Quick installation frame for unmanned aerial vehicle performance lighting
The design of the support and installation mechanism solves the problem of drone performance lights becoming loose or falling off during high-speed flight or complex operations, achieving a stable connection and heat dissipation, and ensuring the safety and practicality of drone performances.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- FUZHOU GOSHAWK AVIATION TECHNOLOGY CO LTD
- Filing Date
- 2025-08-26
- Publication Date
- 2026-06-19
AI Technical Summary
Drone show lights are prone to loosening or falling off during high-speed flight or complex operations, and their installation is complicated, affecting flight safety and cost.
The system employs support and installation mechanisms, including components such as buffer frames, fastening nuts, threaded seats, clamps, mounting frames, and heat dissipation slots, to ensure a stable connection and buffer between the drone body and the light assembly, preventing detachment, and to assist in heat dissipation through airflow.
It improves the installation stability and reliability of drone performance lights, prevents the lights from falling off, ensures flight safety, and maintains the normal operation of the lights through heat dissipation channels.
Smart Images
Figure CN224375893U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of drone technology, and in particular to a quick-mounting bracket for drone performance lighting. Background Technology
[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and onboard program control devices. With the popularization of UAV technology, the uses and application scenarios of UAVs are becoming more and more extensive. At the same time, there are also higher demands for the appearance, lighting effects and performance effects of UAVs. In order to meet the needs of UAV light shows, formation lights for light shows are installed on UAVs. A large number of UAVs equipped with formation lights are used to form various light patterns for light shows.
[0003] Existing drone performance lighting is prone to problems such as loosening or falling off during high-speed flight or complex operations, affecting flight safety. Under some extreme flight conditions, such as high-speed flight or high-intensity maneuvers, the lights may be affected by vibration, causing them to flicker or fall off. In addition, installation requires special tools or accessories, which increases the complexity and cost of operation. Utility Model Content
[0004] To solve the above-mentioned technical problems, this utility model provides a quick mounting bracket for drone performance lights.
[0005] This utility model is achieved by the following technical solution: a quick mounting frame for drone performance lights, including a drone body, a support mechanism provided on the surface of the drone body, and a mounting mechanism provided at the bottom of the support mechanism;
[0006] The support mechanism includes a docking frame, a buffer frame fixedly connected to the bottom of the docking frame, a threaded seat fixedly connected to the surface of the docking frame, a clamping plate hinged to the top of the docking frame, and a fastening nut rotatably connected to the inner wall of the clamping plate.
[0007] As a further improvement to the above solution, the inner wall of the docking frame is slidably connected to the surface of the UAV body, and the inner wall of the docking frame is provided with a buffer pad.
[0008] The above technical solution, by setting up a buffer frame and working in conjunction with the buffer pad on the inner wall of the docking frame, buffers the impact force when the drone lands, preventing the main body of the drone from being damaged by the impact and ensuring the reliability of the device.
[0009] As a further improvement to the above solution, the inner wall of the fastening nut is threadedly connected to the surface of the threaded seat.
[0010] Through the above technical solution, by setting a fastening nut, after the main body of the UAV is inserted into the docking frame, the threaded seat and the docking frame clamp the main body of the UAV, and the fastening nut is threadedly connected to the threaded seat, ensuring a stable connection between the support mechanism and the main body of the UAV, and ensuring the structural stability of the UAV during flight.
[0011] As a further improvement to the above solution, the mounting frame is provided with heat dissipation grooves on its surface, a spring is fixedly connected to the inner wall of the mounting frame, a spring plate is provided at the end of the spring away from the mounting frame, a thread is provided on the surface of the mounting frame, a mounting groove is provided on the inner wall of the mounting frame, a thread cover is threadedly connected to the surface of the thread, a mounting plate is slidably connected to the inner wall of the mounting frame, and a lamp assembly is fixedly connected to the bottom of the mounting plate.
[0012] As a further improvement to the above solution, the top of the mounting frame is fixedly connected to the bottom of the docking frame, and the surface of the spring plate is slidably connected to the inner wall of the mounting frame.
[0013] The above technical solution involves setting an installation slot, inserting the installation plate into the installation frame, rotating it, and then using a spring to push the installation plate to fix it to the inner wall of the threaded cover, preventing the lamp assembly from coming out. At the same time, the threaded cover with threaded connection on the surface of the installation frame serves as a secondary safety measure to ensure the installation stability of the lamp assembly and improve the reliability of the device.
[0014] As a further improvement to the above solution, the surface of the lamp assembly is slidably connected to the inner wall of the threaded cover.
[0015] As a further improvement to the above solution, the number of heat dissipation slots is set to several, which are evenly distributed on the surface of the mounting frame.
[0016] Through the above technical solution, by setting up heat dissipation slots, part of the airflow blown downwards by the rotating fan blades of the drone body enters the mounting frame through the heat dissipation slots to assist in the heat dissipation of the light assembly, ensuring the normal operation of the light assembly and guaranteeing the practicality of the device.
[0017] Compared with the prior art, the beneficial effects of this utility model are as follows:
[0018] This utility model incorporates a support mechanism, specifically a fastening nut. After the drone body is inserted into the docking frame, the threaded seat and docking frame clamp the drone body, and the fastening nut is threadedly connected to the threaded seat. This ensures a stable connection between the support mechanism and the drone body, guaranteeing structural stability during drone flight. Furthermore, a buffer frame, working in conjunction with the buffer pad on the inner wall of the docking frame, buffers the impact force when the drone lands, preventing structural damage to the drone body and ensuring the reliability of the device.
[0019] This utility model incorporates an installation mechanism, specifically a heat dissipation groove. A portion of the airflow blown downwards by the rotating fan blades of the drone enters the mounting frame through the heat dissipation groove, providing auxiliary heat dissipation for the light assembly, ensuring its normal operation and guaranteeing the device's practicality. By inserting the mounting plate into the mounting frame through the mounting groove, it rotates, and then a spring pushes the mounting plate to fix it to the inner wall of the threaded cover via a spring plate, preventing the light assembly from detaching. Simultaneously, the threaded cover on the surface of the mounting frame acts as a secondary safety measure, ensuring the installation stability of the light assembly and improving the device's reliability. Attached Figure Description
[0020] Figure 1 This is a schematic diagram of the overall structure of this utility model;
[0021] Figure 2 This is a schematic diagram of the structure of this utility model from below;
[0022] Figure 3 This is a top view of the structure of this utility model;
[0023] Figure 4 This is a schematic cross-sectional view of the present invention.
[0024] Figure 5 This is an exploded view of the installation mechanism structure of this utility model.
[0025] Explanation of key symbols:
[0026] 1. UAV body; 2. Support mechanism; 201. Docking frame; 202. Buffer frame; 203. Threaded seat; 204. Clamping plate; 205. Fastening nut; 3. Mounting mechanism; 301. Mounting frame; 302. Heat dissipation groove; 303. Spring; 304. Spring plate; 305. Thread; 306. Mounting groove; 307. Threaded cover; 308. Mounting plate; 309. Light assembly. Detailed Implementation
[0027] The present invention will be further described below with reference to the accompanying drawings and specific embodiments. It should be noted that, without conflict, the various embodiments or technical features described below can be arbitrarily combined to form new embodiments.
[0028] Example:
[0029] Please combine Figure 1-5 This embodiment of a drone performance lighting quick mounting frame includes a drone body 1, a support mechanism 2 is provided on the surface of the drone body 1, and an installation mechanism 3 is provided at the bottom of the support mechanism 2;
[0030] The support mechanism 2 includes a docking frame 201, a buffer frame 202 fixedly connected to the bottom of the docking frame 201, a threaded seat 203 fixedly connected to the surface of the docking frame 201, a clamping plate 204 hinged to the top of the docking frame 201, and a fastening nut 205 rotatably connected to the inner wall of the clamping plate 204.
[0031] The inner wall of the docking frame 201 is slidably connected to the surface of the UAV body 1. The inner wall of the docking frame 201 is provided with a buffer pad. By setting a buffer frame 202, it works in conjunction with the buffer pad on the inner wall of the docking frame 201 to buffer the impact force when the UAV lands on the ground, preventing the UAV body 1 from being damaged by the impact structure and ensuring the reliability of the device.
[0032] The inner wall of the fastening nut 205 is threadedly connected to the surface of the threaded seat 203. By setting the fastening nut 205, after the UAV body 1 is inserted into the docking frame 201, the threaded seat 203 and the docking frame 201 clamp the UAV body 1. The fastening nut 205 is threadedly connected to the threaded seat 203, ensuring a stable connection between the support mechanism 2 and the UAV body 1, and ensuring the structural stability of the UAV during flight.
[0033] The system includes a mounting frame 301, with heat dissipation grooves 302 on its surface. A spring 303 is fixedly connected to the inner wall of the mounting frame 301, and a spring plate 304 is provided at the end of the spring 303 away from the mounting frame 301. The surface of the mounting frame 301 has threads 305, and the inner wall of the mounting frame 301 has mounting grooves 306. After inserting the mounting plate 308 into the mounting frame 301 and rotating it 90 degrees, the spring 303 pushes the mounting plate 308 to fix it to the inner wall of the threaded cover 307 through the spring plate 304, preventing the lamp assembly 309 from coming out. At the same time, the threaded cover 307 on the surface of the mounting frame 301 acts as a secondary safety measure to ensure the installation stability of the lamp assembly 309. The threaded cover 307 is threadedly connected to the surface of the threads 305. The mounting plate 308 is slidably connected to the inner wall of the mounting frame 301, and the lamp assembly 309 is fixedly connected to the bottom of the mounting plate 308.
[0034] The top of the mounting frame 301 is fixedly connected to the bottom of the docking frame 201, and the surface of the spring plate 304 is slidably connected to the inner wall of the mounting frame 301.
[0035] The surface of the lamp assembly 309 is slidably connected to the inner wall of the threaded cover 307.
[0036] Several heat dissipation slots 302 are provided and evenly distributed on the surface of the mounting frame 301. Part of the airflow blown downward by the rotating fan blades of the UAV body 1 enters the mounting frame 301 through the heat dissipation slots 302 to assist in the heat dissipation of the light assembly 309 and ensure the normal operation of the light assembly 309.
[0037] The implementation principle of a quick-mounting bracket for drone performance lights in this embodiment is as follows: During use, after the drone body 1 is inserted into the docking frame 201, the threaded seat 203 and the docking frame 201 clamp the drone body 1. Then, the fastening nut 205 is threadedly connected to the threaded seat 203, ensuring a stable connection between the support mechanism 2 and the drone body 1. Next, the mounting plate 308 is inserted into the mounting frame 301 and rotated 90 degrees. Then, the spring 303 pushes the mounting plate 308 through the spring plate 304 to fix it to the inner wall of the threaded cover 307, preventing the lights from malfunctioning. When assembly 309 is disengaged, the threaded cover 307 connected to the surface thread of the mounting frame 301 serves as a secondary safety measure to ensure the installation stability of the light assembly 309. During flight, part of the airflow blown downward by the rotating fan blades of the UAV body 1 enters the mounting frame 301 through the heat dissipation slot 302 to assist in the heat dissipation of the light assembly 309 and ensure its normal operation. During landing, the buffer frame 202 and the buffer pad on the inner wall of the docking frame 201 work together to buffer the impact force when the UAV lands on the ground and prevent the UAV body 1 from being damaged by the impact structure.
[0038] The above embodiments are merely preferred embodiments of this utility model and should not be construed as limiting the scope of protection of this utility model. Any non-substantial changes and substitutions made by those skilled in the art based on this utility model shall fall within the scope of protection claimed by this utility model.
Claims
1. A quick-mounting bracket for drone performance lighting, characterized in that, It includes a drone body (1), a support mechanism (2) is provided on the surface of the drone body (1), and an installation mechanism (3) is provided at the bottom of the support mechanism (2); The support mechanism (2) includes a docking frame (201), a buffer frame (202) is fixedly connected to the bottom of the docking frame (201), a threaded seat (203) is fixedly connected to the surface of the docking frame (201), a clamping plate (204) is hinged to the top of the docking frame (201), and a fastening nut (205) is rotatably connected to the inner wall of the clamping plate (204).
2. The drone performance lighting quick-mount frame as described in claim 1, characterized in that: The inner wall of the docking frame (201) is slidably connected to the surface of the UAV body (1), and the inner wall of the docking frame (201) is provided with a buffer pad.
3. The drone performance lighting quick-mount frame as described in claim 1, characterized in that: The inner wall of the fastening nut (205) is threadedly connected to the surface of the threaded seat (203).
4. The quick mounting rack for drone show lights of claim 1, wherein: The mounting mechanism includes a mounting frame (301), the surface of which is provided with heat dissipation grooves (302), a spring (303) is fixedly connected to the inner wall of the mounting frame (301), a spring plate (304) is provided at the end of the spring (303) away from the mounting frame (301), a thread (305) is provided on the surface of the mounting frame (301), a mounting groove (306) is provided on the inner wall of the mounting frame (301), a thread cover (307) is threadedly connected to the surface of the thread (305), a mounting plate (308) is slidably connected to the inner wall of the mounting frame (301), and a lamp assembly (309) is fixedly connected to the bottom of the mounting plate (308).
5. A quick mounting rack for drone show lights as claimed in claim 4, wherein: The top of the mounting frame (301) is fixedly connected to the bottom of the docking frame (201), and the surface of the spring plate (304) is slidably connected to the inner wall of the mounting frame (301).
6. A quick mounting rack for drone show lights as claimed in claim 4, wherein: The surface of the lamp assembly (309) is slidably connected to the inner wall of the threaded cover (307).
7. The quick mounting rack for drone show lights of claim 4, wherein: The number of heat dissipation slots (302) is set to a certain extent, and they are evenly distributed on the surface of the mounting frame (301).