EA201800448A1 - HELICOPTER WITH ELECTRIC MOTOR USING ATMOSPHERIC ELECTRICITY "RUSELECTRO17" - Google Patents
HELICOPTER WITH ELECTRIC MOTOR USING ATMOSPHERIC ELECTRICITY "RUSELECTRO17"Info
- Publication number
- EA201800448A1 EA201800448A1 EA201800448A EA201800448A EA201800448A1 EA 201800448 A1 EA201800448 A1 EA 201800448A1 EA 201800448 A EA201800448 A EA 201800448A EA 201800448 A EA201800448 A EA 201800448A EA 201800448 A1 EA201800448 A1 EA 201800448A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- helicopter
- dielectric
- capacitor
- needle
- electric motor
- Prior art date
Links
- 230000005611 electricity Effects 0.000 title abstract 3
- 239000003990 capacitor Substances 0.000 abstract 4
- 238000004870 electrical engineering Methods 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 230000001681 protective effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
Изобретение относится к электротехнике, а именно к устройствам для использования атмосферного электричества. Вертолет отличается тем, что в его состав входит электродвигатель, преобразователь напряжения, расположенное в вертолете аэроустройство для использования атмосферного электричества, содержащее приемный блок, выполненный в виде фюзеляжа вертолета и на нем закреплена игла, соединённая с верхним диском конденсатора, на основании устройства закреплена игла, соединенная своей вершиной с нижним диском конденсатора, к иглам присоединена сеть, имеющая на верхней ветви искровой разрядник, второй электрод которого соединен с катушкой индуктивности, которая соединена с нижней иглой, а вторая катушка самоиндукции соединена с выпрямителем, который соединен с конденсатором большой емкости, соединенным с аккумулятором, камера из диэлектрика, в которой размещен конденсатор с верхним и нижним дисками, снабженный искровым разрядником, при этом верхняя и нижняя иглы выполнены с покрытием из диэлектрика, блок дистанционного управления, соединенный с двойным выключателем на верхней и нижней игле и индикатором заряженности аккумулятора, соединенным с аккумулятором, металлический защитный кожух, покрытый диэлектриком, приемным блоком является поверхность фюзеляжа вертолета, а нижняя игла, изолированная диэлектриком от фюзеляжа, выходит через нижнюю поверхность фюзеляжа вертолета в атмосферу. Устройство можно использовать в качестве дополнительного электродвигателя в вертолетах.The invention relates to electrical engineering, namely to devices for using atmospheric electricity. The helicopter differs in that it includes an electric motor, a voltage converter, an aero device located in the helicopter for using atmospheric electricity, containing a receiving unit made in the form of a helicopter fuselage and a needle connected to the upper disk of the capacitor is fixed on it, a needle is fixed on the base of the device, connected by its top to the lower disk of the capacitor, a network is connected to the needles, which has a spark gap on the upper branch, the second electrode of which is connected to an inductance coil, which is connected to the lower needle, and the second self-induction coil is connected to a rectifier, which is connected to a large capacitor connected with a battery, a dielectric chamber in which a capacitor with upper and lower disks is located, equipped with a spark gap, while the upper and lower needles are coated with a dielectric, a remote control unit connected to a double switch on the upper and lower needles and an indicator With the battery charge connected to the battery, a metal protective casing covered with a dielectric, the receiving unit is the surface of the helicopter fuselage, and the lower needle, insulated with a dielectric from the fuselage, exits through the lower surface of the helicopter fuselage into the atmosphere. The device can be used as an additional electric motor in helicopters.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EA201800448A EA038395B1 (en) | 2018-08-28 | 2018-08-28 | Helicopter with electric motor using atmospheric electricity "ruselectro17" |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EA201800448A EA038395B1 (en) | 2018-08-28 | 2018-08-28 | Helicopter with electric motor using atmospheric electricity "ruselectro17" |
Publications (2)
Publication Number | Publication Date |
---|---|
EA201800448A1 true EA201800448A1 (en) | 2020-03-31 |
EA038395B1 EA038395B1 (en) | 2021-08-20 |
Family
ID=69942781
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EA201800448A EA038395B1 (en) | 2018-08-28 | 2018-08-28 | Helicopter with electric motor using atmospheric electricity "ruselectro17" |
Country Status (1)
Country | Link |
---|---|
EA (1) | EA038395B1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008014404B4 (en) * | 2008-03-14 | 2011-03-03 | Swiss Uav Gmbh | Unmanned aerial vehicle |
RU2482640C2 (en) * | 2011-02-11 | 2013-05-20 | Борис Иванович Блёскин | Device for usage of atmospheric electricity "ruselectro" |
RU2571237C2 (en) * | 2014-01-22 | 2015-12-20 | Борис Иванович Блескин | Ruselectro 2 device for atmospheric electricity usage |
EA029621B1 (en) * | 2015-06-29 | 2018-04-30 | Борис Иванович Блескин | Airplane with an aero-device for atmospheric electricity utilization |
-
2018
- 2018-08-28 EA EA201800448A patent/EA038395B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EA038395B1 (en) | 2021-08-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2011105234A (en) | DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO" | |
EA201500585A1 (en) | AERO DEVELOPMENT FOR THE USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 4" | |
EA201800448A1 (en) | HELICOPTER WITH ELECTRIC MOTOR USING ATMOSPHERIC ELECTRICITY "RUSELECTRO17" | |
RU2014101919A (en) | DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 2" | |
EA201800433A1 (en) | REACTIVE AIRCRAFT WITH A REACTIVE ELECTRIC MOTOR USING ATMOSPHERIC ELECTRICITY "RUSELECTRO 16" | |
EA201700150A3 (en) | AERO DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 1" | |
RU2663237C2 (en) | Aerial device for the atmospheric electricity usage | |
US2459856A (en) | Transformer spark plug | |
EA040590B1 (en) | JET AIRCRAFT WITH AN ADDITIONAL REACTIVE ELECTRIC MOTOR AND A BATTLE LASER DEVICE USING ATMOSPHERIC ELECTRICITY (JET AIRCRAFT BLESKIN-CHURAKOVOY "BECH") | |
EA201500548A1 (en) | MARINE DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 3" | |
EA201800161A3 (en) | WATER PURIFICATION STATION BY OZONIZATION METHOD USING ATMOSPHERIC ELECTRICITY | |
EA201800017A1 (en) | ELECTRIC MOTOR USING ATMOSPHERIC ELECTRICITY | |
EA201900531A1 (en) | AIRCRAFT FOR DESTRUCTION OF ASTEROIDS USING ATMOSPHERIC ELECTRICITY | |
RU2012101923A (en) | METHOD FOR TRANSMISSION OF INFORMATION ON ELECTROMAGNETIC COMMUNICATION CHANNEL WHEN OPERATING A WELL AND A DEVICE FOR ITS IMPLEMENTATION | |
EA201700179A1 (en) | AIRCRAFT USING ATMOSPHERIC ELECTRICITY | |
EA201800063A1 (en) | ELECTRIC STATION USING ATMOSPHERIC ELECTRICITY | |
GB1028593A (en) | Electrical apparatus | |
EA201800039A1 (en) | SEA WATER DESCRIPTION STATION USING ATMOSPHERIC ELECTRICITY | |
EA034107B1 (en) | Underwater vessel with aerial device to use atmospheric electricity and energy of triboelectrification of hull surface (ruselectro 12) | |
RU144894U1 (en) | CAPACITIVE IGNITION SYSTEM | |
RU2013145932A (en) | DUPLEX SHOCK EXCITER | |
RU2544845C2 (en) | High-current nanosecond electron beam accelerator | |
RU115564U1 (en) | POWER HIGH VOLTAGE SEMICONDUCTOR PIN PIN DEVICE | |
SU843186A1 (en) | Device for burning-through defective insulation of electric cables | |
SU150135A1 (en) | Rectangular high voltage pulse generator |
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 |