RU2009134290A - PLASMA-REACTIVE ENGINE - Google Patents
PLASMA-REACTIVE ENGINE Download PDFInfo
- Publication number
- RU2009134290A RU2009134290A RU2009134290/06A RU2009134290A RU2009134290A RU 2009134290 A RU2009134290 A RU 2009134290A RU 2009134290/06 A RU2009134290/06 A RU 2009134290/06A RU 2009134290 A RU2009134290 A RU 2009134290A RU 2009134290 A RU2009134290 A RU 2009134290A
- Authority
- RU
- Russia
- Prior art keywords
- plasma
- creates
- magnetic field
- constant
- electromagnet
- 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
- F03H1/0081—Electromagnetic plasma thrusters
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
Устройство для создания реактивной тяги, именуемое «Плазменно-реактивный двигатель», содержит два основных компонента - один из которых создает постоянное магнитное поле и может быть выполнен как постоянный либо электромагнит, а второй создает вращающееся магнитное поле, и может быть выполнен, например, как кольцевой магнитопровод с многофазной обмоткой, или как статор асинхронного двигателя; а также один вспомогательный компонент - приспособление для предварительной ионизации газа.A device for creating reactive thrust, referred to as a "Plasma-jet engine", contains two main components - one of which creates a constant magnetic field and can be performed either as a constant or an electromagnet, and the second creates a rotating magnetic field, and can be performed, for example, as ring magnetic core with multiphase winding, or as a stator of an induction motor; and also one auxiliary component - a device for preliminary ionization of gas.
Claims (1)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009134290/06A RU2009134290A (en) | 2009-09-15 | 2009-09-15 | PLASMA-REACTIVE ENGINE |
| PCT/RU2010/000501 WO2011034466A2 (en) | 2009-09-15 | 2010-09-13 | Plasma jet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2009134290/06A RU2009134290A (en) | 2009-09-15 | 2009-09-15 | PLASMA-REACTIVE ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2009134290A true RU2009134290A (en) | 2010-03-27 |
Family
ID=42138165
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2009134290/06A RU2009134290A (en) | 2009-09-15 | 2009-09-15 | PLASMA-REACTIVE ENGINE |
Country Status (2)
| Country | Link |
|---|---|
| RU (1) | RU2009134290A (en) |
| WO (1) | WO2011034466A2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012021537A1 (en) * | 2010-08-09 | 2012-02-16 | Msnw Llc | Apparatus, systems and methods for establishing plasma and using plasma in a rotating magnetic field |
-
2009
- 2009-09-15 RU RU2009134290/06A patent/RU2009134290A/en unknown
-
2010
- 2010-09-13 WO PCT/RU2010/000501 patent/WO2011034466A2/en not_active Ceased
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012021537A1 (en) * | 2010-08-09 | 2012-02-16 | Msnw Llc | Apparatus, systems and methods for establishing plasma and using plasma in a rotating magnetic field |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011034466A2 (en) | 2011-03-24 |
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