Detection vehicle for anti-unmanned aerial vehicle equipment

Abstract

The utility model discloses a detection vehicle for anti-unmanned aerial vehicle equipment, which comprises a vehicle body, the top surface of the vehicle body is fixedly connected with a carrying plate, one side of the top surface of the carrying plate is provided with a double-shaft moving mechanism, the double-shaft moving mechanism is provided with an interference assembly, and one side of the top surface of the carrying plate far away from the double-shaft moving mechanism is provided with a detection assembly. The double-shaft moving mechanism comprises a top groove formed in the top face of the carrying plate, and two side plates are fixedly connected to the two sides of the top groove. The double-shaft moving mechanism is adopted to carry the interference assembly, the double-shaft moving mechanism carries the interference assembly through the sliding rod to move in one direction, the sliding sleeve drives the interference assembly to move in the other direction, the position of the interference assembly can be adjusted within the range of the top groove, the vehicle body does not need to be operated to move when fine adjustment is needed, and more convenience is achieved. The interference assembly drives the interference radar to rotate through the rotating table, the angle of the interference radar can be adjusted through the rotating block, multi-angle adjustment of the interference radar is achieved, and the unmanned aerial vehicle can be interfered more accurately.

Description

Technical Field

[0001] The utility model relates to the technical field of anti-UAV equipment, in particular to a detection vehicle for anti-UAV equipment. Background Art

[0002] Unmanned aerial vehicles, or UAVs, are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices, or are operated completely or intermittently autonomously by on-board computers. With the rapid increase in the number of civilian UAVs, the number of various "illegal" or even "illegal" black flying incidents has also increased rapidly. Therefore, counter-detection methods are often used to prevent and solve problems. Among them, anti-UAV detection vehicles are easy to move and can detect in a large area. They are widely used in the field of anti-UAVs. Currently, detection vehicles are equipped with UAV detection mechanisms and UAV countermeasures. UAV detection mechanisms use multi-spectrum scanning methods to detect drones that fly into the air. The UAV anti-control mechanism uses jammers to interfere with UAVs, such as radars. For example, the Chinese utility model patent with the authorization announcement number CN214375266U discloses an anti-UAV mobile detection and control vehicle, including a spectrum detection device, a control device and a mobile vehicle. The spectrum detection device and the control device are both arranged on the roof of the mobile vehicle. A control console is arranged in the mobile vehicle. The spectrum detection device and the control device are connected by signal transmission, and the control device and the control console are connected by signal transmission. However, the current anti-UAV detection vehicle has the following defects:

[0003] The jamming mechanism in the current detection vehicle is directly fixed on the vehicle body. When the position needs to be fine-tuned during jamming of the drone, the vehicle body needs to be moved, which is inconvenient to operate. In addition, the direction of the jamming mechanism is also fixed, which makes it inconvenient to adjust the angle, and the position is not accurate enough during jamming.

[0004] To this end, we propose an anti-UAV equipment detection vehicle to solve the above problems. Utility Model Content

[0005] The purpose of the utility model is to provide a detection vehicle for anti-UAV equipment to solve the problems raised in the above-mentioned background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a detection vehicle for anti-UAV equipment, comprising a vehicle body, the top surface of the vehicle body is fixedly connected to a mounting plate, a double-axis moving mechanism is arranged on one side of the top surface of the mounting plate, an interference component is arranged on the double-axis moving mechanism, and a detection component is arranged on the side of the top surface of the mounting plate away from the double-axis moving mechanism;

[0007] The biaxial moving mechanism comprises a top groove provided on the top surface of the mounting plate, two side plates are fixedly connected on both sides of the top groove, two side slide grooves are provided on one side of the two side plates close to each other, two side sliders are horizontally slidably connected in the two side slide grooves, a sliding rod is horizontally fixedly connected between the two side sliders, a sliding sleeve is horizontally slidably sleeved on the sliding rod, and the interference component is arranged on the top surface of the sliding sleeve;

[0008] The interference component includes a first hinge seat, the first hinge seat is fixed on the top surface of the sliding sleeve, the first hinge seat is rotatably connected to one end of the first support rod, the other end of the first support rod is fixed to the base, the surface of the base is rotatably connected to the rotating table, the rotating table is fixed to the third hinge seat, the third hinge seat is rotatably connected to the rotating block, and the end of the rotating block is fixed to the interference radar.

[0009] Preferably, the detection assembly includes a second hinge seat fixedly connected to the top surface of the mounting plate, the second hinge seat is rotatably connected to the second support rod, the end of the second support rod is fixedly connected to the spectrum detector, the side wall of the second hinge seat is fixedly connected to the sixth servo reduction motor, and the shaft end of the sixth servo reduction motor is fixedly connected to the shaft of the second support rod.

[0010] Preferably, a transmission cavity is opened inside the mounting plate near the top groove position, the transmission cavity is horizontally rotatably connected to a driving long rod, the driving long rod is fixedly sleeved with two driving pulleys near two side plates, the side plate is rotatably connected to a driven pulley at one end away from the transmission cavity, a synchronous belt is sleeved on the driving pulley and the driven pulley, the side slider is fixedly connected to the synchronous belt, one end of the transmission cavity is fixedly connected to a first servo reduction motor, and the rotating shaft end of the first servo reduction motor is fixedly connected to the end of the driving long rod.

[0011] Preferably, a top sliding groove is provided on the top surface of the sliding rod, a top sliding block is fixedly connected to the inner top surface of the sliding sleeve, a screw rod is rotatably connected in the top sliding groove, a threaded sleeve is fixedly connected to the top sliding block, the screw rod is threadedly connected to the threaded sleeve, the bottom surface of one end of the sliding rod is fixedly connected to the second servo reduction motor, the top end of the rotating shaft of the second servo reduction motor is located inside the sliding rod and fixedly connected to the driving bevel gear, the end of the screw rod close to the driving bevel gear is fixedly connected to the driven bevel gear, and the driving bevel gear is meshedly connected to the driven bevel gear.

[0012] Preferably, one side of the base is fixedly connected to the fourth servo reduction motor, the shaft end of the fourth servo reduction motor is fixedly connected to the driving gear, the peripheral side of the rotating table is fixedly sleeved with the driven gear ring, and the driving gear is meshedly connected to the driven gear ring.

[0013] The side wall of the first hinge seat is fixedly connected to the third servo reduction motor, the end of the third servo reduction motor shaft is fixedly connected to the first support rod shaft, the side wall of the third hinge seat is fixedly connected to the fifth servo reduction motor, the end of the fifth servo reduction motor shaft is fixedly connected to the rotating block shaft, and the top side wall of the first support rod is fixedly connected to the step block.

[0014] Compared with the prior art, the beneficial effects of the utility model are:

[0015] The utility model adopts a dual-axis moving mechanism to carry the interference component. The dual-axis moving mechanism carries the interference component to move in one direction through a sliding rod, and the sliding sleeve drives the interference component to move in another direction. In this way, the interference component can adjust its position within the top groove range. When fine-tuning is required, there is no need to operate the vehicle body to move, which is more convenient; the interference component drives the interference radar to rotate through the rotating table, and the angle of the interference radar can be adjusted through the turning block, thereby realizing multi-angle adjustment of the interference radar, which is convenient for more accurate interference with drones. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the main structure in the first and second embodiments of the utility model;

[0017] Figure 2 It is a schematic diagram of the structure of the main body in the first and second embodiments of the utility model when in operation;

[0018] Figure 3 It is a schematic diagram of the cross-section structure of the mounting plate in the first and second embodiments of the utility model;

[0019] Figure 4 It is a structural schematic diagram of the interference component in the second embodiment of the utility model.

[0020] In the figure: 1, vehicle body; 2, mounting plate; 3, dual-axis moving mechanism; 4, interference component; 5, detection component; 31, top groove; 32, side plate; 33, side slide groove; 34, side slider; 35, sliding rod; 36, sliding sleeve; 37, transmission cavity; 38, driving long rod; 39, driving pulley; 310, driven pulley; 311, synchronous belt; 312, first servo reduction motor; 313, top slide groove; 314, top slider; 315, screw rod; 316, threaded sleeve; 317, second servo reduction motor ; 318, active bevel gear; 319, driven bevel gear; 41, first hinge seat; 42, first support rod; 43, base; 44, rotating table; 45, third hinge seat; 46, rotating block; 47, interference radar; 48, third servo reduction motor; 49, fourth servo reduction motor; 410, active gear; 411, driven gear ring; 412, fifth servo reduction motor; 413, stepping block; 51, second hinge seat; 52, second support rod; 53, spectrum detector; 54, sixth servo reduction motor. DETAILED DESCRIPTION

[0021] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0022] Embodiment 1:

[0023] See also Figure 1-3 The utility model provides a technical solution: a detection vehicle for anti-UAV equipment, comprising a vehicle body 1, a mounting plate 2 is fixedly connected to the top surface of the vehicle body 1, a double-axis moving mechanism 3 is arranged on one side of the top surface of the mounting plate 2, an interference component 4 is arranged on the double-axis moving mechanism 3, and a detection component 5 is arranged on the side of the top surface of the mounting plate 2 away from the double-axis moving mechanism 3;

[0024] The double-axis moving mechanism 3 includes a top groove 31 provided on the top surface of the mounting plate 2, two side plates 32 are fixedly connected on both sides of the top groove 31, two side slide grooves 33 are provided on one side of the two side plates 32 close to each other, two side sliders 34 are horizontally slidably connected in the two side slide grooves 33, a sliding rod 35 is horizontally fixed between the two side sliders 34, a sliding sleeve 36 is horizontally slidably sleeved on the sliding rod 35, and an interference component 4 is arranged on the top surface of the sliding sleeve 36. The double-axis moving mechanism 3 is used to carry the interference component 4, and the double-axis moving mechanism 3 carries the interference component 4 in one direction through the sliding rod 35, and the sliding sleeve 36 drives the interference component 4 to move in the other direction, so that the interference component 4 can adjust its position within the range of the top groove 31, and when fine-tuning is required, there is no need to operate the vehicle body 1 to move, which is more convenient;

[0025] The interference component 4 includes a first hinge seat 41, which is fixed on the top surface of the sliding sleeve 36. The first hinge seat 41 is rotatably connected to one end of the first support rod 42, and the other end of the first support rod 42 is fixed to the base 43. The surface of the base 43 is rotatably connected to the rotating table 44. The rotating table 44 is fixed with a third hinge seat 45, which is rotatably connected to a rotating block 46. The end of the rotating block 46 is fixed to an interference radar 47. The interference radar 47 is driven to rotate by the rotating table 44, and the angle of the interference radar 47 can be adjusted by the rotating block 46, thereby realizing multi-angle adjustment of the interference radar 47, which is convenient for more precise interference with drones.

[0026] Embodiment 2:

[0027] See also Figure 1-4, which is the second embodiment of the utility model. This embodiment is based on the previous embodiment. The detection component 5 includes a second hinge seat 51 fixedly connected to the top surface of the mounting plate 2, the second hinge seat 51 is rotatably connected to the second support rod 52, the end of the second support rod 52 is fixedly connected to the spectrum detector 53, the side wall of the second hinge seat 51 is fixedly connected to the sixth servo reduction motor 54, the shaft end of the sixth servo reduction motor 54 is fixedly connected to the shaft of the second support rod 52, the second support rod 52 is driven to rotate into a vertical state by the sixth servo reduction motor 54, and the spectrum detector 53 determines the UAV within the radius and height range by spectrum scanning.

[0028] A transmission cavity 37 is provided inside the mounting plate 2 near the top groove 31, and a driving long rod 38 is connected to the transmission cavity 37 for horizontal rotation. The driving long rod 38 is fixedly sleeved with two active pulleys 39 near the two side plates 32, and the side plate 32 is rotatably connected to a driven pulley 310 at one end away from the transmission cavity 37. A synchronous belt 311 is sleeved on the active pulley 39 and the driven pulley 310, and a side slider 34 is fixedly connected to the synchronous belt 311. One end of the transmission cavity 37 is fixedly connected to a first servo reduction motor 312, and a rotating shaft end of the first servo reduction motor 312 is fixedly connected to an end of the driving long rod 38. The first servo reduction motor 312 is used to drive the two side sliders 34 to move, thereby driving the sliding rod 35 to move.

[0029] A top slide groove 313 is provided on the top surface of the sliding rod 35, and a top slider 314 is fixedly connected to the inner top surface of the sliding sleeve 36. A screw rod 315 is rotatably connected in the top slide groove 313, and a threaded sleeve 316 is fixedly connected to the top slider 314. The screw rod 315 is threadedly connected to the threaded sleeve 316. The bottom surface of one end of the sliding rod 35 is fixedly connected to the second servo reduction motor 317. The top end of the rotating shaft of the second servo reduction motor 317 is located inside the sliding rod 35 and is fixedly connected to the driving bevel gear 318. One end of the screw rod 315 close to the driving bevel gear 318 is fixedly connected to the driven bevel gear 319. The driving bevel gear 318 is meshedly connected to the driven bevel gear 319, and the top slider 314 is driven to move by the second servo reduction motor 317, thereby driving the interference component 4 to move.

[0030] One side of the base 43 is fixedly connected to the fourth servo reduction motor 49, the shaft end of the fourth servo reduction motor 49 is fixedly connected to the driving gear 410, the peripheral side of the rotating table 44 is fixedly sleeved with the driven gear ring 411, and the driving gear 410 is meshedly connected to the driven gear ring 411 to drive the rotating table 44 to rotate.

[0031] The side wall of the first hinge seat 41 is fixedly connected to the third servo reduction motor 48, the end of the rotating shaft of the third servo reduction motor 48 is fixedly connected to the rotating shaft of the first support rod 42, the side wall of the third hinge seat 45 is fixedly connected to the fifth servo reduction motor 412, the end of the rotating shaft of the fifth servo reduction motor 412 is fixedly connected to the rotating shaft of the rotating block 46, and the top side wall of the first support rod 42 is fixedly connected to the building block 413. When in a non-operating state, the first support rod 42 is in a horizontal state, and at this time, the building block 413 can be supported on the sliding rod 35.

[0032] Embodiment 3:

[0033] See also Figure 1-4 , which is the third embodiment of the utility model. This embodiment is based on the above two embodiments. After the utility model reaches the detection position, the first support rod 42 in the interference component 4 is in a vertical state, and the second support rod 52 in the detection component 5 is in a vertical state. The spectrum detector 53 determines the position and model of the drone within the range by spectrum scanning, and interferes with it through the interference radar 47; the utility model adopts a dual-axis moving mechanism 3 to carry the interference component 4, and the dual-axis moving mechanism 3 carries the interference component 4 in one direction through the sliding rod 35, and the sliding sleeve 36 drives the interference component 4 to move in another direction. In this way, the interference component 4 can adjust its position within the range of the top groove 31. When fine-tuning is required, there is no need to operate the vehicle body 1 to move, which is more convenient; the interference component 4 drives the interference radar 47 to rotate through the rotating table 44, and the angle of the interference radar 47 can be adjusted through the rotating block 46, thereby realizing multi-angle adjustment of the interference radar 47, which is convenient for more accurate interference with drones.

[0034] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A detection vehicle for anti-UAV equipment, comprising a vehicle body (1), characterized in that: The top surface of the vehicle body (1) is fixedly connected to a carrying plate (2); a double-axis moving mechanism (3) is arranged on one side of the top surface of the carrying plate (2); an interference component (4) is arranged on the double-axis moving mechanism (3); and a detection component (5) is arranged on the side of the top surface of the carrying plate (2) away from the double-axis moving mechanism (3); The dual-axis moving mechanism (3) comprises a top groove (31) provided on the top surface of the mounting plate (2), two side plates (32) are fixedly connected on both sides of the top groove (31), two side sliding grooves (33) are provided on one side of the two side plates (32) close to each other, two side sliding blocks (34) are horizontally slidably connected in the two side sliding grooves (33), a sliding rod (35) is horizontally fixedly connected between the two side sliding blocks (34), a sliding sleeve (36) is horizontally slidably sleeved on the sliding rod (35), and the interference component (4) is arranged on the top surface of the sliding sleeve (36); The interference component (4) includes a first hinge seat (41), the first hinge seat (41) is fixedly connected to the top surface of the sliding sleeve (36), the first hinge seat (41) is rotatably connected to one end of the first support rod (42), the other end of the first support rod (42) is fixedly connected to the base (43), the surface of the base (43) is rotatably connected to the rotating table (44), the rotating table (44) is fixedly connected to the third hinge seat (45), the third hinge seat (45) is rotatably connected to the rotating block (46), and the end of the rotating block (46) is fixedly connected to the interference radar (47).

2. The anti-UAV equipment detection vehicle according to claim 1, characterized in that: The detection assembly (5) comprises a second hinge seat (51) fixedly connected to the top surface of the mounting plate (2); the second hinge seat (51) is rotatably connected to a second support rod (52); the end of the second support rod (52) is fixedly connected to a spectrum detector (53); the side wall of the second hinge seat (51) is fixedly connected to a sixth servo reduction motor (54); the shaft end of the sixth servo reduction motor (54) is fixedly connected to the shaft of the second support rod (52).

3. The anti-UAV detection vehicle according to claim 1, characterized in that: A transmission cavity (37) is provided inside the mounting plate (2) near the top groove (31); a driving long rod (38) is horizontally rotatably connected inside the transmission cavity (37); the driving long rod (38) is fixedly sleeved with two driving pulleys (39) near the two side plates (32); one end of the side plate (32) away from the transmission cavity (37) is rotatably connected inside with a driven pulley (310); a synchronous belt (311) is sleeved on the driving pulley (39) and the driven pulley (310); the side slider (34) is fixedly connected with the synchronous belt (311); one end of the transmission cavity (37) is fixedly connected with a first servo reduction motor (312); and the rotating shaft end of the first servo reduction motor (312) is fixedly connected to the end of the driving long rod (38).

4. The anti-UAV detection vehicle according to claim 1, characterized in that: A top sliding groove (313) is provided on the top surface of the sliding rod (35), a top sliding block (314) is fixedly connected to the inner top surface of the sliding sleeve (36), a screw rod (315) is rotatably connected in the top sliding groove (313), a threaded sleeve (316) is fixedly connected to the top sliding block (314), the screw rod (315) is threadedly connected to the threaded sleeve (316), a bottom surface of one end of the sliding rod (35) is fixedly connected to a second servo reduction motor (317), a top end of a rotating shaft end of the second servo reduction motor (317) is located inside the sliding rod (35) and is fixedly connected to a driving bevel gear (318), one end of the screw rod (315) close to the driving bevel gear (318) is fixedly connected to a driven bevel gear (319), and the driving bevel gear (318) is meshedly connected to the driven bevel gear (319).

5. The anti-UAV detection vehicle according to claim 1, characterized in that: One side of the base (43) is fixedly connected to a fourth servo reduction motor (49), a rotating shaft end of the fourth servo reduction motor (49) is fixedly connected to a driving gear (410), a peripheral side of the rotating platform (44) is fixedly sleeved to a driven gear ring (411), and the driving gear (410) is meshingly connected to the driven gear ring (411).

6. The anti-UAV detection vehicle according to claim 1, characterized in that: The side wall of the first hinge seat (41) is fixedly connected to the third servo reduction motor (48), the end of the rotating shaft of the third servo reduction motor (48) is fixedly connected to the rotating shaft of the first support rod (42), the side wall of the third hinge seat (45) is fixedly connected to the fifth servo reduction motor (412), the end of the rotating shaft of the fifth servo reduction motor (412) is fixedly connected to the rotating shaft of the rotating block (46), and the top side wall of the first support rod (42) is fixedly connected to the stepping block (413).

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