Illuminating unmanned aerial vehicle

Abstract

The lighting unmanned aerial vehicle comprises an unmanned aerial vehicle body and a supporting rod, a shell is fixedly connected to the bottom of the unmanned aerial vehicle body, first springs are fixedly connected to the two sides of an inner cavity of the shell, a connecting block is fixedly connected to one side of each first spring, a first limiting rod is fixedly connected to one side of each connecting block, and a pull rod is fixedly connected to the other side of each connecting block. When the illuminating lamp needs to be installed, a pull rod is pulled, a connecting block is driven by the pull rod to move towards one side, a first spring is extruded, a first limiting rod is driven by the connecting block to move towards one side, a supporting rod is inserted into an inner cavity of a shell, the top of the supporting rod is attached to the bottom of a limiting concave block, the pull rod is loosened, and the illuminating lamp is installed. The structure is reset, the second limiting rod is limited through the first limiting rod, in a similar way, the supporting rod can be taken out by pulling the pull rod and releasing limiting of the first limiting rod on the second limiting rod, the function of rapid disassembly and assembly can be achieved, the operation steps are simple, and time and labor are saved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a lighting unmanned aerial vehicle. Background Art

[0002] Unmanned aircraft, also known as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices. When using drones at night, it is necessary to add lights to the drones to achieve the lighting function;

[0003] At present, lighting lamps are generally installed on drones. The lighting lamps can illuminate the ground, water, mountains, and the exterior of buildings. During the flight of the drone, the lighting lamps are used for lighting work. However, in actual use, since the lighting lamps need to be used for lighting work for a long time, the lighting lamps are easily damaged. When the lighting lamps need to be replaced, it takes a lot of time for the user to disassemble and assemble the lighting lamps. The operation steps are cumbersome, time-consuming and labor-intensive, which greatly increases the user's workload and cannot achieve the function of quick disassembly and assembly. At the same time, when the drone lands, due to the high pressure generated during landing, the pressure generated cannot be effectively released, which can easily cause damage to the drone due to excessive pressure, thereby reducing the service life of the drone. Therefore, we provide a lighting drone. Utility Model Content

[0004] 1. Technical issues to be resolved

[0005] In view of the deficiencies in the prior art, the purpose of the utility model is to provide a lighting drone. When the lighting lamp needs to be installed, the pull rod is pulled, and the connecting block is driven to move to one side through the pull rod, and the first spring is squeezed, and the first limiting rod is driven to move to one side through the connecting block, and the support rod is inserted into the inner cavity of the shell, and the top of the support rod is made to fit with the bottom of the limiting recessed block, and the pull rod is released to reset the structure, and the second limiting rod is limited by the first limiting rod. Similarly, the pull rod is pulled to release the limiting of the second limiting rod by the first limiting rod, and the support rod can be taken out, so as to achieve the function of quick disassembly and assembly. The operation steps are simple, time-saving and labor-saving, so as to solve the problems raised in the above-mentioned background technology.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a technical solution adopted by a lighting drone is: it includes a drone and a support rod, the bottom of the drone is fixedly connected with a shell, both sides of the inner cavity of the shell are fixedly connected with a first spring, one side of the first spring is fixedly connected with a connecting block, one side of the connecting block is fixedly connected with a first limiting rod, the other side of the connecting block is fixedly connected with a pull rod, a limiting recessed block is fixedly connected at the center of the top of the inner cavity of the shell, both sides of the support rod are fixedly connected with a second limiting rod, and a lighting lamp is fixedly installed on the bottom of the support rod.

[0008] As a preferred solution, the front and rear ends of the bottom of the drone are fixedly connected to a connecting box, a plurality of dampers are fixedly connected to the top of the inner cavity of the connecting box, a second spring is wound around the surface of the damper, the bottom of the damper is fixedly connected to a cross plate, both sides of the bottom of the cross plate are fixedly connected to connecting rods, and the bottom of the connecting rods is fixedly connected to a bottom plate.

[0009] Optionally, when the UAV lands, the pressure generated during landing drives the bottom plate to move upward, which in turn drives the connecting rod to move upward, which in turn drives the cross plate to move upward, and the damper and the second spring are squeezed by the cross plate. The characteristics of the second spring are used to effectively release the pressure generated during landing, thereby achieving a buffering function, preventing the UAV from being damaged during landing, and increasing the service life of the UAV.

[0010] As a preferred solution, a power supply box is fixedly connected to the top of the drone, and a battery is provided in the inner cavity of the power supply box.

[0011] Optionally, the device is powered by a power supply box and a battery.

[0012] As a preferred solution, both sides of the bottom of the inner cavity of the shell are provided with sliding grooves, the bottom of the connecting block is fixedly connected with a sliding block, and the bottom of the sliding block is slidably connected to the inner cavity of the sliding groove.

[0013] Optionally, the moving position of the connecting block is limited by setting the sliding groove and the sliding block.

[0014] As a preferred solution, both sides of the transverse plate are fixedly connected with sliding sleeves, and the inner cavity of the sliding sleeve is slidably connected with a sliding rod.

[0015] Optionally, the sliding rod and the sliding sleeve are provided to reduce the shaking of the horizontal plate during the movement.

[0016] As a preferred solution, a cover plate is provided on the surface of the connection box, and the cover plate and the connection box are fixedly connected by mounting bolts.

[0017] Optionally, by installing bolts and a cover plate, it is convenient for users to inspect and maintain the parts in the inner cavity of the connection box.

[0018] (III) Beneficial effects

[0019] Compared with the prior art, the utility model provides a lighting drone with the following beneficial effects.

[0020] 1. When the lighting lamp needs to be installed, the utility model pulls the pull rod, drives the connecting block to move to one side through the pull rod, and squeezes the first spring, drives the first limiting rod to move to one side through the connecting block, inserts the support rod into the inner cavity of the shell, and makes the top of the support rod fit with the bottom of the limiting recessed block, loosens the pull rod, resets the structure, and limits the second limiting rod through the first limiting rod. Similarly, pulls the pull rod to release the limiting of the second limiting rod by the first limiting rod, and can take out the support rod, so as to achieve the function of quick disassembly and assembly, and the operation steps are simple, saving time and effort.

[0021] 2. When the drone lands, the pressure generated during landing drives the bottom plate to move upward, drives the connecting rod upward through the bottom plate, drives the cross plate upward through the connecting rod, squeezes the damper and the second spring through the cross plate, and uses the characteristics of the second spring to effectively release the pressure generated during landing, thereby achieving a buffering function, preventing the drone from being damaged during landing, and increasing the service life of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 It is a schematic diagram of the structure of the utility model;

[0023] Figure 2 This is a bottom view of the UAV of the utility model;

[0024] Figure 3 This is a cross-sectional view of the housing of the utility model;

[0025] Figure 4 This is a cross-sectional view of the connection box of the utility model.

[0026] In the figure: 1. battery; 2. power supply box; 3. bottom plate; 4. connecting rod; 5. connecting box; 6. drone; 7. shell; 8. pull rod; 9. support rod; 10. lighting lamp; 11. first spring; 12. connecting block; 13. first limit rod; 14. second limit rod; 15. limit recess; 16. slide groove; 17. slider; 18. damper; 19. second spring; 20. slide rod; 21. sleeve; 22. cross plate. DETAILED DESCRIPTION

[0027] The following is a further detailed description of the implementation of the present invention in conjunction with the accompanying drawings and examples. The following examples are used to illustrate the present invention, but cannot be used to limit the scope of the present invention.

[0028] See also Figure 1-4 , the embodiments of the utility model will be further described below in conjunction with the accompanying drawings.

[0029] Example

[0030] A technical solution adopted by a lighting drone is: it includes a drone 6 and a support rod 9, the bottom of the drone 6 is fixedly connected to a shell 7, both sides of the inner cavity of the shell 7 are fixedly connected to a first spring 11, one side of the first spring 11 is fixedly connected to a connecting block 12, one side of the connecting block 12 is fixedly connected to a first limiting rod 13, the other side of the connecting block 12 is fixedly connected to a pull rod 8, a limiting recessed block 15 is fixedly connected at the center of the top of the inner cavity of the shell 7, both sides of the support rod 9 are fixedly connected to a second limiting rod 14, and a lighting lamp 10 is fixedly installed on the bottom of the support rod 9.

[0031] Specifically: when the lighting lamp 10 needs to be installed, the user holds the pull rod 8 and pulls the pull rod 8 outward, drives the connecting block 12 to move to one side through the pull rod 8, and squeezes the first spring 11, drives the first limiting rod 13 to move to one side through the connecting block 12, and makes the first limiting rod 13 move to one side of the inner cavity of the shell 7. At this time, the user inserts the support rod 9 into the inner cavity of the shell 7, and makes the top of the support rod 9 fit with the bottom of the limiting recess 15, and drives the second limiting rod 14 to move into the inner cavity of the shell 7 through the support rod 9. At this time, the user releases the pull rod 8 to reset the structure, so that the first limiting rod 13 is located at the bottom of the second limiting rod 14, and the second limiting rod 14 is limited by the first limiting rod 13 to complete the installation. Similarly, pull the pull rod 8 to release the limiting of the first limiting rod 13 on the second limiting rod 14, and the support rod 9 can be taken out to achieve quick disassembly, which can achieve the function of quick disassembly and assembly. The operation steps are simple, saving time and effort.

[0032] The front and rear ends of the bottom of the drone 6 are fixedly connected to a connection box 5, a plurality of dampers 18 are fixedly connected to the top of the inner cavity of the connection box 5, a second spring 19 is wound on the surface of the damper 18, a cross plate 22 is fixedly connected to the bottom of the damper 18, connecting rods 4 are fixedly connected to both sides of the bottom of the cross plate 22, the bottom of the connecting rod 4 is fixedly connected to the bottom of the bottom plate 3, a power supply box 2 is fixedly connected to the top of the drone 6, a battery 1 is provided in the inner cavity of the power supply box 2, slide grooves 16 are provided on both sides of the bottom of the inner cavity of the shell 7, a slider 17 is fixedly connected to the bottom of the connection block 12, and the bottom of the slider 17 is slidably connected to the inner cavity of the slide groove 16, a sliding sleeve 21 is fixedly connected to both sides of the cross plate 22, and a sliding rod 20 is slidably connected to the inner cavity of the sliding sleeve 21, a cover plate is provided on the surface of the connection box 5, and the cover plate and the connection box 5 are fixedly connected by mounting bolts.

[0033] Specifically, when the drone 6 completes the lighting work and lands, the pressure generated during landing drives the bottom plate 3 to move upward, drives the connecting rod 4 to move upward through the bottom plate 3, drives the cross plate 22 to move upward through the connecting rod 4, and squeezes the damper 18 and the second spring 19 through the cross plate 22. The pressure generated during landing is effectively released by utilizing the characteristics of the second spring 19, thereby achieving a buffering function, and the drone 6 will not be damaged during landing, thereby increasing the service life of the drone 6. The drone 6 is powered by the battery 1 and the power supply box 2 to maintain normal operation of the drone 6. During the movement of the connecting block 12, the connecting block 12 drives the slider 17 to slide in the inner cavity of the slide groove 16, thereby limiting the movement range of the connecting block 12; during the movement of the cross plate 22, the cross plate 22 drives the sliding sleeve 21 to slide on the surface of the slide rod 20, thereby reducing the shaking of the cross plate 22 during the movement, and greatly improving the stability of the cross plate 22 during the movement. The user uses an external tool to rotate the mounting bolts, and turns the mounting bolts out of the inner cavity of the cover plate and the connecting box 5, so that the cover plate can be removed, which is convenient for the user to inspect and maintain the parts in the inner cavity of the connecting box 5.

[0034] The working principle of the utility model is as follows: when the lighting lamp 10 needs to be installed, the user holds the pull rod 8 and pulls the pull rod 8 outward, drives the connecting block 12 to move to one side through the pull rod 8, and squeezes the first spring 11, drives the first limiting rod 13 to move to one side through the connecting block 12, and moves the first limiting rod 13 to one side of the inner cavity of the shell 7. At this time, the user inserts the support rod 9 into the inner cavity of the shell 7, and makes the top of the support rod 9 fit with the bottom of the limiting concave block 15, and drives the second limiting rod 14 to move into the inner cavity of the shell 7 through the support rod 9. At this time, the user releases the pull rod 8 to reset the structure, so that the first limiting rod 13 is located at the bottom of the second limiting rod 14, and the first limiting rod 13 is used to press the second limiting concave block 15. The installation can be completed by limiting the rod 14. Similarly, by pulling the pull rod 8, the limiting of the first limiting rod 13 on the second limiting rod 14 can be released, and the support rod 9 can be taken out to achieve quick disassembly, thereby achieving the function of quick disassembly and assembly. The operation steps are simple, saving time and effort. When the drone 6 completes the lighting work and lands, the pressure generated when landing drives the bottom plate 3 to move upward, and the connecting rod 4 is driven upward by the bottom plate 3, and the cross plate 22 is driven upward by the connecting rod 4, and the damper 18 and the second spring 19 are squeezed by the cross plate 22. The characteristics of the second spring 19 are used to effectively release the pressure generated when landing, thereby achieving the buffering function, and the drone 6 will not be damaged when landing, thereby improving the service life of the drone 6.

[0035] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit the protection scope of the utility model. Although the utility model has been described in detail with reference to the preferred embodiments, ordinary technicians in this field should understand that the technical solution of the utility model can be modified or replaced by equivalents without departing from the essence and scope of the technical solution of the utility model.

Claims

1. A lighting drone, comprising a drone (6) and a support rod (9), characterized in that: The bottom of the drone (6) is fixedly connected to a shell (7), both sides of the inner cavity of the shell (7) are fixedly connected to a first spring (11), one side of the first spring (11) is fixedly connected to a connecting block (12), one side of the connecting block (12) is fixedly connected to a first limiting rod (13), the other side of the connecting block (12) is fixedly connected to a pull rod (8), a limiting recessed block (15) is fixedly connected at the center of the top of the inner cavity of the shell (7), both sides of the support rod (9) are fixedly connected to a second limiting rod (14), and a lighting lamp (10) is fixedly installed at the bottom of the support rod (9).

2. The lighting drone according to claim 1, characterized in that: The front and rear ends of the bottom of the drone (6) are fixedly connected to a connection box (5), the top of the inner cavity of the connection box (5) is fixedly connected to a plurality of dampers (18), the surface of the damper (18) is wound with a second spring (19), the bottom of the damper (18) is fixedly connected to a cross plate (22), both sides of the bottom of the cross plate (22) are fixedly connected to connecting rods (4), and the bottom of the connecting rod (4) is fixedly connected to a bottom plate (3).

3. The lighting drone according to claim 1, characterized in that: The top of the drone (6) is fixedly connected to a power supply box (2), and a storage battery (1) is arranged in the inner cavity of the power supply box (2).

4. The lighting drone according to claim 1, characterized in that: Slide grooves (16) are provided on both sides of the bottom of the inner cavity of the shell (7), a slider (17) is fixedly connected to the bottom of the connecting block (12), and the bottom of the slider (17) is slidably connected to the inner cavity of the slide groove (16).

5. The lighting drone according to claim 2, characterized in that: Both sides of the transverse plate (22) are fixedly connected with a sliding sleeve (21), and the inner cavity of the sliding sleeve (21) is slidably connected with a sliding rod (20).

6. The lighting drone according to claim 2, characterized in that: A cover plate is provided on the surface of the connection box (5), and the cover plate and the connection box (5) are fixedly connected by mounting bolts.

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