EA201700179A1 - AIRCRAFT USING ATMOSPHERIC ELECTRICITY - Google Patents
AIRCRAFT USING ATMOSPHERIC ELECTRICITYInfo
- Publication number
- EA201700179A1 EA201700179A1 EA201700179A EA201700179A EA201700179A1 EA 201700179 A1 EA201700179 A1 EA 201700179A1 EA 201700179 A EA201700179 A EA 201700179A EA 201700179 A EA201700179 A EA 201700179A EA 201700179 A1 EA201700179 A1 EA 201700179A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- fuselage
- dielectric
- needle
- covered
- disk
- Prior art date
Links
- 230000005611 electricity Effects 0.000 title abstract 3
- 239000003990 capacitor Substances 0.000 abstract 3
- 239000002184 metal Substances 0.000 abstract 2
- 101100114828 Drosophila melanogaster Orai gene Proteins 0.000 abstract 1
- 229910001254 electrum Inorganic materials 0.000 abstract 1
- 239000003779 heat-resistant material Substances 0.000 abstract 1
- 238000005507 spraying Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05F—STATIC ELECTRICITY; NATURALLY-OCCURRING ELECTRICITY
- H05F7/00—Use of naturally-occurring electricity, e.g. lightning or static electricity
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Direct Current Feeding And Distribution (AREA)
- Catching Or Destruction (AREA)
Abstract
Летательный аппарат с использованием атмосферного электричества, отличающийся тем, что состоит из шара, изготовленного из прочного эластичного, устойчивого к нагреванию материала с металлизированным напылением снаружи, наполненного воздухом, имеет внутри нагреватель воздуха, фюзеляж из металла в виде усеченного конуса и кабину с пультом управления, крыло в виде диска, включающее четыре подкрылка, в центре руль, расположенный вертикально между фюзеляжем и крылом, под которым имеются крестообразно соплами кнаружи четыре реактивных электродвигателя, электрическая станция расположена в фюзеляже, который является ее приемным блоком, с его поверхности опускается игла, покрытая диэлектриком, конец которой соединен с верхним диском конденсатора, который заключен в камеру из диэлектрика и имеет искровой разрядник, от основания идет игла, покрытая диэлектриком, на вершине которой закреплен нижний диск конденсатора, к верхней игле присоединена воздушная сеть, на верхней ветке которой размещен искровой разрядник, второй электрод которого соединен с катушкой индуктивности, которая соединена с нижней иглой, вторая катушка самоиндуктивности соединена с выпрямителем, соединенным с конденсатором большой емкости, соединенным с аккумуляторами, заряжаемыми от электросети и от атмосферного электричества, блок дистанционного управления, соединенный с двойным выключателем на верхней и нижней игле, индикатором заряженности аккумулятора, соединенным с аккумулятором, изолирующий электростанцию металлический кожух, покрытый диэлектриком, причем нижняя игла, изолированная диэлектриком от основания фюзеляжа, выходит через нижнюю поверхность фюзеляжа в атмосферу.Aircraft using atmospheric electricity, characterized in that it consists of a ball made of durable elastic, heat resistant material with metallized spraying on the outside, filled with air, has an air heater inside, a fuselage made of metal in the form of a truncated cone and a cockpit with a control panel, a wing in the form of a disk, including four flaps, in the center of the steering wheel, located vertically between the fuselage and the wing, under which there are four jet electrums with cross-shaped nozzles outwardly The power unit is located in the fuselage, which is its receiving unit, a needle covered with a dielectric drops from its surface, the end of which is connected to the upper capacitor disk, which is enclosed in a dielectric chamber and has a spark gap, the needle covered with a dielectric goes from the base, on the top of which the lower capacitor disk is fixed, an air network is attached to the upper needle, on the upper branch of which a spark gap is placed, the second electrode of which is connected to an inductance coil, The orai 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, a remote control unit connected to a double switch on the upper and lower needle, a battery charge indicator connected with a battery, a metal casing insulating a power plant, covered with a dielectric, the lower needle insulated by a dielectric from the base of the fuselage coming out Erez lower fuselage surface to the atmosphere.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EA201700179A EA034178B1 (en) | 2017-05-03 | 2017-05-03 | Aircraft using atmospheric electricity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EA201700179A EA034178B1 (en) | 2017-05-03 | 2017-05-03 | Aircraft using atmospheric electricity |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EA201700179A1 true EA201700179A1 (en) | 2018-11-30 |
| EA034178B1 EA034178B1 (en) | 2020-01-15 |
Family
ID=64453208
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EA201700179A EA034178B1 (en) | 2017-05-03 | 2017-05-03 | Aircraft using atmospheric electricity |
Country Status (1)
| Country | Link |
|---|---|
| EA (1) | EA034178B1 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6565037B1 (en) * | 2002-06-04 | 2003-05-20 | Tonkovich Gregory P | Hybrid aircraft and methods of flying |
| RU2333134C2 (en) * | 2006-10-24 | 2008-09-10 | Российская Академия сельскохозяйственных наук Государственное научное учреждение Всероссийский научно-исследовательский институт электрификации сельского хозяйства (ГНУ ВИЭСХ РОССЕЛЬХОЗАКАДЕМИИ) | Multi-purpose balloon |
| RU2555461C1 (en) * | 2014-03-03 | 2015-07-10 | Михаил Григорьевич Карпухин | Steam-lifted airship and complex electric power station as automatic high-altitude flying versatile station |
-
2017
- 2017-05-03 EA EA201700179A patent/EA034178B1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EA034178B1 (en) | 2020-01-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ KZ KG TJ TM RU |
|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): BY |