CN223899534U - Radiating air duct of satellite internet terminal shell - Google Patents
Radiating air duct of satellite internet terminal shellInfo
- Publication number
- CN223899534U CN223899534U CN202520330587.6U CN202520330587U CN223899534U CN 223899534 U CN223899534 U CN 223899534U CN 202520330587 U CN202520330587 U CN 202520330587U CN 223899534 U CN223899534 U CN 223899534U
- Authority
- CN
- China
- Prior art keywords
- plate
- terminal housing
- heat dissipation
- satellite internet
- internet terminal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model discloses a radiating air duct of a satellite internet terminal shell, which comprises a terminal shell, wherein an air inlet net mouth is arranged at the lower end of the surface of the terminal shell, one end of the air inlet net mouth extends into the terminal shell, an air outlet net mouth is arranged at the top end of the terminal shell, the bottom end of the air outlet net mouth extends into the terminal shell, a bottom plate is arranged on the surface of the terminal shell below the air inlet net mouth, side supporting plates are arranged at two sides of the top end of the bottom plate, a top plate is arranged at one end of the side supporting plates, far away from the bottom plate, of the top plate, a lifting cylinder is arranged at the central position of the top end of the top plate, the bottom end of the lifting cylinder penetrates through the top plate and is provided with a lifting plate, guide cylinders are arranged at two sides of the interior of the lifting plate, the two ends of the guide cylinders extend to the exterior of the lifting plate, and guide rods are movably connected in the guide cylinders. The utility model not only ensures the heat radiation performance of the heat radiation air duct, but also achieves the aim of easily radiating the satellite internet terminal body, and improves the energy conservation performance of the heat radiation air duct when in use.
Description
Technical Field
The utility model relates to the technical field of satellite communication, in particular to a radiating air duct of a satellite internet terminal shell.
Background
With the rapid development of satellite internet technology, the performance requirements of satellite internet terminal equipment are increasingly improved, especially in terms of data transmission rate, equipment power consumption, heat dissipation performance and the like, the traditional heat dissipation mode, such as natural heat dissipation or simple fan heat dissipation, is difficult to meet the requirements of current high-performance terminal equipment, and especially in complex and changeable outer space environments, the heat dissipation problem of the satellite internet terminal equipment is particularly prominent, so that the development of an efficient and reliable heat dissipation air duct design has important significance for improving the stability and service life of the satellite internet terminal equipment.
The utility model provides a mainboard heat abstractor of video terminal with reference publication number CN212936512U, it includes terminal casing and the mainboard that sets up in terminal casing, still be provided with the guide duct in the terminal casing and be used for carrying out radiating fin to the mainboard, fin and mainboard interval set for the clearance setting, the one end of guide duct communicates with the air outlet in fin heat dissipation wind channel, the other end communicates with the apopore of seting up on the terminal casing, be provided with the radiator fan that is used for carrying out ventilation and heat dissipation to the mainboard in the terminal casing, radiator fan's air outlet communicates with the income wind gap in fin heat dissipation wind channel, through carrying out radiating noncontact structure to the mainboard, the radiating effect of mainboard in the video terminal has been improved, according to the above-mentioned, although the device can obtain better application, but generally be inconvenient for carrying out brushing clean to the inlet net mouth region, make the dust easily adhere to the inlet net mouth region and cause the phenomenon of jam, trouble user often.
Disclosure of utility model
The utility model aims to provide a radiating air duct of a satellite internet terminal shell, so as to solve the problems that although the device provided in the background art can be well applied, brushing cleaning is not convenient to be carried out on an air inlet net mouth area, and dust is easy to adhere to the air inlet net mouth area to cause a blocking phenomenon.
The technical scheme includes that the cooling air duct of the satellite Internet terminal shell comprises a terminal shell body, an air inlet net opening is formed in the lower end of the surface of the terminal shell body, one end of the air inlet net opening extends to the inside of the terminal shell body, an air outlet net opening is formed in the top end of the terminal shell body, the bottom end of the air outlet net opening extends to the inside of the terminal shell body, a bottom plate is arranged on the surface of the terminal shell body below the air inlet net opening, side supporting plates are arranged on two sides of the top end of the bottom plate, a top plate is arranged at one end, far away from the bottom plate, of the side supporting plates, a lifting cylinder is arranged at the central position of the top end of the top plate, the bottom end of the lifting cylinder penetrates through the top plate and is provided with a lifting plate, guide cylinders are arranged on two sides of the inside of the lifting plate, two ends of each guide cylinder extend to the outside of the lifting plate, guide rods are movably connected to the inside of the guide cylinders, the two ends of each guide rods extend to the outside of the guide cylinders and are fixedly connected with the bottom end of the top plate and the top plate, a brush plate is arranged at the bottom end of the lifting plate, one end of the brush plate, the brush plate is arranged on the inner wall of the brush plate, and the inner wall of the brush plate is arranged on the inner wall of the brush head, and the surface of the terminal shell.
Preferably, a piece placing plate is arranged at the lower end inside the terminal box shell, a satellite internet terminal body is installed at the top end of the piece placing plate, and the satellite internet terminal body is supported and placed through the piece placing plate.
Preferably, a side seat body is mounted on the inner wall of one side of the terminal box shell above the satellite internet terminal body, and a heat dissipation fin column is arranged on the inner wall of the side seat body, so that the heat dissipation fin is arranged and treated.
Preferably, a plurality of radiating fins are arranged on the outer wall of the radiating fin column, the bottom ends of the radiating fins are contacted with the top end of the satellite internet terminal body, and the heat energy generated by the satellite internet terminal body is absorbed through the arrangement of the radiating fins.
Preferably, a cooling fan is installed at the top end of the cooling fin, a singlechip is installed on the inner wall of the terminal box shell at one side of the cooling fan, the output end of the singlechip is electrically connected with the input end of the cooling fan, and the cooling fan is arranged to cool the satellite internet terminal body in an air-cooling manner.
Preferably, a temperature sensor is installed on the inner wall of the terminal case shell far away from one side of the singlechip, and the output end of the temperature sensor is electrically connected with the input end of the cooling fan, so that the temperature inside the terminal case shell is subjected to heat dissipation treatment through the arrangement of the temperature sensor.
Compared with the prior art, the satellite internet terminal shell has the beneficial effects that the heat dissipation air duct of the satellite internet terminal shell not only ensures the heat dissipation performance of the heat dissipation air duct, but also achieves the aim of easily dissipating heat of a satellite internet terminal body, and improves the energy conservation performance of the heat dissipation air duct when in use;
(1) The lifting air cylinder drives the lifting plate to lift, so that the lifting plate drives the guide cylinder to slide on the outer wall of the guide rod, and the lifting plate drives the brush plate to stably lift, and the brush head is arranged on the inner wall of the brush plate, the inner wall of the brush head is contacted with the surface of the terminal box shell, so that the brush head can brush and clean dust attached to the surface of the air inlet net opening, the phenomenon of blockage caused by the attached surface of the dust is reduced, and the heat radiation performance of the heat radiation air duct is ensured;
(2) The bottom ends of the radiating fins are contacted with the top end of the satellite internet terminal body, so that high-temperature heat energy generated by the satellite internet terminal body is absorbed by the radiating fins, when the radiating fan is electrified and started, the radiating fan blows the heat energy absorbed by the radiating fins out of the terminal box shell through the air outlet net opening, and external cold air flows into the terminal box shell through the air inlet net opening, so that the aim of easily radiating the satellite internet terminal body is fulfilled;
(3) The temperature sensor monitors the internal temperature of the terminal box shell, if the internal temperature of the terminal box shell is higher, the cooling fan is electrified to operate, if the internal temperature of the terminal box shell is lower and does not reach a set value, the cooling fan is closed to stop operating, and the satellite internet terminal body can be intelligently cooled by air, so that the energy conservation performance of a cooling air duct during use is improved.
Drawings
FIG. 1 is a schematic view of a three-dimensional structure of the present utility model;
FIG. 2 is an enlarged schematic view of the structure of FIG. 1A according to the present utility model;
FIG. 3 is a schematic diagram of the front view of the present utility model;
fig. 4 is a schematic cross-sectional elevation view of the present utility model.
The device comprises a terminal case, a 2, an air inlet net opening, a 3, an air outlet net opening, a 4, a bottom plate, a 5, a side supporting plate, a 6, a top plate, a 7, a lifting cylinder, a 8, a lifting plate, a 9, a guide rod, a 10, a guide cylinder, a 11, a brush plate, a 12, a brush head, a 13, a piece placing plate, a 14, a satellite internet terminal body, a 15, a temperature sensor, a 16, a singlechip, a 17, a side seat, a 18, a heat dissipation fin column, a 19, a heat dissipation fin, a 20 and a heat dissipation fan.
Detailed Description
The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. 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.
Referring to fig. 1-4, the heat dissipation air duct of a satellite internet terminal housing provided by the embodiment of the utility model comprises a terminal housing 1, wherein a piece placing plate 13 is arranged at the lower end inside the terminal housing 1, and a satellite internet terminal body 14 is arranged at the top end of the piece placing plate 13;
in use, the satellite internet terminal body 14 is supported and arranged by the arrangement of the piece placing plate 13;
a side seat body 17 is arranged on the inner wall of one side of the terminal box shell 1 above the satellite internet terminal body 14, and a heat dissipation fin column 18 is arranged on the inner wall of the side seat body 17;
In use, the heat dissipation fin 19 is arranged by the arrangement of the heat dissipation fin posts 18;
A plurality of radiating fins 19 are arranged on the outer wall of the radiating fin column 18, and the bottom ends of the radiating fins 19 are contacted with the top end of the satellite internet terminal body 14;
In use, the heat energy generated by the satellite internet terminal body 14 is absorbed by the heat radiating fins 19;
A cooling fan 20 is arranged at the top end of the cooling fin 19, a singlechip 16 is arranged on the inner wall of the terminal box shell 1 at one side of the cooling fan 20, and the output end of the singlechip 16 is electrically connected with the input end of the cooling fan 20;
In use, the satellite internet terminal body 14 is subjected to air cooling and heat dissipation by the arrangement of the heat dissipation fan 20;
The inner wall of the terminal box shell 1 at one side of the cooling fan 20 far away from the singlechip 16 is provided with a temperature sensor 15, and the output end of the temperature sensor 15 is electrically connected with the input end of the cooling fan 20;
When in use, the temperature sensor 15 is arranged so as to radiate the temperature inside the terminal box shell 1;
The lower end of the surface of the terminal box shell 1 is provided with an air inlet net mouth 2, one end of the air inlet net mouth 2 extends into the terminal box shell 1, the top end of the terminal box shell 1 is provided with an air outlet net mouth 3, the bottom end of the air outlet net mouth 3 extends into the terminal box shell 1, the surface of the terminal box shell 1 below the air inlet net mouth 2 is provided with a bottom plate 4, both sides of the top end of the bottom plate 4 are provided with side support plates 5, one end of the side support plates 5 far away from the bottom plate 4 is provided with a top plate 6, the center position of the top end of the top plate 6 is provided with a lifting cylinder 7, the bottom end of the lifting cylinder 7 penetrates through the top plate 6 and is provided with a lifting plate 8, both sides of the inside of the lifting plate 8 are provided with guide cylinders 10, and both ends of the guide cylinders 10 extend to the outside of the lifting plate 8;
The inside swing joint of guide cylinder 10 has guide bar 9, and guide bar 9's both ends all extend to the outside of guide cylinder 10 and respectively with the bottom of roof 6 and the top fixed connection of bottom plate 4, the bottom of lifter plate 8 is equipped with brush board 11, installs brush head 12 on the inner wall of brush board 11, and the inner wall of brush head 12 touches with the surface of terminal case 1 mutually.
When the embodiment of the application is used, firstly, the bottom ends of the radiating fins 19 are contacted with the top end of the satellite internet terminal body 14, so that high-temperature heat energy generated by the satellite internet terminal body 14 is absorbed by the radiating fins 19, when the radiating fan 20 is electrified and started, the radiating fan 20 blows out heat energy absorbed by the radiating fins 19 to the outside of the terminal box shell 1 through the air outlet net opening 3, external cold air flows into the terminal box shell 1 through the air inlet net opening 2 to easily cool the satellite internet terminal body 14, then the temperature inside the terminal box shell 1 is monitored through the temperature sensor 15, if the temperature inside the terminal box shell 1 is higher, the radiating fan 20 is electrified and runs, if the temperature inside the terminal box shell 1 is lower than a set value, the radiating fan 20 is closed and stops running, so that the satellite internet terminal body 14 can be intelligently cooled and radiated, so as to improve the energy conservation of the radiating, and finally, the lifting air cylinder 7 drives the lifting plate 8 to lift the guide cylinder 10 to slide on the outer wall of the guide rod 9, so that the lifting plate 8 drives the brush plate 11 to smoothly, and the brush head 11 is smoothly to be blocked by the inner wall 12 of the air duct 12, and the dust is adhered to the surface of the air duct 12, thereby the surface of the air duct 12 is blocked by the air duct 12, and the surface of the air duct is cleaned.
Claims (6)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202520330587.6U CN223899534U (en) | 2025-02-27 | 2025-02-27 | Radiating air duct of satellite internet terminal shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202520330587.6U CN223899534U (en) | 2025-02-27 | 2025-02-27 | Radiating air duct of satellite internet terminal shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN223899534U true CN223899534U (en) | 2026-02-10 |
Family
ID=98678368
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202520330587.6U Active CN223899534U (en) | 2025-02-27 | 2025-02-27 | Radiating air duct of satellite internet terminal shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN223899534U (en) |
-
2025
- 2025-02-27 CN CN202520330587.6U patent/CN223899534U/en active Active
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