CA1163231A - Reactive plating method and product - Google Patents
Reactive plating method and productInfo
- Publication number
- CA1163231A CA1163231A CA000382527A CA382527A CA1163231A CA 1163231 A CA1163231 A CA 1163231A CA 000382527 A CA000382527 A CA 000382527A CA 382527 A CA382527 A CA 382527A CA 1163231 A CA1163231 A CA 1163231A
- Authority
- CA
- Canada
- Prior art keywords
- substrate
- coating
- zinc
- vacuum chamber
- gas
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/32—Gas-filled discharge tubes
- H01J37/32009—Arrangements for generation of plasma specially adapted for examination or treatment of objects, e.g. plasma sources
- H01J37/32018—Glow discharge
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/0021—Reactive sputtering or evaporation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
Abstract
ABSTRACT OF THE DISCLOSURE
A method is disclosed for the reactive plating of substrates to produce transparent conducting films and photoactive coatings. Reactive gases at low pressures are introduced into a vacuum chamber having a partial vacuum therein. A substrate located in the vacuum chamber is subjected to a glow discharge in the partial vacuum. A
coating material, such as zinc or silicon is vaporized in the vacuum chamber to react with the gases, with the resulting compound being deposited on the substrate by the effect of the glow discharge. The power in the glow discharge and the partial pressures of the vaporized coating material and gases introduced into the vacuum chamber can all be controlled separately to vary the stoichiometric ratios and the properties of the coatings.
The electrode geometry is arranged and the operation maintained such that the power density distribution in the discharge is fixed and controlled.
A method is disclosed for the reactive plating of substrates to produce transparent conducting films and photoactive coatings. Reactive gases at low pressures are introduced into a vacuum chamber having a partial vacuum therein. A substrate located in the vacuum chamber is subjected to a glow discharge in the partial vacuum. A
coating material, such as zinc or silicon is vaporized in the vacuum chamber to react with the gases, with the resulting compound being deposited on the substrate by the effect of the glow discharge. The power in the glow discharge and the partial pressures of the vaporized coating material and gases introduced into the vacuum chamber can all be controlled separately to vary the stoichiometric ratios and the properties of the coatings.
The electrode geometry is arranged and the operation maintained such that the power density distribution in the discharge is fixed and controlled.
Description
~ 163231 This invention relates to the coating or plating of substrates using glow discharge and thermal vaporization in a vacuum chamber.
In the past, various techniques have been used to S deposit a film or coating on a substrate located in a vacuum chamber. One technique simply is to thermally vaporize or evaporate a metal, permitting the vapor to condense and be deposited on the substrate. Another method is referred to as chemical vapor deposition wherein different gases are introduced into the vacuum chamber to react and form a compound on the substrate. Yet another prior art method is referred to as sputtering. In this method, a vacuum or gas filled discharge tube has a cathode that is disintegrated by bombardment, so that the cathode material is vaporized and deposited on the substrate.
A variation of these methods is shown in United States Patent ~o. 2,501~563 issued to W.H. Colbert. In this patent, vacuum evaporation is used to vaporize and deposit a metal substrate. Gas is then introduced into the vacuum ~hamber to oxidize the metal and form a metallic compound coating. Another variation of the prior art ~.
methods is shown in United States Patent No. 3,318,790 issued to B.G. Carbajal III, et al. In this patent, a gaseous organic source material is introduced into a vacuum chamber and a glow discharge is established to polymerize S the source material and deposit same on the substrate.
A difficulty with the prior art methods is that they generally do not permit individual and independent control of each parameter of the process and hence do not permit the fabrication of "tailor-made" compounds having predetermined atom ratios and hence predetermined properties.
In the present invention, a glow discharge in a reacting gas is provided in a vacuum chamber and a coating material is vaporized therein to be deposited on a substrate. Independent adjustment of each of the parameters of the process is possible allowing for control of the reaction and deposition of the coating material,~and thus the properties of the film deposited on the substrate.
According to one aspect of the invention, there is provided a method of coating a substrate comprising the steps of providing a vacuum chamber communicating with a surface of the substrate to be coated. A glow discharge is produced in the vacuum chamber in contact with the substrate surface. Coating material is vaporized in the chamber, and a gas is introduced into the vacuum chamber to react with the vaporized coating material forming a compound to be deposited on the substrate by the glow discharge.
~6~231 ~, According to another aspect of the invention, a coated substrate is provided comprising a substrate having a coating produced by the method described above.
According to yet another aspect of the invention, there is provided a coated subs1:rate comprising a substrate having a coating deposited thereon by glow discharge in a partial vacuum, the coating consisting of a non-stoichiometric compound produced by reacting a vaporized metal and a gas.
A preferred embodiment of the invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Figure l is a vertical diagrammatic sectional view of a vacuum chamber used to perform the method of the lS present invention;
Figure 2 is a perspective view from above and from the front showing the upper internal components of the vacuum chamber of Figure l;
Figure 3 i8 a perspective view from above and from the front showing the lower internal components of the vacuum chamber of Figure l; and Figure 4 is a perspective view, partly broken away, taken along lines 4-4 of Figure 3.
The following description of a preferred embodiment is given in reference to a laboratory test and demonstration unit for carrying out the preferred method to produce the preferred coated substrate. Specific values are given for the various parameters, but it should be emphasized that these values are only exemplary. It will be appreciated that all of the parameters have a range of values as indicated. Further, the ranges of values may vary as the invention i8 scaled up for commercial production. It is believed, however, that appropriate values for the parameters for apparatus on a larger scale will be readily apparent or perceivable by those skilled in the art.
Referring to the drawings, a vacuum chamber for carrying out a preferred method of the present invention is generally indicated in Figure 1 by reference number 10.
Vacuum chamber 10 is in the form of a bell jar 12 supportèd on a base 14. Bell jar 12 has a removable lid 16 which seals the upper opening of the bell jar when the latter is evacuated. Bell jar 12 also has an evacuation port 18 which is connected to a vacuum pump (not shown) for evacuating vacuum chamber 10.
A substrate holder 20 is connected to lid 16 by a support rod 22. Substrate holder 20 is in the form of a loo~ having a central opening 24 (see Figure 2). A
substrate 26 is shown located on holder 20 over opening 24.
In the embodiment shown in the drawings, substrate 26 is a square glass pane approximately 2 inches square. For the purposes of this disclosure, the term substrate includes any object or article which is desired to be coated. The substrate does not have to be flat and the substrate can be made of materials other than glass. In the vacuum chamber shown in the drawings, the underside or lower side of substrate 26 is the surface that is to be coated in vacuum chamber 10.
~ 16323~
A screen or shutter 28 is located adjacent to, but spaced closely to the underside of substrate holder 20.
Shutter 28 is connected to lid 16 by an upright support rod 30. Support rod 30 is rotatably mounted in lid 16 using a suitable seal 32. Rod 30 has an upper end portion ~4 projecting above lid 16. End portion 34 may be rotated to rotate shutter 28 transversely away from subst rate 26 when it is desired to commence the coating of the substrate, as described further below.
A high voltage electrode forms a cathode 36 in vacuum chamber 10. Another high voltage electrode forms an anode 38. As seen best in Figure 2, cathode 36 is in the form a circular loop spaced below shutter 28, the loop having a diameter slightly larger than substrate holder 20.
i5 Cathode 36 includes an upright portion 40 which is electrically connected to a connector 42. Connector 42 provides a seal for lid 16 and permits cathode 36 to be connected to a source of power. Anode 38 also has an upright portion 44 electrically connected to a similar sealing connector 46 for connecting the anode to the source of power. Shields 48, 50 are provided around the upright portions 44, 40 of the respective anode and cathode.
Shields 48, 50 are in the form of inverted insulating cups, and they are provided in the event that a conducting film is being deposited on substrate 26. Without the shields, stray conducting coating material could be deposited on upright portions 44, 46 and the underside of lid 16 causing a short or arcing between the cathode and anode, which is undesirable. Shields 48, 50 also serve to maintain the 1 1~3231 electrode geometry and enhance the plasma power density when conducting films are deposited.
Referring in particular to Figures 1, 3 and 4, a coating material source is generally indicated by reference number 54. Source 54 is formed of carbon and has a conical upper portion 56 and a cylindrical lower portion 58. This results in a high resistance joint 77 (see Figure 4) between upper and lower portions 56, 58, so that electrical current passing therethrough causes heating in the area of joint 77. This heating in the area of joint 77 causes material in source 54 to be heated and vaporized mainly at the top of the material. Conical upper portion 56 has a top orifice 78 typically 0.024 inches in diameter in the laboratory apparatus shown in the drawings. Vapor produced in source 54 emerges through orifice 7~ into vacuum chamber 10 as the material in source 54 is heated.
Upper portion 56 is conductibly or electrically connected to an upper element 60, which, in turn, is conductibly connected to a terminal 62 projecting from the underside of base 14. The lower portion 58 of material source 54 is conductibly connected to a lower element 64, which in turn is conductibly connected to a terminal 66 projecting from the underside of base 14.
Terminals 62, 66 are connected to a suitable source of electrical power to produce the desired heating and vaporization of the material inside source 54.
A thermocouple 68 communicates with the inside of material source 54 for measuring the temperature of the coating material therein. Thermocouple 68 has leads 71, 73 passing through base 14 for connection to a temperature indicating device (not shown).
A gas inlet tube 70 passes through base 14 and has an upper circular loop 72. Loop 72 is formed with a plurality of equally spaced openings 74 through which gas emerges into vacuum chamber 10. Gas inlet tube 70 has a needle valve 76 attached thereto outside vacuum chamber 10 to control the flow o~ gas passing through tube 70 and entering the vacuum chamber.
The operation of vacuum chamber 10 and the preferred method of the present invention will now be described with reference to the coating of a glass substrate 26 using zinc as the source material and oxygen as the gas inside vacuum chamber 10, to produce a thin, ~inc oxide type transparent film on the substrate. Coating material source 54 is filled with zinc metal, and a glass substrate 26 is positioned on substrate holder 20. Shutter 28 is rotated into position so that it is directly beneath~
substràte 26 to block the substrate and prevent coating material from being deposited on substrate 26 until conditions have reached steady state inside vacuum chamber 10. Evacuation port 18 is connected to a vacuum pump and vacuum chamber 10 is evacuated. Needle valve 76 is opened to allow oxygen to flow through inlet tube 70 and out through loop 72 to fill the vacuum chamber with oxygen.
Vacuum chamber 10 is partially evacuated until the oxygen pressure therein is approximately O.Q35 torr., and a small amount of oxygen is continuously fed into vacuum chamber 10 to maintain this pr~ssure level.
1 16323~
g Cathode 36 and ~node 38 are connected to respective negative and positive terminals of a DC power source through connectors 42, 46. Power is applied to the cathode and anode to produce a glow discharge. The power dissipated in the glow discharge is approximately 0.5 watts in the laboratory apparatus shown in the drawings, - and this is just above the threshold power required to maintain the glow discharge in the vacuum chamber.
The zinc in coating material source 54 is heated by passing a current therethrough; terminals 62 and 66 being connected to a suitable power source for this purpose. The zinc is typically heated to a temperature of about 585 degress Centigrade in the laboratory apparatus shown, where it is vaporized at the top of coating material source 54. The zinc vapor thus produced in source 54 then passes through orifice 78 in the top of conical upper portion 56 into vacuum chamber 10.
The glow discharge produced between cathode 36 and anode 38 envelops or contacts the underside of substrate 26. Once this glow discharge has been established, and the oxygen pressure in vacuum chamber 10 is at the desired level, and the zinc is being vaporized in coating material source 54, shutter 28 is rotated out of the way. The zinc vapor and oxygen react forming a compound which is deposited on the underside of substrate 26 by the glow discharge. After the compound has been deposited for 50 to 100 seconds, the glow discharge can be turned off and the oxygen and zinc reaction continued. The coating will continue to be deposited on substrate 26 1 ~6323t without the glow discharge, and the coating will grow to the thickness desired.
The coating produced as described above is a transparent conducting film having low resistivity, in which the film is ZnO , wherein x is less than one.
Typical properties of this non stoichiometric tran~parent conducting film are as follows:
1. 93~ light transmission over the visible spectrum with much less than 1% absorption losses
In the past, various techniques have been used to S deposit a film or coating on a substrate located in a vacuum chamber. One technique simply is to thermally vaporize or evaporate a metal, permitting the vapor to condense and be deposited on the substrate. Another method is referred to as chemical vapor deposition wherein different gases are introduced into the vacuum chamber to react and form a compound on the substrate. Yet another prior art method is referred to as sputtering. In this method, a vacuum or gas filled discharge tube has a cathode that is disintegrated by bombardment, so that the cathode material is vaporized and deposited on the substrate.
A variation of these methods is shown in United States Patent ~o. 2,501~563 issued to W.H. Colbert. In this patent, vacuum evaporation is used to vaporize and deposit a metal substrate. Gas is then introduced into the vacuum ~hamber to oxidize the metal and form a metallic compound coating. Another variation of the prior art ~.
methods is shown in United States Patent No. 3,318,790 issued to B.G. Carbajal III, et al. In this patent, a gaseous organic source material is introduced into a vacuum chamber and a glow discharge is established to polymerize S the source material and deposit same on the substrate.
A difficulty with the prior art methods is that they generally do not permit individual and independent control of each parameter of the process and hence do not permit the fabrication of "tailor-made" compounds having predetermined atom ratios and hence predetermined properties.
In the present invention, a glow discharge in a reacting gas is provided in a vacuum chamber and a coating material is vaporized therein to be deposited on a substrate. Independent adjustment of each of the parameters of the process is possible allowing for control of the reaction and deposition of the coating material,~and thus the properties of the film deposited on the substrate.
According to one aspect of the invention, there is provided a method of coating a substrate comprising the steps of providing a vacuum chamber communicating with a surface of the substrate to be coated. A glow discharge is produced in the vacuum chamber in contact with the substrate surface. Coating material is vaporized in the chamber, and a gas is introduced into the vacuum chamber to react with the vaporized coating material forming a compound to be deposited on the substrate by the glow discharge.
~6~231 ~, According to another aspect of the invention, a coated substrate is provided comprising a substrate having a coating produced by the method described above.
According to yet another aspect of the invention, there is provided a coated subs1:rate comprising a substrate having a coating deposited thereon by glow discharge in a partial vacuum, the coating consisting of a non-stoichiometric compound produced by reacting a vaporized metal and a gas.
A preferred embodiment of the invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Figure l is a vertical diagrammatic sectional view of a vacuum chamber used to perform the method of the lS present invention;
Figure 2 is a perspective view from above and from the front showing the upper internal components of the vacuum chamber of Figure l;
Figure 3 i8 a perspective view from above and from the front showing the lower internal components of the vacuum chamber of Figure l; and Figure 4 is a perspective view, partly broken away, taken along lines 4-4 of Figure 3.
The following description of a preferred embodiment is given in reference to a laboratory test and demonstration unit for carrying out the preferred method to produce the preferred coated substrate. Specific values are given for the various parameters, but it should be emphasized that these values are only exemplary. It will be appreciated that all of the parameters have a range of values as indicated. Further, the ranges of values may vary as the invention i8 scaled up for commercial production. It is believed, however, that appropriate values for the parameters for apparatus on a larger scale will be readily apparent or perceivable by those skilled in the art.
Referring to the drawings, a vacuum chamber for carrying out a preferred method of the present invention is generally indicated in Figure 1 by reference number 10.
Vacuum chamber 10 is in the form of a bell jar 12 supportèd on a base 14. Bell jar 12 has a removable lid 16 which seals the upper opening of the bell jar when the latter is evacuated. Bell jar 12 also has an evacuation port 18 which is connected to a vacuum pump (not shown) for evacuating vacuum chamber 10.
A substrate holder 20 is connected to lid 16 by a support rod 22. Substrate holder 20 is in the form of a loo~ having a central opening 24 (see Figure 2). A
substrate 26 is shown located on holder 20 over opening 24.
In the embodiment shown in the drawings, substrate 26 is a square glass pane approximately 2 inches square. For the purposes of this disclosure, the term substrate includes any object or article which is desired to be coated. The substrate does not have to be flat and the substrate can be made of materials other than glass. In the vacuum chamber shown in the drawings, the underside or lower side of substrate 26 is the surface that is to be coated in vacuum chamber 10.
~ 16323~
A screen or shutter 28 is located adjacent to, but spaced closely to the underside of substrate holder 20.
Shutter 28 is connected to lid 16 by an upright support rod 30. Support rod 30 is rotatably mounted in lid 16 using a suitable seal 32. Rod 30 has an upper end portion ~4 projecting above lid 16. End portion 34 may be rotated to rotate shutter 28 transversely away from subst rate 26 when it is desired to commence the coating of the substrate, as described further below.
A high voltage electrode forms a cathode 36 in vacuum chamber 10. Another high voltage electrode forms an anode 38. As seen best in Figure 2, cathode 36 is in the form a circular loop spaced below shutter 28, the loop having a diameter slightly larger than substrate holder 20.
i5 Cathode 36 includes an upright portion 40 which is electrically connected to a connector 42. Connector 42 provides a seal for lid 16 and permits cathode 36 to be connected to a source of power. Anode 38 also has an upright portion 44 electrically connected to a similar sealing connector 46 for connecting the anode to the source of power. Shields 48, 50 are provided around the upright portions 44, 40 of the respective anode and cathode.
Shields 48, 50 are in the form of inverted insulating cups, and they are provided in the event that a conducting film is being deposited on substrate 26. Without the shields, stray conducting coating material could be deposited on upright portions 44, 46 and the underside of lid 16 causing a short or arcing between the cathode and anode, which is undesirable. Shields 48, 50 also serve to maintain the 1 1~3231 electrode geometry and enhance the plasma power density when conducting films are deposited.
Referring in particular to Figures 1, 3 and 4, a coating material source is generally indicated by reference number 54. Source 54 is formed of carbon and has a conical upper portion 56 and a cylindrical lower portion 58. This results in a high resistance joint 77 (see Figure 4) between upper and lower portions 56, 58, so that electrical current passing therethrough causes heating in the area of joint 77. This heating in the area of joint 77 causes material in source 54 to be heated and vaporized mainly at the top of the material. Conical upper portion 56 has a top orifice 78 typically 0.024 inches in diameter in the laboratory apparatus shown in the drawings. Vapor produced in source 54 emerges through orifice 7~ into vacuum chamber 10 as the material in source 54 is heated.
Upper portion 56 is conductibly or electrically connected to an upper element 60, which, in turn, is conductibly connected to a terminal 62 projecting from the underside of base 14. The lower portion 58 of material source 54 is conductibly connected to a lower element 64, which in turn is conductibly connected to a terminal 66 projecting from the underside of base 14.
Terminals 62, 66 are connected to a suitable source of electrical power to produce the desired heating and vaporization of the material inside source 54.
A thermocouple 68 communicates with the inside of material source 54 for measuring the temperature of the coating material therein. Thermocouple 68 has leads 71, 73 passing through base 14 for connection to a temperature indicating device (not shown).
A gas inlet tube 70 passes through base 14 and has an upper circular loop 72. Loop 72 is formed with a plurality of equally spaced openings 74 through which gas emerges into vacuum chamber 10. Gas inlet tube 70 has a needle valve 76 attached thereto outside vacuum chamber 10 to control the flow o~ gas passing through tube 70 and entering the vacuum chamber.
The operation of vacuum chamber 10 and the preferred method of the present invention will now be described with reference to the coating of a glass substrate 26 using zinc as the source material and oxygen as the gas inside vacuum chamber 10, to produce a thin, ~inc oxide type transparent film on the substrate. Coating material source 54 is filled with zinc metal, and a glass substrate 26 is positioned on substrate holder 20. Shutter 28 is rotated into position so that it is directly beneath~
substràte 26 to block the substrate and prevent coating material from being deposited on substrate 26 until conditions have reached steady state inside vacuum chamber 10. Evacuation port 18 is connected to a vacuum pump and vacuum chamber 10 is evacuated. Needle valve 76 is opened to allow oxygen to flow through inlet tube 70 and out through loop 72 to fill the vacuum chamber with oxygen.
Vacuum chamber 10 is partially evacuated until the oxygen pressure therein is approximately O.Q35 torr., and a small amount of oxygen is continuously fed into vacuum chamber 10 to maintain this pr~ssure level.
1 16323~
g Cathode 36 and ~node 38 are connected to respective negative and positive terminals of a DC power source through connectors 42, 46. Power is applied to the cathode and anode to produce a glow discharge. The power dissipated in the glow discharge is approximately 0.5 watts in the laboratory apparatus shown in the drawings, - and this is just above the threshold power required to maintain the glow discharge in the vacuum chamber.
The zinc in coating material source 54 is heated by passing a current therethrough; terminals 62 and 66 being connected to a suitable power source for this purpose. The zinc is typically heated to a temperature of about 585 degress Centigrade in the laboratory apparatus shown, where it is vaporized at the top of coating material source 54. The zinc vapor thus produced in source 54 then passes through orifice 78 in the top of conical upper portion 56 into vacuum chamber 10.
The glow discharge produced between cathode 36 and anode 38 envelops or contacts the underside of substrate 26. Once this glow discharge has been established, and the oxygen pressure in vacuum chamber 10 is at the desired level, and the zinc is being vaporized in coating material source 54, shutter 28 is rotated out of the way. The zinc vapor and oxygen react forming a compound which is deposited on the underside of substrate 26 by the glow discharge. After the compound has been deposited for 50 to 100 seconds, the glow discharge can be turned off and the oxygen and zinc reaction continued. The coating will continue to be deposited on substrate 26 1 ~6323t without the glow discharge, and the coating will grow to the thickness desired.
The coating produced as described above is a transparent conducting film having low resistivity, in which the film is ZnO , wherein x is less than one.
Typical properties of this non stoichiometric tran~parent conducting film are as follows:
1. 93~ light transmission over the visible spectrum with much less than 1% absorption losses
2. 1.3 x 10 3 ohm cm. resistivity
3. 102 per cm.3 carrier density (electrons)
4. 25 to 35 cm. /volt-second mobility
5. 4.24 e.v. work function Having described the preferred method of operation to produce transparent high conductivity films, many variations are possible to obtain other properties.
For example, in the laboratory test and demonstration unit shown in the drawings, the power in the glow discharge for the entire film deposition process can range from 0.1 watts to 20 watts to produce a very large change in the film resistivity. Different power levels, source temperatures and gas pressures produce films with different opacity and/or different electrical resistivities, which can range from opaque to clear and resistivities differing by as much as eleven orders of magnitude. The glow discharge appears to "clean" the substrate and promote uniform nucleation of the coating thickness. Once a continuous molecular layer ~ 16323~
:. 1 1 of coating compounds is deposited on the substrate, the glow discharge can be turned off and a film will continue to grow uniformly. In fact, with a higher power glow discharge (near 20 watts) operating for about 200 seconds, in the laboratory unit the zinc source can remain cold until after the glow discharge is terminated, and if the zinc source is then heated to vaporize the zinc, a film will be deposited, but it may not have the desired properties.
The amount of zinc being vaporized in coating material source 54 can also be varied by changing the diameter of orifice 78 and by changing the temperature to which the zinc is heated in source 54. The zinc source orifice size and the temperature can also be varied to produce the same rate of vaporization of zinc. For example, orifice 78 could have a diameter of 0.030 inches, and the zinc heated to a temperature of 430 degrees Centigrade or lower, or an orifice diameter of .024 inches and a temperature of 585 degrees Centigrade might be used as described above. The higher the zinc temperature, the higher is the zinc partial pressure or the amount of zinc vapor in vacuum chamber lO. Higher temperatures result in a coating compound having a higher percentage of zinc.
This would result in a coating or film being deposited on the substrate having an even lower resistivity (at the same 2 pressure), but increased optical absorption.
Lowering the zinc partial pressure by decreasing the zinc temperature (again at the same 2 pressure) could ' produce a zinc oxide compound coating at the stoichiometric ratio, and this would have a very high resistivity. Normal operating temperatures for a zinc source or;fice size of 0.024 inches are between 550 and 600 degrees Centigrade.
The oxygen gas pressure inside vacuum chamber lO
can also be varied independently. For a fixed glow discharge power and source temperature, the range can be between O.OlO and 0.070 torr. Higher oxygen pressures result in coatings having higher resistivity and lower opacity, and vice versa. Increasing the amount or pressure of the oxygen causes the coated film to approach the stoichiometric ratio of zinc oxide and high resistivity films, but for low resistivity, a non-stoichiometric compound should be deposited on the substrate. It will be appreciated that the stoichiometric ratio of the coating can be varied by changing either the rate of vaporization of the zinc or the oxygen pressure, so stoichiometric coatings can be produced by increas-ing the oxygen pressure.
Other materials and gases could also be used with the method of this invention. For example, silicon can be vaporized in coating material source 54, and hydrogen can be introduced into the vacuum chamber through gas inlet tube 70. In this case, the glow discharge must be operating for the entire deposition process. This produces hydrogenated silicon. Other gases, such as nitrogen~
fluorine and oxygen, and mixtures of same such as nitrogen and oxygen, could also be used with silicon to produce correspondingly similar types of coatings.
1 16323t The method as described above could be adapted to a continuous process wherein the substrate passes through a vacuum chamber, or a vacuum chamber passes over the substrate. It will be appreciated that forms of vacuum chambers can be used other than the bell jar type container described above. The polarity of the electrodes forming the glow discharge can be reversed, and in fact, alternating current can be used to produce the glow discharge. It is preferred to have the dimensions of the cathode and anode comparable to the substrate size and the cathode spaced about 1 cm. from the substrate, but this can be varied. However, the film uniformity and the rate of deposition would change. The term "transparent" as used in as60ciation with the zinc and oxygen coating described I5 above refers to the visible spectrum only, and the degree of transparency is dependent upon the opacity or stoichiometric ratio of the compound deposited on the substrate.
From the above, it will be appreciated that the present invention provides a vèry flexible method of coating substrates wherein the properties of the coatings can be changed as desired by varying the three parameters involved, namely, the glow discharge power, the vaporization rate of the coating material, and the reactive gas pressure in the vacuum chamber.
These parameters are interrelated but can be controlled and adjusted separately. For example, in the ~1~323~
case of ZnO , the three parameters, discharge power density, Zn partial pressure, and oxygen gas pressure can be varied to produce a range of properties from good conductivity and good transparency to high resi~tivity and good transparency by adjusting one, two or all three of these parameters. Any given set of parameters is not neces~arily unique, since for example, an increase in the gas pressure can be offset by an appropriate change in the zn partial pressure, and an appropriate change in the discharge power density to achieve films with similar properties.
The parameters can be changed even during the coating process to produce a coating with varying properties across the coating thickness. For example, the index of refraction can be varied from 2.3 to 1.8 for ZnOx, or a non-stoichiometric zinc and oxygen coating can be produced by this method having very low resistivity and high visible light transmission characteristics. In fact, the resistivity of this coating can be varied between
For example, in the laboratory test and demonstration unit shown in the drawings, the power in the glow discharge for the entire film deposition process can range from 0.1 watts to 20 watts to produce a very large change in the film resistivity. Different power levels, source temperatures and gas pressures produce films with different opacity and/or different electrical resistivities, which can range from opaque to clear and resistivities differing by as much as eleven orders of magnitude. The glow discharge appears to "clean" the substrate and promote uniform nucleation of the coating thickness. Once a continuous molecular layer ~ 16323~
:. 1 1 of coating compounds is deposited on the substrate, the glow discharge can be turned off and a film will continue to grow uniformly. In fact, with a higher power glow discharge (near 20 watts) operating for about 200 seconds, in the laboratory unit the zinc source can remain cold until after the glow discharge is terminated, and if the zinc source is then heated to vaporize the zinc, a film will be deposited, but it may not have the desired properties.
The amount of zinc being vaporized in coating material source 54 can also be varied by changing the diameter of orifice 78 and by changing the temperature to which the zinc is heated in source 54. The zinc source orifice size and the temperature can also be varied to produce the same rate of vaporization of zinc. For example, orifice 78 could have a diameter of 0.030 inches, and the zinc heated to a temperature of 430 degrees Centigrade or lower, or an orifice diameter of .024 inches and a temperature of 585 degrees Centigrade might be used as described above. The higher the zinc temperature, the higher is the zinc partial pressure or the amount of zinc vapor in vacuum chamber lO. Higher temperatures result in a coating compound having a higher percentage of zinc.
This would result in a coating or film being deposited on the substrate having an even lower resistivity (at the same 2 pressure), but increased optical absorption.
Lowering the zinc partial pressure by decreasing the zinc temperature (again at the same 2 pressure) could ' produce a zinc oxide compound coating at the stoichiometric ratio, and this would have a very high resistivity. Normal operating temperatures for a zinc source or;fice size of 0.024 inches are between 550 and 600 degrees Centigrade.
The oxygen gas pressure inside vacuum chamber lO
can also be varied independently. For a fixed glow discharge power and source temperature, the range can be between O.OlO and 0.070 torr. Higher oxygen pressures result in coatings having higher resistivity and lower opacity, and vice versa. Increasing the amount or pressure of the oxygen causes the coated film to approach the stoichiometric ratio of zinc oxide and high resistivity films, but for low resistivity, a non-stoichiometric compound should be deposited on the substrate. It will be appreciated that the stoichiometric ratio of the coating can be varied by changing either the rate of vaporization of the zinc or the oxygen pressure, so stoichiometric coatings can be produced by increas-ing the oxygen pressure.
Other materials and gases could also be used with the method of this invention. For example, silicon can be vaporized in coating material source 54, and hydrogen can be introduced into the vacuum chamber through gas inlet tube 70. In this case, the glow discharge must be operating for the entire deposition process. This produces hydrogenated silicon. Other gases, such as nitrogen~
fluorine and oxygen, and mixtures of same such as nitrogen and oxygen, could also be used with silicon to produce correspondingly similar types of coatings.
1 16323t The method as described above could be adapted to a continuous process wherein the substrate passes through a vacuum chamber, or a vacuum chamber passes over the substrate. It will be appreciated that forms of vacuum chambers can be used other than the bell jar type container described above. The polarity of the electrodes forming the glow discharge can be reversed, and in fact, alternating current can be used to produce the glow discharge. It is preferred to have the dimensions of the cathode and anode comparable to the substrate size and the cathode spaced about 1 cm. from the substrate, but this can be varied. However, the film uniformity and the rate of deposition would change. The term "transparent" as used in as60ciation with the zinc and oxygen coating described I5 above refers to the visible spectrum only, and the degree of transparency is dependent upon the opacity or stoichiometric ratio of the compound deposited on the substrate.
From the above, it will be appreciated that the present invention provides a vèry flexible method of coating substrates wherein the properties of the coatings can be changed as desired by varying the three parameters involved, namely, the glow discharge power, the vaporization rate of the coating material, and the reactive gas pressure in the vacuum chamber.
These parameters are interrelated but can be controlled and adjusted separately. For example, in the ~1~323~
case of ZnO , the three parameters, discharge power density, Zn partial pressure, and oxygen gas pressure can be varied to produce a range of properties from good conductivity and good transparency to high resi~tivity and good transparency by adjusting one, two or all three of these parameters. Any given set of parameters is not neces~arily unique, since for example, an increase in the gas pressure can be offset by an appropriate change in the zn partial pressure, and an appropriate change in the discharge power density to achieve films with similar properties.
The parameters can be changed even during the coating process to produce a coating with varying properties across the coating thickness. For example, the index of refraction can be varied from 2.3 to 1.8 for ZnOx, or a non-stoichiometric zinc and oxygen coating can be produced by this method having very low resistivity and high visible light transmission characteristics. In fact, the resistivity of this coating can be varied between
6 x 10 4 and 108 ohm cm.
Claims (29)
1. A method of coating a substrate comprising:
providing a vacuum chamber communicating with a surface of the substrate to be coated;
producing a glow discharge in the vacuum chamber in contact with said substrate surface;
vaporizing coating material in said chamber; and introducing a gas into the vacuum chamber to react with said vaporized coating material forming a compound to be deposited on the substrate by the glow discharge.
providing a vacuum chamber communicating with a surface of the substrate to be coated;
producing a glow discharge in the vacuum chamber in contact with said substrate surface;
vaporizing coating material in said chamber; and introducing a gas into the vacuum chamber to react with said vaporized coating material forming a compound to be deposited on the substrate by the glow discharge.
2. A method of coating a substrate as claimed in claim 1 wherein the production of the glow discharge, the vaporization of the coating material and the introduction of the gas are all done simultaneously.
3. A method of coating a substrate as claimed in claim 1 wherein the production of the glow discharge and the introduction of the gas are done before the coating material is vaporized.
4. A method of coating a substrate as claimed in claim 2 and further comprising the step of terminating the glow discharge after at least a continuous molecular layer of coating compound has been coated on the substrate.
5. A method of coating a substrate as claimed in claim 3 and further comprising the step of terminating the glow discharge after the introduction of the gas and during the vaporization of the coating material.
6. A method of coating a substrate as claimed in claim 1, 3 or 4 wherein the glow discharge is produced having a discharge power just above the threshold power required to maintain the discharge in the vacuum chamber.
7. A method of coating a substrate as claimed in claim 1, 3 or 4 wherein the coating material is vaporized at a rate such that its reaction with the gas produces a non-stoichiometric compound being deposited on the substrate.
8. A method of coating a substrate as claimed in claim 1, 3 or 4 wherein the gas is introduced at a rate such that its reaction with the vaporized coating material produces a non-stoichiometric compound being deposited on the substrate.
9. A method of coating a substrate as claimed in claim 1 wherein the coating material is zinc and the gas is oxygen.
10. A method of coating a substrate as claimed in claim 9 wherein the zinc is vaporized by providing a heated zinc source having a discharge orifice between 0.024 and 0.030 inches in diameter, the zinc being heated between 430 degrees Centigrade and 600 degrees Centigrade.
11. A method of coating a substrate as claimed in claim 9 wherein the zinc is vaporized by providing a heated zinc source having a discharge orifice of 0.024 inches in diameter, the zinc being heated between 550 and 600 degrees Centigrade.
12. A method of coating a substrate as claimed in claim 9 wherein the oxygen is introduced into the vacuum chamber and the chamber is evacuated to produce an oxygen pressure between 0.010 and 0.070 torr. in the vacuum chamber.
13. A method of coating a substrate as claimed in claim 9 wherein the oxygen is introduced into the vacuum chamber and the chamber is evacuated to produce an oxygen pressure between 0.035 and 0.055 torr.
14. A method of coating a substrate as claimed in claim 9 wherein the glow discharge is produced having a discharge power between 0.1 watts and 20 watts.
15. A method of coating a substrate as claimed in claim 14 wherein the glow discharge power is substantially 0.5 watts.
16. A method of coating a substrate as claimed in claim 9 wherein the zinc is vaporized by providing a heated zinc source having a discharge orifice of 0.024 inches, the zinc being heated to 585 degrees Centigrade, wherein the oxygen is introduced into the vacuum chamber and the chamber is evacuated to produce an oxygen pressure substantially about 0.050 torr., and wherein the glow discharge power is 0.5 watts.
17. A method of coating a substrate as claimed in claim 1 wherein the coating material is silicon and the gas is hydrogen.
18. A method of coating a substrate as claimed in claim l wherein the coating material is silicon and the gas is nitrogen.
19. A method of coating a substrate as claimed in claim l wherein the coating material is silicon and the gas is oxygen.
20. A method of coating a substrate as claimed in claim l wherein the coating material is silicon and the gas is a mixture of nitrogen and oxygen.
21. A coated substrate comprising: a substrate having a coating produced by the method of claim 1.
22. A coated substrate comprising: a substrate having a coating produced by the method of claim 9.
23. A coated substrate comprising: a substrate having a coating produced by the method of claim 17.
24. A coated substrate comprising: a substrate having a coating produced by the method of claim 20.
25. A coated substrate comprising: a substrate having a coating deposited thereon by glow discharge in a partial vacuum, the coating consisting of a non-stoichiometric compound produced by reacting a vaporized material and a gas.
26. A coated substrate as claimed in claim 25 wherein the material is zinc, the gas is oxygen, and the non-stoichiometric compound is oxygen deficient zinc oxide.
27. A coated substrate as claimed in claim 25 wherein said material is silicon, the gas is hydrogen and the non-stoichiometric compound is hydrogenated silicon.
28. A coated substrate as claimed in claim 22 wherein the oxygen is introduced into the vacuum chamber to produce an oxygen pressure therein between 0.035 and 0.055 torr., and wherein the glow discharge is produced having a power of 0.5 watts.
29. A coated substrate as claimed in claim 28 wherein the zinc is vaporized by providing a zinc source having a discharge opening of 0.024 inches and heating the zinc therein to a temperature between 550 and 600 degrees Centigrade.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000382527A CA1163231A (en) | 1981-07-24 | 1981-07-24 | Reactive plating method and product |
| US06/365,116 US4415602A (en) | 1981-07-24 | 1982-04-05 | Reactive plating method and product |
| JP57127783A JPS5848664A (en) | 1981-07-24 | 1982-07-23 | Coating method and coated matter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000382527A CA1163231A (en) | 1981-07-24 | 1981-07-24 | Reactive plating method and product |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1163231A true CA1163231A (en) | 1984-03-06 |
Family
ID=4120528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000382527A Expired CA1163231A (en) | 1981-07-24 | 1981-07-24 | Reactive plating method and product |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US4415602A (en) |
| JP (1) | JPS5848664A (en) |
| CA (1) | CA1163231A (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4525381A (en) * | 1983-02-09 | 1985-06-25 | Ushio Denki Kabushiki Kaisha | Photochemical vapor deposition apparatus |
| JPS60251273A (en) * | 1984-05-28 | 1985-12-11 | Mitsubishi Heavy Ind Ltd | Method for controlling extent of evaporation in vacuum depositing apparatus |
| JPH02150025A (en) * | 1988-08-05 | 1990-06-08 | Univ Toronto Innov Found | Plasma etching by d.c. glow or plasma discharge, base-material washing or method and device for evaporating material onto base body |
| US6261694B1 (en) * | 1999-03-17 | 2001-07-17 | General Electric Company | Infrared reflecting coatings |
| JP4168676B2 (en) * | 2002-02-15 | 2008-10-22 | コニカミノルタホールディングス株式会社 | Film forming method |
| US7318948B1 (en) * | 2002-04-30 | 2008-01-15 | United States Of America As Represented By The Secretary Of The Air Force | Light transmissive films |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA643527A (en) * | 1962-06-26 | Radiation Research Corporation | Dielectric coated electrodes | |
| CA770566A (en) * | 1967-10-31 | Western Electric Company, Incorporated | Deposition of insulating films | |
| CA884480A (en) * | 1971-10-26 | L. Whitaker Howard | Method and apparatus for coating a substrate by utilizing the hollow cathode effect with rf sputtering | |
| CA855193A (en) * | 1970-11-03 | D. Davidse Pieter | Apparatus for the radio frequency sputtering of materials | |
| US2501563A (en) * | 1946-02-20 | 1950-03-21 | Libbey Owens Ford Glass Co | Method of forming strongly adherent metallic compound films by glow discharge |
| US2539149A (en) * | 1948-10-21 | 1951-01-23 | Rca Corp | Vapor coating process |
| US2904452A (en) * | 1956-04-16 | 1959-09-15 | Heraeus Gmbh W C | Oxide coating |
| US2996418A (en) * | 1957-06-05 | 1961-08-15 | Gen Motors Corp | Method and apparatus for vapor depositing thin films |
| US3108900A (en) * | 1959-04-13 | 1963-10-29 | Cornelius A Papp | Apparatus and process for producing coatings on metals |
| US3068510A (en) * | 1959-12-14 | 1962-12-18 | Radiation Res Corp | Polymerizing method and apparatus |
| US3208873A (en) * | 1962-01-05 | 1965-09-28 | Ibm | Method and apparatus for depositing films of refractory metal oxides and refractory metals |
| US3165405A (en) * | 1962-09-05 | 1965-01-12 | Eastman Kodak Co | Zinc oxide xerographic layers for bireflex copying |
| US3318790A (en) * | 1964-04-29 | 1967-05-09 | Texas Instruments Inc | Production of thin organic polymer by screened glow discharge |
| US3473959A (en) * | 1964-08-10 | 1969-10-21 | Licentia Gmbh | Method for coating semiconductors and apparatus |
| US3549411A (en) * | 1967-06-27 | 1970-12-22 | Texas Instruments Inc | Method of preparing silicon nitride films |
| US3655438A (en) * | 1969-10-20 | 1972-04-11 | Int Standard Electric Corp | Method of forming silicon oxide coatings in an electric discharge |
| GB1336559A (en) * | 1970-05-20 | 1973-11-07 | Triplex Safety Glass Co | Metal oxide coatings |
| DE2063726C3 (en) * | 1970-12-24 | 1979-09-06 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Method for manufacturing a semiconductor component |
| GB1365492A (en) * | 1971-02-05 | 1974-09-04 | Triplex Safety Glass Co | Metal oxide films |
| US3847658A (en) * | 1972-01-14 | 1974-11-12 | Western Electric Co | Article of manufacture having a film comprising nitrogen-doped beta tantalum |
| CA1006847A (en) * | 1972-11-29 | 1977-03-15 | Robert Hiscutt | Metal oxide coatings |
| US3900592A (en) * | 1973-07-25 | 1975-08-19 | Airco Inc | Method for coating a substrate to provide a titanium or zirconium nitride or carbide deposit having a hardness gradient which increases outwardly from the substrate |
-
1981
- 1981-07-24 CA CA000382527A patent/CA1163231A/en not_active Expired
-
1982
- 1982-04-05 US US06/365,116 patent/US4415602A/en not_active Expired - Fee Related
- 1982-07-23 JP JP57127783A patent/JPS5848664A/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US4415602A (en) | 1983-11-15 |
| JPS5848664A (en) | 1983-03-22 |
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