EA201700150A2 - AERO DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 1" - Google Patents

AERO DEVICE FOR USE OF ATMOSPHERIC ELECTRICITY "RUSELECTRO 1"

Info

Publication number
EA201700150A2
EA201700150A2 EA201700150A EA201700150A EA201700150A2 EA 201700150 A2 EA201700150 A2 EA 201700150A2 EA 201700150 A EA201700150 A EA 201700150A EA 201700150 A EA201700150 A EA 201700150A EA 201700150 A2 EA201700150 A2 EA 201700150A2
Authority
EA
Eurasian Patent Office
Prior art keywords
needle
dielectric
capacitor
fuselage
battery
Prior art date
Application number
EA201700150A
Other languages
Russian (ru)
Other versions
EA038604B1 (en
EA201700150A3 (en
Inventor
Борис Иванович Блескин
Константин Егорович Иванов
Татьяна Владимировна Моисеева
Екатерина Юрьевна Чуракова
Original Assignee
Борис Иванович Блескин
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Борис Иванович Блескин filed Critical Борис Иванович Блескин
Priority to EA201700150A priority Critical patent/EA038604B1/en
Publication of EA201700150A2 publication Critical patent/EA201700150A2/en
Publication of EA201700150A3 publication Critical patent/EA201700150A3/en
Publication of EA038604B1 publication Critical patent/EA038604B1/en

Links

Classifications

    • 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

  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
  • Measurement Of Resistance Or Impedance (AREA)

Abstract

Изобретение относится к электротехнике, а именно к устройствам для использования атмосферного электричества. Устройство для использования атмосферного электричества, содержащее приемный блок, выполненный в виде фюзеляжа самолета (2), на котором закреплена игла (10), соединенная с верхнем диском конденсатора, на основании (8) устройства закреплена игла (9), соединенная своей вершиной с нижним диском конденсатора, к иглам присоединена сеть, имеющая на верхней ветви искровой разрядник (11), второй электрод которого соединен с катушкой индуктивности (12), которая соединена с нижней иглой (9), а вторая катушка самоиндукции (15) соединена с выпрямителем (16), который соединен с конденсатором большой емкости (13), соединенным с аккумулятором (14) камеры из диэлектрика (17), в которой размещен конденсатор с верхним и нижним дисками, снабженный искровым разрядником (3), при этом верхняя и нижняя иглы выполнены с покрытием из диэлектрика, блок дистанционного управления (1) соединен с двойным выключателем (5) на верхней и нижней игле и индикатором заряженности аккумулятора (4), соединенным с аккумулятором, металлический защитный кожух покрыт диэлектриком (6), отличающееся тем, что устройство расположено в самолете, приемным блоком является фюзеляж самолета, а нижняя игла (7), изолированная диэлектриком от фюзеляжа, выходит через нижнюю поверхность фюзеляжа самолета. Устройство можно использовать для дополнительного электрообеспечения самолетов, космических кораблей, а также для других технических целей.The invention relates to electrical engineering, and in particular to devices for using atmospheric electricity. A device for using atmospheric electricity, comprising a receiving unit made in the form of an airplane fuselage (2), on which a needle (10) is fixed, connected to the upper capacitor disk, and on the base (8) of the device, a needle (9) is connected, connected by its apex to the lower a capacitor disk, a network is attached to the needles, having a spark gap (11) on the upper branch, the second electrode of which is connected to an inductance coil (12), which is connected to the lower needle (9), and the second self-induction coil (15) is connected to a rectifier (16 ) which The second one is connected to a large-capacity capacitor (13) connected to the battery (14) of the dielectric chamber (17), in which a capacitor with upper and lower disks is placed, equipped with a spark gap (3), while the upper and lower needles are made of dielectric, the remote control unit (1) is connected to a double switch (5) on the upper and lower needle and the battery charge indicator (4) connected to the battery, the metal protective cover is covered with a dielectric (6), characterized in that the device is located in an airplane , The receiving unit is the aircraft fuselage, and the lower needle (7), a dielectric isolated from the fuselage, exits through a bottom surface of the aircraft fuselage. The device can be used for additional power supply of aircraft, space ships, as well as for other technical purposes.

EA201700150A 2017-04-13 2017-04-13 Aircraft equipped with an aerial device for the utilization of atmospheric electricity EA038604B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EA201700150A EA038604B1 (en) 2017-04-13 2017-04-13 Aircraft equipped with an aerial device for the utilization of atmospheric electricity

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EA201700150A EA038604B1 (en) 2017-04-13 2017-04-13 Aircraft equipped with an aerial device for the utilization of atmospheric electricity

Publications (3)

Publication Number Publication Date
EA201700150A2 true EA201700150A2 (en) 2019-08-30
EA201700150A3 EA201700150A3 (en) 2019-11-29
EA038604B1 EA038604B1 (en) 2021-09-22

Family

ID=67734909

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201700150A EA038604B1 (en) 2017-04-13 2017-04-13 Aircraft equipped with an aerial device for the utilization of atmospheric electricity

Country Status (1)

Country Link
EA (1) EA038604B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1014719A (en) * 1911-01-04 1912-01-16 Walter I Pennock Apparatus for collecting electrical energy.
RU2482640C2 (en) * 2011-02-11 2013-05-20 Борис Иванович Блёскин Device for usage of atmospheric electricity "ruselectro"
RU2499372C1 (en) * 2012-03-30 2013-11-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Липецкий государственный технический университет (ЛГТУ) Device for static electricity take off
CN203537651U (en) * 2013-10-23 2014-04-09 国家电网公司 System achieving power supplying through thunder and lightning

Also Published As

Publication number Publication date
EA038604B1 (en) 2021-09-22
EA201700150A3 (en) 2019-11-29

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