Unmanned aerial vehicle detection auxiliary device

By designing an auxiliary detection device for drones and adjusting the position of the detection equipment, the problem of drone center of gravity shift was solved, and flight stability was improved.

CN224184517UActive Publication Date: 2026-05-01PINGDINGSHAN UNIVERSITY
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
PINGDINGSHAN UNIVERSITY
Filing Date
2025-06-19
Publication Date
2026-05-01

AI Technical Summary

Technical Problem

When a drone is equipped with additional detection equipment, its mass distribution changes, causing a shift in its center of gravity and affecting its flight stability.

Method used

A drone detection auxiliary device was designed, comprising a drone body, a mounting frame, a U-shaped box, a rotating block, a helical gear, and a lateral adjustment mechanism. The center of gravity of the drone is adjusted by adjusting the longitudinal and lateral positions of the detection device.

Benefits of technology

It effectively adjusts the drone's center of gravity, improves flight stability, and prevents the drone from veering off course during takeoff and landing.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an unmanned aerial vehicle detection auxiliary device which comprises an unmanned aerial vehicle body, the bottom of the unmanned aerial vehicle body is fixedly connected with a mounting frame, the bottom of the mounting frame is fixedly connected with a U-shaped box, and the rear side of the U-shaped box is movably connected with a rotating block through a bearing. The front side of the rotating block penetrates to the rear side of the inner wall of the U-shaped box and is fixedly connected with a first bevel gear, the left side and the right side of the first bevel gear are engaged with second bevel gears, the outer sides of the second bevel gears are fixedly connected with a transverse rod, and the surface of the transverse rod is movably connected with the inner wall of the U-shaped box through a bearing. According to the utility model, the rotating block is firstly rotated, the first rotating block screw rotates, the first screw drives the detector mounting rack and the detection equipment to move longitudinally, the longitudinal position of the detection equipment can be adjusted, then the rectangular sleeve transversely slides on the surface of the rectangular rod, and the transverse position of the detection equipment can be adjusted. Therefore, the gravity center adjusting function is achieved.
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Description

A drone detection auxiliary device Technical Field

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

[0002] Drone detection refers to the process of detecting, identifying, and tracking aerial drones using various technical means. These detection technologies each have their own advantages and disadvantages and are suitable for different scenarios and needs. For example, radar detection is suitable for long-distance and high-altitude targets, while photoelectric detection is more suitable for daytime and nighttime use. With the development of technology, the application of multi-source data fusion and artificial intelligence algorithms has made drone detection more intelligent and efficient.

[0003] When drones are conducting reconnaissance, they need to carry additional detection equipment. After carrying the additional detection equipment, these extra payloads will change the original mass distribution of the drone, causing the overall center of gravity of the drone to shift, thereby reducing the flight stability of the drone. Summary of the Invention

[0004] To address the problems mentioned in the background art, the purpose of this utility model is to provide a drone detection auxiliary device with the advantage of center of gravity adjustment function. This solves the problem that when additional detection equipment is mounted, these additional loads will change the original mass distribution of the drone, causing the overall center of gravity of the drone to shift, thereby reducing the flight stability of the drone.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a drone detection auxiliary device, comprising a drone body, a mounting frame fixedly connected to the bottom of the drone body, a U-shaped box fixedly connected to the bottom of the mounting frame, a rotating block movably connected to the rear side of the U-shaped box via a bearing, a helical gear one fixedly connected to the front side of the rotating block extending through to the rear side of the inner wall of the U-shaped box, helical gear two meshing on both sides of the helical gear one, a crossbar fixedly connected to the outer side of the helical gear two, the surface of the crossbar movably connected to the inner wall of the U-shaped box via a bearing, a helical gear three fixedly connected to the outer side of the crossbar, a helical gear four meshing on the front side of the helical gear three, a screw one fixedly connected to the front side of the helical gear four, the front side of the screw one movably connected to the front side of the inner wall of the U-shaped box via a bearing, a threaded sleeve threadedly connected to the surface of the screw one, a rectangular rod fixedly connected to the inner side of the threaded sleeve, and a lateral adjustment mechanism sleeved on the surface of the rectangular rod.

[0006] As a preferred embodiment of this utility model, the lateral adjustment mechanism includes a rectangular sleeve slidably connected to the surface of a rectangular rod, with screws threaded to both the front and rear sides of the rectangular sleeve, the inner side of the screws penetrating into the interior of the rectangular sleeve and fixedly connected to a friction block, and a detector mounting bracket fixedly connected to the bottom of the rectangular sleeve.

[0007] As a preferred embodiment of this invention, the bottom of the U-shaped box is fixedly connected with two support legs.

[0008] As a preferred embodiment of this invention, the bottom of the support leg is fixedly connected with an anti-slip pad.

[0009] As a preferred embodiment of this invention, a knob is fixedly connected to the outer side of the screw, and the knob is T-shaped.

[0010] As a preferred embodiment of this invention, friction strips are fixedly connected to both the front and rear sides of the rectangular rod.

[0011] As a preferred embodiment of this invention, the surface of the rotating block is provided with anti-slip texture.

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

[0013] 1. In this utility model, the rotating block is first rotated. As the rotating block screw rotates, the screw drives the detector mounting bracket and the detection equipment to move longitudinally. At this time, the longitudinal position of the detection equipment can be adjusted. Then, the rectangular sleeve slides laterally on the surface of the rectangular rod. At this time, the lateral position of the detection equipment can be adjusted, thereby achieving the effect of center of gravity adjustment.

[0014] 2. By setting a lateral adjustment mechanism, this utility model can adjust the position of the detection device laterally, thereby increasing the adjustment range of the detection device's position. Attached Figure Description

[0015] Figure 1 is a three-dimensional view of the main structure of the UAV of this utility model;

[0016] Figure 2 is a bottom view of the main structure of the UAV of this utility model;

[0017] Figure 3 is a top sectional view of the U-shaped box structure of this utility model;

[0018] Figure 4 is a top sectional view of the lateral adjustment mechanism structure of this utility model.

[0019] In the diagram: 1. UAV body; 2. Mounting bracket; 3. U-shaped box; 4. Rotating block; 5. Helical gear one; 6. Helical gear two; 7. Crossbar; 8. Helical gear three; 9. Helical gear four; 10. Screw one; 11. Screw sleeve; 12. Rectangular rod; 181. Rectangular sleeve; 182. Screw two; 183. Friction block; 184. Detector mounting bracket; 13. Leg; 14. Anti-slip pad; 15. Knob; 16. Friction strip; 17. Anti-slip texture; 18. Lateral adjustment mechanism. Detailed Implementation

[0020] 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.

[0021] As shown in Figures 1 to 4, the present invention provides a drone detection auxiliary device, including a drone body 1. A mounting frame 2 is fixedly connected to the bottom of the drone body 1. A U-shaped box 3 is fixedly connected to the bottom of the mounting frame 2. A rotating block 4 is movably connected to the rear side of the U-shaped box 3 via a bearing. A helical gear 5 is fixedly connected to the front side of the rotating block 4 through the rear side of the inner wall of the U-shaped box 3. Helical gears 6 mesh on both sides of the helical gear 5. A crossbar 7 is fixedly connected to the outer side of the helical gears 6. The surface of the crossbar 7 is movably connected to the inner wall of the U-shaped box 3 via a bearing. A helical gear 8 is fixedly connected to the outer side of the crossbar 7. A helical gear 9 meshes on the front side of the helical gear 8. A screw 10 is fixedly connected to the front side of the helical gear 9. The front side of the screw 10 is movably connected to the front side of the inner wall of the U-shaped box 3 via a bearing. A screw sleeve 11 is threadedly connected to the surface of the screw 10. A rectangular rod 12 is fixedly connected to the inner side of the screw sleeve 11. A lateral adjustment mechanism 18 is sleeved on the surface of the rectangular rod 12.

[0022] Referring to Figure 4, the lateral adjustment mechanism 18 includes a rectangular sleeve 181 that is slidably connected to the surface of the rectangular rod 12. Both the front and rear sides of the rectangular sleeve 181 are threaded with screws 182. The inner side of the screws 182 extends into the interior of the rectangular sleeve 181 and is fixedly connected with a friction block 183. The bottom of the rectangular sleeve 181 is fixedly connected with a detector mounting bracket 184.

[0023] As a technical optimization of this utility model, by setting the lateral adjustment mechanism 18, the position of the detection device can be adjusted laterally, thereby increasing the adjustment range of the detection device position.

[0024] Referring to Figure 1, the bottom of the U-shaped box 3 is fixedly connected with two support legs 13.

[0025] As a technical optimization of this utility model, by setting the support legs 13, the drone body 1 can be supported, preventing the detection equipment from landing first when the drone body 1 takes off and lands.

[0026] Referring to Figure 1, the bottom of the support leg 13 is fixedly connected with an anti-slip pad 14.

[0027] As a technical optimization of this utility model, by setting the anti-slip pad 14, the friction between the outrigger 13 and the ground can be increased, preventing the drone body 1 from slipping and deviating during take-off and landing.

[0028] Referring to Figure 4, a knob 15 is fixedly connected to the outside of the screw. The knob 15 is T-shaped.

[0029] As a technical optimization of this utility model, by setting the knob 15, the contact area between the user's hands and the screw 182 can be increased, making it easier for the user to rotate the screw 182.

[0030] Referring to Figure 4, friction strips 16 are fixedly connected to both the front and rear sides of the rectangular rod 12.

[0031] As a technical optimization of this utility model, by setting the friction strip 16, the friction force between the friction block 183 and the rectangular rod 12 can be increased, which makes it more convenient for users to use.

[0032] Referring to Figure 3, the surface of the rotating block 4 is provided with anti-slip texture 17.

[0033] As a technical optimization of this utility model, by setting anti-slip texture 17, the friction between the user's hands and the rotating block 4 can be increased, preventing the rotating block 4 from slipping out of the hand during use.

[0034] The working principle and usage process of this utility model are as follows: In use, firstly, the detection device is fixed to the bottom of the detector mounting bracket 184 using bolts. Next, the rotating block 4 is rotated, which drives the first helical gear 5 to rotate. The first helical gear 5 drives the second helical gear 6 to rotate, which in turn drives the crossbar 7 to rotate. The crossbar 7 drives the third helical gear 8 to rotate, which in turn drives the fourth helical gear 9 and the first screw 10 to rotate. The first screw 10 drives the screw sleeve 11 to move longitudinally, which in turn drives the rectangular rod 12 to move longitudinally. The rectangular rod 12 drives the rectangular sleeve 181, the detector mounting bracket 184, and the detection device to move longitudinally. At this point, the detection device can be moved according to the UAV body 1. The longitudinal position of the detection device is adjusted by adjusting the center of gravity. Then, the rectangular sleeve 181 slides laterally on the surface of the rectangular rod 12. The rectangular sleeve 181 drives the detector mounting bracket 184 and the detection device to move laterally. At this time, the lateral position of the detection device can be adjusted according to the center of gravity of the UAV body 1. After the adjustment is completed, the knob 15 is turned. The knob 15 drives the screw 182 to rotate. The screw 182 moves inward using the thread. The screw 182 drives the friction block 183 to move inward, so that the friction block 183 and the friction strip 16 are tightly fitted. At this time, the rectangular sleeve 181 can be fixed on the rectangular rod 12 to achieve the effect of center of gravity adjustment.

[0035] In summary, this UAV detection auxiliary device, by setting up the UAV body 1, mounting frame 2, U-shaped box 3, rotating block 4, helical gear 1 5, helical gear 2 6, crossbar 7, helical gear 3 8, helical gear 4 9, screw 1 10, screw sleeve 11, rectangular rod 12, and lateral adjustment mechanism 18, solves the problem that when additional detection equipment is mounted, these additional loads will change the original mass distribution of the UAV, causing the overall center of gravity of the UAV to shift, thus reducing the flight stability of the UAV.

[0036] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0037] 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. An unmanned aerial vehicle detection assistance device comprising an unmanned aerial vehicle body (1), characterized in that: A mounting bracket (2) is fixedly connected to the bottom of the UAV body (1). A U-shaped box (3) is fixedly connected to the bottom of the mounting bracket (2). A rotating block (4) is movably connected to the rear side of the U-shaped box (3) via a bearing. The front side of the rotating block (4) extends through to the rear side of the inner wall of the U-shaped box (3) and is fixedly connected to a helical gear (5). Helical gears (6) mesh on both the left and right sides of the helical gears (5). A crossbar (7) is fixedly connected to the outer side of the helical gears (6). The surface of the crossbar (7) is connected to the U-shaped box (3) via a bearing. The inner wall is movably connected, and a helical gear three (8) is fixedly connected to the outer side of the crossbar (7). A helical gear four (9) meshes with the front side of the helical gear three (8). A screw one (10) is fixedly connected to the front side of the helical gear four (9). The front side of the screw one (10) is movably connected to the front side of the inner wall of the U-shaped box (3) through a bearing. A screw sleeve (11) is threadedly connected to the surface of the screw one (10). A rectangular rod (12) is fixedly connected to the inner side of the screw sleeve (11). A transverse adjustment mechanism (18) is sleeved on the surface of the rectangular rod (12).

2. The unmanned aerial vehicle detection assistance device of claim 1, wherein: The lateral adjustment mechanism (18) includes a rectangular sleeve (181) slidably connected to the surface of the rectangular rod (12). The front and rear sides of the rectangular sleeve (181) are threaded with screws (182). The inner side of the screws (182) extends into the interior of the rectangular sleeve (181) and is fixedly connected with a friction block (183). The bottom of the rectangular sleeve (181) is fixedly connected with a detector mounting bracket (184).

3. The unmanned aerial vehicle detection assistance device of claim 1, wherein: The bottom of the U-shaped box (3) is fixedly connected with two support legs (13).

4. The unmanned aerial vehicle detection assistance device of claim 3, wherein: The bottom of the support leg (13) is fixedly connected to an anti-slip pad (14).

5. The UAV detection auxiliary device according to claim 2, characterized in that: A knob (15) is fixedly connected to the outside of the screw, and the knob (15) is T-shaped.

6. The unmanned aerial vehicle detection assistance device of claim 1, wherein: Friction strips (16) are fixedly connected to both the front and rear sides of the rectangular rod (12).

7. The unmanned aerial vehicle detection assistance device of claim 1, wherein: The surface of the rotating block (4) is provided with anti-slip texture (17).