Airborne searchlight structure of unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle airborne searchlight structure which comprises a placing main body, a cavity is formed in the placing main body, a first electric push rod is fixedly connected in the cavity, one end of the first electric push rod is fixedly connected with a gear plate, and the surface of the gear plate is meshed with a gear. According to the airborne searchlight structure of the unmanned aerial vehicle, through arrangement of a first electric push rod, a gear plate, a gear, a rotating shaft and a fixing block, after a searchlight is fixed, a user starts a power source of the first electric push rod, the first electric push rod is started to enable the gear plate to move downwards, and the gear plate moves to enable the gear to rotate; the rotating shaft is driven to rotate through rotation of the gear, the angle of the fixing block is adjusted through rotation of the rotating shaft, then a user can adjust the angle of the searchlight according to the requirement of the use condition, and therefore the use convenience of the structure is improved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to an airborne searchlight structure for UAVs. Background Technology

[0002] A drone-borne searchlight is a device installed on a drone to provide illumination and assist navigation. It enhances the drone's ability to operate at night or in low-light environments, improving image quality, navigation accuracy, and safety.

[0003] However, existing UAV-borne searchlight structures have the following drawbacks:

[0004] (1) When the user fixes the searchlight through the airborne structure, the searchlight's illumination angle is relatively fixed, and it is inconvenient for the user to adjust the searchlight angle according to the actual needs.

[0005] (2) When the user fixes the searchlight, it is inconvenient for the user to clamp and fix searchlights of different sizes, which makes the structure have certain limitations.

[0006] Therefore, this utility model provides a structure for an airborne searchlight for unmanned aerial vehicles (UAVs). Utility Model Content

[0007] (a) Technical problems to be solved

[0008] The technical problem solved by this utility model is to provide a UAV-borne searchlight structure that is highly practical, easy to operate, and has a simple structure. This solves the problems mentioned in the background art, such as the fixed illumination angle of the searchlight when the user fixes it through the airborne structure, making it inconvenient for the user to adjust the angle of the searchlight according to actual needs, and the inconvenience for the user to clamp and fix searchlights of different sizes, which makes the structure have certain limitations.

[0009] (II) Technical Solution

[0010] To achieve the above objectives, this utility model provides the following technical solution: a UAV-borne searchlight structure, comprising a placement body, an interior cavity, a first electric push rod fixedly connected inside the cavity, a gear plate fixedly connected to one end of the first electric push rod, a gear meshing on the surface of the gear plate, a through hole on one side of the gear, a rotating shaft fixedly connected inside the through hole, a fixing block fixedly connected to the edge of the rotating shaft, a fixing frame fixedly connected to the bottom of the fixing block, a circular hole on the inner wall of the fixing frame, a second electric push rod fixedly connected inside the circular hole, a T-shaped block fixedly connected to one end of the second electric push rod, and a movable block slidably connected to the surface of the T-shaped block.

[0011] Optionally, a connecting rod is fixedly connected to one end of the movable block, and a clamping plate is fixedly connected to one end of the connecting rod. The clamping plate serves to hold the searchlight.

[0012] Optionally, a groove is provided at one end of the fixed frame, and the movable block is slidably connected inside the groove, which facilitates the sliding of the movable block.

[0013] Optionally, the bottom of the placement body is provided with a groove, the size of which is adapted to the gear, and the groove facilitates the rotation of the gear.

[0014] Optionally, a fixing plate is fixedly connected to the top of the placement body, and the surface of the fixing plate is provided with threaded holes, which serves to fix the placement body.

[0015] Optionally, the internal threaded connection of the threaded hole is provided with four fixing bolts, which serve to fix the structure.

[0016] (III) Beneficial Effects

[0017] This utility model provides an airborne searchlight structure for unmanned aerial vehicles (UAVs), which has the following beneficial effects:

[0018] 1. The UAV-borne searchlight structure, through the arrangement of a first electric push rod, gear plate, gear, rotating shaft, and fixing block, allows the user to adjust the angle of the fixing block after the searchlight is fixed. The first electric push rod activates the power supply, causing the gear plate to move downwards. The gear plate movement causes the gear to rotate, which in turn drives the rotating shaft to rotate. The rotation of the rotating shaft adjusts the angle of the fixing block, allowing the user to adjust the angle of the searchlight according to the needs of the usage, thus improving the ease of use of the structure.

[0019] 2. This UAV-borne searchlight structure, through the setting of a fixed frame, a second electric push rod, a T-block, and a movable block, allows the user to take out the searchlight, and then the user turns on the power of the second electric push rod. The activation of the second electric push rod causes the T-block to move, which in turn causes the movable block to slide. The sliding of the movable block drives the clamping plate to move, thereby fixing the searchlight. This allows the user to clamp and fix searchlights of different sizes, thus improving the practicality of the structure. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0021] Figure 2 This is a schematic diagram of the overall disassembled structure of this utility model;

[0022] Figure 3 This is a schematic diagram of the T-block structure of this utility model;

[0023] Figure 4 This is a schematic diagram of the cross-sectional structure of the main body of this utility model.

[0024] In the diagram: 1. Main body; 2. First electric push rod; 3. Gear plate; 4. Gear; 5. Rotating shaft; 6. Fixing block; 7. Fixing frame; 8. Second electric push rod; 9. T-block; 10. Moving block; 11. Connecting rod; 12. Clamping plate; 13. Fixing disc; 14. Fixing bolt. Detailed Implementation

[0025] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the scope of protection of the present utility model.

[0026] Please see Figures 1 to 4This utility model provides a technical solution: a UAV-borne searchlight structure, including a placement body 1, with a cavity inside the placement body 1. A first electric push rod 2 is fixedly connected inside the cavity. A gear plate 3 is fixedly connected to one end of the first electric push rod 2. A gear 4 meshes with the surface of the gear plate 3. A through hole is opened on one side of the gear 4, and a rotating shaft 5 is fixedly connected inside the through hole. A fixing block 6 is fixedly connected to the edge of the rotating shaft 5. Through the arrangement of the first electric push rod 2, gear plate 3, gear 4, rotating shaft 5, and fixing block 6, after the searchlight is fixed, the user turns on the power of the first electric push rod 2. The activation of the first electric push rod 2 causes the gear plate 3 to move downwards. The movement of the gear plate 3 causes the gear 4 to rotate. The rotation of the gear 4 drives the rotating shaft 5 to rotate. The rotation of the rotating shaft 5 adjusts the angle of the fixing block 6, thereby allowing the user to... The angle of the searchlight can be adjusted according to the needs of use, thus improving the ease of use of the structure. The bottom of the fixed block 6 is fixedly connected to the fixed frame 7. The inner wall of the fixed frame 7 has a round hole, and the inside of the round hole is fixedly connected to the second electric push rod 8. One end of the second electric push rod 8 is fixedly connected to the T-shaped block 9. The surface of the T-shaped block 9 is slidably connected to the moving block 10. With the setting of the fixed frame 7, the second electric push rod 8, the T-shaped block 9, and the moving block 10, the user takes out the searchlight and then turns on the power of the second electric push rod 8. The second electric push rod 8 starts, causing the T-shaped block 9 to move. The movement of the T-shaped block 9 causes the moving block 10 to slide. The sliding of the moving block 10 drives the clamping plate 12 to move, so that the clamping plate 12 fixes the searchlight. In this way, the user can clamp and fix searchlights of different sizes, thereby improving the practicality of the structure.

[0027] One end of the movable block 10 is fixedly connected to a connecting rod 11, and one end of the connecting rod 11 is fixedly connected to a clamping plate 12. The clamping plate 12 serves to hold the searchlight.

[0028] A groove is provided at one end of the fixed frame 7. The groove facilitates the sliding of the movable block 10, which is slidably connected to the inside of the groove.

[0029] The bottom of the main body 1 is provided with a groove, which facilitates the rotation of the gear 4. The size of the groove is adapted to the gear 4.

[0030] A fixing plate 13 is fixedly connected to the top of the main body 1. The fixing plate 13 serves to fix the main body 1. Threaded holes are provided on the surface of the fixing plate 13.

[0031] The internal threaded connection of the threaded hole is provided with a fixing bolt 14, which serves to fix the structure. There are four fixing bolts 14.

[0032] In this invention, the working steps of the device are as follows:

[0033] First step: First, personnel take out the searchlight, then personnel turn on the power of the second electric push rod 8. The second electric push rod 8 is turned on, causing the T-block 9 to move. The movement of the T-block 9 causes the moving block 10 to slide. The sliding of the moving block 10 drives the clamping plate 12 to move, so that the clamping plate 12 fixes the searchlight.

[0034] Second step: After the searchlight is fixed, the user turns on the power of the first electric push rod 2. The first electric push rod 2 causes the gear plate 3 to move downward. The movement of the gear plate 3 causes the gear 4 to rotate. The rotation of the gear 4 drives the rotating shaft 5 to rotate. The rotation of the rotating shaft 5 adjusts the angle of the fixing block 6.

[0035] The third step: Finally, the structure is fixed to the drone using fixing bolt 14.

[0036] It should be noted that the device structure and accompanying drawings of this utility model mainly describe the principle of this utility model. In terms of the technical aspects of this design principle, the setting of the power mechanism, power supply system and control system of the device is not fully described. However, under the premise that those skilled in the art understand the principle of the above utility model, the specific details of its power mechanism, power supply system and control system can be clearly understood. The control method in the application document is automatic control through a controller. The control circuit of the controller can be implemented by those skilled in the art through simple programming.

[0037] All standard parts used can be purchased from the market, and can be customized according to the instructions and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the existing technology. The machinery, parts and equipment adopt conventional models in the existing technology, and the structure and principle of the components known to those skilled in the art can be known by those skilled in the art through technical manuals or conventional experimental methods.

[0038] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A UAV-borne searchlight structure, comprising a mounting body (1), characterized in that: The placement body (1) has an internal cavity, and a first electric push rod (2) is fixedly connected inside the cavity. A gear plate (3) is fixedly connected to one end of the first electric push rod (2). A gear (4) meshes with the surface of the gear plate (3). A through hole is opened on one side of the gear (4). A rotating shaft (5) is fixedly connected inside the through hole. A fixing block (6) is fixedly connected to the edge of the surface of the rotating shaft (5). A fixing frame (7) is fixedly connected to the bottom of the fixing block (6). A round hole is opened on the inner wall of the fixing frame (7). A second electric push rod (8) is fixedly connected inside the round hole. A T-shaped block (9) is fixedly connected to one end of the second electric push rod (8). A moving block (10) is slidably connected to the surface of the T-shaped block (9).

2. The UAV airborne searchlight structure according to claim 1, characterized in that: One end of the movable block (10) is fixedly connected to a connecting rod (11), and one end of the connecting rod (11) is fixedly connected to a clamping plate (12).

3. The UAV airborne searchlight structure according to claim 1, characterized in that: One end of the fixed frame (7) is provided with a sliding groove, and the moving block (10) is slidably connected to the inside of the sliding groove.

4. The UAV airborne searchlight structure according to claim 1, characterized in that: The bottom of the placement body (1) is provided with a groove, the size of which is adapted to the gear (4).

5. The UAV airborne searchlight structure according to claim 1, characterized in that: The top of the placement body (1) is fixedly connected to a fixing plate (13), and the surface of the fixing plate (13) is provided with threaded holes.

6. The UAV airborne searchlight structure according to claim 5, characterized in that: The internal threaded connection of the threaded hole is provided with a fixing bolt (14), and the number of fixing bolts (14) is four.

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