EA038395B1

EA038395B1 - Helicopter with electric motor using atmospheric electricity "ruselectro17"

Info

Publication number: EA038395B1
Application number: EA201800448A
Authority: EA
Inventors: Борис Иванович Блескин; Константин Егорович Иванов; Екатерина Юрьевна Чуракова
Original assignee: Борис Иванович Блескин
Priority date: 2018-08-28
Filing date: 2018-08-28
Publication date: 2021-08-20
Also published as: EA201800448A1

Abstract

The invention relates to electrical engineering, in particular to devices for atmospheric electricity use. A helicopter distinguished by having an electric motor, a voltage converter, an aerial device for atmospheric electricity use located in the helicopter that contains a receiving unit shaped as a helicopter fuselage with a fixed needle connected with the upper disk of the condenser; the device base features a needle connected by its tip with the lower disk of the condenser; a network having a spark detector on its upper branch is connected to the needles, the second electrode of this detector is connected with an induction coil which is connected with the lower needle, and the second self-induction coil is connected with a rectifier which is connected with a condenser of a bigger capacity attached to the battery; a dielectric chamber, in which a capacitor with upper and lower discs is placed, equipped with a spark arrester, with the upper and lower needles coated with dielectric, a remote control unit connected to a double switch on the upper and lower needle and an indicator of battery charge, connected to the battery, a metal protective casing covered with dielectric, its receiving unit being the surface of the helicopter fuselage, and the lower needle, insulated with dielectric from the fuselage, exiting through the lower surface of the helicopter fuselage into the atmosphere. The device can be used as an additional electric motor in helicopters.

Description

Изобретение относится к электротехнике, а именно к устройствам для использования атмосферного электричества.The invention relates to electrical engineering, namely to devices for using atmospheric electricity.

Известны устройства для использования атмосферного электричества: патенты № 2332816,Known devices for using atmospheric electricity: patents No. 2332816,

2000128, 2369991, 2482640, 2030132, 25712237, евразийские патенты № 028414, 029621.2000128, 2369991, 2482640, 2030132, 25712237, Eurasian patents No. 028414, 029621.

Данные технические решения рассчитаны на аккумуляцию атмосферного электричества в условиях Земли, моря и в воздушном пространстве.These technical solutions are designed for the accumulation of atmospheric electricity in the conditions of the Earth, sea and airspace.

Недостатком таких устройств является отсутствие возможности использовать аккумулирование атмосферного электричества из воздушного пространства в вертолетах с применением электродвигателей.The disadvantage of such devices is the inability to use the accumulation of atmospheric electricity from the air in helicopters using electric motors.

Предлагается новое, неизвестное ранее техническое решение - вертолет с электродвигателем, использующим аэроустройство для аккумуляции атмосферного электричества из воздушного пространства (атмосферы) с сохранением при полете его баллистики.A new, previously unknown technical solution is proposed - a helicopter with an electric motor using an aero device to accumulate atmospheric electricity from the airspace (atmosphere) while maintaining its ballistics during flight.

Предлагаемое нами техническое решение отличается от известных ранее тем, что состоит из электродвигателя 19, преобразователя напряжения 18, аэроустройство для использования атмосферного электричества, находящегося в фюзеляже вертолета, и содержит приемный блок трибоэлемент 2 в виде фюзеляжа вертолета и от него опускается игла 10, покрытая диэлектриком, конец которой соединен с верхним диском конденсатора, который заключен в камеру из диэлектрика 17, от основания 8 идет игла 9, покрытая диэлектриком, на вершине которой закреплен нижний диск конденсатора. К верхней игле присоединена воздушная сеть, на верхней ветке которой размещен искровой разрядник 11, второй электрод которого соединен с катушкой индуктивности 12, которая соединена с нижней иглой 9, вторая катушка самоиндуктивности 15 соединена с выпрямителем 16, соединенным с конденсатором большой емкости 13, соединенным с аккумулятором 14. Конденсатор заключен в камеру из диэлектрика и имеет искровой разрядник 3. Для защиты аккумулятора от избыточной перезарядки на верхней и нижней игле введен двойной выключатель 5, индикатор заряженности аккумулятора 4 соединен с ним (аккумулятором). Для дистанционного управления устройством введен блок дистанционного управления 1, соединенный с двойным выключателем и индикатором заряженности аккумулятора, например вольтметр. Защиту устройства от внешних воздействий, безопасность эксплуатации осуществляет металлический кожух, покрытый диэлектриком 6, устройство располагается в вертолете, при этом приемным блоком 2 является поверхность фюзеляжа, а нижняя игла, изолированная диэлектриком от фюзеляжа ,7 выходит через нижнюю поверхность фюзеляжа в атмосферу.The technical solution proposed by us differs from the previously known ones in that it consists of an electric motor 19, a voltage converter 18, an aero device for using atmospheric electricity located in the fuselage of a helicopter, and contains a receiving unit triboelement 2 in the form of a helicopter fuselage and a needle 10, covered with a dielectric, is lowered from it , the end of which is connected to the upper disc of the capacitor, which is enclosed in a chamber made of dielectric 17, from the base 8 there is a needle 9 covered with a dielectric, at the top of which the lower disc 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. 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 (the battery). For remote control of the device, a remote control unit 1 is introduced, connected to a double switch and a battery charge indicator, for example, a voltmeter. The device is protected from external influences, operational safety is provided by a metal casing covered with a dielectric 6, the device is located in a helicopter, while the receiving unit 2 is the fuselage surface, and the lower needle, insulated with a dielectric from the fuselage, 7 exits through the lower surface of the fuselage into the atmosphere.

Устройство работает следующим образом.The device works as follows.

Вертолет при полете в атмосфере за счет трибоэлектрилизации фюзеляжа создает аккумулирование атмосферного электричества. В результате этого процесса возникает разница потенциалов между дисками конденсатора, находящимися на верхней и нижней иглах. При пробитии искрового промежутка, вызванного ростом напряжения на конденсаторе под влиянием атмосферного электричества, возникает переменный ток в катушке самоиндукции, связанное с током в катушке индуктивности электричество поступает через выпрямитель в конденсатор большой емкости, а с него в аккумулятор и через преобразователь напряжения в электродвигатель.The helicopter, when flying in the atmosphere, due to triboelectricization of the fuselage creates an accumulation of atmospheric electricity. As a result of this process, a potential difference arises between the capacitor discs located on the upper and lower needles. When a spark gap is broken through, caused by an increase in the voltage across the capacitor under the influence of atmospheric electricity, an alternating current arises in the self-induction coil, electricity associated with the current in the inductor coil flows through the rectifier into the large-capacity capacitor, and from it into the battery and through the voltage converter into the electric motor.

Предлагаемое техническое решение - вертолет с электродвигателем, использующим атмосферное электричество, является основой создания нового неизвестного ранее типа вертолетов, имеющих дополнительный электродвигатель.The proposed technical solution - a helicopter with an electric motor using atmospheric electricity, is the basis for the creation of a new previously unknown type of helicopters with an additional electric motor.

Claims

CLAIM

Helicopter, which includes an aero device for using atmospheric electricity, located in the helicopter, containing a receiving unit made in the form of a helicopter fuselage and a needle connected to the upper disk of the condenser is fixed on it, a needle is fixed on the base of the device, connected by its top to the lower disk of the condenser , 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-capacity capacitor connected to a battery, a dielectric chamber, which contains a capacitor with upper and lower disks, equipped with a spark gap, while the upper and lower needles are made with a dielectric coating, a remote control unit connected to a double switch on the upper and lower needles and a battery charge indicator connected to the battery, a metal protective casing covered with a dielectric, the receiving unit is the surface of the fuselage, the lower needle, insulated with a dielectric from the fuselage, exits through the lower surface of the helicopter fuselage into the atmosphere, characterized in that it includes an electric motor and a voltage converter connected to the battery.