Anti-unmanned aerial vehicle air defense weapon system
The modularly designed anti-drone air defense weapon system, which utilizes pneumatic weapons and monitoring equipment in conjunction with a robotic arm and rotating base platform, overcomes the limitations of existing drone air defense systems, achieving efficient strikes and countermeasures against drones, and features economic reliability and sustained firepower.
Patent Information
- Application Number
- CN202423022318.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-09
- Publication Date
- 2025-11-11
- Estimated Expiration
- 2034-12-09
AI Technical Summary
Existing anti-drone air defense weapon systems have limitations, such as radio jamming being ineffective against some drones, laser strikes being costly, net capture depending on weather, and close-in weapon systems and missile interception having limited effectiveness against multiple targets, making it difficult to continuously and effectively counter drone threats.
Design a modular anti-drone air defense weapon system, including a pneumatic weapon, monitoring equipment, a robotic arm assembly, a rotating base platform, and a power supply device. The system enables rapid assembly and disassembly through modular design and standardized interfaces. The monitoring equipment detects and identifies drone targets, the pneumatic weapon fires pneumatic bullets to engage them, and the robotic arm and rotating base platform are used to adjust the firing angle and direction.
It achieves economical and reliable firepower output, can continuously and efficiently respond to the needs of different air defense scenarios, effectively strike and counter drones, and is characterized by easy mobility and rapid assembly.
Smart Images

Figure CN223538205U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the field of military equipment technology, and specifically relates to an air defense weapon system for detecting, identifying and engaging unmanned aerial vehicles (UAVs). Background Technology
[0002] With the rapid development and widespread adoption of small unmanned aerial vehicle (UAV) technology, its applications in both civilian and military fields are becoming increasingly extensive, posing a serious challenge to public safety. Therefore, the research and development and application of anti-small UAV air defense weapon systems are of great practical significance. To address the security threats posed by small UAVs, it is necessary to develop a continuous, efficient, and modular anti-UAV air defense weapon system.
[0003] Existing anti-drone air defense weapon systems employ various technologies to detect, identify, jam, and destroy illegally intruding drones, thereby eliminating the drone threat and protecting personnel and property. These technologies encompass radio jamming, laser strikes, net capture, close-in weapon systems (CIWS), missile interception, and acoustic dispersal, among others. However, these methods have limitations. For instance, radio jamming weapons are ineffective against some hardened or autonomous drones; laser strike weapons are costly and pose safety hazards in urban areas; net capture weapons are dependent on weather conditions and have insufficient firepower; and CIWS and missile interception weapons have limited effectiveness against numerous high-speed moving targets.
[0004] Therefore, how to overcome the above-mentioned technical defects is a problem that urgently needs to be solved by those skilled in the art. Utility Model Content
[0005] The purpose of this invention is to provide an anti-drone air defense weapon system that is economical, reliable, and has strong sustained firepower, effectively addressing the needs of different air defense scenarios and achieving effective strikes and countermeasures against drones.
[0006] To solve the above-mentioned technical problems, this utility model provides an anti-drone air defense weapon system, comprising:
[0007] Pneumatic weapons are used to fire pneumatic bullets and strike drone targets.
[0008] Monitoring equipment is used to detect, identify, and track drone targets;
[0009] The robotic arm assembly includes both the pneumatic weapon and the monitoring device, which are mounted on the robotic arm assembly to drive the pneumatic weapon and the monitoring device to rotate.
[0010] A rotating base platform, wherein the robotic arm assembly is mounted on the upper surface of the rotating base platform, and is used to drive the robotic arm assembly to rotate 360° in the horizontal plane;
[0011] The power supply device and the command console are provided. The power supply device is used to supply power to the pneumatic weapon, the monitoring equipment, the robotic arm assembly and the rotating base platform, and to supply air to the pneumatic weapon. The command console is connected to the pneumatic weapon, the monitoring equipment, the robotic arm assembly, the rotating base platform and the power supply device by signal or electrical connection.
[0012] When the monitoring equipment detects and identifies a drone target, the command console can control the robotic arm assembly and the rotating base platform to rotate to the target position, and control the power supply device and the pneumatic weapon to cooperate in order to strike the drone target.
[0013] Optionally, in the above-mentioned anti-drone air defense weapon system, the pneumatic weapon, the monitoring equipment, the robotic arm assembly, the rotating base platform, the power supply device, and the command console are all modularly designed;
[0014] The pneumatic weapon, the monitoring equipment, the robotic arm assembly, the rotating base platform, and the power supply device are connected via a standardized interface.
[0015] Optionally, in the above-mentioned anti-drone air defense weapon system, the pneumatic weapon includes a pneumatic launching device and a pneumatic bullet, wherein the pneumatic launching device is used to launch the pneumatic bullet.
[0016] Optionally, in the above-mentioned anti-drone air defense weapon system, the pneumatic weapon further includes an air compressor and a high-pressure gas cylinder, wherein the air compressor and the high-pressure gas cylinder are used to provide a high-pressure gas source for the pneumatic launching device;
[0017] And / or, the pneumatic launching device uses the explosion of combustible gas or combustible liquid to generate power.
[0018] Optionally, in the aforementioned anti-drone air defense weapon system, the high-pressure gas cylinder is a high-strength composite material container.
[0019] Optionally, in the aforementioned anti-drone air defense weapon system, the air compressor and the high-pressure gas cylinder are controlled to open and close via electromagnetic valves.
[0020] Optionally, in the aforementioned anti-drone air defense weapon system, the monitoring equipment includes integrated radar and photoelectric sensors.
[0021] Optionally, in the aforementioned anti-drone air defense weapon system, the rotating base platform includes a housing, a rotary motor, and a main shaft. The rotary motor is connected to one end of the main shaft via a coupling, and the other end of the main shaft passes through the housing and is connected to the bottom of the robotic arm assembly.
[0022] Optionally, in the aforementioned anti-drone air defense weapon system, the outer shell is made of a lightweight alloy material.
[0023] Optionally, in the aforementioned anti-drone air defense weapon system, the power supply device includes a battery management unit, a high-energy-density battery, and a generator. The battery management unit is used to allocate and plan the power supply of the high-energy-density battery and the generator.
[0024] This utility model provides an anti-drone air defense weapon system, the advantages of which are:
[0025] The system utilizes monitoring equipment to detect, identify, and track drone targets. Pneumatic weapons fire pneumatic bullets to engage the drones. A robotic arm assembly and a rotating base platform work together to adjust the firing angle and direction of the pneumatic weapons. A power supply unit provides power and air to the pneumatic weapons and other subsystems. When the monitoring equipment detects and identifies a drone target, the command console receives instructions from higher command to rotate the robotic arm assembly and rotating base platform to the target position, and coordinates the power supply unit and pneumatic weapons to engage the drone. Because the pneumatic weapons and their compatible subsystems are compact, easy to move and quickly assemble, economical, reliable, and possess strong sustained firepower, they can effectively address the needs of different air defense scenarios, achieving effective strikes and countermeasures against drones. Attached Figure Description
[0026] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on the provided drawings without creative effort.
[0027] Figure 1 A schematic diagram of the structure of an anti-drone air defense weapon system provided in this embodiment of the present invention;
[0028] Figure 2 A schematic diagram of the structure of the command and control console provided in an embodiment of this utility model.
[0029] In the image above:
[0030] 100-Pneumatic weapon;
[0031] 200 - Monitoring equipment;
[0032] 300-robotic arm assembly;
[0033] 400-Rotating base platform;
[0034] 500-Power supply unit;
[0035] 600 - Command and Control Console. Detailed Implementation
[0036] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.
[0037] The core of this invention is to provide an anti-drone air defense weapon system that is economical, reliable, and has strong sustained firepower output, effectively addressing the needs of different air defense scenarios and achieving effective strikes and countermeasures against drones.
[0038] To enable those skilled in the art to better understand the technical solutions provided by this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments.
[0039] For details, please refer to Figures 1-2 The present invention provides an anti-drone air defense weapon system, which includes multiple subsystems, namely: a pneumatic weapon 100, a monitoring device 200, a robotic arm assembly 300, a rotating base platform 400, a power supply device 500, and a command and control console 600.
[0040] The pneumatic weapon 100 is used to output pneumatic bullets for the system to strike targets such as drones.
[0041] Monitoring equipment 200 is used to detect and identify UAV targets and track targets.
[0042] The robotic arm assembly 300 is used to drive the pneumatic weapon 100 and the monitoring device 200 to rotate, so as to adjust the firing angle of the pneumatic weapon 100 in real time according to the target positioning of the monitoring device 200, thereby achieving all-around strike. Specifically, both the pneumatic weapon 100 and the monitoring device 200 are mounted on the robotic arm assembly 300. The robotic arm assembly 300 includes, but is not limited to, […]. Figure 1 The multi-joint robotic arm mentioned can also be a robotic arm with 6 axes or more. Any robotic arm component with a structure capable of precisely controlling the firing angle of a pneumatic weapon at 100 degrees is within the protection scope of this solution. Generally, robotic arms with 6 axes or more can also be called robots. Robots can include military robots such as reconnaissance robots, industrial robots such as robotic arms, humanoid robots, and biomimetic robots such as robot dogs.
[0043] The rotating base platform 400 is used to drive the robotic arm assembly 300 to rotate 360° in the horizontal plane. After assembly, each subsystem is mounted on the rotating base platform 400 via the robotic arm assembly 300, making it a whole and easy to transport.
[0044] The power supply unit 500 is used to supply power to the pneumatic weapon 100, the monitoring equipment 200, the robotic arm assembly 300 and the rotating base platform 400, and to supply air to the pneumatic weapon 100.
[0045] The command console 600 receives instructions from higher command for target identification, tracking, and strike control. Specifically, the control modules within the command console 600 are connected via signal or electrical connections to the pneumatic weapon 100, monitoring equipment 200, robotic arm assembly 300, rotating base platform 400, and power supply unit 500. The command console 600 includes a computer, communication equipment, and data analysis software. The computer possesses real-time data collection and processing capabilities and can seamlessly interface with relevant subsystems. The communication equipment employs encrypted communication technology to ensure the security and reliability of command transmission, and is also a tactical-level device with anti-jamming capabilities, ensuring stable communication in complex electromagnetic environments. Operators can use the command console 600 to search, lock onto, track, and strike UAV targets. The data analysis software can process radar data in real time and generate optimal strike strategies.
[0046] When the monitoring equipment 200 detects and identifies the UAV target, the command console 600 can control the robotic arm assembly 300 and the rotating base platform 400 to rotate to the target position, and control the power supply device 500 and the pneumatic weapon 100 to cooperate in order to strike the UAV target.
[0047] It should be noted that the control method of the command console 600 is to transmit the feedback signal of component A to the command console 600, and then the command console 600 controls components B, C, D and other components to perform their respective actions. The above-mentioned control method of receiving instructions and using the computer's real-time data processing capability to quickly parse the instructions is a conventional technical means.
[0048] The anti-drone air defense weapon system provided in this solution utilizes monitoring equipment 200 to detect, identify, and track drone targets. A pneumatic weapon 100 fires pneumatic bullets to engage the drone targets. The firing angle and direction of the pneumatic weapon 100 are adjusted via a robotic arm assembly 300 and a rotating base platform 400. A power supply unit 500 provides power and air to the pneumatic weapon 100 and other subsystems. When the monitoring equipment 200 detects and identifies a drone target, the command console 600 receives instructions from higher command, controlling the robotic arm assembly 300 and the rotating base platform 400 to rotate to the target position. It also controls the power supply unit 500 and the pneumatic weapon 100 to coordinate the engagement of the drone target. Because the pneumatic weapon 100 and its compatible subsystems occupy a small footprint, they are easy to move and quickly assemble. They are economical, reliable, and have strong sustained firepower, effectively addressing the needs of different air defense scenarios and achieving effective strikes and countermeasures against drones.
[0049] In a specific embodiment, the anti-drone air defense weapon system is composed of several modular devices connected together. These modular devices include a pneumatic weapon 100, a monitoring device 200, a robotic arm assembly 300, a rotating base platform 400, a power supply device 500, and a command and control console 600. All of these subsystems are modularly designed, facilitating rapid replacement, upgrades, and maintenance, thus improving the system's flexibility and scalability. Standardized interfaces are provided on the pneumatic weapon 100, monitoring device 200, robotic arm assembly 300, rotating base platform 400, and power supply device 500. These components are connected via standardized interfaces, enabling rapid assembly and disassembly, reducing maintenance costs, supporting immediate use, and allowing for rapid replacement or upgrades according to the battlefield environment, effectively improving the system's compatibility and interchangeability.
[0050] Specifically, all components on the pneumatic weapon 100 are assembled using standard Picatinny rails. For example, a standard Picatinny rail is installed on the outside of the pneumatic weapon 100's housing, and various accessories such as sights, night vision devices, laser designators / aims, flashlights, and bayonet mounts can be mounted on the standard Picatinny rail.
[0051] In a specific embodiment, the pneumatic weapon 100 includes a pneumatic launching device and pneumatic bullets. The pneumatic bullets are made of high-density materials, and different types of pneumatic bullets can be used according to the target characteristics to improve the strike effect. The pneumatic launching device can fire pneumatic bullets and adopts adaptive adjustment technology, allowing each gun / cannon barrel to adjust the firing angle and automatically adjust the firing pressure according to the target distance. The pneumatic launching device has low cost and long firepower duration. The pneumatic bullets are small, have a high rate of fire, and do not eject casings, therefore, they are very effective against small moving targets such as drones.
[0052] In the first embodiment, the pneumatic weapon 100 also includes an air compressor and a high-pressure gas cylinder, which provide a high-pressure gas source and generate power for the pneumatic launching device. The pneumatic weapon 100 uses a gas cylinder, an electric motor, or an engine to generate compressed gas for power. In the second embodiment, the pneumatic weapon 100 uses the explosion of gas or other combustible gases or combustible liquids for power. In the third embodiment, the pneumatic weapon 100 can adopt a dual-mode combination of the first and second embodiments to provide firepower output power.
[0053] To ensure safety and stability under high-pressure conditions, the high-pressure gas cylinder is made of high-strength composite material. The air compressor and the high-pressure gas cylinder are controlled by a solenoid valve. When the command console 600 receives the target signal from the monitoring device 200, it opens the solenoid valve, and the high-pressure gas enters the pneumatic launching device through the high-pressure gas cylinder, propelling the pneumatic bullet to launch, achieving rapid response and precise strike.
[0054] In a specific embodiment, the monitoring device 200 includes an integrated radar and photoelectric sensor. The radar employs advanced electronic scanning technology, featuring long detection range, large scanning area, and high detection speed, enabling rapid and accurate target detection and tracking, and even accurate prediction of target trajectory. The photoelectric sensor utilizes Doppler effect and pulse compression technology, accurately identifying targets, determining their attributes and types, and is unaffected by electronic interference, effectively improving target recognition rate and anti-interference capability. This configuration fully utilizes the advantages of both sensors, compensating for their weaknesses, and improving monitoring efficiency and accuracy. Based on target information, the robotic arm assembly 300 and the rotating base platform 400 are controlled to adjust their orientation, track and aim at the target, and launch an attack.
[0055] The rotating base platform 400 includes a housing, a rotary motor, and a main shaft. The rotary motor is connected to one end of the main shaft via a coupling, and the other end of the main shaft passes through the housing and is connected to the bottom of the robotic arm assembly 300. The housing serves as the supporting component of the rotating base platform 400, and the rotary motor, as the rotational power source of the rotating base platform 400, drives the main shaft and the robotic arm assembly 300 to rotate together. The housing and the main shaft are connected by bearings to achieve rotational stability.
[0056] Rotary motors can be composed of servo motors and encoders to achieve precise angle control and positioning.
[0057] To achieve a lightweight design, the outer shell of the rotating base platform 400 is made of lightweight alloy material with a modular design, facilitating disassembly, transport, and rapid assembly. The power supply unit 500 is located at the bottom of the rotating base platform 400. The rotating base platform 400 or the power supply unit 500 can be mounted on robots, armored vehicles, warships, and airships for anti-drone air defense.
[0058] In a specific embodiment, the power supply unit 500 supplies power to the pneumatic weapon 100 and other subsystems, specifically including a battery management unit, batteries, and a generator. The batteries have charging and discharging protection functions and can be high-energy-density batteries. Connected to other subsystems, the batteries can meet the system's long-term operational needs. The generator serves as a backup power source to meet the power requirements of the entire system during prolonged, high-intensity combat operations. The power management unit allocates and plans the power supply to the high-energy-density batteries and the generator, achieving optimal energy utilization through intelligent power distribution technology. For example, when the generator charges the battery, the battery management unit can control parameters such as charging current and voltage to prevent overcharging, thereby protecting the battery and extending its lifespan. Energy recovery technology is employed to reduce the overall energy consumption of the system.
[0059] Of course, depending on the battlefield situation, this utility model can also support the coordinated operation of the entire anti-drone air defense weapon system with electronic warfare, cyber warfare and other means. Through data fusion technology, it can achieve information complementarity of different detection methods, form a comprehensive drone defense system, and improve the effectiveness of anti-drone operations.
[0060] In summary, this utility model discloses an anti-drone air defense weapon system integrating a pneumatic weapon 100, a radar system and photoelectric sensors, and a robotic arm assembly 300. It has functions such as command and control, radar detection, pneumatic weapon strike, and intelligent robot as a platform. It is characterized by modularity, lightweight, portability, long firepower duration, and low ammunition consumption cost. It can achieve the identification and continuous precision strike of drone targets and has broad application prospects and military value.
[0061] In the description of this application, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this application.
[0062] In the description of the embodiments of this application, unless otherwise stated, " / " means "or", for example, A / B can mean A or B; "and / or" in this document is merely a description of the relationship between related objects, indicating that three relationships can exist. For example, A and / or B can represent: A existing alone, A and B existing simultaneously, and B existing alone. Furthermore, in the description of the embodiments of this application, "multiple" refers to two or more.
[0063] In the description of this application, unless otherwise expressly defined, terms such as "setup," "installation," and "connection" should be interpreted broadly, and those skilled in the art can reasonably determine the specific meaning of the above terms in this application in conjunction with the specific content of the technical solution.
[0064] The various embodiments in this specification are described in a progressive manner, with each embodiment focusing on the differences from other embodiments. The same or similar parts between the various embodiments can be referred to each other.
[0065] This article uses specific examples to illustrate the principles and implementation methods of this utility model. The descriptions of the above embodiments are only for the purpose of helping to understand the method and core ideas of this utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made to this utility model without departing from the principles of this utility model, and these improvements and modifications also fall within the protection scope of the claims of this utility model.
Claims
1. An anti-drone air defense weapon system, characterized in that, include: Pneumatic weapon (100) for firing pneumatic bullets and striking drone targets; Monitoring equipment (200) is used to detect and identify unmanned aerial vehicle (UAV) targets and track them; The robotic arm assembly (300) is provided with the pneumatic weapon (100) and the monitoring device (200) both mounted on it, and is used to drive the pneumatic weapon (100) and the monitoring device (200) to rotate. A rotating base platform (400) is provided, and the robotic arm assembly (300) is mounted on the upper surface of the rotating base platform (400) to drive the robotic arm assembly (300) to rotate 360° in the horizontal plane. A power supply device (500) and a command console (600) are provided. The power supply device (500) is used to supply power to the pneumatic weapon (100), the monitoring device (200), the robotic arm assembly (300), and the rotating base platform (400), and to supply air to the pneumatic weapon (100). The command console (600) is connected to the pneumatic weapon (100), the monitoring device (200), the robotic arm assembly (300), the rotating base platform (400), and the power supply device (500) by signal or electrical connection. When the monitoring device (200) detects and identifies the UAV target, the command console (600) can control the robotic arm assembly (300) and the rotating base platform (400) to rotate to the target position, and control the power supply device (500) and the pneumatic weapon (100) to cooperate in order to strike the UAV target.
2. The anti-drone air defense weapon system according to claim 1, characterized in that, The pneumatic weapon (100), the monitoring equipment (200), the robotic arm assembly (300), the rotating base platform (400), the power supply device (500), and the command console (600) are all modular designs; The pneumatic weapon (100), the monitoring device (200), the robotic arm assembly (300), the rotating base platform (400), and the power supply device (500) are connected via a standardized interface.
3. The anti-drone air defense weapon system according to claim 1, characterized in that, The pneumatic weapon (100) includes a pneumatic launching device and a pneumatic bullet, the pneumatic launching device being used to launch the pneumatic bullet.
4. The anti-drone air defense weapon system according to claim 3, characterized in that, The pneumatic weapon (100) also includes an air compressor and a high-pressure gas cylinder, which are used to provide a high-pressure gas source for the pneumatic launching device; And / or, the pneumatic launching device uses the explosion of combustible gas or combustible liquid to generate power.
5. The anti-drone air defense weapon system according to claim 4, characterized in that, The high-pressure gas cylinder is a high-strength composite material container.
6. The anti-drone air defense weapon system according to claim 4, characterized in that, The air compressor and the high-pressure gas cylinder are controlled to open and close via a solenoid valve.
7. The anti-drone air defense weapon system according to claim 1, characterized in that, The monitoring device (200) includes integrated radar and photoelectric sensors.
8. The anti-drone air defense weapon system according to claim 1, characterized in that, The rotating base platform (400) includes a housing, a rotary motor and a main shaft. The rotary motor is connected to one end of the main shaft via a coupling, and the other end of the main shaft passes through the housing and is connected to the bottom of the robotic arm assembly (300).
9. The anti-drone air defense weapon system according to claim 8, characterized in that, The outer shell is made of lightweight alloy material.
10. The anti-drone air defense weapon system according to claim 1, characterized in that, The power supply device (500) includes a battery management unit, a high-energy-density battery, and a generator. The battery management unit is used to allocate and plan the power supply of the high-energy-density battery and the generator.