RU219725U1 - UNMANNED AERIAL VEHICLE Grenade Launcher - Google Patents

Abstract

The utility model relates to the field of weapons, namely to devices for placing and throwing ammunition from an unmanned aerial vehicle. The technical objective of the proposed device is to expand the capabilities of the device for tasks related to the destruction of enemy firing points in buildings and structures in a city or on rough terrain. For this, an unmanned aerial vehicle grenade launcher is proposed, containing a magazine and a mechanism for feeding and throwing grenades through the grenade launcher barrel towards the target. The store is made in the form of a cylindrical drum, inside which there is a disk with radially oriented slots for placing grenades in them. A hole is made in the bottom of the drum body for feeding a grenade into the barrel of a grenade launcher. The grenade throwing mechanism contains a solenoid, the ferromagnetic core of which is installed coaxially with the grenade launcher barrel and equipped with a return spring. The magazine is equipped with a drive with an electric motor for rotating the slotted disk.

Description

The utility model relates to the field of weapons, namely to devices for placing and throwing ammunition from an unmanned aerial vehicle.

The closest technical solution to the proposed one is an unmanned aerial vehicle grenade launcher containing a grenade feed and drop mechanism (see patent RU No. 2733904 publ. 10/08/2020).

Its disadvantage is the limited possibilities of use, namely, only for targets located under the aircraft.

The technical objective of the proposed device is to expand the capabilities of the device for tasks related to the destruction of enemy firing points in buildings and structures in a city or on rough terrain.

For this, an unmanned aerial vehicle grenade launcher is proposed, containing a magazine and a mechanism for feeding and throwing a grenade through the grenade launcher barrel towards the target, while the magazine is made in the form of a cylindrical drum, inside of which there is a disk with radially oriented slots for placing grenades in them, and in the bottom of the case the drum has a hole for feeding a grenade into the grenade launcher barrel, the grenade throwing mechanism contains a solenoid, the ferromagnetic core of which is installed coaxially with the grenade launcher barrel and equipped with a return spring, the magazine is equipped with a drive with an electric motor for rotating a slotted disk.

A distinctive feature of the proposed technical solution is that the store is made in the form of a cylindrical drum, inside which there is a disk with radially oriented slots for placing grenades in them, and in the bottom of the drum body there is a hole for feeding a grenade into the barrel of a grenade launcher, the grenade throwing mechanism contains a solenoid, the ferromagnetic core of which is installed coaxially with the grenade launcher barrel and is equipped with a return spring, the store is equipped with a drive with an electric motor for rotating a slotted disk.

The essence of the proposed device is illustrated by drawings, where

in fig. 1 shows the general scheme of the device;

on fi. 2 section of FIG. 1 in A-A;

in fig. 3 section of FIG. 1 on B-B.

The grenade launcher of an unmanned aerial vehicle contains a magazine 1 and a mechanism for feeding and throwing a grenade 2 through the grenade launcher barrel towards the target. Shop 1 is made in the form of a cylindrical drum, inside which there is a disk 3 with radially oriented slots 4 for placing grenades 2 in them. A hole 6 is made in the bottom of the drum body for feeding a grenade into the barrel 7 of the grenade launcher. The grenade throwing mechanism contains a solenoid 8, the ferromagnetic core 9 of which is installed coaxially with the barrel 7 of the grenade launcher and is equipped with a return spring 10. The magazine is equipped with a drive with an electric motor 11 for rotating the disk 3 with slots. The grenade launcher works as follows. Targeting is carried out by means of remote control of the unmanned vehicle through the installed video camera, which helps the operator to control the aircraft and the grenade throwing mechanism. Power is supplied to the electric motor 11 at the command of the operator, and it rotates disk 3 with slots 4 through a drive in the form of a gear train. solenoid 8 is energized and ferromagnetic core 9 acts on the grenade and throws it at the target set by the operator. In this case, the return spring 10 is compressed, and when the voltage is removed, it returns the ferromagnetic core 9 to its original position.

This embodiment of the device allows you to hit targets located in buildings and structures in a city or on rough terrain.

Claims (1)

A grenade launcher of an unmanned aerial vehicle containing a magazine and a mechanism for feeding and throwing a grenade through the grenade launcher barrel towards the target, characterized in that the magazine is made in the form of a cylindrical drum, inside of which there is a disk with radially oriented slots for placing grenades in them, and in the bottom of the drum body a hole is made for feeding a grenade into the grenade launcher barrel, the grenade throwing mechanism contains a solenoid, the ferromagnetic core of which is installed coaxially with the grenade launcher barrel and equipped with a return spring, the magazine is equipped with a drive with an electric motor for rotating a slotted disk.

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