An integrated compressor thermal management module

CN224644591UActive Publication Date: 2026-08-18SUZHOU ZHONGCHENG NEW ENERGY TECH CO LTD
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Patent Information

Application Number
CN202521864280.0
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-08-29
Publication Date
2026-08-18
Estimated Expiration
2035-08-29

AI Technical Summary

Technical Problem

[0004]现有的热管理系统中,蒸发器、冷凝器等结构多以紧固件连接的形式临近压缩机安装,一般安装在压缩机的缸体上,或安装在对应的转接、支撑结构上,因此,由于插接管路较多且无法避免,整体结构相对松散,且密封性不佳

Benefits of technology

本实用新型的一体式压缩机热管理集成模块,可通过将蒸发器、冷凝器、容器机构、压缩机的缸体等结构一体式焊接构造,减少插接管路数量,具有较佳的密封性。具体地,蒸发器和冷凝器直接焊接式的一体连接在压缩机的缸体顶部,而容器机构则借助缸体形成空腔的异形腔体,并通过第一封板焊接形成,其一体化程度高,结构之间直接借助缸体上的形成的流道机构相互连通,密封性得到提升。

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Abstract

The utility model relates to an integrated compressor heat management integrated module, wherein the integrated compressor heat management integrated module includes a compressor, the compressor includes cylinder body, motor end cover and cylinder end cover, one end of cylinder body is connected with motor end cover, the other end of cylinder body is connected with cylinder end cover, the outer wall between both ends of cylinder body has the flow channel mechanism formed by a plurality of through holes or grooves, a condenser, the condenser is integrally welded on the top surface or side surface of cylinder body, an evaporator, the evaporator is integrally welded on the top surface or side surface of cylinder body, a container mechanism, the container mechanism includes the side wall in the recess of cylinder body and forms the special-shaped cavity, and the first sealing plate of welding cover is arranged outside the special-shaped cavity, wherein the condenser, the evaporator, the container mechanism are connected with the flow channel mechanism respectively. The utility model can be through the integrated welding structure of evaporator, condenser, container mechanism, cylinder body and other structures of compressor, reduces the number of insertion pipe line, has better sealing property.
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Description

Technical Field

[0001] This utility model relates to a thermal management system, and more particularly to an integrated thermal management module for an integrated compressor. Background Technology

[0002] The description in this section provides only background information related to the disclosure of this utility model and does not constitute prior art.

[0003] In existing integrated thermal management modules for vehicle-mounted compressors, heat exchange can be achieved by thermally coupling the refrigerant and coolant in the evaporator or condenser and then introducing the coolant into the corresponding functional components. Therefore, heat exchange with the outside is mainly achieved by relying on the coolant, which can reduce the length of the refrigerant pipeline and has higher safety.

[0004] In existing thermal management systems, structures such as evaporators and condensers are often installed close to the compressor using fasteners. They are typically installed on the compressor block or on corresponding adapters or support structures. As a result, due to the large number of connecting pipes that cannot be avoided, the overall structure is relatively loose and has poor sealing.

[0005] It should be noted that the above introduction to the technical background is only for the purpose of providing a clear and complete explanation of the technical solutions of this utility model and facilitating understanding by those skilled in the art. It should not be assumed that these technical solutions are known to those skilled in the art simply because they have been described in the background section of this utility model. Utility Model Content

[0006] The purpose of this invention is to provide an integrated compressor thermal management module that integrates the evaporator, condenser, container mechanism, and compressor cylinder into a single welded structure, thereby reducing the number of connecting pipes and providing better sealing.

[0007] To achieve the above objectives, this utility model discloses an integrated compressor thermal management module, which includes: The compressor includes a cylinder body, a motor end cover, and a cylinder end cover. One end of the cylinder body is connected to the motor end cover, and the other end of the cylinder body is connected to the cylinder end cover. The outer wall between the two ends of the cylinder body has a flow channel mechanism formed by multiple through holes or grooves. A condenser, which is integrally welded to the top or side surface of the cylinder block; Evaporator, which is integrally welded to the top or side surface of the cylinder body; A container mechanism, the container mechanism including a shaped cavity formed by the inward recess of one side wall of the cylinder, and a first sealing plate welded to cover the shaped cavity; The condenser, the evaporator, and the container mechanism are respectively connected to the flow channel mechanism.

[0008] As a further description of the above technical solution, the flow channel mechanism includes a first condensation channel and a second condensation channel for circulating coolant; one end of the first condensation channel is connected to the condensate inlet, and the other end of the first condensation channel is connected to a first condensate external connector; one end of the second condensation channel is connected to the condensate outlet, and the other end of the second condensation channel is connected to a second condensate external connector.

[0009] As a further description of the above technical solution, the first condenser external connector and the second condenser external connector are spaced apart and arranged on the same side of the cylinder body.

[0010] As a further description of the above technical solution, the flow channel mechanism includes a first evaporation channel and a second evaporation channel for circulating coolant; one end of the first evaporation channel is connected to the evaporation inlet, and the other end of the first evaporation channel is connected to a first evaporation external connector; one end of the second evaporation channel is connected to the evaporation outlet, and the other end of the second evaporation channel is connected to a second evaporation external connector.

[0011] As a further description of the above technical solution, the first evaporator external connector and the second evaporator external connector are spaced apart and disposed on the same side of the cylinder body opposite to the first condenser external connector and the second condenser external connector.

[0012] As a further description of the above technical solution, the integrated compressor thermal management module also includes a first valve seat, a first expansion valve, and a first switching valve. The first valve seat is welded to the side wall of the first sealing plate away from the cylinder body. The first expansion valve and the first switching valve are installed on the first valve seat, and the first expansion valve and the first switching valve pass through the first sealing plate and the irregular cavity and are connected to the flow channel mechanism.

[0013] As a further description of the above technical solution, the integrated compressor thermal management module also includes a second sealing plate, a second valve seat, and a second switching valve. The second sealing plate is welded to the side wall of the cylinder body away from the first sealing plate. The second valve seat is welded to the side wall of the second sealing plate away from the cylinder body. The second switching valve is installed on the second valve seat and passes through the second sealing plate and is connected to the flow channel mechanism.

[0014] As a further description of the above technical solution, the integrated compressor thermal management module also includes a second expansion valve, which is installed on one side wall of the cylinder and connected to the flow channel mechanism.

[0015] As a further description of the above technical solution, the irregular cavity includes a plurality of spaced reinforcing ribs, one end of each reinforcing rib being connected to the bottom surface of the irregular cavity, and the other end being welded to the side of the first sealing plate facing the irregular cavity.

[0016] This utility model also discloses a compressor, wherein the compressor comprises: The cylinder body has a first flow channel mechanism and a second flow channel mechanism formed by multiple through holes or grooves on its top; and a third flow channel mechanism formed by multiple through holes or grooves on its side. A condensing shell having a condensing cavity is welded to the top surface of the cylinder body, and the condensing cavity of the condensing shell and the first flow channel mechanism form a condensing mechanism; An evaporating shell having an evaporating chamber is welded to the top surface of the cylinder body, and the evaporating chamber of the evaporating shell and the second flow channel mechanism form an evaporating mechanism; the evaporating shells are arranged parallel to each other; The first sealing plate is welded and fixed to the side of the cylinder body, thereby sealing the third flow channel mechanism.

[0017] Based on the above technical solution, the beneficial effects of this utility model are as follows: This utility model discloses an integrated compressor thermal management module that reduces the number of connecting pipes and achieves better sealing by integrally welding the evaporator, condenser, container mechanism, and compressor cylinder. Specifically, the evaporator and condenser are directly welded to the top of the compressor cylinder, while the container mechanism is formed by forming an irregular cavity with the cylinder and welded together with a first sealing plate. This high degree of integration, with the structures directly interconnected via flow channels formed on the cylinder, enhances sealing.

[0018] To further understand the features and technical content of this utility model, please refer to the following detailed description and drawings of this utility model. However, the drawings provided are for reference and illustration only and are not intended to limit this utility model. Attached Figure Description

[0019] To more clearly illustrate the technical solutions in the embodiments or prior art of this specification, the drawings used in the description of the embodiments or prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in this specification. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1This is a three-dimensional schematic diagram of an integrated compressor thermal management module provided in the embodiments of this specification; Figure 2-4 This is an exploded view of an integrated compressor thermal management module provided in the embodiments of this specification; Figure 5-7 This is a schematic diagram of the cylinder block of an integrated compressor thermal management module provided in the embodiments of this specification; Figure 8 This is a schematic diagram of the welding surface of an integrated compressor thermal management module provided in the embodiments of this specification; In the picture: 1. Cylinder block; 11. Flow channel mechanism; 111. First flow channel; 112. Second flow channel; 113. Third flow channel; 114. Fourth flow channel; 115. Fifth flow channel; 116. Sixth flow channel; 117. Seventh flow channel; 118. Eighth flow channel; 12. First condensation channel; 13. Second condensation channel; 14. First evaporation channel; 15. Second evaporation channel; 16. Exhaust port; 17. Intake port; 18. Welded surface; 2. Condenser; 21. Condenser inlet; 22. Condenser outlet; 23. Condenser inlet; 24. Condenser outlet; 25. First external condenser connector; 26. Second external condenser connector; 3. Evaporator; 31. Evaporation inlet; 32. Evaporation outlet; 33. Evaporation inlet; 34. Evaporation outlet; 35. First external evaporation connector; 36. Second external evaporation connector; 4. Container structure; 41. Irregularly shaped cavity; 411. Reinforcing rib; 42. First sealing plate; 43. Liquid storage inlet; 5. First valve seat; 51. First expansion valve; 52. First switching valve; 6. Second valve seat; 61. Second switching valve; 62. Second sealing plate; 7. Second expansion valve.

[0021] 8. Motor end cover; 9. Cylinder end cap. Detailed Implementation

[0022] To enable those skilled in the art to better understand the technical solutions in this specification, the technical solutions in the embodiments of this specification will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this specification, and not all embodiments. Based on the embodiments in this specification, all other embodiments obtained by those skilled in the art without creative effort should fall within the scope of protection of this specification.

[0023] The following specific embodiments illustrate the implementation of this utility model. Those skilled in the art can understand the advantages and effects of this utility model from the content disclosed in this specification. This utility model can be implemented or applied through other different specific embodiments, and various details in this specification can also be modified and changed based on different viewpoints and applications without departing from the concept of this utility model. Furthermore, the accompanying drawings of this utility model are for simple illustration only and are not depictions of actual dimensions, as stated in advance. The following embodiments will further describe the relevant technical content of this utility model in detail, but the disclosed content is not intended to limit the scope of protection of this utility model.

[0024] It should be understood that while terms such as "first," "second," and "third" may be used in this document to describe various components or signals, these components or signals should not be limited by these terms. These terms are primarily used to distinguish one component from another, or one signal from another. Furthermore, the term "or" as used herein should, as appropriate, include any combination of one or more of the related listed items.

[0025] Please see Figure 1-4 This embodiment provides an integrated compressor thermal management module, which includes: The integrated compressor thermal management module includes: The compressor includes a cylinder body 1, a motor end cover and a cylinder end cover 9. One end of the cylinder body 1 is connected to the motor end cover and the other end of the cylinder body 1 is connected to the cylinder end cover 9. The outer wall between the two ends of the cylinder body 1 has a flow channel mechanism 11 formed by multiple through holes or grooves. Condenser 2 is integrally welded to the top surface of cylinder block 1; Evaporator 3 is integrally welded to the top surface of cylinder 1, and evaporator 3 is arranged parallel to condenser 2. The container mechanism 4 includes a shaped cavity 41 formed by recessing one side wall of the cylinder 1, and a first sealing plate 42 welded to cover the outside of the shaped cavity 41. The condenser 2, evaporator 3, and container mechanism 4 are respectively connected to the flow channel mechanism 11.

[0026] Based on the above structure, the number of connecting pipes can be reduced and better sealing can be achieved by integrating the evaporator 3, condenser 2, container mechanism 4, and compressor cylinder 1 into a single welded structure. Specifically, the evaporator 3 and condenser 2 are directly welded to the top of the compressor cylinder 1, while the container mechanism 4 is formed by forming an irregular cavity 41 with the cylinder 1 and welding it together with the first sealing plate 42. The integration is high, and the structures are directly interconnected through the flow channel mechanism 11 formed on the cylinder 1, thus improving the sealing performance.

[0027] In the above structure, the flow channel mechanism 11 can be pre-formed as part of the cylinder body 1 during the production and design stage. Therefore, the original external pipelines of the cylinder body 1 can be set inside the cylinder body 1, which improves the system integration. Furthermore, as part of the cylinder body 1, the flow channel mechanism 11 avoids the problem of fluid and gas leakage that needs to be considered when there are more plugs, and achieves complete sealing of the flow channel.

[0028] Specifically, during the processing, due to the design of the fly-through piping, the condenser 2 or evaporator 3 can be directly connected to the cylinder 1 face-to-face by welding. For example, brazing can be used, and the welding surface 18 can be directly machined during the machining stage of the outer wall of the cylinder 1. A composite layer for brazing is set at the corresponding position on the structure of the condenser 2 and other components. During welding, the composite layer is directly heated and melted to achieve a rapid welding connection, so that the corresponding interface of the condenser 2 or evaporator 3 and the flow channel mechanism 11 are connected face-to-face, with extremely high integration and sealing performance.

[0029] In other words, in this application, the corresponding heat exchange components can be directly welded to the compressor cylinder 1 and connected directly through the integrated flow channel of the cylinder 1 itself. This facilitates installation, reduces size, and improves sealing. During the production stage, most of the piping used for circulating refrigerant or coolant is directly integrated into the flow channel mechanism 11 formed by the cylinder 1. This simplifies the plug-in method of the integrated compressor thermal management module and allows for direct welding of the corresponding components to the pipe interface. The sealing performance is significantly higher than that of plug-in connections, thus improving the overall system safety.

[0030] The condenser 2 is welded to the top surface of the cylinder block 1. The flow channel mechanism 11 includes a first condensation channel 12 and a second condensation channel 13 for the flow of coolant. One end of the first condensation channel 12 is connected to the condensate inlet 21, and the other end is connected to the first external condenser connector 25. One end of the second condensation channel 13 is connected to the condensate outlet 22, and the other end is connected to the second external condenser connector 26. Specifically, the first condensation channel 12 can be located at the edge of the cylinder block 1, making it form an L-shaped bend with the shortest flow channel distance, avoiding excessive heat changes in the condensate. Simultaneously, the first external condenser connector 25 is located facing outwards from the cylinder block 1, facilitating the installation of external piping. The second condensation channel 13 and the second external condenser connector 26 are combined on a similar principle, and are located at horizontally spaced ends, which can be adjusted according to the rectangular structure of the condenser 2.

[0031] Similarly, the evaporator 3 is welded to the top surface of the cylinder 1. The flow channel mechanism 11 includes a first evaporation channel 14 and a second evaporation channel 15 for circulating coolant. One end of the first evaporation channel 14 is connected to the evaporation inlet 31, and the other end of the first evaporation channel 14 is connected to the first evaporation external connector 35. One end of the second evaporation channel 15 is connected to the evaporation outlet 32, and the other end of the second evaporation channel 15 is connected to the second evaporation external connector 36. The evaporators 3 are arranged in parallel on the top of the cylinder 1. That is, in this embodiment, the two rectangular structures of the evaporators 3 and evaporators 3, which are similar in size and weight, are arranged in parallel above the cylinder 1 and are designed to cover the top of the cylinder 1 as much as possible along the projection plane. This design can make full use of the cylinder 1 for load-bearing and the layout is more stable and compact. It is worth noting that the first evaporator external connector 35 and the second evaporator external connector 36 mentioned above are also located on the same side of the cylinder 1. However, considering that the layout positions of the evaporation inlet 33 and the evaporation outlet 34 of the evaporator 3 itself are different, the gap can be flexibly adjusted. The distance between the first evaporator external connector 35 and the second evaporator external connector 36 in this application is closer than that between the first condenser external connector 25 and the second condenser external connector 26.

[0032] In this invention, a concave cavity 41 is formed on one side wall of the cylinder 1. The cavity 41 is connected to the flow channel mechanism 11. A first sealing plate 42 is welded to the outside of the cavity 41 to form a closed container mechanism 4. Specifically, a large concave cavity 41 is formed on one side wall of the cylinder 1 in the vertical direction between its two ends. The main part of the cavity is composed of the cylinder 1. The cavity 41 is sealed by the first sealing plate 42 to achieve a complete container mechanism 4 structure. Based on the above solution, the original container mechanism 4 structure that required external installation is directly integrated into the cylinder 1. This allows for more space above the cylinder 1 to be used for installing the condenser 2 or evaporator 3, or makes the overall structure more compact. The container mechanism 4 can also be connected to the flow channel mechanism 11 of the cylinder 1 through multiple channels, enabling the container mechanism 4 to be integrated into the integrated compressor thermal management module. The container mechanism 4 can be used as a liquid storage tank or a gas-liquid separator, and can be arranged according to different functional needs. Furthermore, the irregular cavity 41 includes a plurality of spaced reinforcing ribs 411. One end of each reinforcing rib 411 is connected to the bottom surface of the irregular cavity 41, and the other end is welded to the side of the first sealing plate 42 facing the irregular cavity 41. The reinforcing rib 411 structure can not only enhance the connection strength between the first sealing plate 42 and the irregular cavity 41, but also form an internal flow channel design to improve the internal flow field. When a liquid storage tank is provided, the container flow channel guides the outlet of the liquid storage tank to the bottom of the container mechanism 4. When a gas-liquid separator is provided, the container flow channel guides the outlet of the gas-liquid separator to the top of the container mechanism 4. At the same time, when the container mechanism 4 includes a gas-liquid separator, the gas-liquid separator also includes an oil return hole for communicating the bottom of the container mechanism 41 with the compressor suction cavity.

[0033] The first sealing plate 42 used for welding can be set as a vertical surface and is horizontally attached to the cylinder 1 before welding, so that the irregular cavity 41 is completely sealed by the first sealing plate 42.

[0034] Furthermore, the integrated compressor thermal management module also includes a first valve seat 5, a first expansion valve 51, and a first switching valve 52. The first valve seat 5 is welded to the side wall of the first sealing plate 42 away from the cylinder body 1. The first expansion valve 51 and the first switching valve 52 are mounted on the first valve seat 5, and the first expansion valve 51 and the first switching valve 52 pass through the first sealing plate 42 and the irregular cavity 41 and are connected to the flow channel mechanism 11. The first valve seat 5 serves as an adapter for mounting the first expansion valve 51 and the first switching valve 52, and plays a role in fixing the first expansion valve 51 and the first switching valve 52. The interior of the first valve seat 5 is equipped with corresponding flow channels for connecting the first expansion valve 51 and the first switching valve 52 to the flow channel mechanism 11. The first sealing plate 42 also has corresponding through holes to avoid the flow channels.

[0035] Similarly, the integrated compressor thermal management module also includes a second sealing plate 62, a second valve seat 6, and a second switching valve 61. The second sealing plate 62 is welded to the side wall of the cylinder 1 opposite to the first sealing plate 42. The second valve seat 6 is welded to the side wall of the second sealing plate 62 opposite to the cylinder 1. The second switching valve 61 is mounted on the second valve seat 6 and passes through the second sealing plate 62 and is connected to the flow channel mechanism 11. The integrated compressor thermal management module also includes a second expansion valve 7, which is mounted on the side wall of the cylinder 1 and connected to the flow channel mechanism 11. The second switching valve 61 is mounted on the other end of the cylinder 1 opposite to the first expansion valve 51 and the first switching valve 52 via the second valve seat 6. The second expansion valve 7 is also mounted on the other end of the cylinder 1 opposite to the first expansion valve 51 and the first switching valve 52, thus making full use of the outer space of the cylinder 1. Thus, the cylinder body 1 has corresponding compressor components such as motor end cover 8 and cylinder end cover 9 at both ends. There are corresponding components or devices on the top and left and right sides of the cylinder body 1. The overall integrated compressor thermal management module has a high degree of integration.

[0036] Based on the above structure and corresponding components and devices, the flow channel mechanism 11 connects them in series according to a specified flow direction, enabling the refrigerant and coolant to flow along the preset flow channels. Specifically, the flow channel mechanism 11 includes a first flow channel 111, a second flow channel 112, a third flow channel 113, a fourth flow channel 114, a fifth flow channel 115, a sixth flow channel 116, a seventh flow channel 117, and an eighth flow channel 118 for the flow of refrigerant. The compressor's exhaust port 16 is connected to the condenser inlet 23 of the condenser 2 via the first flow channel 111; the condenser outlet 24 of the condenser 2 is connected to the liquid storage inlet 43 of the container mechanism 4 via the second flow channel 112; and the liquid storage outlet of the container mechanism 4 is connected to... The liquid outlet of the container mechanism 4 is connected to the first expansion valve 51 through the third flow channel 113; the first switching valve 52 is connected to the first switching valve 52 through the fourth flow channel 114; the first switching valve 52 is connected to the second expansion valve 7 through the fifth flow channel 115; the second expansion valve 7 is connected to the evaporation inlet 33 of the evaporator 3 through the sixth flow channel 116; the evaporation outlet 34 of the evaporator 3 is connected to the suction port 17 of the compressor through the seventh flow channel 117; and the second switching valve 61 is connected to the suction port 17 of the compressor through the eighth flow channel 118.

[0037] In one embodiment, with the above-mentioned flow channel system connected in series, the compressor's exhaust port 16 can output high-temperature and high-pressure refrigerant to the condenser 2. The condenser 2 thermally couples the refrigerant and refrigerant liquid and outputs refrigerant liquid for heat exchange. Then, the condenser 2 can output the refrigerant to the container mechanism 4. The container mechanism 4 mainly plays the role of buffering and gas-liquid separation for the high-pressure refrigerant. Then, the container mechanism 4 can output the refrigerant to the first expansion valve 51 for throttling and output it externally. Alternatively, the container mechanism 4 can output the refrigerant to the opened first switching valve 52. After passing through the first switching valve 52, the refrigerant can be delivered to the second expansion valve 7. The second expansion valve 7 can throttle the refrigerant and output low-temperature and low-pressure refrigerant to the evaporator 3. The condenser 2 thermally couples the refrigerant and refrigerant liquid and outputs refrigerant liquid for heat exchange. Then, the condenser 2 can output the refrigerant to the compressor's suction port 17, completing one internal refrigerant cycle.

[0038] In the above-mentioned interconnection structure, in addition to the internal circulation, the first expansion valve 51 throttles the corresponding received refrigerant and guides it to the outdoor heat exchanger in the vehicle front compartment for heat exchange. The outdoor heat exchanger in the vehicle front compartment then introduces the refrigerant from the second switching valve 61 into the integrated compressor thermal management module of this embodiment. For example, the second switching valve 61 can input the refrigerant input from the external system through the eighth flow channel 118 into the compressor's suction port 17.

[0039] Of course, in addition to the above-mentioned flow channel mechanism 11, the number and position of the flow channels can be adjusted or increased or decreased according to the actual pipeline layout needs and the addition of corresponding components.

[0040] Furthermore, the simultaneous welding of the corresponding components, sealing plates, and cylinder 1 before welding helps to improve the stability of the welding process.

[0041] In one embodiment, the integrated compressor thermal management module has a preset center of mass, and the center of mass of the evaporator 3 and condenser 2 is adjacent to or located on the vertical plane of the preset center of mass. By placing the evaporator 3 and condenser 2 at the top, their centers of mass are balanced, thereby improving the stability of the overall structure.

[0042] This utility model also discloses a compressor, wherein the compressor includes: The cylinder body has a first flow channel mechanism and a second flow channel mechanism formed by multiple through holes or grooves on its top; and a third flow channel mechanism formed by multiple through holes or grooves on its side. A condenser shell with a condensation chamber is welded to the top surface of the cylinder block, and the condensation chamber of the condenser shell and the first flow channel mechanism form a condensation mechanism; An evaporator shell with an evaporation chamber is welded to the top surface of the cylinder body, and the evaporation chamber of the evaporator shell and the second flow channel mechanism form an evaporation mechanism; the evaporator shells are arranged in parallel with each other; The first sealing plate is welded and fixed to the side of the cylinder body, thereby sealing the third flow channel mechanism.

[0043] The above-disclosed content is only a preferred and feasible embodiment of the present utility model, and is not intended to limit the scope of the patent application of the present utility model. Therefore, all equivalent technical changes made using the contents of the present utility model specification and drawings are included in the scope of the patent application of the present utility model.

[0044] The various embodiments in this specification are described in a progressive manner. The same or similar parts between the various embodiments can be referred to each other. Each embodiment focuses on describing the differences from other embodiments.

[0045] Although this application has been described by way of examples, those skilled in the art will know that this application has many modifications and variations without departing from the spirit of this application, and it is intended that the appended embodiments include these modifications and variations without departing from this application.

Claims

1. An integrated thermal management module for an integrated compressor, characterized in that, The integrated compressor thermal management module includes: The compressor includes a cylinder body, a motor end cover, and a cylinder end cover. One end of the cylinder body is connected to the motor end cover, and the other end of the cylinder body is connected to the cylinder end cover. The outer wall between the two ends of the cylinder body has a flow channel mechanism formed by multiple through holes or grooves. A condenser, which is integrally welded to the top or side surface of the cylinder block; Evaporator, which is integrally welded to the top or side surface of the cylinder body; A container mechanism, the container mechanism including a shaped cavity formed by the inward recess of one side wall of the cylinder, and a first sealing plate welded to cover the shaped cavity; The condenser, the evaporator, and the container mechanism are respectively connected to the flow channel mechanism.

2. The integrated compressor thermal management module according to claim 1, characterized in that: The flow channel mechanism includes a first condensation channel and a second condensation channel for circulating coolant; one end of the first condensation channel is connected to a condenser inlet, and the other end of the first condensation channel is connected to a first condenser external connector; one end of the second condensation channel is connected to a condenser outlet, and the other end of the second condensation channel is connected to a second condenser external connector.

3. The integrated compressor thermal management module according to claim 2, characterized in that: The first condenser external connector and the second condenser external connector are spaced apart and arranged on the same side of the cylinder body.

4. The integrated compressor thermal management module according to claim 3, characterized in that: The flow channel mechanism includes a first evaporation channel and a second evaporation channel for circulating coolant; one end of the first evaporation channel is connected to the evaporation inlet, and the other end of the first evaporation channel is connected to the first evaporation external connector; one end of the second evaporation channel is connected to the evaporation outlet, and the other end of the second evaporation channel is connected to the second evaporation external connector.

5. The integrated compressor thermal management module according to claim 4, characterized in that: The first evaporator external connector and the second evaporator external connector are spaced apart and disposed on the same side of the cylinder body opposite to the first condenser external connector and the second condenser external connector.

6. The integrated compressor thermal management module according to claim 1, characterized in that: The integrated compressor thermal management module further includes a first valve seat, a first expansion valve, and a first switching valve. The first valve seat is welded to the side wall of the first sealing plate away from the cylinder body. The first expansion valve and the first switching valve are installed on the first valve seat, and the first expansion valve and the first switching valve pass through the first sealing plate and the irregular cavity and are connected to the flow channel mechanism.

7. The integrated compressor thermal management module according to claim 1, characterized in that: The integrated compressor thermal management module also includes a second sealing plate, a second valve seat, and a second switching valve. The second sealing plate is welded to the side wall of the cylinder away from the first sealing plate. The second valve seat is welded to the side wall of the second sealing plate away from the cylinder. The second switching valve is mounted on the second valve seat and passes through the second sealing plate and is connected to the flow channel mechanism.

8. The integrated compressor thermal management module according to claim 1, characterized in that: The integrated compressor thermal management module also includes a second expansion valve, which is installed on one side wall of the cylinder and connected to the flow channel mechanism.

9. The integrated compressor thermal management module according to claim 1, characterized in that: The irregular cavity includes a plurality of spaced reinforcing ribs. One end of each reinforcing rib is connected to the bottom surface of the irregular cavity, and the other end is welded to the side of the first sealing plate facing the irregular cavity.

10. A compressor, characterized in that, The compressor includes: The cylinder body has a first flow channel mechanism and a second flow channel mechanism formed by multiple through holes or grooves on its top; and a third flow channel mechanism formed by multiple through holes or grooves on its side. A condensing shell having a condensing cavity is welded to the top surface of the cylinder body, and the condensing cavity of the condensing shell and the first flow channel mechanism form a condensing mechanism; An evaporating shell having an evaporating chamber is welded to the top surface of the cylinder body, and the evaporating chamber of the evaporating shell and the second flow channel mechanism form an evaporating mechanism; the evaporating shells are arranged parallel to each other; The first sealing plate is welded and fixed to the side of the cylinder body, thereby sealing the third flow channel mechanism.