EP1269803A2 - Plasma-beschleuniger-anordnung - Google Patents
Plasma-beschleuniger-anordnungInfo
- Publication number
- EP1269803A2 EP1269803A2 EP01933575A EP01933575A EP1269803A2 EP 1269803 A2 EP1269803 A2 EP 1269803A2 EP 01933575 A EP01933575 A EP 01933575A EP 01933575 A EP01933575 A EP 01933575A EP 1269803 A2 EP1269803 A2 EP 1269803A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- arrangement
- plasma
- magnet
- plasma chamber
- longitudinal axis
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
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
- F03H1/0037—Electrostatic ion thrusters
- F03H1/0062—Electrostatic ion thrusters grid-less with an applied magnetic field
- F03H1/0075—Electrostatic ion thrusters grid-less with an applied magnetic field with an annular channel; Hall-effect thrusters with closed electron drift
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/54—Plasma accelerators
Definitions
- the invention relates to a plasma accelerator arrangement with a plasma chamber about a longitudinal axis, with an electrode arrangement for generating an electrical acceleration field for positively charged ions over an acceleration path parallel to the longitudinal axis and with means for introducing a focused electron beam into the plasma chamber and its guidance through a magnet system.
- US 5 329 258 A shows a plasma accelerator arrangement in the form of a so-called Hall thruster with an annular acceleration chamber and an essentially radial magnetic field through the plasma chamber.
- the anode and the anode-stage part of the plasma chamber are magnetically shielded.
- a gas is introduced into the plasma chamber, which is open on one side in the longitudinal direction, and is ionized by electrons, which are accelerated from a cathode located outside the piasma chamber to an anode located at the base of the plasma chamber, and is accelerated and expelled away from the anode.
- the radial magnetic field forces the electrons on closed circular orbits around the longitudinal axis of the arrangement and thus increases their residence time and probability of impact in the plasma chamber.
- a hollow ion beam is ejected from an annular opening.
- DE 198 28 704 A1 discloses a plasma accelerator arrangement with a plasma chamber about a longitudinal axis, with an electrode arrangement and a magnet system, and means for introducing an electron beam into the plasma chamber
- a circular-cylindrical plasma chamber into which a sharply focused electron beam generated by a beam generating device is introduced along the longitudinal axis of the cylinder.
- the electron beam is along the cylinder axis through a magnet system
- the i plasma Chamber is an ionizable gas, in particular a noble gas which is ionized by the electrons of the introduced electron beam and by secondary electrons.
- the positive ions that are created are accelerated along the longitudinal axis of the plasma chamber by the potential difference and move in the same direction as the Introduced electron beam
- the ions are also guided along the longitudinal axis by the magnet arrangement and by space charge effects and occur together with some of the electrons of the electron beam at the end of the plasma chamber in the form of a neutral plasma beam
- the electron beam is not introduced as a sharply focused beam into a circular cylindrical plasma chamber, but which, for example, generates a cylindrical hollow jet via an annular cathode surface which is introduced into a toroidal plasma chamber.
- the plasma chamber is radially delimited by an outer chamber wall and an inner chamber wall and the hollow jet is small with respect to the radius s of the hollow cylinder
- the wall thickness is fed between these walls and guided through a magnet system.
- the entire arrangement is preferably at least approximately rotationally symmetrical or at least rotationally symmetrical about a longitudinal axis of the arrangement.
- the magnet system preferably also has a double toroidal structure with a first magnet arrangement lying radially outside with respect to the plasma chamber and one second internal magnet arrangement
- the arrangement according to the invention preferably also contains at least one intermediate electrode in the longitudinal direction of the plasma chamber, the intermediate electrode being on a
- the intermediate potential of the potential difference lies along the longitudinal direction of the plasma chamber.
- the division into several intermediate potentials enables a significant improvement in the efficiency by capturing electrons with a lower kinetic on an intermediate electrode with a small potential difference compared to the current potential of an electron.
- the efficiency increases monotonically with the number of hissing potential stages
- the magnet system can be designed in one stage, with one pole change for the external and the internal magnet system by opposite magnetic poles spaced in the longitudinal direction. At least one of the two magnetic poles is located in the longitudinal direction in the region of the plasma chamber. Both are preferably spaced in the longitudinal direction Poles of the single-stage magnet system within the longitudinal extension of the plasma chamber. tion in which the magnet system is designed in several stages with a plurality of successive subsystems in the longitudinal direction, each of which has an external and an internal magnet arrangement, and in which the subsystems which are successive in the longitudinal direction are alternately oriented in opposite directions
- a plasma accelerator arrangement according to the invention is particularly advantageous, in which at least one intermediate electrode arrangement is arranged in the longitudinal direction of the plasma chamber in the region of the side walls of the plasma chamber.
- the electrodes are placed in the longitudinal direction between the pole ends of a magnet system or magnet subsystem favorable course of electrical and magnetic fields
- Fig. 1 is a sectional view of a side view
- Fig. 2 is a view in the direction of the longitudinal axis
- FIG. 3 shows a stage of a magnet arrangement 4 shows a plasma distribution in a multi-stage arrangement
- the plasma approximates the potential of the electrode with the higher potential for the positive ions (anode) because the electrons move very quickly to the anode until the potential of the plasma rises is the approximately constant potential of the anode and the plasma is thus field-free. Only in a comparatively thin boundary layer on the cathode does the potential drop steeply in the so-called cathode case
- FIG. 1 shows a multi-stage arrangement according to the present invention in which a hollow cylindrical electron beam ES is supplied to a plasma chamber which is toroidal essentially about a longitudinal axis LA as the axis of symmetry, the shape of which is accessible in individual variations, the cylinder axis of which coincides with the longitudinal axis LA and whose beam wall thickness DS (FIG. 2) is small compared to the radius RS of the hollow cylindrical beam shape.
- a hollow beam can be generated, for example, by means of an annular cathode and an adapted beam system.
- the electrons of the electron beam have a kinetic energy of typically> 1 when they enter the plasma chamber keV
- the annular plasma chamber PK is laterally delimited by an inner wall W1 and an outer wall WA
- the magnet system no longer has a single ring about the longitudinal axis LA, but that there is a magnet arrangement RMA with respect to the outside of the plasma chamber, which has mutually opposite magnetic poles spaced apart in the longitudinal direction LR
- a further magnet arrangement RMI which is located radially on the inside of the plasma chamber, is provided, which in turn has both magnetic poles spaced apart in the longitudinal direction LR
- the two magnet arrangements RMA and RMI are radially opposite one another with essentially the same extent in the longitudinal direction LR.
- the two magnet arrangements are aligned with the same orientation, ie in the longitudinal direction LR with the same pole sequence.
- the same poles (NN or SS) are radially opposed and the magnetic fields are for each of the two closed magnetic arrangements
- the course of the magnetic fields of radially opposed magnetic arrangements RMA and RMI can thus be viewed separately by a central surface lying essentially in the middle of the plasma chamber.
- the magnetic field lines B run between the magnetic poles of each arrangement without being curved through this central surface, which is not necessarily so is to pass through it.
- essentially only the magnetic field of one of the two magnet arrangements RMA or RMI acts on each radial side of such a center surface
- Such a magnet arrangement can be formed, for example, by two concentric annular permanent magnets with poles spaced essentially parallel to the axis of symmetry LA. Such an arrangement is isolated in FIG. sheet
- a particularly advantageous embodiment of the invention provides for two or more such arrangements to be arranged one behind the other in the longitudinal direction LR, the pole orientation of successive magnet arrangements as in the known arrangement mentioned at the outset being opposite, so that the poles of successive magnet arrangements opposing one another in the longitudinal direction are of the same type and are therefore not a magnetic field short circuit occurs and the field courses described for the single-stage execution remain essentially for all successive stages
- a plasma accelerator arrangement is preferred in which at least one further intermediate electrode is provided in the longitudinal course of the plasma chamber and is at an intermediate potential of the potential drop.
- Such an intermediate electrode is advantageously on at least one side wall, preferably in the form of two sub-electrodes on the inner and outer side wall of the plasma chamber
- the electrode 10 arranged It is particularly advantageous to position the electrode in the longitudinal direction between two magnetic poles.
- several stages SO S1 S2 are provided in the longitudinal direction, each with a magnetic subsystem and an electrode system in each case.
- the magnetic subsystems each consist of an inner one RMI and an outer RMA magnetic ring as outlined in FIG. 3.
- the partial electrode systems each comprise an outer electrode ring AAO, AA1 AA2 in the successive stages SO S1 S2 and an inner electrode ring AlO, AM, AI2 radially opposite one another, the extension of the electrodes in the longitudinal direction for the outer and inner rings are essentially the same.
- the 0 opposing electrode rings of each subsystem ie AAO and AlO or AA1 and AM or AA2 and AI2, are each at the same potential, in particular the electrodes AAO and AlO being at ground potential of the entire arrangement k
- the inner and outer electrodes can AAO AA1, as well as the poles of the magnet arrangements or inner wall may also be integrated in the outer
- the electric fields generated by the electrodes run approximately perpendicular to the magnetic field lines in areas essential for the formation of the plasma, in particular in the area of the largest electric Potential gradients between the electrodes of successive stages are essentially crossed, so that the secondary electrons generated along the path of the focused primary electrons, including completely decelerated particle electrons, cannot cause a direct short circuit of the electrodes, since the secondary electrons only move along the magnetic field lines of the the toroidal multi-stage magnet system, the plasma beam generated remains essentially limited to the cylinder layer volume of the focused primary electrons.
- the working gas AG supplied to the plasma chamber in particular xenon, is ionized by the primary electrons and in particular the secondary electrons.
- the accelerated ions are together with i decelerated primary electrons of the introduced electron beam are expelled as a neutral plasma beam PB
- the plasma in the individual successive stages can advantageously be adjusted to the stepwise different potentials of the successive electrodes
- the electrodes and the magnet arrangements are arranged in the longitudinal direction so that the spatial phase positions of the quasi-periodic magnetic field compared to the likewise quasi-periodic electric field measured between the minimum amount of the magnetic axial field and the center of the electrodes by max +/- 45 °, in particular max + / - 15 ° are shifted
- a contact of the magnetic field lines with that on the Side wall of the plasma chamber arranged electrode is reached and the plasma potential is set to the electrode potential of this stage due to the easy displacement of the electrons along the magnetic field lines.
- the plasma concentrations at different successive stages are thus at different potentials
- the location of the greatest potential gradient in the axial direction thus lies in a plasma layer, which is characterized by the radial magnetic field profiles that have an electrically insulating effect in the axial direction.
- the above-mentioned favorable phase shift of the quasi-periodic magnetic and electrical structures can be achieved on the one hand by an arrangement according to FIG. 2 with the above-mentioned permissible shift by max +/- 45 °, in particular max +/- 15 °.
- An alternative variant is outlined in FIG , where the penode length of the longitudinally spaced electrode stages AL ,, Al, + ⁇ is twice as large as the period range of successive magnetic ring arrangements.
- Such an arrangement can also be divided into stages with double length compared to FIG. 1, which then each have two opposing magnetic subsystems and contain an electrode system In the arrangement sketched in FIG.
- opposing outer magnetization and inner magnetic ring of the magnet system or of a magnet subsystem can also be provided with opposite pole alignment, so that a longitudinal quadrant through the arrangement corresponding to FIG. 1 results in a magnetic quadropole field Currents IA, II lying on a plane perpendicular to the longitudinal direction are then in the same direction.
- the other measures described according to the invention can be used in a corresponding manner in such an arrangement
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
- Electron Sources, Ion Sources (AREA)
- Semiconductor Lasers (AREA)
- Particle Accelerators (AREA)
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10014034A DE10014034C2 (de) | 2000-03-22 | 2000-03-22 | Plasma-Beschleuniger-Anordnung |
DE10014034 | 2000-03-22 | ||
PCT/DE2001/001105 WO2001072093A2 (de) | 2000-03-22 | 2001-03-22 | Plasma-beschleuniger-anordnung |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1269803A2 true EP1269803A2 (de) | 2003-01-02 |
EP1269803B1 EP1269803B1 (de) | 2008-09-17 |
Family
ID=7635807
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01933575A Expired - Lifetime EP1269803B1 (de) | 2000-03-22 | 2001-03-22 | Plasma-beschleuniger-anordnung |
Country Status (11)
Country | Link |
---|---|
US (1) | US6798141B2 (de) |
EP (1) | EP1269803B1 (de) |
JP (1) | JP4944336B2 (de) |
KR (1) | KR20030014373A (de) |
CN (1) | CN1418453A (de) |
AT (1) | ATE408978T1 (de) |
AU (1) | AU6004801A (de) |
DE (2) | DE10014034C2 (de) |
ES (1) | ES2312434T3 (de) |
RU (1) | RU2239962C2 (de) |
WO (1) | WO2001072093A2 (de) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10014033C2 (de) * | 2000-03-22 | 2002-01-24 | Thomson Tubes Electroniques Gm | Plasma-Beschleuniger-Anordnung |
US6922019B2 (en) * | 2001-05-17 | 2005-07-26 | The Regents Of The University Of California | Microwave ion source |
DE10153723A1 (de) * | 2001-10-31 | 2003-05-15 | Thales Electron Devices Gmbh | Plasmabeschleuniger-Anordnung |
DE10318925A1 (de) * | 2003-03-05 | 2004-09-16 | Thales Electron Devices Gmbh | Antriebsvorrichtung eines Raumflugkörpers und Verfahren zur Lagesteuerung eines Raumflugkörpers mit einer solchen Antriebsvorrichtung |
US7624566B1 (en) | 2005-01-18 | 2009-12-01 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | Magnetic circuit for hall effect plasma accelerator |
US7500350B1 (en) | 2005-01-28 | 2009-03-10 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Elimination of lifetime limiting mechanism of hall thrusters |
KR101094919B1 (ko) * | 2005-09-27 | 2011-12-16 | 삼성전자주식회사 | 플라즈마 가속기 |
US7870720B2 (en) * | 2006-11-29 | 2011-01-18 | Lockheed Martin Corporation | Inlet electromagnetic flow control |
DE102006059264A1 (de) * | 2006-12-15 | 2008-06-19 | Thales Electron Devices Gmbh | Plasmabeschleunigeranordnung |
EP2120255B1 (de) * | 2007-02-16 | 2018-07-18 | National Institute of Information and Communications Technology | Ionenpumpeneinrichtung |
US8016246B2 (en) * | 2007-05-25 | 2011-09-13 | The Boeing Company | Plasma actuator system and method for use with a weapons bay on a high speed mobile platform |
US8016247B2 (en) * | 2007-05-25 | 2011-09-13 | The Boeing Company | Plasma flow control actuator system and method |
WO2011011049A2 (en) * | 2009-07-20 | 2011-01-27 | The Board Of Trustees Of The Leland Stanford Junior University | Method and apparatus for inductive amplification of ion beam energy |
CN102782320B (zh) * | 2010-03-01 | 2015-01-28 | 三菱电机株式会社 | 霍尔推进器及宇宙航行体及推进方法 |
GB201012626D0 (en) * | 2010-07-28 | 2010-09-08 | Rolls Royce Plc | Controllable flameholder |
RU2500046C2 (ru) * | 2011-04-05 | 2013-11-27 | Геннадий Викторович Карпов | Способ получения ускоренных ионов в нейтронных трубках и устройство для его осуществления |
WO2013019667A1 (en) * | 2011-07-29 | 2013-02-07 | Walker Mitchell L R | Ion focusing in a hall effect thruster |
RU2517184C2 (ru) * | 2012-05-18 | 2014-05-27 | Федеральное государственное бюджетное учреждение науки Институт общей физики им. А.М. Прохорова Российской академии наук | Способ управляемого коллективного ускорения электрон - ионных сгустков |
KR101420716B1 (ko) * | 2012-05-23 | 2014-07-22 | 성균관대학교산학협력단 | 사이클로트론 |
CN103037609B (zh) * | 2013-01-10 | 2014-12-31 | 哈尔滨工业大学 | 射流等离子体电子能量调节器 |
CN104001270B (zh) * | 2014-05-07 | 2016-07-06 | 上海交通大学 | 超高能电子束或光子束放射治疗机器人系统 |
US10428806B2 (en) * | 2016-01-22 | 2019-10-01 | The Boeing Company | Structural Propellant for ion rockets (SPIR) |
CN108915969B (zh) * | 2018-07-18 | 2020-09-22 | 北京理工大学 | 一种多模式螺旋波离子推力器 |
CN111111581B (zh) * | 2019-12-19 | 2021-07-02 | 中国科学院电工研究所 | 一种等离子体燃料重整装置 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3626305A (en) * | 1969-01-27 | 1971-12-07 | Atomic Energy Commission | High energy ion accelerator |
US3719893A (en) * | 1971-12-23 | 1973-03-06 | Us Navy | System and method for accelerating charged particles utilizing pulsed hollow beam electrons |
US4233537A (en) * | 1972-09-18 | 1980-11-11 | Rudolf Limpaecher | Multicusp plasma containment apparatus |
JPS55102162A (en) * | 1979-01-31 | 1980-08-05 | Toshiba Corp | Ion source |
US4486665A (en) * | 1982-08-06 | 1984-12-04 | The United States Of America As Represented By The United States Department Of Energy | Negative ion source |
US5359258A (en) * | 1991-11-04 | 1994-10-25 | Fakel Enterprise | Plasma accelerator with closed electron drift |
FR2693770B1 (fr) * | 1992-07-15 | 1994-10-14 | Europ Propulsion | Moteur à plasma à dérive fermée d'électrons. |
JPH06151093A (ja) * | 1992-11-11 | 1994-05-31 | Mitsubishi Heavy Ind Ltd | プラズマ生成加速装置 |
DE4302630C1 (de) * | 1993-01-30 | 1994-05-26 | Schwerionenforsch Gmbh | Koaxial-Beschleuniger zum axialen Beschleunigen eines Plasmarings |
CA2141605A1 (en) * | 1993-06-21 | 1995-01-05 | Alexei Morozov | Device for measuring changes in the thrust of a plasma engine with closed electron drift |
DE19828704A1 (de) * | 1998-06-26 | 1999-12-30 | Thomson Tubes Electroniques Gm | Plasmabeschleuniger-Anordnung |
-
2000
- 2000-03-22 DE DE10014034A patent/DE10014034C2/de not_active Expired - Fee Related
-
2001
- 2001-03-22 AT AT01933575T patent/ATE408978T1/de not_active IP Right Cessation
- 2001-03-22 CN CN01806885A patent/CN1418453A/zh active Pending
- 2001-03-22 DE DE50114337T patent/DE50114337D1/de not_active Expired - Lifetime
- 2001-03-22 ES ES01933575T patent/ES2312434T3/es not_active Expired - Lifetime
- 2001-03-22 JP JP2001568665A patent/JP4944336B2/ja not_active Expired - Fee Related
- 2001-03-22 RU RU2002125111/06A patent/RU2239962C2/ru not_active IP Right Cessation
- 2001-03-22 KR KR1020027012562A patent/KR20030014373A/ko not_active Application Discontinuation
- 2001-03-22 WO PCT/DE2001/001105 patent/WO2001072093A2/de active IP Right Grant
- 2001-03-22 AU AU60048/01A patent/AU6004801A/en not_active Abandoned
- 2001-03-22 EP EP01933575A patent/EP1269803B1/de not_active Expired - Lifetime
- 2001-03-22 US US10/239,274 patent/US6798141B2/en not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
---|
See references of WO0172093A2 * |
Also Published As
Publication number | Publication date |
---|---|
ES2312434T3 (es) | 2009-03-01 |
JP2003528423A (ja) | 2003-09-24 |
WO2001072093A3 (de) | 2002-04-04 |
DE10014034A1 (de) | 2001-10-04 |
US20030057846A1 (en) | 2003-03-27 |
DE50114337D1 (de) | 2008-10-30 |
DE10014034C2 (de) | 2002-01-24 |
ATE408978T1 (de) | 2008-10-15 |
KR20030014373A (ko) | 2003-02-17 |
RU2239962C2 (ru) | 2004-11-10 |
JP4944336B2 (ja) | 2012-05-30 |
AU6004801A (en) | 2001-10-03 |
US6798141B2 (en) | 2004-09-28 |
EP1269803B1 (de) | 2008-09-17 |
WO2001072093A2 (de) | 2001-09-27 |
CN1418453A (zh) | 2003-05-14 |
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