EA040117B1 - AIRCRAFT FOR DESTROYING ASTEROIDS USING ATMOSPHERIC ELECTRICITY (GRAVITALET BLESKIN-CHURAKOVOY "BECH"2) - Google Patents

Description

The invention relates to aircraft used in aviation and astronautics to destroy asteroids by laser beam action using atmospheric electricity.

It is known that at present there are no such aircraft in the world.

Known devices for the use of atmospheric electricity: patents for invention No. 2332816, 2000128, 2369991, 2482640, 2030132, 2693166, 2571237, 2663237, EA 029621, EA 028417, EA 039838, Eurasian application for invention No. 0.2017

Known laser devices powered by non-renewable sources of electricity: the Russian combat laser Peresvet, the Laws system in the USA, the US-Israeli Nautilus missile defense system.

The disadvantages of these laser devices are dependence on a powerful source of non-renewable electricity, deployment time, heaviness, and large dimensions.

A new previously unknown technical solution is presented for the destruction or displacement of asteroids from a dangerous trajectory, which is a complex consisting of three interconnected devices

1) aircraft, aircraft, using atmospheric electricity;

2) voltage converter, PN;

3) laser device, LU.

1. The aircraft is a device consisting of a ball 18 made of a durable elastic, heat-resistant material with a metallized coating on the outside, filled with air, having an air heater 19 inside, powered by a battery, outside - an air supply compressor 31 and an air discharge valve from the ball 32. The ball is tightly coupled with the fuselage 2, which has the shape of a cone truncated from above with a base in the form of a disk 20 made of metal. Inside the fuselage there is a hemispherical metal recess. Wing 21 made of metal is made in the form of a disc, including in its plane four fender liner 22, located parallel to the base under the fuselage and attached to it by four metal supports 23. Rudder 24 is located vertically in the center between the base of the fuselage and the wing, four rods for controlling the movement of the wing liner 25, under the lower surface of the wing - four rocket motors 26 located crosswise with nozzles outward from the center and four support legs 27. In the fuselage there is a cockpit 7, isolated from it by a coating of a material with thermal protection from the effects of an elevated temperature of the ball and a low air atmosphere 31. In the cabin is the control panel (PU) 30 LA (Fig. 2, 3).

Electric station 28 (Fig. 1), which consists of a receiving unit in the form of a fuselage, and from it, from its surface, a needle 10, covered with a dielectric, is lowered, the end of which is connected to the upper disk of the capacitor, which is enclosed in a chamber of dielectric 17, from the base 8 there is a needle 9, covered with a dielectric, on top of which the lower disk of the capacitor is fixed. An air network is connected to the upper needle, on the upper branch of which there is a spark gap 11, the second electrode of which is connected to an inductance coil 12, which is connected to the lower needle 9, the second self-inductance coil 15 is connected to a rectifier 16 connected to a large capacitor 13 connected to battery 14 and 29 (charged initially from the mains, then from atmospheric electricity). The capacitor is enclosed in a dielectric chamber and has a spark gap 3. To protect the battery from overcharging, a double switch 5 is introduced on the upper and lower needles, the battery charge indicator 4 is connected to it (battery). For remote control of the station, a remote control unit 1 was introduced, connected to a double switch and a battery charge indicator, for example, a voltmeter. The protection of the power plant 28, which is located inside the fuselage of the aircraft, from external influences, the safety of operation is carried out by an insulating all-metal casing coated with a dielectric 6, the fuselage is covered with a material with high electrical conductivity (for example, high-grade gold) to enhance the accumulation of atmospheric electricity, and the lower needle 9 , insulated with a dielectric from the base of the fuselage 20, exits through the lower surface of the fuselage into the atmosphere through a switch 36, connecting with a dielectric-coated folding antenna, the peripheral end of which is bare 35.

The proposed aircraft differs from previously known ones in that it is connected through a switch to a folding antenna coated with a dielectric, the peripheral end of which is bare.

LA works as follows.

To take off the aircraft from the ground and surface position to heat the air in the balloon, placed in it by an electric heater, initially the battery 29 is charged from the mains, later - in flight, this battery, like the battery 14, will be charged from the atmospheric electricity used by the power plant (the complex can be used batteries). Heating the air in the ball reduces the air density in it due to the splitting of water molecules by high temperature. This process of creating a difference in the density of the air in the balloon relative to the air of the atmosphere provides a smooth controlled takeoff and climb of the aircraft. A controlled decrease in the temperature of the air in the balloon creates a smooth descent and landing, as well as a controlled hover of the aircraft.

- 1 040117

During the flight of an aircraft in the atmosphere due to the triboelectrollization of the fuselage, an accumulation of atmospheric electricity is created. As a result of this process, a potential difference arises between the capacitor disks located on the upper and lower needles. When the spark gap is broken, caused by an increase in the voltage on the capacitor, under the influence of atmospheric electricity, an alternating current arises in the self-inductance coil 15, associated with the current in the inductor 12, electricity flows through the rectifier 16 into the high-capacity capacitor 13, and from it to the battery 14 and 29.

The surface of the heated ball activates the ionization of the air around the aircraft, creating a zone of electrical breakdown of the air, increasing the efficiency of capturing and accumulating electrical energy from the atmosphere into the battery 14 and 29 (batteries). The accumulation of electrical energy from the atmosphere is carried out by the aircraft in a continuous mode (in flight).

E _z - the vertical component of the Earth is 200 V/m. Depending on the height of the aircraft's ascent into the atmosphere from the Earth's surface, the voltage in the capacitor and the charge of the batteries 14 and 29 increase.

The vertical increase in the distance between the receiver unit and the peripheral end of the antenna 35 increases the electricity storage efficiency of the power plant.

The controlled horizontal movement of the aircraft is carried out by turning on four jet motors 26 placed crosswise, in which the nozzles are directed away from the center of the wing and which can be directed downward by the nozzles. Controlling from the control panel (PU) 30 the sequence of turning on jet motors, the movement of the aircraft is carried out without turning horizontally in any direction, as well as upwards.

The control panel (CP), located in cockpit 7 in the fuselage, remotely monitors and controls the temperature and air density in the balloon, the position of the rudder, fender liner, the sequence of switching on and off jet motors and their position (horizontal or vertical), control of the operation of the power plant, in including behind the remote control unit 1 for altitude and flight speed, charging, aiming and operation of LU 34 in pulsed and continuous mode.

The disc-shaped wing, located parallel to the base of the fuselage, creates an increased stability of the movement of the aircraft in the airspace, the ability to plan.

A vertically located rudder capable of turning 360°, and wing flaps (raised and lowered relative to the main horizontal position of the entire wing), controlled from the PU of the aircraft, allow maneuvering during the flight.

The lightness of the aircraft, its streamlined configuration and spatial arrangement, adapted to gliding in air currents, has the feature of hovering for a long time at the point of the atmosphere necessary for the operation of the LA.

2. Voltage converter PN 33 received by LU 34 from power plant 28 (Fig. 1).

3. The LU differs from the previously known ones by the ability to work from a continuously renewable source of electricity obtained from atmospheric electricity by the power plant 28.

The LU is fixed to the fuselage and has a dielectric coating. The LL, using the saturation of the atmosphere with electric charges accumulated by the aircraft power plant, especially in the upper layers of the atmosphere, makes it possible to accelerate the charging of the LN and carry out work on the destruction or displacement of the asteroid's trajectory both in pulsed and continuous modes.

Charging, aiming at the asteroid and destructive (or shifting the trajectory of movement) impact on the asteroid is carried out through PU 30.

The device of the aircraft differs from the previously known ones in that the lower needle, insulated with a dielectric from the base of the fuselage, exits through the lower surface of the fuselage into the atmosphere and is connected through a switch to a folding antenna coated with a dielectric, the peripheral end of which is bare.

The aircraft has the following features.

For the movement of the aircraft, atmospheric electricity is used;

The aircraft is able to overcome gravity;

The aircraft does not need refueling and refueling with fuels and lubricants;

Aircraft in good condition do not sink;

The aircraft performs silent vertical takeoff and landing on land and sea (water basin);

The aircraft is capable of hovering at a given point in the atmosphere for a long time;

The aircraft is capable of long silent flight, including round-the-world flight (around the globe);

LA is environmentally friendly;

The aircraft is capable of carrying out accelerated charging of the LU and carrying out work to destroy or shift the trajectory of the asteroid in both pulsed and continuous modes.

Aircraft for the destruction of asteroids by laser beam action using atmospheric electricity can also be used to destroy other space objects threatening the Earth and aircraft;

The aircraft is able to overcome gravity and enter the stratosphere and space, to carry out control

Claims (1)

CLAIM Aircraft for destroying asteroids by laser beam action using atmospheric electricity contains a ball made of a durable elastic, heat-resistant material with a metallized coating on the outside, filled with air, having an air heater inside, on the outside - a compressor for supplying air to the ball and an air discharge valve from the ball , coupled with a fuselage made of metal coated with a material with high electrical conductivity, in the form of a cone truncated from above with a base in the form of a disk, inside the fuselage there is a hemispherical recess, a wing made of metal in the form of a disk, which includes four wing liners located parallel to the base under the fuselage and attached to it by four metal supports, a rudder located vertically in the center between the fuselage base and the wing, four wing liner control rods, four rocket motors located crosswise under the lower surface of the wing with nozzles outward from the center, and four re support legs, control panel in the fuselage cockpit, power plant consists of a receiving unit in the form of a fuselage, from which a needle coated with a dielectric is lowered from its surface, the end of which is connected to the upper disk of the capacitor, which is enclosed in a chamber of dielectric, a needle comes from the base , covered with a dielectric, on top of which the lower disk of the capacitor is fixed, an air network is connected to the upper needle, on the upper branch of which there is a spark gap, the second electrode of which is connected to an inductance coil, which is connected to the lower needle, the second self-inductance coil is connected to a rectifier connected to a high-capacity capacitor connected to batteries charged from the mains and from atmospheric electricity, the capacitor is enclosed in a dielectric chamber and has a spark gap, a double switch is introduced on the upper and lower needles to protect the battery from overcharging, a battery charge indicator is connected to it battery and laser device, remote control box connected to the double switch on the upper and lower needle, battery and laser device charge indicator, insulating power plant, metal casing coated with dielectric, voltage converter connected to the battery and laser device coated with dielectric, attached to the fuselage , the lower needle, covered with a dielectric, exits through the lower surface of the fuselage into the atmosphere, differs in that the lower needle is connected through a switch to a folding antenna coated with a dielectric, the peripheral end of which is bare.