An unmanned aerial vehicle mounting device

Abstract

The utility model discloses an unmanned plane mounting device, including unmanned plane body, the mounting plate of fixed connection in the inside of unmanned plane body, set up in the mounting material subassembly of mounting plate top, the front side fixed connection of mounting plate top has automatic positioning mechanism, automatic positioning mechanism includes the base, the top fixed connection of base has double -end motor, the output fixed connection of double -end motor has the rotation rod no.

Description

Technical Field

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

[0002] Unmanned aerial vehicles (UAVs) are intelligent aircraft that can fly autonomously according to preset programs or remote commands without direct human control. Like "aerial robots," they can flexibly carry cameras, sensors, and even robotic arms, thanks to their lightweight fuselage, efficient power systems, and precise navigation technology. They play a significant role in scenarios such as aerial surveying and mapping, logistics and distribution, agricultural plant protection, emergency rescue, and environmental monitoring. They reduce the risks of high-risk operations and break through the application boundaries of traditional aircraft, becoming "all-rounders" in the integration of modern technology and industry. UAV mounting devices are the core components that expand the functions of UAVs. Through precisely designed mechanical structures or modular interfaces, they can securely fix various professional equipment (such as cameras, sensors, robotic arms, capture nets, etc.) to the UAV, while ensuring that the equipment remains stable during flight and does not interfere with the control of the UAV. They also support quick assembly and disassembly to adapt to different mission requirements.

[0003] According to a patent published on the China Patent Network, the patent title is: "A UAV Mounting Device," patent application number: 202323177662.X. It includes a main body with a mounting box at its bottom. The mounting / dismounting mechanism includes a first wedge, a moving groove, a second wedge, and a support leg. The first wedge is fixedly mounted on the top of the mounting box and extends into the interior of the main body. The moving groove is located inside the main body, and the second wedge is slidably mounted inside the moving groove. The left side of the second wedge extends into the interior of the first wedge. This utility model, through its design... The disassembly and assembly mechanism inserts the first wedge into the main body and starts the drone. Due to the relatively heavy weight of the support block, after the drone takes off, the support block drives the power rod to move, which compresses the connecting block and, through the cooperation of the return spring, causes the second wedge to insert into the first wedge, thus facilitating the disassembly and assembly of the mounting box. However, the drone mounting device described above requires manual operation to position the mounting box, which is time-consuming and greatly affects the positioning efficiency, thus delaying subsequent flight missions and making it inconvenient for users.

[0004] Therefore, it is necessary to redesign and modify the drone mounting device to effectively prevent the slow efficiency of manual positioning. Utility Model Content

[0005] To address the problems mentioned in the background art, the purpose of this utility model is to provide a drone mounting device that has the advantage of automatic and rapid positioning, thus solving the problem of slow manual positioning efficiency.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a drone mounting device, comprising a drone body;

[0007] Mounting plate fixedly connected to the inside of the drone body;

[0008] Mounting components are mounted on top of the mounting plate;

[0009] An automatic positioning mechanism is fixedly connected to the front side of the top of the mounting plate. The automatic positioning mechanism includes a base, a double-ended motor is fixedly connected to the top of the base, a rotating rod is fixedly connected to the output end of the double-ended motor, a helical gear is fixedly connected to the outer side of the rotating rod, and rotating rods are movably connected to both sides of the top of the mounting plate via bearings. A helical gear is fixedly connected to the front of the rotating rod, and the inner side of the helical gear meshes with the helical gear. An L-shaped rod is fixedly connected to the front and rear sides of the top of the rotating rod, and a vertical plate assembly is fixedly connected to the inner side of the L-shaped rod. A pressure plate is provided on the inner side of the vertical plate assembly, and the bottom of the pressure plate contacts the mounting assembly.

[0010] As a preferred embodiment of this utility model, a compaction adjustment mechanism is fixedly connected to the top of the inner side of the vertical plate assembly. The compaction adjustment mechanism includes a convex plate assembly. A spring assembly is fixedly connected to the front and rear sides of the bottom of the convex plate assembly. The bottom of the spring assembly is fixedly connected to the pressure plate, and the outer side of the pressure plate is slidably connected to the vertical plate assembly.

[0011] As a preferred embodiment of the present invention, a sliding groove assembly is provided on the inner side of the vertical plate assembly, and the outer side of the pressure plate is slidably connected to the inside of the sliding groove assembly.

[0012] As a preferred embodiment of this utility model, protective covers are provided on both sides of the top of the dual-end motor, and the bottom of the protective covers is fixedly connected to the mounting plate.

[0013] In a preferred embodiment of this invention, an extension plate is fixedly connected to both the front and back of the pressure plate, and the bottom of the extension plate contacts the hanging component.

[0014] As a preferred embodiment of this utility model, a limiting block is sleeved on the front side of the second surface of the rotating rod, and the bottom of the limiting block is fixedly connected to the mounting plate.

[0015] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0016] 1. This utility model of drone mounting device changes the traditional manual positioning method. It adopts a dual-end motor to drive the rotating rod to rotate, which in turn drives the pressure plate to flip, so that the pressure plate presses on the top of the mounting component, which can achieve automatic positioning, increase positioning efficiency, and ensure the quality of subsequent flight.

[0017] 2. This utility model, through the setting of a compaction adjustment mechanism, can adjust the compaction range of the pressure plate, thereby increasing its adaptability to different sizes of loads.

[0018] 3. By setting the sliding groove assembly, this utility model enables the pressure plate to slide more smoothly inside the vertical plate assembly, reducing the friction between the pressure plate and the vertical plate assembly, extending the service life of the pressure plate, and at the same time limiting the pressure plate.

[0019] 4. This utility model can protect the double-ended motor by setting a protective cover, so as to prevent it from falling off.

[0020] 5. By adding an extension plate, this utility model can increase the contact area between the pressure plate and the hanging component, thereby increasing the stability of compaction.

[0021] 6. By setting a limiting block, this utility model enables the rotating rod two to rotate more stably and avoids tilting. Attached Figure Description

[0022] Figure 1 This is a schematic diagram of the structure of this utility model;

[0023] Figure 2 This is a structural diagram of the automatic positioning mechanism and the compaction adjustment mechanism of this utility model;

[0024] Figure 3 The structure of this utility model Figure 2 Enlarged structural diagram at point A in the middle;

[0025] Figure 4 This is a partial three-dimensional view of the present invention.

[0026] In the diagram: 1. Unmanned aerial vehicle (UAV) body; 2. Mounting plate; 3. Mounting assembly; 4. Automatic positioning mechanism; 5. Base; 6. Dual-end motor; 7. Rotating rod one; 8. Helical gear one; 9. Rotating rod two; 10. Helical gear two; 11. L-shaped rod; 12. Vertical plate assembly; 13. Pressure plate; 14. Compaction adjustment mechanism; 15. Convex plate assembly; 16. Spring assembly; 17. Slide groove assembly; 18. Protective cover; 19. Extension plate; 20. Limiting block. Detailed Implementation

[0027] 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.

[0028] like Figures 1 to 4 As shown, the present invention provides a drone mounting device, including a drone body 1;

[0029] Mounting plate 2 is fixedly connected to the inside of the drone body 1;

[0030] Mounting assembly 3 is installed on top of mounting plate 2;

[0031] An automatic positioning mechanism 4 is fixedly connected to the front side of the top of the mounting plate 2. The automatic positioning mechanism 4 includes a base 5. A double-end motor 6 is fixedly connected to the top of the base 5. A rotating rod 7 is fixedly connected to the output end of the double-end motor 6. A helical gear 8 is fixedly connected to the outer side of the rotating rod 7. A rotating rod 9 is movably connected to both sides of the top of the mounting plate 2 through bearings. A helical gear 10 is fixedly connected to the front of the rotating rod 9. The inner side of the helical gear 10 meshes with the helical gear 8. An L-shaped rod 11 is fixedly connected to the front and rear sides of the top of the rotating rod 9. A vertical plate assembly 12 is fixedly connected to the inner side of the L-shaped rod 11. A pressure plate 13 is provided on the inner side of the vertical plate assembly 12. The bottom of the pressure plate 13 contacts the mounting assembly 3.

[0032] refer to Figure 1 , Figure 2 and Figure 3 A compaction adjustment mechanism 14 is fixedly connected to the top of the inner side of the vertical plate assembly 12. The compaction adjustment mechanism 14 includes a convex plate assembly 15. A spring assembly 16 is fixedly connected to the front and rear sides of the bottom of the convex plate assembly 15. The bottom of the spring assembly 16 is fixedly connected to the pressure plate 13, and the outer side of the pressure plate 13 is slidably connected to the vertical plate assembly 12.

[0033] As a technical optimization of this utility model, the compaction adjustment mechanism 14 can be set to adjust the compaction range of the pressure plate 13, thereby increasing the adaptability to different sizes of loads.

[0034] refer to Figure 2 The inner side of the vertical plate assembly 12 is provided with a sliding groove assembly 17, and the outer side of the pressure plate 13 is slidably connected to the inside of the sliding groove assembly 17.

[0035] As a technical optimization of this utility model, by setting the sliding groove assembly 17, the pressure plate 13 can slide more smoothly inside the vertical plate assembly 12, reducing the friction between the pressure plate 13 and the vertical plate assembly 12, extending the service life of the pressure plate 13, and at the same time limiting the pressure plate 13.

[0036] refer to Figure 2 The double-ended motor 6 has protective covers 18 on both sides of its top, and the bottom of the protective covers 18 is fixedly connected to the mounting plate 2.

[0037] As a technical optimization of this utility model, the protective cover 18 can protect the double-ended motor 6 and prevent it from falling off.

[0038] refer to Figure 2 An extension plate 19 is fixedly connected to both the front and back of the pressure plate 13, and the bottom of the extension plate 19 is in contact with the hanging component 3.

[0039] As a technical optimization of this utility model, by setting the extension plate 19, the contact area between the pressure plate 13 and the hanging component 3 can be increased, thereby increasing the stability of compaction.

[0040] refer to Figure 2 A limiting block 20 is fitted on the front side of the surface of the rotating rod 29, and the bottom of the limiting block 20 is fixedly connected to the mounting plate 2.

[0041] As a technical optimization of this utility model, by setting the limiting block 20, the rotating rod 9 can rotate more stably and avoid tilting.

[0042] The working principle and usage process of this utility model are as follows: First, the double-end motor 6 in the automatic positioning mechanism 4 is turned on. The double-end motor 6 starts to run, and its output end drives the rotating rod 7 to rotate. When the rotating rod 7 rotates, the helical gear 8 fixedly connected to the outside rotates accordingly. Since the helical gear 10 meshes with the helical gear 8 and the helical gear 10 is fixed on the front of the rotating rod 9, the helical gear 10 will drive the rotating rod 9 to rotate on both sides of the top of the mounting plate 2 through the bearing. The rotation of the rotating rod 9 causes the L-shaped rod 11 fixedly connected to the front and rear sides of the top to rotate synchronously, thereby driving the vertical plate assembly 12 fixedly connected to the inner side of the L-shaped rod 11 to move inward. During the inward movement of the vertical plate assembly 12, the pressure plate 13 in the compaction adjustment mechanism 14 gradually approaches. The load assembly 3 is positioned from multiple directions until the bottom of the pressure plate 13 contacts the load assembly 3. At the same time, the extension plate 19, which is fixedly connected to the front and back of the pressure plate 13, also contacts the load assembly 3. This achieves automatic and rapid positioning. After the pressure plate 13 contacts the load assembly 3, the vertical plate assembly 12 continues to move inward a certain distance. At this time, the spring assembly 16 in the compaction adjustment mechanism 14 is compressed. The spring assembly 16 applies a stable and moderate pressure to the pressure plate 13 through its own elastic force, so that the pressure plate 13 can tightly compact the load assembly 3. This ensures that the load assembly 3 will not shift or fall off due to vibration or shaking during flight, achieving the effect of adapting to loads of different sizes.

[0043] In summary, this drone mounting device changes the traditional manual positioning method by using a dual-end motor 6 to drive the rotating rod 7 to rotate, which in turn drives the pressure plate 13 to flip, so that the pressure plate 13 presses on the top of the mounting component 3, thus enabling automatic positioning, increasing positioning efficiency and ensuring the quality of subsequent flights.

[0044] 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.

[0045] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A drone mounting device, comprising a drone body (1); Mounting plate (2) is fixedly connected to the inside of the UAV body (1); Mounting assembly (3) is set on top of mounting plate (2); Its features are: An automatic positioning mechanism (4) is fixedly connected to the front side of the top of the mounting plate (2). The automatic positioning mechanism (4) includes a base (5). A double-end motor (6) is fixedly connected to the top of the base (5). A rotating rod (7) is fixedly connected to the output end of the double-end motor (6). A helical gear (8) is fixedly connected to the outer side of the rotating rod (7). A rotating rod (9) is movably connected to both sides of the top of the mounting plate (2) through bearings. A helical gear (10) is fixedly connected to the front of the rotating rod (9). The inner side of the helical gear (10) meshes with the helical gear (8). An L-shaped rod (11) is fixedly connected to the front and rear sides of the top of the rotating rod (9). A vertical plate assembly (12) is fixedly connected to the inner side of the L-shaped rod (11). A pressure plate (13) is provided on the inner side of the vertical plate assembly (12). The bottom of the pressure plate (13) contacts the mounting assembly (3).

2. The UAV mounting device according to claim 1, characterized in that: The top of the inner side of the vertical plate assembly (12) is fixedly connected to a compaction adjustment mechanism (14). The compaction adjustment mechanism (14) includes a convex plate assembly (15). The front and rear sides of the bottom of the convex plate assembly (15) are fixedly connected to spring assemblies (16). The bottom of the spring assembly (16) is fixedly connected to the pressure plate (13). The outer side of the pressure plate (13) is slidably connected to the vertical plate assembly (12).

3. The UAV mounting device according to claim 2, characterized in that: The inner side of the vertical plate assembly (12) is provided with a sliding groove assembly (17), and the outer side of the pressure plate (13) is slidably connected to the inside of the sliding groove assembly (17).

4. The UAV mounting device according to claim 1, characterized in that: The dual-end motor (6) has protective covers (18) on both sides of its top, and the bottom of the protective cover (18) is fixedly connected to the mounting plate (2).

5. The UAV mounting device according to claim 1, characterized in that: The front and back of the pressure plate (13) are fixedly connected to extension plates (19), and the bottom of the extension plates (19) is in contact with the hanging assembly (3).

6. The UAV mounting device according to claim 1, characterized in that: A limiting block (20) is fitted on the front side of the surface of the rotating rod (9), and the bottom of the limiting block (20) is fixedly connected to the mounting plate (2).

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