An electronic countermeasure device for unmanned aerial vehicles

Abstract

This utility model relates to the field of electronic countermeasures equipment technology, specifically a drone electronic countermeasures device, comprising: a drone countermeasures device body, a control panel provided on the side wall of the drone countermeasures device body, and symmetrically fixed bosses provided on the side wall of the drone countermeasures device body, with protective glass rotatably connected to the bosses at both ends; a fixing component is provided on the drone countermeasures device body; by rotating the protective glass to cover the control panel until the pad is engaged with the side wall of the drone countermeasures device body, the compressed spring resets and pushes the locking block to reset and move, so that the back of the locking block engages with the first locking plate, thereby fixing the position of the pad, thus fixing the position of the protective glass to protect the control panel, preventing damage to the control panel in the event of a fall of the drone countermeasures device body, ensuring the normal use of the drone countermeasures device, and providing a detachable V-shaped elastic piece for easy popping up and rotating of the protective glass.

Description

Technical Field

[0001] This utility model relates to the field of electronic countermeasures equipment, specifically an electronic countermeasures device for unmanned aerial vehicles (UAVs). Background Technology

[0002] Chinese patent document CN222617736U discloses an electronic countermeasure device for unmanned aerial vehicles (UAVs), belonging to the field of UAV technology. It includes a main body of the UAV countermeasure device, an observation mirror mounted on the upper surface of the main body, and two mounting plates mounted on the lower surface of the main body. A rotating column is installed between the two mounting plates, and a support plate is rotatably mounted on the rotating column. A support column is mounted on the lower surface of the support plate, and a groove is formed on the lower surface of the support column. This UAV electronic countermeasure device, through the setting of support legs, hanging rings, and hooks, utilizes the extension rod and grooves to facilitate the retraction of the extension rod within the grooves. The hooks and hanging rings facilitate the easy retraction and fixation of the support column and support legs. By tilting the support legs at a certain angle, the ends of the support legs contact the placement surface, ensuring stable placement of the UAV countermeasure device and preventing wobbling.

[0003] However, in the above-mentioned solutions and existing technologies, the drone countermeasure equipment has a control panel on its side wall. After the drone countermeasure equipment is adjusted through the control panel, it is aimed at the drone for countermeasure. When the operator holds the drone countermeasure equipment and it is hit, the drone countermeasure equipment is easy to slip out of their hand and fall. Since the control panel of the drone countermeasure equipment lacks a protective device, when the drone countermeasure equipment slips out of their hand and falls, the control panel is easily damaged when it hits a hard object, which affects the normal use of the drone countermeasure equipment. Utility Model Content

[0004] The purpose of this invention is to provide an electronic countermeasure device for unmanned aerial vehicles (UAVs) to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: an electronic countermeasure device for unmanned aerial vehicles (UAVs), comprising: a main body of the UAV countermeasure device, a control panel provided on the side wall of the main body of the UAV countermeasure device, and symmetrically fixed protrusions provided on the side wall of the main body of the UAV countermeasure device, the protrusions being located on the upper and lower sides of the control panel, and protective glass being rotatably connected to the protrusions at both ends, the protective glass covering the control panel; a fixing component is provided on the main body of the UAV countermeasure device, the fixing component including a pad, a locking block, a protrusion, and a V-shaped elastic sheet.

[0006] Preferably, a pad is fixedly provided at the end of the protective glass, a first clamping plate is fixedly provided at the bottom of the pad, a second clamping plate is fixedly provided at the top of the pad, and a straight groove is provided on the side wall of the boss.

[0007] Preferably, the boss has a circular groove, a locking block is movably engaged in the straight groove, one end of the locking block is inclined, a fixing post is fixedly installed on the side wall of the locking block, and a lever is fixedly installed on the side wall of the locking block.

[0008] Preferably, a limiting block is fixedly installed at the end of the fixed column through the circular groove. The limiting block is movably engaged in the circular groove. A spring is sleeved on the fixed column. The spring engages with the locking block. The locking block engages with the first locking plate.

[0009] Preferably, the protrusion is fixedly mounted on the side wall of the main body of the UAV countermeasure device. A T-shaped groove is provided on the side wall of the protrusion, and a T-shaped block is inserted into the T-shaped groove. A V-shaped elastic sheet is fixedly mounted on the side wall of the T-shaped block. The other end of the V-shaped elastic sheet abuts against the side wall of the main body of the UAV countermeasure device, and the V-shaped elastic sheet is engaged with the second card plate.

[0010] Preferably, the bottom wall of the T-shaped groove is provided with a threaded groove, and the side wall of the T-shaped block is provided with a mounting hole, through which the screw passes and is threadedly connected to the threaded groove.

[0011] Compared with the prior art, the beneficial effects of this utility model are:

[0012] By rotating the protective glass to cover the control panel until the pad engages with the side wall of the drone countermeasure device, the compressed spring returns to its original position, pushing the locking block to move so that the back of the locking block engages with the first locking plate, thereby fixing the position of the pad. This fixes the position of the protective glass, protecting the control panel and preventing damage from impacts if the drone countermeasure device is dropped. This ensures the normal operation of the drone countermeasure device. A detachable V-shaped elastic piece is provided to facilitate the pop-up rotation of the protective glass. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of the structure of this utility model;

[0014] Figure 2 This is an exploded view of the structural connection of this utility model;

[0015] Figure 3 This utility model Figure 2 A magnified view of a portion of the image;

[0016] Figure 4 This is a half-sectional view of the boss structure connection of this utility model.

[0017] In the diagram: 1. Main body of the drone countermeasure equipment; 2. Control panel; 3. Boss; 4. Protective glass; 5. Pad; 6. First clamping plate; 7. Second clamping plate; 8. Straight groove; 9. Circular groove; 10. Clamping block; 11. Fixing post; 12. Limiting block; 13. Spring; 14. Paddle; 15. Protrusion; 16. T-slot; 17. T-block; 18. V-shaped elastic sheet; 19. Threaded groove; 20. Mounting hole. Detailed Implementation

[0018] To make the objectives, technical solutions, and advantages of this utility model clear and complete, the embodiments of this utility model will be further described in detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are only some, not all, embodiments of this utility model, and are merely used to explain the embodiments of this utility model. They are not intended to limit the embodiments of this utility model. All other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this utility model.

[0019] Please see Figures 1-4 The present invention provides the following two preferred embodiments:

[0020] Example 1: An electronic countermeasure device for unmanned aerial vehicles (UAVs) includes: a main body 1 for the UAV countermeasure device; a control panel 2 is provided on the side wall of the main body 1; symmetrical bosses 3 are fixedly provided on the side wall of the main body 1, the bosses 3 being located on the upper and lower sides of the control panel 2; protective glass 4 is rotatably connected to the bosses 3 at both ends, and the protective glass 4 covers the control panel 2; a fixing component is provided on the main body 1, the fixing component including a pad 5, a locking block 10, a protrusion 15, and a V-shaped elastic sheet 18; a pad 5 is fixedly provided at the end of the protective glass 4, and the bottom of the pad 5... A first locking plate 6 is fixedly installed at one end, and a second locking plate 7 is fixedly installed at the upper end of the pad 5. A straight groove 8 is opened on the side wall of the boss 3. A circular groove 9 is opened in the boss 3. A locking block 10 is movably engaged in the straight groove 8. One end of the locking block 10 is set with an inclined surface. A fixing post 11 is fixedly installed on the side wall of the locking block 10. A paddle 14 is fixedly installed on the side wall of the locking block 10. A limit block 12 is fixedly installed through the circular groove 9 at the end of the fixing post 11. The limit block 12 is movably engaged in the circular groove 9. A spring 13 is sleeved on the fixing post 11. The spring 13 is engaged with the locking block 10. The locking block 10 is engaged with the first locking plate 6.

[0021] In use, after adjusting the main body 1 of the drone countermeasure device via the control panel 2, rotate the protective glass 4 to cover the control panel 2 until the pad 5 engages with the side wall of the main body 1. During this process, the first locking plate 6 first contacts the inclined surface of the locking block 10. Then, as the protective glass 4 rotates, the first locking plate 6 presses against the inclined surface of the locking block 10, thereby pushing the locking block 10 to move and compress the spring 13. The limiting block 12 is movably engaged in the circular groove 9 to prevent the locking block 10 from falling off. After the pad 5 engages with the side wall of the main body 1, the first locking plate 6 separates from the inclined surface of the locking block 10. The compressed spring 13 resets and pushes the locking block 10 to reset and move, so that the back of the locking block 10 engages with the first locking plate 6, thereby fixing the position of the pad 5. This ensures that the protective glass 4, after covering the control panel 2, is fixed in position, protecting the control panel 2 and preventing damage to the control panel 2 in the event of a fall of the main body 1, thus ensuring the normal operation of the drone countermeasure device.

[0022] Example 2: Based on Example 1, the protrusion 15 is fixedly installed on the side wall of the main body 1 of the UAV countermeasure device. A T-shaped groove 16 is provided on the side wall of the protrusion 15. A T-shaped block 17 is inserted into the T-shaped groove 16. A V-shaped elastic piece 18 is fixedly installed on the side wall of the T-shaped block 17. The other end of the V-shaped elastic piece 18 abuts against the side wall of the main body 1 of the UAV countermeasure device. The V-shaped elastic piece 18 is engaged with the second clamping plate 7. A threaded groove 19 is provided on the bottom wall of the T-shaped groove 16. An installation hole 20 is provided on the side wall of the T-shaped block 17. A screw passes through the installation hole 20 and is threadedly connected to the threaded groove 19.

[0023] When in use, the protective glass 4 covers the control panel 2 and is fixed in position. At this time, the second clamping plate 7 presses the bent part of the V-shaped elastic piece 18, causing the V-shaped elastic piece 18 to deform elastically. When the control panel 2 needs to be readjusted, the lever 14 is moved to control the clamping block 10 to separate from the first clamping plate 6. The V-shaped elastic piece 18 then resets and pops open the second clamping plate 7, making it easy to rotate the protective glass 4 to expose the control panel 2. After long-term use, the screws at the mounting hole 20 and the threaded groove 19 are unscrewed, and the T-shaped block 17 is separated from the T-groove 16, so that the worn V-shaped elastic piece 18 can be replaced.

[0024] 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 electronic countermeasure device for unmanned aerial vehicles (UAVs), comprising: The main body (1) of the anti-drone device is provided with a control panel (2) on the side wall of the anti-drone device (1). Bosses (3) are symmetrically fixed on the side wall of the anti-drone device (1). The bosses (3) are located on the upper and lower sides of the control panel (2). The protective glass (4) is rotatably connected to the bosses (3) at both ends. The protective glass (4) covers the control panel (2). The feature is that the main body (1) of the UAV countermeasure device is provided with a fixing component, which includes a pad (5), a locking block (10), a protrusion (15), and a V-shaped elastic sheet (18).

2. The electronic countermeasure device for unmanned aerial vehicles according to claim 1, characterized in that: A pad (5) is fixedly installed at the end of the protective glass (4), a first clamping plate (6) is fixedly installed at the bottom of the pad (5), a second clamping plate (7) is fixedly installed at the top of the pad (5), and a straight groove (8) is opened on the side wall of the boss (3).

3. The electronic countermeasure device for unmanned aerial vehicles according to claim 2, characterized in that: The boss (3) has a circular groove (9) and a locking block (10) is movably engaged in the straight groove (8). One end of the locking block (10) is inclined. A fixing post (11) is fixedly installed on the side wall of the locking block (10) and a paddle (14) is fixedly installed on the side wall of the locking block (10).

4. The electronic countermeasure device for unmanned aerial vehicles according to claim 3, characterized in that: The end of the fixed column (11) is fixedly provided with a limiting block (12) through the circular groove (9). The limiting block (12) is movably snapped into the circular groove (9). The fixed column (11) is sleeved with a spring (13). The spring (13) is snapped into the locking block (10). The locking block (10) is snapped into the first locking plate (6).

5. The electronic countermeasure device for unmanned aerial vehicles according to claim 1, characterized in that: The protrusion (15) is fixedly installed on the side wall of the main body (1) of the UAV countermeasure device. A T-shaped groove (16) is provided on the side wall of the protrusion (15). A T-shaped block (17) is inserted into the T-shaped groove (16). A V-shaped elastic piece (18) is fixedly installed on the side wall of the T-shaped block (17). The other end of the V-shaped elastic piece (18) abuts against the side wall of the main body (1) of the UAV countermeasure device. The V-shaped elastic piece (18) is engaged with the second card plate (7).

6. The electronic countermeasure device for unmanned aerial vehicles according to claim 5, characterized in that: The bottom wall of the T-shaped groove (16) is provided with a threaded groove (19), and the side wall of the T-shaped block (17) is provided with a mounting hole (20). The screw passes through the mounting hole (20) and is threadedly connected to the threaded groove (19).

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