A mounting structure for a drone lighting lamp

Abstract

The utility model relates to an unmanned plane technical field especially relates to a kind of for unmanned plane lighting lamp's mounting structure, including mounting structure ontology, mounting structure ontology includes carbon tube, mounting plate, first quick clamp device and second quick clamp device, a plurality of lighting lamps are provided on carbon tube, lighting lamp is cooperatively provided with buckle structure, and is installed on carbon tube by buckle structure, carbon tube is cooperatively provided with first quick clamp device, is fixed on mounting plate by first quick clamp device, the two sides of mounting plate are provided with second quick clamp device, mounting plate cooperatively provided with rack, mounting plate is fixed by second quick clamp device with rack, the utility model a kind of for unmanned plane lighting lamp's mounting structure, by setting carbon tube collocation lighting lamp with buckle structure, realize lighting lamp convenient installation;Carbon tube is fixed on mounting plate using first quick clamp device, second quick clamp device makes mounting plate and rack firm connection, realizes the efficient, stable mounting of lighting lamp on unmanned plane.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a mounting structure for a UAV lighting device. Background Technology

[0002] With the continuous expansion of drone applications, the drone lighting mounting structure, as a key component to ensure the stable realization of lighting functions, is becoming increasingly important.

[0003] Traditional drone lighting mounting methods have several shortcomings. Firstly, installation has traditionally relied on conventional methods like bolt fastening, which is cumbersome, time-consuming, and labor-intensive. Furthermore, disassembly is difficult during subsequent maintenance and replacement, significantly reducing work efficiency. Secondly, this method requires high precision; improper installation can lead to loosening of the lights, affecting illumination, or even causing them to detach during drone flight due to vibration, posing a safety hazard.

[0004] On the other hand, traditional methods struggle to balance stability and convenience in connecting the mounting structure to the drone frame. Some connections are not secure enough, and during drone flight, factors such as airflow and vibration can cause swaying, affecting the stability of the lighting and consequently, the lighting quality. Conversely, some securely connected structures are difficult to disassemble and assemble, failing to meet the need for quick replacement or adjustment of the mounting structure. Utility Model Content

[0005] To address some of the problems existing in the prior art, this utility model provides a mounting structure for drone lighting. This mounting structure for drone lighting utilizes a carbon tube paired with a lighting lamp featuring a snap-fit ​​mechanism, enabling convenient installation of the lighting lamp. A first quick-clamp device secures the carbon tube to the mounting plate, while a second quick-clamp device firmly connects the mounting plate to the frame. The quick-clamp devices include an electric drive module and multi-joint electric grippers, enhancing operational flexibility and stability, thus achieving efficient and stable mounting of the lighting lamp on the drone.

[0006] To achieve the above objectives, this utility model provides a mounting structure for drone lighting, comprising a mounting structure body, the mounting structure body including a carbon tube, a mounting plate, a first quick-clamp device, and a second quick-clamp device. Multiple lighting lamps are mounted on the carbon tube, and each lighting lamp is fitted with a snap-fit ​​structure and mounted on the carbon tube via the snap-fit ​​structure. The carbon tube is fitted with the first quick-clamp device and fixed to the mounting plate via the first quick-clamp device. Second quick-clamp devices are provided on both sides of the mounting plate. The mounting plate is fitted with a frame, and the mounting plate is fixed to the frame via the second quick-clamp devices.

[0007] As a further improvement of this utility model, in order to make the connection between the lighting lamp and the carbon tube more secure, reduce the damage to the connection part caused by external impact, and at the same time ensure the tightness of the connection, prevent the lighting lamp from loosening due to vibration during the flight of the UAV, and improve the stability and durability of the mounting structure, the buckle structure includes an elastic buckle component that is connected to the lighting lamp. The elastic buckle component is fitted with a buckle base. The buckle base has a mating hole at the top center, which extends inward by a certain distance. The buckle base has slots on both sides that cooperate with the elastic buckle component.

[0008] As a further improvement of this utility model, in order to make the connection between the elastic buckle assembly and the buckle base more precise and stable, prevent the lighting lamp from moving in the horizontal direction, improve the safety of the lighting lamp mounting, further strengthen the connection strength between the lighting lamp and the carbon tube, and ensure that the lighting lamp can work stably under various harsh conditions, the elastic buckle assembly includes a support plate. One side of the support plate is connected to the lighting lamp, and the other side of the support plate is provided with a connecting buckle. The connecting buckle is configured to cooperate with the buckle groove. A docking shaft is provided between the two connecting buckles and is configured to cooperate with the docking hole.

[0009] As a further improvement of this utility model, in order to realize the automated installation and disassembly of the mounting structure, improve work efficiency and operational accuracy, and adapt to the needs of large-scale production and maintenance, the first quick clamp device includes a quick clamp body, the quick clamp base is set on the mounting plate, the top of the quick clamp body is provided with a connecting seat, and the quick clamp body is connected and fixed to the mounting plate through the connecting seat. The quick clamp body is internally integrated with an electric drive module, and the quick clamp body is externally provided with electric grippers distributed on both sides of the top of the quick clamp body.

[0010] As a further improvement of this utility model, in order to enhance the flexibility and adaptability of the electric gripper and enable it to better cope with the changes of carbon tubes under different working conditions and ensure the stability of the mounting structure, the electric gripper is symmetrically installed on both sides of the upper part of the quick clamp body. Each electric gripper has multiple joint structures. The electric gripper includes a gripper seat disposed on the quick clamp body. At least two movable joints are connected and disposed above the gripper seat. A bearing is disposed at the connection of each movable joint.

[0011] As a further improvement of this utility model, in order to enhance the friction between the electric gripper and the carbon tube, improve the clamping stability, and ensure the safety of the lighting mounting structure under extreme working conditions, the end of the movable joint is designed with a textured mechanism.

[0012] As a further improvement of this utility model, in order to make the connection between the mounting plate and the frame more secure and reliable, and to prevent the mounting plate from loosening due to vibration during the flight of the UAV, the connection method between the mounting plate and the frame is optimized to improve the stability and reliability of the connection, while ensuring the convenience of operation and reducing maintenance costs. The second quick-clamp device includes a quick-clamp support seat set at the bottom of the mounting plate. A clamping arm is connected to the other side of the quick-clamp support seat. An anti-slip rubber pad is provided at the inner end of the clamping arm. The clamping arm is locked by screws.

[0013] When this invention is in operation, the second quick-clamp device is activated. The quick-clamp support at the bottom of the mounting plate is connected to the clamping arm. The mounting plate is brought close to the corresponding position on the drone frame, aligning the clamping arm with the frame. The anti-slip rubber pad at the inner end of the clamping arm increases friction. After adjusting the position, the clamping arm is locked to the frame with screws. In this way, the mounting plate is tightly connected to the frame via the second quick-clamp device.

[0014] The quick-clamp body is connected and fixed to the quick-clamp base on the mounting plate via a connecting seat at the top. The internal electric drive module activates, providing power to the external electric grippers. The electric grippers are symmetrically distributed on both sides of the top of the quick-clamp body, and the movable joints on their gripper seats begin to move under electric drive. Bearings at the joint connections ensure smooth movement, and the multiple joint structures allow the electric grippers to flexibly adjust their posture, precisely clamping the carbon nanotube and firmly fixing it to the mounting plate.

[0015] One side of the carrier plate of the flexible snap-fit ​​assembly is connected to the lighting lamp, while the connecting snap-fit ​​on the other side and the central mating shaft are ready for installation. Position the lighting lamp close to the corresponding snap-fit ​​base on the carbon tube, ensuring the mating shaft on the carrier plate is precisely inserted into the mating hole at the center of the top of the snap-fit ​​base, while simultaneously engaging the connecting snap-fit ​​into the slots on both sides of the snap-fit ​​base. The elasticity of the flexible snap-fit ​​assembly ensures a tight and secure connection, guaranteeing the lighting lamp is firmly installed on the carbon tube.

[0016] The beneficial effects of this utility model are as follows:

[0017] The lighting fixtures are easy and secure to install: the carrier plate of the elastic buckle assembly connects to the lighting fixture, the docking shaft is inserted into the docking hole of the buckle base, and the connecting buckle is embedded in the slot. The elasticity makes the connection tight, allowing multiple lighting fixtures to be installed quickly to meet diverse lighting needs, and they are not easy to loosen during flight.

[0018] Precise and efficient carbon nanotube fixing: The quick-clamp body is fixed to the quick-clamp base on the mounting plate via a connecting seat, and the internal electric drive module supplies power to the electric grippers. The multi-joint structure and bearings of the electric grippers allow them to flexibly adjust their posture and precisely clamp the carbon nanotubes, achieving rapid and stable fixing, thus improving installation efficiency and accuracy.

[0019] Reliable and durable mounting plate connection: The second quick-clamp device ensures a stable connection between the mounting plate and the frame. The quick-clamp support connects to the clamping arm, and the anti-slip rubber pad on the inner side of the clamping arm increases friction. The screw locking further ensures a secure connection. During drone flight, it effectively resists vibration and external forces, preventing the mounting plate from loosening and ensuring stable operation of the lighting system. Attached Figure Description

[0020] To facilitate understanding by those skilled in the art, the present invention will be further described below with reference to the accompanying drawings:

[0021] Figure 1 This is a structural diagram of the present invention.

[0022] Figure 2 This is a structural diagram of the snap-fit ​​structure.

[0023] Figure 3 This is a top structural diagram of the snap-fit ​​base.

[0024] Figure 4 This is a side view of the snap-fit ​​base.

[0025] Figure 5 This is a structural diagram of the elastic snap-fit ​​assembly.

[0026] Figure 6 This is a structural diagram of the first quick-clamping device.

[0027] Figure 7 This is a structural diagram of the second quick-clamping device.

[0028] The components are as follows: 1. Carbon tube, 2. Mounting plate, 3. First quick clamp device, 4. Second quick clamp device, 5. Snap-on structure, 6. Frame, 7. Elastic snap-on assembly, 8. Snap-on base, 9. Docking hole, 10. Slot, 11. Bearing plate, 12. Connecting snap, 13. Docking shaft, 14. Quick clamp body, 15. Connecting seat, 16. Electric gripper, 17. Gripper seat, 18. Movable joint, 19. Bearing, 20. Texture mechanism, 21. Quick clamp support seat, 22. Grip arm, 23. Anti-slip rubber pad. Detailed Implementation

[0029] To enable those skilled in the art to better understand the technical solutions in this application, the following description is provided in conjunction with the appendix. Figure 1-7 The present invention will be further described below. The following embodiments are only used to illustrate the technical solution of the present invention more clearly, and should not be used to limit the protection scope of the present invention.

[0030] like Figure 1-7The diagram shows a mounting structure for a drone lighting device, comprising a mounting structure body, which includes a carbon fiber tube 1, a mounting plate 2, a first quick-clamp device 3, and a second quick-clamp device 4. Multiple lighting lamps are mounted on the carbon fiber tube 1, and each lighting lamp is fitted with a snap-fit ​​structure 5 and mounted on the carbon fiber tube 1. The carbon fiber tube 1 is fitted with the first quick-clamp device 3 and fixed to the mounting plate 2. Second quick-clamp devices 4 are located on both sides of the mounting plate 2. A frame 6 is mounted on the mounting plate 2, and the mounting plate 2 is fixed to the frame 6 via the second quick-clamp devices 4.

[0031] The buckle structure 5 includes an elastic buckle component 7 that is connected to the lighting lamp. The elastic buckle component is fitted with a buckle base 8. The buckle base 8 has a docking hole 9 at the top center, which extends inward by a certain distance. The buckle base 8 has slots 10 on both sides that cooperate with the elastic buckle component 7.

[0032] The elastic buckle assembly 7 includes a support plate 11. One side of the support plate 11 is connected to a lighting lamp, and the other side of the support plate 11 is provided with a connecting buckle 12. The connecting buckle 12 is configured to cooperate with the slot 10. A docking shaft 13 is provided between the two connecting buckles 12 and is configured to cooperate with the docking hole 9.

[0033] The first quick clamp device 3 includes a quick clamp body 14, the quick clamp base is mounted on the mounting plate 2, the top of the quick clamp body 14 is provided with a connecting seat 15, and the quick clamp body 14 is connected and fixed to the mounting plate 2 through the connecting seat 15. The quick clamp body 14 is internally integrated with an electric drive module, and the quick clamp body 14 is externally provided with electric grippers 16, which are distributed on both sides of the top of the quick clamp body 14.

[0034] The electric grippers 16 are symmetrically mounted on the upper sides of the quick clamp body 14. Each electric gripper 16 has multiple joint structures. Each electric gripper 16 includes a gripper seat 17 disposed on the quick clamp body 14. At least two movable joints 18 are connected and disposed on the upper side of the gripper seat 17. Each movable joint 18 is provided with a bearing 19 at the connection point of the joint.

[0035] The end of the movable joint 18 is designed with a texture mechanism 20.

[0036] The second quick clamp device 4 includes a quick clamp support 21 disposed at the bottom of the mounting plate 2. A clamp arm 22 is connected to the other side of the quick clamp support 21. An anti-slip rubber pad 23 is provided at the inner end of the clamp arm 22. The clamp arm 22 is locked by screws.

[0037] When this invention is in operation, the second quick-clamp device 4 is activated. The quick-clamp support 21 at the bottom of the mounting plate 2 is connected to the clamping arm 22. The mounting plate 2 is brought close to the corresponding position on the drone frame 6, aligning the clamping arm 22 with the frame 6. The anti-slip rubber pad 23 at the inner end of the clamping arm 22 increases friction. After adjusting the position, the clamping arm 22 is locked onto the frame 6 with screws. In this way, the mounting plate 2 is tightly connected to the frame 6 through the second quick-clamp device 4.

[0038] The quick-clamp body 14 is connected and fixed to the quick-clamp base on the mounting plate 2 via the top connecting seat 15. The internal electric drive module is activated to provide power to the external electric grippers 16. The electric grippers 16 are symmetrically distributed on both sides of the top of the quick-clamp body 14, and the movable joints 18 on their gripper seats 17 begin to move under electric drive. The bearings 19 at the connection of the movable joints 18 ensure smooth movement, and the multiple joint structures allow the electric grippers 16 to flexibly adjust their posture, accurately clamp the carbon tube 1, and firmly fix it on the mounting plate 2.

[0039] One side of the support plate 11 of the elastic snap-fit ​​assembly 7 is connected to the lighting lamp, while the connecting snap 12 on the other side and the intermediate docking shaft 13 are ready for installation. The lighting lamp is brought close to the corresponding snap-fit ​​base 8 on the carbon tube 1, ensuring that the docking shaft 13 on the support plate 11 is precisely inserted into the docking hole 9 at the top center of the snap-fit ​​base 8, while simultaneously allowing the connecting snap 12 to engage with the slots 10 on both sides of the snap-fit ​​base 8. The elasticity of the elastic snap-fit ​​assembly 7 ensures a tight and secure connection, guaranteeing that the lighting lamp is firmly installed on the carbon tube 1.

[0040] This utility model is not limited to the above embodiments. Based on the technical solutions disclosed in this utility model, those skilled in the art can make some substitutions and modifications to some of the technical features without creative labor, and these substitutions and modifications are all within the protection scope of this utility model.

Claims

1. A mounting structure for a drone light, comprising a mounting structure body, characterized by, The mounting structure includes a carbon tube (1), a mounting plate (2), a first quick-clamp device (3), and a second quick-clamp device (4). The carbon tube (1) is provided with multiple lights, and the lights are equipped with a snap-fit ​​structure (5) and are installed on the carbon tube (1) through the snap-fit ​​structure (5). The carbon tube (1) is equipped with the first quick-clamp device (3) and is fixed on the mounting plate (2) through the first quick-clamp device (3). The second quick-clamp device (4) is provided on both sides of the mounting plate (2). The mounting plate (2) is equipped with a frame (6), and the mounting plate (2) is fixed to the frame (6) through the second quick-clamp device (4).

2. The mounting structure for a drone lighting device according to claim 1, characterized in that, The buckle structure (5) includes an elastic buckle component (7) that is connected to the lighting lamp. The elastic buckle component is fitted with a buckle base (8). The buckle base (8) has a docking hole (9) at the top center. The docking hole (9) extends inward a certain distance. The buckle base (8) has slots (10) on both sides that cooperate with the elastic buckle component (7).

3. The mounting structure for a drone lighting device according to claim 2, characterized in that, The elastic buckle assembly (7) includes a support plate (11), one side of which is connected to a lighting lamp, and the other side of which is provided with a connecting buckle (12). The connecting buckle (12) is configured to cooperate with the slot (10). A docking shaft (13) is provided between the two connecting buckles (12) and is configured to cooperate with the docking hole (9).

4. The mounting structure for a drone lighting device according to claim 1, characterized in that, The first quick clamp device (3) includes a quick clamp body (14), the quick clamp base is set on the mounting plate (2), the top of the quick clamp body (14) is provided with a connecting seat (15), and the quick clamp body (14) is connected and fixed to the mounting plate (2) through the connecting seat (15). The quick clamp body (14) is internally integrated with an electric drive module, and the quick clamp body (14) is externally provided with electric grippers (16), which are distributed on both sides of the top of the quick clamp body (14).

5. The mounting structure for a drone lighting lamp of claim 1, wherein, The electric grippers (16) are symmetrically mounted on the upper sides of the quick clamp body (14). Each electric gripper (16) has multiple joint structures. The electric gripper (16) includes a gripper seat (17) disposed on the quick clamp body (14). At least two movable joints (18) are connected and disposed above the gripper seat (17). A bearing (19) is disposed at the connection of each movable joint (18).

6. The mounting structure for a drone lighting device according to claim 5, characterized in that, The end of the movable joint (18) is designed with a textured mechanism (20).

7. The mounting structure for a drone lighting device according to claim 1, characterized in that, The second quick clamp device (4) includes a quick clamp support (21) disposed at the bottom of the mounting plate (2), and a clamp arm (22) is connected to the other side of the quick clamp support (21). An anti-slip rubber pad (23) is provided at the inner end of the clamp arm (22), and the clamp arm (22) is locked by screws.

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