RU2009134290A - PLASMA-REACTIVE ENGINE - Google Patents

PLASMA-REACTIVE ENGINE Download PDF

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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
Application number
RU2009134290/06A
Other languages
Russian (ru)
Inventor
Михаил Алексеевич Игнатов (RU)
Михаил Алексеевич Игнатов
Original Assignee
Михаил Алексеевич Игнатов (RU)
Михаил Алексеевич Игнатов
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 Михаил Алексеевич Игнатов (RU), Михаил Алексеевич Игнатов filed Critical Михаил Алексеевич Игнатов (RU)
Priority to RU2009134290/06A priority Critical patent/RU2009134290A/en
Publication of RU2009134290A publication Critical patent/RU2009134290A/en
Priority to PCT/RU2010/000501 priority patent/WO2011034466A2/en

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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)

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.
RU2009134290/06A 2009-09-15 2009-09-15 PLASMA-REACTIVE ENGINE RU2009134290A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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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