KR980701342A - AN ION IMPLANTER WITH POST MASS SELECTION DECELERATION - Google Patents

Abstract

A decelerating lens assembly (9) disposed between the mass selective flight tube and the substrate holder is a first electrode (65) of substrate potential, a second electrode (60) of flight tube potential and two negative potentials to provide focus. and a field electrode 61 between them. The axial spacing in the beam direction between the first and second electrodes is smaller than the smallest transverse dimension of the field electrode. The decelerating lens assembly 9 is installed directly opposite the outside of the vacuum pump from the processing chamber to maximize the evacuation effect. A further screen electrode 56 is provided between the second electrode of the decelerating lens assembly and the outlet aperture of the mass selector. A perforated screen cylinder 54 is mounted on the flight tube with the second electrode of the lens assembly mounted on the lower beam end of the cylinder. The first electrode has a cylinder screen flange extending around the field electrode. An additional screen electrode is placed at the inlet to the electronic confinement tube of the PFS system.

Description

Ion implanters with mass selective deceleration

The ion implantation technique is a technique commonly used as one of the processes employed in the manufacture of integrated circuits, and is a technique for changing the electrical conductivity properties in a given region of a semiconductor material by doping a given region of a semiconductor material with a predetermined concentration of impurity atoms. . Such ion implantation techniques generally include generating a beam of desired ions and directing the ion beam towards a target substrate. The depth of the ion implantation depends, inter alia, on the energy of the ion beam at the substrate. Since ultra-large-scale integrated circuits (ULSIs) require increasing the density of devices on a single wafer and reducing the lateral dimensions of individual devices, for example, shallow junctions can be formed using low-energy ions of about 2-10 KeV The performance of the injector has become increasingly important. At the same time, it is also important to be able to process individual wafers in the shortest possible time during ion implantation on a mass production scale, which requires that the ion beam current be as large as possible. However, the requirement of a low energy beam is on top of that of a high current beam because it is very difficult to transport the ion beam at low energy and high current due to the space charge effect.

A known method to avoid beam expansion problems and loss of beam current is to transport an ion beam at a high energy and then decelerate it to the required low energy just before the beam strikes the substrate. For example, on pages 1741-1743 in Applied Physics Letters 53(18), published on October 31, 1988, described by S. N. HONG. et al., the depth of implantation by incorporating a decelerating lens system into the implantation chamber in which a fixed target substrate is maintained. A conventional ion implanter modified so that a cross-section can be observed is disclosed. In this ion implanter, a decelerating power supply is connected between the decelerating lens and the beam extraction power supply so that the final energy of the ions just before impacting the target is determined only by the decelerating potential generated by the decelerating power supply. Ions are extracted from the ion source with an energy of 35 KeV and passed through an Analyzer Magnet that analyzes the ions transported by the beam according to the mass of the ions. The mass analyzed beam is then passed through an X-Y scanner, which deflects the beam from the path between the magnet and the scanner to another path directed to the substrate. A decelerating lens and substrate biased at 34 kV decelerates the beam from 35 KeV to a fixed implant energy of 1 KeV. Therefore, ions are transported at high energy along the path between the ion source and the implantation chamber to minimize beam expansion and consequent current loss due to space charge effects. The energy of the ion beam is reduced only in front of the substrate before impact, so that the beam travels a very short distance with low energy, minimizing beam expansion.

One problem with methods of transporting an ion beam at relatively high energy and then decelerating the ion beam at a location very close to the substrate is that as the high energy beam passes, a portion of the ion beam undergoes a charge exchange process with the remaining gas atoms. Exchange Processes) to neutralize to become high-energy neutrons, and when these high-energy neutrons are directed to the substrate, they will pass through the decelerating lens without being decelerated. These high-energy neutrons penetrate deeper into the substrate than low-energy ions, which is particularly undesirable when forming shallow junctions. The effect of these high-energy neutrons on implantation depth will appear as a high-energy tail in the depth section as measured by secondary ion mass spectroscopy (SIMS).

A. H. Al-Bayati et al., Review of Scientific Instruments 65(8) published in August 1994, pages 2680-2692, disclose a mass spectrometric low-energy dual ion beam system for material studies. The device comprises a pair of Freeman sources, each connected to an extraction electrode, an analysis magnet for mass spectrometry of the ion beam, an additional magnet for focusing the beam, and an electrostatic force for scanning and gating the ion beam. It includes a deflector and a decelerating lens for reducing the energy of the ion beam and an ultra-high vacuum (UHV) deposition chamber containing a substrate mounted therein. The device is designed to allow material to be deposited as well as implanted into the substrate, and the ion arrival energy can be controlled from 5 to 10 KeV. The dual ion source together with the mass spectrometry magnet allows alternating layers of different materials to be deposited. The ultra-high vacuum deposition chamber houses facilities for Auger Electron Spectroscopy and deflected high-energy electron diffraction analysis of the deposited material. A secondary UHV chamber, connected to the deposition chamber by a vacuum fixture and sample transport device, houses a time-of-flight facility for dispersing and collecting low-energy electron diffraction and spectral devices. The deposition chamber is maintained at an extremely high vacuum to minimize contamination of the substrate surface during the deposition process. After the beam is mass analyzed, the secondary magnet refocuses the beam a few centimeters in front of the substrate. The ion beam is delivered with an energy of 10 KeV into the deposition chamber, in which the energy of the beam is reduced to the required value by a decelerating lens. Therefore, some of the beam ions will be converted to 10 KeV neutrons by a charge exchange process as the beam travels to the substrate. The number of neutrons that actually reach the substrate is reduced by the secondary magnet, which bends the ion beam from the beam trajectory of the primary magnet to prevent neutrons generated between the primary and secondary magnets from reaching the substrate. Neutron generation is further reduced by keeping the deposition chamber below an extremely high vacuum so that neutrons generated along a straight path between the primary and secondary magnets are minimized. The decelerating lens has a cup shape in which a lens-side portion is parallel to the beam axis and an end portion on which the substrate is mounted is perpendicular to the beam axis. In practice, the deceleration lens and substrate are kept at ground level, and the Flight Tube is negatively biased with respect to ground level. An additional electrode is positioned at the entrance of the decelerating lens, which accelerates electrons into the decelerating lens, resulting in a loss of beam neutralization and along the flight tube causing an increase in contaminants proportional to beam concentration in the flight tube. It is slightly negatively biased with respect to the flight tube to prevent a deceleration field extending from the rear. Both the entry aperture of the suppression electrode and the diameter of the cup electrode are significantly larger than the beam diameter.

Although the reported current densities are quite low, the on-target maximum ion current density achievable with this device is about 100 μA cm ^-2 . Since the target chamber is maintained below the UHV state of, for example, 10 ^-4 ∼10 ^-8 Pa (10 ^-6 ∼10 ^-10 mbar) and the source operates at a pressure of 1 Pa (10 ^-2 mbar), the beam line Different pumping stages are required accordingly, increasing the length of the beam line to nearly 4 m. Moreover, there is no way to neutralize surface charge formation as required to inject higher currents into the semiconductor substrate. Nuclear Instruments and Methods in Physics Research by DF Downey et al. B74 (1993), pages 160-169, disclose various methods of characterizing the performance of an ion implanter in implanting ions at low energy. As in the aforementioned documents, the ion beam is first transported at a relatively high energy and then decelerated to the required implantation energy. The specific implanter disclosed in each document includes a multi-electrode accelerator tube that distributes the deceleration voltage over the length of the accelerator tube rather than decelerating the beam to the energy required right in front of the substrate to step down the ion beam. A method of gradually decelerating an ion beam along an accelerating tube has been reported to improve beam transport by optimizing the beam current by minimizing the focusing effect of the tube. Such devices have also been reported to minimize neutron formation. In one investigation, implantation depth sections were studied as a function of beam extraction voltage to determine the extent to which neutrons affect depth sections at ion implantation energies between 3 and 10 KeV. Neutron peaks were readily observed in the depth section for higher extraction voltages, indicating that neutron contamination is an important factor in determining the energy the ion beam must transport before it is decelerated to the required energy. The maximum achievable beam current for a 5 KeV boron implant is on the order of 1 mA.

The present invention relates to an ion implanter for implanting ions into a substrate such as a semiconductor wafer in manufacturing an electronic device, and more particularly, to an ion implanter capable of economically processing a wafer with relatively low implantation energy.

1 is a plan view of an ion implanter according to an embodiment of the present invention.

2 is a plan view of an ion implanter according to a preferred embodiment.

FIG. 3 is an exploded view of the decelerating lens assembly and the lens blocking device of the embodiment shown in FIG. 2 ;

4 is a front view of the field electrode shown in FIGS. 2 and 3 ;

5 is a front view of the first aperture plate electrode shown in FIGS. 2 and 3 ;

It is an object of the present invention to provide an improved ion implanter capable of implanting ions at low energies and beam current densities with which semiconductor wafers are processed on a commercial scale.

An ion implanter operating at low implantation energy and having a substantial beam current is disclosed in a co-pending application claiming priority to German Patent 9522883.9. In such devices a decelerating lens assembly is provided between the flight tube and the substrate holder through which the beam is delivered with a transfer energy that is generally above the desired implantation energy. The decelerating lens assembly relates to the first electrode held at substantially substrate potential and relative to the first electrode to create a focused field at the first electrode to counteract the tendency of the beam ions to swell under the effect of space charge while the beam is in the decelerating field. at least two, and generally three, electrodes having adjacent field electrodes to be biased to a sufficient potential. Typically, for positive beam ions, the field electrode is biased to a negative potential relative to the first electrode of sufficient magnitude such that the field electrode is substantially negative in relation to the flight tube potential. Thus, the field electrode acts as an electron suppression electrode that prevents electrons of the beam in the flying tube from being pulled out of the beam by the decelerating field. However, the potential of the field electrode is only greater (in the negative direction) than required for the electron suppression method, so that the field electrode engaging the first electrode at the substrate potential can provide the necessary focusing effect.

When testing with a beam decelerating injector of the kind described above, the inventors have found that at energies above the transmission energy of the beam through the flight tube, there is a problem of high energy contamination of the substrate. The inventors have found that higher energy contamination arises from neutralized beam ions when the ions are temporarily accelerated by the field electrode before being decelerated between the field electrode and the first electrode at substrate potential. It is an object of embodiments of the present invention to reduce high energy pollution to negligible levels.

According to one aspect of the present invention, an ion implanter for implanting ions into a substrate and including an ion beam generator for generating an ion beam, a tube for transmitting the beam at a transfer energy, and a substrate into which the beam ions are to be implanted a substrate holder for supporting, a decelerating potential generator connected to apply a decelerating potential between the flight tube and the substrate holder to decelerate the beam ions to a desired implant energy, disposed between the flight tube and the substrate holder and substantially equal to the substrate potential A reduction lens comprising a first aperture plate electrode connected, a second aperture plate electrode having a beam aperture and substantially connected to a flight tube potential, and a field electrode disposed between and near each of the first and second aperture plate electrodes an assembly, a potential bias supply connected to bias the field electrode to have the same polarity with respect to each of the first and second electrodes, the electrodes being arranged and the bias passing through the first electrode The first and second electrodes are spaced apart in the beam direction by a distance smaller than the smallest transverse dimension of the beam aperture of the field electrode.

By keeping the beam direction distance between the first and second electrodes at a small value, the time during which the beam ions are temporarily accelerated by the field electrode to an energy greater than or equal to the energy transferred through the flight tube is kept to a minimum. As a result, the likelihood of beam ions experiencing electron exchange collisions with residual gas ions at these high energies is reduced. In the invention described above, the beam ions are temporarily accelerated only at a short distance between the slightly upper point of the second electrode and the midpoint of the field electrode, and then the beam is decelerated again. Since this distance is too short and the residence time of the beam ions in this area is very short, high energy contamination is reduced.

In a preferred embodiment, the ion implanter further comprises a mass selection aperture of the flight tube for selecting a desired mass of ions for delivery of the ion beam from the flight tube, wherein the mass selection aperture comprises an electric field generated below the beam direction. and an electromagnetic screen to the flying tube potential to protect the mass selective aperture from, the screen providing an exit aperture for the mass selected ion beam from the flying tube. The injector may then include at least one additional mass selection aperture comprising a flight tube potential aperture plate disposed between the second electrode and the outlet aperture.

This additional screen electrode prevents the field from the field electrode that can penetrate through the aperture of the second electrode extending beyond the location of this additional screen electrode considerably. It allows the distance between the field electrode and the mass selection hole to be kept to a minimum without an electric field passing through the mass selection hole and interfering with the mass selection method. Consequently, the time of flight of the beam ions at the transfer energy from the mass selective aperture towards the decelerating lens assembly is kept to a minimum such that the potential for neutral contamination of the target at the transfer energy is reduced. Also, by preventing the accelerating field generated by the field electrode from penetrating upwards along the beam, neutralizing electrons can be present in the beam over a greater distance towards the field electrode so that the tendency of the beam to swell through space charge effects is reduced. have.

Preferably, the implanter comprises a screen cylinder mounted on the flight tube at flight tube potential and extending toward the axis of the field electrode to contain the ion beam, the second aperture plate electrode being at an end of the screen cylinder adjacent the field electrode. installed and the screen cylinder is perforated to aid in evacuation of the inside of the cylinder. Then, an aperture plate forming the additional screen electrode may be disposed in the screen cylinder.

In a preferred embodiment, the implanter comprises a neutralizing aperture disposed between the substrate holder and the first electrode to provide a supply of low energy charged species of opposite polarity to the beam ions for neutralizing surface charge accumulation on the substrate during implantation. do. The injector then includes a neutralizing aperture screen electrode comprising an aperture plate disposed between the first electrode and the neutralizing aperture. In a preferred embodiment, the neutralizing aperture comprises an electron confinement tube that surrounds the direct front of the substrate holder, and the neutralizing aperture screen electrode may be installed directly on the upper end of the electron confinement tube.

This structure is very important for placing the field electrode as close as possible to the substrate while a neutral hole is placed between the two. Since the neutral hole operates by providing electrons for a flow of low energy charged species, typically a positive ion beam, it is very important to prevent an external electric field from penetrating into the neutral region. The presence of an additional screen electrode is made relatively short while allowing the first electrode to be placed very closely to the upper end of the electron confinement tube and providing adequate neutrality of the substrate to be implanted for the confinement tube itself.

Preferably, the first aperture plate electrode has a cylindrical screen flange extending axially from the first electrode towards the field electrode and the field electrode is mounted inside the flange such that the flange surrounds the outer periphery of the field electrode. This structure minimizes the tendency of the electric field from the field electrode to penetrate the substrate holder and the outer periphery of the first electrode towards the neutral aperture.

In a further preferred embodiment, the injector comprises a processing chamber comprising the substrate holder and having an evacuation port, and a vacuum pump connected to the evacuation port for emptying the processing chamber, the decelerating lens assembly being adapted to the vacuum pump. It is disposed directly in front of the discharge port. This is another feature that is very important for reducing neutral contamination in the energy that is temporarily accelerated as the beam ions pass through the field electrode. By disposing the decelerating lens assembly when the beam ions are temporarily accelerated, the residual gas pressure in this region of the decelerating lens assembly, directly in front of the emission port relative to the vacuum pump, is minimized, thereby minimizing the possibility of electron exchange collisions in this region.

The aperture plate electrode comprises a plate extending transversely in the beam direction and comprising an aperture for the beam, the axial size of the aperture (in the beam direction) being negligible compared to the smallest transverse size of the aperture.

1 , an ion implanter 1 includes an ion beam generator 3 for generating an ion beam, a magnet adjacent to the ion beam generator 5 for spatially analyzing the ion beam according to their mass, and the analysis magnet 5 ), an ion selector 7 that selects the type of ions to be implanted into the target substrate and rejects other ions in the spatially analyzed beam from the magnet, adjacent to the ion selector 7 An electrode assembly (9) arranged to control the final energy of the ion beam before implantation, a support or holder (11) spaced apart from the electrode assembly (9) and supporting a target substrate (12) into which the beam ions are to be implanted; and an electron generator 13 disposed between the electrode assembly 9 and the substrate support 11 and introducing electrons into the ion beam in the vicinity of the target surface to neutralize the beam and the wafer surface. An ion beam collector 14 is positioned under the substrate support 11 which functions as a beam stopper and an ion current detector for Dosimetry Measurement.

More specifically, the ion beam generator 3 comprises an ion source 15 comprising an arcuate chamber 17 having an exit aperture 19 formed thereon. A pair of extraction electrodes 21 and 23 are spaced apart from the exit aperture 19 to extract ions from the arcuate chamber to form an ion beam 25 . The extraction electrode 21 closest to the exit aperture 19 of the arcuate chamber functions as a suppression electrode to prevent electrons in front of the beam generator from flowing into the arcuate chamber. The flight tube 27 is positioned between two poles (only one is shown) of the mass spectrometry magnet 5 , receives the ion beam from the beam generator 3 , and the flight tube 27 and the ion source ( 15) Controls the transport energy of the ion beam while passing between the poles of the magnet 5, which is determined by the potential difference between them. In this particular embodiment, the magnetic field strength of the analysis magnet and the energy of the ion beam passing through the magnet are selected such that ions of suitable mass are deflected by approximately 90°, the flight tube 27 is configured accordingly, and the analysis magnet outlet Aperture 31 is substantially perpendicular to magnet entry aperture 29 . The ion selector 7 includes a series of discrete elements 35 , 39 , 41 , 43 spaced apart from each other along the beamline 45 to form a series of apertures, the series of apertures The perchers combine with each other to select the correct mass of ions to be implanted into the target substrate while rejecting other spatially resolved ions passing through the analysis magnet 5 . In this particular embodiment, the ion selector 7 comprises a plate electrode 35 that rejects most of the unsourced ion species emitted from the magnet, and a pair of configuration forming a variable width mass spectrometry slit that allows only the selected ion species to pass through. elements 39 , 41 and a further component 43 limiting the height of the ion beam. However, the number of mass spectrometry components and their composition may vary.

The ion selector assembly is housed in a chamber 47 that forms part of the flight tube 27 and is disposed between the magnet and the electrode assembly 9 . A flight tube 27 containing a mass spectrometry chamber 47 provides a means for transporting the beam from the ion beam generator to the electrode assembly 9 . The mass spectrometry chamber wall 49 constitutes a cone 51 extending in the direction of the beamline and forming a generally conical cover, and a plate electrode disposed transverse to the beamline adjacent the cone 51 and through which the beam It comprises an intersection (53) forming a passable aperture (55), the aperture (55) adjoining the final component (43) of the ion selector (7). The cross section 53 provides an electrostatic screen that shields the ion selector 7 from the electric field generated underneath the ion selector, as will be described in detail below.

In this particular embodiment, a vacuum port 57 is formed in the chamber wall 49 adjacent the assay magnet 5 and is connected to a vacuum pump 59 for evacuating the chamber 47 . This vacuum port may be omitted in other embodiments.

The outlet aperture 55 of the mass spectrometry chamber 47 and the electrode assembly 9 to reduce the penetration of the electric field from the electrode assembly 9 into the mass spectrometry chamber 47 through the outlet aperture 55 . A blocking assembly 52 is installed between them. The blocking assembly 52 includes a conical electrode 54 and a field forming electrode 56 . The conical electrode 54 is arranged coaxially with the outlet aperture 55 of the mass spectrometry chamber, and has one end 58 adjacent to the intersection (or front end 53) of the mass spectrometry chamber wall 49 this intersection. connected to the unit 53 . The conical electrode 54 extends forward of the mass spectrometry chamber 47 and has an inwardly extending radiating flange 60 formed adjacent or at the other end of the conical electrode 54 to provide additional shielding, the outlet An aperture 62 is formed.

The field forming electrode 56, which may not be used in some cases, comprises a circular plate having an aperture 64 formed in the center. Field forming electrode 56 is mounted within conical electrode 54 and supported by conical electrode 54, located approximately halfway between the ends of conical electrode 54 (which may vary), and beamline 45 ) intersect. The aperture 64 is preferably rectangular or square, and in one embodiment may be smoothly cut outward toward the electrode assembly 9 . In this embodiment, the aperture is square and has a width of about 60 mm. Conical electrode 54 and field forming electrode 56 may be constructed of graphite or other suitable material.

An electrode assembly (9) for controlling the implantation energy of the ion beam is positioned directly past the blocking assembly (52) and includes a field or ring electrode (61) and an aperture plate electrode (65). The field electrode 61 is generally circularly symmetric and defines an aperture 63 adjacent the exit aperture 64 of the blocking assembly 52 and substantially coaxial with the exit aperture 64 . A plate electrode 65 is generally disposed intersecting the beamline 45 and forms an additional aperture 67 through which the ion beam may pass. This additional aperture 67 is located adjacent to the field electrode aperture 63 . In this embodiment, the diameters of the field electrode aperture and the plate electrode aperture are about 90 mm and 80 mm, respectively. The field electrode and plate electrode may be constructed of graphite or other suitable material.

In this embodiment, the electron generator 13 includes a Plasma Flood System that introduces low-energy electrons into the ion beam in the vicinity of the substrate. The plasma flood system includes a guide or tube 69 through which the ion beam passes from the plate electrode aperture 67 to the target substrate 12, and the tube 69 directs electrons from the plasma flood system to the ion beam. Keep a portion of the ion beam between the plate electrode aperture and the wafer from the stray electric field. The aperture plate electrode 70 is disposed adjacent to the aperture plate electrode of the deceleration assembly at the upper end of the confinement tube to further block the inside of the confinement tube from the electric field generated by the field electrode 61 .

The apertures 63, 67 formed in the field electrode 61 and the plate electrode 65 are configured to be larger than the beam cross-sectional area at these apertures so that the ion beam can pass straight through the electrodes 61, 65 without clipping. . For a given mass of ions and the distance between each of these apertures 63, 67 and the analyte magnet 5, the beam cross-sectional area depends on factors such as the ion beam generator and magnet optics, the analytical power of the magnet and the width of the mass analysis slit. Each of these elements can be used to control the beam cross-section at the deceleration device and the target substrate.

In this embodiment, the ion implanter includes a source voltage supply 71 for biasing the ion source, a suppression electrode voltage supply 73 for biasing the suppression electrode 21, a flight tube 27, and mass spectrometry. A flight tube voltage supply 75 for biasing the chamber 47 , the blocking assembly 52 and the other extraction electrode 23 , and a field electrode voltage supply for biasing the field electrode 61 of the electrode assembly 9 . It further includes a device 77 and a plasma flood voltage supply 79 for biasing the electron confinement electrode 69 and the aperture blocking plate electrode 70 . In this embodiment, the aperture plate electrode 65 of the decelerating lens, the target substrate holder 11 and the substrate 12 are kept at ground potential, thereby facilitating the processing of the target substrate, simplifying the target support assembly, It serves as a convenient reference potential for the other electrodes.

A method of operating an ion implanter to implant ions with low energy will be described with reference to specific examples of use for illustration.

The ion implantation energy is determined by the potential difference between the substrate 12 and the ion source 15 . When the substrate is held at ground potential, the ion source voltage supply 71 is positively biased with respect to the ground potential by an amount corresponding to the required ion implantation energy. For example, for a 2 KeV implant, the ion source voltage supply is biased at +2 kV. The transport energy of the ion beam through the analysis magnet 5 and mass spectrometry chamber 47, also referred to as the extraction energy of the ion beam, is determined by the potential difference between the ion source 15 and the flight tube, the transfer potential being the flight tube voltage. Controlled by the feeder 75 . Thus, for example, to transport an ion beam through the flight tube at an energy of 10 KeV, the flight tube is biased at -10 kV relative to the ions itself or -8 kV relative to the ground potential. The ion beam is carried with almost constant energy through the analysis magnet, and the different ion types in the ion beam are spatially analyzed by the magnet according to their mass. The spatially analyzed beam is passed into a mass spectrometry chamber, in which the beam first passes through a preformed aperture formed by the plate electrode 35 closest to the analysis magnet 5 . The plate electrode 35 acts as a first stage filter for the course, i.e., spatially resolved beam, and blocks some of the spatially resolved ion species not required for implantation. Second and third components 39 , 41 spaced apart from the analysis magnet 5 and arranged coaxially with each other along the beamline are mass spectrometry slits of variable width for selecting the type of ions to be implanted from the filtered beam. 42, this variable width mass spectrometry slit 42 can be changed transverse to the beamline.

As an example, the spatially resolved beam remaining on the analysis magnet upon implantation of boron will contain BF ₃ , BF ₂ , BF, B and F ions, which boron ions may contain one of the isotopes of boron, B ₁₀ and B ₁₁ . will include Therefore, in the case of B ₁₁ implantation, the preforming component 35 and the mass spectrometry components 39 , 41 will filter out all ion types except for B ₁₁ . As the beam crosses the mass spectrometry chamber 47, the energy of the beam remains constant, such as 10 KeV in this example. The 10 KeV mass analyzed beam 46 passes from the blocking assembly 52 to the electrode assembly 9 through the outlet aperture 55 of the mass spectrometry chamber 47 .

A potential smaller than the potential of the mass spectrometry chamber 47 is applied to the field electrode 61 . The magnitude of the potential applied to the field electrode 61 is sufficient to form an electrostatic focusing field in the region of the final aperture 67 of the grounded plate electrode 65 . The inventors of the present invention are concerned with the potential of the plate electrode 65 in forming the required focusing field in the final lens aperture 67 to keep the beam ions in the beam between the final lens aperture 67 and the target substrate. It was concluded that a potential between 5 kV and -30 kV, preferably a potential of -25 kV, is sufficient. When the flight tube and the mass spectrometry chamber are -8 kV, the field electrode 61 is biased to a potential lower than the potential of the flight tube, and acts to prevent electrons in the mass spectrometry region from being attracted to the plate electrode 65. This destroys space charge neutralization within this region and results in beam expansion and current loss.

In this example, when the mass analyzed beam 46 approaches the field electrode 61, the beam is spatially Accelerates faster than the energy formed. The beam passes through the field electrode aperture 63 , and then decelerates to approximately the required injection energy at the cap between the field electrode aperture 63 and the final aperture 67 . At the same time, in the area between the mass spectrometry chamber exit aperture 55 and the field electrode 61, the area between the field electrode 61 and the plate electrode 65 of the decelerating lens, and the area immediately following the ion beam A Net Focusing Force is applied.

The ion beam is then passed into the region between the final lens aperture 67 and the target substrate. In this area, the ion beam is delivered to the substrate with approximately the required implantation energy. At this time, the expansion of the low-speed beam is minimized by flooding the beam with low-energy electrons by the plasma flood system 13 . The plasma flood system also minimizes the surface charge of the target substrate during ion implantation, while simultaneously reducing the potential of the ion beam to minimize the extent to which the beam expands before reaching the substrate.

The reduction gear of the present invention exhibits significant advantages over prior art systems. First, the decelerating device of the present invention can neutralize the ion beam after the beam is decelerated, which is not possible in the prior art system. Since the deceleration field accelerates electrons away from the beam ions when the ions are decelerated in the deceleration field, it is not easy to space charge neutralize the ion beam at the substrate by using a system that introduces electrons into the beam, thereby making it difficult for the electron injector to efficiency is very low. In the case of a plasma flood system in which the ion beam is neutralized by low-energy electrons contained in a stable plasma, a strong electric field from the decelerating lens will prevent this plasma from forming. In the present arrangement, the plasma flood system is arranged under the deceleration device and is isolated from the deceleration device, so that the plasma flood system is not exposed to the strong deceleration field. The critical conditions for forming the required low energy plasma are thereby achieved and maintained.

Second, the loss of space charge neutralization is essential when the ion beam passes through a strong decelerating field. Thus, in prior art devices, the decelerating lens is positioned as close to the substrate as possible so that the beam travels the minimum distance without space charge neutralization. In contrast, in the present device, the deceleration device is located above the substrate, between the neutralizer and the mass spectrometry chamber, and applies a focusing force to the ion beam during deceleration in this region where space charge neutralization of the ion beam is markedly lacking. arranged to suppress beam expansion. By constructing the final lens aperture 67 of the decelerating electrode 65 at least 15% larger than the beam cross-sectional area at the final aperture, and by creating a sufficiently high potential difference between the field electrode 61 and the plate electrode 65 between these electrodes. By applying the ion beam in the region in a decelerating direction, very high current densities at the target substrate can be achieved. For example, for low-energy beams of 2 KeV and 10 KeV, the on-target ion current densities are 70 μA cm ^-2 and 250 μA cm ^-2 , respectively, and for the ultra-low energy (1 KeV) of 200 eV and 500 eV, the on-target ion current densities are respectively. The ion current densities are 5.0 μA cm ^-2 and 20.0 μA cm ^-2 , respectively.

The aperture 63 of the field electrode 61 is also larger than the beam cross-sectional area therein so that all the beam current can be transmitted. In this embodiment, the aperture size is almost constant along the beamline, and the depth of the aperture in the direction of the beamline is relatively small.

The aperture 64 of the field forming electrode 56 and the outlet electrode 55 of the mass spectrometry chamber also have a size greater than the beam cross-sectional area therein, thereby resulting in the mass spectrometry slit 42 and the beam height forming aperture 44 ), the transmitted beam current flows into the deceleration region. Therefore, all apertures after the beam height forming aperture 44 through which the beam passes until it reaches the substrate, each aperture so that all the beam current from the beam height forming component 43 can be transmitted to the substrate. larger than the cross-sectional area of the beam in the perch. This is because, for example, a lower potential is applied to the electrode or to limit the width and shape of the beam at the substrate or to provide an impedance to the gas flowing through the aperture so that a differential pressure can be maintained across the aperture. This is a significant difference from prior art devices in which the size of the aperture is limited along the beam line in order to bring the inner surface of the aperture as close to the ion beam as possible.

If the ratio of the cross-sectional area of the beam in the aperture to the area of the predetermined aperture is referred to as the filling rate, the filling rate of the connection electrode 61 and the lens plate electrode 65 is less than 85% for all kinds of dopant ions. it is preferable A fill factor of less than 85% was found to allow a higher beam current density to be transported along the beamline. The electric field generated by the electrodes intersecting the beamline interferes less with ions and electrons transported in the periphery of the ion beam than when the inner surface of the electrode aperture is close to the ion beam. It turns out that installing the right gap can reduce the beam expansion due to the space charge effect. Therefore, by making the aperture size of the electrode under the mass spectrometry slit larger than the beam cross-section therein, the beam expansion can be reduced and the beam current density increased. Moreover, contamination of the beam by graphite, metallic materials or other materials that would otherwise be sputtered from the surface of the electrode is significantly reduced by making the aperture larger than the beam cross-section by preventing the beam ions from striking the electrode.

It has been found that at energies above the transport energy, the problem of Energy Contamination of the slowed low-energy ion beam may appear, and furthermore, this contamination occurs before the beam ions are decelerated in the region between the field electrode and the lens plate electrode before the field electrode. It turned out to result from the neutralization of the beam ions when temporarily accelerated by

Figure 2 shows a plan view of a preferred embodiment of a beam transport apparatus for low energy ion implantation that substantially eliminates such high energy contamination of the ion beam. In FIG. 2 , the beam spots of the ion beam generator, most of the mass spectrometry magnets and the ion implanter are omitted for simplicity of illustration, but they are the same as those shown in FIG. 1 and described above. In FIG. 2 , the device comprises a flight tube 27 comprising a mass spectrometry chamber 47 containing a selector 7 for selecting the desired implanted ions in a mass analyzed beam from a magnet 5 , the mass A decelerating lens assembly 9 positioned at the lower portion of the analysis chamber 47 to decelerate the ion beam, a beam neutralizing device disposed adjacent to a lower portion of the decelerating lens assembly, and a location adjacent to the lower portion of the beam neutralizing device 13 . A target substrate holder 11 is provided.

The ion selector 7 comprises a pair of components 39, forming a plate electrode 35 that rejects most of the unsourced ion species from the magnet and a variable width mass spectrometry slit 42 that passes only the selected ion species. 41). The mass spectrometry chamber wall 49 includes a portion 51 extending in the direction of the beamline and forming a generally conical cover, and a front end 53 constituting a plate electrode extending across the beamline. The front end 53 defines an aperture 55 adjacent the mass spectrometry slit through which the ion beam can pass and which forms the components 39 , 41 .

2 to 5 , the decelerating lens assembly is located adjacent to the beam neutralizing device 13 and is a first aperture plate electrode 65 for controlling the injection energy, a lower portion of the first aperture plate electrode 65 . A second aperture plate electrode (60) positioned and positioned between and adjacent to the first and second aperture plate electrodes (65, 60) and passing through the first aperture plate electrode (65) It includes a field electrode 61 that provides a focused field to the ions. In order to provide further shielding of the ion selector 7 from the electric field generated underneath the ion selector 7 , in particular from the field generated at the field electrode 61 , a further aperture plate electrode 56 is provided in the second It is positioned under the aperture plate electrode 60 . In this particular embodiment, an additional blocking electrode 56 is mounted on a stand-off 66 extending back from the second aperture plate electrode 60 .

A blocking cylinder 54 is mounted on the flight tube 27 and extends along the axis towards the field electrode 61 . A second aperture plate electrode (60) is mounted on the front end of a blocking cylinder (54), which surrounds an additional blocking electrode (56). In this embodiment, the blocking cylinder 54 , the second aperture plate electrode 60 and the additional aperture plate electrode 56 are all electrically connected to the flight tube 27 .

In the decelerating lens assembly, the beam aperture formed in both the field electrode 61 and the first aperture electrode 65 is rectangular, and the widths W _f and W _d of the apertures in each case are greater than the heights h _f and h _d . short. The aperture formed in the first aperture electrode 65 is smaller than the field electrode 61 in height and width to improve the blocking of the beam neutralizing device 13 from the electric field emitted by the field electrode 61 . In one embodiment, the beam aperture 63 of the field electrode has a diameter of about 86 x 100 mm and the beam aperture 67 of the first aperture plate electrode has a diameter of about 60 x 86 mm.

The fractional decrease in the aperture width between the field electrode and the first aperture plate electrode 65 is greater than the fractional decrease in the aperture height between the field electrode and the first aperture plate electrode. In this embodiment, the beam has a pencil-shaped cross-sectional topography so that when the ion beam passes through the mass spectrometry slit, it extends laterally at a faster rate than it does vertically due to space charge effects. By further reducing the width between the apertures, the connecting force is enhanced laterally across the ion beam, reducing the higher expansion rate in this direction. The beam aperture structure of the first aperture plate electrode 65 and the field electrode 61 increases the focusing ability of the decelerating lens, thereby increasing the focusing capability of the first and second aperture electrodes necessary to provide proper focusing of the beam. The potential of the field electrode can be reduced, and thus, the energy obtained in an instant by the ions above the transport energy immediately after passing through the field electrode aperture can be reduced. As a result, it reduces the energy of the fast neutrons generated in this region by charge exchange with the remaining gas atoms.

In FIG. 2 , the first and second aperture plate electrodes 65 , 60 are spaced apart in the beam direction by a distance a less than the smallest transverse dimension W _f (in this case the width) of the beam aperture of the field electrode 61 . do. This is another important feature of a preferred decelerating lens assembly. The short distance between the first and second aperture plate electrodes 65 and 60 allows the time that ions have energy above their transport energy when accelerated by the field electrode 61 can be kept to a minimum. Consequently, the likelihood of these higher-energy beam ions to undergo charge exchange with residual gas atoms is reduced with a decrease in the number of high-energy neutrons formed in this region.

The field electrode 61 is generally conical and has a length in the beam direction of at least 10% of the smallest transverse dimension of the beam aperture (aperture width in this case). In this particular embodiment, the axial length is about 23% of the aperture width. This structure improves the focusing effect while allowing the aperture of the field electrode 61 to be larger than the expanded beam width when the beam passes through the field electrode.

A conical flange 89 extends along the axis from the first aperture plate electrode 65 towards the field electrode 61 . The conical flange (89) and the first aperture plate electrode (65) form a shield around the ion beam and the field electrode (61) to form a potential difference applied between the field electrode (61) and the first aperture plate electrode (65). constrains the electric field established by It blocks the ion beam from stray electric fields appearing in the processing chamber 81 that may result.

The field electrode 61 is positioned inside the flange 89 so that the flange surrounds the outer periphery of the field electrode 61 . In this embodiment, the field electrode 61 is mounted within the conical blocking flange 89 and is attached to the conical blocking flange 89 via a plurality of stand-offs 68 positioned radially around the circumference of the field electrode 61 . supported by The field electrode and first aperture plate electrode assembly are mounted on the processing chamber wall 85 by a plurality of stand-offs 72 . In this embodiment, the conical blocking flange 89 is provided so that the gap 95 between the field electrode and the second aperture intercostal space can easily access and communicate directly with the surrounding space within the processing chamber 81. 61) to a minimum distance exceeding the rear surface. This open structure allows the area between the field electrode 61 and the second aperture plate electrode 60 to be more easily evacuated, thereby reducing the residual gas pressure in this area and otherwise avoiding high energy contamination. Minimize the generation of fast neutrons that may cause

A vacuum port 83 is formed in the wall of the processing chamber 81 to allow the processing chamber to be in a vacuum state. The opening of the vacuum port is relatively large and extends parallel to the beam line in the region of the target substrate to collect sputtered particles from the substrate during implantation. The decelerating lens assembly, particularly the area between the field electrode 61 and the second aperture plate electrode 60, is located directly in front of the vacuum exhaust port 83 of the processing chamber 81, thereby making the interior of the lens more efficient. As a result, it can be in a vacuum state, which has the effect of further reducing the high-energy contamination of the ion beam and the generation of high-speed neutrons.

Therefore, the decelerating lens assembly shown in Fig. 2 allows the space within the lens to be effectively vacuumed to minimize the residual gas pressure and injection energy inside the lens, particularly the generation of neutrons in this region above the flight tube transport energy. is composed

In this embodiment, the beam neutralizing apparatus 13 has a plasma flood system including a plasma source 14 for introducing electrons into an ion beam adjacent to the surface of the target substrate. The plasma flood system includes a low and low confinement tube 69 that surrounds the ion beam and is positioned immediately proximate the front surface of the substrate holder 11 . A blocking electrode 70 for blocking the plasma flood system from the electric field generated in the decelerating lens assembly is mounted on the upper end of the confinement tube 69 and is located adjacent to the first aperture plate electrode 65 . This structure allows the lens assembly 9 to be positioned as close to the target substrate 12 as possible while the neutralizing device 13 is still positioned between the lens assembly 9 and the target substrate 12 . The additional blocking electrode 70 has a beam opening 74 approximately the same size as the beam opening 67 in the first aperture plate electrode 65, and prevents the extra electric field from penetrating into the neutralization region. The additional blocking electrode 70 allows the first aperture electrode 65 to be positioned very close to the top of the electron confinement tube 69, and is configured to be relatively short with respect to the confinement electrode 69 itself, so that it is still injected. Provides adequate neutralization of the substrate 12 being subjected to.

FIG. 2 also shows an example of how the beamwidth cross-section changes along the beamline as the beam passes from the analysis magnet 5 via the decelerating lens assembly to the target substrate 12 . Magnet optics directs the ion beam to a narrow focus at the mass spectrometry slit 42 formed by the mass spectrometry components 39 , 41 . As the ion beam passes through the mass analysis slit 42 and the beam apertures 55 and 58 of the mass analysis chamber 47 and the additional blocking plate electrode 56, respectively, the beam width gradually expands. When the beam approaches the beam aperture 62 of the second aperture plate electrode 60, the electric field between the field electrode 61 and the second aperture plate electrode 60 first applies a focusing force to the ion beam It reduces the rate of expansion and subsequently applies a defocusing force to the ion beam when the beam approaches the field electrode 61 and accelerates rapidly above its transport energy. However, the electric field between the field electrode 61 and the second aperture plate electrode 60 causes the ion beam to have a low velocity and thus exert a focusing force in the region closer to the beam aperture of the second aperture plate electrode 60 . The more time you receive, the more time you spend, so you apply total focus.

When the ion beam passes through the field electrode 61 into the gap between the field electrode 61 and the first aperture plate electrode 65, the beam is decelerated to the required implantation energy, and the electric field between these electrodes is A strong focusing force is applied to the ion beam, whereby the beam width is narrowed to pass through the beam aperture 67 of the first aperture plate electrode 65 .

Finally, the ion beam passes through the electron confinement tube 69 of the neutralization device 13 while the beam width is dispersed to a negligible degree, narrows the beam aperture 74 of the blocking plate electrode 70, and passes to the substrate. .

Another important feature of the present invention is that the ion implanter is arranged such that the path length between the mass spectrometry magnet and the decelerating device can be shortened significantly compared to prior art implanters. As described above, this configuration not only makes the implanter smaller, but also reduces the generation of high-speed neutrons that cause energy contamination of the low-energy ion beam. It is inevitable that high-speed neutrons capable of impinging on the substrate can be generated anywhere on top of the decelerating electrode positioned in a straight line with the substrate. Neutrons generated in the region between the first aperture plate electrode of the decelerating lens and the substrate will have an energy equal to or less than the injection energy, and thus will not result in high energy contamination. In order to shorten the critical path length through which fast neutrons can be produced, the flight tube underneath the analysis magnet is shortened as much as possible by including only the mass analysis assembly between the magnet and the decelerating lens assembly. The unique decelerating lens assembly may allow the distance between the first apertured plate electrode and the end of the mass spectrometry assembly to be shortened as much as possible even if the structure becomes somewhat complicated. 1 and 2 , the first aperture plate electrode 65 , which controls the final energy of the ion beam, is positioned as close as possible to the exit aperture 55 of the mass spectrometry chamber 47 . . The decelerating device controls the shape of the beam in the deceleration region when the apertures of both the field electrode 61 and the final aperture 67 are larger than the beam cross-section therein and passes through the final aperture 67 of the lens assembly to the target substrate. Only one additional electrode, the field electrode 61, is positioned between the first aperture plate electrode 65 and the end 53 of the mass spectrometry chamber 47 to achieve nearly 100% transfer of the beam current to the includes

the end of the mass spectrometry chamber 47 to incorporate blocking means extending along the beamline to reduce the penetration of the electric field from the focusing electrode 61 through the mass spectrometry chamber exit aperture 55 to an acceptable level. It is necessary to include a finite gap between 53 and the field electrode 61 . It is evident that it is impossible to provide sufficient blocking by only reducing the size of the exit aperture 55 without the edge of the exit aperture 55 clipping the beam. In order to sufficiently block the electric field without clipping the beam, a shield must be included around the ion beam that extends beyond the finite length of the beam line between the field electrode 61 and the end of the mass spectrometry chamber. In the embodiment shown in FIGS. 1 and 2 , the blocking means comprises a common conical electrode 54 which is an extension of the flight tube and a further aperture plate electrode 56 . For a given size of the mass spectrometry chamber outlet aperture 55, it is preferred that the blocking length be configured as short as possible. It has been found that the cutoff length provided by the conical shield can be significantly shortened by placing an additional aperture plate electrode 56 between the field electrode 61 and the front end 53 of the mass spectrometry chamber. Reducing the blocking length not only contributes to a shortening of the overall beam path length between the magnet and the first aperture plate electrode of the decelerating lens, but also minimizes the distance at which the ions are instantaneously accelerated beyond the extraction energy, thereby in Reduce energy pollution.

Another advantage of reducing the path length of the ion beam between the magnet and the first aperture plate electrode of the decelerating lens is that the beam width due to space charge expansion at the first aperture plate electrode becomes smaller for longer path lengths. that it will be That is, as the path length becomes shorter, the beam expansion can be further suppressed. This unique offers a significant advantage, allowing the inno beam to be transported with low energy, whereby the difference between the injection energy and the transport energy can be reduced. Therefore, the ion implanter can be controlled so that any neutrons generated on top of the first aperture plate electrode have an energy somewhat greater than the implantation energy and penetrate into the target substrate slightly deeper than the implanted ions. Moreover, reducing the beam path length between the ion beam generator and the target substrate reduces the number of neutralization reactions, thereby reducing the loss of ion current during neutron generation. 1 and 2, the length of the injector from the magnet to the end of the processing chamber is about 2 m, the distance between the magnet outlet aperture 31 and the target substrate 12 is about 90 cm, The distance between the magnet outlet aperture 31 and the first aperture plate electrode 65 is approximately 60 cm. High-energy neutrons, which may cause energy contamination of the ion beam in the substrate, may form in the upper region of the exit aperture 31 of the analysis magnet 5 . The length of this region, which is straight to the substrate, has the advantage that it can be shortened by increasing the magnetic field strength of the analysis magnet so that the ion beam bends in a tighter arc. A miniature beamline device comprising a reduction device between the analysis magnet and the target substrate has a magnetic arc radius

can be reduced significantly, with a radius of 23 cm in the embodiment shown in FIGS. 1 and 2 . This can shorten the overall beam path length from the ion beam generator to the substrate, thereby reducing the size of the beam cross section at the substrate and reducing the loss of beam current from the ion beam generator to the substrate.

The ion implanter may also be used such that the final implantation energy is greater than the energy with which the beam is transported through the analysis magnet (referred to as an acceleration mode). In this case, referring to FIGS. 1 and 2 , the ion beam is transported with a predetermined energy through the mass analysis magnet 5 and the mass analysis chamber 47 , and then as a final implantation energy using the electrode assembly 9 . accelerated For example, in the case of an implantation energy of 80 KeV, the ion source potential is set to 80 KeV with respect to the first aperture plate electrode 65 and the target substrate 11 both at ground potential. The blocking device comprising the extraction electrode 23 and the flight tube and the second aperture plate electrode 60 are all set in relation to the potential of the ion source which determines the transport energy of the ion beam along the flight tube. For example, for an extraction energy of 30 KeV, the potential of the flight tube with respect to ground potential is set to +50 kV. For the case where the implantation energy is lower than the extraction energy (referred to as a deceleration or deceleration mode), the field electrode 61 establishes an intermediate focusing force in the region of the final aperture 67 of the lens assembly to direct the ion beam to this region. It is biased again to a lower potential than the first aperture plate electrode 65 to focus on . For example, the field electrode 61 would be biased at -25 kV with respect to the first aperture plate electrode. When the ion beam passes through the mass spectrometry chamber exit aperture 55, the beam is first accelerated to an energy above the implantation energy by the field between the end 53 of the mass spectrometry chamber 47 and the field electrode 61, It is then decelerated to a final implantation energy of 80 KeV in the region between the conical electrode 61 and the plate electrode 65 . Both the high-energy beam and the low-energy beam can be successfully transmitted by operating the ion implanter in acceleration mode and deceleration mode, respectively, with little change in the potential difference applied between the first aperture plate electrode 65 and the conical electrode 61 . It turned out that there is Therefore, when the potential difference is set between these electrodes, no additional potential difference adjustment is required, which has the advantage that switching between low-energy injection and high-energy injection can be simplified.

To successfully transport an ion beam, the pressure of the gas through which the beam passes must be high enough to provide a sufficient number of electrons to neutralize the beam. Electrons are created when the ion beam interacts with residual gas atoms and are trapped in a potential well formed by the electrostatic charge of negative ions. Gas pressures of 10 ^-3 to 10 ^-4 Pa (10 ^-5 to 10 ^-4 mbar) are often used in most commercial ion implanters. However, the decelerating electrode arrangement of the present invention allows the residual gas pressure in the decelerating region to be pumped with lower energy when the aperture formed in both the first aperture plate electrode and the field electrode is larger than the beam cross-section. Therefore, the gas in the deceleration zone can be pumped through the aperture at a higher rate, thereby lowering the gas pressure in this zone. Moreover, when a field electrode is used as the only other electrode required in addition to the first aperture plate electrode to decelerate the ion beam and transmit it to the substrate at a remote location, the electrode assembly is very compact and can be effectively evacuated. It can be easily configured as a structure. Reducing the residual gas pressure in the deceleration zone has the advantage that the number of interactions between the beam ions and residual gas atoms is reduced, thereby reducing the loss of ion current and reducing energy contamination of the ion beam. It has been found that the residual gas pressure can be reduced to at least 10 ^-6 mbar without significantly increasing the proportion of beam dispersion. However, reducing the pressure by an order of magnitude results in at least an order of magnitude reduction in energy pollution. It has the advantage that the focusing action of the decelerating device can compensate for any rate of increase in beam dispersion in this area, thereby reducing the gas pressure.

Referring back to FIG. 2 , the deceleration reds assembly 9 , the plasma flood system 13 and the target substrate support 11 are all located adjacent to the mass spectrometry chamber 47 and at the front end 53 of the mass spectrometry chamber. It is housed in a processing chamber 81 in communication with the mass spectrometry chamber through an aperture 55 formed therein. A blocking cylinder 52 between the front end wall 53 of the mass spectrometry chamber 47 and the second aperture plate electrode 60 blocks the ion beam from the stray electric field in the processing chamber 81, and this portion of the beamline It is penetrated so that it can be effectively vacuumed. A vacuum evacuation port 83 is formed in the wall 85 of the processing chamber 81 and is connected to a vacuum pump 86 (shown in FIG. 1 ). The vacuum pump is preferably a cryogenic pump capable of pumping at a rate of about 10,000 liters per second. The mass spectrometry chamber wall 49 is electrically insulated from the processing chamber wall by an electrically insulating chamber 87 that forms part of the wall of the processing chamber 81 .

The mass spectrometry chamber 47 forms part of the critical path length between the analysis magnet 5 and the first aperture plate electrode 65 where fast neutrons can be produced which may result in energy contamination of the ion beam. Although a finite residual gas pressure is required within the mass spectrometry chamber to provide space charge neutralization of the ion beam, the pressure is reduced to a significant extent beyond the extent that the ion beam is sufficiently neutralized to reduce the number of fast neutrons generated in this region. pressure exists. The advantage of making the critical path length as short as possible is that a higher rate of expansion of the ion beam can be allowed, making good space charge neutralization less important. A feature of the present invention exploits the tolerance for higher beam inflation created by a shortened critical path length by reducing the pressure within the mass spectrometry chamber. Although a vacuum evacuation port 57 is formed in the wall 49 of the mass spectrometer 47 and connected to a vacuum pump 59 (shown in FIG. Limited by the length of the chamber, it must be shortened as much as possible. The mass spectrometry chamber communicates with the processing chamber 81 through an outlet aperture 55 formed in the end portion 53 and to some extent the mass spectrometry chamber is evacuated by the processing chamber 81 through this aperture. Although possible, the size of this aperture is limited in cases where the electric field generated in the field electrode 61 hardly penetrates into the mass spectrometry chamber 47 . The mass spectrometry chamber may be evacuated by the process chamber vacuum pump 86 via the process chamber vacuum port 83 to allow the pressure in the mass spectrometry chamber 47 to be reduced significantly below previously possible levels. A plurality of additional apertures 103 are formed in the dividing wall 51 between the mass spectrometry chamber 47 and the processing chamber 81 to provide additional outlets in the space. In this embodiment the aperture is formed in a portion of the mass spectrometry chamber that generally extends in the direction of the beamline, and in other embodiments may be formed in another portion of the wall and a portion of the wall may extend across the beamline. have. The size and spacing of the apertures are carefully chosen to preserve the blocking of the ion beam provided by the splitting wall and not to be disturbed by discontinuities in the equipotential surface in the splitting wall that could result in loss of beam current. In one embodiment, the aperture is formed as an elongated slot, but may be square, rectangular, circular, rhombic or other suitable shape.

The combination of the relatively large aperture of the decelerating lens assembly and the aperture formed between the mass spectrometry chamber and the processing chamber allows the critical beam path length between the analysis magnet and the decelerating electrode 65 to pump to a pressure much lower than previously possible pressures. This has the advantage that this is achieved without increasing the length of the mass spectrometry chamber to accommodate additional vacuum pumps or larger vacuum ports. Indeed, the additional evacuation aperture between the mass spectrometry chamber 47 and the processing chamber 81 will provide results to the extent that a separate mass spec chamber vacuum pump is not required, thereby simplifying the injector and reducing cost. . Moreover, a short beam path length may allow the overall volume to be vacuumed to be significantly reduced. One embodiment of the present invention includes a wafer support assembly comprising a plurality of individual support plates positioned about and supported by a hub rotatable through a plurality of radially extending spokes. FIG. 2 shows such a support plate in which a support plate 107 supporting a target substrate such as, for example, a semiconductor wafer 12 is connected to a spoke 109 . The wafer support assembly can be moved in a direction intersecting the beamline so that the wafer can be scanned across the beam.

A further advantage of the present device is that the focusing action of the deceleration device can be used to reduce the processing time of a single wafer, thereby increasing the wafer throughput of the ion implanter. For a low-energy ion beam of typically 10 KeV or less, there is no requirement to use a relatively wide beam to prevent energy density problems such as excessive charging and heating of the target substrate. It can be reduced below the beamwidth of the energy beam. The focusing action of the deceleration device can be used to reduce the on-target beamwidth to reduce the distance the rotating wafer support assembly must be scanned so that the wafer is uniformly doped by the ion beam. This can reduce the processing time for a given batch of wafers, thereby increasing the throughput of the implantation apparatus.

In another embodiment of the ion implanter, one or more aperture plate electrodes and field electrodes or blocking electrodes of the processing chamber are at least therein to provide an additional outlet through which any sealed volume can be pumped to a lower pressure. One additional aperture may be formed. The electrode may include an arrangement of such apertures or may include a mesh. The dividing wall between the mass spectrometry chamber and the processing chamber may also include a mesh so that a lower pressure can be achieved within the mass spectrometry chamber. However, the size of the mesh should be large enough to provide adequate blocking of the ion beam.

In other embodiments, the first aperture plate electrode and the focusing electrode or field electrode may have a suitable shape and structure, each of which may include one or more individual electrodes. For example, the decelerating electrode may include a conical or ring-shaped electrode. In other embodiments, the decelerating electrode and the plasma flood guide tube may comprise single electrodes or be electrically connected to each other. In another embodiment, the deceleration electrode may be arranged to be biased to a potential different from that of the target substrate.

In other embodiments, the focusing positive or field electrode may comprise an extension of the flight tube and may be substantially the flight tube potential. In this embodiment, the potential difference between the flight tube and the first aperture plate electrode or deceleration electrode must be sufficient to apply a focusing force to the ion beam in the deceleration region. An additional electrode, located on top of the deceleration electrode, located inside the flight tube, and biased to a potential lower than that of the flight tube, should be installed on the deceleration electrode to prevent loss of electrons. Modified embodiments of the present invention described above will be apparent to those skilled in the art.

Additional features described herein are claimed in a co-pending patent application in the name of the present applicant, filed on the same date as this patent application and claiming priority to British Patent Application No. 9522883.9.

Claims (19)

An implanter for inserting ions into a substrate, comprising: an ion beam generator for generating an ion beam; a flight tube for delivering the beam with transfer energy; a substrate holder for supporting a substrate into which beam ions are to be implanted; a first aperture plate electrode disposed between the flight tube and the substrate holder and connected substantially to the substrate potential, a second aperture plate electrode substantially connected to the flight tube potential and the beam aperture to decelerate the beam ions to a desired implantation energy. a deceleration lens assembly having a field electrode disposed between and near each of said first and second aperture plate electrodes; and a potential bias supply connected to bias the field electrode to have the same polarity with respect to each of the first and second electrodes, the electrode being arranged and the biasing beam passing through the first electrode to provide a focused field for ions, wherein the first and second electrodes are spaced apart in the beam direction by a distance less than the smallest transverse dimension of the beam aperture of the field residual pole. 2. The flight tube of claim 1, further comprising a mass selection aperture in the flight tube to select ions of a desired mass for transmission of the ion beam from the flight tube, wherein the mass selection aperture selects a mass from an electric field generated below the beam direction. and an electric field screen at the flight tube potential to screen the aperture, the screen providing an exit aperture for the mass selective ion beam from the flight tube. 3. The ion implanter of claim 2, comprising at least one additional mass selective aperture screen electrode comprising an aperture plate at the flight tube potential disposed between the second electrode and the exhaust aperture. 4. A screen according to claim 2 or 3, comprising a screen cylinder mounted on a flight tube of flight tube potential and extending in an axis toward the electric field to contain an ion beam, wherein the second aperture plate electrode is adjacent to the field electrode. An ion implanter installed at the end of the cylinder and wherein the screen cylinder is pierced to aid in emptying the cylinder interior. 5. The ion implanter according to claim 3, wherein an aperture plate forming the additional screen electrode is disposed in the screen cylinder. 6 . The method of claim 1 , between the substrate holder and the first electrode to provide a supply of low energy charged species of opposite polarity to the beam ions for neutralizing surface charge accumulation on the substrate during implantation. An ion implanter comprising a neutralization hole disposed in the ion implanter. 7. The ion implanter of claim 6 including a neutralizing aperture screen electrode having an aperture plate disposed between the first electrode and the neutralizing aperture. 8. The field electrode according to claim 6 or 7, wherein the first aperture plate electrode has a cylinder screen flange extending axially from the first electrode towards the field electrode and the field electrode is flanged such that the flange surrounds the outer periphery of the field electrode. Ion implanter, characterized in that installed inside. 9. The decelerating lens assembly according to any one of claims 1 to 8, comprising a processing chamber including the substrate holder and having an evacuation port, and a vacuum pump connected to the evacuation port for emptying the processing chamber. is disposed directly in front of the discharge port with respect to the vacuum pump. An ion implanter for implanting ions into a substrate, comprising: An ion beam generator for generating an ion beam, a flight tube for delivering the beam with transfer energy, a processing chamber having an emission port, a vacuum pump connected to the emission port for emptying the processing chamber, a substrate into which beam ions are to be implanted a substrate holder in the processing chamber for supporting a decelerating lens assembly comprising a first aperture plate electrode substantially connected and a field electrode disposed adjacent and over the beam direction relative to the first electrode, and biasing the field electrode relative to the first electrode and a potential bias supply connected to said electrode arranged and said bias to provide a focused field for beam ions passing through said first electrode, said decelerating lens assembly comprising said discharge port to a vacuum pump. An ion implanter, characterized in that it is disposed directly in front of the. An implanter for implanting ions into a substrate, comprising: An ion beam generator for generating an ion beam, a flying tube for delivering the beam with transfer energy, a substrate holder for supporting a substrate into which the beam ions are to be implanted, a flying tube and a substrate for decelerating the beam ions to a desired implantation energy. a decelerating potential generator connected to apply a decelerating potential between the holders, a first aperture plate electrode disposed between the flight tube and the substrate holder and substantially connected to the substrate potential, and adjacent to the beam direction relative to the first electrode; a decelerating lens assembly comprising a field electrode disposed thereon, and a potential bias supply coupled to bias the field electrode relative to the first electrode, wherein the electrode is arranged and the bias biases the first electrode. to provide a focused field for beam ions passing therethrough, the decelerating lens assembly comprising a second aperture plate electrode substantially connected to the flying tube potential and disposed adjacent and overlying the beam direction relative to the field electrode further comprising: a mass selection aperture in the flight tube adapted to select a desired mass of ions for delivery of the ion beam from the flight tube; a screen, wherein the screen provides an emission aperture for the mass selected ion beam from the flight tube, wherein at least one additional mass selection aperture for screening an electrode is disposed between the second electrode and the emission aperture. An ion implanter comprising a dislocation aperture plate. An ion implanter for implanting ions into a substrate, comprising: An ion beam generator for generating an ion beam, a flying tube for delivering the beam with transfer energy, a substrate holder for supporting a substrate into which the beam ions are to be implanted, a flying tube and a substrate for decelerating the beam ions to a desired implantation energy. a decelerating potential generator connected to apply a triple potential between the holders, a first aperture plate disposed between the flight tube and the substrate holder and substantially connected to the substrate potential, and adjacent to and above the beam direction with respect to the first electrode a decelerating lens assembly including a field electrode disposed thereon, a potential bias supply connected to bias the field electrode relative to the first electrode, the electrode being arranged and the bias passing through the first electrode for providing a focused field for beam ions, the deceleration reds assembly further comprising a second aperture plate electrode disposed substantially over and adjacent to the beam direction relative to the field electrode and connected to the flight tube potential; the mass selection aperture in the flight tube for selecting a desired mass of ions for transfer of the ions from the flight tube comprises an electric field screen of flight tube potential to screen the mass selection aperture from an electric field generated below the beam direction; wherein the screen provides an exit aperture for the mass selective ion beam from the flight tube and includes a screen cylinder mounted on the flight tube at flight tube potential to contain the ion beam and extending axially towards the field electrode; A two-hole plate electrode is installed on the end of the screen cylinder adjacent to the field electrode and the screen cylinder is penetrated to empty the inside of the cylinder. An ion implanter for implanting ions into a substrate, comprising: An ion beam generator for generating an ion beam, a flying tube for delivering the beam with a transfer energy, a substrate holder for supporting a substrate into which the beam ions are to be implanted, a flying tube and a substrate for decelerating the beam ions to a desired implantation energy. a decelerating potential generator connected to apply a decelerating potential between the holders, a first aperture plate disposed between the flight tube and the substrate holder and substantially connected to the substrate potential, and adjacent to and above the beam direction with respect to the first electrode a decelerating lens assembly comprising a field electrode disposed thereon, a potential bias supply connected to bias the field electrode relative to the first electrode, wherein the electrode is arranged and the bias passes through the first electrode between the substrate holder and the first electrode to provide a focused field for the beam ions to be removed, and to provide a polarized, low energy charged species supply for the beam ions to neutralize surface charge build-up on the substrate during implantation. wherein the first aperture plate electrode has a cylinder screen flange extending accumulatively from the first electrode towards the field electrode, the field electrode being disposed within the flange such that the flange surrounds the outer perimeter of the field electrode. An ion implanter, characterized in that it is installed. An implanter for implanting ions into a substrate, comprising: An ion beam generator for generating an ion beam, a flying tube for delivering the beam with a transfer energy, a substrate holder for supporting a substrate into which the beam ions are to be implanted, a flying tube and a substrate for decelerating the beam ions to a desired implantation energy. a decelerating potential generator connected to apply a decelerating potential between the holders, a first aperture plate electrode disposed between the flight tube and the substrate holder and substantially connected to the substrate potential, and adjacent the beam direction relative to the first electrode and a decelerating lens assembly comprising a field electrode disposed thereon, a potential bias supply connected to bias the field electrode relative to the first electrode, the electrode being arranged and the bias being applied through the first electrode between the substrate holder and the first electrode to provide a focused field for passing beam ions and to provide a low energy charged species supply of opposite polarity to the beam ions for neutralizing surface charge accumulation on the substrate during implantation. An ion implanter comprising a neutralizing device disposed in the ion implanter, wherein the neutralizing device for screening the electrode includes a hole plate disposed between the first electrode and the neutralizing device. 15. The method according to any one of claims 1 to 14, a beam forming aperture disposed between the field electrode and the ion beam generator effective to define a width of the beam in at least one direction perpendicular to the beam direction as it passes through the beam field electrode and the first electrode; The field electrode has an aperture that is larger in the one direction than the beam width in the one direction as the beam passes through the field electrode and the first electrode allows the beam ions to deflect the ions out of the beam. and having an aperture sufficiently large in said one direction than the width of the beam in said one direction when a beam passes through said first electrode avoiding high radiative field components around the aperture of said electrode. 16. The method according to any one of claims 1 to 15, and a beam aperture of the first electrode is smaller than a beam aperture of the field electrode for at least one direction perpendicular to the beam direction. 17. The method according to any one of claims 1 to 16, and the potential bias supply is arranged to provide a bias such that the field electrode is at a negative potential of at least 5 Kv with respect to the flight tube. 18. An ion implanter according to any one of the preceding claims, characterized in that the field electrode is cylindrical with an axis in the beam direction and has at least 10% of the smallest transverse dimension of the cylinder. 19. The method according to any one of claims 1 to 18, a magnet for spatially decomposing beam ions according to mass, a processing chamber including the substrate holder and having an emission port, a first vacuum pump connected to the emission port for emptying the processing chamber, between the processing chamber and the magnet. a mass selection chamber, a second vacuum pump connected to empty the mass selection chamber, an aperture for passing a beam from the mass selection chamber to the processing chamber and the mass selection chamber and the mass selection chamber to improve emptying of one or the other of the chamber An ion implanter having at least one additional aperture between the processing chambers.