Unmanned aerial vehicle convenient to disassemble

Abstract

An unmanned aerial vehicle convenient to disassemble comprises an unmanned aerial vehicle shell, an unmanned aerial vehicle supporting structure used for supporting the whole unmanned aerial vehicle and an unmanned aerial vehicle flying structure used for flying of the unmanned aerial vehicle, the unmanned aerial vehicle shell is connected to the unmanned aerial vehicle supporting structure, and the unmanned aerial vehicle flying structure is connected to the outer side of the unmanned aerial vehicle supporting structure relative to the unmanned aerial vehicle shell for driving; the unmanned aerial vehicle supporting structure is provided with a first unmanned aerial vehicle supporting seat for connecting an unmanned aerial vehicle shell and a second unmanned aerial vehicle supporting seat for connecting an unmanned aerial vehicle flight structure, the second unmanned aerial vehicle supporting seat is provided with a second connecting mounting position, and the first unmanned aerial vehicle supporting seat is provided with a first connecting mounting position; the second connecting mounting position is connected to the first connecting mounting position, so that the second unmanned aerial vehicle supporting seat is detachably connected to the first unmanned aerial vehicle supporting seat. According to the scheme, the structural design of split assembly of the unmanned aerial vehicle body is adopted, and the effects of effectively shortening the production time of the unmanned aerial vehicle body, improving the production efficiency of the unmanned aerial vehicle and expanding the selection diversity of production materials of the second unmanned aerial vehicle supporting seat are achieved.

Description

Technical Field

[0001] This utility model belongs to the technical field of unmanned aerial vehicles (UAVs), and in particular relates to an unmanned aerial vehicle that is easy to disassemble. Background Technology

[0002] In the prior art, 3D printing technology is mostly used to produce drones of specific shapes. However, 3D printing technology has low production efficiency, which makes it difficult to mass-produce drones. Therefore, this utility model proposes a new solution to the above-mentioned technical problems. Utility Model Content

[0003] The purpose of this utility model is to provide a drone that is easy to disassemble. It adopts a structural design for the drone body to be assembled in separate parts, which effectively shortens the production time of the drone body, improves the production efficiency of the drone, and expands the variety of materials to be selected for the production of the second drone support.

[0004] Based on this, the present invention provides an easily disassembled drone, comprising:

[0005] The drone shell, the drone support structure for supporting the entire drone, and the drone flight structure for drone flight, wherein the drone shell is connected to the drone support structure, and the drone flight structure is connected to the outside of the drone support structure relative to the drone shell and is driven.

[0006] The drone support structure includes a first drone support base for connecting to the drone shell and a second drone support base for connecting to the drone flight structure. The second drone support base has a second connection mounting position, and the first drone support base has a first connection mounting position. The second connection mounting position is connected to the first connection mounting position, so that the second drone support base can be detachably connected to the first drone support base.

[0007] As described above, a drone that is easy to disassemble has a first drone support plate 1 and a second drone support plate 2. The first drone support plate 1 and the second drone support plate 2 are arranged opposite to each other to form the first connection mounting position for connection to the second connection mounting position.

[0008] As described above, the second drone support base is provided with a second drone support base one and a second drone support base two. The second drone support base one and the second drone support base two are connected to each other at the first connection mounting position for fastening.

[0009] As described above, in a type of drone that is easy to disassemble, the second drone support base one and the second drone support base two are respectively provided with a second drone support base mounting position one and a second drone support base mounting position two. The second drone support base mounting position one and the second drone support base mounting position two are connected to the first connection mounting position to form the second connection mounting position.

[0010] As described above, in a type of easily disassembled drone, the second drone support base one and the second drone support base two are respectively provided with flight structure mounting position one and flight structure mounting position two. The flight structure mounting position one is located at the other end of the second drone support base one, and the flight structure mounting position two is located at the other end of the second drone support base two, and the drone flight structure is connected to the flight structure mounting position one or the flight structure mounting position two for fastening.

[0011] As described above, the drone support structure is further provided with a first support and stabilization structure and a second support and stabilization structure. The second drone support base one and the second drone support base two are further provided with a support and stabilization mounting part one and a support and stabilization mounting part two, respectively. The first support and stabilization structure and the second support and stabilization structure are respectively connected to the support and stabilization mounting part one and the support and stabilization mounting part two to support the drone.

[0012] As described above, in a type of easily disassembled drone, the first support and stabilization structure is provided with a first support limiting slot and a first support stabilization protrusion. The first support limiting slot is provided with a first support limiting block, and the first support stabilization mounting part is provided with a first support stabilization connection hole. The first support and stabilization structure is connected to the first support limiting block through the first support stabilization connection hole, and then connected to the first support limiting slot and supported by the first support limiting block.

[0013] The second support and stabilizing structure is provided with a second support limiting slot and a second support stabilizing protrusion. The second support limiting slot is provided with a second support limiting block. The second support stabilizing mounting part is provided with a second support stabilizing connecting hole. The second support and stabilizing structure is connected to the second support limiting block through the second support stabilizing connecting hole, and then connected to the second support limiting slot and supported by the second support stabilizing protrusion.

[0014] As described above, the easily detachable drone further includes a main control module for controlling the drone's flight. The drone shell is connected to the first drone support plate 2 and forms a control structure mounting cavity. The first drone support plate 1 is disposed within the control structure mounting cavity. The main control module is connected to the first drone support plate 1 and provides electrical connection to the drone flight structure.

[0015] The aforementioned detachable drone also includes a waterproof layer, which is provided on the main control module and the drone's flight structure for waterproofing.

[0016] As described above, the second drone support base is also provided with connecting support components. The second drone support base one and the second drone support base two are integrally formed structural designs, and multiple connecting support components are respectively connected to the second drone support base one and the second drone support base two for support.

[0017] Implementing the embodiments of this utility model has the following beneficial effects:

[0018] 1. This solution adopts a modular assembly structure for the drone fuselage, comprising a drone shell, a drone support base, and a drone flight structure. The drone support base includes a first drone support base and a second drone support base, each with a first and a second connection mounting position. The second drone support base is detachably connected to the first drone support base via the second connection mounting position. By connecting the drone shell to the first drone support base and the drone flight structure to the second drone support base relative to the second connection mounting position, modular assembly of the drone fuselage is achieved. Furthermore, the second drone support base can be manufactured separately using injection molding and then assembled onto the second drone support base. This effectively optimizes the drone production process, shortening the drone fuselage production time, improving drone production efficiency, and expanding the variety of materials available for the second drone support base. Attached Figure Description

[0019] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1 This is a schematic diagram of the structure of an embodiment of the present utility model;

[0021] Figure 2 For the corresponding Figure 1 A structural diagram from another direction;

[0022] Figure 3 For the corresponding Figure 2 A structural diagram from another direction;

[0023] Figure 4 For the corresponding Figure 3 A structural diagram from another direction;

[0024] Figure 5 This is an exploded view of the structure of an embodiment of the present utility model;

[0025] Figure 6 For the corresponding Figure 5 A structural diagram from another direction;

[0026] Figure 7 For the corresponding Figure 6 A structural diagram from another direction;

[0027] Figure 8 For the corresponding Figure 7 A structural diagram from another direction;

[0028] Figure 9 A schematic diagram showing the connection between the first and second support stabilizing structures and the second UAV support base;

[0029] Figure 10 For the corresponding Figure 9 Exploded view of the structure;

[0030] Figure 11 For the corresponding Figure 10 A schematic diagram of the structure from another direction.

[0031] In the diagram: 1-UAV shell, 11-UAV side panel, 12-GPS mounting position; 2-UAV support structure, 21-First UAV support base, 211-First connection mounting position, 212-First UAV support plate one, 213-First UAV support plate two, 22-Second UAV support base, 221-Second connection mounting position, 222-Second UAV support base one, 2221-Second UAV support base mounting position one, 2222-Flight structure mounting position one, 2223-Support and stabilization mounting part one, 22231-Support and stabilization connection hole one, 2224-Second UAV support base connection groove one, 223-Second UAV support base 2. 2231 - Second UAV support mounting position 2; 2232 - Flight structure mounting position 2; 2233 - Support and stabilization mounting part 2; 22331 - Support and stabilization connection hole 2; 2234 - Second UAV support connecting groove 2; 226 - Connecting support component; 23 - First support and stabilization structure; 231 - First support limiting slot; 2311 - First support limiting block; 232 - First support and stabilization protrusion; 24 - Second support and stabilization structure; 241 - Second support limiting slot; 2411 - Second support limiting block; 242 - Second support and stabilization protrusion; 3 - UAV flight structure; 31 - Flight structure connecting seat; 4 - Main control module. Detailed Implementation

[0032] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0033] like Figures 1 to 11 As shown, this utility model embodiment provides an easily disassembled drone, comprising:

[0034] The system comprises a drone shell 1, a drone support structure 2 for supporting the entire drone, and a drone flight structure 3 for drone flight. The drone shell 1 is connected to the drone support structure 2, and the drone flight structure 3 is connected to the outside of the drone support structure 2 relative to the drone shell 1, so as to provide sufficient lift and drop power to drive the drone. The drone support structure 2 has a first drone support base 21 for connecting the drone shell 1 and a second drone support base 22 for connecting the drone flight structure 3. The second drone support base 22 has a second connection mounting position 221, and the first drone support base 21 has a first connection mounting position 211. The second connection mounting position 221 is connected to the first connection mounting position 211, so that the second drone support base 22 can be detachably connected to the first drone support base 21 to improve the convenience of installation.

[0035] Specifically, the first UAV support base 21 is provided with a first UAV support plate 212 and a second UAV support plate 213. The first UAV support plate 212 and the second UAV support plate 213 are arranged opposite to each other to form the first connection mounting position 211 for connection with the second connection mounting position 221. The relative arrangement of the first UAV support plate 212 and the second UAV support plate 213 forms a precisely matched installation space between them, and the installation space is adapted to the shape and size of the second connection mounting position 221, thereby achieving a fast and accurate connection, effectively improving the efficiency and accuracy of UAV assembly, and reducing possible errors during the installation process.

[0036] Furthermore, the second drone support 22 is provided with a second drone support 1 222 and a second drone support 223. The second drone support 1 222 and the second drone support 223 are connected to each other at the first connection mounting position 211 for fastening. In this embodiment of the present invention, the second drone support 1 222 and the second drone support 223 are produced by injection molding. Preferably, each side of the drone is provided with one second drone support 1 222 and one second drone support 223. The two second drone support 1 222 are diagonally connected at the first connection mounting positions 211 on both sides, and the two second drone support 223 are diagonally connected at the first connection mounting positions 211 on both sides, so as to improve the stability of the drone during flight and improve the production convenience of the second drone support 1 222 and the second drone support 223.

[0037] Furthermore, the second UAV support base 1 222 and the second UAV support base 223 are respectively provided with second UAV support base mounting positions 1 2221 and 2231. The second UAV support base mounting positions 1 2221 and 2231 are connected to the first connecting mounting position 211 to form the second connecting mounting position 221. The second UAV support base mounting position 1 2221 is provided with a second UAV support base connecting half hole 1, and the second UAV support base mounting position 2231 is provided with a second UAV support base connecting half hole 2. The second UAV support base connecting half hole 1 and the second UAV support base connecting half hole 2 are connected to form a complete second UAV support base connecting hole 1, so that the second UAV support base 1 222 and the second UAV support base 223 can be connected through the second UAV support base connecting hole 1, improving the installation positioning accuracy and facilitating the fastening of the second UAV support base 22 to the first UAV support base 21 through the second connecting mounting position 221, thereby enhancing the stability after connection.

[0038] Furthermore, the second UAV support base 1 222 and the second UAV support base 223 are respectively provided with flight structure mounting positions 1 2222 and 2232. The flight structure mounting position 1 2222 is located at the other end of the second UAV support base 1 222, opposite to the second UAV support base mounting position 1 2221. The flight structure mounting position 2232 is located at the other end of the second UAV support base 223, opposite to the second UAV support base mounting position 2231. The UAV flight structure 3 is fastened to the flight structure mounting position 1 2222 or the flight structure mounting position 2232. This design allows the UAV flight structure 3 to be secured via the flight structure mounting positions 1 2222 and 2232. The drone flight structure 3 is securely connected to the second drone support 22, thereby stably mounting the drone flight structure 3 on the drone support 2, ensuring power transmission and control precision during flight, and improving flight stability and reliability. The flight structure mounting position 2222 is provided with a first flight structure connection hole and a second flight structure connection hole, with the second flight structure connection hole equidistantly surrounding the first flight structure connection hole. The drone flight structure 3 is provided with a flight structure connection seat 31, which has flight structure mating holes corresponding to the second flight structure connection holes, so as to secure the drone flight structure 3 to the flight structure mounting position 2222 through a first threaded connector, thereby improving the tightness of the connection of the drone flight structure 3.

[0039] The second flight structure mounting position 2232 is provided with a third flight structure connection hole and a fourth flight structure connection hole. The fourth flight structure connection hole is equidistantly arranged around the third flight structure connection hole, and the four flight structure connection holes correspond one-to-one with the flight structure mating holes, so as to fasten the UAV flight structure 3 to the second flight structure mounting position 2232 through the second threaded connector, thereby improving the tightness of the connection of the UAV flight structure 3.

[0040] Furthermore, the UAV support structure 2 is also provided with a first support stabilization structure 23 and a second support stabilization structure 24. The second UAV support base 1 222 and the second UAV support base 223 are also provided with a first support stabilization mounting part 2223 and a second support stabilization mounting part 2233. The first support stabilization structure 23 and the second support stabilization structure 24 are respectively connected to the first support stabilization mounting part 2223 and the second support stabilization mounting part 2233 to support the UAV, so as to ensure that the UAV can be stably docked on the ground after the flight, avoiding damage to the UAV by direct docking and improving the safety of UAV docking. At the same time, it ensures the levelness of the second UAV support base 1 222 and the second UAV support base 223 after connection, so as to reduce wear on the connection of the second UAV support base 1 222 and the second UAV support base 223, thereby extending the service life of the UAV.

[0041] Furthermore, the first support and stabilizing structure 23 is provided with a first support limiting groove 231 and a first support and stabilizing protrusion 232. The first support limiting groove 231 is provided with a first support limiting block 2311, and the support and stabilizing mounting part 2223 is provided with a support and stabilizing connecting hole 22231. The first support and stabilizing structure 23 is connected to the first support limiting block 2311 through the support and stabilizing connecting hole 22231, and then connected within the first support limiting groove 231 and supported by the first support limiting block 2311. This provides double limiting for the first support and stabilizing structure 23 through the first support limiting groove 231 and the first support limiting block 2311, thereby ensuring that the grounding stability of the first support and stabilizing structure 23 is enhanced when the first support and stabilizing protrusion 232 abuts against the ground. The contact area between the first support and stabilizing protrusion 232 and the ground is designed as a plane to increase the contact area between the first support and stabilizing protrusion 232 and the ground, thereby enhancing the grounding stability of the first support and stabilizing structure 23.

[0042] The second support and stabilizing structure 24 is provided with a second support limiting groove 241 and a second support and stabilizing protrusion 242. The second support limiting groove 241 is provided with a second support limiting block 2411. The second support and stabilizing mounting part 2233 is provided with a second support and stabilizing connecting hole 22331. The second support and stabilizing structure 24 is connected to the second support limiting block 2411 through the second support and stabilizing connecting hole 22331, and then connected in the second support limiting groove 241. It is supported by the second support and stabilizing protrusion 242, so that the second support and stabilizing structure 24 is doubly limited by the second support limiting groove 241 and the second support limiting block 2411, thereby ensuring that the second support and stabilizing protrusion 242 abuts the ground, thus enhancing the grounding stability of the second support and stabilizing structure 24. The contact area between the second support and stabilizing protrusion 242 and the ground is designed as a plane to increase the contact area between the second support and stabilizing protrusion 242 and the ground, thereby enhancing the grounding stability of the second support and stabilizing structure 24.

[0043] Furthermore, the present invention provides a detachable drone, which also includes a main control module 4 for controlling the drone's flight. The drone shell 1 is connected to the first drone support plate 213 and forms a control structure mounting cavity. The first drone support plate 212 is disposed within the control structure mounting cavity. The second drone support base 222 and the second drone support base 223 are also provided with a second drone support base connecting groove 2224 and a second drone support base connecting groove 2234, which are respectively connected to the first flight structure connecting hole and the third flight structure connecting hole. The main control module 4 is connected to the first UAV support plate 212. The UAV flight structure 3, which is set in the second UAV support base 222 and the second UAV support base 223, is connected to the main control module 4 through connecting lines installed in the second UAV support base connecting cable grooves 2224 and 2234, respectively. The main control module 4 controls the rotation of the UAV flight structure 3, thereby driving the UAV to fly. This design, with the connecting lines installed in the second UAV support base connecting cable grooves 2224 and 2234, effectively improves the stability and safety of the UAV during operation.

[0044] Furthermore, the detachable drone provided in this embodiment of the present invention also includes a Parylene waterproof layer for waterproofing. The Parylene waterproof layer is disposed on the main control module 4 and the drone flight structure 3 for waterproofing. In this embodiment, the Parylene waterproof layer is vacuum-coated using Parylene coating technology, an advanced process that utilizes parylene as a coating material. The Parylene coating is deposited on the surface of an object via chemical vapor deposition, specifically through three steps: vaporization, pyrolysis, and polymerization. First, the Parylene raw material is vaporized at 150°C, and then pyrolyzed into monomers at 650°C. Finally, the coating is uniformly deposited onto the surface of the object at room temperature using vapor deposition. The entire Parylene coating process must be carried out under vacuum conditions to ensure that the coating is uniform and without dead corners, covering all parts of the object to be coated, including sharp edges, gaps, and extremely fine pinholes. This provides waterproof, moisture-proof, dustproof, and insulating protection for electronic components, thereby improving the reliability and lifespan of electronic products. In this embodiment of the invention, the main control module 4, the UAV flight structure 3, and the connecting lines are coated with a nano- to micron-sized Parylene waterproof layer using Parylene coating technology to enhance the applicability to different UAV models, thereby improving the overall waterproof performance of the UAV and extending its lifespan.

[0045] Furthermore, the second drone support base 22 is also provided with connecting support members 226, and the second drone support base one 222 and the second drone support base two 223 are integrally molded to improve the convenience of injection molding production of the second drone support base one 222 and the second drone support base two 223; multiple connecting support members 226 are respectively connected to the second drone support base one 222 and the second drone support base two 223 for support, so as to avoid damage to the second drone support base one 222 and the second drone support base two 223 due to excessive local stress, thereby extending the service life of the second drone support base one 222 and the second drone support base two 223; in this embodiment of the present invention, the connecting support members 226 are connected to the second drone support base one 222 and the second drone support base two 223 by glue connection to improve the convenience of connection.

[0046] In this embodiment of the utility model, the drone shell 1 is provided with a drone side panel 11 and a GPS mounting position 12. The drone side panel 11 adopts a laser engraving light-transmitting process, which can enhance the aesthetics and technological feel of the drone, thereby enhancing the market competitiveness of the drone. The GPS mounting position 12 is used to install a GPS. The GPS is electrically connected to the main control module 4 and is coated with a nano- to micron-level waterproof layer. The origin information can be preset through the main control module 4, so that the drone can automatically return to home through GPS positioning in case of an accident, thereby reducing losses.

[0047] It should be understood that the terms "first," "second," etc., are used in this utility model to describe various information, but this information should not be limited to these terms. These terms are only used to distinguish information of the same type from each other. For example, without departing from the scope of this utility model, "first" information can also be referred to as "second" information, and similarly, "second" information can also be referred to as "first" information. In addition, the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0048] The above description is the preferred embodiment of this utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the principle of this utility model, and these improvements and modifications are also considered to be within the protection scope of this utility model.

Claims

1. A drone that is easy to disassemble, characterized by, The utility model relates to a kind of unmanned aerial vehicle, including: Unmanned aerial vehicle shell (1), unmanned aerial vehicle support structure (2) for unmanned aerial vehicle whole machine support, unmanned aerial vehicle flight structure (3) for unmanned aerial vehicle flight, the unmanned aerial vehicle shell (1) is connected in the unmanned aerial vehicle support structure (2), the unmanned aerial vehicle flight structure (3) is connected in the unmanned aerial vehicle support structure (2) outside relative to the unmanned aerial vehicle shell (1) and is driven; The unmanned aerial vehicle support structure (2) is provided with first unmanned aerial vehicle support seat (21) for the connection of the unmanned aerial vehicle shell (1), second unmanned aerial vehicle support seat (22) for the connection of the unmanned aerial vehicle flight structure (3), the second connection mounting position (221) is provided in the second unmanned aerial vehicle support seat (22), and the first connection mounting position (211) is provided in the first unmanned aerial vehicle support seat (21);The second connection mounting position (221) is connected in the first connection mounting position (211), so that the second unmanned aerial vehicle support seat (22) can be detachably connected in the first unmanned aerial vehicle support seat (21).

2. The drone of claim 1, wherein, The first unmanned aerial vehicle support seat (21) is provided with first unmanned aerial vehicle support plate one (212) and first unmanned aerial vehicle support plate two (213), and the first unmanned aerial vehicle support plate one (212) and the first unmanned aerial vehicle support plate two (213) are oppositely arranged to form the first connection mounting position (211) for the connection of the second connection mounting position (221).

3. The drone of claim 1, wherein, The second unmanned aerial vehicle support seat (22) is provided with second unmanned aerial vehicle support seat one (222) and second unmanned aerial vehicle support seat two (223), and the second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) are oppositely connected in the first connection mounting position (211) to be fastened.

4. The easily detachable drone of claim 3, wherein, The second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) are respectively provided with second unmanned aerial vehicle support seat mounting position one (2221) and second unmanned aerial vehicle support seat mounting position two (2231), and the second unmanned aerial vehicle support seat mounting position one (2221) and the second unmanned aerial vehicle support seat mounting position two (2231) are connected in the first connection mounting position (211) to form the second connection mounting position (221).

5. The easily detachable drone of claim 4, wherein, The second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) are respectively provided with flight structure mounting position one (2222) and flight structure mounting position two (2232), and the flight structure mounting position one (2222) is arranged at the other end of the second unmanned aerial vehicle support seat one (222) relative to the second unmanned aerial vehicle support seat mounting position one (2221), and the flight structure mounting position two (2232) is arranged at the other end of the second unmanned aerial vehicle support seat two (223) relative to the second unmanned aerial vehicle support seat mounting position two (2231), and the unmanned aerial vehicle flight structure (3) is connected in the flight structure mounting position one (2222) or flight structure mounting position two (2232) to be fastened.

6. The easily detachable drone of claim 4, wherein, The unmanned aerial vehicle support structure (2) is further provided with a first support stabilizing structure (23) and a second support stabilizing structure (24), the second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) are further provided with a support stabilizing mounting part one (2223) and a support stabilizing mounting part two (2233), and the first support stabilizing structure (23) and the second support stabilizing structure (24) are connected to the support stabilizing mounting part one (2223) and the support stabilizing mounting part two (2233) respectively to support the unmanned aerial vehicle.

7. The easily detachable drone of claim 6, wherein, The first support stabilizing structure (23) is provided with a first support limiting slot (231) and a first support stabilizing protrusion (232), the first support limiting slot (231) is provided with a first support limiting block (2311), the support stabilizing mounting part one (2223) is provided with a support stabilizing connecting hole one (22231), the first support stabilizing structure (23) is connected to the first support limiting block (2311) through the support stabilizing connecting hole one (22231), and then is connected into the first support limiting slot (231) and supported through the first support limiting block (2311). The second support stabilizing structure (24) is provided with a second support limiting slot (241) and a second support stabilizing protrusion (242), the second support limiting slot (241) is provided with a second support limiting block (2411), the support stabilizing mounting part two (2233) is provided with a support stabilizing connecting hole two (22331), the second support stabilizing structure (24) is connected to the second support limiting block (2411) through the support stabilizing connecting hole two (22331), and then is connected into the second support limiting slot (241) and supported through the second support stabilizing protrusion (242).

8. The easily detachable drone of claim 2, wherein, A main control module (4) for controlling the flight of the unmanned aerial vehicle is further included, the unmanned aerial vehicle shell (1) is connected to the first unmanned aerial vehicle support plate two (213) and surrounds a control structure mounting cavity, and the first unmanned aerial vehicle support plate one (212) is arranged in the control structure mounting cavity; the main control module (4) is connected to the first unmanned aerial vehicle support plate one (212) and is electrically connected to the unmanned aerial vehicle flight structure (3).

9. The easily detachable drone of claim 8, wherein, A parry waterproof layer for waterproofing is further included, and the parry waterproof layer is arranged on the main control module (4) and the unmanned aerial vehicle flight structure (3) to prevent water.

10. The easily detachable drone of claim 3, wherein, The second unmanned aerial vehicle support seat (22) is further provided with a connecting support (226), and the second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) are designed in an integral molding structure, and a plurality of connecting supports (226) are connected to the second unmanned aerial vehicle support seat one (222) and the second unmanned aerial vehicle support seat two (223) respectively to support.

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