CN118882408A - A rocket blaster and a drone blasting device - Google Patents

Abstract

The present application provides a rocket blaster, including: a launch box, the launch box includes a box body and a box cover; a launch tube, which is arranged in the box body; a rocket engine, which is arranged in the launch tube; an explosive belt, which is arranged in the box body, the explosive belt includes a head connector and a tail connector, and the head connector is connected to the rocket engine; a fuze assembly, the fuze assembly includes a fuze combiner and a fuze, one end of the fuze combiner is connected to the fuze, and the other end of the fuze combiner is connected to the tail connector; a control device, which is arranged in the box body, and the control device is connected to the fuze assembly to trigger the fuze action and ignite the explosive belt; and a command control box, which is arranged outside the box body to receive an external control signal to trigger an ignition signal to ignite the rocket engine for launch. The present application also includes a drone blasting device.

Description

A rocket blaster and a drone blasting device

Technical Field

The present application belongs to the technical field of blasting materials, and specifically relates to a rocket blaster and an unmanned aerial vehicle blasting device.

Background Art

The minesweeping equipment used on the battlefield can be roughly divided into mechanical minesweepers and explosive minesweepers. The main combat use scenarios of these two types of minesweepers are different. Mechanical minesweepers are heavy and inefficient, so they are mainly used to clear minefields after the war. In the process of offensive operations at the front of the position or the rapid assembly of troops, explosive minesweepers are mainly used to clear minefields or obstacles such as barbed wire.

Rocket blasters are mainly used to open pathways in anti-tank minefields and anti-infantry minefields. Rocket blasters used to open pathways in anti-tank minefields are mostly vehicle-mounted, generally installed on the fenders on both sides of the tank or on special mine-sweeping vehicles. However, vehicle-mounted blasters are usually large in size and cannot be carried by a single soldier. At the same time, vehicle-mounted blasters require vehicles for transportation and loading, and vehicles are large targets and easily discovered, thus limiting the concealment of the blasters.

Summary of the invention

The present application aims to provide a rocket blaster which is portable, easy to operate and highly concealed by a single soldier.

This application adopts the following technical solutions:

A rocket blaster, comprising:

A launch box, comprising a box body and an openable and closable box cover;

A launching tube, wherein the launching tube is arranged in the box;

A rocket engine, wherein the rocket engine is arranged in the launch tube;

An explosive belt, the explosive belt is arranged in the box, the explosive belt comprises a head connecting piece and a tail connecting piece, and the head connecting piece is connected to the rocket engine;

A fuze assembly, the fuze assembly comprising a fuze combiner and a fuze, one end of the fuze combiner is connected to the fuze, and the other end of the fuze combiner is connected to the tail connector;

A control device, the control device is disposed in the box, the control device is connected to the fuze assembly to trigger the fuze action and ignite the explosive belt; and

A command and control box is disposed outside the box body and is used to receive an external control signal to trigger an ignition signal to ignite and launch the rocket engine.

Furthermore, the control device includes a front control rope and a control parachute connected to the front control rope, and the front control rope is provided with a rope ring and a fire hook.

Furthermore, a connecting rope is provided on the fuze assembly, and the connecting rope is inserted into the rope ring;

A trigger rope is provided on the fuse, and the trigger rope is hung in the trigger hook.

Furthermore, the command and control box includes:

a main control board, the main control board being used to receive external control signals, process external control signals, and send internal control signals; and

Battery.

Furthermore, the rocket engine includes a warhead, an electric igniter, a combustion chamber, a propellant column, and a nozzle seat.

Furthermore, a shoulder strap ring is provided on the box body for installing a shoulder strap.

Furthermore, a ground support frame is provided on the box body.

Furthermore, a plurality of lifting rings are arranged on the box body.

The present application provides a drone blasting device, including the rocket blaster as described above, and also includes a drone, wherein a mounting mechanism is provided at the bottom of the drone, and the rocket blaster is mounted on the mounting mechanism through the hanging ring.

Beneficial effects of this application:

The present application integrates the launch tube, rocket engine, explosive belt and control components into a launch box, which not only reduces the space occupied by the rocket blaster during launch, improves the convenience and concealment of individual carrying, but also effectively reduces the operating steps of equipment installation and improves operational efficiency.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG1 is a side cross-sectional view of an embodiment of the present application;

FIG2 is a schematic diagram of the internal structure of an embodiment of the present application;

FIG3 is a schematic diagram of the structure of a control device according to an embodiment of the present application;

FIG4 is a schematic diagram of the structure of a UAV blasting device according to an embodiment of the present application;

In the figure:

1 rocket launcher;

100 launch box, 110 box body, 111 ground support frame, 112 lifting ring, 113 shoulder strap ring, 120 box cover, 121 foam board;

200 launch tubes;

300 rocket engine, 310 warhead, 320 electric igniter, 330 combustion chamber, 340 propellant column, 350 nozzle seat,

400 command and control box;

500 explosive belt, 510 traction rope, 520 head connector, 530 tail connector;

600 control device, 610 front control rope, 611 rope ring, 612 fire hook, 620 control parachute;

700 fuze assembly, 710 fuze combiner, 720 fuze, 730 trigger rope, 740 connecting rope;

800 drones;

900 mounting mechanism.

DETAILED DESCRIPTION

In order to make the above-mentioned features and advantages of the present application more obvious and easy to understand, the specific implementation methods of the present application are described in detail below in conjunction with the accompanying drawings. In the following description, many specific details are set forth to facilitate a full understanding of the present application. However, the present application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without violating the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.

In the description of the present application, it should be understood that the terms "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present application.

1-3, the present application provides a rocket blaster, comprising:

A launch box 100, the launch box 100 comprises a box body 110 and an openable and closable box cover 120;

A launching tube 200, wherein the launching tube 200 is disposed in the box body 110;

A rocket engine 300, wherein the rocket engine 300 is disposed in the launch tube 200;

An explosive belt 500, wherein the explosive belt 500 is disposed in the box body 110, and the explosive belt 500 comprises a head connector 520 and a tail connector 530, wherein the head connector 520 is connected to the rocket engine 300;

A fuze assembly 700, wherein the fuze assembly 700 comprises a fuze combiner 710 and a fuze 720, wherein one end of the fuze combiner 710 is connected to the fuze 720, and the other end of the fuze combiner 710 is connected to the tail connector 530;

A control device 600, wherein the control device 600 is disposed in the housing 110, and the control device 600 is connected to the fuze assembly 700 to trigger the fuze 720 to ignite the explosive belt 500; and

The command and control box 400 is disposed outside the housing 110 and is used to receive an external control signal to trigger an ignition signal to ignite and launch the rocket engine 300.

Specifically, when the present application is used, it is placed in a suitable position and the box cover 120 is opened; a control signal is sent to the command and control box 400 through an external control system, and the command and control box 400 processes the signal after receiving the external control signal and then sends an internal control signal to control the ignition of the rocket engine 300; the rocket engine 300 ignites and launches and brings out the explosive belt 500 and the control device 600, and under the action of the control device 600, the fuse 720 is triggered to ignite the explosive belt 500, thereby completing a large-scale blasting and obstacle clearance operation.

In the present application, the launch tube 200, rocket engine 300, explosive belt 500 and control device 600 are integrated into the launch box 100, which effectively improves the convenience and concealment of individual carrying. At the same time, the present application has a simple structure and is easy to set up.

Specifically, the box cover 120 is further provided with a foam plate 121 capable of placing the fuze assembly 700 , and the foam plate 121 is provided with grooves.

1-3 , it can be understood that the control device 600 includes a front control rope 610 and a control parachute 620 connected to the front control rope 610 , and the front control rope 610 is provided with a rope ring 611 and a fire hook 612 .

Specifically, the front control rope 610 is connected to the fuze assembly 700. The rocket engine 300 ignites and flies out of the launch tube 200, dragging the explosive belt 500 to fly over the target area. The control device 600 flies out of the launch box 100 under the traction of the explosive belt 500, and the control parachute 620 is deployed against the wind. Under the combined effect of gravity and the resistance of the control parachute 620, the explosive belt 500 is straightened in the air and falls above the obstacles in the target area. At the same time, the fuze 720 is activated and delayed to detonate the explosive belt 500, and the explosion removes obstacles such as mines or barbed wire.

3 , it can be understood that the fuze assembly 710 is provided with a connecting rope 740 , and the connecting rope 740 is inserted into the rope ring 611 ;

The fuse 720 is provided with a trigger rope 730 , and the trigger rope 730 is hung in the trigger hook 612 .

Specifically, the length of the connecting rope 740 should be greater than the overall length of the ignition rope 730, the ignition hook 612 and the ignition hook connecting rope; when the rocket engine 300 is launched, the explosive belt 500 is dragged out of the box 110, and the fuse assembly 700 and the control device 600 are dragged out of the box 110. When the fuze assembly 700 is dragged, the ignition rope 730, the ignition hook 612 and the ignition hook connecting rope are acted upon by the front control rope 610 to trigger the action of the fuze 720. After the fuze 720 is triggered and pulled off, the connecting rope 740 is tightened and the front control rope 610 and the control parachute 620 are brought out. The control parachute 620 unfolds against the wind to stretch the explosive belt as a whole.

It is understandable that the command and control box 400 includes:

a main control board, the main control board being used to receive external control signals, process external control signals, and send internal control signals; and

Battery.

Specifically, the main control board may be a PCB control board integrated with a wireless signal transceiver or a wired signal transceiver and other electrical components. It is understandable that those skilled in the art may use existing technical means to implement the functions of the controller.

1 , it can be understood that the rocket engine 300 includes a warhead 310 , an electric igniter 320 , a combustion chamber 330 , a propellant charge 340 , and a nozzle seat 350 .

2 , it can be understood that the box body 110 is provided with a shoulder strap ring 113 for installing a shoulder strap.

Specifically, by providing the shoulder strap ring 113, it is convenient for a single soldier to install the shoulder strap for carrying, thereby improving portability.

1 , it can be understood that a ground support frame 111 is disposed on the box body 110 .

Specifically, by providing a ground support, the present application can be placed on the ground or other locations at a more suitable angle, making it easier to open the box cover 120 and launch it.

2 , it can be understood that a plurality of lifting rings 112 are provided on the box body 110 .

Specifically, by providing the lifting ring 112, the present application can be hoisted on equipment such as drones.

Referring to Figure 4, it can be understood that the present application also provides a UAV blasting device, including the rocket blaster described above, and the UAV blasting device also includes a UAV 800, and a mounting mechanism 900 is arranged at the bottom of the UAV 800. The mounting mechanism 900 can be made of a lightweight material with a certain strength as a frame structure, such as an aluminum profile, wherein the mounting mechanism 900 has an opening at the bottom, and the mounting mechanism 900 is provided with a hook compatible with the lifting ring, so as to mount the rocket blaster on the mounting mechanism 900 through the lifting ring.

The above description is only the preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the principles of the present application shall be included in the protection scope of the present application.

Claims (9)

1. A rocket blaster, comprising:

The transmitting box comprises a box body and an openable box cover;

the transmitting cylinder is arranged in the box body;

The rocket engine is arranged in the launching cylinder;

The explosion belt is arranged in the box body and comprises a head connecting piece and a tail connecting piece, and the head connecting piece is connected with the rocket engine;

The fuze assembly comprises a fuze combiner and a fuze, one end of the fuze combiner is connected with the fuze, and the other end of the fuze combiner is connected with the tail connecting piece;

The control device is arranged in the box body and connected with the fuze component to trigger the fuze to act and ignite the explosion belt; and

And the command control box is arranged outside the box body and is used for receiving an external control signal to trigger an ignition signal so as to enable the rocket engine to ignite and emit.

2. A rocket blaster as recited in claim 1, wherein said control means comprises a front control cord and a control umbrella connected to said front control cord, said front control cord having a loop and a pulling hook disposed thereon.

3. A rocket blaster according to claim 2, wherein the fuze combiner is provided with a connecting rope which penetrates into the rope loop;

The fuse is provided with a fire pulling rope which is hung in the fire pulling hook.

4. A rocket blaster as recited in claim 1, wherein said command and control box comprises: the main control board is used for receiving external control signals, processing the external control signals and sending out internal control signals; and

And a battery.

5. A rocket blaster as recited in claim 1, wherein said rocket engine comprises a warhead, an electric igniter, a combustion chamber, a firing cartridge, and a nozzle block.

6. A rocket blaster as claimed in any one of claims 1 to 5, wherein a strap ring is provided on said housing for mounting straps.

7. A rocket blaster as claimed in any one of claims 1-5, wherein said tank is provided with a ground support frame.

8. A rocket blaster as claimed in any one of claims 1-5, wherein said tank is provided with a plurality of hanging rings.

9. Unmanned aerial vehicle blasting device, its characterized in that includes a rocket blaster of claim 8, still includes unmanned aerial vehicle, the unmanned aerial vehicle bottom is provided with the mount mechanism, rocket blaster passes through rings are hung on the mount mechanism.