CN112208778A - Oil-electricity hybrid power cooling system for unmanned aerial vehicle - Google Patents
Oil-electricity hybrid power cooling system for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN112208778A CN112208778A CN202011100985.7A CN202011100985A CN112208778A CN 112208778 A CN112208778 A CN 112208778A CN 202011100985 A CN202011100985 A CN 202011100985A CN 112208778 A CN112208778 A CN 112208778A
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- water
- outer heat
- heat conduction
- cooling
- mounting shell
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- 238000001816 cooling Methods 0.000 title claims abstract description 98
- 238000009434 installation Methods 0.000 claims abstract description 58
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 55
- 230000017525 heat dissipation Effects 0.000 claims abstract description 30
- 239000003814 drug Substances 0.000 claims description 36
- 238000007789 sealing Methods 0.000 claims description 7
- 230000005855 radiation Effects 0.000 claims 2
- 239000000575 pesticide Substances 0.000 abstract description 13
- 238000010521 absorption reaction Methods 0.000 abstract description 10
- 239000000110 cooling liquid Substances 0.000 abstract description 6
- 238000005507 spraying Methods 0.000 abstract description 2
- 238000005192 partition Methods 0.000 description 13
- 239000007788 liquid Substances 0.000 description 5
- 239000002826 coolant Substances 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
- B64D33/10—Radiator arrangement
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention discloses an oil-electricity hybrid power heat dissipation system for an unmanned aerial vehicle, pesticide spraying is carried in a flexible pesticide box, the top of the mounting shell is wrapped, the first water-cooling guide pipes at the four ends of the top of the mounting shell, the second water-cooling guide pipes at the four ends of the bottom of the mounting shell, the circulation conduits at the four ends of the installation shell in the vertical direction absorb heat and cool the eight end positions of the installation shell, so that the water of the first water-cooling conduit flows into the drainage grooves of the outer heat-conducting grid, the side surface of the mounting shell is subjected to heat absorption and temperature reduction, so that through the flowing of cooling liquid and the heat absorption of pesticide sprayed in the flexible pesticide box at the top, the driving equipment is cooled by water on the basis of ensuring the minimum load capacity, so that the normal operation of the driving equipment is ensured.
Description
Technical Field
The invention relates to the technical field of power heat dissipation of unmanned aerial vehicles, in particular to an oil-electricity hybrid power heat dissipation system for an unmanned aerial vehicle.
Background
Drones are currently unmanned aircraft that are operated by radio remote control devices and self-contained program control devices or are operated autonomously, either completely or intermittently, by an on-board computer. Compared with manned flight, the unmanned aerial vehicle is more suitable for too many tasks, is applied to the fields of aerial photography, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting and the like at present, and greatly expands the application of the unmanned aerial vehicle.
Because unmanned aerial vehicle's drive arrangement calorific capacity is huge after long-time work, and then need cool down drive arrangement, inside current cooling mode was through making outside air get into drive arrangement, carried out the forced air cooling to drive arrangement, nevertheless because unmanned aerial vehicle's wind direction often changes, and drive arrangement can't guarantee that every direction can both the air inlet to influence drive arrangement's cooling effect.
Disclosure of Invention
The invention aims to provide an oil-electricity hybrid power heat dissipation system for an unmanned aerial vehicle, and aims to solve the technical problem that in the prior art, external air enters driving equipment to cool the driving equipment in an air cooling mode, but the driving equipment cannot ensure that air can enter in each direction due to frequent change of the wind direction of the unmanned aerial vehicle, so that the cooling effect of the driving equipment is influenced.
In order to achieve the purpose, the oil-electricity hybrid power heat dissipation system for the unmanned aerial vehicle comprises a rack, a mounting shell, driving equipment and a heat dissipation device, wherein the mounting shell is arranged on the rack; the mounting shell is fixedly connected with the rack and positioned on one side of the rack, and the driving device is rotatably connected with the mounting shell; the heat dissipation device comprises a flexible medicine box, an outer heat conduction grid, a sealing cover plate, a first water cooling pipe, a second water cooling pipe and a drainage assembly, the flexible medicine box is detachably connected with the installation shell and is positioned on one side of the installation shell far away from the driving equipment, the outer heat conduction grid is fixedly connected with the installation shell and is positioned on one side of the installation shell close to the flexible medicine box, the outer heat conduction grid is provided with a drainage groove, the drainage groove is positioned on one side of the outer heat conduction grid far away from the installation shell, the sealing cover plate is fixedly connected with the outer heat conduction grid and is covered with the drainage groove and is positioned on one side of the outer heat conduction grid close to the drainage groove, the first water cooling pipe is fixedly connected with the installation shell and is positioned between the flexible medicine box and the outer heat conduction grid, and the second water cooling pipe is fixedly connected with the installation shell, the first water-cooling guide pipe is communicated with the outer heat conduction grid, and the outer heat conduction grid is located on one side, away from the flexible medicine box, of the outer heat conduction grid; the drainage subassembly includes circulation pipe, diversion joint and water gathering joint, the circulation pipe with installation casing fixed connection, and one end with first water-cooling pipe switch-on, the other end with second water-cooling pipe link up, and is located first water-cooling pipe with between the second water-cooling pipe, the diversion joint with outer heat conduction grid fixed connection, and one side with the drainage groove link up, the opposite side with first water-cooling pipe link up, and is located outer heat conduction grid with between the first water-cooling pipe, one side of gathering water joint with outer heat conduction grid fixed connection, and one side with second water-cooling pipe link up, the opposite side with the drainage groove link up, and is located second water-cooling pipe with between the outer heat conduction grid.
The heat dissipation device further comprises a medicine box fixing frame, the medicine box fixing frame is fixedly connected with the installation shell, detachably connected with the flexible medicine box and located on one side, close to the flexible medicine box, of the installation shell.
The driving device comprises a stator and a rotor, wherein the stator is fixedly connected with the mounting shell and is positioned inside the mounting shell; the rotor is rotationally connected with the stator and is positioned on one side of the stator, which is far away from the mounting shell.
The driving device further comprises a heat dissipation fan, and the heat dissipation fan is fixedly connected with the rotor and is located at one end, far away from the stator, of the rotor.
The driving equipment further comprises an air inlet grid and an air supply grid, wherein the air inlet grid is fixedly connected with the mounting shell, penetrates through the mounting shell and is positioned on one side of the mounting shell, which is close to the heat dissipation fan; the air supply grille is fixedly connected with the mounting shell, penetrates through the mounting shell and is positioned on one side, far away from the air supply grille, of the mounting shell.
The oil-electricity hybrid power heat dissipation system for the unmanned aerial vehicle further comprises a rotor, wherein the rotor is connected with the rack in a rotating mode and located on one side of the installation shell, and the rack is far away from the installation shell.
The oil-electricity hybrid power heat dissipation system for the unmanned aerial vehicle further comprises an adjusting bracket, the adjusting bracket is detachably connected with the rack, is connected with the rotor in a rotating mode, and is located close to one side of the rotor.
The oil-electricity hybrid power heat dissipation system for the unmanned aerial vehicle is characterized in that pesticide spraying is loaded in the flexible pesticide box, the top of the mounting shell is wrapped, the first water-cooling guide pipes at the four ends of the top of the mounting shell, the second water-cooling guide pipes at the four ends of the bottom of the mounting shell, the circulation conduits at the four ends of the installation shell in the vertical direction absorb heat and cool the eight end positions of the installation shell, so that the water of the first water-cooling conduit flows into the drainage grooves of the outer heat-conducting grid, the side surface of the mounting shell is subjected to heat absorption and temperature reduction, so that through the flowing of cooling liquid and the heat absorption of pesticide sprayed in the flexible pesticide box at the top, the driving equipment is cooled by water on the basis of ensuring the minimum load capacity, so that the normal operation of the driving equipment is ensured.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic view of a rotor mounting structure of the present invention.
Fig. 2 is a schematic structural diagram of the heat dissipation device of the present invention.
FIG. 3 is a schematic view of the construction of the drainage assembly of the present invention.
Fig. 4 is a schematic structural view of the flexible medicine chest of the present invention.
Fig. 5 is a schematic view of a connection structure of a first water-cooling duct and a second water-cooling duct of the present invention.
Fig. 6 is a schematic structural view of the driving apparatus of the present invention.
In the figure: 1-frame, 2-installation shell, 3-driving equipment, 4-heat dissipation device, 5-rotor wing, 6-adjustment bracket, 31-stator, 32-rotor, 33-cooling fan, 34-air inlet grid, 35-air supply grid, 41-flexible medicine chest, 42-outer heat conduction grid, 43-sealing cover plate, 44-first water cooling conduit, 45-second water cooling conduit, 46-drainage component, 47-medicine chest fixing frame, 100-unmanned aerial vehicle oil-electricity hybrid power heat dissipation system, 421-drainage groove, 461-circulation conduit, 462-water diversion joint, 463-water gathering joint, 464-water diversion partition plate and 465-water gathering partition plate.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1 to 5, the present invention provides an oil-electric hybrid power heat dissipation system 100 for an unmanned aerial vehicle, which includes a frame 1, a mounting housing 2, a driving apparatus 3, and a heat dissipation device 4; the mounting shell 2 is fixedly connected with the rack 1 and is positioned on one side of the rack 1, and the driving device 3 is rotatably connected with the mounting shell 2; the heat dissipation device 4 comprises a flexible medicine box 41, an outer heat conduction grid 42, a sealing cover plate 43, a first water cooling pipe 44, a second water cooling pipe 45 and a drainage assembly 46, the flexible medicine box 41 is detachably connected with the installation casing 2 and is located at one side of the installation casing 2 far away from the driving device 3, the outer heat conduction grid 42 is fixedly connected with the installation casing 2 and is located at one side of the installation casing 2 close to the flexible medicine box 41, the outer heat conduction grid 42 is provided with a drainage groove 421, the drainage groove 421 is located at one side of the installation casing 2 far away from the outer heat conduction grid 42, the sealing cover plate 43 is fixedly connected with the outer heat conduction grid 42 and is covered with the drainage groove 421 and is located at one side of the outer heat conduction grid 42 close to the drainage groove 421, the first water cooling pipe 44 is fixedly connected with the installation casing 2, the second water-cooling duct 45 is fixedly connected to the mounting case 2, is communicated with the first water-cooling duct 44, and is located on the side of the outer heat-conducting grid 42 away from the flexible medicine box 41; the drainage assembly 46 includes a circulation conduit 461, a water diversion connector 462 and a water collection connector 463, the circulation conduit 461 is fixedly connected with the installation housing 2, and one end of the circulation conduit 461 is communicated with the first water-cooling conduit 44, the other end of the circulation conduit is communicated with the second water-cooling conduit 45 and is located between the first water-cooling conduit 44 and the second water-cooling conduit 45, the water diversion connector 462 is fixedly connected with the outer heat-conducting grid 42, and one side of the water diversion connector 462 is communicated with the drainage groove 421, the other side of the water diversion connector is communicated with the first water-cooling conduit 44 and is located between the outer heat-conducting grid 42 and the first water-cooling conduit 44, one side of the water collection connector 463 is fixedly connected with the outer heat-conducting grid 42, and one side of the water diversion connector is communicated with the second water-cooling conduit 45, and the other side of the water diversion connector 463 is communicated with the drainage groove 421 and.
In the present embodiment, the driving device 3 is installed in the installation housing 2, the bottom of the installation housing 2 is screwed to the upper surface of the rack 1, the flexible medicine box 41 is installed on the top of the installation housing 2 by a bracket to wrap the surface of the installation housing 2, the flexible medicine box 41 is a customized pesticide box, the outer layer of the flexible medicine box is made of a flexible material, the interior of the flexible medicine box 41 is filled with a liquid pesticide spray, and the liquid pesticide spray has heat absorption property to absorb heat to the installation housing 2, so that heat in the installation housing 2 is conducted; the first water-cooling guide pipes 44 are respectively installed at four end positions of the top of the installation shell 2, the second water-cooling guide pipes 45 are respectively installed at four end positions of the bottom of the installation shell 2, the circulation guide pipes 461 are installed at four end portions of the installation shell 2 in the vertical direction, the first water-cooling guide pipes 44, the circulation guide pipes 461 and the second water-cooling guide pipes 45 are communicated, and cooling liquid is filled in the guide pipes, so that the cooling liquid flows among the first water-cooling guide pipes 44, the circulation guide pipes 461 and the second water-cooling guide pipes 45, and the eight end positions of the installation shell 2 are subjected to heat absorption and temperature reduction; the outer heat conducting grids 42 are fixed on four sides of the installation shell 2 in a threaded manner, each outer heat conducting grid 42 is provided with a plurality of drainage grooves 421, the length direction of each drainage groove 421 faces the bottom and the top of the installation shell 2, the top of each outer heat conducting grid 42 is communicated with the first water cooling pipe 44 through the water diversion connector 462, the bottom of each outer heat conducting grid 42 is connected with the second water cooling pipe 45 through the water collection connector 463, so that the water of the first water cooling pipe 44 flows into the drainage grooves 421 of the outer heat conducting grids 42, and the sides of the installation shell 2 are subjected to heat absorption and temperature reduction, and thus, the flexible medicine box 41 is loaded with sprayed pesticide and wraps the top of the installation shell 2, the first water cooling pipes 44 on four ends of the top of the installation shell 2, and the second water cooling pipes 45 on four ends of the bottom of the installation shell 2, and four tip of the vertical direction of installation casing 2 the circulation pipe 461 is right eight tip positions of installation casing 2 carry out the heat absorption cooling, make the rivers of first water-cooling pipe 44 flow into outer heat conduction grid 42 in the drainage groove 421, it is right the side of installation casing 2 carries out the heat absorption cooling, so through the flow and the top of coolant liquid spray the heat absorption of pesticide in the flexible medical kit 41, make on the basis of guaranteeing minimum loading capacity to drive apparatus 3 carries out the water-cooling, thereby has guaranteed drive apparatus 3's normal operating.
Further, referring to fig. 3, the flow guiding assembly 46 further includes a water guiding partition plate 464, one side of the water guiding partition plate 464 is fixedly connected to the outer heat conducting grid 42, and the other side is fixedly connected to the first water cooling conduit 44 and is located between the first water cooling conduit 44 and the outer heat conducting grid 42.
In this embodiment, the bottom of the first water-cooling duct 44 has an opening, one end of the water-guiding partition plates 464 is screwed to the first water-cooling duct 44, and the water-guiding partition plates are plural in number and extend into the opening inside the first water-cooling duct 44 respectively, and the other end of the water-guiding partition plates are screwed to the outer heat-conducting grid 42, and the water-guiding partition plates 464 are connected to the drainage grooves 421 of the outer heat-conducting grid 42 one by one, so that the two adjacent water-guiding partition plates 464 guide the cooling liquid of the first water-cooling duct 44 into one drainage groove 421, thereby dispersing the cooling liquid and increasing the cooling area.
Further, referring to fig. 3, the drainage assembly 46 further includes a water collecting partition plate 465, the water collecting partition plate 465 is fixedly connected with the water collecting joint 463, and one side of the water collecting partition plate 465 is fixedly connected with the outer heat conducting grid 42, and the other side of the water collecting partition plate 465 is fixedly connected with the second water cooling conduit 45 and is located between the second water cooling conduit 45 and the outer heat conducting grid 42.
In this embodiment, the top of second water-cooling pipe 45 has an opening, gather water division board 465 one end with second water-cooling pipe 45 thread tightening to the quantity is a plurality of, is close to respectively the opening of second water-cooling pipe 45, the other end with outer heat conduction grid 42 thread tightening, it is a plurality of gather water division board 465 respectively with a plurality of outer heat conduction grid 42 drainage groove 421 one-to-one, thereby make adjacent two gather water division board 465 with the coolant liquid in the drainage groove 421 is introduced in the second water-cooling pipe 45, thereby has accelerated the flow of coolant liquid.
Further, referring to fig. 4, the heat dissipation device 4 further includes a medicine box fixing frame 47, and the medicine box fixing frame 47 is fixedly connected to the installation housing 2, detachably connected to the flexible medicine box 41, and located on one side of the installation housing 2 close to the flexible medicine box 41.
In the present embodiment, the medicine-box fixing frame 47 is screwed to the top portion of the attachment case 2, and the side ends of the flexible medicine boxes 41 are fixed by the medicine-box fixing frame 47 near the first water-curtain duct, so that the stability of the flexible medicine boxes 41 is improved.
Further, referring to fig. 6, the driving device 3 includes a stator 31 and a rotor 32, the stator 31 is fixedly connected to the mounting housing 2 and is located inside the mounting housing 2; the rotor 32 is rotatably connected to the stator 31 and is located on a side of the stator 31 remote from the mounting housing 2.
In the present embodiment, the rotor 32 is located inside the stator 31, is connected to the mounting case 2 through a bearing, and is driven to rotate by a motor, thereby outputting power.
Further, referring to fig. 6, the driving apparatus 3 further includes a heat dissipation fan 33, and the heat dissipation fan 33 is fixedly connected to the rotor 32 and is located at an end of the rotor 32 away from the stator 31.
In this embodiment, the outer shell of the heat dissipation fan 33 is fixed to the inner side surface of the mounting housing 2 through threads, and the helical blades are fixed to the rotor 32 through threads, so that the heat dissipation fan 33 is driven to rotate through the rotation of the rotor 32, and the air cooling of the driving device 3 is further performed.
Further, referring to fig. 6, the driving apparatus 3 further includes an air inlet grille 34 and an air outlet grille 35, wherein the air inlet grille 34 is fixedly connected to the mounting housing 2, penetrates through the mounting housing 2, and is located on one side of the mounting housing 2 close to the heat dissipation fan 33; the air supply grille 35 is fixedly connected with the mounting housing 2, penetrates through the mounting housing 2, and is located on one side of the mounting housing 2 far away from the air supply grille 34.
In the present embodiment, both the air intake grill 34 and the air supply grill 35 have small holes for ventilation, so that external air can enter the inside of the mounting case 2, the air intake grill 34 is located on the side of the mounting case 2 close to the heat dissipation fan 33, and the air supply grill 35 is located on the side of the mounting case 2 away from the air intake grill 34, so that the heat dissipation fan 33 drives the air inside the mounting case 2 to circulate, thereby cooling the drive device 3.
Further, referring to fig. 1, the oil-electric hybrid cooling system 100 for the unmanned aerial vehicle further includes a rotor 5, where the rotor 5 is rotatably connected to the rack 1 and is located on a side of the rack 1 away from the mounting housing 2.
Further, referring to fig. 1, the oil-electric hybrid cooling system 100 for the unmanned aerial vehicle further includes an adjusting bracket 6, where the adjusting bracket 6 is detachably connected to the frame 1, is rotatably connected to the rotor 5, and is located on one side of the frame 1 close to the rotor 5.
In this embodiment, rotatory quantity is four, and installs the top of frame 1 is enclosed and is established a week of installation casing 2, through adjust 6 bottoms of support with the rotation installation of frame 1, thereby change rotor 5 produces the direction of air current, and then makes rotor 5's rotation drives the air flow, thereby it is right drive equipment 3 cools down.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (7)
1. An oil-electricity hybrid power cooling system for an unmanned aerial vehicle is characterized by comprising a rack, a mounting shell, driving equipment and a cooling device;
the mounting shell is fixedly connected with the rack and positioned on one side of the rack, and the driving device is rotatably connected with the mounting shell;
the heat dissipation device comprises a flexible medicine box, an outer heat conduction grid, a sealing cover plate, a first water cooling pipe, a second water cooling pipe and a drainage assembly, the flexible medicine box is detachably connected with the installation shell and is positioned on one side of the installation shell far away from the driving equipment, the outer heat conduction grid is fixedly connected with the installation shell and is positioned on one side of the installation shell close to the flexible medicine box, the outer heat conduction grid is provided with a drainage groove, the drainage groove is positioned on one side of the outer heat conduction grid far away from the installation shell, the sealing cover plate is fixedly connected with the outer heat conduction grid and is covered with the drainage groove and is positioned on one side of the outer heat conduction grid close to the drainage groove, the first water cooling pipe is fixedly connected with the installation shell and is positioned between the flexible medicine box and the outer heat conduction grid, and the second water cooling pipe is fixedly connected with the installation shell, the first water-cooling guide pipe is communicated with the outer heat conduction grid, and the outer heat conduction grid is located on one side, away from the flexible medicine box, of the outer heat conduction grid;
the drainage subassembly includes circulation pipe, diversion joint and water gathering joint, the circulation pipe with installation casing fixed connection, and one end with first water-cooling pipe switch-on, the other end with second water-cooling pipe link up, and is located first water-cooling pipe with between the second water-cooling pipe, the diversion joint with outer heat conduction grid fixed connection, and one side with the drainage groove link up, the opposite side with first water-cooling pipe link up, and is located outer heat conduction grid with between the first water-cooling pipe, one side of gathering water joint with outer heat conduction grid fixed connection, and one side with second water-cooling pipe link up, the opposite side with the drainage groove link up, and is located second water-cooling pipe with between the outer heat conduction grid.
2. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 1,
the heat dissipation device further comprises a medicine box fixing frame, the medicine box fixing frame is fixedly connected with the installation shell, detachably connected with the flexible medicine box and located on one side, close to the flexible medicine box, of the installation shell.
3. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 1,
the driving device comprises a stator and a rotor, wherein the stator is fixedly connected with the mounting shell and is positioned in the mounting shell; the rotor is rotationally connected with the stator and is positioned on one side of the stator, which is far away from the mounting shell.
4. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 3,
the driving equipment further comprises a heat radiation fan, and the heat radiation fan is fixedly connected with the rotor and is positioned at one end, far away from the stator, of the rotor.
5. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 4,
the driving equipment further comprises an air inlet grille and an air supply grille, the air inlet grille is fixedly connected with the mounting shell, penetrates through the mounting shell and is positioned on one side, close to the heat dissipation fan, of the mounting shell; the air supply grille is fixedly connected with the mounting shell, penetrates through the mounting shell and is positioned on one side, far away from the air supply grille, of the mounting shell.
6. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 1,
the oil-electricity hybrid power cooling system for the unmanned aerial vehicle further comprises a rotor, wherein the rotor is connected with the rack in a rotating mode and is located on one side of the installation shell, and the rack is kept away from the rotor.
7. The unmanned aerial vehicle gasoline-electric hybrid cooling system of claim 6,
the oil-electricity hybrid power cooling system for the unmanned aerial vehicle further comprises an adjusting support, the adjusting support is detachably connected with the rack, is connected with the rotor in a rotating mode, and is located the rack is close to one side of the rotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011100985.7A CN112208778A (en) | 2020-10-15 | 2020-10-15 | Oil-electricity hybrid power cooling system for unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011100985.7A CN112208778A (en) | 2020-10-15 | 2020-10-15 | Oil-electricity hybrid power cooling system for unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN112208778A true CN112208778A (en) | 2021-01-12 |
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| CN202011100985.7A Pending CN112208778A (en) | 2020-10-15 | 2020-10-15 | Oil-electricity hybrid power cooling system for unmanned aerial vehicle |
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| CN211167436U (en) * | 2019-12-11 | 2020-08-04 | 福建省惠和城市规划设计有限公司 | Unmanned aerial vehicle engine heat abstractor |
| CN211623597U (en) * | 2019-12-23 | 2020-10-02 | 北京福田康明斯发动机有限公司 | Heating device for engine functional liquid |
| CN112234745A (en) * | 2020-10-09 | 2021-01-15 | 江苏欣弘实业有限公司 | Novel high-efficient automobile-used generator |
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2020
- 2020-10-15 CN CN202011100985.7A patent/CN112208778A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205686617U (en) * | 2016-06-25 | 2016-11-16 | 漯河职业技术学院 | A kind of novel unmanned plane heat abstractor |
| CN107834753A (en) * | 2017-12-15 | 2018-03-23 | 成都千里之行科技有限公司 | A kind of unmanned plane motor waterproof heat-dissipation shell |
| CN211127464U (en) * | 2019-12-03 | 2020-07-28 | 江门市永乐电机有限公司 | Novel water-cooled motor |
| CN211167436U (en) * | 2019-12-11 | 2020-08-04 | 福建省惠和城市规划设计有限公司 | Unmanned aerial vehicle engine heat abstractor |
| CN211623597U (en) * | 2019-12-23 | 2020-10-02 | 北京福田康明斯发动机有限公司 | Heating device for engine functional liquid |
| CN112234745A (en) * | 2020-10-09 | 2021-01-15 | 江苏欣弘实业有限公司 | Novel high-efficient automobile-used generator |
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Application publication date: 20210112 |