CN214930687U

CN214930687U - Staying unmanned aerial vehicle illumination lamps and lanterns

Info

Publication number: CN214930687U
Application number: CN202121352706.6U
Authority: CN
Inventors: 丁牛欢
Original assignee: Dongguan Zhufeng Intelligent Machinery Co Ltd
Current assignee: Dongguan Zhufeng Intelligent Machinery Co Ltd
Priority date: 2021-06-18
Filing date: 2021-06-18
Publication date: 2021-11-30
Anticipated expiration: 2031-06-18

Abstract

The utility model discloses a staying unmanned aerial vehicle illumination lamp, which relates to the technical field of lamps, through the cooperation of a first motor and a second motor, a bulb can transversely rotate by 180 degrees in the longitudinal direction for the autonomous rotation of the lamp without the help of the self-rotation of an unmanned aerial vehicle, the workload of the unmanned aerial vehicle is reduced, the illumination range of the lamp is wide, thereby the best illumination effect is obtained, the practicability is strong, support columns are arranged at the corners of the lower surface of a fixed seat, a fixed plate is jointly arranged at the bottom ends of the two support columns, the surface of the fixed plate is connected with two corresponding connecting pieces in a sliding way, a spring is arranged on the surface of each connecting piece, a buffer plate is jointly arranged at one end of each corresponding connecting piece, the connecting pieces, the springs and the buffer plate jointly form a buffer device, the force brought to the support columns by the self gravity and inertia of the device when the unmanned aerial vehicle lands on the ground is buffered, and the deformation and the damage of the support columns is avoided, the safety of the lighting lamp is protected, and the service life of the device is prolonged.

Description

Staying unmanned aerial vehicle illumination lamps and lanterns

Technical Field

The utility model relates to the technical field of lighting fixtures, specifically be a staying unmanned aerial vehicle illumination lamps and lanterns.

Background

At present mooring unmanned aerial vehicle's illumination lamps and lanterns, most all are unable autogiration, can only rely on unmanned aerial vehicle self to rotate and drive lamps and lanterns rotatory, unmanned aerial vehicle's work load has been increased, the phase change has increased unmanned aerial vehicle's energy loss, and though also can't shine the unmanned family under the region, irradiation range is narrow and small, and lamps and lanterns are installed in the unmanned aerial vehicle bottom surface, when unmanned aerial vehicle falls to the ground, because the support column of lamps and lanterns does not have buffer, lead to falling back unmanned aerial vehicle's gravity and inertia extrusion supporting leg, cause deformation damage to the supporting leg easily, it can make lamps and lanterns striking ground damage lamps and lanterns to warp when serious, therefore, the technical personnel in the field have proposed a mooring unmanned aerial vehicle illumination lamps and lanterns.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides a staying unmanned aerial vehicle illumination lamps and lanterns has solved lamps and lanterns irradiation range little to and the supporting leg does not have buffer's problem.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a lighting lamp for a staying unmanned aerial vehicle comprises a fixed seat, wherein a first motor is installed at the center inside the fixed seat, a first shaft rod is installed at the output end of the first motor, a rotating disc is installed at the lower end of the first shaft rod, a steering seat is installed at the center of the lower surface of the rotating disc, a through groove is formed in the steering seat, a first gear is rotatably connected inside the steering seat, a second motor is installed on one side of the steering seat on the lower surface of the rotating disc, a second shaft rod is installed at the output end of the second motor, a first gear at one end of the second shaft rod is connected, and a second gear is rotatably connected below the first gear inside the steering seat;

the utility model discloses a buffer board, including fixing base, support column, fixed plate, every the surperficial sliding connection of fixed plate has two connecting pieces that correspond, every the surface mounting of connecting piece has a spring, two correspondences the buffer board is installed jointly to the lower surface corner of fixing base, two sets of two that correspond in both sides the bottom of support column installs the fixed plate jointly.

As a further technical scheme of the utility model, every the limiting plate is all installed to the other end of connecting piece, two sets of correspondences around install the connecting rod between the support column respectively.

As a further technical scheme of the utility model, the connecting plate is installed, two to the both sides of second gear the lamp stand is installed jointly to the one end of connecting plate, the surface mounting of lamp stand has the bulb.

As a further technical scheme of the utility model, two corresponding connecting seats, every are installed respectively to the both sides of fixing base the internally mounted of connecting seat has the bolt.

As a further technical scheme of the utility model, first motor and second motor are electric connection with unmanned aerial vehicle control panel.

As a further technical scheme of the utility model, the lower surface of fixing base set up with the through-hole of primary shaft pole looks adaptation, the hole with second axostylus axostyle looks adaptation is seted up to one side of turning to the seat.

Advantageous effects

The utility model provides a staying unmanned aerial vehicle illumination lamps and lanterns. Compared with the prior art, the method has the following beneficial effects:

1. the utility model provides a staying unmanned aerial vehicle illumination lamps and lanterns, through first motor and second motor mating reaction, can make the horizontal 360 vertical 180 rotations of bulb, for the autonomic rotation of lamps and lanterns, unnecessarily rotatory with the help of unmanned aerial vehicle self, reduced unmanned aerial vehicle's work load, and the irradiation range of lamps and lanterns is wide to obtain the best illuminating effect, the practicality is strong.

2. The utility model provides a staying unmanned aerial vehicle illumination lamps and lanterns, constitutes buffer jointly through connecting piece, spring and buffer board, cushions the power that unmanned aerial vehicle self gravity and inertia brought for the support column when falling to the ground, has avoided the deformation damage of support column, has protected illumination lamps and lanterns's safety, has strengthened the life of device.

Drawings

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

fig. 2 is a front view of a tethered drone lighting fixture;

fig. 3 is a cross-sectional view of a tethered drone lighting fixture.

In the figure: 1. a fixed seat; 2. a first motor; 3. a first shaft lever; 4. rotating the disc; 5. a steering seat; 6. a first gear; 7. a second gear; 8. a support pillar; 9. a fixing plate; 10. a connecting member; 11. a spring; 12. a buffer plate; 13. a limiting plate; 14. a connecting rod; 15. a connecting plate; 16. a lamp socket; 17. a bulb; 18. a connecting seat; 19. a bolt; 20. a second motor; 21. a second shaft.

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.

Please refer to fig. 1-3, the utility model provides a mooring unmanned aerial vehicle illumination lamps and lanterns technical scheme: a lighting lamp for a staying unmanned aerial vehicle comprises a fixed seat 1, wherein a first motor 2 is installed at the center inside the fixed seat 1, a first shaft rod 3 is installed at the output end of the first motor 2, a rotating disc 4 is installed at the lower end of the first shaft rod 3, a steering seat 5 is installed at the center of the lower surface of the rotating disc 4, a through groove is formed in the steering seat 5, a first gear 6 is rotatably connected inside the steering seat 5, a second motor 20 is installed on one side of the steering seat 5 on the lower surface of the rotating disc 4, a second shaft rod 21 is installed at the output end of the second motor 20, the first gear 6 at one end of the second shaft rod 21 is connected, and a second gear 7 is rotatably connected below the first gear 6 inside the steering seat 5;

support column 8 is all installed at the lower surface corner of fixing base 1, and fixed plate 9 is installed jointly to two sets of bottoms that correspond two support columns 8 in both sides, and the sliding surface of every fixed plate 9 is connected with two connecting pieces 10 that correspond, and the surface mounting of every connecting piece 10 has spring 11, and buffer board 12 is installed jointly to the one end of two connecting pieces 10 that correspond.

Limiting plate 13 is all installed to the other end of every connecting piece 10, installs connecting rod 14 between the support column 8 of two sets of correspondences around respectively, and when using, limiting plate 13 plays limiting displacement to connecting piece 10, prevents because spring 11 elasticity connecting piece 10 breaks away from fixed plate 9, and connecting rod 14 plays fixed action to support column 8.

Connecting plates 15 are mounted on two sides of the second gear 7, a lamp holder 16 is mounted at one end of each of the two connecting plates 15, a bulb 17 is mounted on the surface of each lamp holder 16, when the LED lamp is used, the connecting plates 15 are used for connecting the lamp holders 16 with the second gear 7, the lamp holders 16 are used for fixing the bulbs 17, and the bulbs 17 are used for lighting.

Two connecting seats 18 that correspond are installed respectively to the both sides of fixing base 1, and the internally mounted of every connecting seat 18 has bolt 19, and first motor 2 is electric connection with second motor 20 and unmanned aerial vehicle control panel, when using, fixes lamps and lanterns in unmanned aerial vehicle's bottom surface through connecting seat 18 and bolt 19's cooperation work, through first motor 2 of unmanned aerial vehicle control panel and second motor 20, realizes the rotation to bulb 17.

The lower surface of fixing base 1 is seted up with the through-hole of 3 looks adaptations of primary shaft pole, turns to one side of seat 5 and sets up the hole with 21 looks adaptations of second axostylus axostyle, and when using, the through-hole is used for 1 outsides of the fixing base that stretches out of primary shaft pole 3, and the hole that turns to seat 5 is used for second axostylus axostyle 21 to stretch into and turns to 5 insidely and be connected with first gear 6.

The utility model discloses a theory of operation: when the unmanned aerial vehicle is used, the unmanned aerial vehicle stays in the air, but the light does not irradiate the designated direction, at the moment, a controller operates the control panel of the unmanned aerial vehicle, the first motor 2 and the second motor 20 work, the first motor 2 drives the rotary disc 4 to transversely rotate for 360 degrees through the first shaft lever 3, so as to drive the bulb to rotate for 360 degrees, the second motor 20 drives the first gear 6 to rotate through the second shaft lever 21, the first gear 6 drives the second gear 7 to rotate, so as to realize the longitudinal 180-degree rotation of the bulb, until the bulb 17 irradiates the designated direction, the operation is finished, when the unmanned aerial vehicle lands, the buffer plate 12 firstly lands on the ground, at the moment, due to the self gravity and inertia of the device, the support column 8 and the fixed plate 9 are driven to continuously descend, the fixed plate 9 starts to compress the spring 11, the elasticity of the spring 11 gradually offsets the inertia of the device, then the spring 11 starts to rebound, the positions of the support fixed plate 9 and the support column 8 are restored, the operation is complete.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A lighting lamp for mooring an unmanned aerial vehicle comprises a fixed seat (1) and is characterized in that, a first motor (2) is arranged at the center of the interior of the fixed seat (1), a first shaft lever (3) is arranged at the output end of the first motor (2), a rotating disc (4) is arranged at the lower end of the first shaft lever (3), a steering seat (5) is arranged at the center of the lower surface of the rotating disc (4), a through groove is arranged in the steering seat (5), a first gear (6) is rotatably connected in the steering seat (5), a second motor (20) is arranged on one side of the steering seat (5) on the lower surface of the rotating disc (4), a second shaft lever (21) is installed at the output end of the second motor (20), a first gear (6) at one end of the second shaft lever (21) is connected, a second gear (7) is rotatably connected below the first gear (6) in the steering seat (5);

support column (8) are all installed to the lower surface corner of fixing base (1), two sets of two that correspond in both sides fixed plate (9), every are installed jointly to the bottom of support column (8) the sliding surface of fixed plate (9) is connected with two connecting pieces (10) that correspond, every the surface mounting of connecting piece (10) has spring (11), two correspondences buffer board (12) are installed jointly to the one end of connecting piece (10).

2. A tethered unmanned aerial vehicle lighting fixture as claimed in claim 1, characterised in that a limiting plate (13) is mounted at the other end of each connector (10) and a connecting rod (14) is mounted between the front and back sets of corresponding support posts (8).

3. A tethered unmanned aerial vehicle lighting fixture as claimed in claim 1, characterised in that the second gear (7) has connection plates (15) mounted on both sides, a lamp socket (16) is mounted together at one end of both connection plates (15), and a bulb (17) is mounted on the surface of the lamp socket (16).

4. A tethered unmanned aerial vehicle lighting fixture as claimed in claim 1, characterised in that two corresponding connection sockets (18) are mounted on each side of the fixed base (1), a bolt (19) being mounted inside each connection socket (18).

5. The tethered drone lighting fixture of claim 1, wherein the first motor (2) and the second motor (20) are electrically connected to the drone control panel.

6. The tethered unmanned aerial vehicle lighting fixture of claim 1, wherein the lower surface of the fixed base (1) is provided with a through hole adapted to the first shaft (3), and one side of the steering base (5) is provided with a hole adapted to the second shaft (21).