High-altitude lighting device suitable for field operation
By designing support legs, mounting structures, and multi-angle lighting panels in the high-altitude lighting device, the problem of difficult disassembly and assembly of existing devices has been solved, enabling rapid connection and flexible lighting.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CHENGDU ZHONGDE INTELLIGENT TECH GRP CO LTD
- Filing Date
- 2025-05-09
- Publication Date
- 2026-04-28
AI Technical Summary
Existing high-altitude lighting devices suitable for field operations cannot quickly detach and install drones and lighting control cabinets.
A device was designed that includes a drone, support legs, a lighting control box, a mounting structure, side lighting panels, and a bottom lighting panel. The mounting structure enables quick connection between the drone and the lighting control box, the side lighting panels and the bottom lighting panel expand the illumination range, and the illumination angle is adjusted by a motor.
It enables rapid assembly and disassembly of drones and lighting control cabinets, expands the lighting range, and improves the flexibility and efficiency of lighting devices.
Smart Images

Figure CN224171190U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of high-altitude lighting technology, specifically a high-altitude lighting device suitable for field operations. Background Technology
[0002] Combining drones with lighting equipment makes them suitable for field operations, allowing the lighting equipment to be suspended high in the air for high-altitude illumination, thus expanding the illumination range. The drones carry batteries with ultra-long battery life, extending the illumination time.
[0003] Chinese utility model patent CN207917172U discloses a high-altitude lighting drone, comprising a fuselage, landing gear, shooting device, and lighting device. The landing gear is fixed directly below the fuselage, and the shooting device and lighting device are both located inside the landing gear below the fuselage. The brightness and focal length of the lighting device are adjustable. The telescopic lens of the lighting device can be moved back and forth along the direction of the light by a cylinder to adjust to the desired focal length. In addition, a brightness adjuster is provided between the light source and the power supply, which can adjust the brightness of the lighting while adjusting the focal length, enabling the drone to obtain a wider field of view at different distances, reducing the exposure rate when shooting at close range. The structure is simple, the cost is low, and the practicality is high.
[0004] Based on existing solutions and actual production and processing, the existing high-altitude lighting devices suitable for field operations cannot quickly assemble and disassemble drones and lighting control boxes. Therefore, we propose a high-altitude lighting device suitable for field operations to solve the problems mentioned above. Utility Model Content
[0005] The purpose of this invention is to provide a high-altitude lighting device suitable for field operations, in order to solve the problem mentioned in the background art that existing high-altitude lighting devices suitable for field operations cannot quickly assemble and disassemble drones and lighting control boxes.
[0006] To achieve the above objectives, this utility model provides the following technical solution: a high-altitude lighting device suitable for field operations, comprising a drone, a lighting control box, side lighting panels, and bottom lighting panels:
[0007] The drone has integrated support legs installed on both the front and rear sides of its bottom.
[0008] The lighting control box is fixedly connected to the support legs via an installation structure. A side plate is fixed to the side of the lighting control box. A side lighting plate is installed on the inner side of the side plate. The outer side of the side lighting plate is fixedly connected to the output end of the second motor. The second motor is fixed to the side plate. A bottom lighting plate is installed on the lower surface of the lighting control box.
[0009] Preferably, the mounting structure includes a first mounting box, a second mounting box, a first motor, a reverse lead screw, a connecting frame, and a housing. The first mounting box is fixed to the front end of the upper surface of the lighting control box, and the second mounting box is fixed to the rear end of the upper surface of the lighting control box. The first motor is fixed to the right side of the first mounting box, and the output end of the first motor is fixed to the reverse lead screw. The outer end of the reverse lead screw is threadedly connected to the connecting frame. The end of the reverse lead screw away from the first motor is rotatably mounted on the first mounting box, and the top end of the connecting frame is fixed to the housing.
[0010] Preferably, the rear end of the first mounting box and the front end of the second mounting box are both provided with sliding grooves, and the connecting frame forms a sliding structure with the rear end of the first mounting box and the second mounting box through a reverse lead screw.
[0011] Preferably, the housing is symmetrically arranged about the center line of the first mounting box, and the housing is connected to the support leg by a snap-fit connection.
[0012] Preferably, the side lighting panel is rotatably mounted on the side panel.
[0013] Preferably, the side lighting panels are installed on the front, rear, left, and right sides of the lighting control box.
[0014] Compared with the prior art, the beneficial effects of this utility model are: the high-altitude lighting device suitable for field operations has an installation structure that allows for quick assembly and disassembly of the drone and the lighting control box, expands the illumination range by utilizing the side lighting panels on the front, back, left, and right sides as well as the bottom lighting panel, and facilitates adjustment of the illumination angle of the side lighting panels;
[0015] 1. The drone has integrated support legs installed on both the front and rear sides of its bottom. The lighting control box is fixedly connected to the support legs through the mounting structure. After aligning the drone with the lighting control box, the first motor drives the reverse screw to rotate clockwise. The connecting bracket, which is threaded to the reverse screw, moves inward, thereby moving the housing inward so that the housing fits over the outer end of the support leg, enabling quick connection between the drone and the lighting control box.
[0016] 2. When the drone is in motion, the lighting control box is suspended in the air, and the lighting is provided by the side lighting panels and bottom lighting panels on the lighting control box, which is suitable for field operations;
[0017] 3. Side lighting panels are installed on the front, back, left, and right sides of the lighting control box, and the illumination range is expanded by using the side lighting panels on the front, back, left, and right sides as well as the bottom lighting panel.
[0018] The side lighting panels are rotatably mounted on the side plate, and the outer side of the side lighting panels is fixedly connected to the output end of the second motor. The second motor facilitates the control of the illumination angle of each side lighting panel. Attached Figure Description
[0019] Figure 1 This is a schematic diagram of the first axial side structure of the present invention;
[0020] Figure 2 This is a cross-sectional view of the first and second mounting boxes of this utility model;
[0021] Figure 3 This is a cross-sectional view of the first mounting box of this utility model;
[0022] Figure 4 This is a schematic diagram of the second axial side structure of the present invention;
[0023] Figure 5 This is a schematic diagram of the third axial side structure of this utility model.
[0024] In the diagram: 1. Drone; 2. Support leg; 3. Lighting control box; 4. First mounting box; 5. Second mounting box; 6. First motor; 7. Reverse lead screw; 8. Connecting frame; 9. Housing; 10. Side plate; 11. Second motor; 12. Side lighting plate; 13. Bottom lighting plate. Detailed Implementation
[0025] 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.
[0026] Please see Figures 1-5 Existing high-altitude lighting devices suitable for field operations cannot quickly detach and assemble the drone 1 and the lighting control box 3. To solve this technical problem, this embodiment discloses the following technical content;
[0027] A high-altitude lighting device suitable for field operations includes a drone 1, a support leg 2, a lighting control box 3, a first mounting box 4, a second mounting box 5, a first motor 6, a reverse lead screw 7, a connecting frame 8, a housing 9, a side plate 10, a second motor 11, a side lighting plate 12, and a bottom lighting plate 13.
[0028] The drone 1 has integrated support legs 2 mounted on both the front and rear sides of its bottom. The lighting control housing 3 is fixedly connected to the support legs 2 via a mounting structure. Figures 1-3 and Figure 5As shown, the installation structure includes a first mounting box 4, a second mounting box 5, a first motor 6, a reverse lead screw 7, a connecting frame 8, and a housing 9. The first mounting box 4 is fixed to the front end of the upper surface of the lighting control box 3, and the second mounting box 5 is fixed to the rear end of the upper surface of the lighting control box 3. The first motor 6 is fixed to the right side of the first mounting box 4. The output end of the first motor 6 is fixed to the reverse lead screw 7, and the outer end of the reverse lead screw 7 is threadedly connected to the connecting frame 8. The end of the reverse lead screw 7 away from the first motor 6 is rotatably mounted on the first mounting box 4. The housing 9 is fixed to the top of the connecting frame 8. Sliding grooves are provided at the rear end of the first mounting box 4 and the front end of the second mounting box 5. The connecting frame 8 forms a sliding structure with the rear end of the first mounting box 4 and the second mounting box 5 through the reverse lead screw 7. The housing 9 is symmetrically arranged about the center line of the first mounting box 4. The housing 9 is connected to the support leg 2 by a snap-fit connection.
[0029] When assembling the drone 1 and the lighting control box 3, place the lighting control box 3 below the drone 1, align the left and right sets of housings 9 with the support legs 2, start the first motor 6, the first motor 6 drives the reverse lead screw 7 to rotate clockwise, the connecting frame 8 threaded to the reverse lead screw 7 moves inward, the connecting frame 8 moves in the sliding groove of the first mounting box 4 and the second mounting box 5, thereby moving the housings 9 fixedly connected to the connecting frame 8 inward, so that the housings 9 fit on the rods at the outer end of the support legs 2, and the rods at the outer end of the support legs 2 fit against the inner wall of the housings 9, thereby fixing the drone 1 and the lighting control box 3;
[0030] A side plate 10 is fixed to the side of the lighting control box 3. A side lighting plate 12 is installed on the inner side of the side plate 10. The outer side of the side lighting plate 12 is fixedly connected to the output end of the second motor 11. The second motor 11 is fixed on the side plate 10. A bottom lighting plate 13 is installed on the lower surface of the lighting control box 3. The side lighting plate 12 is rotatably installed on the side plate 10. The side lighting plate 12 is installed on the front, back, left and right sides of the lighting control box 3.
[0031] When the staff are working in the field, the battery inside the lighting control box 3 provides power to the side lighting panel 12 and the bottom lighting panel 13. The side lighting panels 12 illuminate the field in all directions. The second motor 11 drives the side lighting panels 12 to rotate, adjusting the illumination angle of the side lighting panels 12 in all directions. The bottom lighting panel 13 illuminates the area directly below the drone 1.
[0032] The above completes a series of operations for this high-altitude lighting device suitable for field operations. Any content not described in detail in this instruction belongs to the prior art known to those skilled in the art.
[0033] All standard parts used in this utility model can be purchased from the market, and irregular parts can be customized according to the description and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the prior art. The machinery, parts and equipment adopt conventional models in the prior art, and the circuit connection adopts conventional connection methods in the prior art, which will not be described in detail here.
[0034] Although the present invention 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 the present invention should be included within the protection scope of the present invention.
Claims
1. A high-altitude lighting device suitable for field operations, comprising a drone (1), a lighting control box (3), a side lighting panel (12), and a bottom lighting panel (13), characterized in that: The unmanned aerial vehicle (1) has support legs (2) integrally installed on both the front and rear sides of its bottom end. The lighting control box (3) is fixedly connected to the support leg (2) through the mounting structure. A side plate (10) is fixed on the side of the lighting control box (3). A side lighting plate (12) is installed on the inner side of the side plate (10). The outer side of the side lighting plate (12) is fixedly connected to the output end of the second motor (11). The second motor (11) is fixed on the side plate (10). A bottom lighting plate (13) is installed on the lower surface of the lighting control box (3).
2. The high-altitude lighting device suitable for field operations according to claim 1, characterized in that: The mounting structure includes a first mounting box (4), a second mounting box (5), a first motor (6), a reverse lead screw (7), a connecting frame (8), and a housing (9). The first mounting box (4) is fixed to the front end of the upper surface of the lighting control box (3), and the second mounting box (5) is fixed to the rear end of the upper surface of the lighting control box (3). The first motor (6) is fixed to the right side of the first mounting box (4). The reverse lead screw (7) is fixed to the output end of the first motor (6), and the connecting frame (8) is threaded to the outer end of the reverse lead screw (7). The end of the reverse lead screw (7) away from the first motor (6) is rotatably mounted on the first mounting box (4), and the housing (9) is fixed to the top of the connecting frame (8).
3. A high-altitude lighting device suitable for field operations according to claim 2, characterized in that: The rear end of the first mounting box (4) and the front end of the second mounting box (5) are both provided with sliding grooves. The connecting frame (8) forms a sliding structure with the rear end of the first mounting box (4) and the second mounting box (5) through the reverse lead screw (7).
4. A high-altitude lighting device suitable for field operations according to claim 2, characterized in that: The housing (9) is symmetrically arranged about the center line of the first mounting box (4), and the housing (9) is connected to the support leg (2) by a snap-fit connection.
5. A high-altitude lighting device suitable for field operations according to claim 1, characterized in that: The side lighting panel (12) is rotatably mounted on the side plate (10).
6. A high-altitude lighting device suitable for field operations according to claim 1, characterized in that: The side lighting panel (12) is installed on the front, back, left and right sides of the lighting control box (3).
Citation Information
Patent Citations
High altitude illumination unmanned aerial vehicle
CN207917172U