RU2481244C1 - Bognatov's aircraft rocket system - Google Patents

Abstract

FIELD: transport.

SUBSTANCE: invention relates to aircraft rocket systems and is intended for atmospheric flights. Proposed system comprises aircraft, rocket and docking device. Rocket incorporates system for guidance to docking device. For additional acceleration of aircraft in flight said rocket is coupled with therewith by coupler.

EFFECT: additional acceleration.

9 cl, 3 dwg

Description

The invention relates to the field of aviation missile systems. It can be used in aviation.

Known aircraft missile system [1], containing an airplane, a glider and a rocket made inside the glider. The plane takes off, a glider with a rocket is towed, then the glider is separated and a rocket starts from it.

The disadvantage of this device is the low speed of the aircraft on the main section of the track for systems containing passenger civilian passenger aircraft, taking off at civilian airports and meeting international standards for low noise levels during take-off.

The challenge facing the invention is to provide the possibility of additional acceleration of the aircraft for flight in the areas between the starting and landing points in combination with the low noise level of the aircraft during take-off, meeting international standards for low noise during take-off at the airport.

This problem is solved in that the aviation missile system containing the aircraft and the rocket further comprises a docking device and it is possible to connect the aircraft with a docking device and a rocket during flight with the ability to accelerate the aircraft with a rocket, and the rocket contains a guidance system to the docking device.

An aviation missile system comprises an MHD generator, an air ionizer, and an electric and magnetic field generating device configured to accelerate ionized air and remove ionized air from the flight path in front of the device.

The docking device comprises an emitter configured to generate radiation for the guidance system.

The docking device comprises a shock absorber.

The docking device comprises a shock absorber comprising a bellows, with the possibility of filling the bellows with gas and discharging gas from the bellows.

An aviation missile system that contains an additional aircraft configured to connect in flight with the first aircraft and further accelerate the first aircraft during the flight, while the additional aircraft is made in the form of a jet aircraft.

The additional aircraft is made in the form of a supersonic aircraft.

An aviation missile system contains at least two docking devices and at least two missiles.

An aviation missile system comprises a missile launcher.

Such a technical solution will allow passenger aircraft of civil aviation to take off and land at civilian airports with low noise levels and additionally be accelerated outside airports by missiles or additional jet aircraft that are interfaced with passenger aircraft in flight. This will significantly increase flight speed and reduce flight time over long and medium distances, for example, several times.

No technical solutions were found that fulfill the task with the same technical means.

Figure 1 shows a schematic diagram of the Bogdanov aviation missile system, the main view with a local section at the junction of the docking device with the rocket.

Figure 2 shows a schematic diagram of a Bogdanov aviation missile system, front view.

Figure 3 shows a schematic diagram of the Bogdanov aviation missile system, top view.

Bogdanova aviation missile system consists of the following elements.

A docking device 2 is attached to the airplane 1. A rocket 3 is attached to the docking device 2. For example, a single-stage ballistic missile or the first stage of an intercontinental ballistic missile equipped with a fairing. In the head part of the rocket 3, a guidance system is made, made with the ability to direct the rocket during flight to the docking device 2.

Bogdanova aviation missile system, hereinafter simply a system, works as follows.

Aircraft 1, for example, a civilian aircraft having a low noise level during take-off, permitted by GOST, EU standards and standards, launches (takes off) from a civilian airport.

After the start (take-off) of the aircraft 1, the docking device 2, connected to the airplane, constantly emits special radiation, for example, infrared, for the missile guidance system at the docking device, for example, rocket 3, which starts from a launching unit located at a great distance from the civilian airport , which is guaranteed not to be heard the sound of a rocket launch. For example, at a distance of over 10 km from the civilian airport.

The distance is chosen so that the noise from the launch of rocket 3 was not heard at the civilian airport. After the launch of rocket 3, the aircraft engines are turned off, it is put into planning mode, and using the guidance system, the rocket 3 and docking device 2 are docked. After that, rocket 3 accelerates airplane 1 to supersonic speed and quickly flies airplane 1 over a long distance. For example, the route Moscow - New York in 30 minutes. After the rocket has consumed all the fuel, the plane 1 with the spent stage of the rocket 1, mounted in the docking device 2, lands like a regular plane. In this case, the weight of the aircraft, docking device and spent rocket stage without spent fuel coincides with the estimated weight of the aircraft with fuel, what would it be without a docking device and without a rocket.

Various options and additions.

The system may comprise an MHD generator, an air ionizer, and an electric and magnetic field generating device configured to accelerate ionized air and remove ionized air from the flight path in front of the device. A device for generating electric and magnetic fields, configured to accelerate ionized air and remove ionized air from the flight path in front of the device, is described by the author in his patented invention "Bogdanov’s electric rocket engine" [2]. The difference lies in the magnetic field coil, which in the proposed system consists of wires of a self-excited MHD generator.

In this case, the MHD generator is self-excited, connected to the rocket engine and connected to a device for creating electric and magnetic fields, configured to accelerate ionized air and remove ionized air from the flight path in front of the device. The system contains a complex of sectioned electrodes made along a magnetic field coil, the wires of which are connected to the wires of a self-excited MHD generator.

When the rocket engine is running, the flame creates current in the MHD generator. During the operation of the MHD rocket engine, the generator self-excites and amplifies the current. Current flows through a coil of magnetic field, partially made along the wings of the aircraft, and creates a magnetic field. Voltage is applied to the sectioned electrodes, they create crossed electric and magnetic fields, an ionizer ionizes the air in the direction of the ionizing radiation, air plasma enters the crossed electric and magnetic fields and spreads to the sides, reducing air resistance during flight.

The system may comprise an additional aircraft that interfaces with the first aircraft, for example, before being accelerated by a rocket. In this case, as an additional aircraft, a supersonic military aircraft is used, which starts from a military airfield, which has no low noise requirements like a civilian airfield. During the flight, the additional aircraft is connected by a tow rope to the first aircraft, additionally accelerates it, then undocked and lands at the military airfield.

The system may include a docking device that contains a shock absorber containing a bellows, while it is possible to fill the bellows with gas before docking and to release gas from the bellows.

In this case, the bellows of the shock absorber is filled with gas, for example, air, before joining under pressure. During docking with the rocket, the shock absorber bellows contracts and extinguishes the first pulse of the rocket, protecting the docking device.

An additional supersonic jet aircraft may be connected by a towing cable to the docking device to further accelerate the first aircraft.

An aviation missile system may contain several docking devices and several missiles with missile launchers. For example, one docking device is made over the fuselage of the aircraft, and several docking devices are made on its wings. In this case, during the flight, the missiles alternately join with various docking devices and accelerate the aircraft. Missiles accelerate the aircraft either in turn, or first alone, then others, or all together at the same time.

Information sources

1. Patent RU 2353546 C2.

2. Bogdanov I.G. Electric rocket engine Bogdanov. Patent No. 2046210. Application No. 5064411. Priority of the invention October 5, 1992

Claims (9)

1. An aviation missile system comprising an airplane and a missile, characterized in that it comprises a docking device, and it is possible to connect the airplane with a docking device to the missile during flight, with the ability to accelerate the airplane with a missile, the missile comprising a guidance system to the docking device. 2. The aviation rocket system according to claim 1, characterized in that it contains an MHD generator, an air ionizer and a device for generating electric and magnetic fields, configured to accelerate ionized air and remove ionized air from the flight path in front of the device. 3. The aviation missile system according to claim 1, characterized in that the docking device comprises an emitter configured to generate radiation for the guidance system. 4. The aviation missile system according to claim 1, characterized in that the docking device comprises a shock absorber. 5. The aviation missile system according to claim 1, characterized in that the docking device comprises a shock absorber comprising a bellows, while it is possible to fill the bellows with gas and to release gas from the bellows. 6. The aviation missile system according to claim 1, characterized in that it comprises an additional aircraft configured to connect in flight with the first aircraft and additionally accelerate the first aircraft during flight, while the additional aircraft is made in the form of a jet aircraft. 7. The aviation missile system according to claim 1, characterized in that the additional aircraft is made in the form of a supersonic aircraft. 8. The aviation missile system according to claim 1, characterized in that it contains at least two docking devices and at least two missiles. 9. The aviation missile system according to claim 1, characterized in that it contains a missile launcher.

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