Illuminating device based on unmanned aerial vehicle platform

Abstract

The utility model discloses a lighting device based on an unmanned aerial vehicle platform, and relates to the technical field of lighting devices. The unmanned aerial vehicle comprises an unmanned aerial vehicle body, and the unmanned aerial vehicle body is provided with a disassembly and assembly mechanism and an anti-falling mechanism; the dismounting and mounting mechanism comprises a supporting frame fixedly connected to the bottom of the unmanned aerial vehicle body, sleeves are arranged on the left side and the right side of the supporting frame in a communicating mode, telescopic rods are fixedly connected to the inner walls of the sides, close to each other, of the two sleeves, and the anti-falling mechanism comprises two rectangular supporting plates fixedly connected to the bottom of the unmanned aerial vehicle body. A threaded rod is rotationally connected between the two rectangular supporting plates. By arranging the dismounting mechanism, the problems that in the using process of an existing lighting device based on an unmanned aerial vehicle platform, when a lamp needs to be replaced, a large amount of time and energy need to be consumed for dismounting related parts, so that the maintenance time is greatly prolonged, an unmanned aerial vehicle cannot be put into use in time, and the maintenance cost is reduced are solved. And the working efficiency is influenced.

Description

Technical Field

[0001] This utility model belongs to the field of lighting device technology, and in particular relates to a lighting device based on a drone platform. Background Technology

[0002] When natural disasters such as earthquakes, fires, and mudslides occur, they are often accompanied by large-scale power outages. The on-site environment is complex and dimly lit. Rescue personnel need to conduct a comprehensive survey and rescue work in the disaster area in a short period of time. Traditional lighting equipment such as flashlights and large searchlights either have limited illumination range or are difficult to deploy to designated locations quickly. Lighting devices based on drone platforms can quickly fly to the disaster area and provide large-area, high-brightness lighting, helping rescue personnel to carry out their work better, improving rescue efficiency, and saving more lives.

[0003] However, when existing drone-based lighting devices need to be replaced, a lot of time and effort is required to disassemble the relevant parts, which greatly extends the maintenance time and prevents the drone from being put into use in a timely manner, thus affecting its work efficiency. Utility Model Content

[0004] The purpose of this utility model is to provide a lighting device based on a drone platform. By setting up a disassembly and assembly mechanism, it solves the problem that existing drone-based lighting devices require a lot of time and effort to disassemble related parts when the lamps need to be replaced, which greatly extends the maintenance time and causes the drone to be unable to be put into use in a timely manner, thus affecting its working efficiency.

[0005] To solve the above-mentioned technical problems, this utility model is achieved through the following technical solution:

[0006] This utility model is a lighting device based on a drone platform, including a drone body, on which a disassembly and assembly mechanism and an anti-fall-off mechanism are provided;

[0007] The disassembly and assembly mechanism includes a support frame fixedly connected to the bottom of the drone body. Sleeves are provided on both the left and right sides of the support frame. Telescopic rods are fixedly connected to the inner walls of the two sleeves on the side closest to each other. The anti-fall mechanism includes two rectangular support plates fixedly connected to the bottom of the drone body. A threaded rod is rotatably connected between the two rectangular support plates. The front side of the threaded rod passes through the rectangular support plate located on the front side.

[0008] Furthermore, trapezoidal blocks are fixedly connected to the sides of the two telescopic rods that are close to each other, and springs are fitted on the outer walls of the two telescopic rods.

[0009] Further, two sides of the two springs away from each other are fixedly connected with two sleeves respectively, and two sides of the two springs close to each other are fixedly connected with two trapezoidal blocks respectively.

[0010] Further, a connecting rod is through the support frame, a limiting sleeve is fixedly connected to the outer wall of the connecting rod, a clamping block one is slidably connected to the outer wall of the connecting rod, and a clamping block two is fixedly connected to the outer wall of the connecting rod.

[0011] Further, a support block is threadedly connected to the outer wall of the threaded rod, the bottom of the support block is in contact with the connecting rod, a sliding rod is fixedly connected between the two rectangular support plates, the sliding rod penetrates the support block, and the sliding rod is slidably connected with the support block.

[0012] Further, the bottom of the unmanned aerial vehicle body is fixedly connected with two supporting legs, and the bottom of the connecting rod is fixedly connected with a lighting lamp.

[0013] The utility model has the advantages of the following beneficial effects:

[0014] 1. When the lighting lamp needs to be installed, the lighting lamp is pushed upwards, the clamping block two is driven upwards by the connecting rod, the two trapezoidal blocks are between the clamping block one and the clamping block two, when the clamping block two contacts the two trapezoidal blocks, the two trapezoidal blocks are away from each other due to the upward movement of the clamping block two, and the two telescopic rods and the springs are compressed, in the compression process, the springs are elastically deformed and generate elastic force, when the clamping block two is completely above the two trapezoidal blocks, the two springs release the elastic force, and the lighting lamp is clamped on the unmanned aerial vehicle body, if the lighting lamp needs to be disassembled, the lighting lamp is continuously pushed upwards, the clamping block one is driven upwards by the connecting rod and the limiting sleeve, the clamping block one is above the two trapezoidal blocks, and then the lighting lamp is pulled downwards, so that the lighting lamp cannot be easily loosened or fallen off during the flight of the unmanned aerial vehicle body, reliable connection stability is provided, the lighting device can normally work under various flight conditions, no additional tool is needed, the operation difficulty is reduced, and the work efficiency is improved.

[0015] 2. When the lighting lamp is installed, the support block is screwed, the support block is above the connecting rod, the connecting rod is prevented from moving upwards due to uncertain factors during the flight of the unmanned aerial vehicle body, the lighting lamp is prevented from falling off, when the lighting lamp is disassembled, the threaded rod is screwed before the lighting lamp is pushed upwards, the support block is separated from the connecting rod, the connecting rod is provided with additional support and limiting, the connecting rod is prevented from moving upwards due to these uncertain factors, and the lighting lamp is prevented from falling off, the flight safety is greatly ensured, and the serious consequences such as equipment damage, personnel injury or task failure caused by the falling of the lighting lamp are avoided.

[0016] Of course, implementing any product of the present application does not necessarily need to achieve all the advantages described above at the same time. BRIEF DESCRIPTION OF DRAWINGS

[0017] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the description of the embodiments. Obviously, the drawings described in the following only constitute some of the embodiments of the present application, and for those skilled in the art, other drawings can also be obtained without creative labor on the basis of these drawings.

[0018] Figure 1 It is a schematic diagram of the overall structure of the present application;

[0019] Figure 2 It is a schematic diagram of the bottom structure of the present application;

[0020] Figure 3 It is a schematic diagram of the partial sectional structure of the dismounting mechanism of the present application;

[0021] Figure 4 It is a schematic diagram of the partial structure of the anti-falling mechanism of the present application;

[0022] Figure 5 It is a schematic diagram of the enlarged structure of A in the present application. Figure 3

[0023] In the drawings, the component list represented by each number is as follows:

[0024] 1, unmanned aerial vehicle body; 101, support leg; 102, illuminating lamp; 2, dismounting mechanism; 211, support frame; 212, sleeve; 213, telescopic rod; 214, trapezoidal block; 215, spring; 216, connecting rod; 217, limiting sleeve; 218, clamping block one; 219, clamping block two; 3, anti-falling mechanism; 311, rectangular support plate; 312, threaded rod; 313, support block; 314, sliding rod. DETAILED DESCRIPTION

[0025] The technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments only constitute some of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the present application.

[0026] Please refer to Figures 1-5 ​As shown, the utility model is a kind of lighting device based on unmanned plane platform, including unmanned plane body 1, and is provided with dismounting mechanism 2 and anti-falling mechanism 3 on unmanned plane body 1, the bottom of unmanned plane body 1 is fixedly connected with two support legs 101, the bottom of connecting rod 216 is fixedly connected with illuminating lamp 102, wherein, illuminating lamp 102 adopts advanced high-quality coated optical lens to condense light, ensure that the illumination intensity is not less than 60000 lumen under one meter distance, provide strong and uniform lighting effect for unmanned plane night operation.The device is compatible with DJISkyPortV2.0 interface and DJI M300RTK series unmanned plane, can be easily integrated into existing unmanned plane platform, meet the diversified night operation demand, this compatibility advantage not only simplifies installation process, also greatly improves the flexibility and diversity of unmanned plane night operation.

[0027] Dismounting mechanism 2 includes the support frame 211 fixedly connected at the bottom of unmanned plane body 1, the left side and the right side of support frame 211 are both communicated with sleeve 212, the inner wall of the side close to each other of two sleeves 212 is fixedly connected with telescopic rod 213, the side close to each other of two telescopic rods 213 is fixedly connected with trapezoidal block 214, the outer wall of two telescopic rods 213 is all set with spring 215, the side away from each other of two springs 215 is respectively fixedly connected with two sleeves 212, the side close to each other of two springs 215 is respectively fixedly connected with two trapezoidal blocks 214, the outer wall of connecting rod 216 is fixedly connected with the limit sleeve 217, the outer wall of connecting rod 216 is slidably connected with the clamping block one 218, the outer wall of connecting rod 216 is fixedly connected with the clamping block two 219, by setting dismounting mechanism 2, it can be ensured that illuminating lamp 102 will not easily loosen or fall off during the flight of unmanned plane body 1, provide reliable connection stability, ensure that lighting device can work normally under various flight conditions, and without using additional tools, reduce the operation difficulty, can improve work efficiency.

[0028] The anti-falling mechanism 3 comprises two rectangular support plates 311 fixedly connected at the bottom of the unmanned aerial vehicle body 1, a threaded rod 312 rotatably connected between the two rectangular support plates 311, the threaded rod 312 penetrating through the rectangular support plate 311 located at the front side, a support block 313 threadedly connected to the outer wall of the threaded rod 312, the bottom of the support block 313 being in contact with the connecting rod 216, a sliding rod 314 fixedly connected between the two rectangular support plates 311, the sliding rod 314 penetrating through the support block 313, the sliding rod 314 being in sliding connection with the support block 313. By arranging the anti-falling mechanism 3, additional support and limiting for the connecting rod 216 are provided, the upward movement of the connecting rod 216 caused by uncertain factors is effectively prevented, the lighting lamp 102 is prevented from falling, flight safety is greatly ensured, and serious consequences such as equipment damage, personnel injury or task failure caused by the falling of the lighting lamp 102 are avoided.

[0029] One specific application of the embodiment is: when the lighting lamp 102 needs to be installed, the lighting lamp 102 is pushed upward, the connecting rod 216 drives the clamping block two 219 to move upward, and the two trapezoidal blocks 214 are located between the clamping block one 218 and the clamping block two 219. When the clamping block two 219 is in contact with the two trapezoidal blocks 214, the two trapezoidal blocks 214 move away from each other due to the upward movement of the clamping block two 219, and the two telescopic rods 213 and the springs 215 are compressed. During the compression process, the springs 215 are elastically deformed and generate elastic force. When the clamping block two 219 is completely above the two trapezoidal blocks 214, the two springs 215 release the elastic force and clamp the lighting lamp 102 on the unmanned aerial vehicle body 1. If the lighting lamp 102 needs to be disassembled, the lighting lamp 102 is continuously pushed upward, the connecting rod 216 and the limiting sleeve 217 drive the clamping block one 218 to move upward, the clamping block one 218 is above the two trapezoidal blocks 214, and then the lighting lamp 102 is pulled downward. After the lighting lamp 102 is installed, the support block 313 is twisted, at this time, the support block 313 is above the connecting rod 216 in cooperation with the sliding rod 314, the upward movement of the connecting rod 216 caused by uncertain factors during the flight of the unmanned aerial vehicle body 1 is prevented, and the falling of the lighting lamp 102 is avoided. When the lighting lamp 102 is disassembled, the threaded rod 312 is twisted before the lighting lamp 102 is pushed upward, so that the support block 313 is separated from the connecting rod 216.

[0030] In the description of the specification, the description of the terms "one embodiment", "an example", "a specific example" and the like means that the specific features, structures, materials or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the utility model. In the specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0031] The preferred embodiments of the utility model disclosed above are only used for helping to explain the utility model. The preferred embodiments do not describe all the details exhaustively, and also do not limit the utility model to only the specific implementation manners described. Obviously, according to the content of the specification, many modifications and changes can be made. The specification selects and specifically describes these embodiments in order to better explain the principles and practical applications of the utility model, so that the persons skilled in the art can well understand and utilize the utility model. The utility model is limited only by the claims and the entire scope and equivalents thereof.

Claims

1. A lighting device based on an unmanned aerial vehicle (UAV) platform, characterized in that: Includes a drone body (1), on which a disassembly and assembly mechanism (2) and an anti-fall-off mechanism (3) are provided; The disassembly and assembly mechanism (2) includes a support frame (211) fixedly connected to the bottom of the UAV body (1). Sleeves (212) are connected to the left and right sides of the support frame (211). Telescopic rods (213) are fixedly connected to the inner walls of the two sleeves (212) on the side close to each other. The anti-fall mechanism (3) includes two rectangular support plates (311) fixedly connected to the bottom of the UAV body (1). A threaded rod (312) is rotatably connected between the two rectangular support plates (311). The front side of the threaded rod (312) passes through the rectangular support plate (311) located on the front side.

2. The lighting device based on a drone platform according to claim 1, characterized in that, A trapezoidal block (214) is fixedly connected to one side of each of the two telescopic rods (213) that are close to each other, and a spring (215) is sleeved on the outer wall of each of the two telescopic rods (213).

3. A lighting device based on a drone platform according to claim 2, characterized in that, The two springs (215) are fixedly connected to two sleeves (212) on the side away from each other, and the two springs (215) are fixedly connected to two trapezoidal blocks (214) on the side close to each other.

4. A lighting device based on a drone platform according to claim 3, characterized in that, A connecting rod (216) runs through the support frame (211), and a limit sleeve (217) is fixedly connected to the outer wall of the connecting rod (216).

5. A lighting device based on a drone platform according to claim 4, characterized in that, A first locking block (218) is slidably connected to the outer wall of the connecting rod (216), and a second locking block (219) is fixedly connected to the outer wall of the connecting rod (216).

6. A lighting device based on a drone platform according to claim 5, characterized in that, A support block (313) is threadedly connected to the outer wall of the threaded rod (312). The bottom of the support block (313) is in contact with the connecting rod (216). A slide rod (314) is fixedly connected between the two rectangular support plates (311). The slide rod (314) passes through the support block (313) and is slidably connected to the support block (313).

7. A lighting device based on a drone platform according to claim 6, characterized in that, The bottom of the drone body (1) is fixedly connected to two support legs (101), and the bottom of the connecting rod (216) is fixedly connected to a lighting lamp (102).

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