Patent Application
20050237000
1. Field of the Invention
This invention relates generally to technology of ion and plasma sources, and more particularly to Hall-type ion sources producing high-current ion beams that can be utilized in thin film processing technology. Historically, thrusters, or accelerators of ions were utilized for space application to move, or stabilize space satellites since early 70-ies. Ion sources that can be considered a spin-off of electric propulsion thrusters have the same operational principles. However, they do not need to be light and efficient as thrusters; they need to accelerate ions, produce high ion beam currents with regulated ion beam mean energy, be efficient in vacuum etching, deposition, in assisting to certain physical processes involving interaction of sputtered particles with surface of a substrate. Hall current in ion and plasma sources is a result of interaction of electrical charge carriers—electrons and ions caused by separate direction of electric and magnetic fields. Change of conditions leading to a value of charged particles density by a value and geometry of magnetic field, shape of electrodes and discharge channel leads to separation of charged particles caused by particles different trajectories and appearance of Hall current, which is directed to a normal to vectors of electric field, E and magnetic field, B.
2. Description of the Prior Art
For technological applications, one of Hall-type ion sources was introduced in 1989 in U.S. Pat. No. 4,862,032 by Kaufman, et al., which in 2003 was modified in form of a modular ion source by Kaufman, U.S. Pat. No. 6,608,431 B1. This ion source also considered as gridless ion source with a discharge chamber determined by a conical shape of a hollow anode, and also called an end-Hall ion source with a circular discharge region and only an outside boundary. In 2003 Sainty obtained a U.S. Pat. No. 6,645,301 B2 called “Ion Source”. This patent has a very similar concept and design of a Hall ion source as in U.S. Pat. No. 4,862,032 by Kaufman et al., and practically the same conical shape of a hollow anode, with some minor changes such as a gas distributing system (reflector), which in Sainty's patent is at an anode potential. In Kaufman et al., U.S. Pat. No. 4,862,032, and in Kaufman U.S. Pat. No. 6,608,431 B1 a gas distributing system is at floating potential. These publications are incorporated herein by reference.
In general, among gridless ion sources there are two most common types of ion sources, both also called as Hall ion sources: a closed drift ion source with annular discharge chamber and an end-Hall ion source with a circular discharge chamber occupied mostly by a hollow anode of a conical shape. However, for a distinction, the first one will be called a closed-drift ion source and the second one, an end-Hall ion source. Both types of ion sources utilize a Hall effect that playing a major role in acceleration of ions.
Ion sources with closed electron drift have been utilized from early seventies, since appearance in space of first Russian thrusters with closed electron drift in 1972. A detailed review of closed drift ion sources/thrusters features, which is applied to any Hall-current sources, is described by Zhurin, et al., in article “Physics of Closed Drift Thrusters” in Plasma Sources Science & Technology, Vol. 8 (1999), beginning on page R1. This publication is incorporated herein by reference.
Such ion sources operate in a following way. Working gas supplied into a channel close to anode is ionized by electrons moving under impact of electric field from cathode to anode in a radial magnetic field. In a traditional performance, an ion source comprises of anode, cathode, discharge chamber with accelerating channel, a magnetic system with magnetic poles, magnetic means provided by electromagnetic coils, or permanent magnets, a central core and a magnetic path. A magnetic system is designed in a way that in an annular accelerating channel a mainly radial magnetic field is realized. An electric potential is applied between anode and cathode, and an electric field in a discharge channel is directed approximately parallel to an ion sources axis. A working gas, which must be ionized, is supplied into a discharge channel through anode. Though it is possible, and used frequently, working gas is applied through a separate gas distributor, regularly placed under anode area, and from this area a working gas is directed into an anode area.
In closed drift ion sources, there are two main types of ion sources distinguished with length and material of a discharge channel. One type, called a magnetic layer ion source, which has a discharge channel length that is greater than its width and usually has discharge channel made of dielectric material; though, there are types of a magnetic layer ion source that discharge channel walls made of a conducting material. The other type, called an anode layer ion source has a discharge region length that is less than its width and its walls made of conducting material. Both sources have very similar characteristic performance with some non-fundamental differences.
In Hall ion sources a magnetic field value is selected in such a way that Larmour radii for electrons, rLe and ions, rLi calculated through energy corresponding to applied potential difference satisfy to a condition: rLe<<L<<rLi, where L is a characteristic dimension of an acceleration region in an ion source's discharge channel. In Hall ion sources a cyclotron frequency of electrons, ωe must be greater than a frequency of electron collisions, ν with other particles and discharge channel walls, i.e. ωe>>ν=1/τe, where τe is an average time between electron collisions with other particles and discharge channel walls. That is why so-called Hall parameter, ωeτe that utilized for a characterization of electron magnetization is ωeτe>>1.
The condition for magnetization of electron component in plasma (ωeτe>>1) and, at the same time, an ion component is not magnetized (ωiτI<<1) means that a determining process in closed drift ion sources is an ion current motion in a discharge region, and an electric field is “suspended” on a magnetized electron component. In end-Hall ion and some other types of ion sources, electrons in certain areas of discharge channel occupied by plasma (at exit in end-Hall ion sources) can be only partially magnetized. In such cases, Hall effect leads to a change of direction of electron motion and to a corresponding change of volumetric forces forming and accelerating plasma flow. Hall parameter, βe determines a relative value of a Hall electromotive force and influence of a magnetic field on plasma electric conductivity, σ:βe=EHall/E==|j×B|/[(1/σ)|j|en]=σB/en=ωeτe. With the increase of a Hall parameter, ωeτe a motion of charged particles across of a magnetic field becomes more difficult and particles begin to drift with a velocity, ν=(E×B)/B2, or in mutually orthogonal fields, E and B. A drift velocity can be determined through a ratio of electric and magnetic fields, νdrift=E/B.
In closed-drift and in certain area of end-Hall ion sources a primary motion of electrons is in azimuthal direction. Because an azimuthal electron velocity is significantly higher than a longitudinal electron velocity component, electron trajectories are almost closed. And this determines a name of a first one: a source (or a thruster) with a closed electron drift.
End-Hall ion sources also can be called sources with closed electron drift, however, a situation here is different. A Larmour electron radius, rLe is smaller than L, but only at a gas distributor/reflector, where a magnetic field usually is quite strong. In existing end-Hall ion sources this value is from 600 to 1000 G. And a magnetic field in this area has mainly an axial direction. Magnetic field decreases significantly from a gas distributing area and at the discharge channel's exit it is only about 50-60 G. In general, in existing closed-drift ion sources, a magnetic circuit is designed in such a way that a magnetic field increases from anode to a discharge channel's exit. The best efficient operating closed drift ion sources have a magnetic maximum optimum value of about 200-450 G for Argon and 450-750 G for xenon. In end-Hall ion sources the applied magnetic field lines are mainly axial at the top of gas distributing system-reflector and are mainly radial at exit of discharge channel, close to an external magnetic pole. The end-Hall ion sources have a negative magnetic gradient and the closed-drift ion sources have a positive magnetic gradient in a discharge channel.
In a process of ion sources operation, a motion of electrons takes place from cathode to anode region and to anode itself, this motion is accompanied by collisions with atoms of working material, with ions, with discharge chamber walls and due to discharge oscillations. As it was above noted, ions are practically not magnetized and they move mainly along applied electric field and are accelerated in this field. A flow of ions “captures” necessary number of electrons produced by an external source of electrons, so these ions become neutralized and together they develop a plasma flow.
Since electrons drifting in an azimuthal direction neutralize an ion volumetric charge in an ion source's discharge channel, in closed drift and end-Hall ion sources there is no limit for an ion beam current by a space electric charge. This feature is a significant advantage of closed-drift and end-Hall ion sources in comparison with electrostatic or so-called gridded ion sources.
Because electrons in magnetic field are moving along magnetic field lines relatively free before their collisions with neutral atoms, in a first approximation it is possible to consider the surfaces going through magnetic field lines in an azimuthal direction as surfaces of equal potential. This is one of major ideas in a possibility and necessity to control and focus an ion flow through a selection of a corresponding configuration of magnetic field lines.
In both types of ion sources, end-Halls and closed-drift types it is necessary to have a source of electrons to start a discharge and ionization of a working gas. Analysis of discharge at low pressure (rarefied regimes, P≦1 mtorr) and moderate discharge voltages (50-1000 V) and currents (1-20 A) shows that from about 50 to 350 V a discharge represents itself so-called a non-self-sustained discharge and from about 350 V and higher it represents a self-sustained discharge. It means that, in order to maintain a discharge in a discharge channel of these ion sources, it is necessary to provide a source of electrons at discharge voltages under about 350 V. For ion sources with operating discharge voltages over 350 V it is necessary to start discharge and after its beginning it can maintain itself providing electrons from small sparks in vacuum chamber and ion source's discharge chamber itself.
Hot filaments and hollow cathode electron sources are generally used as cathodes in closed drift and end-Hall ion sources. Hot filaments, which utilize a tantalum and tungsten wire, can produce electron currents from about 0.1 A to about 30 A. Modern hollow cathode-neutralizers make possible to obtain electron currents from 0.5 A to 75-100 A with a flow of working material that in 10-50 times lower than in an ion source itself. However, there are other types of cathodes that can be utilized for neutralization of Hall-current ion source's ion beam, such as a “plasma bridge” and a “cold hollow cathode”, a device utilizing a glow discharge in a longitudinal magnetic field.
One of the most distinguished features of a U.S. Pat. No. 4,862,032 by Kaufman, et al., as it was above mentioned, is that a magnetic field strength decreases in a direction from anode to cathode: page 2, lines 55-59; page 10, claim 1, lines 60-64; page 11, claim 4, lines 55-59. This provision is very distinct and emphasized through the whole patent and makes it, as was above mentioned, an ion source with a negative gradient of magnetic field. And this particular feature, a decreased value of a magnetic field along an ion source's discharge region, substantially reduces a range of operation conditions of an end-Hall ion source, especially in the range of discharge voltages over 300 V, and can be considered as a major shortcoming of that type of ion source.
There are other important shortcomings of existing end-Hall ion sources caused by a negative magnetic gradient of magnetic field in a discharge channel of such an ion source. These are the following shortcomings that necessary to mention:
Thin film deposition in many cases requires ion assisting of low energy ion sources. Magnetic field configuration with strong axial component of magnetic field makes possible for end-Hall type ion sources to operate at discharge voltages, Vd lower than 100 V, at 40-50 V with Argon and at 20-30 V with Xenon. Closed drift ion sources with strong radial component of magnetic field at ion source's exit make possible to start discharge at voltages from 100 V to over 1000 V with practically all working gases. A combination of both types of ion sources helps to extend a range of operating conditions.
A B-E (magnetic-electric fields) discharge should effectively combine several functions: to prevent direct motion of electrons from cathode to anode, forcing electrons to drift to anode in closed loops, to generate and accelerate ions in a discharge channel. In general, a B-E discharge always has oscillations and instabilities of main operating parameters: discharge current, Id and voltage, Vd. Oscillations and instabilities were found by researchers from the beginning of studying closed-drift and end-Hall ion sources and thrusters. However, most instabilities and oscillations actually is a part of normal operation of ion sources. And, a presence of oscillations in plasma with intensity that does not exceed certain critical value, even if they lead to a partial decrease of efficiency of ion production, can provide stable operation of ion source in regimes that could not be realized otherwise. However, instabilities and oscillations that become about 100% of discharge current, Id and voltage, Vd can destroy normal discharge and extinguish ion source operation.
In general, there are many different types of oscillations accompanying B-E discharge. Among them there are several groups of the most prominent and important oscillations that can disrupt normal operation of an ion source. More detailed information about oscillations in B-E discharge can be found in a mentioned article by Zhurin, et al., “Physics of Closed Drift Thrusters” in Plasma Sources Science & Technology, Vol. 8 (1999), beginning on Page R1. These oscillations are:
Contour oscillations are longitudinal oscillations with a characteristic frequency of 1-30 kHz. Their mechanism is due to instability of ionization region in a discharge area. These oscillations are most intense oscillations and at the regimes with developed oscillations of this type there are observed a 100% modulations of discharge parameters. Contour oscillations can be suppressed by a correct configuration of a magnetic field, discharge voltage, working mass flow, and parameters of power supply.
Ionization oscillations have maximum frequencies in a range of tens to hundreds of kHz. These oscillations are caused by an azimuthal wave traveling in a direction of electron drift; they are connected with an ionization wave of a working material. This instability appears beginning from a certain critical value of a parameter IdB/ma (where Id is a discharge current, B is a magnetic field, and ma is a working material mass flow); with a growth of this parameter an amplitude of a discharge voltage increases achieving 15-25% of a nominal discharge voltage. Ionization instability can be decreased substantially with a higher discharge current, when a regime of complete ionization is observed.
Flight oscillations are characterized by a broad spectrum of frequencies in a range of 100 kHz up to 10 MHz and they correspond to an ion flight time through a discharge channel. Amplitude of flight oscillations can achieve 20-30% of value of discharge parameters. Plasma potential and particles density are pulsed along an ion source synchronously; however, these oscillations are non-symmetrical along azimuth, and this leads to development of alternating electric fields. Plasma turbulence increases with appearance of flight oscillations.
Spoke-type oscillations. Every type of ion source always has a certain range of optimum operation parameters such as discharge current, Id and voltage, Vd, working material (gas) mass flow, ma, magnetic field, B. Before an ion source starts operation in optimum regime, at a low-voltage part of volt-ampere characteristics of discharge there always takes place an ionization instability of a spoke type that rotates in an azimuthal direction with a constant velocity, vφ≈cvEz/Br, where cv is a constant in a range of 0.4-0.8. A structure of this oscillation wave (20-60 kHz) is characterized by an increased electron concentration, ne.
High-frequency oscillations are typically in a range of 1-100 MHz. They are hybrid azimuthal oscillations developed in an ion source with a negative gradient of a magnetic field. These oscillations are harmful for end-Hall type ion source in a whole discharge channel and in closed drift ion sources they are important at an ion source's exit, where magnetic field changes from positive to negative gradient.
The most intensive are contour oscillations. These oscillations are also a problem for end-Hall type ion sources, where a magnetic field decreases in a discharge region. Such oscillations lead to a substantial divergence of ion flow, to sputtering of a discharge channel, to unnecessary discharge channel's heating.
Due to great importance for solution of oscillation problem for optimization of processes in closed drift and Hall-type ion sources, it is necessary to use different ways for stabilization and suppression of instabilities. Besides of above mentioned article by Zhurin, et al., “Physics of Closed Drift Thrusters” in Plasma Sources Science & Technology, Vol. 8, beginning on page R1, there are many other studies devoted to oscillation problem in ion and plasma ion sources/thrusters such as Zhurin, et al., “Dynamic Characteristics of Closed Drift Thrusters”, published at 23rd International Electric Propulsion Conference, Sep. 13-16, 1993, IEPC-93-095, beginning on page 1, and Randolph, et al., “The Mitigation of Discharge Oscillations in the Stationary Plasma Thruster”, published at 30th AIAA Joint Propulsion Conference, Jun. 27-29, 1994, beginning on page 1. These publications are also incorporated herein by reference.
A fundamental criterion for suppression of instabilities in Hall-current closed drift ion sources/thrusters was introduced by Morozov in article “On Equilibrium and Stability of Flows in Accelerators with Closed Electron Drift” in Russian publication “Plasma Accelerators”, Proceeding of 1st All-Union Conference on Plasma Accelerators, Moscow, Publishing House “Mashinostroenie”, 1973, beginning on page 85, that in Hall-current ion sources/thrusters with closed electron drift, in order to have a flow with suppressed oscillations, it is necessary to utilize in a discharge channel a magnetic field with a positive magnetic gradient: ∂Br/∂x>0. Morozov's publication is incorporated herein by reference. In above mentioned article by Zhurin, et al., in an article Physics of Closed Drift Thrusters” in Plasma Sources & Technology, Vol. 8, on page R8 there is information about this stability criterion.
In light of foregoing, it is an object of the invention to introduce an ion source of a Hall-current type with improved positive magnetic field gradient. Such magnetic field configuration in a cylindrical and cone shape discharge channel makes possible to suppress oscillations and instabilities.
Another object of the present invention is to provide an ion source with a high efficiency of ionization in a discharge channel. Such efficient ionization leads to a conversion of a discharge current to about 90% of particles into an ion beam current. In other words, in contrast with existing end-Hall ion sources with a conversion of only about 20-25% of a discharge current into an ion beam current, the invented ion source provides about 90% of a discharge current into an ion beam current.
Still another object of the present invention is to expand operating conditions of the invented ion source for discharge voltages from about 20 V to over 1000 V, and for discharge currents from about 1 A to over 20 A, so a total power applied to the invented ion source can be about 1.5-2 kW without a water cooled anode, and substantially and over 10 kW with a water cooled anode.
Yet a further object of the present invention is to make an ion source with wider range of operation parameters at different magnetic field distributions. This flexibility is provided by following means: a) a placement of magnets in area around a discharge region; b) a placement of a magnetic shunts around an anode area, so that magnetic field lines will go around this magnetic shunt and will develop a positive magnetic gradient in a discharge region, and an anode will be in area with minimum of magnetic field; c) by a gas feed area under anode, this gas volume is a subject of electrons penetration into area under anode and a photo-ionization radiation from a region of ionization and acceleration located downstream from anode area; this gas volume provides a working gas into a discharge area with more higher and uniform initial ionization; d) working gas supplied into a gas volume goes through a series of small holes placed on a periphery of an external magnetic screen with holes having inclination so, that working gas is introduced through a tangential entrance with development of a vortex flow that provides uniform distribution of working gas into gas volume under anode and into anode area.
A further object of the present invention is to provide potential distribution conditions that help to have acceleration of ions mainly in a discharge chamber exit close to a maximum of magnetic field distribution. Such a potential distribution helps to reduce significantly a damage to a gas-distributor/reflector and to make this part of an ion source with longer operating lifetime. An ion beam focusing by a separation of ionization and ion acceleration makes possible to substantially reduce a discharge channel sputtering and a thermal contact of high energy particles and discharge channel walls.
Features of the present invention, which believed to be patentable are set forth with particularity in the appended claims. The organization and operation manner of the invention, together with further objectives and advantages thereof, may be understood by reference to the following descriptions of specific embodiments taken in connection with accompanying drawings, in the several figures of which like reference numerals identify similar elements and in which:
Referring to
An end-Hall ion source shown in
Anode 13 made of a non-magnetic material but of good electric conductivity; it has a hollow conical shape and connected through a conducting plate 30 with an anode power supply (not shown); at an anode's exit, its area is substantially wider than at place where a working gas is applied.
Working gases such as Argon and other noble or reactive gases are applied to anode area 37 through a gas distributor/reflector 15 with holes 17.
Hot filament (usually a Tungsten or Tantalum wire) cathode 12 is placed between two cathode supports 18 and electrically isolated from an outer pole piece 19. Cathode supports 18 are connected by a solid insulated wiring (not shown here) through an ion source body 10 to a cathode power supply (not shown). Also, a cathode wiring can be placed outside a main body of an ion source. In many cases, instead of a hot filament there is utilized a hollow cathode, which in design is not so simple as a hot filament, but can provide higher emission currents and much longer lifetime. For end-Hall ion source, hot filament cathodes of 0.020 mil thickness at discharge currents, Id of about 5 A and discharge voltage, Vd of 150 V (typical operation parameters) can serve from 4 to 6 hours with Argon from 6 to 8 hours with Oxygen, and from 8 to 14 hours with Nitrogen as working gases.
A hollow cathode with the same anode discharge parameters (Id=5 A, Vd=150 V) usually operates on noble gases such as Argon (in technology), Xenon (in space, for thrusters) and can serve over 100 hours with Argon utilized in anode and hollow cathode. However, when a hollow cathode (on Argon) utilized with reactive gases such as Oxygen in anode area, its lifetime becomes shorter due to penetration of reactive gases into a hollow cathode area that becomes “poisoned” (oxidized) with reactive gases. Reactive gases sharply reduce emissive ability of a hollow cathode, usually made of Tantalum foil or other emissive materials. Lifetime of hollow cathodes working with reactive gases is usually a half of lifetime of work with noble gases.
An ion beam is developed in area between an anode 13 and cathode 12. Electrons (shown as circles with a sign −) supplied by a cathode are used for ionization of a working gas neutral particles (shown as circles with a sign o) and for neutralization of appeared ions (shown as circles with sign +). In result, neutralized plasma flow 11 exits from an ion source. A negative aspect of this Hall-current ion source is existence of strong plasma flow not only in an ion source exit direction, but also into opposite direction, into a gas distributor/reflector, 15. Such strong plasma flow leads into a severe damage of a gas distributor/reflector, 15 reducing its lifetime significantly. Besides a gas distributor/reflector damage, its sputtered particles fly back into a discharge channel's exit, into a vacuum chamber area leading into contamination of an etching/deposition process involving ion source.
Referring to
Working gas is applied through a system 22, 24 and through a gas distributor 27 that has a semi-spherical shape with holes 26 for a working gas and is placed at anode basis 13′ with an anode potential.
Magnet 16 develops magnetic field that decreases its strength in a direction to an ion source's exit and produces a negative gradient magnetic field in a discharge chamber. A magnetic field maximum value is at an anode bottom part where a gas distributor 27 is located.
Referring to
A discharge channel with external cylindrical wall made of a conducting material consists of three parts: upper part 46, anode 37, and bottom part 48. Parts 46 and 48 are under a floating potential. It means that an anode 47 is separated from conductive walls 46, 48 either by a dielectric material, or by a gap that prevents from high voltage potential to be applied to parts 46 and 48.
A permanent magnet or a magnetic coil 40 is placed in the central part of ion source's discharge channel and serves as a pole piece 44. A central pole piece 44 is isolated from discharge chamber by a dielectric material 42, and its top is protected by a graphite piece 49 for operation with noble gases such as Argon, or by a stainless steel piece 49 for operation with reactive gases such as Oxygen.
Magnetic screens 41 and 45 are placed outside a central magnet and serve for producing a positive magnetic gradient in a discharge channel.
A magnet placement in a protrusion is similar to regular closed drift ion sources, but this protrusion is extended not for a whole discharge channel length. Such a magnet placement can be called a hybrid placement of central magnetic pole, which is in about a middle of a discharge channel length. In closed drift ion sources a central magnetic pole is extended from gas distributing system a way up to an ion source end-side.
In alternate way, four magnets, 40′ are placed outside of a discharge channel as a continuation of a magnetic path, 43. A central magnet, 40 also can be utilized, because with all five magnets it is easy to regulate magnetic field in a discharge channel. In another approach of this invention, four magnets are utilized on external upper part of a magnetic path and a central protrusion made of magnetically soft material that serves as an internal pole. In this case, magnets are outside of a discharge channel and are less influenced by hot plasma of a discharge channel.
Value Rs is a radius of ion source from axis to external magnetic path;
Value Rex is a radius of discharge channel exit;
Value Rch is a radius of discharge channel, which is usually is less than Rex;
Value d1 is a discharge channel thickness;
Value Rsh is a radius of ion source's external magnetic screen;
Value rsh is a radius of internal magnetic pole;
Value rins is a radius of insulator separating internal magnetic pole and discharge chamber internal wall;
Value L1 is an ion source length from a magnetic screen base to an external magnetic pole;
Value L2 is a discharge channel length;
Value l1 is an internal magnetic screen length;
Value l2 is an external magnetic screen length;
Value l3 is a distance between anode and a source's base of a gas distributing system;
Value l4 is a central magnet's length; this distance is variable and, in case of utilizing a magnetically soft material as a central magnetic pole, can be a distance of a permanent magnet from a central dielectric surrounding a central magnetic pole;
Value l5 is a distance between magnetic poles;
Value h is anode thickness;
Value d2 is a magnetic shunt thickness;
Value d3 is a dielectric material thickness serving for protection of a central magnetic pole;
Value d4 is a distance between ion source external magnetic path and an external magnetic screen.
A variation of ratio of magnetic screens lengths, l1 and l2 and also a value of a distance between both magnetic poles, l5, or a height of an internal magnetic pole length, l3 and a placement of central magnet, l4 helps to establish necessary magnetic field distributions with a positive magnetic field gradient and a magnetic field strength.
In
A distance, l5 (
Internal and external magnetic screens, 41, 42 (
A maximum ratio of an ion beam current, Ib to a discharge current, Id, or Ib/Id≈0.8-0.9;
A maximum ratio of an ion beam mean energy, Eb to an applied potential, which is a discharge voltage, Vd, or Eb/Vd≈0.8-0.9;
A minimum mass flow of working gas, {dot over (m)}a.
The invented Hall-current ion source with a hybrid positioning of a central magnetic pole of a bout a half a distance between a gas distributing system and an external magnetic pole and with a high positive gradient of magnetic field helps to improve also electromagnetic focusing of plasma flow inside a discharge chamber from discharge chamber walls into a median part of a discharge chamber. In invented ion source maximum values of electric field are realized in a region of maximum values of magnetic field (
In conclusion, the invented Hall current ion source with high gradient of magnetic field has another definite advantage over end-Hall ion source. The so-called “flight” oscillations with a wide range of frequencies practically disappear. There are only large-scale low-frequency oscillations (about 10-25 kHz) providing transfer of electrons from an electron source (hot filament or hollow cathode) to anode, but not leading to motion of ions to discharge channel sides. A suppression of oscillations by high gradient of magnetic field and high values of mobility of electrons help to separate ionization and acceleration areas in the region of high magnetic gradient, to separate this region from anode to cathode, i.e. to realize a closure of electron current with minimum energy spent for transportation despite of significant distances between this region and cathode.
This application is based upon, and claims the benefit of Provisional Application No. 60/565,115 filed on Apr. 23, 2004.
| Number | Date | Country | |
|---|---|---|---|
| 60565115 | Apr 2004 | US |
