Unmanned aerial vehicle mounting device

Abstract

The unmanned aerial vehicle mounting device comprises a vehicle body, a mounting column is fixedly connected to the bottom of the vehicle body, a bottom plate is arranged at the bottom of the vehicle body, a connecting sleeve is fixedly connected to the top of the bottom plate, the mounting column is inserted into the connecting sleeve, and inner cavities are formed in the two sides of the connecting sleeve. In the actual use process, the bottom of the clamping plate is pressed to compress the second spring, the first spring is kept in a tightened state, the connecting sleeve is installed on the installation column at the bottom of the machine body, when the limiting ring is located below the bottom end of the clamping plate, the pressure of the clamping plate is released, the second spring is automatically bounced off to the original position, and the first spring is pulled back; the top end of the clamping plate is close to the limiting ring and limited on the inner rod through the limiting sleeve, so that the clamping plate rotates at a fixed point and is completely clamped on the limiting ring, the connecting sleeve and the bottom plate are installed, rapid installation is achieved, the problems that a traditional device is complex in installation process and low in efficiency are solved, and working efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a mounting device for an unmanned aerial vehicle. Background Art

[0002] A drone mounting device is a mechanical structure used to install various additional equipment or loads on a drone. This device usually includes brackets, connectors, stabilizers and other components, which can be fixed on the fuselage or bottom of the drone to install various sensors, cameras, cargo delivery devices, communication equipment, etc. The design of this device enables drones to have a wider range of functions and application scenarios, such as aerial photography, search and rescue, agricultural spraying, logistics and distribution, etc.

[0003] After searching, the Chinese patent with the announcement number: CN220809844U discloses a UAV mounting device. The patent records that by adjusting the center of gravity position of the mounting device, the UAV can avoid unstable flight due to unbalanced center of gravity. The camera can be protected by the provision of a rubber shock-absorbing pad to prevent frequent vibration of the lens from affecting shooting. The device has a simple structure and is easy to mount and adjust.

[0004] In this solution, the mounting device is not convenient to install on the drone during use. The traditional installation method is to install and fix it by screws or welding. The installation of the mounting device is troublesome, and the installation process is time-consuming and labor-intensive. At the same time, when disassembly is required, professional tools must be used to complete it, resulting in a problem of greatly reduced work efficiency. In order to solve this technical problem, the utility model proposes a drone mounting device. Summary of the invention

[0005] 1. Technical issues to be resolved

[0006] In this solution, the mounting device is not convenient to install on the drone during use. The traditional installation method is to install and fix it by screws or welding. The installation of the mounting device is troublesome, and the installation process is time-consuming and labor-intensive. At the same time, when disassembly is required, professional tools must be used to complete it, resulting in a problem of greatly reduced work efficiency. In order to solve this technical problem, the utility model proposes a drone mounting device.

[0007] (II) Technical solution

[0008] To achieve the above objectives, the utility model is implemented through the following technical solutions: a drone mounting device comprises a fuselage, a mounting column is fixedly connected to the bottom of the fuselage, a bottom plate is arranged at the bottom of the fuselage, a connecting sleeve is fixedly connected to the top of the bottom plate, the mounting column is inserted into the interior of the connecting sleeve, an inner cavity is opened on both sides of the connecting sleeve, and a clamping plate is arranged on both sides of the connecting sleeve, a mounting plate 1 is fixedly connected to the inner wall above the clamping plate, a spring 1 is fixedly connected to the inner side wall of the mounting plate 1, and the other end of the spring 1 is fixedly connected to the outer wall above the connecting sleeve, a mounting plate 2 is fixedly connected to the inner wall below the clamping plate, a spring 2 is fixedly connected to the inner side wall of the mounting plate 2, and the other end of the spring 2 is fixedly connected to the outer wall below the connecting sleeve, a limiting sleeve is fixedly connected to the inner side of the middle part of the clamping plate, an inner rod is rotatably connected to the inside of the limiting sleeve, and the inner rod is fixedly connected to the inner cavity, a limiting ring is fixedly connected to the outer wall above the mounting column, and the top end of the clamping plate is engaged with the limiting ring.

[0009] Preferably, connecting plates are fixedly connected to both sides of the bottom wall of the base plate, a bidirectional threaded rod is rotatably connected between the connecting plates on both sides, and a positioning rod is fixedly connected between the connecting plates on both sides.

[0010] Preferably, two pairs of vertical plates 1 are provided at the bottom of the base plate, and one side of the vertical plate 1 is threadedly connected to the two ends of the outer wall of the bidirectional threaded rod.

[0011] Preferably, the vertical plate on the other side is slidably connected to the outer wall of the positioning rod.

[0012] Preferably, a plurality of inner holes 2 are opened inside the vertical plate 1, and a latch is arranged outside the vertical plate 1, and the latch is slidably connected in the inner hole 2.

[0013] Preferably, a pair of vertical plates 2 are provided at the bottom of the vertical plate 1, and the vertical plate 2 is U-shaped, and the two walls of the vertical plate 2 are respectively slidably connected to the vertical plate 1, and a pair of inner holes 1 are opened inside the vertical plate 2, and the inner hole 1 corresponds to the inner hole 2, and the pin passes through the vertical plate 2 and extends to the outside of the vertical plate 1.

[0014] (III) Beneficial effects

[0015] The utility model provides a drone mounting device, which has the following beneficial effects:

[0016] (1) By pressing the bottom of the card plate, spring 2 is compressed and spring 1 is kept in a taut state. The connecting sleeve is installed on the mounting column at the bottom of the fuselage. When the limit ring is located below the bottom end of the card plate, the pressure of the card plate is released, spring 2 automatically pops open to its original position, spring 1 is pulled back, the top end of the card plate approaches the limit ring and is limited on the inner rod by the limit sleeve, so that the card plate rotates at a fixed point and is completely stuck on the limit ring. The connecting sleeve and the bottom plate are installed, realizing quick installation, solving the problem of complex installation process and low efficiency of traditional devices, and improving work efficiency.

[0017] (2) By adjusting the height of the vertical plate 2 and ensuring that the inner hole 1 is aligned with the inner hole 2, inserting the pin to fix the position, and then rotating the two-way threaded rod to make the vertical plate 1 move up and down under the support of the vertical plate 2, the positioning rod is limited to prevent displacement. This system can flexibly adapt to loads of different sizes, solves the problem of cumbersome fixing and adjustment processes, and improves the convenience and efficiency of operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0019] Figure 2 It is a schematic diagram of the overall side structure of the utility model;

[0020] Figure 3 This is a schematic diagram of the bottom structure of the bottom plate of the utility model;

[0021] Figure 4 for Figure 2 Enlarged view of point A in the middle.

[0022] In the figure: 1. body; 2. mounting column; 3. limiting ring; 4. connecting sleeve; 5. inner rod; 6. spring 1; 7. clamping plate; 8. spring 2; 9. limiting sleeve; 10. inner cavity; 11. bottom plate; 12. connecting plate; 13. bidirectional threaded rod; 14. positioning rod; 15. vertical plate 1; 16. vertical plate 2; 17. latch; 18. inner hole 1; 19. inner hole 2; 20. mounting plate 1; 21. mounting plate 2. DETAILED DESCRIPTION

[0023] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0024] See also Figure 1-4 , the utility model provides a technical solution:

[0025] Embodiment 1: A UAV mounting device comprises a fuselage 1, a mounting column 2 is fixedly connected to the bottom of the fuselage 1, a bottom plate 11 is arranged at the bottom of the fuselage 1, a connecting sleeve 4 is fixedly connected to the top of the bottom plate 11, the mounting column 2 is inserted into the inside of the connecting sleeve 4, an inner cavity 10 is opened on both sides of the connecting sleeve 4, and a clamping plate 7 is arranged on both sides of the connecting sleeve 4, a mounting plate 20 is fixedly connected to the inner wall above the clamping plate 7, a spring 6 is fixedly connected to the inner wall of the mounting plate 20, and the other end of the spring 6 is fixedly connected to the outer wall above the connecting sleeve 4, a mounting plate 21 is fixedly connected to the inner wall below the clamping plate 7, and a spring 28 is fixedly connected to the inner wall of the mounting plate 21, and the other end of the spring 28 is fixedly connected to the outer wall below the connecting sleeve 4, a limiting sleeve 9 is fixedly connected to the inner side of the middle part of the clamping plate 7, an inner rod 5 is rotatably connected inside the limiting sleeve 9, and the inner rod 5 is fixedly connected in the inner cavity 10, a limiting ring 3 is fixedly connected to the outer wall above the mounting column 2, and the top of the clamping plate 7 is engaged with the limiting ring 3.

[0026] By pressing the two sides of the bottom of the card plate 7, the spring 2 8 is compressed, while the spring 1 6 is kept in a taut state. Subsequently, the connecting sleeve 4 is put on the mounting column 2 at the bottom of the fuselage 1. When the limiting ring 3 on the mounting column 2 is located below the bottom end of the card plate 7, the pressure on the card plate 7 is released. In this way, the spring 2 8 will naturally spring open to the restored state, and the spring 1 6 will be retracted to the restored state. As the top of the card plate 7 gradually approaches the limiting ring 3, the card plate 7 is limited on the inner rod 5 by the limiting sleeve 9, thereby realizing the fixed-point rotation of the card plate 7. When the top of the card plate 7 is completely stuck on the limiting ring 3, the installation of the connecting sleeve 4 and the bottom plate 11 is completed. This cooperative installation method not only realizes quick installation, but also provides convenience for subsequent maintenance and replacement operations, thereby improving work efficiency.

[0027] Embodiment 2: The difference between this embodiment and embodiment 1 is that, the bottom plate 11 has connecting plates 12 fixedly connected to both sides of the lower wall, and a bidirectional threaded rod 13 is rotatably connected between the connecting plates 12 on both sides, and a positioning rod 14 is fixedly connected between the connecting plates 12 on both sides, and two pairs of vertical plates 15 are arranged at the bottom of the bottom plate 11, one side of the vertical plate 15 is threadedly connected to the two ends of the outer wall of the bidirectional threaded rod 13, and the other side of the vertical plate 15 is slidably connected to the outer wall of the positioning rod 14, and the inside of the vertical plate 15 is A plurality of inner holes 19 are provided, and a latch 17 is provided on the outside of the vertical plate 15, and the latch 17 is slidably connected in the inner hole 19. A pair of vertical plates 16 are provided at the bottom of the vertical plate 15, and the vertical plate 16 is U-shaped. At the same time, the two walls of the vertical plate 16 are slidably connected in the vertical plate 15, and a pair of inner holes 18 are provided in the vertical plate 16, and the inner hole 18 corresponds to the inner hole 19. At the same time, the latch 17 penetrates the vertical plate 16 and extends to the outside of the vertical plate 15.

[0028] According to the height requirement of the object to be loaded, the vertical plate 16 needs to be adjusted. By pulling the vertical plate 16 up and down, it will be limited inside the vertical plate 15 and have the function of lengthening and shortening. Once adjusted to the appropriate position, it is necessary to ensure that the inner hole 18 on the vertical plate 16 is aligned with the inner hole 19, and then insert the pin 17 to fix the position. Once the height is determined, the object to be loaded is placed between the vertical plates 16 on both sides. Next, by rotating the bidirectional threaded rod 13, the action of the bidirectional threaded rod 13 will drive the vertical plates 15 at both ends to move in the opposite direction. When the load is small, the vertical plate 15 can be moved inward by rotating the bidirectional threaded rod 13, and at the same time, the vertical plate 16 can be driven to move until it is close to the load to ensure its fixation. The vertical plate 15 will be limited by the positioning rod 14 when moving to prevent deviation. This synergy ensures the effective fixation and installation of loads of different sizes, thereby greatly improving work efficiency.

[0029] During operation, when the staff uses the fuselage 1 to carry objects, they first install the loading rack on the fuselage 1. At this time, they press the bottom of the card plates 7 on both sides so that the spring 2 8 is in a compressed state and the spring 1 6 is in a tight state. At this time, the connecting sleeve 4 is put on the mounting column 2 at the bottom of the fuselage 1. When the limiting ring 3 on the mounting column 2 is located below the bottom end of the card plate 7, the card plate 7 is released. At this time, the spring 2 8 will bounce outward until it is restored, and the spring 1 6 will be pulled back inward to restore. At this time, the top of the card plate 7 will move closer to the limiting ring 3. At the same time, the card plate 7 is limited on the inner rod 5 by the limiting sleeve 9, so that the card plate 7 can rotate at a fixed point. When the top of the card plate 7 is completely stuck on the limiting ring 3, the connecting sleeve 4 and the bottom plate 11 are installed after completion. Through their cooperation, the effect of quick installation is achieved, and it is also convenient for later maintenance and replacement operations and improves work efficiency. After the installation is completed, the vertical plate 16 needs to be adjusted according to the height of the object to be loaded. By pulling the vertical plate 16 up and down, the vertical plate 16 will be limited inside the vertical plate 15, and the effect of lengthening and shortening can be achieved. After adjusting the position, the inner hole 18 on the vertical plate 16 needs to be aligned with the inner hole 19, and the pin 17 is inserted to fix it. After the height is determined, the object to be loaded is placed between the vertical plates 16 on both sides, and the two-way threaded rod 13 is rotated. Under the action of the two-way threaded rod 13, the vertical plates 15 at both ends will be driven to move in the opposite direction. When the object is small, the vertical plate 15 is driven to move inward by rotating the two-way threaded rod 13, and the vertical plate 16 is driven to move until it is close to the object to fix it. At the same time, the vertical plate 15 will be limited by the positioning rod 14 when moving to prevent the vertical plate 15 from deviating when moving. Through their cooperation, it is achieved that objects of different sizes can be effectively fixed and installed, and through their cooperation, the work efficiency is greatly improved.

[0030] It should be noted that, in this document, relational terms such as first and second, etc. are merely used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations.

Claims

1. A UAV mounting device, characterized in that: The invention comprises a fuselage (1), wherein a mounting column (2) is fixedly connected to the bottom of the fuselage (1), a bottom plate (11) is arranged at the bottom of the fuselage (1), a connecting sleeve (4) is fixedly connected to the top of the bottom plate (11), the mounting column (2) is inserted into the interior of the connecting sleeve (4), an inner cavity (10) is provided on both sides of the connecting sleeve (4), and a clamping plate (7) is arranged on both sides of the connecting sleeve (4), a mounting plate (20) is fixedly connected to the inner wall above the clamping plate (7), a spring (6) is fixedly connected to the inner wall of the mounting plate (20), and the other end of the spring (6) is fixedly connected to the The upper outer wall of the connecting sleeve (4) and the lower inner wall of the clamping plate (7) are fixedly connected to the second mounting plate (21), and the inner wall of the second mounting plate (21) is fixedly connected to the second spring (8), and the other end of the second spring (8) is fixedly connected to the lower outer wall of the connecting sleeve (4). The inner side of the middle part of the clamping plate (7) is fixedly connected to the limiting sleeve (9), and the inner rod (5) is rotatably connected inside the limiting sleeve (9), and the inner rod (5) is fixedly connected in the inner cavity (10). The upper outer wall of the mounting column (2) is fixedly connected to the limiting ring (3), and the top end of the clamping plate (7) is engaged with the limiting ring (3).

2. The UAV mounting device according to claim 1, characterized in that: Connecting plates (12) are fixedly connected to both sides of the lower wall of the bottom plate (11), and a bidirectional threaded rod (13) is rotatably connected between the connecting plates (12) on both sides. At the same time, a positioning rod (14) is fixedly connected between the connecting plates (12) on both sides.

3. The UAV mounting device according to claim 2, characterized in that: Two pairs of vertical plates (15) are arranged at the bottom of the base plate (11), and one side of the vertical plate (15) is threadedly connected to the two ends of the outer wall of the bidirectional threaded rod (13).

4. The UAV mounting device according to claim 3, characterized in that: The vertical plate (15) on the other side is slidably connected to the outer wall of the positioning rod (14).

5. The UAV mounting device according to claim 4, characterized in that: A plurality of inner holes (19) are provided inside the vertical plate (15), and a latch (17) is provided outside the vertical plate (15), and the latch (17) is slidably connected inside the inner hole (19).

6. The UAV mounting device according to claim 5, characterized in that: A pair of vertical plates (16) are arranged at the bottom of the vertical plate (15), and the vertical plate (16) is in a U shape. At the same time, the two walls of the vertical plate (16) are respectively slidably connected to the vertical plate (15). At the same time, a pair of inner holes (18) are opened inside the vertical plate (16), and the inner hole (18) corresponds to the inner hole (19). At the same time, the pin (17) passes through the vertical plate (16) and extends to the outside of the vertical plate (15).

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