Heat pipe type heat dissipation assembly suitable for underwater unmanned vehicle
By designing heat pipe heat dissipation components in underwater unmanned aircraft, the problem of heat accumulation in high-power equipment inside underwater unmanned aircraft is solved, the rapid transfer of heat and large-area heat dissipation are achieved, and the service life and reliability of the equipment are improved.
Patent Information
- Application Number
- CN202411565713.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-05
- Publication Date
- 2025-03-18
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
High-power electronic equipment inside underwater unmanned aircraft generates a large amount of heat during high load operation, resulting in heat accumulation and affecting the service life and reliability of the equipment. The existing natural air-cooled heat dissipation methods cannot solve this problem quickly and effectively.
A heat pipe type heat dissipation assembly is designed, including a heat collector, a heat pipe and a condenser. The heat pipe is pre-buried inside the heat collector, absorbs heat and extends to the inner wall of the cabin. The condenser is fitted with the bulkhead, and the heat pipe penetrates the condenser, achieving rapid heat transfer and large-area heat dissipation.
Through the heat pipe heat dissipation component, the internal heating elements of the underwater unmanned aircraft are quickly transferred and large-area heat dissipated, which improves the service life and reliability of the equipment, and meets the heat dissipation needs of underwater unmanned aircraft.
Smart Images

Figure CN119653700A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to a heat dissipation component, in particular to a heat pipe type heat dissipation component, and belongs to the technical field of heat dissipation of underwater unmanned vehicles. Background Art
[0002] The heat dissipation of underwater unmanned vehicles is closely related to the overall performance indicators of the vehicle, and has a significant impact on the temperature resistance and reliability of the vehicle's electrical equipment. Therefore, the transfer of heat inside the vehicle and the thermal management of electrical equipment are extremely important to the vehicle's performance indicators and the reliability of the equipment.
[0003] There are many kinds of electronic equipment inside underwater unmanned vehicles. Their internal chips, motherboards and other high-power heating devices will generate a lot of heat during high load, high power and long-term operation. Ordinary natural air cooling has reached its limit and cannot quickly transfer the heat of hot end components. Long-term heat accumulation will seriously affect the service life of electronic components and reduce the reliability of electronic equipment. Therefore, finding a fast and efficient heat dissipation measure is an urgent problem to be solved in the field of thermal management technology. Summary of the invention
[0004] In view of this, the present invention provides a heat pipe type heat dissipation component suitable for an underwater unmanned vehicle, which can realize rapid heat transfer and meet the heat dissipation requirements of the underwater unmanned vehicle.
[0005] The technical solution of the present invention is: a heat pipe type heat dissipation component suitable for underwater unmanned vehicles, comprising: a collector, a heat pipe and a condenser;
[0006] The components to be cooled inside the underwater unmanned vehicle are mounted on the upper surface of the collector;
[0007] A portion of the heat pipe is pre-buried inside the heat collector 1 to absorb the heat from the heat collector; a portion of the heat pipe extends to the inner wall surface of the cabin of the underwater unmanned vehicle;
[0008] The condenser is in contact with the inner wall surface of the cabin wall, and the portion of the heat pipe extending to the inner wall surface of the cabin wall runs through the entire interior of the condenser.
[0009] As a preferred embodiment of the present invention: a plurality of the heat pipes are arranged in parallel, and the heat pipes have a horizontal portion pre-buried in the collector and an arc portion having the same shape as the inner wall of the cabin.
[0010] As a preferred embodiment of the present invention: a plurality of heat pipes are symmetrically arranged on both sides of the collector to diffuse the heat collected by the collector to the cabin walls on both sides.
[0011] As a preferred embodiment of the present invention: thermal conductive silicone grease is applied on the upper surface of the heat collector.
[0012] As a preferred embodiment of the present invention, the condenser is of segmented type, including a plurality of arc-shaped condensing sections arranged at intervals along the circumference of the cabin.
[0013] Beneficial effects:
[0014] (1) The present invention uses heat pipes to dissipate heat in underwater unmanned vehicles, and uses heat pipes to transfer heat from the internal heating elements of the unmanned vehicle to the cabin, and then uses the cabin wall surface to dissipate heat over a large area; it can achieve rapid heat transfer and meet the heat dissipation requirements of the underwater unmanned vehicle.
[0015] (2) In the present invention, a plurality of heat pipes are symmetrically arranged on both sides of the collector, so as to diffuse the heat collected by the collector to the cabin walls on both sides, thereby increasing the heat dissipation area.
[0016] (3) In the present invention, the condenser adopts a segmented type, which is convenient for the processing and installation of the condenser. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 It is a schematic diagram of the overall structure of the heat pipe type heat dissipation assembly of the present invention;
[0018] Figure 2 is a schematic diagram of the collector structure;
[0019] Figure 3 is a schematic diagram of the heat pipe structure;
[0020] Figure 4 is a schematic diagram of the condenser structure;
[0021] Figure 5 This is a schematic diagram of the cabin structure.
[0022] Among them: 1-collector, 2-heat pipe, 3-condenser, 4-cabin. DETAILED DESCRIPTION
[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0024] The present embodiment provides a heat pipe type heat dissipation component suitable for an underwater unmanned vehicle, which utilizes a heat pipe to dissipate heat from internal heating elements of the unmanned vehicle, can achieve rapid heat transfer, and meet the heat dissipation requirements of the underwater unmanned vehicle.
[0025] like Figure 1 As shown, the heat dissipation component includes: a collector 1, a heat pipe 2 and a condenser 3.
[0026] like Figure 2As shown, the collector 1 serves as the heat collecting end of the heat dissipation assembly; the components to be dissipated (i.e., components with a large amount of heat) inside the underwater unmanned vehicle are mounted on the upper surface of the collector 1, so that the heat of the components to be dissipated is transferred to the inside of the collector 1 through heat conduction. The collector 1 generally uses materials with high thermal conductivity, such as aluminum alloy, copper alloy, etc., which can achieve rapid heat transfer of the components to be dissipated. Mounting holes are reserved on the surface of the collector 1, and its upper surface fits the components to be dissipated and is connected by tightening screws. In order to ensure more uniform heat transfer between the components to be dissipated and the collector 1, thermal grease can be evenly applied on the upper surface of the collector 1 to increase the thermal conductivity between the hot end components and the collector 1, so as to ensure that heat can be quickly transferred from the components to be dissipated to the collector 1.
[0027] The dimensions and corresponding mounting interfaces of the heat collector 2 can be appropriately adjusted according to the dimensions and mechanical interfaces of the actual heat dissipation components. At the same time, the material of the heat collector 2 can be selected according to the actual heat transfer, such as aluminum alloy or other materials with high thermal conductivity, to ensure rapid heat transfer.
[0028] like Figure 3 As shown, the heat pipe 2 serves as the heat transfer end of the heat dissipation component, a part of which is pre-buried inside the collector 1 to absorb the heat from the collector 1, and a part of which extends to the inner wall of the cabin 4, thereby transferring the heat collected by the collector 1 to the wall of the cabin 4. The circulating working fluid in the heat pipe 2 is generally selected from copper / water, stainless steel / ammonia, aluminum / acetone, etc.; the circulating working fluid inside the heat pipe 2 absorbs the heat from the collector 1, causing the circulating working fluid to undergo phase change and absorb heat, and the working fluid moves inside the heat pipe 2 in a two-phase state. The interior of the heat pipe 2 is a porous structure of sintered metal powder, and the porous structure provides the capillary force required for the working fluid circulation, so that the circulating working fluid can transfer heat to the arc position of the cabin 4, thereby realizing the transfer and diffusion of heat.
[0029] As an example, Figure 3 As shown, a plurality of heat pipes 2 are arranged in parallel, and the heat pipes 2 have a horizontal portion pre-buried inside the collector 1 and an arc portion having the same shape as the inner wall surface of the chamber 4 .
[0030] As an example, a plurality of heat pipes 2 are symmetrically arranged on both sides of the collector 1, so as to diffuse the heat collected by the collector 1 to the walls of the cabin 4 on both sides.
[0031] like Figure 4As shown, the condenser 3 serves as the heat dissipation end of the heat dissipation component. The circulating medium inside the heat pipe 2 undergoes a phase change at the condenser end. Part of the gaseous medium changes phase into a liquid medium, releasing a large amount of latent heat of vaporization, transferring the heat from the collector end to the condenser end, releasing heat at the condenser end, and recondensing into liquid. The liquid then flows back to the evaporator end under the capillary force inside the heat pipe 2, and the cycle continues. The shape of the condenser 3 is consistent with the shape of the inner wall of the cabin 4, so that it can fit closely with the inner wall of the cabin 4, and then transfer heat to the wall of the cabin 4, realize heat exchange, and then dissipate heat through the wall of the cabin 4.
[0032] The portion of the heat pipe 2 extending to the inner wall of the cabin 4 passes through the entire condenser 3, transferring the heat absorbed by the heat pipe 2 to the condenser 3; corresponding mounting holes are reserved between the condenser 3 and the inner wall of the cabin 4, and the condenser 3 is tightly fitted to the inner wall of the cabin 4 by tightening the screws.
[0033] As an example, in order to facilitate the processing and installation of the condenser 3, the condenser 3 is segmented, including a plurality of arc-shaped condensation sections spaced apart along the circumference of the cabin body 4.
[0034] The number and extension length of the heat pipes 2 can be appropriately adjusted according to the actual dimensions of the cabin 4 to adapt to the cabin installation interface. The mechanical installation interface between the condenser 3 and the cabin 4 can be made into a corresponding matching installation port according to the actual situation of the cabin, which will not affect the actual heat dissipation effect.
[0035] Although the present invention has been described in detail above by general description and specific embodiments, it is obvious to those skilled in the art that some modifications or improvements can be made to the present invention. Therefore, these modifications or improvements made without departing from the spirit of the present invention all belong to the scope of protection claimed by the present invention.
Claims
1. A heat pipe heat dissipation assembly suitable for underwater unmanned vehicles, characterized in that: include: Heat collector (1), heat pipe (2) and condenser (3); The components to be cooled inside the underwater unmanned vehicle are mounted on the upper surface of the heat collector (1); A portion of the heat pipe (2) is pre-buried inside the heat collector (1) to absorb heat from the heat collector (1); a portion of the heat pipe (2) extends to the inner wall surface of the cabin (4) of the underwater unmanned vehicle; The condenser (3) is in contact with the inner wall surface of the cabin (4), and the portion of the heat pipe (2) extending to the inner wall surface of the cabin (4) passes through the entire interior of the condenser (3).
2. The heat pipe heat dissipation assembly suitable for underwater unmanned vehicles according to claim 1, characterized in that: A plurality of the heat pipes (2) are arranged in parallel, and the heat pipes (2) have a horizontal portion pre-buried inside the heat collector (1) and an arc portion having the same shape as the inner wall surface of the cabin (4).
3. The heat pipe heat dissipation assembly suitable for underwater unmanned vehicles according to claim 2, characterized in that: A plurality of heat pipes (2) are symmetrically arranged on both sides of the heat collector (1) for diffusing the heat collected by the heat collector (1) to the walls of the cabin (4) on both sides.
4. The heat pipe heat dissipation assembly suitable for underwater unmanned vehicles according to any one of claims 1 to 3, characterized in that: The upper surface of the heat collector (1) is coated with thermal conductive silicone grease.
5. The heat pipe heat dissipation assembly suitable for underwater unmanned vehicles according to any one of claims 1 to 3, characterized in that: The condenser (3) is of segmented type, comprising a plurality of arc-shaped condensing sections arranged at intervals along the circumference of the cabin (4).
Citation Information
Patent Citations
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