Single-thread device for damaging unmanned aerial vehicles

Abstract

The invention relates to the field of protection against unmanned aerial vehicles. A single-thread device for damaging unmanned aerial vehicles, consisting of one thread, one end of which is fixed with the possibility of the above-mentioned thread being in the airspace. The technical problem being solved is the creation of a single-thread device for damaging unmanned aerial vehicles. The technical result is the implementation of a single-thread device for damaging unmanned aerial vehicles. One independent claim. One illustration.

Description

FIELD OF TECHNOLOGY TO WHICH THE INVENTION RELATES

The field of application of the claimed invention is protection against unmanned aerial vehicles. The claimed invention (hereinafter also referred to as “invention”) relates to technical solutions for protection against unmanned aerial vehicles, i.e. to such a field of technology as protection against unmanned aerial vehicles.

TECHNICAL LEVEL

Various devices for protection against aircraft using cables and similar stretchers are well known. At the same time, there are currently no analogues of the claimed invention; and to achieve which, by obtaining for the first time a technical means having the purpose of a single-thread device for damaging unmanned aerial vehicles, thereby achieving a technical result consisting in the implementation of a single-thread device for damaging unmanned aerial vehicles, the claimed new, industrially applicable technical solution leads, which is unique: a single-thread device for damaging unmanned aerial vehicles, consisting of one thread, one end of which is fixed with the possibility of the above-mentioned thread being in the airspace, not only being thus an obstacle to the movement of the unmanned aerial vehicle in that place of the airspace where the above-mentioned thread is located, but also creating a threat to the flight of the unmanned aerial vehicle in that area of the airspace where the above-mentioned thread may be located. The stated objective is achieved by the device (design) of the Single-thread device for damaging unmanned aerial vehicles, which is a product of human activity, the elements of which are in a constructive unity and functional relationship corresponding to the concept of a device, as an object claimed as an invention.

DISCLOSURE OF THE ESSENCE OF THE INVENTION

The essence of the invention, as a technical solution, is expressed in the following set of essential features:

1. A single-thread device for damaging unmanned aerial vehicles, consisting of one thread, one end of which is fixed with the possibility of the above-mentioned thread being in the airspace;

sufficient to achieve the technical result provided by the above invention—the single-thread device for damaging unmanned aerial vehicles—consisting of one thread, one end of which is fixed with the possibility of the above-mentioned thread being in the airspace.

BRIEF DESCRIPTION OF THE DRAWINGS

The figure shown schematically shows, as an example, when one end of the thread 1 is attached to the aerostat 2, and the other end of the thread 1 is attached to the weight 3.

IMPLEMENTATION OF THE INVENTION

The invention will be described in detail below. However, it should be noted that the embodiments of the invention described below do not limit the invention. In addition, the constituent elements of the embodiments of the invention described below include elements that can be easily imagined by an ordinary person skilled in the relevant technical field, or elements that are essentially the same as elements that can be easily imagined by an ordinary person skilled in the relevant technical field. The invention can be implemented by implementing the claimed Single-thread device for damaging unmanned aerial vehicles, when, for example, thread 1, having characteristics determined depending on the tasks to be solved, for example, but not excluding otherwise, elasticity, strength, thickness, length, design, etc., allowing the aerostat 2 to lift the above-mentioned thread 1 into the airspace, is attached at one end to the aerostat 2 below, which is capable of lifting the above-mentioned thread 1 into the airspace, and the other end is attached to weight 3, which does not allow the aerostat 2 below to lift and/or move thread 1 together with this weight 3, after which the aerostat 2 below is filled with a gas lighter than the surrounding air, for example, but not excluding otherwise, hydrogen, in such a way that the lifting force of this aerostat 2 allows it to rise into the airspace to a flight altitude corresponding to the length connecting this aerostat 2 with the above-mentioned weight 3 of the above-mentioned thread 1, but does not allow lifting and/or moving the above-mentioned weight 3, which is placed on the support surface 5, in the airspace above which the above-mentioned thread 1 connecting this aerostat 2 with the above-mentioned weight 3 must be located, after which the above-mentioned aerostat 2 is allowed to rise into the airspace, as a result of which an obstacle corresponding to at least the length of the above-mentioned thread 1 connecting the above-mentioned aerostat 2 with the above-mentioned weight 3 is created above the support surface 5 for the unmanned aerial vehicle, for which hitting the above-mentioned obstacle, which is practically impossible to notice and determine the boundaries of when approaching, means entanglement of the above-mentioned thread 1 connecting the above-mentioned aerostat 2 with the above-mentioned weight 3 as a result of winding the above-mentioned thread 1 connecting the above-mentioned aerostat 2 with the above-mentioned weight 3 onto at least one rotating element of the unmanned aerial vehicle in contact with the air environment, preventing the normal rotation of this element, and/or covering any of the surfaces and/or clogging any of the internal volumes of the unmanned aerial vehicle connecting the above-mentioned aerostat 2 with the above-mentioned weight 3 by the above-mentioned thread 1 and/or any other damaging effect by any other element of the above-mentioned Single-thread device for damaging unmanned aerial vehicles, and/or any other damaging effect, for example, but not excluding otherwise, combustion upon contact of at least one ignition source with hydrogen filling the above-mentioned aerostat 2, disrupting the normal flight of the unmanned aerial vehicle up to the complete impossibility of flight, including, for example, but not excluding otherwise, without significant mechanical damage, with the possibility of capturing and fully or partially using the captured enemy unmanned aerial vehicle for one's own purposes. If necessary, the statement of the above embodiment of the claimed invention should be considered as a statement of at least the best of the embodiments of the claimed invention contemplated by the applicant.

Finally, it should also be noted that while the invention has been described with reference to exemplary embodiments of its implementation, it should be understood that the invention is not limited to the exemplary embodiments, material or structures described above, but covers any and all variants within the scope of the invention claim. It should also be understood that the invention is intended to cover various modifications and equivalent arrangements and any other variants of using the invention. In addition, it should be understood that while various elements of the exemplary embodiments are described in various combinations and configurations that are exemplary, other combinations and configurations including a greater, lesser number of elements or only one element, having a set of essential features of the invention given in the invention claim, also correspond to the essence and scope of the invention.

INDUSTRIAL APPLICABILITY

Is obvious from the description and the nature of the invention.

Claims

1. A single-thread device for damaging unmanned aerial vehicles, consisting of one thread, one end of which is fixed with the possibility of the above-mentioned thread being in the airspace.