CN221214636U - Unmanned aerial vehicle organism assembly and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle organism assembly and unmanned aerial vehicle Download PDFInfo
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- CN221214636U CN221214636U CN202323250045.8U CN202323250045U CN221214636U CN 221214636 U CN221214636 U CN 221214636U CN 202323250045 U CN202323250045 U CN 202323250045U CN 221214636 U CN221214636 U CN 221214636U
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 66
- 230000004308 accommodation Effects 0.000 claims description 4
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- 238000009825 accumulation Methods 0.000 description 6
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- 229910052751 metal Inorganic materials 0.000 description 5
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- 238000001816 cooling Methods 0.000 description 4
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- 239000004033 plastic Substances 0.000 description 4
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 239000004519 grease Substances 0.000 description 3
- 238000001746 injection moulding Methods 0.000 description 3
- 229920001296 polysiloxane Polymers 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
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- 239000004917 carbon fiber Substances 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 235000008331 Pinus X rigitaeda Nutrition 0.000 description 1
- 235000011613 Pinus brutia Nutrition 0.000 description 1
- 241000018646 Pinus brutia Species 0.000 description 1
- 210000001015 abdomen Anatomy 0.000 description 1
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
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- 238000005192 partition Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle body assembly and an unmanned aerial vehicle, wherein the unmanned aerial vehicle body assembly comprises a body assembly, an airborne computer cabin and a heat dissipation assembly; a first circuit board accommodating section is arranged in the machine body assembly; the first circuit board accommodating section is arranged at the bottom of the machine body assembly; the heat dissipation assembly is arranged at the bottom of the machine body assembly; the onboard computer cabin is arranged at the bottom of the heat dissipation assembly; the heat dissipation assembly is provided with an internal air channel, and the internal air channel is provided with an air inlet and an air outlet which are communicated with the outside; the top of the built-in air duct is tightly attached to the first circuit board accommodating section; the bottom of the built-in air duct is tightly attached to the airborne computer cabin. Therefore, the unmanned aerial vehicle body assembly realizes the design of soaking, heat dissipation, drag reduction and modularization.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle body assembly and an unmanned aerial vehicle.
Background
Because the unmanned aerial vehicle needs to carry a large amount of control circuit boards for controlling the flying attitude or the flying speed and the like in the body assembly, the heat dissipation modes of the circuit boards are often considered to a certain extent on a design thought path, and a heat dissipation assembly is arranged to prevent the condition that the unmanned aerial vehicle is out of control and damaged due to overheat of the circuit boards.
At present, the common heat dissipation design of unmanned aerial vehicle in trade has: the unmanned aerial vehicle body assembly is designed to be made of metal.
However, designing a plurality of heat dissipation components requires carrying a plurality of heat dissipation blocks, which causes difficulty in maintenance of the unmanned aerial vehicle, and uneven split heat dissipation easily causes local heat accumulation with high part of heat generation; the arrangement of the whole external radiating block can damage the streamline design of the engine body assembly, so that the wind resistance in the flying process of the unmanned aerial vehicle is large; the unmanned aerial vehicle body assembly is designed to be made of metal, so that the weight of the unmanned aerial vehicle is too high, the flight energy consumption is improved, and the overall heat dissipation efficiency is reduced. In summary, these existing heat dissipation design methods often lead to problems of large wind resistance, low heat dissipation energy efficiency and the like encountered by the unmanned aerial vehicle in the flight process.
Disclosure of utility model
Based on the above, the utility model aims to provide an unmanned aerial vehicle body assembly and an unmanned aerial vehicle, which realize the design of soaking, efficient heat dissipation, drag reduction and modularization.
The aim of the utility model can be achieved by the following technical scheme:
The unmanned aerial vehicle body assembly comprises a body assembly, an onboard computer cabin and a heat dissipation assembly, wherein a first circuit board accommodating section is arranged in the body assembly; the first circuit board accommodating section is arranged at the bottom of the machine body assembly; the heat dissipation assembly is arranged at the bottom of the machine body assembly; the onboard computer cabin is arranged at the bottom of the heat dissipation assembly; the heat dissipation assembly is provided with an internal air channel, the internal air channel is provided with an air inlet and an air outlet which are communicated with the outside, the air inlet is arranged at one end close to the head of the machine body assembly, and the air outlet is arranged at one end close to the tail of the machine body assembly; the top of the built-in air duct is tightly attached to the first circuit board accommodating section; the bottom of the built-in air duct is tightly attached to the airborne computer cabin.
Compared with the prior art, the built-in air duct is arranged, so that the built-in air duct can simultaneously radiate heat of the circuit board in the machine body assembly of the unmanned aerial vehicle and the onboard computer, the number and the weight of radiating blocks to be carried are reduced, and the pneumatic influence on the unmanned aerial vehicle body caused by the fact that the streamline design of the machine body is damaged due to the arrangement of the large radiating blocks is avoided; meanwhile, the heat dissipation assembly is integrally and independently designed and is connected with the engine body assembly, so that the design aims of soaking, heat dissipation, drag reduction and modularization are fulfilled; overall, the unmanned aerial vehicle's of using this unmanned aerial vehicle organism assembly radiating efficiency has been improved, has solved the unmanned aerial vehicle in the prior art in-process windage greatly, the low technical problem of radiating energy efficiency.
Further, the heat dissipation assembly further comprises a first heat dissipation fin; the first radiating fins are arranged on the inner wall of the part, which is tightly attached to the first circuit board accommodating section, of the built-in air duct. Through setting up radiating fin, improve the radiating area in built-in wind channel, improve radiating efficiency.
Further, the airborne computer cabin is provided with an airborne computer accommodating section and a second circuit board accommodating section. The airborne computer cabin is divided into different areas, so that area heat accumulation caused by accumulation of circuit boards is avoided.
Further, the heat dissipation assembly further comprises a second heat dissipation fin and a third heat dissipation fin; the second radiating fins are arranged on the inner wall of the part of the built-in air duct, which is clung to the accommodating section of the airborne computer; the third radiating fins are arranged on the inner wall of the part, which is tightly attached to the second circuit board accommodating section, of the built-in air duct; the bottom of the accommodating section of the airborne computer is provided with a passive radiating fin. Through setting up more radiating fins in built-in wind channel inner wall, improve radiating efficiency when modularization.
Further, an annular accommodating cavity is arranged in the built-in air duct; the heat dissipation assembly comprises a heat dissipation fan with a shape and a size which are matched with those of the annular accommodating cavity, and the heat dissipation fan is fixedly arranged in the annular accommodating cavity. Through setting up radiator fan in built-in wind channel for the circulation of air speed improves radiating efficiency.
Further, be equipped with the third circuit board accommodation interval in the organism subassembly, the top of third circuit board accommodation interval has first opening, unmanned aerial vehicle organism assembly still includes upper cover subassembly, upper cover subassembly lid in the top of organism subassembly covers first opening. More circuit board accommodating sections are designed, so that area heat accumulation caused by circuit board accumulation is avoided.
Further, the body assembly is provided with a battery compartment provided with a Hall sensor for detecting the battery state. Through setting up hall sensor, whether respond to and detect battery installation status and unmanned aerial vehicle flight in-process because of factors such as vibration produce battery pine and take off scheduling problem.
Further, an equipment expansion cabin is arranged in the machine body assembly, and a second opening is formed in the top of the equipment expansion cabin; the unmanned aerial vehicle organism assembly further comprises an upper cover assembly, the upper cover assembly covers the top of the organism assembly, and a third opening corresponding to the second opening is formed in the upper cover assembly. Through designing the equipment expansion cabin, make full use of organism subassembly inner space is used for holding different equipment, increases unmanned aerial vehicle application.
Furthermore, the machine body component is provided with a plurality of quick-release interfaces; the quick release interface comprises at least one of a horn quick release interface, a wing quick release interface and a universal type interface. Through the design quick detach interface, improve unmanned aerial vehicle work efficiency.
The utility model provides an unmanned aerial vehicle, includes airborne computer, horn, wing and unmanned aerial vehicle organism assembly, its characterized in that, airborne computer sets up airborne computer cabin is inside, the horn set up in organism subassembly, the wing set up in organism subassembly.
For a better understanding and implementation, the present utility model is described in detail below with reference to the drawings.
Drawings
FIG. 1 is an exploded view of the unmanned aerial vehicle body assembly of the present utility model;
fig. 2 is a schematic structural view of a body assembly of the unmanned aerial vehicle body assembly of the present utility model;
fig. 3 is a schematic structural view of a heat dissipating component of an unmanned aerial vehicle body assembly according to the present utility model;
Fig. 4 is a schematic position diagram of a first heat dissipating fin and a third heat dissipating fin of a heat dissipating component of an unmanned aerial vehicle body assembly according to the present utility model;
fig. 5 is a schematic structural view of an onboard computer cabin of the unmanned aerial vehicle body assembly of the present utility model;
fig. 6 is a cross-sectional view of the unmanned aerial vehicle body assembly of the present utility model.
Detailed Description
Example 1
As shown in fig. 1 and 6, the present embodiment provides an unmanned aerial vehicle body assembly and an unmanned aerial vehicle. The unmanned aerial vehicle includes airborne computer, horn, wing and unmanned aerial vehicle organism assembly, airborne computer sets up the inside of unmanned aerial vehicle organism assembly, the horn set up in unmanned aerial vehicle organism assembly, the wing set up in unmanned aerial vehicle organism assembly. Specifically, the unmanned aerial vehicle body assembly comprises a body assembly 100, a heat dissipation assembly 300 arranged at the bottom of the body assembly 100, and an onboard computer cabin 400 arranged at the bottom of the heat dissipation assembly 300. In this embodiment, the body assembly 100 has a shuttle shape as a whole to reduce the aerodynamic influence. This unmanned aerial vehicle organism assembly can avoid influencing unmanned aerial vehicle's streamlined structure and increase the windage, can improve unmanned aerial vehicle's heat dissipation efficiency simultaneously, has taken into account soaking, heat dissipation, drag reduction and modular design purpose promptly.
As shown in fig. 2 and 6, the body assembly 100 is used for carrying a control circuit board for controlling the flying attitude or the flying speed of the unmanned aerial vehicle, other related devices and other components. In this embodiment, the body assembly 100 may be made of plastic material (such as nylon and glass fiber or nylon and carbon fiber, etc.), and is integrally formed by injection molding. Of course, in other alternative embodiments, the body assembly 100 may be made of a composite material such as carbon fiber.
As shown in fig. 6, the body assembly 100 is configured to house a circuit board and a battery, and to connect with an external device, etc., and has a shuttle structure. The body assembly 100 is provided with a first circuit board accommodating section 101 and a third circuit board accommodating section 102, and in some embodiments, the first circuit board accommodating section 101 and the third circuit board accommodating section 102 may be formed by insulating spacers at intervals, or may be formed by increasing the interval distance between circuit boards so as to use the insulation of air. The first circuit board accommodating section 101 is disposed at the bottom of the body assembly 100, and the third circuit board accommodating section 102 is disposed at the top of the body assembly 100. In this embodiment, the circuit board with smaller heat productivity of the displacement portion is adopted to the third circuit board accommodating section 102, so as to avoid the heat accumulation phenomenon in the area formed by stacking the circuit boards, and further influence the heat dissipation effect.
Meanwhile, the body assembly 100 is provided with a battery compartment 104, the battery compartment 104 is provided with a hall sensor for detecting the battery state, in this embodiment, the battery compartment 104 is adapted to the battery in shape and size and is disposed on the abdomen of the body assembly 100, in some embodiments, the battery compartment 104 may be disposed on other parts of the body assembly 100, and the shape and size of the battery compartment is not limited; in other alternative embodiments, the battery compartment 104 may also be provided with a circuit detection loop for detecting whether the drone is in a pass-through state to obtain a battery state. The machine body assembly 100 is internally provided with an equipment expansion cabin 105, the top of the equipment expansion cabin 105 is provided with a second opening 106, in this embodiment, the equipment expansion cabin 105 is approximately in a cube shape and is used for accommodating other unmanned aerial vehicle assemblies (such as parachute assemblies and the like), so that the space utilization rate of the machine body assembly 100 is improved, and in other alternative embodiments, the equipment expansion cabin 105 can be in any other shape.
In addition, the body assembly 100 is provided with a plurality of expansion interfaces 107 and equipment mounting points 108; the device mounting points 108 are symmetrically disposed on two sides of the body assembly 100, in some embodiments, the expansion interface 107 is an interface for connecting various external devices by an unmanned aerial vehicle, the device mounting points 108 are used for mounting various external devices (such as cameras, etc.), the device mounting points 108 can be symmetrically disposed on two sides of the body assembly 100, and can also be symmetrically disposed on two sides of the body assembly 100, and the symmetrical arrangement is used for maintaining overall balance of the unmanned aerial vehicle and avoiding out of control of the flight attitude. The machine body assembly 100 is provided with a plurality of quick-release interfaces 109; the quick release interface 109 includes at least one of a horn quick release interface, a wing quick release interface, and a universal interface. The horn quick detach interface is used for installing the horn, the wing quick detach interface is used for installing the wing, general type interface can be used for installing horn or wing. In this embodiment, the quick-release interfaces of the arm, the wing and the universal type are different quick-release interfaces, and the quick-release interfaces 109 are symmetrically disposed on both sides of the body assembly 100 to maintain the overall balance of the unmanned aerial vehicle, and in other alternative embodiments, the body assembly 100 may be provided with only the universal type interfaces.
As shown in fig. 5 and 6, the onboard computer nacelle 400 is used for mounting an onboard computer, other related circuit boards, and the like. Also, in this embodiment, the onboard computer nacelle 400 may be made of plastic material (such as PC, etc.), and is integrally formed by injection molding. Of course, in other alternative embodiments, the onboard computer nacelle 400 may also be made of a material such as metal.
As shown in fig. 5, the on-board computer room 400 is a housing for housing an on-board computer, a circuit board, and the like. In this embodiment, the on-board computer nacelle 400 is provided with an on-board computer accommodating section 401 and a second circuit board accommodating section 402, and the on-board computer accommodating section 401 and the second circuit board accommodating section 402 may be formed by an insulating partition, or may be provided by increasing the distance between circuit boards so as to use the insulation of air. In this embodiment, a passive heat sink 403 is disposed at the bottom of the accommodating section 401 of the onboard computer, and the passive heat sink 403 is used to further increase the heat dissipation area to improve the heat dissipation efficiency, and in some embodiments, the passive heat sink 403 is connected to the bottom of the accommodating section 401 of the onboard computer through heat-conducting silicone grease. The tail of the onboard computer cabin 400 is provided with a power transmission line 404 connected to an onboard computer arranged in the onboard computer cabin 400, and the other end of the power transmission line 404 is connected to a battery arranged in the battery compartment 104 through the engine body assembly 100. The on-board computer room 400 is further provided with a connection structure for connecting to the bottom of the heat dissipating assembly 300, in this embodiment, the connection structure uses screws and corresponding studs, and in other alternative embodiments, a snap-fit structure may be used.
As shown in fig. 3 and 6, the heat dissipation assembly 300 is configured to implement a heat dissipation function, and to soak and dissipate heat of the whole unmanned aerial vehicle body assembly. In this embodiment, the heat dissipation assembly 300 is mainly made of magnesium aluminum alloy. Of course, in other alternative embodiments, the heat dissipating assembly 300 may be made of plastic, other metal, or the like, or the heat dissipating assembly 300 may be formed by connecting the top and bottom walls of other assemblies.
As shown in fig. 1, the heat dissipating assembly 300 is mounted between the body assembly 100 and the onboard computer nacelle 400. The heat dissipation assembly 300 is disposed at the bottom of the body assembly 100 and is connected to the body assembly 100 by screws in this embodiment, and in other alternative embodiments, a viscous silicone grease with good heat conductivity may be used for connection. The heat dissipation assembly 300 is provided with a built-in air duct 301, the built-in air duct 301 is provided with an air inlet 302 and an air outlet 303 which are communicated with the outside, the air inlet 302 is arranged at one end of the built-in air duct 301 close to the head of the machine body assembly 100, and the air outlet 303 is arranged at one end of the built-in air duct 301 close to the tail of the machine body assembly 100; the top of the built-in air duct 301 is tightly attached to the first circuit board accommodating section 101; the bottom of the built-in air duct 301 is tightly attached to the onboard computer cabin 400, and in some preferred embodiments, the tightly attached portions are all provided with heat-conductive silicone grease.
As shown in fig. 3 and 4, the heat dissipating assembly 300 further includes a first heat dissipating fin 304; the first heat dissipation fins 304 are disposed on the inner wall of the portion of the built-in air duct 301 that is tightly attached to the first circuit board accommodating section 101, and in this embodiment, the heat dissipation fins are comb-shaped and are formed by a plurality of parallel tooth-shaped structures, so as to increase the heat dissipation area. Further, the heat dissipating assembly 300 may further include a second heat dissipating fin 305 and a third heat dissipating fin 306; the second heat dissipation fins 305 are disposed on the inner wall of the portion of the built-in air duct 301 that is tightly attached to the accommodating section 401 of the onboard computer; the third heat dissipation fins 306 are disposed on the inner wall of the portion of the built-in air duct 301 that is tightly attached to the second circuit board accommodating section 402, in this embodiment, for two circuit board stacking areas where heat is easily accumulated by the unmanned aerial vehicle, more heat dissipation fins are adopted, so as to further improve efficiency, and in other alternative embodiments, more heat pipes may be adopted to improve heat dissipation efficiency.
Referring to fig. 3, in some preferred embodiments, an annular accommodating cavity 307 is provided in the internal air duct 301, and the heat dissipating assembly 300 includes a heat dissipating fan 308 having a shape and size corresponding to the annular accommodating cavity 307, and the heat dissipating fan 308 is fixedly disposed in the annular accommodating cavity 307. Therefore, the air circulation rate is quickened, and the heat dissipation efficiency is improved. In other alternative embodiments, a larger built-in air duct 301 may be provided in the heat dissipating assembly 300 for increasing the air flow rate and heat dissipating efficiency.
The working principle of the unmanned aerial vehicle body assembly applied in the unmanned aerial vehicle is as follows: when the unmanned aerial vehicle with the unmanned aerial vehicle body assembly is used for carrying out a flight task, wind can be blown in (sucked by the cooling fan 308) from the air inlet 302 of the built-in air duct 301, heat accumulated on the first cooling fin 304, the second cooling fin 305 and the third cooling fin 306 is taken away, and then the wind is blown out from the air outlet 303, so that soaking and heat dissipation are carried out while wind resistance in the unmanned aerial vehicle flight is not influenced.
Example 2
The unmanned aerial vehicle body assembly and the unmanned aerial vehicle of the embodiment 2 have basically the same structure as the embodiment 1, and only the difference is in the structure of the unmanned aerial vehicle body assembly. The unmanned aerial vehicle body assembly comprises a body assembly 100, a heat dissipation assembly 300 arranged at the bottom of the body assembly 100, an onboard computer cabin 400 arranged at the bottom of the heat dissipation assembly 300, and an upper cover assembly 200 covered on the top of the body assembly 100.
As shown in fig. 1, the upper cover assembly 200 is used to cover the top of the body assembly 100. Also, in the present embodiment, the upper cover assembly 200 may be made of plastic material (such as PC, etc.), and is integrally formed by injection molding. Of course, in other alternative embodiments, the cover assembly 200 may be made of metal or the like.
As shown in fig. 1, the cover assembly 200 is a fitting member fitted to the body assembly 100, and has a shape and size adapted to the shape of the top of the body assembly 100. The edge of the upper cover assembly 200 is provided with an assembly structure adapted to the top of the body assembly 100, and the upper cover assembly 200 may be covered and coupled to the top of the body assembly 100 by the assembly structure. In this embodiment, the top of the third circuit board accommodating section 102 has a first opening 103, and the upper cover assembly 200 covers the top of the body assembly 100, so as to cover the first opening 103 of the third circuit board accommodating section 102, thereby improving the safety performance. The upper cover assembly 200 is provided with a third opening 201 corresponding to the second opening 106 of the equipment expansion cabin 105, and in some embodiments, the upper cover assembly 200 is provided with a cover blocking structure (such as a buckle, etc.) capable of switching between an open state and a closed state at the third opening 201, where the cover blocking structure is used for opening or covering the second opening 106.
Since the operation principle of embodiment 2 is the same as that of embodiment 1, the description thereof will be omitted.
Compared with the prior art, the built-in air duct is arranged, so that the built-in air duct can simultaneously radiate heat of the circuit board in the machine body assembly of the unmanned aerial vehicle and the onboard computer, the number and the weight of radiating blocks to be carried are reduced, and the pneumatic influence on the unmanned aerial vehicle body caused by the fact that the streamline design of the machine body is damaged due to the arrangement of the large radiating blocks is avoided; meanwhile, the heat dissipation assembly is integrally and independently designed and is connected with the engine body assembly, so that the design aims of soaking, heat dissipation, drag reduction and modularization are fulfilled; overall, the unmanned aerial vehicle's of using this unmanned aerial vehicle organism assembly radiating efficiency has been improved, has solved the unmanned aerial vehicle in the prior art in-process windage greatly, the low technical problem of radiating energy efficiency.
The above examples illustrate only a few embodiments of the utility model, which are described in detail and are not to be construed as limiting the scope of the utility model. It should be noted that modifications and improvements can be made by those skilled in the art without departing from the spirit of the utility model, and the utility model is intended to encompass such modifications and improvements.
Claims (10)
1. The unmanned aerial vehicle body assembly comprises a body assembly, an onboard computer cabin and a heat dissipation assembly, and is characterized in that a first circuit board accommodating section is arranged in the body assembly; the first circuit board accommodating section is arranged at the bottom of the machine body assembly; the heat dissipation assembly is arranged at the bottom of the machine body assembly; the onboard computer cabin is arranged at the bottom of the heat dissipation assembly; the heat dissipation assembly is provided with an internal air channel, the internal air channel is provided with an air inlet and an air outlet which are communicated with the outside, the air inlet is arranged at one end close to the head of the machine body assembly, and the air outlet is arranged at one end close to the tail of the machine body assembly; the top of the built-in air duct is tightly attached to the first circuit board accommodating section; the bottom of the built-in air duct is tightly attached to the airborne computer cabin.
2. The unmanned aerial vehicle body assembly of claim 1, wherein: the heat dissipation assembly further comprises a first heat dissipation fin; the first radiating fins are arranged on the inner wall of the part, which is tightly attached to the first circuit board accommodating section, of the built-in air duct.
3. The unmanned aerial vehicle body assembly of claim 1, wherein: the airborne computer cabin is provided with an airborne computer accommodating section and a second circuit board accommodating section.
4. The unmanned aerial vehicle body assembly of claim 3, wherein: the heat dissipation assembly further comprises a second heat dissipation fin and a third heat dissipation fin; the second radiating fins are arranged on the inner wall of the part of the built-in air duct, which is clung to the accommodating section of the airborne computer; the third radiating fins are arranged on the inner wall of the part, which is tightly attached to the second circuit board accommodating section, of the built-in air duct; the bottom of the accommodating section of the airborne computer is provided with a passive radiating fin.
5. The unmanned aerial vehicle body assembly of any of claims 1-4, wherein: an annular accommodating cavity is arranged in the built-in air duct; the heat dissipation assembly comprises a heat dissipation fan with a shape and a size which are matched with those of the annular accommodating cavity, and the heat dissipation fan is fixedly arranged in the annular accommodating cavity.
6. The unmanned aerial vehicle body assembly of any of claims 1-4, wherein: be equipped with the third circuit board accommodation interval in the organism subassembly, the top of third circuit board accommodation interval has first opening, unmanned aerial vehicle organism assembly still includes upper cover subassembly, upper cover subassembly lid in the top of organism subassembly covers first opening.
7. The unmanned aerial vehicle body assembly of any of claims 1-4, wherein: the machine body assembly is provided with a battery compartment, and the battery compartment is provided with a Hall sensor for detecting the state of the battery.
8. The unmanned aerial vehicle body assembly of any of claims 1-4, wherein: an equipment expansion cabin is arranged in the machine body assembly, and the top of the equipment expansion cabin is provided with a second opening; the unmanned aerial vehicle organism assembly further comprises an upper cover assembly, the upper cover assembly covers the top of the organism assembly, and a third opening corresponding to the second opening is formed in the upper cover assembly.
9. The unmanned aerial vehicle body assembly of any of claims 1-4, wherein: the machine body component is provided with a plurality of quick-release interfaces; the quick release interface comprises at least one of a horn quick release interface, a wing quick release interface and a universal type interface.
10. An unmanned aerial vehicle comprising an on-board computer, a horn, a wing and an unmanned aerial vehicle body assembly as claimed in any of claims 1 to 9, wherein the on-board computer is provided inside the on-board computer nacelle, the horn is provided in the body assembly, and the wing is provided in the body assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323250045.8U CN221214636U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle organism assembly and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323250045.8U CN221214636U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle organism assembly and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221214636U true CN221214636U (en) | 2024-06-25 |
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ID=91577091
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323250045.8U Active CN221214636U (en) | 2023-11-29 | 2023-11-29 | Unmanned aerial vehicle organism assembly and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
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| CN (1) | CN221214636U (en) |
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2023
- 2023-11-29 CN CN202323250045.8U patent/CN221214636U/en active Active
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