A detachable drone fuselage

Abstract

This utility model relates to the field of unmanned aerial vehicle (UAV) technology and discloses a detachable UAV fuselage. The detachable UAV fuselage includes: a main body; a limiting plate located at one end of the main body, the limiting plate being used to allow the tail section at one end of the main body to be detached from the main body; a protrusion is provided at one end of the main body, the protrusion being integrally formed with the main body, the other end of the protrusion being connected to the interior of the tail section via an embedded connection; a convex ring is provided on the outer side of the protrusion; through the rebound force of an elastic element, the elastic element pulls the limiting plate back to its original position via a telescopic column, and then a toggle plate rotates the extension column, the extension column moving within the bracket via a thread; the extension column rotates within the connecting column via the limiting rod's limiting bottom, thereby driving the pulley to move upward, lowering the height of the main body and the tail section, thus allowing the UAV fuselage to be detached for easy carrying, demonstrating the practicality of this device.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a detachable UAV fuselage. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously by an onboard computer, either completely or intermittently.

[0003] Before using a drone, it needs to be taken to an open area.

[0004] However, existing drones are generally large in size. In order not to affect the overall strength of the drone body, the drone body is usually integrated, which is inconvenient for users to carry. Only larger transportation vehicles can transport the drone, which is troublesome and cumbersome.

[0005] Furthermore, the wings of existing drones are quite long, and in order to make them easier to carry, the wings are disassembled and then secured with fasteners during use. However, securing them with multiple fasteners is time-consuming and laborious. Utility Model Content

[0006] The purpose of this invention is to provide a detachable drone fuselage to solve the problems mentioned in the background section.

[0007] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a detachable drone fuselage, comprising:

[0008] main body;

[0009] A limiting plate located at one end of the main body, the limiting plate being used to allow the tail section at one end of the main body to be detached from the main body;

[0010] One end of the main body is provided with a protrusion, which is integrally formed with the main body. The other end of the protrusion is connected to the interior of the tail section by embedding. A convex ring is provided on the outside of the protrusion, one end of which is integrally formed with the tail section. The other end of the convex ring is connected to the interior of the main body by embedding. A limiting plate is provided on the outside of the main body and the tail section. The limiting plate passes through and connects the protrusion and the convex ring. A fixing plate is fixedly connected to the top of the main body. Wings are provided on both sides of the fixing plate. One end of the wing is fixedly connected to a fixing post. The other end of the fixing post is connected to the interior of the fixing plate by embedding.

[0011] Preferably, the top of the fixing plate has a groove, the bottom of the support plate is connected to the inside of the groove by a fastener, the inside of the support plate is connected to a threaded ring by rotation, the inside of the threaded ring is connected to a threaded post, and the other end of the threaded post is fastened to the wing.

[0012] Preferably, a baffle is provided at the top of the groove, the baffle is connected to the inner wall of the groove by sliding, a rubber strip is fastened to one end of the baffle, and reinforcing rings are fixedly connected to both sides of the fixing plate.

[0013] Preferably, the main body is connected to a support column by fasteners, one end of the support column is connected to one end of a telescopic column by embedding, the other end of the telescopic column is connected to a limiting plate by fasteners, and the top of the limiting plate is connected to the bottom of the pull plate by fasteners.

[0014] Preferably, the top of the pull plate is slidably connected to the top of the main body, one end of the elastic element is connected to the internal fastener of the fixed column, the other end of the elastic element is connected to the telescopic column through a fastener, the bottom of the main body is connected to the top of the bracket through a fastener, and the top of the extension column is connected to the inside of the bracket through a thread.

[0015] Preferably, the bottom of the extension column is connected to the connecting column by rotation, the bottom of the connecting column is connected to the pulley by rotation, one end of the limiting rod is connected to the side of the extension column by fasteners, the other end of the limiting rod is slidably connected to the bracket, and the outer wall of the extension column is fixedly connected to the actuating plate.

[0016] Compared with the prior art, the beneficial effects achieved by this utility model are:

[0017] First, this utility model, by setting a tail section and a limiting plate, facilitates the disassembly of the drone's body. When it is necessary to carry the drone, push the pull plates to both sides. The pull plates move the limiting plates, which in turn move the telescopic columns, causing one end of the limiting plate to move out of the interior of the protrusion and ring. Then, pull the tail section to one end to separate the tail section from the main body. Release the pull plates, and through the rebound force of the elastic element, the elastic element pulls the limiting plate back to its original position via the telescopic column. Then, rotate the extension column by the actuating plate. The extension column moves inside the bracket through the thread, and rotates inside the connecting column through the limiting rod's bottom limit, thereby driving the pulley to move upward, lowering the height of the main body and tail section. This allows the drone's body to be disassembled for easy carrying, demonstrating the practicality of this device.

[0018] Secondly, this utility model, by setting a fixed post and a threaded post, enables quick disassembly and installation of the wing. When the wing needs to be removed, open the baffle at the top of the groove, allowing the baffle to slide into the interior of the fixed plate. Then, rotate the threaded ring, which pushes the threaded post outward through the threads. The threaded post drives the wing and the fixed post to move until the threaded post is completely outside the threaded ring. Pull the wing outward, causing the wing to move the fixed post out of the interior of the fixed plate, thus removing the wing. When reassembly is required, simply reverse the operation. There is no need to use multiple fasteners for installation and disassembly, saving time and effort and effectively improving work efficiency. Attached Figure Description

[0019] Figure 1 This is a perspective view of the present utility model;

[0020] Figure 2 This is a schematic diagram of the protrusion and convex ring structure of this utility model;

[0021] Figure 3 This is a schematic diagram of the fixing plate and fixing column structure of this utility model;

[0022] Figure 4 This is a schematic diagram of the threaded ring and baffle structure of this utility model;

[0023] Figure 5 This is a schematic diagram of the limiting plate and pull plate structure of this utility model;

[0024] Figure 6 This is a schematic diagram of the extension column and limiting rod structure of this utility model.

[0025] The components are as follows: 1. Main body; 2. Tail; 3. Fixing plate; 4. Wing; 5. Baffle; 6. Bracket; 7. Connecting column; 8. Pulley; 9. Protrusion; 10. Protruding ring; 11. Limiting plate; 12. Fixing column; 13. Threaded column; 14. Extension column; 15. Reinforcing ring; 16. Support plate; 17. Threaded ring; 18. Rubber strip; 19. Groove; 20. Support column; 21. Telescopic column; 22. Elastic element; 23. Pull plate; 24. Limiting rod; 25. Actuating plate. Detailed Implementation

[0026] 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.

[0027] Please see Figure 1-6 A detachable drone fuselage, comprising:

[0028] Entity 1;

[0029] A limiting plate 11 is located at one end of the main body 1. The limiting plate 11 is used to allow the tail 2 at one end of the main body 1 to be detached from the main body 1.

[0030] One end of the main body 1 has a protrusion 9, which is integrally formed with the main body 1. The other end of the protrusion 9 is connected to the interior of the tail 2 by an embedded form. A protruding ring 10 is provided on the outer side of the protrusion 9, one end of which is integrally formed with the tail 2, and the other end of which is connected to the interior of the main body 1 by an embedded form. A limiting plate 11 is provided on the outer side of the main body 1 and the tail 2, and the limiting plate 11 passes through and connects the protrusion 9 and the protruding ring 10. A fixing plate 3 is fixedly connected to the top of the main body 1. Wings 4 are provided on both sides of the fixing plate 3. One end of the wing 4 is fixedly connected to a fixing post 12, and the other end of the fixing post 12 is connected to the interior of the fixing plate 3 by an embedded form. When it is necessary to carry the drone, the pull plate 23 is pushed to both sides, and the pull plate 23 moves the limiting plate 1. 1. Movement: The limiting plate 11 moves the telescopic column 21, causing one end of the limiting plate 11 to move out of the interior of the protrusion 9 and the convex ring 10. Then, the tail 2 is pulled to one end, causing the tail 2 to separate from the main body 1. The pulling plate 23 is released, and through the rebound force of the elastic element 22, the elastic element 22 pulls the limiting plate 11 back to its original position through the telescopic column 21. Then, the extension column 14 is rotated by the actuating plate 25. The extension column 14 moves inside the bracket 6 through the thread. The extension column 14 rotates inside the connecting column 7 through the limiting bottom of the limiting rod 24, thereby driving the pulley 8 to move upward, lowering the height of the main body 1 and the tail 2. This allows the drone body to be disassembled for easy carrying, demonstrating the practicality of this device.

[0031] Specifically, the top of the fixing plate 3 has a groove 19, and the bottom of the support plate 16 is connected inside the groove 19 by fasteners. The support plate 16 is connected inside the threaded ring 17 by rotation. The threaded ring 17 is connected inside the threaded post 13, and the other end of the threaded post 13 is connected to the wing 4 by fasteners.

[0032] Through the above technical solution, the threaded post 13 is used to connect with the threaded ring 17, which facilitates the fixing of the wing 4 and the disassembly and installation of the wing 4.

[0033] Specifically, a baffle 5 is provided at the top of the groove 19. The baffle 5 is connected to the inner wall of the groove 19 by sliding. A rubber strip 18 is fastened to one end of the baffle 5, and reinforcing rings 15 are fixedly connected to both sides of the fixing plate 3.

[0034] With the above technical solution, a rubber strip 18 is provided at one end of the baffle 5 to increase the damping force between the baffle 5 and the inner wall of the groove 19. Only by using a certain force can the baffle 5 be opened or closed. The reinforcing ring 15 is used to increase the strength of the connection between the wing 4 and the fixing plate 3.

[0035] Specifically, the main body 1 is connected to the support column 20 by fasteners. One end of the support column 20 is connected to one end of the telescopic column 21 by embedding. The other end of the telescopic column 21 is connected to the limiting plate 11 by fasteners. The top of the limiting plate 11 is connected to the bottom of the pull plate 23 by fasteners.

[0036] Through the above technical solution, the support column 20 is used to limit the telescopic column 21 and the elastic element 22, to prevent the telescopic column 21 from shifting when it moves, and to prevent the elastic element 22 from tilting when it is squeezed. The limiting plate 11 is respectively set on both sides of the main body 1, and the telescopic column 21 and the elastic element 22 are respectively embedded at both ends of the support column 20.

[0037] Specifically, the top of the pull plate 23 is slidably connected to the top of the main body 1, one end of the elastic element 22 is connected to the inside of the fixed column 12 by a fastener, the other end of the elastic element 22 is connected to the telescopic column 21 by a fastener, the bottom of the main body 1 is connected to the top of the bracket 6 by a fastener, and the top of the extension column 14 is connected to the inside of the bracket 6 by a thread.

[0038] Through the above technical solution, the pull plate 23 is used by the user to push the pull plate 23 in the opposite direction, so that the pull plate 23 can drive the limiting plate 11 to move out of the interior of the convex ring 10 and the convex block 9, so that the two are no longer stuck together.

[0039] Specifically, the bottom of the extension column 14 is connected to the connecting column 7 by rotation, the bottom of the connecting column 7 is connected to the pulley 8 by rotation, one end of the limiting rod 24 is connected to the side of the extension column 14 by fasteners, the other end of the limiting rod 24 is slidably connected to the bracket 6, and the outer wall of the extension column 14 is fixedly connected to the actuating plate 25.

[0040] Through the above technical solution, the limiting rod 24 is used to limit the connecting column 7 to prevent the connecting column 7 from rotating together when the extension column 14 rotates. The pulley 8 can be adjusted in orientation. Two pulleys 8 are provided below the tail 2, and their structure is the same as that of the front bracket 6.

[0041] In use, push the pull plate 23 to both sides. The pull plate 23 moves the limiting plate 11, which in turn moves the telescopic column 21, causing one end of the limiting plate 11 to move out of the interior of the protrusion 9 and the convex ring 10. Then, pull the tail 2 to one end to separate the tail 2 from the main body 1. Release the pull plate 23. Through the rebound force of the elastic element 22, the elastic element 22 pulls the limiting plate 11 back to its original position via the telescopic column 21. Then, rotate the extension column 14 by the actuating plate 25. The extension column 14 moves inside the bracket 6 through the thread. The extension column 14 is controlled by the limiting rod. The bottom limit of 24 rotates inside the connecting column 7, thereby driving the pulley 8 to move upward, lowering the height of the main body 1 and the tail 2, opening the baffle 5 at the top of the groove 19, allowing the baffle 5 to slide into the interior of the fixed plate 3, and then rotating the threaded ring 17. The threaded ring 17 pushes the threaded column 13 to move outward through the thread, and the threaded column 13 drives the wing 4 and the fixed column 12 to move until the threaded column 13 is completely moved outside the threaded ring 17, pulling the wing 4 outward, so that the wing 4 drives the fixed column 12 to move out of the interior of the fixed plate 3, thus completing the work.

[0042] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0043] Finally, it should be noted that the above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A detachable drone body, characterized in that: include: Main body (1); A limiting plate (11) is located at one end of the main body (1), the limiting plate (11) is used to allow the tail (2) at one end of the main body (1) to be detached from the main body (1); One end of the main body (1) is provided with a protrusion (9), which is integrally formed with the main body (1). The other end of the protrusion (9) is connected to the interior of the tail (2) by embedding. A protruding ring (10) is provided on the outside of the protrusion (9), which is integrally formed with the tail (2) and the other end of the protruding ring (10) is connected to the interior of the main body (1) by embedding. A limiting plate (11) is provided on the outside of the main body (1) and the tail (2), and the limiting plate (11) passes through and connects the protrusion (9) and the protruding ring (10). A fixing plate (3) is fixedly connected to the top of the main body (1). Wings (4) are provided on both sides of the fixing plate (3). One end of the wing (4) is fixedly connected to a fixing post (12), and the other end of the fixing post (12) is connected to the interior of the fixing plate (3) by embedding.

2. The detachable unmanned aerial vehicle fuselage according to claim 1, characterized in that: The top of the fixed plate (3) has a groove (19), and the bottom of the support plate (16) is connected inside the groove (19) by fasteners. The support plate (16) is connected inside the threaded ring (17) by rotation. The threaded ring (17) is connected inside the threaded post (13), and the other end of the threaded post (13) is connected to the wing (4) by fasteners.

3. The detachable unmanned aerial vehicle fuselage according to claim 2, characterized in that: The top of the groove (19) is provided with a baffle (5), which is connected to the inner wall of the groove (19) by sliding. One end of the baffle (5) is fastened to a rubber strip (18), and the two sides of the fixing plate (3) are fixedly connected with reinforcing rings (15).

4. The detachable unmanned aerial vehicle fuselage according to claim 1, characterized in that: The main body (1) is connected to a support column (20) by fasteners inside. One end of the support column (20) is connected to one end of a telescopic column (21) by embedding. The other end of the telescopic column (21) is connected to a limiting plate (11) by fasteners. The top of the limiting plate (11) is connected to the bottom of a pull plate (23) by fasteners.

5. A detachable unmanned aerial vehicle fuselage according to claim 4, characterized in that: The top of the pull plate (23) is slidably connected to the top of the main body (1). The fastener inside the fixed column (12) is connected to one end of the elastic element (22). The other end of the elastic element (22) is connected to the telescopic column (21) through a fastener. The bottom of the main body (1) is connected to the top of the bracket (6) through a fastener. The top of the extension column (14) is connected inside the bracket (6) through a thread.

6. A detachable unmanned aerial vehicle fuselage according to claim 5, characterized in that: The bottom of the extension column (14) is connected to the connecting column (7) by rotation. The bottom of the connecting column (7) is connected to the pulley (8) by rotation. The side of the extension column (14) is connected to one end of the limiting rod (24) by fasteners. The other end of the limiting rod (24) is slidably connected to the bracket (6). The outer wall of the extension column (14) is fixedly connected to the actuating plate (25).

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