CN218401006U

CN218401006U - Staying unmanned aerial vehicle illumination lamps and lanterns

Info

Publication number: CN218401006U
Application number: CN202223103902.7U
Authority: CN
Inventors: 曹海霞; 张涛
Original assignee: Guangzhou Senhai Electronic Information Technology Co ltd
Current assignee: Guangzhou Senhai Electronic Information Technology Co ltd
Priority date: 2022-11-22
Filing date: 2022-11-22
Publication date: 2023-01-31
Anticipated expiration: 2032-11-22

Abstract

The utility model discloses a staying unmanned aerial vehicle illumination lamps and lanterns, including unmanned aerial vehicle body, installing frame and landing leg, terminal surface fixedly connected with installing frame under the unmanned aerial vehicle body, the installing frame inboard is provided with lighting assembly, and lighting assembly includes lamps and lanterns, movable plate, spacing slide bar and buffer spring, has seted up the installing port on the installing frame, and the spacing slide bar of installing port both sides fixedly connected with, the movable plate has been cup jointed in the slip of the spacing slide bar outside, is provided with buffer spring between movable plate and the unmanned aerial vehicle body diapire. The utility model discloses in, cause great damage because of assaulting when avoiding unmanned aerial vehicle to meet with the barrier for the messenger, when meetting the barrier, the pressure-bearing rod at first contacts with the barrier, and the pressure-bearing rod receives the impact back, and the illumination lamps and lanterns drive the movable plate and slide on spacing slide bar surface, and the movable plate passes through impact force extrusion buffer spring, plays certain buffering cushioning effect to the unmanned aerial vehicle body through buffer spring, so prolongs the life of unmanned aerial vehicle body, reduces use cost.

Description

Staying unmanned aerial vehicle illumination lamps and lanterns

Technical Field

The utility model relates to an unmanned aerial vehicle lighting apparatus technical field specifically is a staying unmanned aerial vehicle illumination lamps and lanterns.

Background

Mooring unmanned aerial vehicle, also known as mooring unmanned aerial vehicle, for many rotor unmanned aerial vehicle's a special form, use the ground power supply through mooring cable transmission as power source, replace traditional lithium cell, the leading characteristics are long-time stagnation and hang the ability of stopping.

By searching, the notice number is: CN 214930687U's chinese patent discloses a staying unmanned aerial vehicle illumination lamps and lanterns, relate to lamps and lanterns technical field, through first motor and second motor combined action, can make the horizontal 360 vertical 180 rotations of bulb, for the autonomous rotation of lamps and lanterns, unnecessarily rotatory with the help of unmanned aerial vehicle self, unmanned aerial vehicle's work load has been reduced, and the irradiation range of lamps and lanterns is wide, thereby obtain the best illuminating effect, therefore, the clothes hanger is strong in practicability, the support column is all installed to the lower surface corner of fixing base, the fixed plate is installed jointly to the bottom of two support columns, the surface sliding connection of fixed plate has two connecting pieces that correspond, the surface mounting of connecting piece has the spring, the buffer board is installed jointly to the one end of two connecting pieces that correspond, the connecting piece, buffer device is constituteed jointly to spring and buffer board, come the gravity and the inertia of buffering unmanned aerial vehicle self when falling to the ground and give the power that the support column brought, the deformation damage of support column has been avoided, the safety of lamps and lanterns has been protected, the life of device has been strengthened.

This patent suffers from the following disadvantages: current formula unmanned aerial vehicle's that moors lighting device can not stretch out and draw back automatically, leads to meeting when the accident direct and barrier collision, and its damage probability is great, and use cost is high.

Therefore, this application now proposes a staying unmanned aerial vehicle lighting fixtures to solve the problem that the aforesaid appears.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a mooring unmanned aerial vehicle illumination lamps and lanterns to solve current mooring unmanned aerial vehicle's lighting device and can not carry out automatic flexible, direct and barrier collision when leading to meetting the accident, its damage probability is great, problem that use cost is high.

In order to achieve the above object, the utility model provides a following technical scheme:

the lighting lamp for the tethered unmanned aerial vehicle comprises an unmanned aerial vehicle body, a mounting frame and supporting legs, wherein the mounting frame is fixedly connected to the lower end face of the unmanned aerial vehicle body, a lighting assembly is arranged on the inner side of the mounting frame, and the supporting legs are fixedly connected to the four side walls of the mounting frame;

the illumination subassembly includes lamps and lanterns, movable plate, spacing slide bar and buffer spring, the installing port has been seted up on the installing frame, the spacing slide bar of installing port both sides fixedly connected with, the movable plate has been cup jointed in the slip of spacing slide bar outside, be provided with buffer spring between movable plate and the unmanned aerial vehicle body diapire, buffer spring is around locating on the spacing slide bar lateral wall, terminal surface fixed mounting has lamps and lanterns under the movable plate, lamps and lanterns are located the installing port inboard, just terminal surface both sides fixedly connected with pressure-bearing rod under the lamps and lanterns.

Further, the installing frame inboard is provided with elevating gear for the lamps and lanterns go up and down, elevating gear includes cylinder, electronic slide rail, slider, magnet and ironbar, fixed mounting has the cylinder on the relative both sides inner wall of installing frame, the piston end fixed mounting of cylinder has electronic slide rail, be provided with the slider of adaptation on the electronic slide rail, fixedly connected with magnet on the slider lateral wall, movable plate diapire both sides are inlayed and are equipped with the ironbar, magnet and ironbar magnetism are inhaled fixedly.

Further, buffer spring bottom and movable plate up end fixed connection, buffer spring top and unmanned aerial vehicle body diapire fixed connection.

Furthermore, a rubber damping sleeve is fixedly bonded at the end part of the pressure bearing rod.

Further, the mounting frame is used for accommodating a lamp.

Compared with the prior art, the beneficial effects of the utility model are that:

the utility model discloses in, cause great damage because of assaulting when avoiding unmanned aerial vehicle to meet with the barrier for the messenger, when meetting the barrier, the pressure-bearing rod at first contacts with the barrier, and after the pressure-bearing rod received the impact, illumination lamps and lanterns drove the movable plate and slide on spacing slide bar surface, and the movable plate passes through impact force extrusion buffer spring, plays certain buffering cushioning effect to the unmanned aerial vehicle body through buffer spring, so prolongs the life of unmanned aerial vehicle body, reduces use cost.

Drawings

Fig. 1 is a schematic front sectional view of a lighting fixture for a captive drone;

FIG. 2 is an enlarged view of a portion A of FIG. 1;

fig. 3 is a schematic front view of a lighting fixture for a captive drone.

In the figure: 10. an unmanned aerial vehicle body; 11. installing a frame; 12. a support leg; 20. a light fixture; 21. moving the plate; 22. a limiting slide bar; 23. a buffer spring; 24. an installation port; 25. a pressure-bearing rod; 251. a rubber shock-absorbing sleeve; 30. a cylinder; 31. an electric slide rail; 32. a slider; 33. a magnet; 34. and (4) iron bars.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution:

in the scheme, the unmanned aerial vehicle comprises an unmanned aerial vehicle body 10, a mounting frame 11 and supporting legs 12, wherein the mounting frame 11 is fixedly welded on the lower end face of the unmanned aerial vehicle body 10, a lighting assembly is arranged on the inner side of the mounting frame 11, and the supporting legs 12 are fixedly welded on the four side walls of the mounting frame 11;

the lighting assembly includes lamps and lanterns 20, the movable plate 21, spacing slide bar 22 and buffer spring 23, installing port 24 has been seted up on the installing frame 11, installing port 24 both sides welded fastening has spacing slide bar 22, spacing slide bar 22 outside is slided and is cup jointed moving plate 21, be provided with buffer spring 23 between moving plate 21 and the unmanned aerial vehicle body 10 diapire, buffer spring 23 is around locating on spacing slide bar 22 lateral wall, terminal surface has lamps and lanterns 20 through bolt fixed mounting under the moving plate 21, lamps and lanterns 20 are located installing port 24 inboardly, and terminal surface both sides welded fastening has bearing rod 25 under lamps and lanterns 20.

In addition, 11 inboards of installing frame are provided with elevating gear, be used for lift lamps and lanterns 20, elevating gear includes cylinder 30, electronic slide rail 31, slider 32, magnet 33 and ironbar 34, there is cylinder 30 through bolt fixed mounting on the relative both sides inner wall of installing frame 11, there is electronic slide rail 31 through bolt fixed mounting at the piston end of cylinder 30, be provided with the slider 32 of adaptation on the electronic slide rail 31, welded fastening has magnet 33 on the slider 32 lateral wall, 21 diapire both sides of movable plate are inlayed and are equipped with ironbar 34, magnet 33 and ironbar 34 magnetism are inhaled fixedly.

When the lighting lamp 20 needs to be accommodated in the installation frame 11, the cylinder 30 is started, so that the piston end of the cylinder 30 drives the electric slide rail 31 to move transversely, then the sliding block 32 on the electric slide rail 31 drives the magnet 33 to slide to the lowest part of the rail, the sliding block 32 and the moving plate 21 are fixed in a magnetic absorption mode through the arranged magnet 33 and the iron bar 34, then the sliding block 32 drives the moving plate 21 to move upwards by starting the electric slide rail 31, so that the lighting lamp 20 moves upwards synchronously, and the lighting lamp 20 is accommodated in the installation frame 11.

For the messenger avoid buffer spring 23 to take place the displacement at deformation in-process, buffer spring 23 bottom and movable plate 21 up end welded fastening, buffer spring 23 top and the 10 diapire welded fastening of unmanned aerial vehicle body.

Wherein, the end of the pressure-bearing rod 25 is fixedly bonded with a rubber shock-absorbing sleeve 251.

The mounting frame 11 is used for accommodating the lamp 20.

The working principle is as follows: when encountering an obstacle, the pressure-bearing rod 25 firstly contacts with the obstacle, after the pressure-bearing rod 25 is impacted, the lighting fixture 20 drives the movable plate 21 to slide on the outer surface of the limit slide bar 22, the movable plate 21 extrudes the buffer spring 23 through impact force, a certain buffering and damping effect is exerted on the unmanned aerial vehicle body 10 through the buffer spring 23, so that the service life of the unmanned aerial vehicle body 10 is prolonged, the use cost is reduced, when the lighting fixture 20 needs to be stored in the mounting frame 11, the air cylinder 30 is started, the piston end of the air cylinder 30 drives the electric slide rail 31 to transversely move, then the sliding block 32 on the electric slide rail 31 drives the magnet 33 to slide to the lowest part of the rail, the sliding block 32 and the movable plate 21 are fixed in a magnetic absorption mode through the magnet 33 and the iron bar 34, then the electric slide rail 31 is started, the sliding block 32 drives the electric slide rail 21 to move upwards, so that the lighting fixture 20 synchronously moves upwards, and the lighting fixture 20 is stored in the mounting frame 11.

The present invention has been described in terms of the above embodiments, but it is to be understood that the above embodiments are for purposes of illustration and description only and are not intended to limit the invention to the described embodiments.

Claims

1. The utility model provides a staying unmanned aerial vehicle illumination lamps and lanterns, includes unmanned aerial vehicle body (10), installing frame (11) and landing leg (12), its characterized in that: the lower end face of the unmanned aerial vehicle body (10) is fixedly connected with a mounting frame (11), the inner side of the mounting frame (11) is provided with a lighting assembly, and four side walls of the mounting frame (11) are fixedly connected with supporting legs (12);

the lighting assembly comprises a lamp (20), a moving plate (21), a limiting slide rod (22) and a buffer spring (23), a mounting opening (24) is formed in the mounting frame (11), the limiting slide rod (22) is fixedly connected to two sides of the mounting opening (24), the moving plate (21) is sleeved on the outer side of the limiting slide rod (22) in a sliding mode, the buffer spring (23) is arranged between the moving plate (21) and the bottom wall of the unmanned aerial vehicle body (10), the buffer spring (23) is wound on the outer side wall of the limiting slide rod (22), the lamp (20) is fixedly mounted on the lower end face of the moving plate (21), the lamp (20) is located on the inner side of the mounting opening (24), and the bearing rod (25) is fixedly connected to two sides of the lower end face of the lamp (20).

2. A tethered drone lighting fixture as claimed in claim 1, wherein: installing frame (11) inboard is provided with elevating gear for lift lamps and lanterns (20), elevating gear includes cylinder (30), electronic slide rail (31), slider (32), magnet (33) and ironbar (34), fixed mounting has cylinder (30) on the relative both sides inner wall of installing frame (11), the piston end fixed mounting of cylinder (30) has electronic slide rail (31), be provided with slider (32) of adaptation on electronic slide rail (31), fixedly connected with magnet (33) on slider (32) lateral wall, movable plate (21) diapire both sides are inlayed and are equipped with ironbar (34), magnet (33) and ironbar (34) magnetism are inhaled fixedly.

3. The tethered drone lighting fixture of claim 1, wherein: buffer spring (23) bottom and movable plate (21) up end fixed connection, buffer spring (23) top and unmanned aerial vehicle body (10) diapire fixed connection.

4. The tethered drone lighting fixture of claim 1, wherein: and a rubber damping sleeve (251) is fixedly bonded at the end part of the pressure bearing rod (25).

5. A tethered drone lighting fixture as claimed in claim 1, wherein: the mounting frame (11) is used for accommodating a lamp (20).