CN213057542U - Unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep - Google Patents
Unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep Download PDFInfo
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- CN213057542U CN213057542U CN202021263114.2U CN202021263114U CN213057542U CN 213057542 U CN213057542 U CN 213057542U CN 202021263114 U CN202021263114 U CN 202021263114U CN 213057542 U CN213057542 U CN 213057542U
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- unmanned aerial
- aerial vehicle
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- 238000001816 cooling Methods 0.000 title claims abstract description 24
- 230000017525 heat dissipation Effects 0.000 claims abstract description 30
- 238000009434 installation Methods 0.000 claims abstract description 19
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 31
- 238000007789 sealing Methods 0.000 claims description 5
- 239000002826 coolant Substances 0.000 abstract description 15
- 239000007788 liquid Substances 0.000 abstract description 10
- 230000000694 effects Effects 0.000 abstract description 4
- 239000000110 cooling liquid Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep, motor output shaft fixedly connected with rotor, the bracing piece is all fixedly connected with in four corner position departments of unmanned aerial vehicle casing bottom, the inside installation cavity that has seted up of unmanned aerial vehicle casing, installation cavity bottom avris position department installs the electrical apparatus box, the utility model discloses the setting is provided with inlet tube, heat transfer case, outlet pipe, heat dissipation cavity and louvre, through the inlet tube, is convenient for pour into the heat transfer case fast the coolant liquid into, and through the mobility of coolant liquid, be convenient for the coolant liquid carries out the heat transfer to the electrical apparatus box outer end, when passing through the heat transfer cavity, is convenient for lead the heat in the outlet pipe to the louvre, and through rotor constantly rotation, thereby discharge the heat outside of unmanned aerial vehicle casing, thereby make the radiating effect better, make the coolant liquid after the cooling flow into, and then be convenient for carry out the water-cooling heat transfer to the inside electronic component of unmanned aerial vehicle.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep.
Background
With the development of science and technology, more and more consumers begin to pay attention to and use unmanned aerial vehicles, which are unmanned aerial vehicles for short, and are flying devices in rapid development, and the flying devices have the advantages of flexibility, quick response, unmanned flight and low operation requirements;
as disclosed in the prior art, the application number (201720890349.6) of the heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle is that the heat dissipation device for the electromagnetic control valve comprises the electromagnetic control valve, a heat dissipation sheet, a sealing ring and a cover plate, so that the heat dissipation is carried out on the interior of the unmanned aerial vehicle;
however, this patent can't utilize the mobility of coolant liquid to carry out water-cooling heat transfer to unmanned aerial vehicle internals to lead to being not good to unmanned aerial vehicle internals radiating effect, so we to these circumstances, for avoiding above-mentioned technical problem, really need provide an unmanned aerial vehicle solenoid electric control valve water-cooling heat abstractor of antiseep in order to overcome prior art the defect.
SUMMERY OF THE UTILITY MODEL
The utility model provides an unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep can effectively solve the mobility that can't utilize the coolant liquid that proposes among the above-mentioned background art and carry out the water-cooling heat transfer to the unmanned aerial vehicle internals to lead to the not good problem of unmanned aerial vehicle internals radiating effect.
In order to achieve the above object, the utility model provides a following technical scheme: an anti-leakage water-cooling heat dissipation device for an electromagnetic control valve of an unmanned aerial vehicle comprises an unmanned aerial vehicle shell, wherein fixing rods are fixedly connected to four corner positions at the top of the outer end of the unmanned aerial vehicle shell, a motor is installed at the side position at the top end of each fixing rod, a rotor is fixedly connected to an output shaft of the motor, supporting rods are fixedly connected to four corner positions at the bottom end of the unmanned aerial vehicle shell, an installation cavity is formed in the unmanned aerial vehicle shell, an electrical appliance box is installed at the side position at the bottom of the installation cavity, a storage box is fixedly connected to the central position at the bottom of the installation cavity, the electromagnetic control valve is installed at the top end of the storage box, a water inlet pipe is fixedly connected to one end of the storage box, a heat exchange box is fixedly connected to one end of the, the inner wall of the heat dissipation cavity is symmetrically provided with heat dissipation holes, and the input ends of the motor and the electromagnetic control valve are electrically connected with the output end of an internal power supply of the unmanned aerial vehicle;
the unmanned aerial vehicle casing top joint has the apron, apron top middle part is rotated and is connected with the screw rod, the screw rod bottom is rotated and is connected with the swing joint seat, swing joint seat bottom fixedly connected with rubber suction cup, the inside dashpot that has seted up of rubber suction cup, dashpot top central point puts the department and installs buffer spring, buffer spring one end fixedly connected with fly leaf.
Preferably, the heat exchange box is fixedly connected with an electric appliance box, and the bottom end of the electric appliance box is tightly attached to the installation cavity.
Preferably, the louvre runs through heat dissipation cavity inner wall, and the louvre communicates with each other with unmanned aerial vehicle casing one end.
Preferably, one end of the storage box is far away from the water inlet pipe, a water outlet pipe is fixedly connected to one side of the storage box, and sealing gaskets are sleeved at the connection positions of the water outlet pipe, the water inlet pipe and the storage box.
Preferably, the top end of the unmanned aerial vehicle shell is symmetrically provided with clamping grooves at the side positions of the bottom end of the cover plate, the four corner positions of the top end of the cover plate are provided with grooves, threaded grooves are formed in the bottoms of the grooves, and fastening bolts are rotatably connected inside the threaded grooves.
Preferably, the inner diameter of the groove is larger than the outer diameter of the fastening bolt.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model has the advantages of being scientific and reasonable in structure, convenience safe in utilization:
1. be provided with the inlet tube, the heat transfer case, the outlet pipe, heat dissipation cavity and louvre, through the inlet tube, be convenient for with the quick injection heat transfer case of coolant liquid, and mobility through the coolant liquid, the coolant liquid of being convenient for carries out the heat transfer to electrical apparatus box outer end, when through the heat transfer cavity, be convenient for with the inside heat direction louvre of outlet pipe, and constantly rotatory through the rotor, thereby with heat discharge unmanned aerial vehicle casing outside, thereby make the radiating effect better, make the coolant liquid after the cooling flow in the storage box again simultaneously, and then be convenient for carry out the water-cooling heat transfer to the inside electronic component of unmanned aerial vehicle.
2. Be provided with the screw rod, rubber suction cup, buffer spring and fly leaf, be convenient for remove rubber suction cup through the screw rod, when rubber suction cup contacts the storage box, thereby be convenient for extrude fixedly to the storage box, thereby make the storage box fix inside the installation cavity, avoid the storage box to rock inside the installation cavity, make inside water seepage leak, cause the unmanned aerial vehicle short circuit, in addition, through buffer spring and fly leaf cooperation, cushion at the extrusion force of screw rod, avoid the screw rod to cause the damage to the storage box.
3. Be provided with draw-in groove, recess, thread groove and fastening bolt, through the draw-in groove, the unmanned aerial vehicle casing of being convenient for and apron merge and separate to this is convenient for inspect and maintain the inside water-cooling heat transfer device of unmanned aerial vehicle casing, and through thread groove and recess, makes fastening bolt fix unmanned aerial vehicle casing and apron, avoids at the actual flight in-process, thereby apron unmanned aerial vehicle casing top roll-off, thereby causes the equipment part to damage.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.
In the drawings:
fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the structure of the heat dissipation holes of the present invention;
FIG. 3 is a schematic structural view of the rubber suction cup of the present invention;
fig. 4 is a schematic structural diagram of the storage box of the invention;
FIG. 5 is a schematic view of the area A in FIG. 4 according to the present invention;
reference numbers in the figures: 1. an unmanned aerial vehicle housing; 2. fixing the rod; 3. a motor; 4. a rotor; 5. a support bar; 6. an electrical box; 7. a storage box; 8. an electromagnetic control valve; 9. a water inlet pipe; 10. a heat exchange box; 11. a water outlet pipe; 12. a heat dissipation chamber; 13. heat dissipation holes; 14. a cover plate; 15. a screw; 16. a movable connecting seat; 17. a rubber suction cup; 18. a buffer tank; 19. a buffer spring; 20. a movable plate; 21. a card slot; 22. a groove; 23. a thread groove; 24. fastening a bolt; 25. and (5) installing the chamber.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
Example (b): as shown in fig. 1-5, the utility model provides a technical scheme, an unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep, including unmanned aerial vehicle casing 1, dead lever 2 is all fixedly connected with in four corner positions of the outer end top of unmanned aerial vehicle casing 1, motor 3 is installed in dead lever 2 top avris position, motor 3 output shaft fixedly connected with rotor 4, bracing piece 5 is all fixedly connected with in four corner positions of unmanned aerial vehicle casing 1 bottom, unmanned aerial vehicle casing 1 has seted up the installation cavity 25 inside, installation electrical apparatus box 6 is installed in installation cavity 25 bottom avris position, installation cavity 25 bottom central point fixedly connected with storage box 7, electromagnetic control valve 8 is installed on the top of storage box 7;
one end of the storage box 7 is fixedly connected with a water inlet pipe 9, one end of the water inlet pipe 9 is fixedly connected with a heat exchange box 10, the electric appliance box 6 is convenient to seal, the electric appliance box 6 is fixedly connected inside the heat exchange box 10, the bottom end of the electric appliance box 6 is tightly attached to the installation cavity 25, one end of the heat exchange box 10 is fixedly connected with a water outlet pipe 11, the position of one side of the storage box 7, which is far away from the water inlet pipe 9, is fixedly connected with a water outlet pipe 11, the joints of the water outlet pipe 11 and the water inlet pipe 9 and the storage box 7 are respectively sleeved with a sealing gasket, a heat dissipation cavity 12 is arranged at the position of one side of the inner wall of the installation cavity 25 inside the unmanned aerial vehicle shell 1, heat dissipation holes 13 are symmetrically arranged on the inner wall of the heat dissipation cavity 12, the input ends of the motor 3 and the electromagnetic control valve 8 are electrically connected with the output end of an internal power supply of the unmanned aerial vehicle;
the top end of the unmanned aerial vehicle shell body 1 is clamped with a cover plate 14, the middle part of the top end of the cover plate 14 is rotatably connected with a screw rod 15, the bottom end of the screw rod 15 is rotatably connected with a movable connecting seat 16, a rubber suction cup 17 is fixedly connected with the bottom end of the movable connecting seat 16, a buffer groove 18 is formed in the rubber suction cup 17, a buffer spring 19 is installed at the center position of the top of the buffer groove 18, and a movable plate 20 is fixedly connected with one.
Draw-in groove 21 has been seted up to the symmetry on 1 top of unmanned aerial vehicle casing that is located 14 bottom avris positions departments of apron for apron 14 and the separation of unmanned aerial vehicle casing 1, four corner positions departments on 14 tops of apron all seted up recess 22, and thread groove 23 has been seted up to recess 22 bottom, and the inside rotation of thread groove 23 is connected with fastening bolt 24, the fastening bolt 24's of being convenient for rotation, and recess 22 internal diameter is greater than fastening bolt 24 external diameter.
The utility model discloses a theory of operation and use flow: firstly, the unmanned aerial vehicle shell 1 and the cover plate 14 are convenient to combine through the clamping groove 21 and are slowly screwed into the threaded groove 23 through the fastening bolt 24, so that the unmanned aerial vehicle shell 1 and the cover plate 14 are fixed, and the cover plate 14 is prevented from sliding out of the top end of the unmanned aerial vehicle shell 1 in the actual flying process, so that parts are damaged;
the screw rod 15 is rotated, the screw rod 15 is rotated inside the movable connecting seat 16, the movable connecting seat 16 drives the rubber sucker 17 to move downwards, when the rubber sucker 17 contacts the top end of the storage box 7, the screw rod 15 is not rotated any more, the rubber sucker 17 is enabled to fix the storage box 7, the storage box 7 is prevented from lacking a component which is stable in reinforcement, the storage box 7 is enabled to slide inside the installation cavity 25, cooling liquid inside the storage box 7 leaks out, internal elements of the unmanned aerial vehicle are damaged, meanwhile, the cooling liquid is limited inside the storage box 7 through the storage box 7, the water outlet pipe 11 and a sealing gasket at the joint of the water inlet pipe 9, and leakage of the cooling liquid from the joints of the storage box 7, the water outlet pipe 11 and the;
secondly, the coolant in the storage tank 7 is guided to the water inlet pipe 9 through the electromagnetic control valve 8 and is guided to the heat exchange box 10 through the water inlet pipe 9, electronic elements in the unmanned aerial vehicle are installed in the electric appliance box, when the coolant flows into the heat exchange box 10, heat gathered at the outer end of the electric appliance box 6 is guided to the water outlet pipe 11 through the fluidity of the coolant, when the coolant after heat exchange passes through the water outlet pipe 11, the heat in the water outlet pipe 11 is guided to the heat dissipation holes 13 through the heat dissipation cavity 12, and the heat is guided to the outside of the unmanned aerial vehicle shell 1 through the heat dissipation holes 13, and due to the continuous rotation of the rotor wing 4, the ascending air flow blows away the heat, so that the water outlet pipe 11 guides the coolant after internal cooling back to the storage tank 7 again, and the water-cooling heat exchange is performed on;
finally, after flight work, rotate screw rod 15 for screw rod 15 is at the inside rotation of swing joint seat 16, thereby makes swing joint seat 16 drive rubber suction cup 17 and upwards removes, and through unscrewing fastening bolt 24, thereby makes the inside separation of apron 14 draw-in groove 21, and then makes apron 14 and the separation of unmanned aerial vehicle casing 1, so that the staff of being convenient for here inspects and maintains the inside water-cooling heat transfer subassembly of installation cavity 25.
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 described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep, includes unmanned aerial vehicle casing (1), four corner position departments of unmanned aerial vehicle casing (1) outer end top equal fixedly connected with dead lever (2), motor (3) are installed to dead lever (2) top avris position department, motor (3) output shaft fixedly connected with rotor (4), four corner position departments of unmanned aerial vehicle casing (1) bottom equal fixedly connected with bracing piece (5), its characterized in that: an installation cavity (25) is arranged in the unmanned aerial vehicle shell (1), an electric appliance box (6) is installed at the side position of the bottom of the installation cavity (25), a storage box (7) is fixedly connected at the central position of the bottom of the mounting chamber (25), an electromagnetic control valve (8) is installed at the top end of the storage box (7), one end of the storage box (7) is fixedly connected with a water inlet pipe (9), one end of the water inlet pipe (9) is fixedly connected with a heat exchange box (10), one end of the heat exchange box (10) is fixedly connected with a water outlet pipe (11), a heat dissipation chamber (12) is arranged at one side of the inner wall of the mounting chamber (25) in the unmanned aerial vehicle shell (1), the inner wall of the heat dissipation chamber (12) is symmetrically provided with heat dissipation holes (13), and the input ends of the motor (3) and the electromagnetic control valve (8) are electrically connected with the output end of an internal power supply of the unmanned aerial vehicle;
unmanned aerial vehicle casing (1) top joint has apron (14), apron (14) top middle part is rotated and is connected with screw rod (15), screw rod (15) bottom is rotated and is connected with swing joint seat (16), swing joint seat (16) bottom fixedly connected with rubber suction cup (17), inside buffer slot (18) of having seted up of rubber suction cup (17), buffer slot (18) top central point puts the department and installs buffer spring (19), buffer spring (19) one end fixedly connected with fly leaf (20).
2. The anti-leakage water-cooling heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle as claimed in claim 1, wherein: the heat exchange box (10) is internally and fixedly connected with an electric appliance box (6), and the bottom end of the electric appliance box (6) is tightly attached to the installation cavity (25).
3. The anti-leakage water-cooling heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle as claimed in claim 1, wherein: the heat dissipation holes (13) penetrate through the inner wall of the heat dissipation chamber (12), and the heat dissipation holes (13) are communicated with one end of the unmanned aerial vehicle shell (1).
4. The anti-leakage water-cooling heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle as claimed in claim 1, wherein: one end of the storage box (7) is far away from one side of the water inlet pipe (9) and is fixedly connected with a water outlet pipe (11), and the connection part of the water outlet pipe (11) and the water inlet pipe (9) and the storage box (7) is sleeved with a sealing gasket.
5. The anti-leakage water-cooling heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle as claimed in claim 1, wherein: the unmanned aerial vehicle casing (1) top is located apron (14) bottom avris position department symmetry and has seted up draw-in groove (21), four corner positions in apron (14) top all set up fluted (22), thread groove (23) have been seted up to recess (22) bottom, thread groove (23) inside rotation is connected with fastening bolt (24).
6. The anti-leakage water-cooling heat dissipation device for the electromagnetic control valve of the unmanned aerial vehicle as claimed in claim 5, wherein: the inner diameter of the groove (22) is larger than the outer diameter of the fastening bolt (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021263114.2U CN213057542U (en) | 2020-07-02 | 2020-07-02 | Unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021263114.2U CN213057542U (en) | 2020-07-02 | 2020-07-02 | Unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep |
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| Publication Number | Publication Date |
|---|---|
| CN213057542U true CN213057542U (en) | 2021-04-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021263114.2U Expired - Fee Related CN213057542U (en) | 2020-07-02 | 2020-07-02 | Unmanned aerial vehicle solenoid electric valve water-cooling heat abstractor of antiseep |
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| Country | Link |
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| CN (1) | CN213057542U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
-
2020
- 2020-07-02 CN CN202021263114.2U patent/CN213057542U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113329601A (en) * | 2021-07-07 | 2021-08-31 | 辽宁工程技术大学 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
| CN113329601B (en) * | 2021-07-07 | 2023-12-01 | 郑道仓 | Unmanned aerial vehicle remote sensing device for surveying and mapping engineering measurement |
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Granted publication date: 20210427 |