BG4580U1 - Drone interceptor with a blade propeller and marx generator - Google Patents

Abstract

The present utility model pertains to drone interceptor with a blade propeller and a Mark generator and consists of an aerial vehicle which is aerodynamically steered by means of wings and control surfaces, and is accelerated in airspace by a blade propeller. The device is equipped with a Marx generator and an electrode. Said interceptor intercepts and neutralizes drones using electric discharges which develop in the airspace between the interceptor and the drone at a time when the interceptor approaches the drone at a sufficiently close distance. After neutralizing the drone, the interceptor makes a controlled return flight back to the launch site or to another safe landing site. Thus, said interceptor can be used multiple times and, moreover, is capable of striking multiple drones in a single flight. Said interceptor is used to stop drones which violate the airspace of secure sites or State borders, in military operations, for combatting terrorism, etc. According to Fig. 1, said drone interceptor with a blade propeller and a Marx generator consists of an aerodynamically steered aerial vehicle (1), a blade propeller (2), a Marx generator (3) and an electrode (4).

Description

Field of technique

The utility model relates to a Marks generator propeller drone interceptor consisting of an aircraft aerodynamically controlled by means of wings and control surfaces and accelerated through the air by a propeller. The device has a Marx generator and an electrode. The interceptor is used to intercept and neutralize drones using electrical discharges that develop through the air space between the interceptor and the drone when the interceptor is close enough to the drone. After neutralizing the drone, the interceptor flies in a controlled manner back to the launch site or to another safe landing site. In this way, the interceptor can be used repeatedly, and in one flight it is able to hit multiple drones. The application is when stopping drones - violators of the airspace of guarded objects and interstate borders, during military operations, combating terrorism, etc.

Prior art

A multipurpose drone interceptor is known, consisting of an unmanned aerial vehicle (UAV) with a propeller and ram suspended on a damped arm to the airframe of the UAV. Neutralizing drones is done by homing the UAV into contact with the drone, at which point the battering ram attacks the drone and disables it [1].

A disadvantage of the known technique is that the interceptor needs direct physical contact with the drone, which is not always possible due to the need for high precision and flight maneuverability. Another disadvantage of the known technique is that in case of direct contact of the UAV with the drone, constructive destruction of the airframe of the UAV is possible. Another drawback of the existing technique is that in one flight of the interceptor it is possible to neutralize only one drone.

Technical nature of the utility model

The task of the utility model is to create a drone interceptor with a propeller thruster and a Marx generator that can neutralize drones from a certain distance and is used repeatedly so that in one flight it can hit several drones.

According to the utility model, the task was solved by creating a drone interceptor with a propeller engine and a Marx generator, consisting of an aircraft with aerodynamic control by means of a wing and control surfaces, a propeller engine, a Marx generator and an electrode.

The advantages of the utility model are that by using a Marx generator and a drone strike electrode, direct contact of the interceptor with the drone is avoided, thus making the maneuvering of the interceptor easier and more efficient. Also, the interceptor does not come into direct contact with the drone, protecting its glider from damage and destruction. In addition, due to the rapid recharge of Marx's generator, it is possible to hit several drones flying at the same time during the same flight.

Explanation of the attached figure

An exemplary embodiment is shown in the attached Figure 1, which is a general schematic of a drone interceptor with a propeller and a Marks generator.

Example implementation of the utility model

According to fig. 1 the Marks Generator Propeller Drone Interceptor consists of an aerodynamic control aircraft 1, a propeller 2, a Marks Generator 3 and an electrode 4.

Device action

Marx's Propeller Generator Drone Interceptor works as follows. In the presence of a drone that violates the safety of a protected object or air volume, the interceptor is launched, consisting of an aircraft with aerodynamic flight control 1, using the propeller 2 for acceleration. During the flight, the Marks generator 3 is charged. When the interceptor gets close enough to the drone to be neutralized, a series of electric discharges are released from the Marks generator 3 through electrode 4. Electric discharges are formed starting from the electrode 4 and entering the airspace ahead of the interceptor, the discharges reaching the drone and striking its electronics. The Marx generator is able to release discharges of a certain polarity - positive or negative. The discharge is attracted to the drone due to the drone being either of neutral polarity or of known polarity in advance, which depends on the flight conditions in the protected airspace. As a result of the discharge entering the drone and subsequent destruction of its electronics, there is a crash in flight of the drone, which loses control and falls. After releasing the series of discharges, the Marks 3 generator is ready to release a new series of discharges within the same flight in order to neutralize a second drone. The procedure can be repeated many times. After completing the drone neutralization task, the interceptor lands in a controlled manner at a designated location. The interceptor can then be used again for another flight and the neutralization of other drones accordingly.

Claims (1)

A drone interceptor with a propeller engine and a Marx generator, consisting of an aerodynamically controlled aircraft and a propeller engine, characterized in that a propeller engine (2) is installed in the rear part of an aerodynamic aircraft engine (1) and in the front part of the aerodynamically controlled aircraft (1) is mounted a Marx generator (3) to which is connected an electrode (4) projecting forward from the fuselage of the aerodynamically controlled aircraft (1)