Unmanned aerial vehicle detecting and locking device

Abstract

The utility model provides an unmanned aerial vehicle detecting and locking device which comprises a base, a rotary table, a first motor, a second motor, a radar device, an aiming device and a terminal console. The turntable is rotationally connected to the upper surface of the base; the first motor is fixed to the base, and the driving end is arranged upwards and fixed to the bottom of the rotary table so as to drive the rotary table to rotate circumferentially along the upper surface of the base. The second motor is fixed to the rotary table, and the driving end is arranged in the left-right direction and fixed to the aiming device so as to adjust the pitching angle of the aiming device. The radar device is fixed on the turntable for detecting the unmanned aerial vehicle; the first motor, the second motor, the radar device and the aiming device are all in communication connection with the terminal console; a weapon is fixed to the driving end of the second motor. The position of the unmanned aerial vehicle can be effectively detected, and locking striking is carried out.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane detection technical field, specifically, an unmanned plane detection and locking device. BACKGROUND

[0002] With the rapid development of unmanned plane technology, the application of unmanned plane is more and more extensive, and civil unmanned plane can be seen everywhere, but in specific area, such as in airport area, activity security and the like, the takeoff and landing of unmanned plane often cause serious interference to the scene, especially in airport area, serious accident of plane and people may occur, and the flight height of civil unmanned plane is between 50 meters and 120 meters, so that the ground personnel basically cannot intercept by conventional means, so it is very necessary to carry out counter-interception to unmanned plane in these cases. SUMMARY

[0003] The utility model solves the technical problem, provide a kind of unmanned plane detection and locking device, can effectively detect unmanned plane position and carry out locking attack.

[0004] The utility model provides a kind of unmanned plane detection and locking device, including base, rotary table, first motor, second motor, radar device, aiming device and terminal control console;Rotary table rotation is connected on the upper surface of base;First motor is fixed on the base, and drive end is set up and is fixed with rotary table bottom towards up, to drive rotary table to rotate along the circumferential surface of base upper surface;Second motor is fixed on rotary table and drive end is set along left and right direction and is fixed with aiming device, to adjust the pitch angle of aiming device;Radar device is fixed on rotary table for detecting unmanned plane;First motor, second motor, radar device and aiming device are all connected with terminal control console communication;Weapon is fixed on the drive end of second motor.

[0005] Compared with prior art, the following advantages are obtained: when the radar device detects the unmanned plane, the terminal control console controls the first motor and the second motor to work, so that the rotary table rotates circumferentially, and the pitch angle of the aiming device is adjusted to lock, which can effectively detect the position of the unmanned plane and lock.

[0006] In a possible implementation, the rotary table includes a turntable, a housing fixed to the upper surface of the turntable, and an aiming device fixing frame;The turntable is rotationally connected to the upper surface of the base and fixed with the drive end of the first motor;The second motor is fixed in the housing and the drive end extends out of the housing along the left and right directions;The aiming device fixing frame is fixed with the drive end of the second motor, and the aiming device is fixed to the aiming device fixing frame.

[0007] Compared with prior art, the above technical solution can facilitate the circumferential rotation of the rotary table, and the housing can encapsulate the first motor and the second motor without affecting the operation of the aiming device.

[0008] In a possible implementation, the second motor is provided with two driving ends, the two driving ends of the second motor respectively extend in left and right directions and are arranged on the shell; the sighting device fixing frame is in a U-shaped structure, is arranged above the shell, and is arranged with an opening side downward and a closed side leaving a gap between the closed side and the upper end of the shell; the two opening ends of the sighting device fixing frame are respectively fixed with the two driving ends of the second motor; the sighting device is fixed on the upper surface of the closed side of the sighting device fixing frame.

[0009] Compared with the prior art, the above technical scheme can facilitate the pitching adjustment of the sighting device and facilitate independent operation.

[0010] In a possible implementation, the two driving ends of the second motor are further fixed with a weapon fixing frame, and the weapon is fixed on the weapon fixing frame.

[0011] Compared with the prior art, the above technical scheme can be used for installing a laser weapon or a signal interference weapon and used for shooting down after aiming.

[0012] In a possible implementation, the height of the radar device is greater than the height of the sighting device.

[0013] Compared with the prior art, the above technical scheme can make the radar device have a wider transceiving surface and be less likely to be blocked.

[0014] In a possible implementation, a plurality of strip-shaped heat dissipation holes are uniformly arranged on the shell in a vertical direction, and the heat dissipation holes are arranged in extension in left and right directions.

[0015] Compared with the prior art, the above technical scheme can facilitate heat dissipation of the first motor and the second motor. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 is a perspective view of the utility model;

[0017] Figure 2 is a sectional view of the utility model in a side view direction;

[0018] MARKS:

[0019] 1-base, 2-rotary table, 3-first motor, 4-second motor, 5-radar device, 6-sighting device, 7-terminal control console, 8-weapon fixing frame, 21-rotating disc, 22-shell, 23-sighting device fixing frame, 221-heat dissipation hole. DETAILED DESCRIPTION

[0020] First, those skilled in the art should understand that the embodiments are only used to explain the technical principles of the embodiments of the present application, and are not intended to limit the protection scope of the embodiments of the present application. Those skilled in the art can make adjustments as needed to adapt to specific application occasions.

[0021] In the description of the embodiments of the present application, it should be noted that unless otherwise explicitly specified and limited, the terms "connected", "connected" should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or integrally connected; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium. For those skilled in the art, the specific meaning of the above terms in the embodiments of the present application can be understood according to the specific circumstances.

[0022] In the embodiments of the present application, unless otherwise explicitly specified and limited, the first feature is "on" or "under" the second feature, which can be that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediate medium. Moreover, the first feature can be above, above and above the second feature, or only indicates that the horizontal height of the first feature is higher than that of the second feature. The first feature can be below, below and below the second feature, or only indicates that the horizontal height of the first feature is less than that of the second feature.

[0023] The present application will be described in further detail below in conjunction with the drawings and specific embodiments.

[0024] The embodiments of the present application disclose a kind of unmanned plane detection and locking device, including base 1, rotating platform 2, first motor 3, second motor 4, radar device 5, sighting device 6 and terminal control console 7;Rotating platform 2 is rotationally connected on the upper surface of base 1;First motor 3 is fixed on base 1, and the driving end is upwards and is fixed with rotating platform 2 bottom, to drive rotating platform 2 to rotate along the circumference of the upper surface of base 1;Second motor 4 is fixed on rotating platform 2 and the driving end is set along left and right direction and is fixed with sighting device 6, to adjust the pitch angle of sighting device 6;Radar device 5 is fixed on rotating platform 2 for detecting unmanned plane;First motor 3, second motor 4, radar device 5 and sighting device 6 are all in communication connection with terminal control console 7;Second motor 4 driving end is fixed with weapon.

[0025] Specifically, as shown in the accompanying Figure 1 Figure, base 1 is disc structure, and is provided with weight-reducing hole to facilitate transportation and facilitate hand-carrying, as shown in the accompanying Figure 2As shown, the middle part of the base 1 in the up-down direction is provided with a cavity, the first motor 3 is fixed in the cavity, the turntable 2 can be rotatably connected with the upper surface of the base 1 through a bearing structure, and the driving end of the first motor 3 is fixed with the bearing structure; the first motor 3, the second motor 4, the radar device 5 and the aiming device 6 are electrically connected with the terminal control console 7; when the radar device 5 detects the unmanned aerial vehicle, the terminal control console 7 controls the first motor 3 and the second motor 4 to work, so that the turntable 2 rotates in the circumferential direction, and the pitch angle of the aiming device 6 is adjusted to lock, so that the position of the unmanned aerial vehicle can be effectively detected and locked; the terminal control console 7 in the application is a computer; the weapon can be a radio frequency jammer, a laser weapon or a microwave weapon, and a firearm can be installed when necessary.

[0026] As shown in the accompanying drawings, Figure 1 As shown in the accompanying drawings,

[0027] As shown in the accompanying drawings, Figure 2 As shown in the accompanying drawings,

[0028] In some embodiments, the two driving ends of the second motor 4 are also fixed with a weapon fixing frame 8, and a weapon is fixed on the weapon fixing frame 8. The weapon fixing frame 8 can be provided with a laser weapon or a jamming device, and the weapon on the weapon fixing frame 8 in the drawings of the application is replaced by a tubular part.

[0029] As shown in the accompanying drawings, Figure 1 As shown in the accompanying drawings,

[0030] As shown in the accompanying drawings, Figure 1As shown, in some embodiments, the shell 22 is uniformly provided with a plurality of strip-shaped heat dissipation holes 221 in the vertical direction, and the heat dissipation holes 221 are arranged in the left-right direction. In this way, the heat dissipation of the first motor 3 and the second motor 4 can be facilitated, and the long-term combat requirement can be met.

[0031] In the description of the embodiments of the present application, it should be noted that in the description of the present application, the terms indicating the direction or positional relationship of "inner", "outer" and the like are based on the direction or positional relationship shown in the drawings, which is only for the convenience of description, and does not indicate or imply that the device or member must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present application.

[0032] In the description of the present application, the description of the terms "one embodiment", "some embodiments", "in this embodiment", "specific examples" or "some examples" and the like means that the specific features, mechanisms, materials or characteristics described in conjunction with the embodiment or example are contained in at least one embodiment or example of the present application. In the present specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, mechanisms, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. Furthermore, the different embodiments or examples described in the specification and the features of the different embodiments or examples can be combined and combined by those skilled in the art without contradiction.

[0033] The above is only a specific embodiment of the present application, but the protection scope of the present application is not limited thereto, and any person skilled in the art can easily think of changes or replacements within the technical range disclosed in the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. A drone detection and locking device, characterized in that, The system includes a base (1), a turntable (2), a first motor (3), a second motor (4), a radar device (5), an aiming device (6), and a terminal control console (7). The turntable (2) is rotatably connected to the upper surface of the base (1). The first motor (3) is fixed to the base (1), with its drive end facing upward and fixed to the bottom of the turntable (2) to drive the turntable (2) to rotate circumferentially along the upper surface of the base (1). The second motor (4) is fixed to the turntable (2), with its drive end positioned in the left-right direction and fixed to the aiming device (6) to adjust the pitch angle of the aiming device (6). The radar device (5) is fixed to the turntable (2) for detecting the UAV. The first motor (3), the second motor (4), the radar device (5), and the aiming device (6) are all communicatively connected to the terminal control console (7). A weapon is fixed to the drive end of the second motor (4).

2. The UAV detection and locking device according to claim 1, characterized in that, The turntable (2) includes a turntable (21), a housing (22) fixed on the upper surface of the turntable (21), and a aiming device mounting bracket (23); the turntable (21) is rotatably connected to the upper surface of the base (1) and fixed to the drive end of the first motor (3); the second motor (4) is fixed inside the housing (22) and its drive end extends out of the housing (22) in the left and right direction; the aiming device mounting bracket (23) is fixed to the drive end of the second motor (4), and the aiming device (6) is fixed on the aiming device mounting bracket (23).

3. The UAV detection and locking device according to claim 2, characterized in that, The second motor (4) is provided with two drive ends, which extend out of the housing (22) in the left and right directions respectively; the aiming device mounting bracket (23) has a U-shaped structure and is located above the housing (22), with the open side facing down and a gap left between the closed side and the upper end of the housing (22); the two open ends of the aiming device mounting bracket (23) are fixed to the two drive ends of the second motor (4) respectively; the aiming device (6) is fixed to the upper surface of the closed side of the aiming device mounting bracket (23).

4. The UAV detection and locking device according to claim 1, 2 or 3, characterized in that, The two drive ends of the second motor (4) are also fixed with weapon mounting brackets (8), and the weapon is fixed on the weapon mounting brackets (8).

5. The UAV detection and locking device according to claim 1, 2 or 3, characterized in that, The height of the radar device (5) is greater than the height of the aiming device (6).

6. The UAV detection and locking device according to claim 2 or 3, characterized in that, The housing (22) is provided with a number of strip-shaped heat dissipation holes (221) evenly arranged vertically, and the heat dissipation holes (221) are all arranged to extend in the left and right direction.

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