Solar flashing light dismounting structure mounted by using unmanned aerial vehicle

By designing a disassembly structure for solar-powered strobe lights installed on drones, and utilizing the linkage between guide and locking components, the problem of traditional warning lights being difficult to disassemble was solved, achieving efficient and convenient lamp disassembly.

CN223895861UActive Publication Date: 2026-02-10SHENZHEN ZIGUANG NEW ENERGY TECH CO LTD
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Patent Information

Application Number
CN202520627425.9
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-04-03
Publication Date
2026-02-10
Estimated Expiration
2035-04-03

AI Technical Summary

Technical Problem

Traditional warning lights are difficult to install and remove using drones, and lack the corresponding disassembly structure, making it difficult to remove high-altitude warning lights.

Method used

A disassembly structure for a solar-powered strobe light installed by a drone was designed, including a shell, a guide component, a locking component, and a bracket. The drone lifts the shell, and the bracket clamps are unlocked by the linkage of the pull rod and the locking component, thus enabling the high-altitude disassembly of the light fixture.

Benefits of technology

It enables easy disassembly of warning lights, improving their effectiveness and convenience.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a solar flashing light dismounting structure installed by using an unmanned aerial vehicle, which comprises a shell, a guide assembly is arranged at the bottom of the shell, a pull rod is arranged on the guide assembly in a floatable manner, a locking assembly is arranged on the outer side wall of the shell, and the pull rod is in transmission connection with the locking assembly. A first support and a second support are hinged to the two sides of the outer portion of the shell respectively, and the end of the first support and the end of the second support are matched with the locking assembly. The guide assembly and the locking assembly are linked through the pull rod, the unmanned aerial vehicle drives the shell to ascend, the pull rod is pressed downwards under the action of the unmanned aerial vehicle to drive the locking assembly to be unlocked, and therefore the first support and the second support on the two sides of the shell open clamps for fixing the lamp, and high-altitude disassembly of the lamp is achieved; and the using effect and the convenience degree of the warning lamp are effectively improved.
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Description

Technical Field

[0001] This utility model relates to the field of lighting fixtures, and in particular to a disassembly structure for a solar-powered strobe light installed using a drone. Background Technology

[0002] Because of the high position of overhead cables, warning lights are difficult to install manually on the processed cables. With the development of drone technology, the installation of warning devices on overhead cables has gradually become possible. However, traditional warning lights are not equipped with corresponding disassembly structures, making it difficult to disassemble warning lights at high altitudes.

[0003] Therefore, there is an urgent need for a disassembly structure for solar-powered strobe lights that can be installed using drones, which can solve the above problems. Utility Model Content

[0004] The purpose of this invention is to provide a disassembly structure for a solar-powered strobe light installed using a drone, in order to solve the problems existing in the prior art.

[0005] To achieve the above objectives, this utility model provides the following solution:

[0006] This utility model provides a disassembly structure for a solar-powered strobe light installed on a drone, including a housing, a guide assembly at the bottom of the housing, a buoyant pull rod on the guide assembly, a locking assembly on the outer side wall of the housing, the pull rod being throttledly connected to the locking assembly, and a first bracket and a second bracket hinged to the outer sides of the housing, the ends of the first bracket and the ends of the second bracket cooperating with the locking assembly.

[0007] Preferably, the outer casing has a top-opening structure.

[0008] Preferably, the guide assembly has three sets.

[0009] Preferably, the guide assembly includes a sleeve, inside which a guide post is retractably provided, and the pull rod is disposed through the upper part of the guide post.

[0010] Preferably, the locking assembly includes a latch, which is disposed on the side of the housing. A first limiting edge is provided on the outer side of the latch, and a lock head is retractably provided inside the latch. The lock head is connected to the pull rod, and the end of the first bracket is limited by the first limiting edge and the lock head.

[0011] Preferably, the end of the first bracket is provided with a second limiting edge, and the end of the second bracket is provided with a third limiting edge, the second limiting edge and the third limiting edge cooperating with each other.

[0012] Preferably, the upper part of the first bracket and the upper part of the second bracket are provided with a first tension spring mounting hole, the top of the outer shell is provided with a second tension spring mounting hole, and a tension spring is provided between the first tension spring mounting hole and the second tension spring mounting hole.

[0013] Preferably, the top edge of the outer casing is provided with a limiting post for limiting the first bracket and the second bracket.

[0014] The present invention achieves the following beneficial technical effects compared to the prior art:

[0015] This utility model provides a disassembly structure for a solar-powered strobe light installed using a drone. The structure includes a housing, a guide assembly at the bottom of the housing, a buoyant pull rod on the guide assembly, and a locking assembly on the outer side wall of the housing. The pull rod is kinetically connected to the locking assembly. A first bracket and a second bracket are hinged to the outer sides of the housing, respectively, with the ends of the first and second brackets engaging with the locking assembly. The pull rod links the guide assembly and the locking assembly, allowing the drone to lift the housing. The drone then presses down on the pull rod, unlocking the locking assembly. This causes the first and second brackets on both sides of the housing to open the clamps securing the light fixture, enabling high-altitude disassembly of the light fixture. This effectively improves the usability and convenience of the warning light. Attached Figure Description

[0016] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0017] Fig. 1 A schematic diagram of the disassembly structure of a solar-powered strobe light installed using a drone, provided for this utility model;

[0018] Fig. 2 A schematic diagram of the disassembly guide section of a solar-powered strobe light installed using a drone, provided for this utility model;

[0019] Fig. 3 This invention provides a schematic diagram of the locking component of a disassembly structure for a solar-powered strobe light installed using a drone. Detailed Implementation

[0020] 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.

[0021] The purpose of this invention is to provide a disassembly structure for a solar-powered strobe light installed using a drone, in order to solve the problems existing in the prior art.

[0022] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0023] Example 1:

[0024] This embodiment provides a disassembly structure for a solar-powered strobe light installed using a drone, such as... Figs. 1-3 As shown, the device includes a housing 1, a guide assembly 2 at the bottom of the housing 1, a buoyant pull rod 3 on the guide assembly 2, a locking assembly 4 on the outer side wall of the housing 1, the pull rod 3 being pulsatorically connected to the locking assembly 4, and a first bracket 5 and a second bracket 6 hinged to the outer sides of the housing 1 respectively, the ends of the first bracket 5 and the ends of the second bracket 6 cooperating with the locking assembly 4.

[0025] In one embodiment, the housing 1 has a top opening structure, which allows the lamp holder to be installed inside.

[0026] In one implementation, the guide assembly 2 is provided in three sets, which are arranged side by side at the bottom of the housing 1, so that they can synchronously drive the pull rod 3 to move.

[0027] In one embodiment, the guide assembly 2 includes a sleeve 21, inside which a guide post 22 is telescopically provided, and a pull rod 3 is provided through the upper part of the guide post 22, so that when the guide post 22 is pressed down, the pull rod 3 can be driven to move downward.

[0028] In one embodiment, the locking assembly 4 includes a latch 41, which is disposed on the side of the housing 1. A first limiting edge 42 is provided on the outer side of the latch 41. A lock head 43 is retractably provided inside the latch 41 and is connected to the pull rod 3. Thus, the lock head 43 can be retracted into the latch 41 by moving the pull rod 3 downward. It should be understood that, in order to make the extension and retraction of the lock head 43 smoother, it can be designed as a wedge structure. The end of the first bracket 5 is limited by the first limiting edge 42 and the lock head 43. When the lock head 43 is retracted, the first bracket 5 can be unlocked.

[0029] In one implementation, the end of the first bracket 5 is provided with a second limiting edge 51, and the end of the second bracket 6 is provided with a third limiting edge 61. The second limiting edge 51 and the third limiting edge 61 cooperate to achieve linkage between the two.

[0030] In one embodiment, the upper part of the first bracket 5 and the upper part of the second bracket 6 are both provided with a first tension spring mounting hole 52, and the top of the outer shell 1 is provided with a second tension spring mounting hole 11. A tension spring (not shown in the figure) is provided between the first tension spring mounting hole 52 and the second tension spring mounting hole 11. Through the connection of the tension spring, once the lock is released, the first bracket 5 and the second bracket 6 can move towards the center under the action of the tension spring, thereby opening the clip used to fix the warning light to detach from the cable fixation.

[0031] In one embodiment, the top edge of the outer casing 1 is provided with a limiting post 12 for limiting the first bracket 5 and the second bracket 6, thereby preventing them from being overstretched.

[0032] This utility model provides a disassembly structure for a solar-powered strobe light installed using a drone. The method of use is as follows: the drone lifts the outer shell 1, and the drone presses down the pull rod 3 to unlock the locking component 4, thereby opening the clamps that fix the light fixture on the first bracket 5 and the second bracket 6 on both sides of the outer shell 1, thus realizing the high-altitude disassembly of the light fixture, which effectively improves the use effect and convenience of the warning light.

[0033] This utility model uses specific examples to illustrate its principles and implementation methods. The above description of the embodiments is only for the purpose of helping to understand the method and core idea of ​​this utility model. At the same time, for those skilled in the art, there will be changes in the specific implementation methods and application scope based on the idea of ​​this utility model. In summary, the content of this specification should not be construed as a limitation of this utility model.

Claims

1. A disassembly structure for a solar-powered strobe light installed using a drone, characterized in that: The device includes an outer casing, a guide assembly at the bottom of the casing, a buoyant pull rod on the guide assembly, a locking assembly on the outer side wall of the casing, the pull rod being throttledly connected to the locking assembly, and a first bracket and a second bracket hinged to the outer sides of the casing respectively, the ends of the first bracket and the ends of the second bracket cooperating with the locking assembly.

2. The disassembly structure for a solar-powered strobe light installed using a drone as described in claim 1, characterized in that: The outer shell has a top-opening structure.

3. The disassembly structure for a solar-powered strobe light installed using a drone as described in claim 1, characterized in that: The guide assembly has three sets.

4. The disassembly structure for a solar-powered strobe light installed using a drone as described in claim 3, characterized in that: The guide assembly includes a sleeve, inside which a guide post is retractably provided, and a pull rod is provided through the upper part of the guide post.

5. The disassembly structure for a solar-powered strobe light installed using a drone according to claim 1, characterized in that: The locking assembly includes a latch, which is disposed on the side of the housing. A first limiting edge is provided on the outer side of the latch. A lock head is retractably provided inside the latch. The lock head is connected to the pull rod. The end of the first bracket is limited by the first limiting edge and the lock head.

6. The disassembly structure for a solar-powered strobe light installed using a drone as described in claim 5, characterized in that: The first bracket has a second limiting edge at its end, and the second bracket has a third limiting edge at its end, with the second limiting edge and the third limiting edge cooperating with each other.

7. The disassembly structure for a solar-powered strobe light installed using a drone according to claim 1, characterized in that: The upper part of the first bracket and the upper part of the second bracket are both provided with a first tension spring mounting hole, and the top of the outer shell is provided with a second tension spring mounting hole. A tension spring is provided between the first tension spring mounting hole and the second tension spring mounting hole.

8. The disassembly structure for a solar-powered strobe light installed using a drone according to claim 1, characterized in that: The top edge of the outer casing is provided with a limiting post for limiting the first bracket and the second bracket.