CN217624141U - A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D - Google Patents
A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D Download PDFInfo
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- CN217624141U CN217624141U CN202221423783.0U CN202221423783U CN217624141U CN 217624141 U CN217624141 U CN 217624141U CN 202221423783 U CN202221423783 U CN 202221423783U CN 217624141 U CN217624141 U CN 217624141U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D, including the fuselage main part, fuselage main part week equidistance fixedly connected with installation arm, the installation arm is kept away from the equal fixedly connected with motor power of fuselage main part one end, the equal fixedly connected with screw in motor power output shaft top, the equal fixedly connected with support frame in motor power bottom, fuselage main part bottom center fixedly connected with heat-conducting plate. The utility model discloses, dispel the heat to lamp pearl and fixed lamp plate through the heat-conducting plate, realize the circulation flow of cooling water through the micropump, cool down the heat-conducting plate, improve the radiating effect of heat-conducting plate, and spray the cooling water through a plurality of water jet nozzles of sprinkler bead week side, reduce the temperature of cooling water; through setting up miniature fan, improve the inside air fluidity of improvement fuselage main part, cool down heat-conducting plate, battery case and control panel simultaneously.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to fancy stunt performance unmanned aerial vehicle for multi-scene cluster performance 3D.
Background
Along with the increasing application of unmanned aerial vehicles, the unmanned aerial vehicles are more and more integrated into the society, so that the functions of the unmanned aerial vehicles are also expanded; the unmanned aerial vehicle can not only carry out delivery and high-altitude shooting, but also gradually use the unmanned aerial vehicle for the performance of advertisements or programs in a plurality of industries; when the unmanned aerial vehicle performs the cluster performance, generally, a formation lamp for the light performance is installed on the unmanned aerial vehicle, and a large number of unmanned aerial vehicle clusters with the formation lamp are utilized to form various light patterns for performing the light performance.
In use discovers, unmanned aerial vehicle is when carrying out the cluster performance, and unmanned aerial vehicle's formation lamp need send the highlight, after long-time luminous, the temperature of formation lamp can rise, at the inside more heat that produces of unmanned aerial vehicle, thermal piling up can damage the inside various electronic components of unmanned aerial vehicle, consequently need in time dispel the heat, and current radiating mode, generally is simple dispels the heat through the fin, and the radiating efficiency is low.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a fancy stunt performance unmanned aerial vehicle for multi-scene cluster performance 3D can cool down the heat-conducting plate through the water-cooling simultaneously through the heat that heat-conducting plate conduction lamp pearl produced, improves the radiating efficiency.
The utility model discloses the technical scheme who takes specifically as follows:
the utility model provides a fancy stunt performance unmanned aerial vehicle for multi-scene cluster performance 3D, includes the fuselage main part, fuselage main part week side equidistance fixedly connected with installation arm, the installation arm is kept away from fuselage main part one end all fixedly connected with motor power, motor power output shaft top all fixedly connected with screw, motor power bottom all fixedly connected with support frame, fuselage main part bottom center fixedly connected with heat-conducting plate, heat-conducting plate bottom fixedly connected with fixed lamp plate, fixed lamp plate bottom fixedly connected with lamp housing, fixed lamp plate bottom week side equidistance fixedly connected with lamp pearl, fuselage main part both sides have all seted up the fresh air inlet, fuselage main part top has seted up the exhaust vent, fuselage main part bottom internal surface both sides fixedly connected with miniature fan, fuselage main part bottom internal surface one side fixedly connected with battery case, fuselage main part top internal surface center fixedly connected with control panel, fuselage main part bottom internal surface is kept away from battery case one side fixedly connected with a water storage section of thick bamboo;
the utility model discloses a solar water heater, including heat-conducting plate, water storage cylinder, heat-conducting plate, sealing box, heat-conducting plate, water storage cylinder one side bottom fixedly connected with inlet tube, the inlet tube is kept away from water storage cylinder one end with heat-conducting plate fixed connection, the heat-conducting plate is close to water storage cylinder one side bottom fixedly connected with wet return, the central fixedly connected with seal box in water storage cylinder bottom, the seal box center is provided with the micropump, micropump output end fixedly connected with spray pipe, the heat-conducting plate is close to battery case one side bottom fixedly connected with drain pipe.
And blocking nets are arranged at the centers of the air inlet and the air outlet.
The top of the water storage cylinder penetrates through the top of the machine body main body, and a sealing cover is arranged at the top of the water storage cylinder.
The water storage chamber has been seted up at the heat-conducting plate center, just inlet tube, wet return and drain pipe all communicate with the water storage chamber.
The sprinkler pipe top fixedly connected with sprinkler bead, just sprinkler bead week side equidistance is provided with the water spout.
The return water pipe is kept away from heat-conducting plate one end runs through water storage barrel head portion and with micro pump input end fixed connection.
The drain pipe is kept away from heat-conducting plate one end runs through fuselage main part bottom, just the drain pipe is kept away from heat-conducting plate one end is provided with the stopcock.
The utility model discloses the technological effect who gains does:
the utility model discloses, dispel the heat to lamp pearl and fixed lamp plate through the heat-conducting plate, realize the circulation of cooling water through the micropump and flow, lower the temperature to the heat-conducting plate, improve the radiating effect of heat-conducting plate, and spray the cooling water through a plurality of water jet nozzles of sprinkler bead week side, reduce the temperature of cooling water.
The utility model discloses, through setting up miniature fan, improve the inside air mobility of improvement fuselage main part, cool down heat-conducting plate, battery case and control panel simultaneously, avoid high temperature to cause electronic components to damage.
Drawings
FIG. 1 is a schematic structural view of the whole body of the present invention;
fig. 2 is a schematic cross-sectional view of the main body of the middle body of the present invention;
fig. 3 is an enlarged view of a portion a in fig. 2 according to the present invention;
fig. 4 is an enlarged view of the position B in fig. 2 according to the present invention.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a main body of the body; 2. mounting an arm; 3. a power motor; 4. a propeller; 5. a support frame; 6. a heat conducting plate; 7. fixing the lamp panel; 8. a lamp housing; 9. a lamp bead; 10. an air inlet hole; 11. an air outlet; 12. a micro fan; 13. a battery case; 14. a control panel; 15. a water storage cylinder; 16. a sealing cover; 17. a water inlet pipe; 18. a water return pipe; 19. a sealing box; 20. a micro-pump; 21. a water spray pipe; 22. a sprinkler head; 23. a drain pipe; 24. and (4) pipe plugs.
Detailed Description
In order to make the objects and advantages of the present invention more apparent, the present invention will be described in detail with reference to the following embodiments. It is to be understood that the following text is only intended to describe one or several particular embodiments of the invention, and does not strictly limit the scope of the claims specifically claimed.
As shown in figures 1 and 2, an fancy stunt performance unmanned aerial vehicle for multi-scene cluster performance 3D comprises a main body 1, wherein mounting arms 2 are fixedly connected with the periphery of the main body 1 at equal intervals, one ends of the mounting arms 2, which are far away from the main body 1, are fixedly connected with power motors 3, propellers 4 are fixedly connected with the tops of output shafts of the power motors 3, support frames 5 are fixedly connected with the bottoms of the power motors 3, a heat conduction plate 6 is fixedly connected with the center of the bottom of the main body 1, a fixed lamp plate 7 is fixedly connected with the bottom of the heat conduction plate 6, a lamp housing 8 is fixedly connected with the bottom of the fixed lamp plate 7 at equal intervals, air inlet holes 10 are formed in the two sides of the main body 1, air outlet holes 11 are formed in the top of the main body 1, blocking nets are arranged at the centers of the air inlet holes 10 and the air outlet holes 11, and sundries are filtered through the blocking nets, the problem that sundries enter the interior of the main body 1 of the unmanned aerial vehicle from the air inlet 10 or the air outlet 11 to affect the normal operation of the unmanned aerial vehicle is solved, the micro fans 12 are fixedly connected to two sides of the inner surface of the bottom of the main body 1 of the unmanned aerial vehicle, after the two micro fans 12 are started, the micro fans 12 blow air outside the main body 1 of the unmanned aerial vehicle into the main body 1 of the unmanned aerial vehicle, and then the air is discharged from the air outlet 11 to improve the air circulation inside the main body 1 of the unmanned aerial vehicle, the battery box 13 is fixedly connected to one side of the inner surface of the bottom of the main body 1 of the unmanned aerial vehicle, the control panel 14 is fixedly connected to the center of the inner surface of the top of the main body 1 of the unmanned aerial vehicle, the battery box 13 and the control panel 14 are cooled by blowing air through the micro fans 12, the water storage cylinder 15 is fixedly connected to one side of the inner surface of the bottom of the main body 1 of the main body of the unmanned aerial vehicle, the top of the water storage cylinder 15 penetrates through the top of the main body 1, the sealing cover 16 is arranged on the top of the water storage cylinder 15, and cooling water is added into the water storage cylinder 15, and then covered with the sealing cap 16.
According to above-mentioned structure, the heat conduction that produces when a plurality of lamp pearls 9 throw light on gives heat-conducting plate 6, blows through micro fan 12, improves the inside air mobility of fuselage main part 1, can cool down heat-conducting plate 6, and simultaneously, battery and control panel 14 in the battery case 13 also can produce higher temperature at the during operation, cools down battery case 13 and control panel 14 through micro fan 12.
As shown in fig. 3 and 4, a water inlet pipe 17 is fixedly connected to the bottom of one side of the water storage cylinder 15 close to the heat conducting plate 6, one end of the water inlet pipe 17 far away from the water storage cylinder 15 is fixedly connected with the heat conducting plate 6, a water return pipe 18 is fixedly connected to the bottom of one side of the heat conducting plate 6 close to the water storage cylinder 15, a water storage cavity is formed in the center of the heat conducting plate 6, the water inlet pipe 17, the water return pipe 18 and a drain pipe 23 are all communicated with the water storage cavity, cooling water in the water storage cylinder 15 flows into the water storage cavity of the heat conducting plate 6 through the water inlet pipe 17, thereby cooling the heat conducting plate 6 and improving the heat dissipation effect, a sealing box 19 is fixedly connected to the center of the inner surface of the bottom of the water storage cylinder 15, a micro pump 20 is arranged at the center of the sealing box 19, one end of the water return pipe 18 far away from the heat conducting plate 6 penetrates through the bottom of the water storage cylinder 15 and is fixedly connected with the input end of the micro pump 20, after the micro pump 20 is started, higher cooling water of water storage intracavity temperature through wet return 18 extraction heat-conducting plate 6, micropump 20 output end fixedly connected with spray pipe 21, spray pipe 21 top fixedly connected with sprinkler bead 22, and sprinkler bead 22 week side equidistance is provided with the water spout, a plurality of water spouts spray the higher cooling water of temperature to in water storage section of thick bamboo 15, spray through the water spout and cool down the cooling water, heat-conducting plate 6 is close to battery case 13 one side bottom fixedly connected with drain pipe 23 and keeps away from 6 one end of heat-conducting plate and run through fuselage main part 1 bottom, and drain pipe 23 keeps away from 6 one end of heat-conducting plate and is provided with stopcock 24, in normal work, stopcock 24 carries out the shutoff to drain pipe 23, avoid the cooling water to flow out, in the time of stopping working, open stopcock 24, make the cooling water flow out from drain pipe 23.
According to above-mentioned structure, pour into the cooling water into heat-conducting plate 6 through inlet tube 17 inside, lower the temperature to heat-conducting plate 6, improve heat-radiating efficiency of heat-conducting plate 6, through the cooperation of micropump 20 and wet return 18, realize the circulation flow of cooling water, improve cooling efficiency, and conveniently discharge the cooling water through drain pipe 23.
The utility model discloses a theory of operation does: at first in adding the cooling water into water storage cylinder 15, through the heat that 6 conduction lamp pearls 9 of heat-conducting plate produced, the cooling water enters into the inside water storage cavity of heat-conducting plate 6 through inlet tube 17, cool down heat-conducting plate 6, start micropump 20, take out the cooling water that 6 inside temperature risees of heat-conducting plate, a plurality of water jet through sprinkler bead 22 spray the cooling water, cool down the cooling water, then flow into the inside water storage cavity of heat-conducting plate 6 once more, through two micro fan 12, improve the air mobility of 1 inside of fuselage main part, cool down heat-conducting plate 6, cool down battery case 13 and control panel 14 simultaneously.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention. Structures, devices and methods of operation not specifically described or illustrated in the present application are not specifically illustrated or described, but are generally practiced in the art without limitation.
Claims (7)
1. A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D, includes fuselage main part (1), its characterized in that: the novel multifunctional electric vehicle is characterized in that the mounting arms (2) are fixedly connected with the equal intervals of the circumferential sides of the body main body (1), the mounting arms (2) are far away from the equal fixedly connected with power motors (3) at one ends of the body main body (1), the equal fixedly connected with propellers (4) at the tops of output shafts of the power motors (3), the equal fixedly connected with supporting frames (5) at the bottoms of the power motors (3), heat-conducting plates (6) are fixedly connected with the centers of the bottoms of the body main body (1), fixed lamp plates (7) are fixedly connected with the bottoms of the heat-conducting plates (6), and lamp housings (8) are fixedly connected with the bottoms of the fixed lamp plates (7), the lamp beads (9) are fixedly connected with the fixed lamp plate (7) at the bottom of the lamp plate in an equidistant mode, air inlet holes (10) are formed in the two sides of the machine body (1), air outlet holes (11) are formed in the top of the machine body (1), micro fans (12) are fixedly connected with the two sides of the inner surface of the bottom of the machine body (1), a battery box (13) is fixedly connected with one side of the inner surface of the bottom of the machine body (1), a control panel (14) is fixedly connected with the center of the inner surface of the top of the machine body (1), and a water storage barrel (15) is fixedly connected with one side, away from the battery box (13), of the inner surface of the bottom of the machine body (1);
water storage cylinder (15) are close to heat-conducting plate (6) one side bottom fixedly connected with inlet tube (17), keep away from inlet tube (17) water storage cylinder (15) one end with heat-conducting plate (6) fixed connection, heat-conducting plate (6) are close to water storage cylinder (15) one side bottom fixedly connected with wet return (18), water storage cylinder (15) bottom internal surface center fixedly connected with seal box (19), seal box (19) center is provided with micropump (20), micropump (20) output end fixedly connected with spray pipe (21), heat-conducting plate (6) are close to battery case (13) one side bottom fixedly connected with drain pipe (23).
2. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: and blocking nets are arranged at the centers of the air inlet hole (10) and the air outlet hole (11).
3. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: the top of the water storage cylinder (15) penetrates through the top of the machine body main body (1), and a sealing cover (16) is arranged at the top of the water storage cylinder (15).
4. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: the water storage chamber has been seted up at heat-conducting plate (6) center, just inlet tube (17), wet return (18) and drain pipe (23) all communicate with the water storage chamber.
5. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: the top of the water spraying pipe (21) is fixedly connected with a water spraying head (22), and water spraying nozzles are arranged on the periphery of the water spraying head (22) at equal intervals.
6. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: the water return pipe (18) is far away from one end of the heat-conducting plate (6) and penetrates through the bottom of the water storage cylinder (15) and is fixedly connected with the input end of the micro pump (20).
7. Fancy trick drone for multi-scene cluster performance 3D according to claim 1, characterized by: the drain pipe (23) is kept away from heat-conducting plate (6) one end runs through fuselage main part (1) bottom, just drain pipe (23) is kept away from heat-conducting plate (6) one end is provided with stopcock (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221423783.0U CN217624141U (en) | 2022-06-08 | 2022-06-08 | A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221423783.0U CN217624141U (en) | 2022-06-08 | 2022-06-08 | A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217624141U true CN217624141U (en) | 2022-10-21 |
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ID=83625478
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221423783.0U Active CN217624141U (en) | 2022-06-08 | 2022-06-08 | A fancy trick performance unmanned aerial vehicle for multi-scene cluster performance 3D |
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| Country | Link |
|---|---|
| CN (1) | CN217624141U (en) |
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2022
- 2022-06-08 CN CN202221423783.0U patent/CN217624141U/en active Active
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