RU2015101458A - A method of supplying a working fluid to a pulsed plasma electric jet engine and a device for its implementation - Google Patents
A method of supplying a working fluid to a pulsed plasma electric jet engine and a device for its implementation Download PDFInfo
- Publication number
- RU2015101458A RU2015101458A RU2015101458A RU2015101458A RU2015101458A RU 2015101458 A RU2015101458 A RU 2015101458A RU 2015101458 A RU2015101458 A RU 2015101458A RU 2015101458 A RU2015101458 A RU 2015101458A RU 2015101458 A RU2015101458 A RU 2015101458A
- Authority
- RU
- Russia
- Prior art keywords
- working fluid
- storage tank
- wick
- discharge gap
- supplying
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
Landscapes
- Jet Pumps And Other Pumps (AREA)
- Special Spraying Apparatus (AREA)
Abstract
1. Способ подачи жидкого рабочего тела в импульсный плазменный электрический реактивный двигатель, заключающийся в отборе рабочего тела из бака хранения, смачивании подвижной поверхности разрядного промежутка путем контакта капиллярного фитиля, смоченного рабочим телом, указанной поверхности, отличающийся тем, что рабочее тело подают к фитилю под давлением, а избыток рабочего тела с подвижной поверхности снимают другим фитилем, с последующим отсосом в бак хранения рабочего тела, при этом разрядный промежуток располагают между зоной подачи и отсоса излишков рабочего тела.2. Устройство подачи жидкого рабочего тела в импульсный плазменный электрический реактивный двигатель, состоящее из бака хранения, трубопровода подачи рабочего тела к капиллярному фитилю, контактирующему с подвижной поверхностью разрядного промежутка, выполненной из диэлектрика, отличающееся тем, что в трубопроводе подачи дополнительно установлен насос, а после разрядного промежутка с подвижной поверхностью контактирует фитиль, сообщенный с трубопроводом отсоса рабочего тела, снабженного насосом и соединенного с баком хранения рабочего тела.3. Устройство по п. 2, отличающееся тем, что подвижная поверхность и насос имеют общий или синхронизированные между собой электроприводы.1. The method of supplying a liquid working fluid to a pulsed plasma electric jet engine, which consists in selecting the working fluid from the storage tank, wetting the movable surface of the discharge gap by contacting the capillary wick moistened with the working fluid, the specified surface, characterized in that the working fluid is fed to the wick under pressure, and the excess working fluid from the moving surface is removed with another wick, followed by suction into the storage tank of the working fluid, while the discharge gap is located between the giving and suction of surplus working fluid. 2. A device for supplying a liquid working fluid to a pulsed plasma electric jet engine, consisting of a storage tank, a supply pipe of the working fluid to a capillary wick in contact with the moving surface of the discharge gap made of a dielectric, characterized in that the pump is additionally installed in the supply pipe, and after the discharge gap between the moving surface is in contact with the wick in communication with the suction pipe of the working fluid, equipped with a pump and connected to the storage tank of the working th tela.3. The device according to claim 2, characterized in that the movable surface and the pump have common or synchronized electric drives.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2015101458A RU2615306C2 (en) | 2015-01-19 | 2015-01-19 | Method of supplying working medium to plasma electric jet engine and device for its implementation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2015101458A RU2615306C2 (en) | 2015-01-19 | 2015-01-19 | Method of supplying working medium to plasma electric jet engine and device for its implementation |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2015101458A true RU2015101458A (en) | 2016-08-10 |
RU2615306C2 RU2615306C2 (en) | 2017-04-04 |
Family
ID=56612622
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2015101458A RU2615306C2 (en) | 2015-01-19 | 2015-01-19 | Method of supplying working medium to plasma electric jet engine and device for its implementation |
Country Status (1)
Country | Link |
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RU (1) | RU2615306C2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2720602C2 (en) * | 2017-08-07 | 2020-05-12 | Акционерное общество "НАУЧНО-ИССЛЕДОВАТЕЛЬСКИЙ ИНСТИТУТ МАШИНОСТРОЕНИЯ" (АО "НИИМаш") | Pulsed plasma electric jet engine |
RU2757304C2 (en) * | 2019-11-19 | 2021-10-13 | Акционерное общество "НАУЧНО-ИССЛЕДОВАТЕЛЬСКИЙ ИНСТИТУТ МАШИНОСТРОЕНИЯ" (АО "НИИМаш") | Pulsed plasma coaxial rocket engine on a liquid working body |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3636709A (en) * | 1969-10-10 | 1972-01-25 | Aldo V La Rocca | Propellant device |
RU2146776C1 (en) * | 1998-05-14 | 2000-03-20 | Институт электрофизики Уральского отделения РАН | End-type impulse plasma-jet engine operating on solid propulsive mass |
AU3722400A (en) * | 1999-03-05 | 2000-10-16 | Gravitec, Inc. | Propulsion device and method employing electric fields for producing thrust |
RU2266428C2 (en) * | 2002-12-27 | 2005-12-20 | Государственное предприятие Научно-исследовательский институт машиностроения | Impulse plasma electric jet engine |
-
2015
- 2015-01-19 RU RU2015101458A patent/RU2615306C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
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RU2615306C2 (en) | 2017-04-04 |
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Legal Events
Date | Code | Title | Description |
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MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20200120 |