Adjustable unmanned aerial vehicle countering device
By introducing a micro motor-driven adjustment rod and threaded hole system into the drone counter device, the angle and height adjustment of directional and omnidirectional counter equipment is achieved, and the problem that equipment can only adjust horizontal angle in the prior art is solved, and the problem of improving the level of the equipment in the existing technology is improved. The applicability and detection capability of the device are achieved.
Patent Information
- Application Number
- CN202421099475.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-20
- Publication Date
- 2024-12-17
- Estimated Expiration
- 2034-05-20
AI Technical Summary
During use, the existing drone counter device can only adjust the horizontal angle of the directional counter equipment, and cannot be used for detection needs in various environments, resulting in poor counter effect.
An adjustable drone counter device was designed, and the adjustment rod was driven by a micro motor to drive the lifting shell to rotate. The angle and height adjustment of the directional counter equipment and the omnidirectional counter equipment were realized in combination with threaded holes and threaded rods, which added Applicability and detection capabilities of the equipment.
It effectively improves the use effect and detection capabilities of the UAV counter device, can be suitable for detection needs in various environments, and enhances the counter strategy and functionality.
Smart Images
Figure CN222188033U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle countermeasures, in particular to an adjustable unmanned aerial vehicle countermeasure device. Background Art
[0002] Drone countermeasures refer to taking various means and measures to respond to and resist drone threats and attacks. With the rapid development of drone technology, the application scope of drones is becoming more and more extensive, but it also brings a series of security and privacy issues. In order to protect the safety of key facilities, personnel and sensitive areas, drone countermeasures have become more and more important. At present, there are two main types of drone countermeasures: omnidirectional countermeasures and directional countermeasures. The difference between them is that directional countermeasures are more focused and targeted, mainly targeting confirmed single or a few drone targets and the countermeasure distance is longer, while omnidirectional countermeasures focus on global defense and range coverage, and can deal with threats from multiple directions and multiple drone targets, but the countermeasure distance is shorter.
[0003] The utility model with the existing authorization application number CN202321903424.X discloses an adjustable UAV countermeasure device. By adopting the above-mentioned technical solution, a plurality of pulleys are rolled on the supporting rails, so that the working position of the mounting support plate and the directional countermeasure device arranged on the mounting support plate can be quickly adjusted. After reaching the specified position, the pulley can be locked by the locking member, so that the position adjustment of multiple directional countermeasure devices and the relative position adjustment of the directional countermeasure device and the omnidirectional countermeasure device can be finally realized, so that the countermeasure effect in the best range can be achieved according to the actual usage and the changing operation requirements. However, the above-mentioned technical solution cannot meet the applicability and detection capability of the UAV countermeasure device through only simple directional countermeasure devices and omnidirectional countermeasure devices during use, and can only adjust the horizontal angle of the directional countermeasure device during use, resulting in that the adjustment effect cannot be applied to the detection requirements of various environments, thereby reducing the use effect of the UAV countermeasure effect. Utility Model Content
[0004] 1. Technical issues to be resolved
[0005] In view of the shortcomings of the prior art, the utility model provides an adjustable drone counter-device, which has the advantages of increasing the detection capability and applicability of the drone counter-device, increasing the height adjustment capability of the drone counter-device, being suitable for detection in a variety of environments, and increasing the use effect.
[0006] (II) Technical solution
[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an adjustable UAV countermeasure device, comprising an UAV body and two groups of adjusting rods, the upper surface of the UAV body is fixedly connected with an adjusting shell, the inner wall of the adjusting shell is fixedly connected with a micro motor, the outer surface of each group of the adjusting rods is fixedly connected with the outer surface of the output end of the micro motor, the outer surface of each group of the adjusting rods is slidably connected with the inside of the adjusting shell, the upper surface of the adjusting shell is respectively fixedly connected with an integrated radar, a radio interference device and a radio detection device, the outer surface of each group of the adjusting rods is fixedly connected with two lifting shells, the inside of each of the lifting shells is slidably connected with a lifting plate, the outer surface of each of the lifting shells is provided with a plurality of identical threaded holes, the inner wall of each of the lifting plates is threadedly connected with a threaded rod together with the inner wall of one of the threaded holes, the upper surfaces of the four lifting plates are respectively fixedly connected with a directional countermeasure device and three omnidirectional countermeasure devices, the outer surface of each of the lifting plates is fixedly connected with two auxiliary plates, and the outer surface of each of the auxiliary plates is slidably connected with the inside of the lifting shell.
[0008] Preferably, an anti-skid pad is provided below the drone body, and the upper surface of the anti-skid pad is fixedly connected to the bottom surface of the drone body.
[0009] Preferably, a bearing is fixedly connected to the inner wall of the adjusting shell, and the output end of the micro motor is fixedly connected to the inner ring of the bearing.
[0010] Preferably, the inner wall of the adjusting shell is provided with four groups of stabilizing grooves, the interior of each group of the stabilizing grooves is slidably connected with a stabilizing plate, and the outer surface of each stabilizing plate is fixedly connected to the outer surface of the adjusting rod.
[0011] Preferably, two buffer pads are provided on the outer side of each of the stabilizing plates, and the outer surface of each of the buffer pads is fixedly connected to the outer surface of the stabilizing plate.
[0012] Preferably, the outer surface of each adjusting rod is fixedly connected to a reinforcement plate, and the outer surface of each reinforcement plate is fixedly connected to the outer surface of the lifting shell.
[0013] (III) Beneficial effects
[0014] Compared with the prior art, the utility model provides an adjustable drone countermeasure device, which has the following beneficial effects:
[0015] 1. The adjustable UAV countermeasure device is provided with an adjustment shell, an adjustment rod, a micro motor, a lifting shell, a lifting plate, a threaded hole, a threaded rod and an auxiliary plate, which can effectively adjust the angle and height of the directional countermeasure device and the omnidirectional countermeasure device, further increase the use effect of the countermeasure device, directly drive the adjustment rod to rotate through the micro motor, drive the lifting shell to rotate through the adjustment rod, and directly drive the directional countermeasure device and the omnidirectional countermeasure device to rotate and adjust the angle through the lifting shell, and then use the lifting plate to slide inside the lifting shell, and use the threaded holes and threaded rods to fix the position of the lifting plate, so as to facilitate the adjustment of the height of the directional countermeasure device and the omnidirectional countermeasure device, and achieve better application effect, avoiding the problem that only the horizontal angle of the directional countermeasure device can be adjusted during use, resulting in the adjustment effect cannot be applied to the detection needs of various environments.
[0016] 2. The adjustable UAV countermeasure device, by being provided with an integrated radar, a radio jammer and a radio detection device, can conveniently increase the detection capability and applicability of the UAV countermeasure device, effectively increase its functionality, and facilitate use. The integrated radar and the radio detection device can conveniently increase the detection capability of the UAV countermeasure device, and the radio jammer can conveniently increase the countermeasure strategy, increase its functionality and countermeasure means, and avoid the problem that the applicability and detection capability of the UAV countermeasure device cannot be met by using only simple directional countermeasure equipment and omnidirectional countermeasure equipment during use. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 This is a schematic diagram of the overall three-dimensional structure of the adjustable UAV countermeasure device of the utility model;
[0018] Figure 2 This is a schematic diagram of the three-dimensional structure of the regulating shell of the utility model;
[0019] Figure 3 It is a three-dimensional structural diagram of the unmanned aerial vehicle of the utility model;
[0020] Figure 4 This is a schematic diagram of the structure of the regulating shell of the utility model in a three-dimensional cutaway view;
[0021] Figure 5 It is a three-dimensional structural diagram of the adjusting rod of the utility model;
[0022] Figure 6 It is a three-dimensional structural schematic diagram of the lifting plate of the utility model.
[0023] In the figure: 1. Unmanned aerial vehicle body; 2. Adjustment shell; 3. Radio detection equipment; 4. Integrated radar; 5. Radio jammer; 6. Directional countermeasure equipment; 7. Omnidirectional countermeasure equipment; 8. Lifting shell; 9. Adjustment rod; 10. Threaded rod; 11. Reinforcement plate; 12. Anti-slip pad; 13. Stabilizing groove; 14. Micro motor; 15. Buffer pad; 16. Stabilizing plate; 17. Bearing; 18. Threaded hole; 19. Auxiliary plate; 20. Lifting plate. DETAILED DESCRIPTION
[0024] In order to better understand the purpose, structure and function of the present invention, an adjustable UAV countermeasure device of the present invention is further described in detail below in conjunction with the accompanying drawings.
[0025] See also Figure 1-6 The utility model discloses an adjustable UAV countermeasure device, comprising an UAV body 1 and two groups of adjusting rods 9, an upper surface of the UAV body 1 is fixedly connected with an adjusting shell 2, an inner wall of the adjusting shell 2 is fixedly connected with a micro motor 14, an outer surface of each group of adjusting rods 9 is fixedly connected with an outer surface of an output end of the micro motor 14, an anti-skid pad 12 is arranged under the UAV body 1, an upper surface of the anti-skid pad 12 is fixedly connected with the bottom surface of the UAV body 1, and the anti-skid pad 12 can increase the anti-skid effect of the bottom of the UAV body 1, so that it is convenient to land smoothly.
[0026] The outer surface of each set of adjustment rods 9 is slidably connected to the inside of the adjustment shell 2. The upper surface of the adjustment shell 2 is fixedly connected with an integrated radar 4, a radio jammer 5 and a radio detection device 3. The integrated radar 4 is a radar design method that integrates various components of a radar system into a single platform. This method can significantly reduce the volume and weight of the radar system, while improving the performance and reliability of the radar system. It can be used for navigation and terrain mapping of aircraft. In the military field, the integrated radar 4 can be used for battlefield reconnaissance and target tracking. The radio detection device 3 is also called a radar. It is a radio device that uses radio waves to determine the position of an object. The integrated radar 4 is used to increase the detection capability of the UAV countermeasure device. The radio jammer 5 mainly destroys or disrupts the enemy's radio communication by emitting specific electromagnetic waves, so as to achieve the tactical purpose of communication interruption, command failure or communication difficulty, and further increase the countermeasure effect of the UAV countermeasure device. The outer surface of each set of adjustment rods 9 is fixedly connected with two lifting shells 8. The inner wall of the adjustment shell 2 is fixedly connected with a bearing 17. The output end of the micro motor 14 is fixedly connected to the inner ring of the bearing 17. The bearing 17 can increase the stability of the rotation of the micro motor 14, effectively increasing the stabilization effect.
[0027] A lifting plate 20 is slidably connected to the interior of each lifting shell 8, and a number of identical threaded holes 18 are provided on the outer surface of each lifting shell 8. The inner wall of each lifting plate 20 is threadedly connected to the inner wall of one of the threaded holes 18 with a threaded rod 10. Four groups of stabilizing grooves 13 are provided on the inner wall of the adjusting shell 2, and a stabilizing plate 16 is slidably connected to the interior of each group of stabilizing grooves 13. The outer surface of each stabilizing plate 16 is fixedly connected to the outer surface of the adjusting rod 9. The stabilizing plate 16 and the stabilizing groove 13 can conveniently increase the stability of the adjusting rod 9 to prevent shaking and instability.
[0028] The upper surfaces of the four lifting plates 20 are respectively fixedly connected with a directional countermeasure device 6 and three omnidirectional countermeasure devices 7. The outer surface of each lifting plate 20 is fixedly connected with two auxiliary plates 19. Two buffer pads 15 are arranged on the outer side of each stabilizing plate 16. The outer surface of each buffer pad 15 is fixedly connected to the outer surface of the stabilizing plate 16. The buffer pads 15 can increase the buffering of the stabilizing plate 16 to prevent a large impact from causing vibration during equipment adjustment.
[0029] The outer surface of each auxiliary plate 19 is slidably connected to the inside of the lifting shell 8, and the outer surface of each adjusting rod 9 is fixedly connected to a reinforcement plate 11. The outer surface of each reinforcement plate 11 is fixedly connected to the outer surface of the lifting shell 8. Through the reinforcement plate 11, the connection between the adjusting rod 9 and the lifting shell 8 can be conveniently increased to prevent disconnection.
[0030] The working principle of the utility model is: first, the micro motor 14 is connected to the power supply, and then the directional counter-control device 6, the omnidirectional counter-control device 7, the integrated radar 4, the radio jammer 5 and the radio detection device 3 are connected to the computer processing technology. On the basis of the counter-control by the directional counter-control device 6 and the omnidirectional counter-control device 7, the integrated radar 4 and the radio detection device 3 can be used to conveniently increase the detection capability of the UAV counter-control device, and then the radio jammer 5 can be used to conveniently increase the overall counter-control strategy of the UAV, increase its functionality and counter-control means, and avoid the problem that the applicability and detection capability of the UAV counter-control device cannot be met by only simple directional counter-control devices 6 and omnidirectional counter-control devices 7 during use. When it is necessary to adjust the horizontal angles of the directional counter-control device 6 and the omnidirectional counter-control device 7, the micro motor 14 is directly used to drive the adjusting rod 9 to adjust the horizontal angle. The shell 2 rotates inside, and the lifting shell 8 is driven to rotate through the adjusting rod 9. The four lifting shells 8 can respectively drive the directional counter device 6 and the omnidirectional counter device 7 to adjust the angle. During the rotation of the micro motor 14, the distance between the four adjustment holes on the outside of the adjusting shell 2 is repeatedly adjusted. When it is necessary to adjust the height of the directional counter device 6 and the omnidirectional counter device 7, the threaded rod 10 is directly taken out, and the lifting plate 20 is lifted through the auxiliary plate 19. The lifting plate 20 can slide inside the lifting shell 8, and the lifting plate 20 can be fixed inside the lifting shell 8 by the threaded rod 10 and the threaded hole 18, which effectively increases the adjustment effect and increases the adjustment direction of the directional counter device 6 and the omnidirectional counter device 7, avoiding the problem that only the horizontal angle of the directional counter device 6 and the omnidirectional counter device 7 can be adjusted during use, resulting in the adjustment effect not being suitable for the detection needs of various environments.
[0031] It is understood that the present invention is described by some embodiments, and those skilled in the art are aware that various changes or equivalent substitutions may be made to these features and embodiments without departing from the spirit and scope of the present invention. In addition, under the teachings of the present invention, these features and embodiments may be modified to adapt to specific circumstances and materials without departing from the spirit and scope of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed herein, and all embodiments falling within the scope of the claims of this application are within the scope of protection of the present invention.
Claims
1. An adjustable drone countermeasure device, comprising a drone body (1) and two sets of adjustment rods (9), characterized in that: The upper surface of the unmanned aerial vehicle body (1) is fixedly connected to an adjustment shell (2), the inner wall of the adjustment shell (2) is fixedly connected to a micro motor (14), the outer surface of each group of the adjustment rods (9) is fixedly connected to the outer surface of the output end of the micro motor (14), the outer surface of each group of the adjustment rods (9) is slidably connected to the inside of the adjustment shell (2), the upper surface of the adjustment shell (2) is respectively fixedly connected to an integrated radar (4), a radio interference device (5) and a radio detection device (3), the outer surface of each group of the adjustment rods (9) is fixedly connected to two lifting shells (8), and each lifting shell ( 8) are slidably connected to the interior of each of the lifting shells (8), a plurality of identical threaded holes (18) are opened on the outer surface of each of the lifting shells (8), the inner wall of each of the lifting plates (20) is threadedly connected to the inner wall of one of the threaded holes (18) by a threaded rod (10), the upper surfaces of the four lifting plates (20) are respectively fixedly connected to a directional countermeasure device (6) and three omnidirectional countermeasure devices (7), the outer surface of each of the lifting plates (20) is fixedly connected to two auxiliary plates (19), and the outer surface of each of the auxiliary plates (19) is slidably connected to the interior of the lifting shell (8).
2. The adjustable drone countermeasure device according to claim 1, characterized in that: An anti-skid pad (12) is provided below the drone body (1), and the upper surface of the anti-skid pad (12) is fixedly connected to the bottom surface of the drone body (1).
3. The adjustable drone countermeasure device according to claim 1, characterized in that: A bearing (17) is fixedly connected to the inner wall of the adjustment housing (2), and the output end of the micro motor (14) is fixedly connected to the inner ring of the bearing (17).
4. The adjustable drone countermeasure device according to claim 1, characterized in that: The inner wall of the adjustment shell (2) is provided with four groups of stabilizing grooves (13), the interior of each group of the stabilizing grooves (13) is slidably connected to a stabilizing plate (16), and the outer surface of each stabilizing plate (16) is fixedly connected to the outer surface of the adjustment rod (9).
5. The adjustable UAV countermeasure device according to claim 4, characterized in that: Two buffer pads (15) are arranged on the outer side of each stabilizing plate (16), and the outer surface of each buffer pad (15) is fixedly connected to the outer surface of the stabilizing plate (16).
6. The adjustable drone countermeasure device according to claim 1, characterized in that: The outer surface of each adjusting rod (9) is fixedly connected to a reinforcing plate (11), and the outer surface of each reinforcing plate (11) is fixedly connected to the outer surface of the lifting shell (8).