Two-phase flow cooling case for airborne electronic module

By designing a two-phase flow cooling system and deployable side panel structure in the chassis of the onboard electronic module, the problem of limited heat dissipation capability of the single-phase conductive liquid-cooled chassis is solved, and more efficient heat dissipation effect and faster heat dissipation speed are achieved.

CN119815802APending Publication Date: 2025-04-11JIANGSU HUACHUANG MICROSYSTEM CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202510062675.7
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-01-15
Publication Date
2025-04-11

AI Technical Summary

Technical Problem

The existing single-phase conductive liquid-cooled chassis has limited heat dissipation capabilities and cannot effectively solve the high temperature problem of electronic modules.

Method used

A two-phase flow cooling chassis on the airborne electronic module is designed to realize the two-phase flow of heat pipes through the setting of the bottom plate box, two sets of flow guide components and heat exchange box, and the side plate is deployed when the box door is opened to increase the air flow speed.

Benefits of technology

The dual-phase heat dissipation of the electronic module is realized, the heat dissipation efficiency is improved, the long-term and effective operation of the electronic module is ensured, and the heat dissipation speed is accelerated through the side panel deployment.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN119815802A_ABST
    Figure CN119815802A_ABST
Patent Text Reader

Abstract

The airborne electronic module two-phase flow cooling case comprises a case body, the case body comprises a bottom plate box and a heat exchange box, the back of the heat exchange box and the back of the bottom plate box are jointly and fixedly connected with a back plate, and box doors are jointly hinged to the two sides of the front face of the heat exchange box and the two sides of the front face of the bottom plate box; explosion adjusting assemblies are arranged between the opposite sides of the bottom plate box and the heat exchange box. According to the two-phase flow cooling case for the airborne electronic module, through the arrangement of the bottom plate box, the two flow guide assemblies and the heat exchange box, after heat exchange, two-phase flow heat dissipation of the case body is achieved through the heat pipes, the influence of low heat dissipation efficiency caused by sensible heat of cooling liquid is avoided, and in cooperation with the arrangement of the explosion adjusting assembly, the case door and the linkage assembly, after the case door is opened, the heat dissipation efficiency is improved. According to the case, the two side plates can be unfolded, so that unfolding type heat dissipation of the case body is achieved, the heat dissipation speed of the built-in electronic module is increased, and reliable guarantee is provided for long-term effective operation of the electronic module.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The invention relates to the technical field of cooling chassis, in particular to a two-phase flow cooling chassis for an airborne electronic module. Background Art

[0002] Existing airborne electronic equipment mainly uses single-phase liquid cooling, which mainly includes the following two forms: one is single-phase penetrating liquid cooling, that is, the single-phase coolant directly passes through the chassis and enters the electronic module liquid cooling plate to directly take away the heat generated by the electronic module; the other is single-phase conduction liquid cooling, that is, the single-phase coolant only passes into the chassis and does not pass into the electronic module cold plate. The heat generated by the electronic module is transferred to the chassis through the air cooling plate by heat conduction, and then the coolant takes the heat out of the chassis to achieve heat dissipation of the electronic module.

[0003] Since the coolant does not directly flow into the electronic module, the single-phase conductive liquid-cooled chassis avoids the coolant leakage caused by the failure of the liquid-cooled connector or the corrosion of the liquid-cooled plate to a certain extent, reduces the risk of electrical short circuit of the airborne equipment caused by the coolant leakage, and improves the safety of the airborne equipment to a certain extent. However, for the single-phase conductive liquid-cooled chassis, the heat absorbed by the coolant when flowing through the chassis is only converted into the sensible heat of the coolant, which makes its heat dissipation capacity relatively limited. Therefore, a two-phase flow cooling chassis for airborne electronic modules is proposed to realize the two-phase heat dissipation of the electronic module. At the same time, when the temperature inside the chassis is too high, the door of the chassis can be opened and the side panels can be unfolded to accelerate the flow rate of the air inside the chassis. Summary of the invention

[0004] In view of the deficiencies in the prior art, the present invention provides an airborne electronic module two-phase flow cooling chassis, which solves the problem of limited heat dissipation capacity of a single-phase conduction liquid cooling chassis.

[0005] To achieve the above objectives, the present invention is implemented through the following technical solutions: an airborne electronic module two-phase flow cooling chassis, comprising a chassis body, the chassis body comprising a bottom plate box and a heat exchange box, the backs of the heat exchange box and the bottom plate box are commonly fixedly connected with a back plate, the heat exchange box and the bottom plate box are commonly hinged with a box door on both sides of the front, an explosion adjustment component is arranged between the bottom plate box and the opposite side of the heat exchange box, two side panels used in conjunction with the explosion adjustment component are also arranged between the bottom plate box and the heat exchange box, and the top and bottom of the back of the box door are both provided with a linkage component used in conjunction with the explosion adjustment component; The bottom plate box and the heat exchange box are connected via two groups of flow guide components, and the two groups of flow guide components are both arranged between the two side plates.

[0006] The present invention is further configured as follows: the flow guide assembly comprises an upper box and a lower box, and the upper box and the lower box are connected via a plurality of flow guide pipes; The two upper boxes are fixedly installed on both sides of the bottom of the heat exchange box, and the two lower boxes are fixedly installed on both sides of the top of the bottom plate box. Long grooves used in conjunction with the guide pipe are opened on the opposite sides of the two side plates.

[0007] The present invention is further configured as follows: the two upper boxes are both connected to the interior of the heat exchange box through openings, and one lower box is connected to the bottom box through an opening; The back of the bottom box is connected with a cold liquid inlet pipe, and the back of the other lower box is connected with a cold liquid outlet pipe. One end of the cold liquid inlet pipe and the cold liquid outlet pipe both penetrate the back plate and extend to the rear of the back plate.

[0008] The present invention is further configured as follows: the explosion adjustment assembly comprises a threaded barrel, the inner surfaces of both ends of the threaded barrel are threadedly mounted with threaded rods, and the threads of the two threaded rods are arranged in opposite directions; The two threaded cylinders are rotatably mounted on the opposite sides of the heat exchange box and the base box through support blocks, and one end of the two threaded rods on the same side is fixedly mounted on the top and bottom of one side of the side plate, respectively, and one side of the upper box and the lower box are provided with reserved holes for use with the threaded rods.

[0009] The present invention is further configured as follows: the linkage assembly includes a slide plate and a gear sleeve, a tooth plate is fixedly installed on the back of the slide plate, the tooth plate is meshed with the gear sleeve, and linkage plates are rotatably installed on both sides of the front of the slide plate; The two linkage plates are rotatably mounted on the backs of the two box doors respectively, the gear sleeve is sleeved and fixedly mounted on the outer periphery of the threaded cylinder, and the opposite sides of the two slide plates are in sliding contact with the opposite sides of the heat exchange box and the bottom plate box respectively.

[0010] The present invention is further configured as follows: a limiting plate used in conjunction with the tooth plate is fixedly installed on one side opposite to the heat exchange box and the bottom plate box.

[0011] The present invention is further configured as follows: a heat exchange plate is fixedly installed inside the heat exchange box, and a plurality of heat pipes are penetrated and fixedly installed on the top of the heat exchange plate.

[0012] The present invention is further configured as follows: a cover plate is fixedly installed on the top of the heat exchange box, one side of the top of the cover plate is connected to an inlet pipe with a valve, and the back of the heat exchange box and above the heat exchange plate is connected to an outlet pipe with a valve.

[0013] The present invention provides an airborne electronic module two-phase flow cooling chassis. It has the following beneficial effects: The present invention realizes two-phase flow heat dissipation of the chassis body through the arrangement of a bottom plate box, two sets of flow guide components and a heat exchange box after heat exchange through heat pipes, thereby avoiding the influence of low heat dissipation efficiency caused by the sensible heat of the coolant. In addition, with the arrangement of the explosion adjustment component, the box door and the linkage component, after the box door is opened, the two side panels can be unfolded to achieve unfolded heat dissipation of the chassis body, accelerate the heat dissipation speed of the built-in electronic module, and provide reliable guarantee for the long-term and effective operation of the electronic module. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 This is a schematic diagram of the external structure of the present invention when the side panels are not unfolded; Figure 2 This is a schematic diagram of the external structure of the side panels of the present invention after they are unfolded; Figure 3 It is a schematic diagram of the connection of the bottom plate box, the heat exchange box, the explosion adjustment component, the linkage component and the guide component structure of the present invention; Figure 4 It is a schematic diagram of the connection of the box door, explosion adjustment assembly, side plate and linkage assembly structure of the present invention; Figure 5 It is a schematic diagram of the connection between the bottom plate box, the heat exchange box and the flow guide assembly structure of the present invention; Figure 6 This is a schematic diagram of the external structure of the present invention when the side panels are not unfolded from a rear side perspective.

[0015] In the figure: 1. Chassis body; 2. Bottom box; 3. Heat exchange box; 301. Heat exchange plate; 302. Heat pipe; 303. Cover plate; 304. Inlet pipe with valve; 305. Outlet pipe with valve; 4. Back panel; 5. Box door; 6. Explosion adjustment assembly; 601. Threaded barrel; 602. Threaded rod; 7. Side plate; 701. Long groove; 8. linkage assembly; 801. slide plate; 802. gear sleeve; 803. tooth plate; 804. linkage plate; 805. limit plate; 9. Flow guide assembly; 901. upper box; 902. lower box; 903. flow guide pipe; 904. cold liquid inlet pipe; 905. cold liquid outlet pipe; 906. reserved hole. DETAILED DESCRIPTION

[0016] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0017] See also Figure 1-6 , the embodiment of the present invention provides the following two technical solutions: Embodiment 1: A two-phase flow cooling chassis for airborne electronic modules, comprising a chassis body 1, wherein the chassis body 1 comprises a bottom plate box 2 and a heat exchange box 3, side panels 7 are arranged on the left and right sides of the opposite sides of the bottom plate box 2 and the heat exchange box 3, both sides of the front of the heat exchange box 3 and the bottom plate box 2 are hinged with a box door 5, the back of the heat exchange box 3 and the bottom plate box 2 are fixedly connected with a back plate 4, the bottom plate box 2 and the heat exchange box 3 are connected by two sets of guide components 9, and the two sets of guide components 9 are arranged between the two side panels 7, specifically, the guide component 9 comprises an upper box 901 and a lower box 902, the upper box 90 1 and the lower box 902 are connected through a plurality of guide pipes 903, the two upper boxes 901 are respectively fixedly installed on both sides of the bottom of the heat exchange box 3, and the two upper boxes 901 are connected with the inside of the heat exchange box 3 through openings, and the two lower boxes 902 are respectively fixedly installed on both sides of the top of the bottom plate box 2, one lower box 902 is connected with the bottom plate box 2 through an opening, the back of the bottom plate box 2 is connected with a cold liquid inlet pipe 904, and the back of the other lower box 902 is connected with a cold liquid outlet pipe 905, and one end of the cold liquid inlet pipe 904 and the cold liquid outlet pipe 905 both pass through the back plate 4 and extend to the rear of the back plate 4.

[0018] As a preferred solution, in order to achieve the positioning of the side panel 7 and provide more rapid heat dissipation conditions for the chassis body 1, an explosion adjustment component 6 is arranged between the opposite sides of the base box 2 and the heat exchange box 3, and the explosion adjustment component 6 includes a threaded cylinder 601, and the two threaded cylinders 601 are respectively rotatably installed on the opposite sides of the heat exchange box 3 and the base box 2 through support blocks, and the inner surfaces of both ends of the threaded cylinder 601 are threadedly installed with threaded rods 602, and the threads of the two threaded rods 602 are set in opposite directions, and one end of the two threaded rods 602 on the same side is respectively fixedly installed on the top and bottom of one side of the side panel 7, and one side of the upper box 901 and the lower box 902 are provided with reserved holes 906 used in conjunction with the threaded rods 602, and the opposite sides of the two side panels 7 are provided with long grooves 701 used in conjunction with the guide pipe 903.

[0019] As a preferred solution, in order to achieve rapid heat dissipation of two-phase flow, a heat exchange plate 301 is fixedly installed inside the heat exchange box 3, and a number of heat pipes 302 are passed through and fixedly installed on the top of the heat exchange plate 301. The back of the heat exchange box 3 and above the heat exchange plate 301 are connected to a valved outlet pipe 305.

[0020] As a preferred solution, a cover plate 303 is fixedly installed on the top of the heat exchange box 3 , and one side of the top of the cover plate 303 is connected to an inlet pipe 304 with a valve.

[0021] In this embodiment, through the two-phase change of the heat pipe 302, a rapid heat exchange environment is provided for the coolant below the heat exchange plate 301 in the heat exchange box 3, providing convenient and reliable conditions for the dissipation of heat inside the chassis body 1, and through the setting of the explosion adjustment component 6, the side panel 7 can be unfolded to provide a wider contact surface between the chassis body 1 and the outside air, thereby accelerating the dissipation of heat.

[0022] Embodiment 2. This embodiment is an improvement on the previous embodiment. It is a two-phase flow cooling chassis for airborne electronic modules. It also includes a linkage assembly 8 for use with an explosion adjustment assembly 6, which is arranged on the top and bottom of the back of the box door 5. The linkage assembly 8 includes a slide plate 801 and a gear sleeve 802. A tooth plate 803 is fixedly installed on the back of the slide plate 801. The tooth plate 803 is meshed with the gear sleeve 802. Linkage plates 804 are rotatably installed on both sides of the front of the slide plate 801. The two linkage plates 804 are rotatably installed on the backs of the two box doors 5 respectively. The gear sleeve 802 is sleeved and fixedly installed on the outer periphery of the threaded cylinder 601. The opposite sides of the two slide plates 801 and the opposite sides of the two gear plates 803 are respectively in sliding contact with the opposite sides of the heat exchange box 3 and the bottom plate box 2. The opposite sides of the heat exchange box 3 and the bottom plate box 2 are fixedly installed with a limit plate 805 for use with the gear plate 803.

[0023] The advantage of the second embodiment over the first embodiment is that the two side panels 7 can be easily unfolded by simply opening the box door 5, thereby providing convenient conditions for building a heat dissipation environment.

[0024] When in use, the coolant enters the bottom plate box 2 from the cold liquid inlet pipe 904, and enters the heat exchange box 3 through the guide assembly 9 set on the left. During the process, the coolant in the guide assembly 9 exchanges heat with the inside of the chassis body 1 through the guide pipe 903. After the heat exchange, the coolant passes through the heat pipe 302 and flows to the guide assembly 9 on the right, exchanges heat with the inside of the chassis body 1 again, and is finally discharged from the cold liquid outlet pipe 905. During the process, cold water enters the heat exchange box 3 from the valved inlet pipe 304, exchanges heat with the heat pipe 302, and is discharged from the valved outlet pipe 305; When the heat dissipation speed of the chassis body 1 needs to be accelerated, the two cabinet doors 5 are opened synchronously, the cabinet doors 5 drive the linkage plate 804 to move the slide plate 801 forward, the slide plate 801 drives the tooth plate 803 to move forward, the tooth plate 803 drives the gear cylinder sleeve 802 to rotate the threaded cylinder 601, and the threaded cylinder 601 drives the two threaded rods 602 to move to both sides, that is, the two threaded rods 602 push the two side plates 7 away from each other. After the cabinet door 5 rotates 90 degrees, as shown in the attached figure Figure 2 As shown, the side panel 7 is unfolded; After the heat dissipation is completed, the two cabinet doors 5 are closed synchronously to reset the slide plate 801. During the process, the tooth plate 803 drives the gear sleeve 802 to reverse the threaded cylinder 601, and the two threaded rods 602 pull the two side plates 7 closer to each other until the slide plate 801 is reset. Figure 1 Status shown.

[0025] As an extended explanation, the cover plate 303 is not provided, and air flow is used to exchange heat for the heat pipe 302. When the heat exchange efficiency needs to be improved, water is injected into the top of the heat exchange plate 301 in the heat exchange box 3. When the water temperature is high, the valve of the valved outlet pipe 305 is opened to discharge the high-temperature water, and then new cold water can be added.

[0026] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0027] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An airborne electronic module two-phase flow cooling chassis, comprising a chassis body (1), characterized in that: The chassis body (1) comprises a base box (2) and a heat exchange box (3); the backs of the heat exchange box (3) and the base box (2) are fixedly connected to a back plate (4); both sides of the fronts of the heat exchange box (3) and the base box (2) are hingedly connected to a box door (5); an explosion adjustment component (6) is arranged between the base box (2) and the heat exchange box (3) on opposite sides; two side panels (7) used in conjunction with the explosion adjustment component (6) are also arranged between the base box (2) and the heat exchange box (3); and linkage components (8) used in conjunction with the explosion adjustment component (6) are arranged on the top and bottom of the back of the box door (5); The bottom plate box (2) and the heat exchange box (3) are connected via two sets of flow guide components (9), and the two sets of flow guide components (9) are both arranged between the two side plates (7).

2. The two-phase flow cooling chassis for airborne electronic modules according to claim 1, characterized in that: The flow guide assembly (9) comprises an upper box (901) and a lower box (902), and the upper box (901) and the lower box (902) are connected via a plurality of flow guide pipes (903); The two upper boxes (901) are respectively fixedly mounted on two sides of the bottom of the heat exchange box (3), and the two lower boxes (902) are respectively fixedly mounted on two sides of the top of the bottom plate box (2), and the two side plates (7) are provided with long grooves (701) on opposite sides thereof for use with the guide pipe (903).

3. The two-phase flow cooling chassis for airborne electronic modules according to claim 2, characterized in that: The two upper boxes (901) are both connected to the interior of the heat exchange box (3) through an opening, and one lower box (902) is connected to the bottom box (2) through an opening; The back of the bottom plate box (2) is connected to a cold liquid inlet pipe (904), and the back of the other lower box (902) is connected to a cold liquid outlet pipe (905). One end of the cold liquid inlet pipe (904) and the cold liquid outlet pipe (905) both penetrate the back plate (4) and extend to the rear of the back plate (4).

4. The two-phase flow cooling chassis for airborne electronic modules according to claim 2, characterized in that: The explosion adjustment component (6) comprises a threaded barrel (601), and threaded rods (602) are threadedly mounted on the inner surfaces of both ends of the threaded barrel (601), and the threads of the two threaded rods (602) are arranged in opposite directions; The two threaded cylinders (601) are rotatably mounted on opposite sides of the heat exchange box (3) and the bottom plate box (2) via support blocks, one end of the two threaded rods (602) on the same side are fixedly mounted on the top and bottom of one side of the side plate (7), respectively, and one side of the upper box (901) and the lower box (902) are provided with reserved holes (906) for use with the threaded rods (602).

5. The two-phase flow cooling chassis for airborne electronic modules according to claim 4, characterized in that: The linkage assembly (8) comprises a slide plate (801) and a gear sleeve (802); a tooth plate (803) is fixedly mounted on the back of the slide plate (801); the tooth plate (803) is meshed with the gear sleeve (802); linkage plates (804) are rotatably mounted on both sides of the front of the slide plate (801); The two linkage plates (804) are rotatably mounted on the backs of the two box doors (5), respectively; the gear sleeve (802) is sleeved and fixedly mounted on the outer circumference of the threaded cylinder (601), and the opposite sides of the two slide plates (801) are in sliding contact with the opposite sides of the heat exchange box (3) and the bottom plate box (2), respectively.

6. The two-phase flow cooling chassis for airborne electronic modules according to claim 1, characterized in that: A limiting plate (805) used in conjunction with the tooth plate (803) is fixedly mounted on the opposite side of the heat exchange box (3) and the bottom plate box (2).

7. The two-phase flow cooling chassis for airborne electronic modules according to claim 1, characterized in that: A heat exchange plate (301) is fixedly installed inside the heat exchange box (3), and a plurality of heat pipes (302) are passed through and fixedly installed on the top of the heat exchange plate (301).

8. The two-phase flow cooling chassis for airborne electronic modules according to claim 7, characterized in that: A cover plate (303) is fixedly mounted on the top of the heat exchange box (3), one side of the top of the cover plate (303) is connected to an inlet pipe (304) with a valve, and the back of the heat exchange box (3) and located above the heat exchange plate (301) is connected to an outlet pipe (305) with a valve.