An unmanned aerial vehicle detection device with a regulation function

Abstract

This utility model discloses a drone detection device with controllability, including a drone. A guide device is symmetrically fixedly installed on the top of the drone. A positioning device is slidably installed on the top of the guide device. A docking device is fixedly installed on the bottom of the positioning device. The positioning device includes a limiting plate, a return spring, a slider, a positioning pin, a support base, a through rod, a support cavity, and a synchronization plate. The support cavity is symmetrically fixedly installed on the top of the support base. The limiting plate is fixedly installed inside the top of the support cavity. The slider is slidably inserted into the bottom of the support cavity. The positioning pin is fixedly installed at the center of the bottom of the slider. The return spring is fixedly installed between the limiting plate and the slider. The through rod slidably passes through the limiting plate and connects to the top of the positioning pin. This utility model, through the setting of the positioning device, docking device, and guide device, achieves the purpose of rapid installation and disassembly of an airborne weather instrument.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV detection device with control function. Background Technology

[0002] Unmanned aerial vehicles (UAVs), also known as drones, are aircraft that do not require a pilot to operate from inside the aircraft, but instead complete tasks through remote control, autonomous flight, or semi-autonomous flight. With the development of technology, UAVs have been widely used in military, civilian, and commercial fields.

[0003] For example, a drone detection device with Chinese patent announcement number CN208140861U includes a drone body, a detection caliper and a drive mechanism. The drive mechanism is disposed on the drone body. The detection caliper includes a connecting part and a caliper arm. The caliper arm is movably connected to the drone body through the connecting part. The caliper arm is drively connected to the drive mechanism.

[0004] When installing airborne weather instruments on existing drones, the weather instrument base requires multiple bolts for positioning, which makes it impossible to quickly and easily adjust the installation of the weather instrument. This increases the assembly time when assembling or disassembling the weather instrument with the drone. Therefore, a device is needed to improve this process. Utility Model Content

[0005] The purpose of this invention is to provide a drone detection device with control function to solve the problems mentioned in the background art.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a drone detection device with controllability, comprising a drone, a guide device symmetrically fixedly installed at the top of the drone, a positioning device slidably installed at the top of the guide device, and a docking device fixedly installed at the bottom of the positioning device. The positioning device includes a limiting plate, a return spring, a slider, a positioning pin, a support base, a through rod, a support cavity, and a synchronization plate. The support cavity is symmetrically fixedly installed at the top of the support base, the limiting plate is fixedly installed at the top of the inside of the support cavity, the slider is slidably inserted into the bottom of the support cavity, the positioning pin is fixedly installed at the center of the bottom of the slider, the return spring is fixedly installed between the limiting plate and the slider, the through rod slidably passes through the limiting plate and connects to the top of the positioning pin, and the synchronization plate is fixedly installed at the top of the through rod.

[0007] Preferably, the docking device includes a locking key, a chassis, and an airborne meteorological instrument. The airborne meteorological instrument is fixedly installed at the top center of the chassis, and the locking key is fixedly installed on both sides of the chassis.

[0008] Preferably, the guiding device includes a support guide and positioning holes, wherein the positioning holes are symmetrically opened at the top of the support guide.

[0009] Preferably, the support guide is symmetrically fixedly installed on the top of the UAV, the key is slidably inserted into the inside of the side end of the support guide, and the chassis is fixedly installed on the bottom end of the support frame.

[0010] Preferably, the support base has symmetrically arranged circular holes inside.

[0011] Preferably, the synchronization plate has a circular groove at its center, and the support guide has a slot at its side end.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0013] When in use, this device can slide inside the support guide frame via a key, allowing the airborne weather instrument to be quickly pushed onto the drone. Simultaneously, when the positioning pin moves to align with the positioning hole, the return spring can drive it downward into the positioning hole, thus fixing the airborne weather instrument to the top of the drone. When the airborne weather instrument needs to be removed, the synchronization plate can be pulled upward, allowing the airborne weather instrument to be easily pulled out from the top of the drone, completing the quick installation and removal of the airborne weather instrument. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the main structure of this utility model;

[0015] Figure 2 This is a schematic diagram of the positioning device structure of this utility model;

[0016] Figure 3 This is a schematic diagram of the docking device structure of this utility model;

[0017] Figure 4 This is a schematic diagram of the guiding device structure of this utility model.

[0018] In the diagram: 1-Positioning device, 2-Docking device, 3-Guiding device, 4-UAV, 5-Limiting plate, 6-Reset spring, 7-Slider, 8-Positioning pin, 9-Supporting base frame, 10-Through rod, 11-Supporting cavity, 12-Synchronization plate, 13-Key, 14-Chassis, 15-Airborne meteorological instrument, 16-Supporting guide frame, 17-Positioning hole. Detailed Implementation

[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0020] Please see Figure 1-4 This utility model provides an embodiment of a drone detection device with controllability, comprising a drone 4, a guide device 3 symmetrically fixedly installed on the top of the drone 4, a positioning device 1 slidably installed on the top of the guide device 3, and a docking device 2 fixedly installed on the bottom of the positioning device 1. The positioning device 1 includes a limiting plate 5, a return spring 6, a slider 7, a positioning pin 8, a support base 9, a through rod 10, a support cavity 11, and a synchronization plate 12. The support cavity 11 is symmetrically fixedly installed on the top of the support base 9, the limiting plate 5 is fixedly installed inside the top of the support cavity 11, the slider 7 is slidably inserted into the bottom of the support cavity 11, the positioning pin 8 is fixedly installed at the center of the bottom of the slider 7, the return spring 6 is fixedly installed between the limiting plate 5 and the slider 7, the through rod 10 slidably passes through the limiting plate 5 and connects to the top of the positioning pin 8, and the synchronization plate 12 is fixedly installed on the top of the through rod 10.

[0021] The docking device 2 includes a key 13, a chassis 14, and an airborne meteorological instrument 15. The airborne meteorological instrument 15 is fixedly installed at the top center of the chassis 14, and the key 13 is fixedly installed on both sides of the chassis 14. The key 13 cooperates with the support guide 16 to improve the installation efficiency of the airborne meteorological instrument 15.

[0022] The guide device 3 includes a support guide 16 and positioning holes 17. The positioning holes 17 are symmetrically opened at the top of the support guide 16 and can support the installation of the airborne meteorological instrument 15.

[0023] The support guide 16 is symmetrically fixedly installed on the top of the drone 4. The key 13 is slidably inserted into the inside of the side end of the support guide 16. The chassis 14 is fixedly installed on the bottom end of the support base 9. When the support base 9 is displaced, it can drive the chassis 14 to move.

[0024] The support base 9 has symmetrically opened round holes inside, which facilitates the insertion of the positioning pin 8 through the support base 9 into the positioning hole 17.

[0025] The center of the synchronization plate 12 is provided with a circular groove, and the side end of the support guide 16 is provided with a slot, so that the key 13 can support the sliding installation of the chassis 14 and the airborne meteorological instrument 15.

[0026] Working principle: During use, when the airborne weather instrument 15 needs to be installed, the chassis 14 can be moved horizontally to align with the support guide 16 until the locking key 13 aligns with the slot inside the side end of the support guide 16. Then, the chassis 14 is moved until the locking key 13 is inserted into the slot inside the side end of the support guide 16, allowing the chassis 14 to move along a straight line at the top of the UAV 4. Furthermore, because both ends of the support guide 16 are inclined at 45°, and the bottom end of the positioning pin 8 is rounded, the locking key 13 enters the slot inside the support guide 16. The bottom end of the positioning pin 8 can move upward along the slope at the top of the support guide 16, allowing the positioning pin 8 to enter the interior of the support cavity 11. The elasticity of the return spring 6 allows the positioning pin 8 to move upward. Subsequently, when the chassis 14 moves the positioning pin 8 to be vertically aligned with the positioning hole 17, the elasticity of the return spring 6 will move the positioning pin 8 upward. Pin 8 moves rapidly downwards, allowing it to insert into the positioning hole 17. This allows it to penetrate the support base 9 and contact the support guide 16, thus securing the support base 9 to the top of the support guide 16. This completes the rapid adjustment and installation of the airborne weather instrument 15. Subsequently, when the airborne weather instrument 15 needs to be disassembled, the synchronization plate 12 can be pulled upwards. The synchronization plate 12 is connected to the four through rods 10, which are also connected to the positioning pin 8. As the synchronization plate 12 moves upwards, it drives the through rods 10 and the positioning pin 8 to move upwards simultaneously until the positioning pin 8 is pulled out of the positioning hole 17. This unlocks the airborne weather instrument 15. At this point, the user can pull the airborne weather instrument 15 forward until the locking key 13 is removed from the slot inside the side of the support guide 16. This allows the airborne weather instrument 15 to be disassembled as a whole, completing the rapid installation and disassembly of the airborne weather instrument 15.

[0027] 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 drone detection device with controllability function, comprising a drone (4), wherein a guide device (3) is symmetrically fixedly installed on the top of the drone (4), a positioning device (1) is slidably installed on the top of the guide device (3), and a docking device (2) is fixedly installed on the bottom of the positioning device (1), characterized in that: The positioning device (1) includes a limiting plate (5), a return spring (6), a slider (7), a positioning pin (8), a support base (9), a through rod (10), a support cavity (11), and a synchronization plate (12). The support cavity (11) is symmetrically fixedly installed at the top of the support base (9). The limiting plate (5) is fixedly installed at the top of the inside of the support cavity (11). The slider (7) is slidably inserted into the bottom of the inside of the support cavity (11). The positioning pin (8) is fixedly installed at the center of the bottom of the slider (7). The return spring (6) is fixedly installed between the limiting plate (5) and the slider (7). The through rod (10) slides through the top of the limiting plate (5) and the top of the positioning pin (8). The synchronization plate (12) is fixedly installed at the top of the through rod (10).

2. The UAV detection device with control function according to claim 1, characterized in that: The docking device (2) includes a key (13), a chassis (14) and an airborne meteorological instrument (15). The airborne meteorological instrument (15) is fixedly installed at the top center of the chassis (14), and the key (13) is fixedly installed on both sides of the chassis (14).

3. The UAV detection device with control function according to claim 2, characterized in that: The guiding device (3) includes a support guide (16) and a positioning hole (17), the positioning hole (17) being symmetrically opened at the top of the support guide (16).

4. The UAV detection device with control function according to claim 3, characterized in that: The support guide (16) is symmetrically fixedly installed on the top of the UAV (4), the key (13) is slidably inserted into the side end of the support guide (16), and the chassis (14) is fixedly installed on the bottom end of the support base (9).

5. The UAV detection device with control function according to claim 4, characterized in that: The support base (9) has symmetrically arranged circular holes inside.

6. The UAV detection device with control function according to claim 5, characterized in that: The synchronous plate (12) has a circular groove in its center, and the support guide (16) has a slot in its side end.

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