the cooling pipe 15, which is equivalent to increasing the wall thickness of the cooling pipe.

[0082] In this embodiment, combined with Figure 8As shown, the bend 18 extends along the first direction 6 and penetrates the cooling pipe 15 extending along the first direction 6, thereby effectively strengthening the first reinforced cooling pipe 39 and the second reinforced cooling pipe 40 as a whole, which is equivalent to increasing the wall thickness of the cooling pipe 15, and does not affect the flow of hot air when the flow channel 41 is provided.

[0083] In this embodiment, a through hole is started on the main plate 33 at the position corresponding to the cooling pipe 15, and the cooling pipe 15 can pass through the through hole and communicate with the chamber 11.

[0084] Example 2

[0085] This application also provides an automobile that includes the aforementioned intercooler. Therefore, it possesses all the beneficial effects of the aforementioned intercooler, which will not be specifically elaborated upon here.

[0086] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this application, and are not intended to limit them. Although this application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some or all of the technical features therein. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of this application.

Claims

1. An intercooler, characterized in that, This includes upper air chamber components, lower air chamber components, cooling components, and enhanced turbulence components; The cooling component is connected to the upper air chamber component and the lower air chamber component at both ends along the first direction, respectively; The upper air chamber component has a partition that divides the upper air chamber component into two non-communicating cavities. The cooling component includes a plurality of cooling pipes spaced apart along the second direction. With the plane where the partition is located as the reference plane, the reinforcing turbulence component is respectively disposed on the cooling pipes adjacent to the reference plane. The enhanced airflow component includes a fixed part, a redundant part, and a bent part; the bent part extends along a third direction, and at least a portion of the bent part is attached to the side wall of the cooling pipe extending along the third direction; multiple fixed parts are respectively provided at both ends of the bent part along the third direction and spaced apart along the second direction, and the redundant part is provided between adjacent fixed parts.

2. The intercooler according to claim 1, characterized in that, The fixing part is a fixing plate, the redundant part is a redundant arc plate, and the bending part includes multiple first reinforcing plates and second reinforcing plates; Multiple fixing plates arranged at intervals along the second direction are attached to the side wall of the cooling pipe extending along the second direction; The redundant arc-shaped plate is disposed between adjacent fixed plates, and the redundant arc-shaped plate is bent toward the outside of the cooling pipe; A portion of the first reinforcing plate is affixed at intervals along the third direction to one sidewall of the cooling pipe extending along the third direction, and the remaining portion of the first reinforcing plate is affixed at intervals along the third direction to the other sidewall of the cooling pipe extending along the third direction, with the first reinforcing plates affixed to the two sidewalls of the cooling pipe extending along the third direction arranged alternately; the second reinforcing plate extends along the second direction and its two ends along the second direction are respectively connected to the first reinforcing plates affixed to the two sidewalls of the cooling pipe extending along the third direction.

3. The intercooler according to claim 2, characterized in that, The first reinforcing plate, located at the end of one of the side walls along the third direction of the cooling pipe, is connected to the fixing plate.

4. The intercooler according to claim 3, characterized in that, The first reinforcing plate, located at the end of one of the side walls along the third direction of the cooling pipe, is connected to the fixing plate via a first arcuate portion.

5. The intercooler according to claim 4, characterized in that, The enhanced aerodynamic component also includes a tailplate; The tail plate extends along the third direction and is connected to the end of the fixing plate away from the first reinforcing plate.

6. The intercooler according to claim 5, characterized in that, The tail plate is connected to the fixed plate by a second arc-shaped portion.

7. The intercooler according to claim 6, characterized in that, The corner of the cooling pipe is connected by a third arc-shaped section, and the first arc-shaped section, the second arc-shaped section, and the third arc-shaped section have the same curvature.

8. The intercooler according to claim 1, characterized in that, The bent portion extends along the first direction and longitudinally through the cooling pipe that extends along the first direction.

9. The intercooler according to claim 1, characterized in that, The upper air chamber component includes a shell, a main plate, and a partition plate that can serve as the partition portion; The shell is fastened to the main piece and surrounds a cavity; the partition is positioned in the cavity at a preset location and divides the cavity into two non-communicating cavities; The main plate has through holes starting at the positions corresponding to the cooling pipes, and the cooling pipes can pass through the through holes and communicate with the chamber.

10. A car, characterized in that, Includes the intercooler as described in any one of claims 1-9.