The invention relates to a magnet configuration according to the preamble of patent claim 1.
In a sputter installation a plasma is generated in vacuo in a sputter chamber. Positive ions of the plasma are attracted by the negative potential of a cathode, which is provided with a so-called target. The positive ions impinge on this target and knock out small particles, which can become deposited on a substrate. Knocking out these particles is referred to as “sputtering”. The plasma is comprised of gases which, in the case of non-reactive sputtering, can be inert gases, for example argon. In reactive sputtering, for example, oxygen is utilized alone or together with an inert gas.
To improve the sputter effect, magnets are employed in the proximity of the target, whose magnetic field maintains the plasma on the target. The magnetic field forces the electrons in the plasma into a specific path. The electrons ionize the neutral gas, for example argon, on this path and generate positive ions. These ions are much heavier than the electrons and are practically not affected at all. Instead, they fall onto the target, which acts as a negative electrode or cathode, and sputter it. Ionizations substantially take place where the magnetic field vector extends parallel to the target surface. Here the plasma is densest and therefore the target is here most strongly eroded. In the following the plasma path determined by the magnetic field will also be referred to as a plasma tube.
If planar magnet systems are utilized, in which a bar magnet of a first polarity is surrounded by a rectangular magnet of a second polarity, a rectangular erosion track results between these magnets, with the corners of the rectangle being rounded off.
Rotating cylindrical targets are also already known, which rotate about a stationary magnet aggregate (DE 41 17 518 A1). Hereby the rectangular erosion track reaches all sites of the circumference of the target. At the narrow sides of the erosion rectangle a depression forms in the target. The target is eroded uniformly, except for those sites, at which the narrow sides of the plasma rectangle generated an undesirable depression.
Furthermore, magnet configurations are known, in which in the case of a stationary target the erosion track does not form a rectangle but rather a hexagon (WO 96/21750). This hexagon is comprised of two large sides, which are adjoined by triangles on the right and on the left. Instead of adjoining triangles, parabolas or semi-ellipses can also be provided. The changed erosion contours are attained through the corresponding disposition of the magnets. The magnets can herein be disposed stationarily, while the target rotates about them; but it is also possible for the target to be stationary while the magnets rotate.
However, a sputter arrangement is also known, in which by means of a drive a magnet configuration is moved parallel to the planar surface of the target (U.S. Pat. No. 5,873,989). The movement of the magnet configuration is a back and forth movement, i.e. at the ends of the target it reverses its direction of movement. The plasma forms a plasma track, which has the form of an elongated oval. The longitudinal direction of this oval extends perpendicularly to the direction of movement. In the case of this magnet configuration depressions are also formed close to both ends of the target, which are greater than the erosions in the remaining area of the target. To utilize the target better, the magnet configuration is rotated by 90 degrees after a certain length of time, such that now two further depressions are formed perpendicularly to the depressions previously formed. In the case of this linear arrangement, recessed tracks are consequently generated at the margin of the target in the same way as with a rotation configuration.
The objective of the invention is to avoid erosion depressions at the margin of the target in a linear sputter installation, whose magnets move relative to the target.
This objective is attained through the characteristics of patent claims 1 or 2.
Consequently, the invention relates to a sputter arrangement with a magnetron and a target, with the magnetron and the target being movable relative to one another. The magnetron comprises a magnet system, which forms a quasi-rectangular plasma tube, whose two long sides have a distance C from one another. If target and magnet system are moved relative to one another by a path corresponding to distance C, the magnet system is laid out such that the width at the end of the plasma tube is less or equal to the diameter of the plasma tube. However, if the path of the relative movement is less than C, the magnet system is laid out such that the width d of the ends of the plasma tube is less or equal to twice the diameter of the plasma tube.
Embodiment examples of the invention are depicted in the drawing and will be described in further detail in the following. In the drawing depict:
The magnet system 1′ depicted on the right side is the same magnet system 1 shown on the left side. It only assumes a different position, which is indicated by means of dashed reference numbers. The segment A denotes that segment by which the magnet system 1 is shifted above the target 2 to the right. In many cases the section A is selected such that it corresponds to the section C, i.e. the distance between two long parts 16, 17 of the plasma tube 9.
If the movement to the right corresponds to segment C, the magnetic field is moved such that in the course of the movement each part of the rear target surface is covered once by the plasma. In the case of a large-area target 2 this can be realized with several adjacently disposed magnet systems 1. The direction of movement is in general reversed after segment C has been traversed. The erosion depth on the target 2 can in this case be calculated by integration of the erosion rate along the drive path. As an approximation the erosion can also be estimated by the width d of an arm 16, 17 of plasma tube 9, which migrates over a point on the target surface.
In this case at the upper and lower ends of the plasma tube depressions or erosion channels 11, 12 do not occur if B≦d, provided the plasma density is constant.
In a second embodiment 1 segment A, by which the magnet system 1 is moved, is greater than the distance C between the arms 16, 17. The magnetic field of the magnet system 1 is moved such that during the movement each part of the target surface is covered once by both perpendicular arms of the plasma tube 9. This can again be realized with several magnet systems 1, which are disposed one next to the other. The direction of movement is reversed when the outer margin of the target is reached. The erosion depth can also be calculated in this case through integration of the erosion rate along the drive path. The erosion can be approximately estimated by the sum of all widths d of the plasma tube, which migrate over a point on the target surface. At the upper and lower ends 18, 19 of the plasma tube 9 erosion trenches 11, 12 are not generated only if the width B of the lower or upper arm 19, 18 of the plasma tube 9 corresponds maximally to twice the width d of the plasma tube in the vertical arm, thus if B≦2 d applies, provided the plasma density is constant.
In
The entire arrangement shown in
The inner magnet 38 has different diameters in the longitudinal direction, with the central portion having the larger diameter m and the outer parts having smaller diameters n, o.
The inner magnet is formed by a bar magnet 52, which comprises at its ends two reductions by steps 53, 54 or 55, 56, with small diameters.
In
In
As far as the determination of segments B, d and C is concerned, the plasma width B is not determined directly. B and d can therefore only be defined via the magnetic field, since it determines the plasma confinement. The plasma burns essentially at those sites at which the field lines, and consequently the magnetic field vector, extend parallel to the target surface. At these sites the component, perpendicular with respect to the target surface, of the magnetic field vector is zero. These sites can be determined experimentally by measuring the field strength on the target surface. The distance C between two regions 16, 17 of a plasma tube is therefore defined by the distance of the positions on the target surface in the direction of the relative movement, at which the perpendicular component of the field vector becomes zero. The diameter d of the plasma tube 9 is correspondingly defined as the distance of the positions on the target surface in the direction of the relative movement, at which the magnetic field vector forms an angle of 20° with the target surface. This corresponds to the sites at which the field lines intersect the target surface at an angle of 20°. The positions are located in the center of the longitudinal direction of target 2, thus approximately where the distance symbol for C is located in
Consequently, the values B, d and C can be determined precisely through measurements and/or calculations.
Number | Date | Country | Kind |
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10 2004 007 813.0 | Feb 2004 | DE | national |