Networking rocket anti-unmanned aerial vehicle system

Abstract

The utility model discloses a networking rocket anti-unmanned aerial vehicle system which comprises a launching device and a rocket loading bin, a rocket holder is fixedly connected to the upper portion of the interior of the rocket loading bin, a net bag bin is arranged below the rocket loading bin and communicates with the rocket loading bin, and polygonal regular catching net bags are arranged in the net bag bin; a plurality of rocket bins which are evenly distributed at equal intervals are formed in the rocket holder, rockets are arranged in the rocket bins, traction hanging rings are arranged at the tails of the rockets and connected with rocket traction ropes, and the number of the rocket bins is consistent with the number of the edges of the polygonal regular catching net package. The multiple traction hanging rings are connected with the corners of the polygonal regular catching net bag through the rocket traction ropes respectively, the multiple rocket bins are arranged in a scattering mode, the number of the rocket bins is increased, meanwhile, the scattering angles of the rocket bins are increased, the launching device ignites and launches the multiple rockets, and after the rockets are launched, the rocket traction ropes drag the catching net bag to be opened in the air. Large-area interception of the airspace is achieved, and the purpose of resisting the unmanned aerial vehicle is achieved.

Description

Technical Field

[0001] The present application relates to the technical field of anti-UAV devices, and specifically to a networked rocket anti-UAV system. Background Art

[0002] With the development of related hardware and software, drone technology is becoming increasingly mature. Various types of drones are widely used in agriculture and forestry plant protection, aerial photography and mapping, and other aspects. Unexpected incidents such as "illegal" drones interfering with aviation order and drones peeping into privacy are frequent. Drones have also played a huge role in the military field. A large number of military drones have assumed detection and combat functions, which have a great impact on war. It is imperative to develop anti-drone systems.

[0003] Existing anti-drone technologies are mainly based on electromagnetic pulses, radio frequency interference and contact live-fire strikes.

[0004] Electromagnetic pulse and radio frequency interference technology equipment has high production costs and a small coverage frequency band, which is not conducive to popularization. At the same time, the interference equipment is heavy and not conducive to single-soldier combat. At the same time, new fiber-optic anti-interference combat drones have also been put into use, and the role of electromagnetic interference anti-drone systems is weakening.

[0005] Among contact anti-UAV technologies, live-fire anti-UAV technology has a low hit rate and weak counter-UAV capability.

[0006] The existing anti-UAV capture net technology is often dragged by drones, with a small interception area and a low success rate. There is still a gap in net capture technology, and a need for a net capture anti-UAV system that can intercept target drones over a large area, is small in size, light in weight, and easy to carry.

[0007] Therefore, in order to solve the above problems, a networked rocket anti-UAV system is needed. Utility Model Content

[0008] The purpose of this application is to provide a networked rocket anti-UAV system to solve the above-mentioned technical problems.

[0009] To achieve the above-mentioned objectives, the present application provides the following technical solutions: a networked rocket anti-UAV system, comprising: a launch device and a rocket loading compartment, a rocket holder is fixedly connected to the upper part of the rocket loading compartment, a net bag compartment is provided below the rocket loading compartment, the net bag compartment and the rocket loading compartment are connected, a polygonal regular capture net bag is provided in the net bag compartment, a plurality of rocket compartments evenly arranged at equal intervals are provided on the rocket holder, a rocket is built in the rocket compartment, a traction ring is provided at the tail of the rocket, the traction ring is connected to the rocket traction rope, the number of rocket compartments is consistent with the number of sides of the polygonal regular capture net bag, a plurality of traction rings are respectively connected to the corners of the polygonal regular capture net bag through the rocket traction rope, a plurality of rocket compartments are arranged in a scattered manner, and the scattering angle of the rocket compartment increases as the number of rocket compartments increases.

[0010] When using this networked rocket anti-UAV system, the launch device contacts the rocket, and the launch device ignites and launches several rockets. After the rocket is launched, the traction ring at the tail works to drag the rocket traction rope. The rocket traction rope leaves the rocket loading compartment from the connection point between the net bag compartment and the rocket loading compartment, towing and dragging the capture net bag. The capture net bag opens in the air under the traction force of the rocket, thereby realizing large-area interception of the airspace and achieving the purpose of anti-UAV.

[0011] Preferably, the central axis of the launch device and the rocket loading compartment are in the same plane.

[0012] Preferably, the polygonal regular capture net is an equilateral triangle, and three rocket compartments are provided on the rocket holder, and the installation scattering angle of the three rockets is 2-4°.

[0013] Preferably, the polygonal regular capture net is a square, and four rocket compartments are provided on the rocket holder, and the installation scattering angle of the four rockets is 4-6°.

[0014] Preferably, the polygonal regular capture net bag is a regular pentagon, five rocket compartments are opened on the rocket holder, and the installation scattering angle of the five rockets is 6-8°.

[0015] Preferably, the scattering angle of the rocket bay is related to the rocket launch distance and the net deployment area. The longer the distance, the smaller the angle, and the smaller the net area, the smaller the angle.

[0016] Compared with the prior art, the beneficial effects of this application are:

[0017] 1. This networked rocket anti-UAV system can complete the task of intercepting and attacking UAVs and their dropped objects in the air;

[0018] 2. The polygonal rule capture net package of this network rocket anti-UAV system has a large interception area, which can intercept and attack UAV groups with a high success rate;

[0019] 3. This networked rocket anti-UAV system has a compact structure and light weight, making it easy for a single soldier to carry and fight;

[0020] 4. The networked rocket anti-UAV system has a simple structure, low production cost, can be mass-produced and processed, and can be popularized;

[0021] 5. This networked rocket anti-UAV system has high sensitivity and can be quickly loaded and launched when a UAV is detected to protect combat personnel. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 This is a schematic diagram of the three-dimensional structure of the networked rocket anti-UAV system of Example 1 of the present application;

[0023] Figure 2 This is a schematic diagram of the deployment of a polygonal rule capture net package of the networked rocket anti-UAV system after rocket launch in Example 1 of the present application;

[0024] Figure 3 This is a front view of the rocket holder of the networked rocket anti-UAV system of Example 1 of the present application;

[0025] Figure 4 This is a schematic diagram of the structure of the rocket board of the networked rocket anti-UAV system of Example 1 of the present application;

[0026] Figure 5 This is a schematic diagram of the polygonal rule capture net package of the networked rocket anti-UAV system of the second embodiment of the present application after rocket launch and before the expansion;

[0027] Figure 6 Schematic diagram of the expanded polygonal rule capture net package of the networked rocket anti-UAV system after rocket launch in the second embodiment of the present application

[0028] Figure 7 A schematic diagram of a networked rocket anti-UAV system after rocket launch and before the polygonal rule capture net package is expanded in Example 3 of the present application;

[0029] Figure 8 This is a schematic diagram of the unfolded polygonal rule capture network package of the networked rocket anti-UAV system of the application embodiment 3 after rocket launch.

[0030] Figure numerals: 1. rocket; 2. traction ring; 3. rocket traction rope; 4. polygonal regular capture net bag; 5. launching device; 6. rocket loading compartment; 7. rocket retaining frame. DETAILED DESCRIPTION

[0031] The following will be combined with the drawings in the embodiments of the present application to clearly and completely describe the technical solutions in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0032] Embodiment 1

[0033] like Figures 1 to 4As shown, a networked rocket anti-UAV system includes: a launch device 5 and a rocket loading chamber 6, the central axes of the launch device 5 and the rocket loading chamber 6 are in the same plane, a rocket holder 7 is fixedly connected to the upper part of the rocket loading chamber 6, a net bag chamber is provided below the rocket loading chamber 6, the net bag chamber is connected to the rocket loading chamber 6, a polygonal regular capture net bag 4 is provided in the net bag chamber, in this embodiment, the polygonal regular capture net bag 4 is an equilateral triangle, three rocket chambers with equal spacing and uniform arrangement are provided on the rocket holder 7, a rocket 1 is built in the rocket chamber, and a traction ring 2 is provided at the tail of the three rockets 1, the traction ring 2 is connected to the rocket traction rope 3, and the three traction rings 2 are respectively connected to the polygonal regular through three rocket traction ropes 3 At the three corners of the capture net bag 4, the three rocket chambers are arranged in a scattered shape, and the installation scattering angle of the three rockets 1 is 2-4°. The scattering angle of the rocket chamber is related to the rocket launch distance and the net deployment area. The farther the distance, the smaller the angle, the smaller the net area, and the smaller the angle. The launching device 5 contacts the rocket 1, and the launching device 5 ignites the three rockets 1 for launch. After the rocket 1 is launched, the traction ring 2 at the tail works to drag the rocket traction rope 3. The rocket traction rope 3 leaves the rocket loading chamber 6 from the connection point between the net bag chamber and the rocket loading chamber 6, and tows and drags the polygonal regular capture net bag 4. The polygonal regular capture net bag 4 opens in the air under the traction force of the rocket 1, thereby realizing a large-area interception of the airspace and achieving the purpose of anti-UAV.

[0034] Embodiment 2

[0035] like Figure 5 and 6As shown, a networked rocket anti-UAV system comprises: a launching device 5 and a rocket loading chamber 6, wherein the central axes of the launching device 5 and the rocket loading chamber 6 are in the same plane, a rocket holder 7 is fixedly connected to the upper part of the rocket loading chamber 6, a net bag chamber is provided below the rocket loading chamber 6, the net bag chamber is connected to the rocket loading chamber 6, a polygonal regular capture net bag 4 is provided in the net bag chamber, in this embodiment, the polygonal regular capture net bag 4 is a square, four rocket chambers with equal spacing and uniform arrangement are provided on the rocket holder 7, rockets 1 are built in the rocket chamber, and traction rings 2 are provided at the tails of the four rockets 1, the traction rings 2 are connected to the rocket traction ropes 3, and the four traction rings 2 are respectively connected to the polygonal regular capture net bag 4 through four rocket traction ropes 3 At the four corners of the capture net bag 4, the four rocket chambers are arranged in a scattered shape, and the installation scattering angle of the four rockets 1 is 2-4°. The scattering angle of the rocket chamber is related to the rocket launch distance and the net deployment area. The farther the distance, the smaller the angle, the smaller the net area, and the smaller the angle. The launching device 5 contacts the rocket 1, and the launching device 5 ignites the four rockets 1 for launch. After the rocket 1 is launched, the traction ring 2 at the tail works to drag the rocket traction rope 3. The rocket traction rope 3 leaves the rocket loading chamber 6 from the connection point between the net bag chamber and the rocket loading chamber 6, and tows and drags the polygonal regular capture net bag 4. The polygonal regular capture net bag 4 opens in the air under the traction force of the rocket 1, thereby realizing large-area interception of the airspace and achieving the purpose of anti-UAV.

[0036] Embodiment 3

[0037] like Figure 7 and 8As shown, a networked rocket anti-UAV system comprises: a launching device 5 and a rocket loading chamber 6, wherein the central axes of the launching device 5 and the rocket loading chamber 6 are in the same plane, a rocket holder 7 is fixedly connected to the upper part of the rocket loading chamber 6, a net bag chamber is provided below the rocket loading chamber 6, the net bag chamber is connected to the rocket loading chamber 6, a polygonal regular capture net bag 4 is provided in the net bag chamber, in this embodiment, the polygonal regular capture net bag 4 is a pentagon, five rocket chambers are arranged at equal intervals and uniformly, a rocket 1 is built in the rocket chamber, and a traction ring 2 is provided at the tail of each of the five rockets 1, the traction ring 2 is connected to the rocket traction rope 3, and the five traction rings 2 are respectively connected to the polygonal regular capture net bag 4 through four rocket traction ropes 3 At the five corners of the capture net bag 4, the five rocket chambers are arranged in a scattered shape, and the installation scattering angle of the five rockets 1 is 2-4°. The scattering angle of the rocket chamber is related to the rocket launch distance and the net deployment area. The farther the distance, the smaller the angle, the smaller the net area, and the smaller the angle. The launching device 5 contacts the rocket 1, and the launching device 5 ignites the five rockets 1 for launch. After the rocket 1 is launched, the traction ring 2 at the tail works to drag the rocket traction rope 3. The rocket traction rope 3 leaves the rocket loading chamber 6 from the connection point between the net bag chamber and the rocket loading chamber 6, and traction and drags the polygonal regular capture net bag 4. The polygonal regular capture net bag 4 opens in the air under the traction force of the rocket 1, thereby realizing a large-area interception of the airspace and achieving the purpose of anti-UAV.

[0038] It is obvious to those skilled in the art that the present application is not limited to the details of the exemplary embodiments described above, and that the present application can be implemented in other specific forms without departing from the spirit or essential features of the present application. Therefore, the embodiments should be regarded as exemplary and non-limiting in all respects, and the scope of the present application is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present application. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

Claims

1. A networked rocket anti-UAV system, characterized in that: include: A launching device (5) and a rocket loading chamber (6) are provided. A rocket holding frame (7) is fixedly connected to the upper part of the rocket loading chamber (6). A net bag chamber is provided below the rocket loading chamber (6). The net bag chamber and the rocket loading chamber (6) are connected. A polygonal regular capture net bag (4) is provided in the net bag chamber. A plurality of rocket chambers arranged evenly at equal intervals are provided on the rocket holding frame (7). A rocket (1) is provided in the rocket chamber. A traction ring (2) is provided at the tail of the rocket (1). The traction ring (2) is connected to a rocket traction rope (3). The number of rocket chambers is consistent with the number of sides of the polygonal regular capture net bag (4). The plurality of traction rings (2) are respectively connected to the corners of the polygonal regular capture net bag (4) through the rocket traction rope (3). The plurality of rocket chambers are arranged in a scattered manner. As the number of rocket chambers increases, the scattering angle of the rocket chamber increases.

2. A networked rocket anti-UAV system according to claim 1, characterized in that: The central axes of the launching device (5) and the rocket loading chamber (6) are in the same plane.

3. A networked rocket anti-UAV system according to claim 1 or 2, characterized in that: The polygonal regular capture net bag (4) is an equilateral triangle, and three rocket compartments are provided on the rocket retaining frame (7). The installation scattering angle of the three rockets (1) is 2-4 degrees.

4. A networked rocket anti-UAV system according to claim 1 or 2, characterized in that: The polygonal regular capture net bag (4) is a square, and four rocket compartments are provided on the rocket retaining frame (7). The installation scattering angle of the four rockets (1) is 4-6 degrees.

5. A networked rocket anti-UAV system according to claim 1 or 2, characterized in that: The polygonal regular capture net bag (4) is a regular pentagon, and five rocket compartments are provided on the rocket retaining frame (7). The installation scattering angle of the five rockets (1) is 6-8 degrees.

6. A networked rocket anti-UAV system according to claim 1 or 2, characterized in that: The scattering angle of the rocket bay is related to the rocket launch distance and the net deployment area. The longer the distance, the smaller the angle, and the smaller the net area, the smaller the angle.

Images