A mounting device for a lighting drone

Abstract

The utility model provides a kind of lighting unmanned plane's mounting device, it is related to unmanned plane accessory technical field, and it includes: installation platform, installation platform side is equipped with locking assembly, locking assembly at least includes locking collar and cushion block, locking assembly is used to connect with unmanned plane buckle connection upper;Suspension assembly, suspension assembly is equipped in installation platform bottom, and suspension assembly at least includes suspension rod and suspension ring.This kind of device can be flexibly adapted to the connecting part of different specifications unmanned plane by locking assembly, simplifies installation and dismounting process, avoids the limitation that traditional device can only match specific model unmanned plane;At the same time, suspension assembly integrates effective buffer mechanism, can significantly weaken the swing amplitude of lighting equipment when unmanned plane flight steering, encounters airflow jolt, avoids lighting light spot offset, guarantees lighting operation effect, reduces the interference of material swing to unmanned plane flight attitude, improves overall mounting stability and flight safety.

Description

Technical Field

[0001] This utility model relates to the field of drone accessories technology, specifically a mounting device for a lighting drone. Background Technology

[0002] With the rapid iteration of drone technology, its application scenarios have expanded from traditional aerial photography to diverse fields such as emergency rescue, nighttime construction, and power line inspection. Lighting drones, as specialized operational equipment, play an irreplaceable role in complex environments without fixed lighting facilities due to their flexibility and mobility. The mounting device, as a core component of lighting drones, directly undertakes the functions of fixing, bearing weight, and stabilizing the lighting equipment. Its performance not only affects the accuracy of lighting operations but also influences the safety and reliability of the drone's flight. Especially in emergency scenarios such as disaster relief, the mounting device needs to achieve rapid connection with the drone and ensure the stability of the lighting equipment in turbulent high-altitude environments to guarantee continuous lighting coverage in the rescue area.

[0003] Existing lighting drone mounting devices mostly use a single mechanical fastening or bolt fixing structure, which has obvious functional defects: On the one hand, the connection compatibility is poor. Most devices can only match specific drone models. When facing drones of different specifications, it is difficult to achieve a firm fixation. Moreover, the installation and disassembly process is cumbersome and cannot meet the needs of rapid deployment in emergency scenarios. On the other hand, the anti-shaking ability is insufficient. Traditional suspension structures lack an effective buffer mechanism. The lighting equipment is prone to violent shaking when the drone turns or encounters turbulence. This not only causes the lighting spot to shift and affects the operation effect, but may also interfere with the drone's flight attitude due to instability of the center of gravity, and even cause the safety hazard of the mounted materials falling off. Utility Model Content

[0004] The present invention aims to address the shortcomings of the prior art by providing a mounting device for lighting drones, thereby improving the problems of poor installation convenience and poor mounting stability of existing devices.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a mounting device for a lighting drone, comprising: a mounting platform, wherein a locking component is provided on one side of the mounting platform, the locking component including at least a locking collar and a pad, the locking component being used for fastening and connecting with the drone; and a suspension component, wherein the suspension component is located at the bottom of the mounting platform, the suspension component including at least a suspension rod and a suspension ring, the suspension component being used for suspending materials and reducing the swaying of the materials.

[0006] Preferably, the locking assembly includes: a locking collar disposed on the top of one side of the mounting platform; a plurality of pads disposed on the locking collar and the inner wall of the mounting platform; a power chamber disposed inside the mounting platform and the locking collar, one side of the power chamber being connected to a power pipe, and the power pipe communicating with the pads; and adjusting bolts disposed on both sides of the top of the mounting platform, the adjusting bolts being threadedly engaged with the locking collar.

[0007] Preferably, the suspension assembly includes: a suspension rod disposed at the bottom of the mounting platform; and a suspension ring disposed at the bottom of the suspension rod, wherein the bottom of the suspension ring is provided with a mounting hole.

[0008] Preferably, the plurality of pads are arranged at equal intervals.

[0009] Preferably, the bottom of the pad is provided with multiple anti-slip strips, and the multiple anti-slip strips are made of rubber material.

[0010] Preferably, a damping sleeve is provided between the suspension ring and the suspension rod, the damping sleeve is filled with a damping medium, a damping cavity is provided at one end of the suspension ring near the suspension rod, damping rods are provided on both sides of the suspension rod, a damping plate is provided at the end of the damping rod, and the damping plate is slidably connected to the inside of the damping cavity.

[0011] Preferably, the damping plate has a connecting pipe inside, which connects the damping cavities at both ends of the damping plate for the flow of damping medium, and the connecting pipe is arranged in an "S" shape.

[0012] This utility model provides a mounting device for a lighting drone, which has the following beneficial effects: The advantages of this invention lie in its optimized structural design of the locking component, which effectively solves the problems of poor compatibility and cumbersome installation and disassembly in existing devices. The locking component can flexibly adapt to the connection parts of drones of different specifications, simplifying the installation and disassembly process and avoiding the limitation of traditional devices that can only match specific drone models. At the same time, the suspension component integrates an effective buffering mechanism, which can significantly reduce the swaying amplitude of the lighting equipment when the drone turns or encounters turbulence, prevent the lighting spot from shifting, ensure the lighting effect, reduce the interference of material swaying on the drone's flight attitude, and improve the overall mounting stability and flight safety. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of the overall structure of this utility model.

[0014] Figure 2 This is a cross-sectional view of the overall structure of this utility model.

[0015] Figure 3This is a schematic diagram of the suspension assembly structure of this utility model.

[0016] Figure 4 This is a schematic diagram of the pad structure of this utility model.

[0017] Figure 5 For the present utility model Figure 2 Enlarged schematic diagram of the structure at point A in the diagram.

[0018] Figure 1-5 In the middle: 100-mounting platform; 200-locking assembly; 210-locking collar; 211-power bag; 212-power pipe; 220-pad; 221-anti-slip pad; 230-adjusting bolt; 300-suspension assembly; 310-suspension rod; 311-suspension ring; 312-mounting hole; 320-damping sleeve; 321-damping cavity; 330-damping rod; 331-damping plate; 332-connecting pipe. Detailed Implementation The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of this application without creative effort are within the scope of protection of this application.

[0019] The following disclosure provides many different embodiments or examples for implementing different structures of this application. To simplify the disclosure, specific examples of components and arrangements are described below. Of course, these are merely examples and are not intended to limit the scope of this application. Furthermore, reference numerals and / or letters may be repeated in different examples; such repetition is for simplification and clarity and does not in itself indicate a relationship between the various embodiments and / or arrangements discussed. In addition, various specific examples of processes and materials are provided in this application, but those skilled in the art will recognize the application of other processes and / or the use of other materials.

[0020] This application provides a mounting device for a lighting drone. This mounting device effectively solves the problems of poor compatibility and cumbersome installation and disassembly in existing devices by optimizing the structural design of the locking component. The locking component can flexibly adapt to the connection parts of drones of different specifications, simplifying the installation and disassembly process and avoiding the limitation of traditional devices that can only match specific drone models. Simultaneously, the suspension component integrates an effective buffering mechanism, which can significantly reduce the swaying amplitude of the lighting equipment when the drone turns or encounters turbulence, preventing the lighting spot from shifting, ensuring the lighting effect, reducing the interference of material swaying on the drone's flight attitude, and improving the overall mounting stability and flight safety. The mounting device for this lighting drone will be described in detail below. It should be noted that the order of description of the following embodiments is not intended to limit the preferred order of embodiments.

[0021] The present application will now be described in detail with reference to the accompanying drawings and specific embodiments.

[0022] A mounting device for a lighting drone includes: a mounting platform 100, a locking component 200 on one side of the mounting platform 100, the locking component 200 including at least a locking collar 210 and a pad 220, the locking component 200 being used for fastening and connecting with the drone; and a suspension component 300, the suspension component 300 being disposed at the bottom of the mounting platform 100, the suspension component 300 including at least a suspension rod 310 and a suspension ring 311, the suspension component 300 being used for suspending materials and reducing the swaying of the materials; First, the locking component 200 on one side of the mounting platform 100 is used to connect with the drone. Specifically, the locking ring 210 in the locking component 200 and the pad 220 are used to complete the fastening and fixing. After the mounting platform 100 and the drone are stably connected, the materials to be mounted, such as lighting equipment, are suspended on the suspension component 300 at the bottom of the mounting platform 100. The suspension rod 310 of the suspension component 300 supports the weight of the materials, and the suspension ring 311 is used to attach the materials. At the same time, the structural characteristics of the suspension component 300 can reduce the swaying amplitude of the materials during the flight of the drone. By combining the locking collar 210 and the pad 220 of the locking component 200, a reliable connection between the mounting platform 100 and the UAV is achieved, providing a stable foundation for mounting. The suspension rod 310 and the suspension ring 311 of the suspension component 300 not only meet the suspension requirements of the material, but also specifically reduce swaying. The core structure is simple and practical, effectively adapting to the basic mounting scenarios of lighting UAVs and ensuring the basic stability of the material during flight.

[0023] The locking assembly 200 includes: a locking collar 210 located on the top of one side of the mounting platform 100; multiple pads 220 located on the inner wall of the locking collar 210 and the mounting platform 100; a power chamber 211 located inside the mounting platform 100 and the locking collar 210, with a power pipe 212 connected to one side of the power chamber 211 and communicating with the pads 220; and adjusting bolts 230 located on both sides of the top of the mounting platform 100, with the adjusting bolts 230 threadedly engaged with the locking collar 210. When connecting the drone, first align the locking collar 210 on the top side of the mounting platform 100 with the connection part of the drone and put it on; then rotate the adjusting bolts 230 on both sides of the top of the mounting platform 100. Since the adjusting bolts 230 and the locking collar 210 are threadedly engaged, the locking collar 210 can be finely adjusted during the rotation, so that the locking collar 210 and the connection part of the drone are initially in contact; then, power source such as gas or liquid is input into the power bag 211 inside the mounting platform 100 and the locking collar 210 through the power pipe 212. After the power bag 211 expands, the pressure is transmitted through the power pipe 212 to the locking collar 210 and multiple pads 220 on the inner wall of the mounting platform 100, pushing the pads 220 to fit tightly against the surface of the drone, completing the double locking; The threaded engagement structure of the adjusting bolt 230 enables precise fine-tuning of the locking collar 210, improving compatibility with drones of different specifications; the linkage design of the power bag 211, power tube 212 and pad 220 allows the pad 220 to fit evenly against the drone surface, enhancing the locking firmness; the multiple locking mechanisms prevent the mounting platform 100 from loosening during drone flight, significantly improving connection reliability compared to a single snap-fit ​​structure, while the pad 220 prevents rigid damage to the drone surface from the locking components.

[0024] The multiple pads 220 are evenly distributed. When the power bag 211 transmits pressure to the pads 220 through the power pipe 212, the multiple equally distributed pads 220 will be stressed simultaneously and evenly adhere to the surface of the connection part of the UAV, forming a surrounding support and lock. The evenly distributed pads 220 make the stress on the connection part of the UAV more balanced, effectively avoiding deformation or damage to the surface of the UAV caused by local pressure concentration. At the same time, the uniform stress distribution makes the locking component 200 fit better with the UAV, reduces the connection gap, further improves the stability of the connection between the mounting platform 100 and the UAV, and reduces the impact of flight vibration on the connection structure.

[0025] The pad 220 has multiple anti-slip strips 221 at its bottom, and these anti-slip strips 221 are made of rubber. During the locking assembly 200 and the drone are fastened together, the multiple anti-slip strips 221 at the bottom of the pad 220 will make close contact with the surface of the drone connection part. The anti-slip strips 221 made of rubber will undergo a certain deformation, which will enhance the engagement with the contact surface and reduce the possibility of relative slippage.

[0026] The suspension assembly 300 includes: a suspension rod 310 located at the bottom of the mounting platform 100; a suspension ring 311 located at the bottom of the suspension rod 310, with a mounting hole 312 at the bottom of the suspension ring 311; materials such as lighting equipment are fixedly installed through the mounting hole 312 at the bottom of the suspension ring 311, and the supporting force transmitted by the mounting platform 100 is transmitted to the suspension ring 311 through the suspension rod 310, so that the suspension ring 311 directly bears the weight of the materials, thereby realizing the indirect connection between the materials and the drone; A damping sleeve 320 is provided between the suspension ring 311 and the suspension rod 310. The damping sleeve 320 is filled with a damping medium. A damping cavity 321 is provided at one end of the suspension ring 311 near the suspension rod 310. Damping rods 330 are provided on both sides of the suspension rod 310. A damping plate 331 is provided at the end of the damping rod 330. The damping plate 331 is slidably connected to the inside of the damping cavity 321. When the drone experiences turbulence or turns during flight, causing the loaded material to sway, the force of the material will drive the suspension ring 311 to move. The damping cavity 321 at the end of the suspension ring 311 near the suspension rod 310 will move synchronously with the suspension ring 311. At this time, the damping plates 331 at the ends of the damping rods 330 on both sides of the suspension rod 310 will slide in the damping medium inside the damping sleeve 320. The damping medium generates resistance to the sliding of the damping plates 331, thereby consuming the energy of the material swaying and slowing down the swaying speed.

[0027] The damping plate 331 has a connecting pipe 332 inside, which connects the damping cavities 321 at both ends of the damping plate 331 for the flow of damping medium, and the connecting pipe 332 is arranged in an "S" shape. When the damping plate 331 slides in the damping cavity 321 as the material sways, the damping medium in the damping cavity 321 needs to flow through the connecting pipe 332 inside the damping plate 331 at both ends of the damping plate 331. Since the connecting pipe 332 has an "S" shaped structure, it prolongs the flow path of the damping medium and increases the resistance to the flow of the medium, which further limits the sliding speed of the damping plate 331.

[0028] In the above embodiments, the descriptions of each embodiment have different focuses. For parts not described in detail in a certain embodiment, please refer to the relevant descriptions in other embodiments.

[0029] The above provides a detailed description of a lighting drone mounting device provided in the embodiments of this application. Specific examples have been used to illustrate the principles and implementation methods of this application. The description of the above embodiments is only for the purpose of helping to understand the technical solutions and core ideas of this application. Those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. These modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of this application.

Claims

1. A mounting device for a lighting drone, characterized in that, include: Mounting platform (100), one side of which is provided with locking component (200), the locking component (200) includes at least a locking collar (210) and a pad (220), the locking component (200) is used for fastening connection with the drone; A suspension assembly (300) is disposed at the bottom of the mounting platform (100). The suspension assembly (300) includes at least a suspension rod (310) and a suspension ring (311). The suspension assembly (300) is used to suspend materials and reduce the swaying of the materials.

2. The mounting device for the lighting drone according to claim 1, characterized in that, The locking component (200) includes: A locking collar (210) is provided on the top of one side of the mounting platform (100). Multiple pads (220) are provided on the inner walls of the locking collar (210) and the mounting platform (100). A power bag (211) is provided inside the mounting platform (100) and the locking collar (210). A power pipe (212) is connected to one side of the power bag (211), and the power pipe (212) is in communication with the pad (220). Adjusting bolts (230) are provided on both sides of the top of the mounting platform (100), and the adjusting bolts (230) are threadedly engaged with the locking collar (210).

3. The mounting device for the lighting drone according to claim 1, characterized in that, The suspension assembly (300) includes: A suspension rod (310) is provided at the bottom of the mounting platform (100); A suspension ring (311) is provided at the bottom of the suspension rod (310), and the bottom of the suspension ring (311) is provided with a mounting hole (312).

4. The mounting device for the lighting drone according to claim 2, characterized in that, The plurality of pads (220) are arranged at equal intervals.

5. The mounting device for the lighting drone according to claim 2, characterized in that, The bottom of the pad (220) is provided with multiple anti-slip pad strips (221), and the multiple anti-slip pad strips (221) are made of rubber material.

6. The mounting device for the lighting drone according to claim 3, characterized in that, A damping sleeve (320) is provided between the suspension ring (311) and the suspension rod (310). The damping sleeve (320) is filled with a damping medium. A damping cavity (321) is provided at one end of the suspension ring (311) near the suspension rod (310). Damping rods (330) are provided on both sides of the suspension rod (310). A damping plate (331) is provided at the end of the damping rod (330). The damping plate (331) is slidably connected to the inside of the damping cavity (321).

7. The mounting device for the lighting drone according to claim 6, characterized in that, The damping plate (331) has a connecting pipe (332) inside, which connects the damping cavities (321) at both ends of the damping plate (331) for the flow of damping medium, and the connecting pipe (332) is arranged in an "S" shape.

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