EA034178B1 - Aircraft using atmospheric electricity - Google Patents

Abstract

The aircraft using atmospheric electricity is proposed, characterized in that it consists of a ball made of durable elastic heat-resistant material with metalized spraying outside, filled with air, having an air heater inside, fuselage of metal in the form of truncated cone accommodating a cockpit with control panel, wing in the form of disk, including four underwing flaps, rudder vertically positioned in the center between the fuselage and the wing, under which there are four electric jet motors arranged crosswise with their nozzles looking outwards; power station is located in the fuselage, which is its receiving unit; dielectric-coated needle drops from its surface, a needle's end connected to the upper disk of capacitor which is enclosed in a dielectric chamber and has a spark gap; a dielectric-coated needle passes from the base, on top of which the lower capacitor disk is fixed, air mesh is attached to the upper needle, on which upper branch there is a spark gap, its second electrode is connected to an inductance coil connected to the lower needle, the second self-inductance coil is connected to a rectifier connected to a large capacitor, connected to batteries charged from the mains and from the atmospheric electricity, remote control unit connected to a double switch on the upper and lower needle, a battery charge indicator connected to the battery, dielectric-coated metal casing insulating the power station, the lower needle insulated from the fuselage base by dielectric passes through the underside of the fuselage into the atmosphere.

Description

The invention relates to aircraft used in aviation.

It is known that aircraft using atmospheric electricity do not currently exist.

Known inventions for the use of atmospheric electricity No. 2332816, 2000128, 2369991, 2482640, 2030132, 25712237.

A new previously unknown technical solution is introduced - an aircraft using atmospheric electricity, which differs from previously known by the following qualities:

1) atmospheric electricity is used to move the aircraft;

2) the aircraft does not need refueling and refueling with fuels and lubricants;

3) aircraft in good condition unsinkable;

4) the aircraft performs silently vertical take-off and landing on land and sea (water basin);

5) An aircraft is capable of abruptly reversing the direction of its movement in the atmosphere without a turn;

6) aircraft is able to hang in the atmosphere for a long time;

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

The aircraft LA differs from previously known aircraft in that it consists of a ball 18 made of durable, flexible, heat-resistant material with a metallized spraying on the outside, filled with air, having an air heater 19 operating on a battery inside, and an air supply compressor 31 and an air vent valve from the ball 32. The ball is tightly coupled to the fuselage 2 having the shape of a truncated cone on top with a base in the form of a metal disk 20.

Inside the fuselage is a hemispherical metal recess. The metal wing 21 is made in the form of a disk including four wing flaps 22 located parallel to the base under the fuselage and four metal supports 23 attached to it. Wheel 24 located vertically in the center between the fuselage base and the wing, four wing control rods 25, under the lower surface of the wing - four rocket motors 26 located crosswise nozzles outward from the center and four support legs 27. In the fuselage is a cabin 7, isolated from it by a coating of m Therians having thermal protection from exposure to elevated temperature and reduced ball from the atmospheric air 31. In the cab is a control panel (PU) LA 30 (FIG. 2, FIG. 3).

An electric station 28 (Fig. 1), which consists of a receiving unit in the form of a fuselage and from it, a dielectric needle 10 is lowered from its surface, the end of which is connected to the upper capacitor disk, which is enclosed in a dielectric chamber 17, from the base 8 there is a needle 9 covered with a dielectric, on the top of which the lower capacitor disk 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 inductor 12, which is connected to the lower needle 9, the second self-inductance 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 has been introduced, connected to a double switch and an indicator of battery charge, for example, a voltmeter. Protection of the power plant, which is located in the aircraft, from external influences, operation safety is carried out by an insulating all-metal casing covered with a dielectric 6, 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.

Power station 28, located inside the fuselage to protect against external influences and influences, is completely insulated by a metal casing coated with a dielectric 6.

LA works as follows.

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

In flight of an aircraft in the atmosphere due to the triboelectrification 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 a spark gap breaks through due to an increase in the voltage across the capacitor under the influence of atmospheric electricity, an alternating current arises in the self-induction coil 15, which is connected with the current in the inductor 12, the electricity is supplied through the rectifier 16 to the large capacitor 13, and from it to the battery 14 and 29.

- 1 034178

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

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

The controlled horizontal movement of the aircraft is carried out by turning on four cross-reactive electric motors 26, in which the nozzles are directed away from the center of the wing and which can be directed downward by the nozzles. When controlling from the control panel of the reactive electric motors from the control panel (PU) 30, the aircraft moves without turning horizontally in any direction and also up.

The control panel (PU), located in the cockpit 7 in the fuselage, remotely monitors and controls the temperature and air density in the ball, the position of the steering wheel, the wing liner, the sequence of turning on and off the jet motors and their position (horizontal or vertical), monitoring the operation of the power plant, in including behind the remote control unit 1 altitude and speed.

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

A vertically positioned steering wheel that can rotate 360 °, and wing flaps (raised and lowered relative to the main - horizontal - the 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 for planning in air currents, the presence of a constantly renewable source of electricity from an atmosphere saturated with electric charges create the basis for long-term controlled (from launchers in the fuselage cabin) non-stop flight in the atmosphere.

Claims (1)

CLAIM An aircraft using atmospheric electricity is characterized in that it consists of a ball made of a durable, flexible, heat-resistant material with a metallic spraying on the outside, filled with air, having an air heater inside, an outside compressor for supplying air to the ball and an air vent valve from the ball, interlocked with the fuselage in the form of a cone truncated from above with a base in the form of a disk of metal, inside the fuselage a hemispherical recess of metal, a metal wing in the form of a disk, including four fenders, parallel to the base under the fuselage and attached to it by four metal supports, a steering wheel located vertically in the center between the fuselage base and the wing, four traction controls for the fenders, four rocket motors located crosswise under the lower surface of the wing with nozzles outward from the center and four supporting legs, a control panel in the fuselage cockpit, an electric station consisting of a receiving unit in the form of the fuselage and from it, the a dielectric-coated cable, the end of which is connected to the upper capacitor disk, which is enclosed in a dielectric chamber, a dielectric-coated needle goes from the base, on the top of which a lower capacitor disk is fixed, an air network is attached to the upper needle, on the upper branch of which there is a spark gap the second electrode of which is connected to an inductor that is connected to the lower needle, the second self-inductance coil is connected to a rectifier connected to a large capacitor connected to the battery with a battery (initially charged from the mains, then from atmospheric electricity), the capacitor is enclosed in a dielectric chamber and has a spark gap, a double switch is inserted on the upper and lower needles to protect the battery from overcharging, the battery contamination indicator is connected to it (battery), for A remote control unit is connected to the station’s remote control, connected to a double switch and a battery charge indicator, for example, a voltmeter, protection of a power plant is located in the aircraft, from external influences, operation safety is ensured by an insulating all-metal casing covered with a dielectric, and a lower needle insulated by a dielectric from the base of the fuselage exits through the lower surface of the fuselage into the atmosphere, an electric station located inside the fuselage to protect it from external influences and influences are completely insulated by a metal casing coated with a dielectric.