Apparatus, method and system for coating a substrate, in particular a superconducting tape conductor and coated superconducting tape conductor
12435409 · 2025-10-07
Assignee
Inventors
Cpc classification
C23C14/16
CHEMISTRY; METALLURGY
C23C14/26
CHEMISTRY; METALLURGY
C23C14/564
CHEMISTRY; METALLURGY
International classification
C23C14/56
CHEMISTRY; METALLURGY
B05C5/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present invention relates to a method for coating a substrate, in particular a superconducting tape conductor, in a vacuum environment, comprising: generating a metallic material in the gas phase, feeding the gaseous metallic material into an expansion chamber, wherein the expansion chamber is adapted to cause the gaseous metallic material to expand and be directed towards the substrate, and depositing the metallic material on at least part of the surface of the substrate. Further, the present invention relates to a coated superconducting tape conductor comprising: at least one superconducting layer and at least one metallic coating deposited on the tape conductor, wherein the thickness of the metallic coating is at least 1 m and varies over the width of the coated tape conductor by no more than 10%, preferably no more than 5%.
Claims
1. An apparatus for coating a substrate with a metallic coating, in a vacuum environment, wherein a background gas pressure in the vacuum environment is at most 1.Math.10.sup.1 Pascal, comprising: a gas source for generating a metallic material in the gas phase, wherein the vapor pressure of the metallic material in the gas source is at least 1.Math.10.sup.1 Pascal; wherein the gas source comprises an opening from which the gaseous metallic material flows into an expansion chamber installed between the gas source and a coating zone for the substrate; wherein the expansion chamber is formed as a divergent part of a Laval nozzle having an inlet opening directed to the gas source and an outlet opening directed towards the coating zone such that a flow of the gaseous metallic material is parallelized with respect to the substrate; wherein the expansion chamber is coated with an anti-adhesion coating and is actively cooled, and wherein a lamellar diaphragm is arranged between the gas source and the inlet opening of the expansion chamber.
2. The apparatus of claim 1, wherein the expansion chamber is adapted to convert at least a lateral momentum component of the particles of the gaseous metallic material into a longitudinal momentum component in the direction of the substrate; and/or wherein the expansion chamber is adapted to generate a supersonic flow of the gaseous metallic material in the direction of the substrate; and/or wherein the expansion chamber is arranged to direct the particles of the gaseous metallic material onto the substrate so that they impinge at an angle of no more than 15, preferably of no more than 10 and most preferably of no more than 5 to the surface normal of the substrate.
3. The apparatus of claim 1, wherein at least a part of the peripheral surface is treated such that absorption of thermal radiation is increased.
4. The apparatus of claim 1, wherein a ratio of a distance between the inlet opening and the substrate and a distance between the inlet opening and the outlet opening is at least 1.0, and at most 1.4, and/or wherein a ratio between a distance between the outlet and the inlet opening and a diameter of the outlet opening is at least 1.5.
5. The apparatus of claim 1, wherein the expansion chamber widens from the gas source towards the substrate in a conical or bell-shaped manner.
6. The apparatus of claim 1, wherein the expansion chamber is actively cooled by a liquid.
7. The apparatus of claim 1, wherein: the opening of the gas source comprises an opening diaphragm, the opening diaphragm having at least one fin; and/or the gas source and/or the opening diaphragm is made of tungsten, tantalum, molybdenum, carbon and/or heat-resistant ceramic.
8. The apparatus of claim 1, wherein the substrate is a flexible metal tape passing through the coating zone over the expansion chamber.
9. The apparatus of claim 8, wherein the substrate passes at least twice through the coating zone over the expansion chamber and comprises: an intermediate cooling device configured to cool the substrate after a first and before a second pass of the substrate through the coating zone; and/or at least one gas reflector arranged in or around the coating zone, the coating zone being configured to reflect particles of the metallic material in the direction of the substrate.
10. The apparatus of claim 9, wherein: at least part of said at least one gas reflector comprises an anti-adhesion coating; and/or at least part of said at least one gas reflector is configured to increase absorption of heat radiation; and/or at least part of the gas reflector is actively cooled.
11. The apparatus of claim 9, wherein the intermediate cooling device is located outside the coating zone and configured to keep a temperature of the substrate below 180 C., throughout an entire coating period.
12. The apparatus of claim 1, wherein the lamellar diaphragm is configured to reduce splashing of liquid metal droplets from the gas source.
Description
4. DESCRIPTION OF THE DRAWINGS
(1) Selected aspects of the present invention are described below with reference to the attached drawings. These drawings show:
(2)
(3)
(4)
(5)
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(7)
(8) The following reference signs are used in the drawings: 1 vacuum chamber/environment 2 evaporation source/gas source 3 water-cooled expansion chamber/expansion nozzle 4 moving substrate tape (foil) 5 coating zone 6 tape winder/winder arrangement 7a, 7b water-cooled rear reflector/gas reflector 8 intermediate cooling device; 10 diaphragm D distance between evaporation source and substrate tape L length of the expansion chamber/expansion nozzle O.sub.i inlet diameter of the expansion chamber O.sub.a outlet diameter of the expansion chamber
5. DETAILED DESCRIPTION OF SEVERAL EXEMPLARY EMBODIMENTS
(9) A first embodiment of the present invention is illustrated in
(10) In the upper area of the vacuum chamber 1, the substrate 4 to be coated is continuously moved through the coating zone 5 in the form of a flexible, thin tape or foil above the evaporation source 2. The tape can either come from an unwinding and rewinding device in the vacuum chamber or be continuously fed into the vacuum chamber, as described e.g. in DE 10 2009 052 873.
(11) In order to allow the metal vapor 9 to strike the substrate 4 in the area of coating zone 5 as vertically as possiblewithin an angular distribution of 15 to the substrate normaland thus avoid the column growth and high layer porosity described above, an expansion chamber 3 is installed between evaporation source 2 and coating zone 5.
(12) In the embodiment illustrated here, this expansion chamber 3 corresponds in its function to the divergent expansion part of a Laval nozzle, which is mainly used in the aerospace industry or in turbines to generate and bundle supersonic flows. The expansion chamber or Laval nozzle 3 has an inwardly concave bell shape and a round to slightly elliptical diameter. The lower inlet opening (diameter O.sub.i) is slightly wider than the outlet of the evaporation source 2 in order to thermally decouple it. The upper outlet opening (diameter O.sub.a) essentially determines the lateral dimension of coating zone 5.
(13) In some embodiments, the expansion chamber 3 with length L reaches close to the coating zone 5, so that as little metal vapor 9 as possible is laterally lost in the gap between expansion chamber 3 and substrate 4. The distance D-L is dimensioned in such a way that the substrate tape 4 does not come into contact with expansion chamber 3 even if it is slightly sagging and is also not contaminated, for example, by the anti-adhesion coating. Typically, the ratio D:L=1 to 1.4
(14) The geometric ratios of the illustrated expansion chamber or Laval nozzle 3 are as follows: The ratio between the outlet and inlet opening of the nozzle O.sub.a:O.sub.i is preferably greater than 1.5, particularly preferably greater than 2, and the ratio of the nozzle length to the outlet opening diameter is greater than L:O.sub.a=1.5. The effect of the Laval nozzle thus consists in a high separation rate from a parallel gas flow 9 and a very high material yield.
(15) However, the nozzle shapes (e.g. Laval nozzle) of the expansion chamber described here are only one possible way to achieve the directivity provided by the expansion chamber. Other forms and/or types of expansion chambers are also conceivable and are part of the present invention.
(16) In order to prevent the metal vapor 9 from adhering and condensing on the peripheral surface of expansion chamber 3, the latter is provided with an anti-adhesion coating. Suitable coatings preferably consist of long-chain PFPE compounds (trade name e.g. Fomblin). In order to keep the vapor pressure of the PFPE coating low and to dissipate the heat radiation from the gas source 2, the peripheral surface of expansion chamber 3 is actively cooled, e.g. by well heat-coupled pipes through which water flows. To prevent the peripheral surface of the expansion chamber 3 from reflecting the heat radiation from the gas source 2 onto the temperature-sensitive substrate 4, it is advisable to blacken its surface before applying the anti-adhesion coating so that it absorbs the heat radiation and dissipates it into the cooling water.
(17) With this arrangement, extremely high coating rates can be achieved on the substrate 4. For economic reasons, coating rates of more than 20 nm/s, preferably more than 50 nm/s and especially preferably more than 80 nm/s are targeted. The latter can be easily achieved with the present invention even with copper as coating material. Another important economic aspect is the material yield, i.e. the ratio of the amount of material deposited on the substrate 4 to the amount of material evaporated. With the normally undirected vacuum evaporation and with the usual distances D from source 2 to substrate 4 between 30 cm and 50 cm, the material yield is usually only in the low double-digit percentage range. With the present invention, material yields of more than 50%, preferably more than 70%, and especially preferably more than 80% can be achieved without any problems.
(18) A high coating rate in normal vacuum or high vacuum on thin films or tapes inevitably leads to a high energy input due to the released condensation heat, so that the substrate 4 can heat up very quickly. Many substrate materials, such as plastics or HTS tape conductors are temperature-sensitive and can be irreversibly damaged if a temperature threshold is exceeded. The maximum permissible temperature on the one hand and the heat capacity of the substrate 4 on the other therefore determine how much material can be deposited during a run through the coating zone 5.
(19) The coating rate is thus used to calculate the transport speed for the tape substrate 4. If thicker layers are required, the substrate 4 must be coated several times. This can be done by installing several evaporation units in succession, winding the tape several times through the system along its entire length, or by feeding the tape several times through the same coating zone 5 by means of a winding device 6. The latter is particularly suitable for tape that are narrower than the width of coating zone 5. Of course, all three approaches can also be combined with each other. In addition, for all multiple coatings, after passing through coating zone 5, an intermediate cooling device 8 can ensure that heat is removed from the strip substrate and the temperature is lowered to such an extent that a new coating can take place.
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(21) A metallization that is as dense, as smooth and as fully enveloping as possible with very good layer thickness homogeneity is desired. However, the superconducting cuprates tend to lose oxygen by diffusion when heated in a vacuum, which degrades their most important function, the critical current carrying capacity. The coating device in
(22) Outside the coating zone 5, each track runs through an intermediate cooling device 8. In this way, the substrate temperature can be reliably kept below a temperature of 180 C., preferably even below 150 C., throughout the entire coating period and with a layer thickness of more than 30 m of copper.
(23) A rear reflector 7a, 7b is also installed in the winder 6, which scatters the material flowing backwards through the gaps between the tracks back onto the substrate rear side at 7a or back onto the front side at 7b. The rear reflector is water-cooled in the same way as the peripheral surface of the Laval nozzle 3 and has a anti-adhesion coating. As a result, the material yield could be increased by approximately an additional 10%.
(24) In this case, the HTS tape conductor 4 was coated all around with copper. For this purpose, the tape was twisted as it was running back through the system, i.e. the back side was brought forward. The layer thicknesses on the two main surfaces and the edges of the tape 4 can be adjusted as required by the number of passages, the position of the upper reflector 7a, 7b and the width of the gaps between different winding tracks.
(25) In the manufacture of HTS tape conductors, metal layers of silver, copper, gold and tin, their alloys or a sequence of these metals are preferably used. Even though the process described here is not limited to these metals, they are the focus of the application. HTS tape conductors have therefore been coated with silver and copper with and without the process used in the invention and have been examined in detail. They have characteristic features that enable them to be directly distinguished from tape conductors coated by other metallization processes.
(26) For example, electroplated metal layers on tape conductors show a characteristic increase in layer thickness at the edges, which is inevitable due to the electrical field enhancement at the edge and the larger solid angle from which metal ions can accumulate.
(27)
(28) In the electron microscope image of the cut edge in
(29) In the best case, a thickness ratio of edge to center of 1.2-1.3 is observed for electroplated tape conductors, whereas this ratio is below 1.1, preferably even below 1.05 for the PVD metal layers produced here (see
(30) In comparison,
(31) The present invention thus makes it possible to achieve the high quality of PVD deposited metal layers even in the range of high coating rates and large metal layer thicknesses. The process is particularly suitable for the metallization of HTS tape conductors if between 1-30 m, preferably between 1-20 m and especially preferably between 3-20 m of metal layer thickness are applied on each side.
(32)
(33)
(34) In
(35) By contrast,
(36) In the cross-sectional preparation applied here by ion beam etching and electron microscopic observation (magnification 5000) perpendicular to the substrate surface, cavities or pores 440 make up less than 1% of the cross-sectional area and thus also of the volume of the metal layer 320. The thickness variation of the metal layer 320 measured on this cross-sectional preparation by ion beam etching is at least less than 10% in some embodiments even less than 5% of the average local layer thickness.
(37) The HTS tape conductors 300 produced by one of the embodiments of the present invention are also characterized by a very low area density of metal sputter 450 on the surface. During high rate evaporation, crucibles often experience turbulent processes in the molten metal and spattering due to the strong overheating. The resulting metal droplets 450 have a diameter of >10 m, can damage the substrate on impact due to local overheating or can be pressed into the underlying HTS layer 310 when the substrate is guided over rollers and break it. Splashing can be effectively avoided by using an evaporation source with a cover plate made of high-melting material such as W, Ta, Mo, C or ceramic. The metal layers 320 produced here are therefore also characterized by a very low surface density <0.1/cm.sup.2 of splashes and embedded particles 450 with an average diameter of more than 10 m.