CN216070538U - Heat dissipation type unmanned aerial vehicle - Google Patents
Heat dissipation type unmanned aerial vehicle Download PDFInfo
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- CN216070538U CN216070538U CN202121923228.XU CN202121923228U CN216070538U CN 216070538 U CN216070538 U CN 216070538U CN 202121923228 U CN202121923228 U CN 202121923228U CN 216070538 U CN216070538 U CN 216070538U
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- heat dissipation
- heat
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses a heat dissipation type unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein a heat dissipation box is fixedly connected to the surface of the middle part of the bottom end of the unmanned aerial vehicle body, a heat absorption plate is fixedly connected to the middle part of the inner wall of the top end of the heat dissipation box, and a plurality of heat conduction columns are fixedly connected to the upper surface of the heat absorption plate. According to the utility model, the heat absorbing plate is fixed on the inner wall of the top end of the heat dissipation box, the heat absorbing plate absorbs heat generated during the operation of the unmanned aerial vehicle body through the plurality of heat conduction columns, and then the heat is dissipated through the plurality of heat dissipation fins and the plurality of heat dissipation columns arranged on the lower surface of the heat dissipation box, part of heat is dissipated into the protection shell through the plurality of heat dissipation fins for heat dissipation, and the plurality of heat dissipation columns convey the heat to the heat dissipation pipe internally circulating with cooling liquid, so that the heat dissipation effect of the device is improved, and the situation that components inside the unmanned aerial vehicle body are damaged due to overheating is avoided.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a heat dissipation type unmanned aerial vehicle.
Background
The unmanned plane is called as an unmanned plane for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a heat dissipation type unmanned aerial vehicle to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme: a heat dissipation type unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a heat dissipation box is fixedly connected to the surface of the middle of the bottom end of the unmanned aerial vehicle body, a heat absorption plate is fixedly connected to the middle of the inner wall of the top end of the heat dissipation box, a plurality of heat conduction columns are fixedly connected to the upper surface of the heat absorption plate and distributed in a rectangular array, one ends of the heat conduction columns, far away from the heat absorption plate, extend into the unmanned aerial vehicle body, a plurality of heat dissipation fins distributed at equal intervals are fixedly connected to the edges of the two sides of the lower surface of the heat dissipation box, the heat dissipation fins are arranged in an inclined shape, protective shells are fixedly connected to the surfaces of the two sides of the heat dissipation box, one ends of the heat dissipation fins, far away from the heat absorption plate, penetrate through the heat dissipation box and extend into the protective shells, heat dissipation tubes are fixedly connected to the inner wall of the bottom end of the heat dissipation box and are arranged in an S shape, and a plurality of heat dissipation columns distributed in a rectangular array are fixedly connected to the lower surface of the heat dissipation box, the bottom of the heat dissipation column is fixedly connected with the top surface of the heat dissipation pipe.
Preferably, a plurality of air inlet holes are formed in the surfaces of the two ends of the heat dissipation box, and the air inlet holes are distributed in a rectangular array mode.
Preferably, the air inlet hole is arranged in an inclined S shape and communicated with the inside of the heat dissipation box.
Preferably, the bottom middle part fixedly connected with liquid reserve tank of heat dissipation case, the inside coolant liquid that is provided with of liquid reserve tank, the terminal surface top fixedly connected with water pump of liquid reserve tank.
Preferably, the input fixedly connected with liquid suction pipe of water pump, the one end that the water pump was kept away from to the liquid suction pipe extends to the inside bottom of liquid reserve tank, the output fixedly connected with catheter of water pump, the one end that the water pump was kept away from to the catheter run through the heat dissipation case and with the one end bottom fixed connection of cooling tube.
Preferably, the other end bottom fixedly connected with drain pipe of cooling tube, the one end that the cooling tube was kept away from to the drain pipe runs through the heat dissipation case and is connected with the other end fixed surface of liquid reserve tank, the liquid filling opening has been seted up on one side surface top of liquid reserve tank.
Preferably, a plurality of air inlets have all been seted up on the both ends surface of protecting crust, and are a plurality of the air inlet is equidistant vertical distribution, the air inlet sets up to the slope form.
The utility model has the technical effects and advantages that:
according to the utility model, the heat absorbing plate is fixed on the inner wall of the top end of the heat dissipation box, the heat absorbing plate absorbs heat generated during the operation of the unmanned aerial vehicle body through the plurality of heat conduction columns, and then the heat is dissipated through the plurality of heat dissipation fins and the plurality of heat dissipation columns arranged on the lower surface of the heat dissipation box, part of heat is dissipated into the protection shell through the plurality of heat dissipation fins for heat dissipation, and the plurality of heat dissipation columns convey the heat to the heat dissipation pipe internally circulating with cooling liquid, so that the heat dissipation effect of the device is improved, and the situation that components inside the unmanned aerial vehicle body are damaged due to overheating is avoided.
Drawings
Fig. 1 is a schematic top view of the overall structure of the present invention.
FIG. 2 is a cross-sectional view of a heat dissipation box according to the present invention.
FIG. 3 is a schematic top-down view of the heat dissipation box structure of the present invention.
FIG. 4 is a side sectional view of the heat dissipation box structure of the present invention.
Fig. 5 is a perspective view of the structure of the heat dissipation box of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a heat dissipation box; 3. a heat absorbing plate; 4. a heat-conducting column; 5. a heat dissipating fin; 6. a protective shell; 7. a radiating pipe; 8. a heat-dissipating column; 9. an air inlet hole; 10. a liquid storage tank; 11. a water pump; 12. a liquid pumping pipe; 13. a catheter; 14. a liquid outlet pipe; 15. a liquid filling port; 16. an air inlet.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The utility model provides a heat dissipation type unmanned aerial vehicle as shown in figures 1-5, which comprises an unmanned aerial vehicle body 1, wherein a heat dissipation box 2 is fixedly connected to the surface of the middle part of the bottom end of the unmanned aerial vehicle body 1, a heat absorption plate 3 is fixedly connected to the middle part of the inner wall of the top end of the heat dissipation box 2, a plurality of heat conduction columns 4 are fixedly connected to the upper surface of the heat absorption plate 3, the plurality of heat conduction columns 4 are distributed in a rectangular array, one ends of the heat conduction columns 4 far away from the heat absorption plate 3 extend into the unmanned aerial vehicle body 1, a large amount of heat can be generated when the unmanned aerial vehicle body 1 works, the heat absorption plate 3 absorbs the heat through the plurality of heat conduction columns 4, heat dissipation is carried out through a plurality of heat dissipation fins 5 and a plurality of heat dissipation columns 8 arranged on the lower surface of the heat dissipation box 2, a plurality of heat dissipation fins 5 distributed at equal intervals are fixedly connected to the edges of the two sides of the lower surface of the heat dissipation box 2, the heat dissipation fins 5 are arranged in an inclined shape, and protective shells 6 are fixedly connected to the two side surfaces of the heat dissipation box 2, one end of each radiating fin 5, which is far away from the heat absorbing plate 3, penetrates through the radiating box 2 and extends into the protective shell 6, a plurality of radiating fins 5 radiate partial heat into the protective shell 6, meanwhile, external air enters into the protective shell 6 through the air inlet 16 when the unmanned aerial vehicle body 1 operates, circulation of air inside the protective shell 6 is accelerated, so that the heat is discharged, the radiating pipe 7 is fixedly connected to the inner wall of the bottom end of the radiating box 2, the radiating pipe 7 is S-shaped, the lower surface of the radiating box 2 is fixedly connected with a plurality of radiating columns 8 distributed in a rectangular array, the bottom ends of the radiating columns 8 are fixedly connected with the surface of the top ends of the radiating pipes 7, the plurality of radiating columns 8 convey residual heat to the radiating pipes 7 internally circulated with cooling liquid, the cooling liquid inside the radiating pipes 7 takes away the heat, so that the radiating effect of the device is improved, a plurality of air inlet holes 9 are formed in the surfaces of the two ends of the radiating box 2, a plurality of fresh air inlets 9 are the rectangular array and distribute, and fresh air inlet 9 sets up to the S-shaped of slope, and fresh air inlet 9 is linked together with heat dissipation case 2 is inside, makes outside air can enter into heat dissipation case 2 through fresh air inlet 9 inside for the inside circulation of air of heat dissipation case 2 avoids thermal giving off, has improved the radiating effect, and outside dust or water can effectively be avoided entering into inside heat dissipation case 2 to the fresh air inlet 9 of S-shaped simultaneously.
Secondly, a liquid storage tank 10 is fixedly connected to the middle of the bottom end of the heat dissipation tank 2, a cooling liquid is arranged inside the liquid storage tank 10, a water pump 11 is fixedly connected to the top of the surface of one end of the liquid storage tank 10, an input end of the water pump 11 is fixedly connected with a liquid pumping pipe 12, one end of the liquid pumping pipe 12, which is far away from the water pump 11, extends to the bottom of the inside of the liquid storage tank 10, an output end of the water pump 11 is fixedly connected with a liquid guide pipe 13, one end of the liquid guide pipe 13, which is far away from the water pump 11, penetrates through the heat dissipation tank 2 and is fixedly connected with the bottom of one end of the heat dissipation pipe 7, a liquid outlet pipe 14 is fixedly connected to the bottom of the other end of the liquid dissipation pipe 7, one end of the liquid outlet pipe 14, which is far away from the heat dissipation pipe 7, penetrates through the heat dissipation tank 2 and is fixedly connected with the surface of the other end of the liquid storage tank 10, the cooling liquid is guided into the heat dissipation pipe 7 by the cooperation of the liquid pumping pipe 12 and the liquid guide pipe 13, realize the circulation of coolant liquid, liquid filler 15 has been seted up on a side surface top of liquid reserve tank 10, be convenient for the staff to the inside coolant liquid that adds of liquid reserve tank 10, a plurality of air inlets 16 have all been seted up on the both ends surface of protecting crust 6, a plurality of air inlets 16 are equidistant vertical distribution, air inlet 16 sets up to the slope form, outside air when being convenient for unmanned aerial vehicle organism 1 through a plurality of air inlets 16 enters into protecting crust 6 inside, accelerate the inside circulation of air of protecting crust 6, thereby give off radiating fin 5 and take over to the inside heat of protecting crust 6.
The working principle of the utility model is as follows:
when the device is used, firstly, a worker adds cooling liquid into the liquid storage box 10 through the liquid adding port 15, the cooling liquid is guided into the radiating pipe 7 through the cooperation of the water pump 11, the liquid pumping pipe 12 and the liquid guide pipe 13, and then the circulating cooling liquid is discharged back into the liquid storage box 10 through the liquid guide pipe 14, so as to realize the circulation of the cooling liquid, the unmanned aerial vehicle body 1 can generate a large amount of heat during the work, the heat absorption plate 3 absorbs the heat through the heat conducting columns 4, then the heat is radiated through the radiating fins 5 and the radiating columns 8 arranged on the lower surface of the radiating box 2, the radiating fins 5 radiate partial heat into the protective shell 6, meanwhile, the external air enters the protective shell 6 through the air inlet 16 during the operation of the unmanned aerial vehicle body 1, the circulation of the air inside the protective shell 6 is accelerated, so as to discharge the heat, the radiating columns 8 convey the residual heat to the radiating pipe 7 with the cooling liquid circulating inside, the heat is taken away by the inside coolant liquid of cooling tube 7 to improve the radiating effect of this device, avoid the inside components and parts of unmanned aerial vehicle organism 1 to take place the condition emergence of overheated damage.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.
Claims (7)
1. The utility model provides a heat dissipation type unmanned aerial vehicle, includes unmanned aerial vehicle organism (1), its characterized in that: the surface of the middle part of the bottom end of the unmanned aerial vehicle body (1) is fixedly connected with a heat dissipation box (2), the middle part of the inner wall of the top end of the heat dissipation box (2) is fixedly connected with a heat absorption plate (3), the upper surface of the heat absorption plate (3) is fixedly connected with a plurality of heat conduction columns (4), the plurality of heat conduction columns (4) are distributed in a rectangular array, one ends of the heat conduction columns (4) far away from the heat absorption plate (3) extend into the unmanned aerial vehicle body (1), the edges of the two sides of the lower surface of the heat dissipation box (2) are fixedly connected with a plurality of heat dissipation fins (5) distributed at equal intervals, the heat dissipation fins (5) are arranged in an inclined shape, the surfaces of the two sides of the heat dissipation box (2) are fixedly connected with protective shells (6), one ends of the heat dissipation fins (5) far away from the heat absorption plate (3) penetrate through the protective shells (2) and extend into the protective shells (6), and the inner wall of the bottom end of the heat dissipation box (2) is fixedly connected with a heat dissipation pipe (7), the radiating pipe (7) is arranged in an S shape, a plurality of radiating columns (8) distributed in a rectangular array are fixedly connected to the lower surface of the radiating box (2), and the bottom ends of the radiating columns (8) are fixedly connected with the top surface of the radiating pipe (7).
2. The heat dissipation type unmanned aerial vehicle of claim 1, characterized in that: a plurality of air inlet holes (9) are all seted up on the both ends surface of heat dissipation case (2), and are a plurality of air inlet hole (9) are the rectangular array and distribute.
3. The heat dissipation type unmanned aerial vehicle of claim 2, characterized in that: the air inlet hole (9) is arranged in an inclined S shape, and the air inlet hole (9) is communicated with the inside of the heat dissipation box (2).
4. The heat dissipation type unmanned aerial vehicle of claim 3, characterized in that: the bottom middle part fixedly connected with liquid reserve tank (10) of heat dissipation case (2), the inside coolant liquid that is provided with of liquid reserve tank (10), the one end surface top fixedly connected with water pump (11) of liquid reserve tank (10).
5. The heat dissipation type unmanned aerial vehicle of claim 4, characterized in that: the input fixedly connected with liquid suction pipe (12) of water pump (11), the one end that water pump (11) were kept away from in liquid suction pipe (12) extends to the inside bottom of liquid reserve tank (10), output fixedly connected with catheter (13) of water pump (11), the one end that water pump (11) were kept away from in catheter (13) run through heat dissipation case (2) and with the one end bottom fixed connection of cooling tube (7).
6. The heat dissipation type unmanned aerial vehicle of claim 5, characterized in that: the other end bottom fixedly connected with drain pipe (14) of cooling tube (7), the one end that cooling tube (7) were kept away from in drain pipe (14) runs through heat dissipation case (2) and is connected with the other end fixed surface of liquid reserve tank (10), liquid filling opening (15) have been seted up on one side surface top of liquid reserve tank (10).
7. The heat dissipation type unmanned aerial vehicle of claim 6, characterized in that: a plurality of air inlets (16) have all been seted up on the both ends surface of protecting crust (6), and are a plurality of air inlet (16) are equidistant vertical distribution, air inlet (16) set up to the slope form.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121923228.XU CN216070538U (en) | 2021-08-17 | 2021-08-17 | Heat dissipation type unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121923228.XU CN216070538U (en) | 2021-08-17 | 2021-08-17 | Heat dissipation type unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216070538U true CN216070538U (en) | 2022-03-18 |
Family
ID=80670140
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121923228.XU Active CN216070538U (en) | 2021-08-17 | 2021-08-17 | Heat dissipation type unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216070538U (en) |
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2021
- 2021-08-17 CN CN202121923228.XU patent/CN216070538U/en active Active
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