Solar flashing light dismounting structure mounted by using unmanned aerial vehicle

Abstract

The invention provides a solar strobe light dismounting structure installed by using an unmanned aerial vehicle, the solar strobe light dismounting structure 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 mode, 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.

Description

Technical Field

[0001] The invention relates to the field of lamps, and in particular to a disassembly structure of a solar strobe light installed by using an unmanned aerial vehicle. Background Art

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

[0003] Therefore, there is an urgent need for a solar flash light disassembly structure installed using a drone that can solve the above problems. Summary of the invention

[0004] The purpose of the present invention is to provide a solar flash light disassembly structure installed using a drone to solve the problems existing in the above-mentioned prior art.

[0005] To achieve the above object, the present invention provides the following solutions:

[0006] The present invention provides a disassembly structure of a solar-powered flash light installed using a drone, comprising a shell, a guide assembly being provided at the bottom of the shell, a pull rod being provided on the guide assembly in a floating manner, a locking assembly being provided on the outer side wall of the shell, the pull rod being transmission-connected to the locking assembly, a first bracket and a second bracket being hinged on both sides of the outside of the shell, respectively, and an end portion of the first bracket and an end portion of the second bracket being matched with the locking assembly.

[0007] Preferably, the housing is a top-opening structure.

[0008] Preferably, the guide assemblies are provided in three groups.

[0009] Preferably, the guide assembly comprises a sleeve, a guide column is telescopically provided in the sleeve, and the pull rod is arranged to penetrate the upper part of the guide column.

[0010] Preferably, the locking assembly includes a lock buckle, which is arranged on the side of the shell, and a first limiting edge is provided on the outer side of the lock buckle, and a lock head is telescopically provided inside the lock buckle, and 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, a second limiting edge is provided at the end of the first bracket, and a third limiting edge is provided at the end of the second bracket, and the second limiting edge and the third limiting edge cooperate with each other.

[0012] Preferably, a first tension spring mounting hole is provided on the upper portion of the first bracket and the upper portion of the second bracket, a second tension spring mounting hole is provided on the top of the housing, and a tension spring is provided between the first tension spring mounting hole and the second tension spring mounting hole.

[0013] Preferably, a limiting column is provided on the top edge of the shell for limiting the first bracket and the second bracket.

[0014] Compared with the prior art, the present invention has achieved the following beneficial technical effects:

[0015] The present invention provides a disassembly structure of a solar flash light installed using a drone, comprising a shell, a guide assembly is provided at the bottom of the shell, a pull rod is provided on the guide assembly in a floating manner, a locking assembly is provided on the outer wall of the shell, the pull rod is transmission-connected to the locking assembly, a first bracket and a second bracket are hinged on the outer sides of the shell respectively, and the end of the first bracket and the end of the second bracket cooperate with the locking assembly; the guide assembly and the locking assembly are linked by the pull rod, so that the shell is driven to rise by the drone, and the pull rod is pressed down under the action of the drone to unlock the locking assembly, so that the first bracket and the second bracket on both sides of the shell open the clips that fix the lamp, thereby realizing high-altitude disassembly of the lamp, effectively improving the use effect and convenience of the warning lamp. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative labor.

[0017] Figure 1 A schematic diagram of the disassembly structure of a solar strobe light installed using a drone provided by the present invention;

[0018] Figure 2 A schematic diagram of the guiding part of the disassembly structure of a solar strobe light installed by a drone provided by the present invention;

[0019] Figure 3 A partial schematic diagram of a locking assembly of a disassembly structure of a solar strobe light installed using a drone provided by the present invention. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] The purpose of the present invention is to provide a solar strobe light disassembly structure installed by a drone to solve the problems existing in the prior art.

[0022] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0023] Embodiment 1:

[0024] This embodiment provides a solar flash light disassembly structure installed by a drone, such as Figure 1-3 As shown, it includes a shell 1, a guide assembly 2 is provided at the bottom of the shell 1, a pull rod 3 is provided on the guide assembly 2 in a floating manner, a locking assembly 4 is provided on the outer wall of the shell 1, the pull rod 3 is transmission-connected with the locking assembly 4, and a first bracket 5 and a second bracket 6 are hinged on both sides of the outside of the shell 1, and an end of the first bracket 5 and an end of the second bracket 6 cooperate with the locking assembly 4.

[0025] As an implementation manner, the housing 1 is a top-opening structure so that the lamp holder can be installed inside it.

[0026] As an implementation mode, three groups of guide assemblies 2 are provided, and the three groups of guide assemblies 2 are distributed side by side at the bottom of the housing 1, so that they can synchronously drive the pull rod 3 to move.

[0027] As an embodiment, the guide assembly 2 includes a sleeve 21, in which a guide column 22 is telescopically provided, and the pull rod 3 is arranged to pass through the upper part of the guide column 22, so that when the guide column 22 is pressed down, the pull rod 3 can be driven to move downward.

[0028] As an embodiment, the locking assembly 4 includes a lock buckle 41, which is arranged on the side of the shell 1. A first limiting edge 42 is provided on the outer side of the lock buckle 41. A lock head 43 is retractably provided in the lock buckle 41. The lock head 43 is connected to the pull rod 3, so that the lock head 43 can be retracted into the lock buckle 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-shaped 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] As an implementation mode, a second limiting edge 51 is provided at the end of the first bracket 5, and a third limiting edge 61 is provided at the end of the second bracket 6. The second limiting edge 51 and the third limiting edge 61 cooperate with each other to achieve linkage cooperation between the two.

[0030] As an embodiment, a first tension spring mounting hole 52 is provided on the upper portion of the first bracket 5 and the upper portion of the second bracket 6, a second tension spring mounting hole 11 is provided on the top of the housing 1, and 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 toward the middle under the action of the tension spring, thereby stretching the clip used to fix the warning light to break away from the fixation with the cable.

[0031] As an implementation mode, a limiting column 12 is provided on the top edge of the housing 1 for limiting the first bracket 5 and the second bracket 6, so as to prevent the two from being over-extended.

[0032] The present invention provides a solar flash light disassembly structure installed using a drone, and its usage method is: the drone drives the shell 1 to rise, and under the action of the drone, the pull rod 3 is pressed down to drive the locking assembly 4 to unlock, so that the first bracket 5 and the second bracket 6 on both sides of the shell 1 open the clips that fix the lamp, thereby realizing high-altitude disassembly of the lamp, effectively improving the use effect and convenience of the warning lamp.

[0033] The present invention uses specific examples to illustrate the principles and implementation methods of the present invention. The above examples are only used to help understand the method and core ideas of the present invention. At the same time, for those skilled in the art, according to the ideas of the present invention, there will be changes in the specific implementation methods and application scopes. In summary, the content of this specification should not be understood as limiting the present invention.

Claims

1. A solar flash light disassembly structure installed by a drone, characterized by: It includes a shell, a guide assembly is provided at the bottom of the shell, a pull rod is provided on the guide assembly in a floating manner, a locking assembly is provided on the outer wall of the shell, the pull rod is transmission-connected to the locking assembly, and a first bracket and a second bracket are hinged on both sides of the outside of the shell, and the end of the first bracket and the end of the second bracket cooperate with the locking assembly.

2. The solar flash light disassembly structure installed by a drone according to claim 1 is characterized in that: The shell is a top-opening structure.

3. The solar flash light disassembly structure installed by a drone according to claim 1 is characterized in that: The guide components are provided in three groups.

4. The solar flash light disassembly structure installed by a drone according to claim 3 is characterized by: The guide assembly comprises a sleeve, a guide column is telescopically arranged in the sleeve, and the pull rod is arranged to penetrate the upper part of the guide column.

5. The solar flash light disassembly structure installed by a drone according to claim 1, characterized in that: The locking assembly includes a lock buckle, which is arranged on the side of the shell, and a first limiting edge is provided on the outer side of the lock buckle. A lock head is telescopically provided inside the lock buckle, and 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 solar flash light disassembly structure installed by a drone according to claim 5, characterized in that: A second limiting edge is disposed at the end of the first bracket, and a third limiting edge is disposed at the end of the second bracket, and the second limiting edge and the third limiting edge match each other.

7. The solar flash light disassembly structure installed by 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, the top of the 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.

8. The solar flash light disassembly structure installed by a drone according to claim 1, characterized in that: A limiting column is provided on the top edge of the shell for limiting the first bracket and the second bracket.

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