CN219802903U - Heat dissipation mechanism of anti-unmanned aerial vehicle device - Google Patents
Heat dissipation mechanism of anti-unmanned aerial vehicle device Download PDFInfo
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- CN219802903U CN219802903U CN202320510638.4U CN202320510638U CN219802903U CN 219802903 U CN219802903 U CN 219802903U CN 202320510638 U CN202320510638 U CN 202320510638U CN 219802903 U CN219802903 U CN 219802903U
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- aerial vehicle
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- 230000017525 heat dissipation Effects 0.000 title claims abstract description 70
- 230000007246 mechanism Effects 0.000 title claims abstract description 19
- 238000001816 cooling Methods 0.000 claims abstract description 61
- 239000004065 semiconductor Substances 0.000 claims description 17
- 238000009423 ventilation Methods 0.000 claims description 4
- 241001233242 Lontra Species 0.000 claims 2
- 238000000034 method Methods 0.000 abstract description 9
- 230000008569 process Effects 0.000 abstract description 5
- 230000008901 benefit Effects 0.000 abstract description 3
- 230000001681 protective effect Effects 0.000 description 7
- 238000009434 installation Methods 0.000 description 6
- 238000005457 optimization Methods 0.000 description 6
- 230000009471 action Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Devices That Are Associated With Refrigeration Equipment (AREA)
Abstract
The utility model discloses a heat dissipation mechanism of an anti-unmanned aerial vehicle device, which comprises a support, a sliding base, guide rails and unmanned aerial vehicle interference devices, wherein the sliding base is fixedly connected to the top of the support, the guide rails are fixedly connected to the top of the sliding base, the unmanned aerial vehicle interference devices are movably connected to the top of the guide rails, the front surfaces of the unmanned aerial vehicle interference devices are provided with two heat dissipation sleeves, and the heat dissipation sleeves are fixedly connected to the front surfaces and the back surfaces of the unmanned aerial vehicle interference devices and are arranged in an axisymmetric mode. According to the unmanned aerial vehicle heat dissipation device, the heat dissipation sleeve is arranged, the heat dissipation sleeve is matched with the cooling assembly to dissipate heat of the unmanned aerial vehicle interference device, a large amount of heat can be generated when the unmanned aerial vehicle interference device is started for a long time in the use process, a mechanism for dissipating heat of the unmanned aerial vehicle interference device is not arranged, the problem that service life is reduced due to the fact that the unmanned aerial vehicle interference device is in high-temperature work for a long time is solved, and the unmanned aerial vehicle heat dissipation device has the advantage of heat dissipation.
Description
Technical Field
The utility model relates to the technical field of anti-unmanned aerial vehicle equipment, in particular to a heat dissipation mechanism of an anti-unmanned aerial vehicle device.
Background
The Unmanned Aerial Vehicle is an Unmanned Aerial Vehicle (Unmanned-aircraft-Vehicle) and is an Unmanned Aerial Vehicle which utilizes radio remote control equipment and a self-provided program control device, and comprises an Unmanned helicopter, a fixed wing aircraft, a multi-rotor aircraft, an Unmanned airship and an Unmanned parachute wing aircraft.
For example, application number CN202120736462.5 relates to the technical field of anti-unmanned aerial vehicle equipment, and discloses a movable anti-unmanned aerial vehicle device, which comprises a horizontally arranged frame and an unmanned aerial vehicle interference device arranged above the frame, wherein the top side of the frame is fixedly connected with a horizontally arranged guide rail, the outer side of the guide rail is in sliding connection with a sliding base, the unmanned aerial vehicle interference device is fixedly connected with the top side of the sliding base, the top side of the frame is provided with a groove, the inner wall of the bottom of the groove is fixedly connected with a motor, the output shaft of the motor is fixedly connected with a driving sprocket in a sleeved mode, the groove is rotationally connected with two symmetrically arranged driven sprockets, the driven sprockets and the driving sprocket are in transmission connection with the same transmission chain, the front side of the transmission chain is fixedly connected with a round shaft, and the bottom of the sliding base is fixedly connected with two symmetrically arranged clamping plates. The utility model has reasonable design, and the motor can drive the unmanned aerial vehicle interference device to transversely and repeatedly move only by normal operation, thereby increasing the monitoring range of the unmanned aerial vehicle interference device and facilitating the use.
Based on the retrieval of above-mentioned patent to and combine the equipment discovery among the prior art, above-mentioned equipment is when using limited, and can only manual adjustment unmanned aerial vehicle device movable range's position, unmanned aerial vehicle interference ware can't move automatically, has restricted unmanned aerial vehicle interference ware's monitoring range's problem, but unmanned aerial vehicle interference ware is long-time start-up in the in-process of using and uses, can produce a large amount of heats, and the device does not set up the radiating mechanism of unmanned aerial vehicle interference ware, is in high temperature work for a long time and leads to life to decline easily.
Disclosure of Invention
In order to solve the problems in the prior art, the utility model aims to provide a heat dissipation mechanism of an anti-unmanned aerial vehicle device, which has the advantage of heat dissipation, and solves the problems that an unmanned aerial vehicle jammer is started for a long time to use and generates a large amount of heat in the using process, a mechanism for dissipating heat of the unmanned aerial vehicle jammer is not arranged, and the service life is easy to be reduced due to long-time high-temperature work.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a heat dissipation mechanism of anti-unmanned aerial vehicle device, includes support, slide base, guide rail and unmanned aerial vehicle interference device, slide base fixed connection is at the top of support, guide rail fixed connection is at slide base's top, unmanned aerial vehicle interference device swing joint is at the top of guide rail, unmanned aerial vehicle interference device's front is provided with heat dissipation sleeve, heat dissipation sleeve is provided with two, heat dissipation sleeve fixed connection is in unmanned aerial vehicle interference device's front and back and be axisymmetric setting, the ventilation hole has been seted up to the rear side on heat dissipation sleeve surface, heat dissipation sleeve's inside fixedly connected with slope annular plate, the positive fixedly connected with cooling subassembly of slope annular plate.
As the preferable mode of the utility model, the cooling component comprises a plurality of semiconductor refrigerating sheets which are distributed in annular equidistance, the refrigerating surface of the semiconductor refrigerating sheets is movably connected with the inclined annular plate, the front surface of the heat dissipation sleeve is fixedly connected with a heat dissipation fan, the inside of the heat dissipation sleeve is provided with a round table block, the front surface of the round table block is fixedly connected with a connecting frame, the connecting frame is provided with a plurality of annular equidistance, and one side of the connecting frame away from the round table block is fixedly connected with the inner wall of the heat dissipation sleeve.
As preferable, the inside of the round table block is provided with a mounting groove, and the inside of the mounting groove is fixedly connected with a temperature sensor.
Preferably, the front surface of the heat dissipation sleeve is provided with a protection screen plate, and the diameter of the protection screen plate is the same as that of the heat dissipation sleeve.
As the preferable mode of the utility model, the back surfaces of the protection screen plates are fixedly connected with mounting pins, the mounting pins are provided with a plurality of annular equidistant distribution, and one end of each mounting pin, which is far away from the protection screen plate, penetrates through the inside of the heat dissipation sleeve and is movably connected with the heat dissipation sleeve.
As the preferable mode of the utility model, the two sides of the unmanned aerial vehicle interference device are fixedly connected with the display screen, and the display screen is electrically connected with the temperature sensor through a wire.
Preferably, the rear side of the surface of the heat dissipation sleeve is fixedly connected with an annular filter screen.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the unmanned aerial vehicle heat dissipation device, the heat dissipation sleeve is arranged, the heat dissipation sleeve is matched with the cooling assembly to dissipate heat of the unmanned aerial vehicle interference device, a large amount of heat can be generated when the unmanned aerial vehicle interference device is started for a long time in the use process, a mechanism for dissipating heat of the unmanned aerial vehicle interference device is not arranged, the problem that service life is reduced due to the fact that the unmanned aerial vehicle interference device is in high-temperature work for a long time is solved, and the unmanned aerial vehicle heat dissipation device has the advantage of heat dissipation.
2. According to the utility model, the cooling component is arranged, so that the inclined annular plate can be cooled after the semiconductor refrigerating sheet is started, then the cooling fan is started, the air in the cooling sleeve is blown outwards after the cooling fan is started, the inside of the cooling sleeve is in a negative pressure state, so that the outside air enters the inside of the cooling sleeve through the ventilation holes, the air entering through the ventilation holes can be cooled by the inclined annular plate cooled by the semiconductor refrigerating sheet, the air temperature passing through the inclined annular plate is cooled, the surface of the unmanned aerial vehicle interference device is contacted before the inclination of the inclined annular plate, the unmanned aerial vehicle interference device is cooled, meanwhile, the air in the cooling sleeve can be guided through the round table block fixed by the connecting frame, and the temperature sensor in the installation groove can detect the temperature in the cooling sleeve in real time, so that the temperature sensor in the installation groove is convenient for a user to collect data of the temperature in the cooling sleeve.
3. According to the utility model, the protective screen plate is arranged, so that the protective screen plate can protect the cooling fan, meanwhile, the diameter of the protective screen plate is the same as that of the cooling sleeve, and the cooling fan can be more attached to the protective screen plate, and the mounting pins are arranged, so that the protective screen plate can be conveniently mounted by a user, and the cooling fan can be conveniently overhauled by the user.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic perspective view of a heat dissipation sleeve according to the present utility model;
fig. 3 is a schematic perspective sectional view of a heat dissipation sleeve according to the present utility model.
In the figure: 1. a bracket; 2. a slide base; 3. a guide rail; 4. an unmanned aerial vehicle interference device; 5. a heat dissipation sleeve; 6. a vent hole; 7. tilting the annular plate; 8. a cooling component; 81. a semiconductor refrigeration sheet; 82. a heat radiation fan; 83. round table blocks; 84. a connecting frame; 9. a mounting groove; 10. a temperature sensor; 11. a protective screen; 12. a mounting pin; 13. a display screen; 14. an annular filter screen.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
As shown in fig. 1 to 3, the heat dissipation mechanism of the anti-unmanned aerial vehicle device provided by the utility model comprises a bracket 1, a sliding base 2, a guide rail 3 and an unmanned aerial vehicle interference device 4, wherein the sliding base 2 is fixedly connected to the top of the bracket 1, the guide rail 3 is fixedly connected to the top of the sliding base 2, the unmanned aerial vehicle interference device 4 is movably connected to the top of the guide rail 3, the front surface of the unmanned aerial vehicle interference device 4 is provided with two heat dissipation sleeves 5, the heat dissipation sleeves 5 are fixedly connected to the front surface and the back surface of the unmanned aerial vehicle interference device 4 and are axisymmetrically arranged, the rear side of the surface of the heat dissipation sleeve 5 is provided with a vent hole 6, the inner part of the heat dissipation sleeve 5 is fixedly connected with an inclined annular plate 7, and the front surface of the inclined annular plate 7 is fixedly connected with a cooling assembly 8.
Referring to fig. 3, the cooling component 8 includes a semiconductor cooling plate 81, the semiconductor cooling plate 81 is provided with a plurality of and is annular equidistance and distributes, the cooling surface of the semiconductor cooling plate 81 is movably connected with the inclined annular plate 7, the front fixedly connected with radiator fan 82 of the radiator sleeve 5, the inside of the radiator sleeve 5 is provided with a round platform block 83, the front fixedly connected with link 84 of the round platform block 83, the link 84 is provided with a plurality of and is annular equidistance and distributes, one side of the link 84 away from the round platform block 83 is fixedly connected with the inner wall of the radiator sleeve 5.
As a technical optimization scheme of the utility model, by arranging the cooling component 8, the inclined annular plate 7 can be cooled after the semiconductor cooling fin 81 is started, then the cooling fan 82 is started, the air inside the cooling sleeve 5 is blown outwards after the cooling fan 82 is started, the inside of the cooling sleeve 5 is in a negative pressure state, so that the outside air enters the inside of the cooling sleeve 5 through the vent hole 6, the air entering through the vent hole 6 can be cooled by the inclined annular plate 7 cooled by the semiconductor cooling fin 81, the air temperature passing through the inclined annular plate 7 is cooled, the unmanned aerial vehicle interference device 4 is cooled by the inclination of the inclined annular plate 7 before the surface contact of the unmanned aerial vehicle interference device 4, and meanwhile, the air inside the cooling sleeve 5 can be guided by the round table block 83 fixed by the connecting frame 84.
Referring to fig. 3, a mounting groove 9 is formed in the circular truncated cone 83, and a temperature sensor 10 is fixedly connected to the inside of the mounting groove 9.
As a technical optimization scheme of the utility model, the temperature sensor 10 in the installation groove 9 can detect the temperature in the heat dissipation sleeve 5 in real time by arranging the installation groove 9 and the temperature sensor 10, so that the data collection of the temperature in the heat dissipation sleeve 5 is convenient for a user.
Referring to fig. 3, the front surface of the heat dissipation sleeve 5 is provided with a protection screen 11, and the diameter of the protection screen 11 is the same as that of the heat dissipation sleeve 5.
As a technical optimization scheme of the utility model, the protection screen plate 11 is arranged, so that the protection screen plate 11 can protect the cooling fan 82, and meanwhile, the diameter of the protection screen plate 11 is the same as that of the cooling sleeve 5, so that the protection screen plate can be attached to the cooling fan 82 more.
Referring to fig. 3, the back of the protection screen plate 11 is fixedly connected with mounting pins 12, the mounting pins 12 are provided with a plurality of annular equidistant distribution, and one end of the mounting pins 12 far away from the protection screen plate 11 penetrates through the inside of the heat dissipation sleeve 5 and is movably connected with the heat dissipation sleeve 5.
As a technical optimization scheme of the utility model, the installation pins 12 are arranged, so that a user can conveniently install the protective screen 11 by using the installation pins 12, and the user can conveniently overhaul the cooling fan 82.
Referring to fig. 1, two sides of the unmanned aerial vehicle interference device 4 are fixedly connected with display screens 13, and the display screens 13 are electrically connected with the temperature sensor 10 through wires.
As a technical optimization scheme of the utility model, the display screen 13 is arranged, so that the temperature detected by the temperature sensor 10 can be displayed in real time by using the display screen 13, and a user can conveniently observe the temperature inside the heat dissipation sleeve 5.
Referring to fig. 1, an annular filter screen 14 is fixedly connected to the rear side of the surface of the heat dissipation sleeve 5.
As a technical optimization scheme of the utility model, the annular filter screen 14 is arranged, so that the annular filter screen 14 can protect the vent holes 6, foreign matters are prevented from entering the heat dissipation sleeve 5, and the damage of the heat dissipation fan 82 and the semiconductor refrigerating plate 81 caused by the foreign matters is avoided.
The working principle and the using flow of the utility model are as follows: when the cooling fan 82 is started during use, the air inside the cooling sleeve 5 can be discharged outwards after the cooling fan 82 is started, the semiconductor refrigerating plate 81 is started, the inclined annular plate 7 can be cooled after the semiconductor refrigerating plate 81 is started, the inclined annular plate 7 is made of a material with good heat conduction effect, the inside of the cooling sleeve 5 is in a negative pressure state when the air inside the cooling sleeve 5 is discharged outwards, external air can enter the inside of the cooling sleeve 5 through the vent holes 6, the air inside the cooling sleeve 5 is firstly contacted with the inclined annular plate 7, the inclined annular plate 7 can cool the air entering the inside of the cooling sleeve 5, the cooled air is contacted with the surface of the unmanned aerial vehicle interference device 4 through the inclination of the inclined annular plate 7, so that the surface temperature of the unmanned aerial vehicle interference device 4 is driven, then the round table block 83 connected through the connecting frame 84 can guide the air inside the cooling sleeve 5, the air inside the cooling sleeve 5 can be cooled when the air outside is discharged outwards, the effect of the cooling surface of the semiconductor refrigerating plate 81 is achieved, the protection screen plate 11 can protect the cooling fan 82, and the protection screen plate 14 can prevent the cooling fan from entering the inside of the cooling sleeve 6, and the protection screen plate 14 can prevent the cooling screen from entering the inside of the cooling sleeve 5.
To sum up: this anti-unmanned aerial vehicle device's cooling body through setting up heat dissipation sleeve 5, makes heat dissipation sleeve 5 cooperation cooling subassembly 8 can dispel the heat to unmanned aerial vehicle interference device 4, has solved the in-process unmanned aerial vehicle interference ware that uses and is long-time start-up, can produce a large amount of heats, and the device does not set up the radiating mechanism of unmanned aerial vehicle interference ware, is in high temperature work for a long time and leads to the problem that life descends easily.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present utility model 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 therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a heat dissipation mechanism of anti-unmanned aerial vehicle device, includes support (1), slide base (2), guide rail (3) and unmanned aerial vehicle interference device (4), its characterized in that: slide base (2) fixed connection is at the top of support (1), guide rail (3) fixed connection is at the top of slide base (2), unmanned aerial vehicle interference device (4) swing joint is at the top of guide rail (3), the front of unmanned aerial vehicle interference device (4) is provided with heat dissipation sleeve (5), heat dissipation sleeve (5) are provided with two, heat dissipation sleeve (5) fixed connection is at the front and the back of unmanned aerial vehicle interference device (4) and be axisymmetric setting, ventilation hole (6) have been seted up to the rear side on heat dissipation sleeve (5) surface, the inside fixedly connected with slope annular plate (7) of heat dissipation sleeve (5), the front fixedly connected with cooling subassembly (8) of slope annular plate (7).
2. The heat dissipation mechanism of an anti-unmanned aerial vehicle device according to claim 1, wherein: the cooling assembly (8) comprises a semiconductor refrigerating sheet (81), the semiconductor refrigerating sheet (81) is provided with a plurality of annular equidistant distribution, a refrigerating surface of the semiconductor refrigerating sheet (81) is movably connected with an inclined annular plate (7), a cooling fan (82) is fixedly connected with the front side of the cooling sleeve (5), a round table block (83) is arranged in the cooling sleeve (5), a connecting frame (84) is fixedly connected with the front side of the round table block (83), the connecting frame (84) is provided with a plurality of annular equidistant distribution, and one side, away from the round table block (83), of the connecting frame (84) is fixedly connected with the inner wall of the cooling sleeve (5).
3. The heat dissipation mechanism of an anti-unmanned aerial vehicle device according to claim 2, wherein: the inside of round platform piece (83) has seted up mounting groove (9), the inside fixedly connected with temperature sensor (10) of mounting groove (9).
4. The heat dissipation mechanism of an anti-unmanned aerial vehicle device according to claim 1, wherein: the front of the heat dissipation sleeve (5) is provided with a protection screen plate (11), and the diameter of the protection screen plate (11) is the same as that of the heat dissipation sleeve (5).
5. The heat dissipation mechanism of an anti-drone device of claim 4, wherein: the back of protection otter board (11) is all fixedly connected with mounting pin (12), mounting pin (12) are provided with a plurality of and are annular equidistance and distribute, the one end that protection otter board (11) was kept away from to mounting pin (12) runs through to heat dissipation sleeve (5) inside and heat dissipation sleeve (5) swing joint.
6. A heat dissipation mechanism for an anti-drone assembly as recited in claim 3, wherein: both sides of unmanned aerial vehicle interference device (4) are all fixedly connected with display screen (13), display screen (13) pass through wire and temperature sensor (10) electric connection.
7. The heat dissipation mechanism of an anti-unmanned aerial vehicle device according to claim 1, wherein: the rear side of the surface of the heat dissipation sleeve (5) is fixedly connected with an annular filter screen (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320510638.4U CN219802903U (en) | 2023-03-16 | 2023-03-16 | Heat dissipation mechanism of anti-unmanned aerial vehicle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320510638.4U CN219802903U (en) | 2023-03-16 | 2023-03-16 | Heat dissipation mechanism of anti-unmanned aerial vehicle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219802903U true CN219802903U (en) | 2023-10-03 |
Family
ID=88175680
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320510638.4U Active CN219802903U (en) | 2023-03-16 | 2023-03-16 | Heat dissipation mechanism of anti-unmanned aerial vehicle device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219802903U (en) |
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2023
- 2023-03-16 CN CN202320510638.4U patent/CN219802903U/en active Active
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