EP0464383B1 - Plasma neutralisation cathode - Google Patents

Plasma neutralisation cathode Download PDF

Info

Publication number
EP0464383B1
EP0464383B1 EP91109114A EP91109114A EP0464383B1 EP 0464383 B1 EP0464383 B1 EP 0464383B1 EP 91109114 A EP91109114 A EP 91109114A EP 91109114 A EP91109114 A EP 91109114A EP 0464383 B1 EP0464383 B1 EP 0464383B1
Authority
EP
European Patent Office
Prior art keywords
holder
emitter
thermal emitter
passage
thermal
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.)
Expired - Lifetime
Application number
EP91109114A
Other languages
German (de)
French (fr)
Other versions
EP0464383A3 (en
EP0464383A2 (en
Inventor
Arkhipov Boris Alexeevich
Gorbachev Yuriy Mitrofanovich
Ivanov Viktor Alexeevich
Kozubsky Konstantin Nikolaevich
Komarov Georgy Alexeevich
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Hauzer Techno Coating BV
Original Assignee
Hauzer Techno Coating Europe BV
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 Hauzer Techno Coating Europe BV filed Critical Hauzer Techno Coating Europe BV
Publication of EP0464383A2 publication Critical patent/EP0464383A2/en
Publication of EP0464383A3 publication Critical patent/EP0464383A3/en
Application granted granted Critical
Publication of EP0464383B1 publication Critical patent/EP0464383B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J3/00Details of electron-optical or ion-optical arrangements or of ion traps common to two or more basic types of discharge tubes or lamps
    • H01J3/02Electron guns
    • H01J3/025Electron guns using a discharge in a gas or a vapour as electron source

Abstract

A plasma compensation cathode comprises a casing (1) accommodating coaxially with its outlet hole (2) a hollow holder (3) and a thermal emitter (4) with a central passage (5), a layer (10) of material chemically inert at high temperatures to the materials of the holder and emitter being interposed therebetween. The central passage (5) is blind at the side of admission of gas, and is communicated with the interior of the holder (3) by way of a through passage (8) made in the wall of the thermal emitter (4) so that its axis intersects the axis of passage (5), and longitudinal grooves (9) made in the side surface of the thermal emitter (4) at the location of the inlet holes of the through passage (8). The holder (3) is embraced by heater (6) having a support ring (7) positioned in its midportion and secured in an insulation sleeve (18) separating the heater (6) from the coaxial heat screens (11) interconnected successively to define a sealed cavity (14) wherethrough the interior of the holder (3) communicates with the gas feeding pipe (13) secured in the casing (1) through the support insulator (17). Interposed between mechanical filters (16) and between holder (3) and pipe (13) is a getter (15). <IMAGE>

Description

    Field of the Invention
  • This invention relates generally to glowing compensation cathodes, and more particularly to plasma compensation cathodes.
  • Background of the Invention
  • There is known a glowing cathode (cf., Schats M.F."Heaterless Ignition of Inert Gas. Ion Thruster Hollow Cathodes" AJAA Paper, 1985) comprising a casing with a cylindrical insert secured to the inner surface of the casing and functioning as thermal emitter, a heater secured at the outer side of the casing, and an orifice secured to end face of the casing and acting as the outlet hole of the cathode. This construction of cathode requires high power heaters to heat thermal emitter to a temperature ensuring thermoionic emission sufficient for maintaining a stable discharge.
  • There is also known a plasma compensation cathode (cf., L.A. Artsimovich, et al "Razrabotka statsionarnogo plazmennogo dvigatelya i ego ispytanie na iskusstvennom sputnike Zemli Meteor", Kosmicheskie issledovania, 1974, tom XII, vyp. 3, pages 455 and 456, Fig. 5). This compensation cathode has a casing with an outlet hole at one wall thereof, the casing accommodating coaxially to its outlet hole a tubular holder receiving a thermal emitter with a central through passage. The compensation cathode also includes a heater embracing the tubular holder, and heat screens positioned between the holder and casing walls. Connected to the tubular holder is a pipe for feeding gas to the interior of the casing and to the passage of thermal emitter through its inlet portion. This pipe is secured in the casing through an insulator.
  • During operation of the compensation cathode gas is conveyed through the tubular holder to the passage of the thermal emitter. Heated to a high temperature, the thermal emitter ensures emission of electrons sufficient for maintaining stable electric discharge between the inner surface of the thermal emitter and anode of the plasma source. After bringing the device to steady-state operation conditions the heater is deenergized, and the compensation cathode continues to operate automatically, whereby the preferred temperature level is ensured by the energy liberated in the catholyte layer approximating to the product of ionic current resulting from discharge by the potential drop at the cathode. However, in the course of operation the discharge can move from the passage of the thermal emitter to the interior of the tubular holder resulting in evaporation of the material of the holder and fouling of the passage with holder material to almost complete clogging. As a result, thermoemission surfaces tend to degrade, and thermoemission current tends to decrease thereby reducing the service life of the compensation cathode to only tens of hours. In addition, direct connection of the holder of thermal emitter to the gas feeding pipe leads to vigorous heat transfer from the emitter to outer structural parts, and consequently to move prominent catholyte potential drop ensuring the energy necessary for maintaining automatic operating conditions. More prominent catholyte potential drop also leads to reduced service life of the thermal emitter because of intensified ionic bombardment. In addition, tight contact of thermoemissive materials with the holder at high working temperatures is accompanied by active chemical interaction, such as penetration of boron followed by formation of metal borides, which in turn causes embrittlement and cracking of the holder material and thermal emitter to result in irreversible deformation of the holder. This disadvantageous effect is especially pronounced at starting operating conditions accompanied by the highest temperature levels, which limits the service life and reduces the total number of engagements of the compensation cathode. Also, the helical heater embracing the tubular holder is characterized by low rigidity to result in sagging and deformation of its coils resulting in possible contact of the coils with the holder or thermal screens and short-circuiting of the heater. This in turn leads to fewer engagements of the compensation cathode and reduced service life thereof. In addition, the working gas can contain negligible quantities of such admixtures as oxygen, water, or the like, tending to react at high working temperatures with the material of the thermal emitter and affecting the thermoemissive characteristics of the material. Extended operation for tens or hundreds of hours makes this disadvantageous effect even more prominent to reduce the service life of the compensation cathode.
  • Summary of the Invention
  • The present invention aims at providing a plasma compensation cathode which would be so constructed as to lock discharge zone in the passage of the thermal emitter, prevent chemical interaction of the thermal emitter with the material of the holder and with the thermal system maintaining automatically the preferred temperature of the thermal emitter at minimised cathodic potential drop, and also to increase the rigidity of the heater and facilitate additional cleaning of gas from impurities.
  • The aim of the invention is attained by a plasma compensation cathode according to the claim.
  • The use in the proposed plasma compensation cathode of a thermal emitter with a special passage for feeding gas, a layer of chemically inert material, a system of coaxial heat screens, a support ring, an insulation sleeve, a getter, and mechanical filters makes it possible to substantially extend the service life and increase the total number of actuations of the cathode.
  • Brief Description of the Drawings
  • The invention will now be described in greater detail with reference to a specific embodiment thereof taken in conjunction with the accompanying drawings, in which:
    • Fig. 1 shows a general view of the proposed plasma compensation cathode; and
    • Fig. 2 is a section taken along line 11 in Fig. 1
    Best Mode of Carrying out the Invention
  • A plasma compensation cathode comprises a casing 1 (Fig. 1) having an inlet hole 2. The casing accommodates coaxially a hollow holder 3 and a thermal emitter 4 with a central passage 5. The holder 3 is positioned inside casing 1 coaxially with the outlet hole 2 and embraced by a heater 6 fashioned as a spiral one end of which is secured to the casing and the other to the holder 3. The heater 6 is provided with a support ring 7 located at its midportion and functioning as an additional support point.
  • The central passage 5 of the thermal emitter 4 is blind at the side of admission of gas, and is communicated with the interior of the holder 3 by way of a central passage 8 (Fig. 2) made in the wall of the thermal emitter 4, the axis of this passage extending perpendicularly to the axis of the central passage 5, and longitudinal grooves 9 provided at the side surface of the thermal emitter 4 at location of the inlet holes of the through passage 8. Occupying the space between the inner surface of the holder 3 and side surface of the thermal emitter 4 is a layer 10 (Fig. 1) of material chemically inert at high temperatures to the materials of the holder 3 and thermal emitter 4. Positioned between the heater 6 and walls of casing 1 is a system of coaxial heat screens 11 connected successively through spacer rings 12 and secured at pipe 13 for feeding gas to define a sealed cavity 14 wherethrough the interior of the holder 3 communicates with the gas feeding pipe 13. A space between the holder 3 and pipe 13 accommodates a getter 15 positioned between mechanical filters 16, whereas the pipe 13 is secured in a support insulator 17. The heater 6 is separated from the system of heat screens 11 by an insulation sleeve 18 in which the support ring 7 is secured.
  • In operation of the proposed plasma compensation cathode the gas flows along the pipe 13 through the getter 15 and mechanical filters 16 to the interior of the holder 3, and then through the grooves 9 and through passage 8 to the central passage 5 of the thermal emitter 4. The heater 6 acts to heat the thermal emitter 4 to a temperature ensuring emission of electrons sufficient for sustaining a stable electric discharge between the inner surface of the thermal emitter 4 and anode (not shown) of a plasma source. After bringing the device to steady state operating conditions the heater 6 is deenergized and the compensation cathode operates automatically, whereby the required temperature level of the thermal emitter 4 is ensured thanks to the energy resulting from the discharge.
  • When the central passage 5 at the side of admission of gas is blind, the electric discharge in passage 5 can be stabilized by changing the pressure of gas and dimensions of the passage 5. This prevents fixation of discharge at the walls of holder 3 resulting in fouling and clogging of passage 5 of the thermal emitter 4, which facilitates maintaining the initial thermal emission from the inner surface of the thermal emitter 4 and substantially increases the service life of the compensation cathode. Positioning between the inner surface of holder 3 and side surface of the thermal emitter 4 of layer 10 of material chemically inert to the material of holder and thermal emitter 4 obviates chemical interaction and diffusion of materials thereby making impossible irreversible deformation of holder 3 and cracking of holder 3 and thermal emitter 4. The accompanying advantage is substantially increased number of actuations and extended service life of the cathode.
  • The system of coaxial heat screens 11 defining with gas feeding pipe 13 and holder 3 a sealed cavity 14 makes it possible to substantially reduce the heat flow from holder 3 of the thermal emitter 4 to outer parts of the cathode structure and, as a consequence, to reduce the potential drop at the cathode to the level of gas ionization potential and substantially extend the service life of the compensation cathode.
  • Provision of the support ring 7 secured in the insulation sleeve 18 allows to increase rigidity of the spiral of heater 6, prevent short-circuiting of the spiral of heater 6 (viz., engagement of the spiral coils with holder 3 or screens 11) even at a substantial deformation of spiral coils due to multiple engagement thermocycles. This again enables to increase the number of actuations and extend the service life of the compensation cathode.
  • Provision of the proposed compensation cathode with getter 15 positioned between mechanical filters 16 immediately at the location where the gas is admitted to the interior of the holder 3 affords extra fine chemical cleaning of gas from admixtures of oxygen, water, and the like, and ensures more stable thermoemission characteristics of thermal emitter 4 resulting in an extended service life of the compensation cathode.
  • Industrial Applicability
  • The invention can be used for neutralizing ion beams in accelerators with closed electron drift and extended acceleration zone, in accelerators with anodic layer and narrow acceleration zone, in plasma-ion accelerators, and also for compensating space and surface discharges.

Claims (1)

  1. A plasma compensation cathode comprising a casing (1) accommodating coaxially with its outlet hole (2) a hollow, tubular holder (3) which is embraced by a heater (6), and a thermal emitter (4) with a central passage (5) communicating with the interior of the holder (3), whereby said thermal emitter is positioned within the holder, the cathode further comprising coaxial heat screens (11) interposed between the heater (6) and walls of the casing (1), and a pipe (13) for feeding a gas to the interior of the holder (3), said pipe being secured in a support insulator (17),
    CHARACTERIZED in that the central passage (5) of thermal emitter (4) is blind at the end of the emitter which is closer to the gas admission through the pipe, and communicates with the interior of the holder (3) by way of a through passage (8) made in the wall of the thermal emitter (4) so that its axis intersects the axis of the central passage (5), and longitudinal grooves (9) along the side surface of the thermal emitter (4) from the location of the inlet holes of the through passage (8) to the end of the emitter which is closer to the gas feeding pipe (13); a getter (15) is positioned between mechanical filters (16) at the location where the gas is admitted to the interior of the holder; whereby the interior of the holder (3) communicates with the gas feeding pipe (13) through a sealed cavity (14), said cavity being defined by clearances between the coaxial heat screens (11) which are successively connected by spacer rings (12) and secured at the gas feeding pipe (13), a space between the inner surface of the holder (3) and side surface of the thermal emitter (4) accommodating a layer (10) of material chemically inert at high temperatures to the material of the holder (3) and the thermal emitter (4), whereby the the cavity (14) accommodates the getter (15) positioned between the holder and the gas feeding pipe; and the heater (6) at a midportion thereof is provided with a support ring (7) which is secured in an insulation sleeve (18) separating the thermal heater (6) from the coaxial thermal screens (11).
EP91109114A 1990-06-26 1991-06-04 Plasma neutralisation cathode Expired - Lifetime EP0464383B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SU904843045A RU2012946C1 (en) 1990-06-26 1990-06-26 Plasma cathode-compensator
SU4843045 1990-06-26

Publications (3)

Publication Number Publication Date
EP0464383A2 EP0464383A2 (en) 1992-01-08
EP0464383A3 EP0464383A3 (en) 1992-07-15
EP0464383B1 true EP0464383B1 (en) 1994-09-21

Family

ID=21523026

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91109114A Expired - Lifetime EP0464383B1 (en) 1990-06-26 1991-06-04 Plasma neutralisation cathode

Country Status (5)

Country Link
EP (1) EP0464383B1 (en)
JP (1) JP2963903B2 (en)
AT (1) ATE112096T1 (en)
DE (1) DE69104142T2 (en)
RU (1) RU2012946C1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105626410A (en) * 2015-12-25 2016-06-01 上海空间推进研究所 Plume neutralizer of space electric thruster
CN111720281A (en) * 2020-06-24 2020-09-29 遨天科技(北京)有限公司 Array coaxial type vacuum arc thruster device

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19813589C2 (en) * 1998-03-27 2002-06-20 Karlsruhe Forschzent Method for generating a pulsed electron beam and electron beam source for carrying out the method
FR2897747B1 (en) * 2006-02-23 2008-09-19 Commissariat Energie Atomique ARC PLASMA TORCH TRANSFER
CN102355791A (en) * 2011-09-28 2012-02-15 南京创能电力科技开发有限公司 Device for insulation connecting between cathode and anode of plasma generator
RU2502238C2 (en) * 2012-02-07 2013-12-20 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" Plasma cathode
RU2667155C1 (en) * 2017-03-28 2018-09-17 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Hollow cathode
RU2662795C1 (en) * 2017-04-18 2018-07-31 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Hollow cathode
RU2684633C2 (en) * 2017-05-10 2019-04-11 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" (ФГУП "ОКБ "Факел") Cathode-compensator
RU2684309C1 (en) * 2018-03-14 2019-04-08 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Plasma hollow cathode
CN113371233B (en) * 2021-07-29 2022-08-30 哈尔滨工业大学 Anode structure and cusp field thruster
CN114320801B (en) * 2021-12-28 2022-07-01 哈尔滨工业大学 Cold cathode capable of being started quickly
CN114458564B (en) * 2022-04-12 2022-07-12 国科大杭州高等研究院 Hall thruster ring type partial pressure gas path insulation structure
CN115681054B (en) * 2023-01-03 2023-05-09 国科大杭州高等研究院 Self-maintaining Hall thruster

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5853460B2 (en) * 1981-12-14 1983-11-29 株式会社東芝 Hollow cathode discharge device
JPS58169752A (en) * 1982-03-30 1983-10-06 Toshiba Corp Hollow-cathode discharge device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105626410A (en) * 2015-12-25 2016-06-01 上海空间推进研究所 Plume neutralizer of space electric thruster
CN105626410B (en) * 2015-12-25 2018-08-03 上海空间推进研究所 A kind of space electric thruster plume averager
CN111720281A (en) * 2020-06-24 2020-09-29 遨天科技(北京)有限公司 Array coaxial type vacuum arc thruster device

Also Published As

Publication number Publication date
JP2963903B2 (en) 1999-10-18
DE69104142T2 (en) 1995-01-19
RU2012946C1 (en) 1994-05-15
JPH04299000A (en) 1992-10-22
EP0464383A3 (en) 1992-07-15
ATE112096T1 (en) 1994-10-15
DE69104142D1 (en) 1994-10-27
EP0464383A2 (en) 1992-01-08

Similar Documents

Publication Publication Date Title
EP0464383B1 (en) Plasma neutralisation cathode
US5359254A (en) Plasma compensation cathode
US5241243A (en) Device with unheated hollow cathode for the dynamic generation of plasma
US4301391A (en) Dual discharge plasma device
CN111120234B (en) Graphite high-temperature cathode device for electric thruster
US4157471A (en) High temperature ion source for an on-line isotope separator
US4297615A (en) High current density cathode structure
US6870321B2 (en) High-frequency electron source
US4710938A (en) Metal ion laser protected against the deposition of metal vapor on brewster windows
FI68928C (en) CATHODIC FOER LYSROER
US3683295A (en) Gas laser discharge tube
US4954751A (en) Radio frequency hollow cathode
CN100482030C (en) Extreme UV and soft x ray generator
US3304456A (en) Slot cathode
SU1303339A1 (en) Multichannel cathode
JPS55136101A (en) Solid electrolyte oxygen pump
US20240062995A1 (en) Hollow cathode system for generating a plasma and method for operating such a hollow cathode system
US11937361B1 (en) Annular hollow cathode
CN218160268U (en) Tantalum tube insulating part structure of hollow cathode ion source neutralizer
US20240014014A1 (en) High current heaterless hollow cathode
GB2194673A (en) Apparatus for forming an electron beam sheet
JPH10158823A (en) Ion plating device and formation of thin film by this device
RU2139590C1 (en) Cathode unit
SU965289A1 (en) Ion gas laser
SU1523277A1 (en) Torch for welding and building-up in vacuum

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT CH DE FR GB IT LI NL

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT CH DE FR GB IT LI NL

17P Request for examination filed

Effective date: 19920826

17Q First examination report despatched

Effective date: 19940126

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT CH DE FR GB IT LI NL

REF Corresponds to:

Ref document number: 112096

Country of ref document: AT

Date of ref document: 19941015

Kind code of ref document: T

ITF It: translation for a ep patent filed

Owner name: BARZANO' E ZANARDO MILANO S.P.A.

REF Corresponds to:

Ref document number: 69104142

Country of ref document: DE

Date of ref document: 19941027

ET Fr: translation filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Effective date: 19950604

Ref country code: AT

Effective date: 19950604

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19950630

Ref country code: CH

Effective date: 19950630

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19960101

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19950604

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Effective date: 19960229

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 19960101

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19960301

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050604