Rapid heat dissipation enclosure for an on-board device

Abstract

The utility model discloses a quick heat dissipation shell of airborne equipment, including positioning casing, sealing cover and passageway pipe, passageway pipe sets up in the inside of positioning casing, and the top of positioning casing is provided with sealing cover, the inside of the top of positioning casing is equipped with sliding card slot, and the bottom fixed mounting of sealing cover has corresponding sliding bolt with sliding card slot, and sliding bolt sliding installation is in the inside of sliding card slot, and the front end of sealing cover is provided with side position card block, the outer surface of passageway pipe is provided with spiral sleeve, and the outside of side position card block is provided with cooling card plate, and the top of cooling card plate is equipped with the current -collecting pipe mouth of intercommunication with spiral sleeve inner chamber, the utility model discloses a sliding card slot and sliding bolt are set up, realize sealing cover and the quick sliding installation and disassembly of positioning casing, and the maintenance time is greatly shortened, and the joint design of cooling card plate and side position card block adopts the card of engaging piece and engaging groove, and the independent disassembly and replacement of cooling system are supported, and maintenance cost is reduced.

Description

Technical Field

[0001] This utility model relates to the field of heat dissipation shell technology, specifically a rapid heat dissipation shell for airborne equipment. Background Technology

[0002] In the aviation field, airborne equipment (such as electronic control systems, sensors, and communication modules) generates a significant amount of heat during operation. If this heat cannot be dissipated in a timely manner, it can lead to decreased equipment performance, shortened lifespan, or even malfunction, seriously impacting flight safety. Traditional airborne equipment cooling solutions typically employ air cooling or simple liquid cooling structures. However, as aircraft demand increasingly higher levels of equipment integration, power density, and reliability, traditional cooling methods are gradually revealing the following limitations:

[0003] Traditional heat sink casings are often welded or bolted to the equipment housing. Disassembly and assembly require special tools, are time-consuming, and can easily damage the sealing structure. In addition, long-term heat dissipation may cause blockage inside the ventilation ducts, requiring cleaning. Furthermore, the integrated design of the coolant piping and heat dissipation structure means that partial failures require the entire structure to be replaced, resulting in high maintenance costs.

[0004] Due to the limited internal space of aircraft, traditional heat dissipation shells are difficult to adapt to the installation requirements of equipment of different sizes or power. When multiple devices are connected in parallel for heat dissipation, traditional solutions require additional complex piping design, which increases system weight and leakage risk, and makes it difficult to dissipate heat quickly. After long-term high-temperature operation, the heat dissipation pipes are prone to self-heating, thereby reducing the efficiency of heat dissipation.

[0005] To address the above shortcomings, a rapid heat dissipation housing for airborne equipment is proposed. Utility Model Content

[0006] This invention provides a fast heat dissipation housing for airborne equipment, aiming to improve the problems of low maintenance convenience, poor structural expandability, and low heat dissipation efficiency.

[0007] This utility model is implemented as follows: a fast heat dissipation shell for airborne equipment, including a positioning shell, a sealing cover plate and a channel tube, wherein the channel tube is disposed inside the positioning shell and the sealing cover plate is disposed on the top of the positioning shell;

[0008] A sliding groove is provided on the top inner side of the positioning housing, and a sliding bolt corresponding to the sliding groove is fixedly installed on the bottom of the sealing cover. The sliding bolt is slidably installed on the inner side of the sliding groove, and a side locking block is provided at the front end of the sealing cover.

[0009] The outer surface of the channel tube is provided with a spiral sleeve, and a cooling plate is provided on the outside of the side clamping block. The top of the cooling plate is provided with a collecting pipe opening that communicates with the inner cavity of the spiral sleeve.

[0010] Preferably, the inner side of the positioning housing is provided with a positioning groove, the front end of the channel tube is provided with a heat outlet, the back end of the channel tube is provided with a heat inlet, the right side of the positioning housing is provided with an expansion slot, the left side of the positioning housing is provided with an expansion bolt, and adjacent positioning housings are fixed together by the expansion slot and the expansion bolt.

[0011] Preferably, the bottom inner side of the sealing cover is provided with a sealing groove corresponding to the positioning groove. The positioning groove and the sealing groove are tightly fitted with the outer surface of the channel tube. The bottom of the sealing cover is provided with two ribs. The sealing cover can cover the top of the three positioning housings. The ribs are fitted with the top surface of the positioning housings.

[0012] Preferably, a fixing groove is provided on the top side of the positioning housing, and a connecting groove corresponding to the fixing groove is provided on the inner side of the sealing cover plate. A screw that engages with the fixing groove can be installed on the inner side of the connecting groove.

[0013] Preferably, a set of engaging grooves is provided on the front of the side-positioning block, and a flow tube penetrating the inside of the side-positioning block is provided at the bottom of the engaging grooves.

[0014] Preferably, the spiral sleeve is tightly fitted to the outer surface of the channel tube, the spiral sleeve is fixedly installed on the inner side of the sealing groove and the positioning groove, and a transmission pipe connected to the spiral sleeve is opened on the inner side of the front of the positioning housing, and the transmission pipe is connected to the locking groove.

[0015] Preferably, the bottom end of the cooling plate is provided with a set of engaging components, which can be engaged inside the engaging groove. A diverter pipe is provided on the back side of the engaging components, and the diverter pipe is inserted into the inside of the flow pipe.

[0016] Preferably, the inner side of the manifold opening is provided with a pipe connected to the branch pipe, and the bottom of the back end of the cooling plate can be tightly fitted with the bottom surface of the sealing cover.

[0017] Preferably, adjacent positioning housings can be fixed to each other, adjacent sealing cover sides can fit tightly together, and the outer side of the heat inlet can be connected to the housing of the onboard equipment.

[0018] Compared with the prior art, the beneficial effects of this utility model are:

[0019] 1. This utility model achieves rapid sliding installation and disassembly of the sealing cover and positioning housing by setting a sliding slot and a sliding bolt, and their mutual cooperation, which greatly shortens the maintenance time. In addition, the mutual fixation of the sealing slot and the positioning groove ensures the sealing performance of heat dissipation. Furthermore, the cooling plate and the side plate adopt a snap-fit ​​design of snap-fit ​​parts and snap-fit ​​grooves, which supports the independent disassembly and replacement of the cooling system, avoiding the need to replace the entire heat dissipation shell and reducing maintenance costs.

[0020] 2. This utility model is equipped with a spiral sleeve that fits tightly with the channel pipe, extending the coolant flow path, increasing the heat exchange time and area, and significantly improving heat dissipation efficiency. In addition, it is equipped with an expansion slot and an expansion bolt, which supports the horizontal splicing of multiple heat dissipation shells to form a continuous heat dissipation surface, adapting to the heat dissipation needs of different power devices and improving system flexibility. Attached Figure Description

[0021] Figure 1 This is a schematic diagram of the structure of this utility model;

[0022] Figure 2 This is a schematic diagram of the spiral sleeve structure of this utility model;

[0023] Figure 3 This is a schematic diagram of the bottom structure of the sealing cover plate of this utility model;

[0024] Figure 4 This is a schematic diagram of the connection between the positioning shell and the front end of the side plate of this utility model;

[0025] Figure 5 This is a schematic diagram of the cooling plate structure of this utility model;

[0026] Figure 6 This is a schematic diagram of the combined installation state of this utility model.

[0027] In the diagram: 1. Channel pipe; 11. Heat outlet; 12. Heat inlet; 2. Positioning housing; 21. Positioning groove; 22. Sliding slot; 23. Fixing groove; 3. Sealing cover plate; 31. Sealing slot; 32. Sliding bolt; 33. Connecting groove; 34. Rib; 4. Side locking block; 41. Engaging groove; 42. Flow pipe; 5. Cooling plate; 51. Engaging component; 52. Diverter pipe; 53. Collector port; 6. Spiral sleeve; 61. Transfer pipe; 7. Expansion slot; 71. Expansion bolt; 8. Airborne equipment housing. Detailed Implementation

[0028] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0029] In the description of this utility model, it should be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0030] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0031] Example 1

[0032] Please see Figure 1-6 A rapid heat dissipation housing for airborne equipment includes a positioning housing 2, a sealing cover 3, and a channel pipe 1. The channel pipe 1 is disposed inside the positioning housing 2. The sealing cover 3 is disposed on the top of the positioning housing 2. A sliding groove 22 is formed on the inner side of the top of the positioning housing 2. A sliding bolt 32 corresponding to the sliding groove 22 is fixedly installed at the bottom of the sealing cover 3. The sliding bolt 32 is slidably installed inside the sliding groove 22 to realize the rapid installation and removal of the sealing cover 3.

[0033] The front end of the channel pipe 1 is provided with a heat outlet 11 and the back end is provided with a heat inlet 12. It is directly connected to the airborne equipment housing 8 and is used to conduct heat generated by the airborne equipment. The right side of the positioning housing 2 is provided with an expansion slot 7 and the left side of the positioning housing 2 is provided with an expansion bolt 71. A single positioning housing 2 is inserted into the expansion bolt 71 of the adjacent positioning housing 2 through the expansion slot 7 to realize horizontal combination expansion installation. After splicing, the top sides of the adjacent positioning housing 2 fit tightly together to form a continuous heat dissipation surface.

[0034] like Figure 2 , 3 As shown, a positioning groove 21 is provided on the inner side of the positioning housing 2, and a sealing groove 31 corresponding to the positioning groove 21 is provided on the inner bottom of the sealing cover plate 3. The positioning groove 21 and the sealing groove 31 are tightly fitted with the outer surface of the channel pipe 1 to ensure that there are no gaps in the heat conduction path. Two ribs 34 are provided at the bottom of the sealing cover plate 3. The ribs 34 are fitted with the top surface of the positioning housing 2 to enhance the stability of the sealing cover plate 3.

[0035] Among them, the sealing cover plate 3 can cover the top of the three positioning housings 2, and the sliding bolt 32 of the sealing cover plate 3 is slid into the sliding groove 22 of the positioning housing 2 until the rib 34 is in contact with the top surface of the positioning housing 2.

[0036] The top side of the positioning housing 2 is provided with a fixing groove 23, and the inner side of the sealing cover plate 3 is provided with a connecting groove 33 corresponding to the fixing groove 23. A screw that engages with the fixing groove 23 can be installed on the inner side of the connecting groove 33. By passing the screw through the connecting groove 33 and screwing it into the fixing groove 23, the sealing cover plate 3 and the positioning housing 2 are fixed.

[0037] Example 2

[0038] Please see Figure 1 , 2 5, 6. A spiral sleeve 6 is provided on the outer surface of the channel tube 1. The spiral sleeve 6 is tightly fitted to the outer surface of the channel tube 1. The spiral sleeve 6 is fixedly installed on the inner side of the sealing groove 31 and the positioning groove 21. The spiral structure of the spiral sleeve 6 extends the flow path of the coolant and improves the heat exchange efficiency.

[0039] As the coolant flows inside the spiral sleeve 6, it exchanges heat with the outer surface of the channel pipe 1, carrying away heat.

[0040] The front end of the sealing cover 3 is provided with a side locking block 4. The front of the side locking block 4 is provided with a set of locking grooves 41. The bottom end of the locking grooves 41 is provided with a flow pipe 42 that penetrates the inside of the side locking block 4. The side locking block 4 is integrated into the front end of the sealing cover 3, without occupying extra space, thus optimizing the overall size of the heat dissipation shell.

[0041] A cooling plate 5 is provided on the outer side of the side-positioned clamping block 4. The top of the cooling plate 5 is provided with a manifold 53 that communicates with the inner cavity of the spiral sleeve 6. The outer end of the manifold 53 can be connected to a device that provides coolant. The side-positioned clamping block 4 provides a fixed interface for the cooling plate 5, realizing the modular integration of the cooling system and the heat dissipation shell, which is convenient for assembly and maintenance.

[0042] The front inner side of the positioning housing 2 is provided with a transmission pipe 61 that is connected to the spiral sleeve 6. The transmission pipe 61 is connected to the locking groove 41, which improves the stability of transmission.

[0043] like Figure 5 As shown, a set of engaging parts 51 is provided at the bottom of the cooling plate 5. The engaging parts 51 can be engaged inside the engaging groove 41. A diversion pipe 52 is provided on the back side of the engaging parts 51. The diversion pipe 52 is inserted into the inside of the flow pipe 42. The bottom of the back end of the cooling plate 5 can be tightly fitted with the bottom surface of the sealing cover plate 3. The engaging design of the engaging parts 51 and the engaging groove 41 enables the cooling plate 5 to be quickly fixed and separated, improving maintenance efficiency.

[0044] It should be noted that the cooling plate 5 is independent of the sealing cover plate 3, and is combined with the side clamping block 4, which improves the stability of the device and also facilitates individual replacement or maintenance, reducing maintenance costs.

[0045] The inner side of the manifold 53 is provided with a pipe that connects to the branch pipe 52 to ensure that the coolant flows along the designed path, allowing for segmented management and optimizing heat exchange efficiency.

[0046] It should be noted that the locking part 51 of the cooling plate 5 is inserted into the locking groove 41 of the side locking block 4, the diverter pipe 52 is inserted into the flow pipe 42, and the manifold port 53 of the cooling plate 5 is connected to the external coolant circulation system through the pipe. The coolant enters from the manifold port 53, flows into the spiral sleeve 6 through the diverter pipe 52, the flow pipe 42 and the transfer pipe 61, and finally flows out from the outlet of the spiral sleeve 6.

[0047] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A fast heat dissipation housing for airborne equipment, comprising a positioning housing (2), a sealing cover (3) and a channel pipe (1), wherein the channel pipe (1) is disposed on the inner side of the positioning housing (2) and the sealing cover (3) is disposed on the top of the positioning housing (2). characterized in that The top inner side of the positioning housing (2) is provided with a sliding groove (22), and the bottom of the sealing cover (3) is fixedly installed with a sliding bolt (32) corresponding to the sliding groove (22). The sliding bolt (32) is slidably installed on the inner side of the sliding groove (22), and the front end of the sealing cover (3) is provided with a side locking block (4). The outer surface of the channel tube (1) is provided with a spiral sleeve (6), and the outer side of the side clamping block (4) is provided with a cooling plate (5). The top of the cooling plate (5) is provided with a collecting pipe (53) that communicates with the inner cavity of the spiral sleeve (6).

2. The quick heat dissipation enclosure for onboard equipment according to claim 1, characterized in that: The positioning housing (2) has a positioning groove (21) on its inner side, a heat outlet (11) is provided at the front end of the channel tube (1), a heat inlet (12) is provided at the back end of the channel tube (1), an expansion slot (7) is provided on the right side of the positioning housing (2), and an expansion bolt (71) is provided on the left side of the positioning housing (2). Adjacent positioning housings (2) are fixed together by the expansion slot (7) and the expansion bolt (71).

3. The rapid heat dissipation housing for airborne equipment according to claim 2, characterized in that: The bottom inner side of the sealing cover (3) is provided with a sealing groove (31) corresponding to the positioning groove (21). The positioning groove (21) and the sealing groove (31) are tightly fitted with the outer surface of the channel tube (1). The bottom of the sealing cover (3) is provided with two ribs (34). The sealing cover (3) can cover the top of the three positioning shells (2). The ribs (34) are fitted with the top surface of the positioning shells (2).

4. The rapid heat dissipation housing for airborne equipment according to claim 3, characterized in that: The top side of the positioning housing (2) is provided with a fixing groove (23), and the inner side of the sealing cover (3) is provided with a connecting groove (33) corresponding to the fixing groove (23). The inner side of the connecting groove (33) can be fitted with a screw that engages with the fixing groove (23).

5. The rapid heat dissipation housing for airborne equipment according to claim 3, characterized in that: The side-position locking block (4) has a set of locking grooves (41) on its front side, and the bottom end of the locking grooves (41) is provided with a flow tube (42) that penetrates the inside of the side-position locking block (4).

6. The rapid heat dissipation housing for airborne equipment according to claim 5, characterized in that: The spiral sleeve (6) is tightly fitted to the outer surface of the channel tube (1). The spiral sleeve (6) is fixedly installed on the inner side of the sealing groove (31) and the positioning groove (21). The inner side of the front of the positioning housing (2) is provided with a transmission pipe (61) connected to the spiral sleeve (6). The transmission pipe (61) is connected to the locking groove (41).

7. The rapid heat dissipation housing for airborne equipment according to claim 5, characterized in that: The bottom end of the cooling plate (5) is provided with a set of engaging parts (51), which can be engaged in the inner side of the engaging groove (41). A diversion pipe (52) is provided on the back side of the engaging part (51), and the diversion pipe (52) is inserted into the inner side of the flow pipe (42).

8. The rapid heat dissipation housing for airborne equipment according to claim 7, characterized in that: The inner side of the manifold (53) is provided with a pipe that is connected to the branch pipe (52), and the bottom of the back end of the cooling plate (5) can be tightly fitted with the bottom surface of the sealing cover (3).

9. The rapid heat dissipation housing for airborne equipment according to claim 2, characterized in that: The adjacent positioning housings (2) can be fixed to each other, the sides of the adjacent sealing cover plates (3) can be tightly fitted, and the outer side of the heat inlet (12) can be connected to the onboard equipment housing (8).

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