Unmanned aerial vehicle countering vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicle countering, in particular to an unmanned aerial vehicle countering vehicle which comprises a vehicle body, a command and control square cabin and an equipment square cabin are arranged on a vehicle frame platform of the vehicle body, the equipment square cabin is divided into an antenna sub-cabin and an equipment sub-cabin, the equipment sub-cabin is a special-shaped cube with the vertical side face in an L shape, and the antenna sub-cabin and the equipment sub-cabin are arranged on the vehicle frame platform. The antenna sub-cabin and the equipment sub-cabin are combined into a cuboid, the antenna sub-cabin is located at the top of the tail of the equipment sub-cabin, an antenna is arranged in the antenna sub-cabin, a shell of the antenna sub-cabin is provided with a left cabin door and a right cabin door which can be completely opened and closed, and the left cabin door is horizontally and rotatably connected to the left side face of the equipment sub-cabin. The right cabin door is horizontally and rotationally connected to the right side face of the equipment sub-cabin. According to the utility model, the antenna can be fully protected, and the antenna can be fully unfolded when needed, so that the antenna can play a role.

Description

Technical Field

[0001] This utility model relates to the field of drone countermeasure technology, specifically to a drone countermeasure vehicle. Background Technology

[0002] With the development of drone technology, various security issues have frequently arisen. As these security issues become more prominent, counter-drone technology urgently needs development. Current drone countermeasures equipment includes antennas, jamming signal generators, generators, batteries, power sources, displays, and controllers. The jamming signal generator consists of multiple jamming signal transmission modules with different frequency bands, and a flat panel antenna is connected to these jamming signal transmission modules via a signal transmission feeder. Antennas include omnidirectional antennas, directional antennas, phased array antennas, and dedicated antennas, which can concentrate the jamming signal transmission to a specific area or direction. It is clear that antennas play a crucial role in countering drones, but they are also very vulnerable. Conventional drone countermeasures devices expose their antennas, making them extremely susceptible to damage. Furthermore, their high value leads to significant losses. Utility Model Content

[0003] The purpose of this invention is to provide a drone countermeasure vehicle that can fully protect the antenna and can be fully deployed to enable the antenna to function when needed.

[0004] To achieve the above objectives, a drone countermeasure vehicle is provided, comprising a vehicle body, a command and control compartment and an equipment compartment on the vehicle body's frame platform, the equipment compartment being divided into an antenna sub-compartment and an equipment sub-compartment, the equipment sub-compartment being an irregularly shaped cube with an L-shaped vertical side, the antenna sub-compartment and the equipment sub-compartment being combined to form a cuboid, the antenna sub-compartment being located at the top of the rear of the equipment sub-compartment, the antenna sub-compartment containing an antenna, the outer shell of the antenna sub-compartment being configured with a fully openable left door and a right door, the left door being horizontally rotatably connected to the left side of the equipment sub-compartment, and the right door being horizontally rotatably connected to the right side of the equipment sub-compartment.

[0005] Furthermore, the left and right hatches are symmetrically arranged.

[0006] Furthermore, the equipment sub-compartment is equipped with several cabinet doors on its three sides.

[0007] Furthermore, the command and control module is equipped with alarm lights.

[0008] Furthermore, the command and control module is equipped with limiting blocks to prevent the left and right doors from vibrating vertically when closed.

[0009] Furthermore, the left and right hatches are magnetically attached to the left and right sides of the equipment sub-compartment, respectively. The left and right sides of the equipment sub-compartment are equipped with first Hall sensors, which are used to detect the magnetic signals after the left and right hatches are magnetically attached to the left and right hatches, respectively. The first Hall sensors are electrically connected to the controller, which is installed in the command and control container. The command and control container is also equipped with a speaker, which is electrically connected to the controller.

[0010] Furthermore, the left and right hatches close magnetically.

[0011] Furthermore, a second Hall sensor is provided on the upper surface of the equipment sub-compartment and on the contact surface with the left and right hatches when closed. The second Hall sensor is used to detect the magnetic signal when the left and right hatches are closed, and the second Hall sensor is electrically connected to the controller.

[0012] Principles and advantages:

[0013] 1. When drone countermeasures are needed, simply flip the left and right hatches horizontally to expose the antenna. The left and right hatches will not interfere with antenna operation. During long-distance transport, the left and right hatches should be flipped horizontally to close and protect the antenna from damage.

[0014] 2. Several cabinet doors in the equipment sub-compartment facilitate the installation and use of equipment such as antennas and interference signal generators.

[0015] 3. The magnetic attraction design facilitates the securing of the left and right hatches to the left and right sides of the equipment sub-compartment during antenna operation, preventing interference with antenna use. Furthermore, the first Hall sensor detects the securing status of the left and right hatches via magnetic signals. Similarly, when the antenna is not in operation, the left and right hatches can be magnetically attached together for reset, and the second Hall sensor detects whether the left and right hatches are fully closed via magnetic signals. Attached Figure Description

[0016] Figure 1 This is a side view of a drone countermeasure vehicle according to an embodiment of the present invention;

[0017] Figure 2 This is an axonometric drawing of a drone countermeasure vehicle according to an embodiment of the present invention;

[0018] Figure 3 This is a schematic diagram of the left and right hatches of a drone countermeasure vehicle after being unfolded, according to an embodiment of the present invention.

[0019] Figure 4This is a schematic diagram of the antenna of a drone countermeasure vehicle after being unfolded, according to an embodiment of the present invention. Detailed Implementation

[0020] The following detailed description illustrates the specific implementation method:

[0021] The reference numerals in the accompanying drawings include: vehicle body 1, command and control compartment 2, equipment sub-compartment 3, antenna sub-compartment 4, warning light 5, cabinet door 6, left compartment door 7, left compartment door 8, limit block 9, and antenna 10.

[0022] Example 1

[0023] A drone countermeasure vehicle, basically as follows Figures 1-4 As shown, the vehicle includes a main body 1. A command and control cabin 2 and an equipment cabin are mounted on the chassis platform of the main body 1. An alarm light 5 is mounted on the top of the command and control cabin 2. The equipment cabin is divided into an antenna sub-cabin 4 and an equipment sub-cabin 3. The equipment sub-cabin 3 is an irregularly shaped cube with an L-shaped vertical side. The antenna sub-cabin 4 and equipment sub-cabin 3 are combined to form a cuboid. The antenna sub-cabin 4 is located at the top of the rear of the equipment sub-cabin 3. An antenna 10 is installed inside the antenna sub-cabin 4. The outer shell of the antenna sub-cabin 4 is configured with a fully openable left door 7 and a right door. The left door 7 is horizontally rotatably connected to the left side of the equipment sub-cabin 3, and the right door is horizontally rotatably connected to the right side of the equipment sub-cabin 3. The left door 7 and the right door are symmetrically arranged. The left door 7 includes a top panel, a left side panel, and a rear side panel, which are perpendicular to each other. The left side panel is hinged to the left side of the equipment sub-cabin 3. The right hatch includes a top panel, a right side panel, and a rear side panel, which are perpendicular to each other. The right side panel is hinged to the right side of the equipment sub-compartment 3. The equipment sub-compartment 3 has several cabinet doors 6 on its three sides. In this embodiment, the right side of the equipment compartment has two sets of cabinet doors 6, one large and one small; similarly, the left side of the equipment compartment has two sets of cabinet doors 6, one large and one small; and the rear side of the equipment compartment has one set of cabinet doors 6. This transparent structure facilitates the installation and use of equipment such as the antenna 10 and the interference signal generator.

[0024] When the left hatch 7 is opened, its left side panel can be attached to the left side of the equipment container. When the right hatch is opened, its right side panel can be attached to the right side of the equipment container.

[0025] When drone countermeasures are needed, the left and right hatches 7 and 8 can be opened horizontally to expose the antenna 10. The antenna 10 can then be flipped vertically from a horizontal to a vertical position to deploy for drone countermeasures. During long-distance transport, the antenna 10 needs to be flipped vertically from a vertical to a horizontal position, and then the left and right hatches 7 and 8 can be closed horizontally to protect the antenna 10 and prevent damage. The command and control container 2 is equipped with limiting blocks 9 to restrict the vertical vibration of the left and right hatches 7 and 8 when they are closed. This is to prevent vibrations from the left and right hatches 7 and 8 during vehicle movement that could cause the doors to open and damage the antenna 10.

[0026] Example 2

[0027] The left and right hatches 7 and 8 are magnetically attached to the left and right sides of the equipment sub-compartment 3, respectively. The left and right sides of the equipment sub-compartment 3 are equipped with first Hall sensors, which detect the magnetic signals generated after the left and right hatches 7 and 8 are magnetically attached to them. The first Hall sensors are electrically connected to a controller, which is located in the command and control container 2. The command and control container 2 also has a speaker electrically connected to the controller. In this embodiment, magnetic metal and the first Hall sensors are independently installed on the left and right sides of the equipment sub-compartment 3, while magnets, such as neodymium magnets, are installed on the left and right hatches 7 and 8, respectively. This simplifies the wiring layout and simplifies the function implementation. The magnetic attachment method facilitates the fixation of the left and right hatches 7 and 8 to the left and right sides of the equipment sub-compartment 3 during antenna 10 operation, preventing interference with the antenna 10 (which is erected during use; if the left and right hatches 7 and 8 are not fixed, they may damage the antenna 10). On the other hand, the first Hall sensor can detect whether the left hatch 7 and the right hatch 8 have been secured by magnetic signals.

[0028] The left and right hatches 7 and 8 are also closed magnetically. The magnets used for this magnetic closure are positioned at three points: the horizontal end face of the top panel, the vertical end face of the rear panel, and the lower end faces of the left, right, and rear panels that contact the equipment sub-compartment 3. A second Hall sensor is located on the upper end face of the equipment sub-compartment 3, which is in contact with the left and right hatches 7 and 8 when closed. This second Hall sensor detects the magnetic signal when the left and right hatches 7 and 8 are closed, and is electrically connected to the controller. In this embodiment, magnets, such as neodymium magnets, are respectively placed on the lower end faces of the left, rear, and right panels that contact the equipment sub-compartment 3. The placement of the second Hall sensor and magnetic metal on the upper surface of the equipment sub-compartment 3 simplifies the wiring layout and simplifies the functional implementation. This allows the left and right hatches 7 and 8 to be easily attracted and fixed together when the antenna 10 stops working, completing the reset. Furthermore, the first Hall sensor can detect whether the left and right hatches 7 and 8 are fully reset and closed via magnetic signals.

[0029] The above descriptions are merely embodiments of this utility model. Commonly known structures and characteristics are not described in detail here. Those skilled in the art are aware of all common technical knowledge in the field prior to the application date or priority date, are capable of accessing all existing technologies in that field, and possess the ability to apply conventional experimental methods prior to that date. Therefore, those skilled in the art can, based on the guidance provided in this application, improve and implement this solution in conjunction with their own capabilities. Typical known structures or methods should not be obstacles for those skilled in the art to implement this application. It should be noted that those skilled in the art can make several modifications and improvements without departing from the structure of this utility model. These modifications and improvements should also be considered within the scope of protection of this utility model, and will not affect the effectiveness of the implementation of this utility model or the practicality of the patent. The scope of protection claimed in this application should be determined by the content of its claims, and the specific embodiments described in the specification can be used to interpret the content of the claims.

Claims

1. An unmanned aerial vehicle countermeasure vehicle, characterized by: The vehicle body includes a frame platform, a command and control shelter and a device shelter are arranged on the frame platform, the device shelter is divided into an antenna sub-shelter and a device sub-shelter, the device sub-shelter is a special-shaped cuboid with an L-shaped vertical side, the antenna sub-shelter and the device sub-shelter are combined into a cuboid, the antenna sub-shelter is arranged on the top of the tail of the device sub-shelter, an antenna is arranged in the antenna sub-shelter, the outer shell of the antenna sub-shelter is provided with left and right cabin doors which can be completely opened and closed, the left cabin door is horizontally rotationally connected to the left side of the device sub-shelter, and the right cabin door is horizontally rotationally connected to the right side of the device sub-shelter.

2. The drone countermeasure vehicle of claim 1, wherein: The left and right cabin doors are symmetrically arranged.

3. The drone countermeasure vehicle of claim 1, wherein: A plurality of cabinet doors are arranged on three sides of the device sub-shelter.

4. The drone counter vehicle of claim 1, wherein: The command and control shelter is provided with an alarm lamp.

5. The drone countermeasure vehicle of claim 1, wherein: The command and control shelter is provided with a limiting block for limiting the left and right cabin doors from vibrating up and down when being closed.

6. The drone countermeasure vehicle of claim 1, wherein: The left and right cabin doors are respectively fixed to the left and right sides of the device sub-shelter by magnetic attraction, the left and right sides of the device sub-shelter are provided with first Hall sensors, the first Hall sensors are used for detecting the magnetic signals after the left and right cabin doors are respectively magnetically attracted to the left and right cabin doors, the first Hall sensors are electrically connected to a controller, the controller is arranged in the command and control shelter, the command and control shelter is further provided with a loudspeaker, and the loudspeaker is electrically connected to the controller.

7. The drone countermeasure vehicle of claim 6, wherein: The left and right cabin doors are closed by magnetic attraction.

8. The drone countermeasure vehicle of claim 7, wherein: A second Hall sensor is arranged on the upper end surface of the device sub-shelter and the contact surface of the left and right cabin doors when being closed, the second Hall sensor is used for detecting the magnetic signals when the left and right cabin doors are closed, and the second Hall sensor is electrically connected to the controller.

Images