CA1329166C - Plasma thin film deposition process control - Google Patents
Plasma thin film deposition process controlInfo
- Publication number
- CA1329166C CA1329166C CA000571973A CA571973A CA1329166C CA 1329166 C CA1329166 C CA 1329166C CA 000571973 A CA000571973 A CA 000571973A CA 571973 A CA571973 A CA 571973A CA 1329166 C CA1329166 C CA 1329166C
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- CA
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- Prior art keywords
- plasma
- ratio
- emission
- intensity
- chamber
- 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.)
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- 238000004886 process control Methods 0.000 title abstract description 6
- 238000000034 method Methods 0.000 claims abstract description 75
- 230000008569 process Effects 0.000 claims abstract description 51
- 239000000758 substrate Substances 0.000 claims abstract description 34
- 239000010409 thin film Substances 0.000 claims abstract description 22
- 238000000151 deposition Methods 0.000 claims abstract description 21
- 239000007789 gas Substances 0.000 claims description 55
- 239000001257 hydrogen Substances 0.000 claims description 33
- 229910052739 hydrogen Inorganic materials 0.000 claims description 33
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 32
- 229910052734 helium Inorganic materials 0.000 claims description 18
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 18
- 239000001307 helium Substances 0.000 claims description 17
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 15
- 239000001301 oxygen Substances 0.000 claims description 15
- 229910052760 oxygen Inorganic materials 0.000 claims description 15
- 239000000463 material Substances 0.000 claims description 10
- 230000005684 electric field Effects 0.000 claims description 8
- 230000005670 electromagnetic radiation Effects 0.000 claims description 7
- 238000005137 deposition process Methods 0.000 claims description 6
- 239000011261 inert gas Substances 0.000 claims description 4
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- UQEAIHBTYFGYIE-UHFFFAOYSA-N hexamethyldisiloxane Chemical compound C[Si](C)(C)O[Si](C)(C)C UQEAIHBTYFGYIE-UHFFFAOYSA-N 0.000 claims description 2
- 239000010408 film Substances 0.000 abstract description 25
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- 229910052710 silicon Inorganic materials 0.000 description 10
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
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- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
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- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
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- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 1
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- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
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- JCYWCSGERIELPG-UHFFFAOYSA-N imes Chemical class CC1=CC(C)=CC(C)=C1N1C=CN(C=2C(=CC(C)=CC=2C)C)[C]1 JCYWCSGERIELPG-UHFFFAOYSA-N 0.000 description 1
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- 239000006120 scratch resistant coating Substances 0.000 description 1
- 230000003678 scratch resistant effect Effects 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- LIVNPJMFVYWSIS-UHFFFAOYSA-N silicon monoxide Inorganic materials [Si-]#[O+] LIVNPJMFVYWSIS-UHFFFAOYSA-N 0.000 description 1
- 239000002210 silicon-based material Substances 0.000 description 1
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Classifications
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/12—Bonding of a preformed macromolecular material to the same or other solid material such as metal, glass, leather, e.g. using adhesives
-
- 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
- C23C14/0036—Reactive sputtering
- C23C14/0042—Controlling partial pressure or flow rate of reactive or inert gases with feedback of measurements
-
- 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
- C23C14/54—Controlling or regulating the coating process
-
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/50—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating using electric discharges
-
- 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/52—Controlling or regulating the coating process
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- General Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Manufacturing & Machinery (AREA)
- Health & Medical Sciences (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Plasma & Fusion (AREA)
- Chemical Vapour Deposition (AREA)
- Physical Vapour Deposition (AREA)
- Plasma Technology (AREA)
- Electrodes Of Semiconductors (AREA)
- Light Receiving Elements (AREA)
Abstract
PLASMA THIN FILM DEPOSITION PROCESS CONTROL
Abstract of the Disclosure In a process of depositing a thin film onto a surface of a substrate with the use of a plasma, wherein the plasma optical emission is monitored, analyzed, and the results used to automatically control the nature of the plasma in order to control the characteristics of the deposited thin film. One aspect of the emission that is detected is the intensity of each of two emission lines of different wavelength bands from the same plasma species, the intensities being ratioed and the ratio compared to a predetermined value known to provide a resulting film with uniform and repeatable characteristics. This ratio is also related to the average electron temperature of the plasma, which can be calculated from it. Additionally, the intensity of another emission line from another of the plasma species may be measured and ratioed to one of the foregoing line intensifies if additional control is desired.
Abstract of the Disclosure In a process of depositing a thin film onto a surface of a substrate with the use of a plasma, wherein the plasma optical emission is monitored, analyzed, and the results used to automatically control the nature of the plasma in order to control the characteristics of the deposited thin film. One aspect of the emission that is detected is the intensity of each of two emission lines of different wavelength bands from the same plasma species, the intensities being ratioed and the ratio compared to a predetermined value known to provide a resulting film with uniform and repeatable characteristics. This ratio is also related to the average electron temperature of the plasma, which can be calculated from it. Additionally, the intensity of another emission line from another of the plasma species may be measured and ratioed to one of the foregoing line intensifies if additional control is desired.
Description
:` -. 132q'16 ~ PLASMA THIN FILM DEPOSITION PROCESS CONTROL
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Background of the Invention This invention relates generally to plasma diagnostics and process control in depositing thin films on substrates, particularly ~hose processes utilizing sputtering, plasma enhanced chemical vapor deposition (PECVD) and plasma polymerization.
As is well known, a thin film depositing plasma is formed in a chamber by introducing at least one gas into a region of a controlled electrical field. Many such plasma processes operate at low pressure with magnetic confinement. Most plasma processes involve a control of at least the internal pressure level, the electrical field characteristics, and the composition and proportional flow rates of individual gases into the plasma. Selection of these variables, in turn, affects the properties of a resulting thin film. Such properties can include the film's hardness, its adhesion to the substrate, its permeability to certain liquids or gases, optical characteristics of translucence and refractive index, and its general composition. The property or properties of the resulting film that are important depend upon the purpose and application of the resulting product. For example, if a scratch resistant coating is being applied to glass, the film's hardness, adhesion to glass and degree of optical clarity are the most important properties. In another example, wherein a coating is desired to prevent the permeation of oxygen, that property of the thin film is most important~
It is, of course, desired to control the plasma variables in order to produce a product with the desired film properties. ~eretofore, most process control has ,, '' , . .
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been manual, based upon some but incomplete measurement of the resulting plasma characteristics. One such tech-nique is to measure the electron temperature (T ) of the plasma, which is a measure of the average electron energy in the plasma, by the use of available Langmuir ~electro-static) probe(s) positioned in the plasma. The plasma variables are then manually adjusted until the average ,~
electron temperature corresponds to that which has been determined to be necessary for obtaining the desired film .
, properties or rate of deposition of the film on the - substrate. However, since the Langmuir probe(s) must be ; positioned in the plasma, they quickly become coated with the film being deposited and its readings then are subject to considerable error. Also, such an average electron temperature measurement provides only a partial picture 't,' of the plasma's characteristics which, in some thin film processes, is inadequate.
It is still the practice in large-scale commer-., cial thin film deposition processes to adjust the plasma variables to a combination that is believed by the operator to be optimum for a particular application, and then to run and test a sample. Only when the plasma variables have been readjusted in response to many such test cycles is the plasma process adjusted for commercial runs.
Therefore, it is a primary object of the present invention to provide improved monitoring and control of the plasma process in order to provide a higher yield of coated product having films with uniform and repeatable properties.
It is another ob]ect of the present invention to provide a plasma thin film deposition process that is suitable for continuous commercial use in the coating of large substrates such as automobile and architectural glass.
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Summary of the Invention These and additional objects are accomplished by the various aspects of the present invention wherein, briefly and generally, characteristics of the emission of electromagnetic radiation in the visible and near visible regions of the plasma are moni~ored, such as by use of a spectrometer, and input variables to the plasma process are controlled in response to this moni~oring. The purpose of this monitoring and control is to maintain the monitored aspects of the plasma emission at a level that has been determined to relate to certain desired proper-ties of the thin film that is being deposited. Such properties may be resistance to scratching or optical clarity of the film, as examples. Certain aspects of the plasma emission found to correlate with a high film deposition rate can also be controlled. These plasma characteristics are controlled in real time by automa-tically making any adiustments to the plasma input variables that are necessary to maintain the monitored plas~a emission characteristics within close limits.
This results in the thin film coating being uniform and the process being repeatable. The necessity for inde-pendent test depositions and subsequent analysis of the film properties is minimized. A high yield process for commercially coating large substrates is made practical by this diagnostic and control technique.
According to a particular aspect of the present invention, described in detail hereinafter, the intensity of each of a plurality of lines of emission of the plasma is measured and compared. It has been found that the average electron temperature (T ) in the plasma is proportional to a ratio of the intensities of two lines of emissions from a single species in the plasma. Since ' .
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such a species has been excited to emission by absorbing energy from colliding electrons, the intensity of the lines is proportional to such an average energy. By comparing emission line intensities, the distribution of those energies can be estimated and T calculated. The average electron temperature of the plasma af~ects the film deposition rate and properties of the resul~ing film, so it is an important piece of information to have in a real time plasma control system. As an alternative to calculating the average electron temperature, the ratio of intensities of the emission lines in the single species may be controlled directly by adjusting the plasma input variables until a predetermined value of the ratio is obtained, the predetermined value having been earlier determined to provide a film having the desired properties.
By taking another ratio of two emission lines, one produced by a species that necessarily absorbs a high energy from electron collisions with it and another from a species having a probability of having absorbed much lower energy from electron collisions with it to give the measured emission, a declining "tail" of an electron energy (temperature) distribution within the plasma can be monitored and controlled. It has been found that high energy electrons in the plasma can inadvertently be suppressed in the course of optimizing other variables.
Thereforep a separate high energy electron density measurement reveals whether this is happening or not and allows an adjustment to be made in real time to maintain a sufficient proportion of high energy electrons in the plasma. An adequate supply of high energy electrons is important to the hardness of the resulting film.
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Additional objects, advantages and features of the various aspects of the present invention will ~ecome apparent from the following description of its preferred embodiments, such description being given in conjunction . with the accompanying drawings.
. Brief Descri~tion of the Drawings '~ Figure 1 is a general schematic diagram illus-~ trating a plasma system utilizing the various aspects of `. the present invention;
. Figure 2 schematically illustrates a side ~ sectional view of the plasma deposition chamber and its ,` associated equipment;
Figure 3 is an example spectrum of the emission of plasma;
Figures 4A, 4B and 4C illustrate the bonding of components of a molecule of a gas used in an example plasma enhanced chemical vapor deposition process;
Figure 5 includes a series of curves that illustrate the electron energy distribution in an example plasma;
Figure 6 is an example energy level diagram for a single species in a plasma;
Figure 7 is a flow diagram for a computer program that controls plasma process input variables in response to the measured plasma spectra;
Figure 8 shows additional elements added to the plasma system of Figs. 1 and 2 Figure 9 is a partial sectional view of Fig. 8, i taken at section 9-9 thereof; and Figure 10 illustrates one aspect of the opera-tion of the elements shown in Figs. 8 and 9.
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Description of the Preferred Embodiments General System , Referring initially to Figure 1, a system is schematically illustrated that includes an enclosed reac~ion chamber 11 in which a plasma is formed and in which a substrate, such as substrate 13, is placed for depositing a thin film of material on it. The substrate 13 can be any vacuum compatible material, such as metal, glass, some plastics and coated substrates. One or more gases are supplied to the reaction chamber by a gas supply system 15. An electric field is created by a power supply 17, and a low pressure is maintained by a pressure control system 19. An optical emission spectrometer 21 is connected through an optical fiber light transmission medium 23 to the reaction chamber in some appropriate manner to couple the visible and near visible emission (especially the ultraviolet wavelengths) of the plasma to the spectrometer. A quartz window 24 in a side wall of the reaction chamber can be used to optically couple the plasma emission with the external fiber medium 23.
general system control 25, including a computer control portion, is connected to each of the other components of the system in a manner to receive status information from them and send controlling commands to them.
The reaction chamber 11 can, in the system of Figure 1, be of an appropriate type to perform any of the sputtering, plasma~enhanced chemical vapor depo$ition (PECVD), plasma polymerization processes or other vacuum thin film deposition processes. A more detailed explana tion of certain components of the system of Figure 1 is given with respect to Figure 2, an example of the PECVD or , ~
plasma polymerization process being given. The reaction chamber 11 is divided into a load lock compartment 27 and :`
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~ 7 , , a process compartment 29 by an isolation slit valve 31.
The pressure control system 19 includes a mechanical pump ,.
33 connected to the load lock chamber 27 by a valve 35.
The pressure control system also includes diffusion pumps 37 and 39, and an associated mechanical pump 41. The diffusion pump 37 is connected to the load lock chamber 27 through an isolation gate valve 43 and an adjustable baffle 45. Similarly, the diffusion pump 39 is connected to the process chamber 29 through an isolation gate valve 47 and an adjustable baffle 49. The baffle 49 is ., controlled by the system control 25, while a coating process is being carried out, in order to maintain the internal pressure at a desired value.
A substrate to be coated is first loaded into the load lock compartment 27 with the valve 31 closed.
The mechanical pump 33 then reduces the pressure most of the way to the high vacuum region. The diffusion pu~p 37 ~:! iS then operated to reduce the pressure further, to about 5 x 10 Torr. The operating pressure is typically in the neighborhood of 46 microns for a PECVD or plasma polymerization process and is achieved by flowing the process gases into the reaction chamber and throttling i the diffusion pump 39 by use of the baffle 49. During '! loading and unloading operations, the diffusion pump 39 maintains the deposition chamber 29 at the operating pressure. Once the load lock chamber 27 is reduced to ` base pressure, the valve 31 is opened and the substrate 13 moved into the deposition chamber 29.
~ Provision is made for moving the substrate 13 -~ back and forth through a region 51 where a plasma is ~i formed. In the example system being described, this is -' accomplished by a plurality of rollers 53, preferably made of aluminium with substrate supporting, electrically ,' '. ' .
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insulative O-ring spacers attached around outside sur-faces. The rollers are driven by a motor source ~not shown) to rotate about their axes at controllable speeds and thus move the substrate 13. A typical deposition process involves passing the substrate 13 back and forth through the plasma 51 a number of times in order that the thin film deposited on the top of the substrate 13 has a desired uniform thickness.
A magnetron is positioned within the chamber 29, formed of a magnetic structure 55 and a cathode 57.
The power supply 17 has its output connected between the cathode 57 and a metallic body of the reaction chamber 29.
The magnetron creates an appropriate combination of magnetic and electrical fields in the region 51 in order to create a plasma there when the proper gases are introduced into the reaction chamber 29. The substrate 13 is maintained electrically isolated and is passed directly through the plasma region 51.
The gaseous components necessary for the plasma to form in the region 51 are introduced into the deposition chamber 29 by a conduit 59. A tube (not shown) having a plurality of gas supply nozzles along its length is positioned across the width of the chamber 29 (in a direction into the paper of Figure 2) at the position where the conduit 59 enters the chamber. That gas flows within the deposition chamber 29 generally from the supply tube to the diffusion pump 3~, as shown in dotted outline in Figure 2. It has been found preferable to introduce the gas on the side of the plasma region 51 that is closest to the pump 39. A pair of baffles 61 and 63 on either side of the magnetron also helps to confine the gas flow to the plasma region 51.
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g ., A particular gas supply system 15 that is connected to the conduit 59 depends, of course, on how many gases are being combined and their nature. In the example of Figure 2, two separate sources 65 and 67 of gases under high pressure are utilizedr fewer or addi-tional such gas sources being necessary for other processes. Also, in this particular example, a source 69 of a liquid material to be vaporized is provided. A
vaporizing apparatus 71 provides a desired controlled flow of vapor into the input condui~ 59, in accordance with a control signal from the system control 25 that operates upon a flow meter that is part of the apparatus 71. Similarly, the high pressure gases 65 and 67 are delivered through individually controlled flow meters 73 and 75, respectively. An important control of the plasma 51, and thus of the resulting film deposited on the substrate 13, is provided by the ability to adjust the proportions of each gaseous component that is flowing through the inlet tube 59 and into the deposition chamber 29. Each of the flow meters 73 and 75, and that in the apparatus 71, supply the system control 25 with an electrical signal proportional to the flow rate of gas through it, and also responds to a signal from the system control 25 to adjust and control that flow rate.
In some applications, particularly in large-scale commercial plasma coating systems, steps are desirably taken to assure a sufficient supply of ! gases from the supply system 15. In a commercial coater, it is desired that the highest possible deposition rate be achieved without degrading the quality of the deposited thin film. In order to assure that the deposition rate is not limited by the amount of gas that is made available within the reaction chamber 29, the gas supply system 15 .
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The pressure control system 19 needs to have its mechanical pump 41 and dif~usion pump 39 large enough to enable a flow of gases through the reaction chamber 11 sufficient that enough unreacted gas is always available in it. Alternatively, additional such pumps can be added to provide such a flow. To increase the effect of the pump shown in Fig. 2, the baffle 49 at the inlet of the diffusion pump 39 can be removed entirely, thereby causing the diffusion pump 39 to operate unimpeded. The diffusion pump 39 can even be eliminated en~irely, and a larger mechanical pump 41 provided, as another alter-native to providing the ability to reduce the pressure within the reaction chamber 290 Of course, in order to take advantage of a given large pumping capability in the pressure control system 19, the gas supply system 15 must be adequately sized.
The balance between the pumping ability and source gas supply is chosen to result in the desired operating pressure within the chamber 29, and to assure that the thin film deposition process is not limited in any way by a lack of supply of a reactant gas component. The provision of a plurality of gas inlets to the reaction chamber 11 also allows an increased gas flow rate, as well as a good distribution of fresh gas thoughout the chamber.
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~ Plasma Diagnostics and Control ~., A primary goal of the system and procedures to be described in this section is to adapt the system described with respect to Figures 1 and 2 for use in a ; continuous, commercially feasible process that repeat-~, ably produces thin films having uniform characteristics.
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A specific example of such a system is described with respect to Figures 3-7 herein. In this illustrative example, the liquid 69 is an organosilicon, and the pressurized gases 65 and 67 are oxygen and helium, respectively. The particular organosilicon chosen for illustration is hexamethyldisiloxane (~MDSO), its struc-ture being illustrated in Figure 4A. The result of this example PECVD process is a thin film that is very hard, scratch resistant, optically clear and adheres well to substrates. Useful applications of this particular thin film include the coating of automobile or architectural glass substrates, either directly on the glass or on top of one or more other thin films such as a sputter deposited low emissivity coating. As will be recognized, this class of substrates is physically large so the process must be able to form a film having uniform characteristics over the entire surface area of each item. However, the diagnoses and control techniques about to be described with respect to such an example have a wide and general application to numerous other specific . .
plasma processes and starting gaseous materials in thin film deposition processes.
Figure 3 is an example optical emission spec-~;
trum obtained by the spectrometer 21 of Figure 1 from a ` plasma formed in the process chamber 29 from such a combination of gases. The intensities of three strong emission lines are measured and used to diagno$e the characteristic of the plasma and then to make any adiustments to the relative proportion of the gaseous constituents that are required to maintain the plasma in a desired condition. These lines are the hydrogen alpha line 81, at about 657.1 nanometers wavelength, the hydrogen beta line B8, at about 486.1 nanometers wave-~ . ' , ~ .
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length, and a helium emission line 85, at about 501.8 nanometers wavelenqth. Since these three emission peaks are very strong relative to the intensity of the surrounding portion of the spectra, and are very narrow in bandwidth, the spectrometer 21 need have a resolution capability of only 0.5 nanometers, which is well within the resolving power of commercially available instru-ments.
In order to eliminate the effects of unknown variables and undesired optical signal noise, ratios of these intensity levels are utilized to diagnose the plasma and control the process. In this example, the ratio of the intensity of the hydrogen alpha line 81 to the intensity of the helium line 85 is used to control the rate of flow of the silicon source material vapor through the flow meter 71. This material is the source of hydrogen whose emission is being monitored. When that ratio exceeds a reference value, the computer control system 25 causes the flow meter within the apparatus 71 to decrease the rate of flow of the silicon material vapor, without affecting the flow rates of the other ga~es.
Also, if that ratio falls below the reference value, the flow meter 71 is opened to increase the flow of the silicon source material vapor.
A second ratio that is utilized is of the intensities of two emission lines of a single atomic or molecular species in the plasma. In this specific example, the intensities of the hydrogen alpha line 81 and the hydrogen beta line 83 are used. As explained below, this ratio is proportional to the average electron energy (average electron temperature T ) of the plasma. If this ratio, or the T calculated from it, exceeds a reference v=lue, the computer control 25 caoses the flow meter 73 to , , ~ :
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1 329 1 ~16 ; 13 increase the flow of oxygen without affecting the rate of ~; flow of the silicon source vapor or helium. If the ` intensity ratio, or the T calculated from it, falls below a reference value, the rate of oxygen flow is caused to decrease. A higher proportion of oxygen is believed to cause the average electron energy to decrease by combina-tion with atomic hydroqen which is a primary source of electrons in this gaseous mixture.
The nature of our example plasma will now be explored, and the relationship of the emission line intensity ratios to it will be explained. Figure 4A
illustrates a molecule of the silicon source vapor. It is desired that the portion Si-O-Si be deposited on the substrate. As noted in Figure 4A, the bond energy between the silicon and oxygen atoms is significantly higher than that of the other bonds in the molecule. That bond strength is 8.31 electron volts (eV). The bond energy between the silicon atom and the methyl group CH3 is 4.53 electron volts. Figure 4B shows the methyl group with a carbon~hydrogen bond energy of 3.51 electron - volts. Therefore, in a plasma having a distribution of high energy electrons colliding wi~h the silicon source molecules, there is a high probability that a collision of an electron with the molecule will cause a methyl group or hydrogen to be fractured away from the rest of the molecule without affecting the Si-O-Si component. The oxygen introduced into the plasma is believed to combine with the hydrogen and the carbon to form various gas and vapor compounds that are exhausted out of the deposition chamber 29 through the diffusion pump 39. This is another benefit of the oxygen component of the plasma gas.
In this example, it is desired to minimize, or completely eliminate, any carbon from the deposited film. An inorganic thin film is the goal.
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It can be seen from Figure 5 that the proper position for the electron energy distribution curve is where the density of electrons with energy sufficient to break the Si-C bond is much greater than the density of electrons having an energy great enough to undesirably break the Si-O bond. It can be seen from the shape of the curves of Figure 5 that this does indeed occur, keeping in mind that the vertical electron density scale is a logarithmic one. Indeed, it has been found that the distribution represented by the solid line 87 is approxi-mately optimum in the example being described, a T of slightly over 1.0 being desired.
It will also be noted from Figure 5 that the three emission lines discussed with respect to Figure 3 are also represented. The excitation energy that results in the hydrogen alpha line 93 is positioned at about 12 electron volts, that for the hydrogen beta line 95 at about 12~7 electron volts, and that for the helium line 97 at about 23 electron volts. These energies represent that which the hydrogen or helium atom must absorb from a collision with a free electron in order to emit the monitored wavelength of radiation when the a~om relaxes from its excited state.
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Figure 6 shows an energy diagram from the hydrogen ato~ that illustrates this. A collision with an electron of more than 12.07 electron volts can cause the atom to become excited with its electron being moved from a ground energy quantum level n=l ~o a higher energy quantum level n=3. When that excited electron falls to the next lower energy ~uantum level n=2, a hydrogen alpha wavelength photon is emitted. Similarly, a hydro-gen beta wavelength photon is emitted when an excited hydrogen atom having collided with an electron of energy greater than 12.73 electron volts relaxes from its excited n=4 quantum energy level back to the n=2 energy quantum level. As a result, the intensities of these hydrogen emission lines is related to the density of electrons in the plasma having those energy levels~ The ratio of the intensities of these hydrogen emission lines then provides a ratio of those densities. This allows a Maxwellian electron density curve to effectively be fit to those two points~ from which the average electron temperature T may be determined.
e However, the high energy "tail" of the electron energy curve of Figure 5 is desirably separately mea-sured. The hydrogen line intensity ratio is suitable for defining the rest of the curve since the electron densities represented by it are at energy levels in the main part of the energy distribution curve. But the density distribution at higher energy levels can at the same time drop off to very low levels. This is believed due to ineffective energy coupling. Therefore, a separ-ate measurement at a high energy level is also performed.
In this example, a helium line of emission is chosen, and :, ~'~ that is ratioed with one of the hydrogen lines, preferably the hydrogen alpha line, as a reference. This desired ,. ;i~
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A quantity of high energy electrons, repre-sented by the "tail" of the curve of Figure 5, is generally desirable for directly impinging upon the substrate since it is known that this improves the hardness of the resulting deposited film through a higher degree of film cross-linking. Stress in the film also decreases, resulting in better adhesion of the film to the substrate. A low ratio in the plasma emission of the ~ hydrogen alpha line intensity to that of helium predicts ; these beneficial results.
Use of the helium emission line in forming this second ratio is also advantageous since helium is inert.
il The gas does not combine with other gas components of the plasma. Any inert gas has this advantage, as well as providing an emission line in the "tail" portion of the curve. An inert gas is used in this example primarily for facilitating an initial source of electrons when the plasma is initiated by establishing the electric field.
~'~i But it has this additional diagnostic use, as well.
Once it is determined from the measured inten-sities and ratios that the electron energy distribution curve of Figure 5 needs to be altered for a process being ~;j performed, it can be done in any of a number of ways.
-' Increasing the excitation frequency of the power supply 17 tends to increase the average energy of the electrons, .
at least up to a point where the electrons can no longer `~l follow the rapidly changing electric field. The power of the supply 17 may affect the electron energy distri-butionr depending upon the precise geometry of the deposition chamber, an increase in power increasing the , .
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, -electron energy. Another variable that may be ad~usted is the total gas flow which changes the residence time of molecules within the plasma and increases the chance of collision. The pressure in the chamber 29 also affects molecular energy, within limits. The technique used in this specific example, however, keeps these variables at a constant level and instead changes the ratio of the flow rate of the individual gases into the reaction chamber 29.
The determination of average electron tempera-ture T from the ratio of the alpha and beta hydrogen emission line intensities is very significant. Others have suggested that the determination of electron tem-perature of a plasma from its emission spectra is very difficult, if not impossible. The mathematical rela-tionships between electron temperature and the intensity of a particular emission line have long been known.
However, these mathematical relationships also include additional unknowns such as molecular and electron densities in the plasma. With so many unknowns, it is impossible to use these equations directly to accurately determine electron temperature from an intensity of an emission line. However, if the intensities of two such emission lines from a single species within the plasma are ratioed, as is the case with the ratio of the hydrogen alpha and beta lines, these other variables are mathema-tically canceled out and no longer affect the result.
This calculation assumes a "cold" plasma, one where the average ion energy is very low when compared to the average electron energy.
Referring to Figure 7, a flow chart is provided of a controlling computer program that monitors the intensities of the three emission lines and make adjust-ments in the individual gaseous component flow rates as 1 32q 1 66 ., required to maintain the electron temperature distri-bution within acceptable limits. The process of Figure 7 can best be described as several functional modules. A
first module 101 requires information of both the desired plasma parameters and those that actually exist. It is preferable to enter a desired average electron tempera-ture T and then calculate what exists in the plasma, ase shown in Figure 7, since this permits the process operator to deal with known quantities. However, since T is proportional to the ratio of the hydrogen alpha and hydrogen beta emission lines, that ratio itself could more simply be substituted in the flow diagram of Figure 7 where T appears. It would then be that line intensity ratio to which the process is adjusted.
Once the actual and desired quantities are in the system, a next module 105 of the processing algorithm looks at the intensity ratio between the hydrogen alpha and the helium emission lines. A first step 107 compares the actual and desired ratios. If they are within range, then the processing component 105 is omitted completely by jumping to a step 109 in the next module 117. However, if the desired and actual ratios are not equal, a step 111 causes the flow meter 71 to be adjusted to change the flow . ~
`,of silicon source vapor in a direction to move the compared ratios closer together.
~>lA step 113 of the module 105 checks to make sure that the calculated voltage is within the range ~f the flow meter 71. If it is, the processing proceeds to a :1 step 109. If not, the process loop of module 105 is performed again. If the second calculation also results in a voltage that is not within the range of the flow meter 71, then the processing is stopped and an error message displayed for the operator, as indicated at 115.
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Once the silicon source vapor flow rate is adjusted, the next module 117 of the processing adjusts the flow of oxygen to the plasma in response to comparing the desired and actual T . If those quantities are equal within an acceptable tolerance, then the processing loops back to the beginning module 101 and performs the data acquisition and comparison functions once again, and then steps through the remainder of the program. This con-stant monitoring of the plasma characteristics allows real time control of the plasma for uniform film results and repeatability of film properties from substrate to substrate.
The program module 117 operates quite similarly to that of 105. If the newly calculated voltage for the oxygen supply flow meter is not within the range of that flow meter, as determined by the step 119, the calculation is made once more in case some error occurred. If the voltage is not within the range the second time, the processing is s~opped and an error message displayed.
Assuming, however, that the new oxygen flow meter valve control voltage is within its range, the processing is looped back to the beginning module 101 and repeated until the processing modules 101, 105 and 117 have been performed for a total of four times. After the fourth time, and if the last calculation loop resulted in a further adjustment to the oxygen flow meter, a next module 121 of processing is undertaken. After four ~imes through the silicon source and oxygen flow rate adjust-ments, it is concluded that some other adjustment must be made. Of course, the precise number of processing cycles that are allowed before going to the next calculation module 121 can vary.
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The module 121 also looks at T, but in this case adjusts the helium gas flow to the plasma chamber.
An increase of the inert gas supply provides more electrons, and a decrease in the gas fewer electrons.
The same check on the calculated voltage for the helium <, flow meter is made in the module 121 as in the modules 1~5 and 117, in step 123. Once a proper adjustment to the helium flow is made, the processing again loops back to the beginning module 101 to start the cycle over again.
Of course, there are many variations in the ; details of the process being described that can be changed without sacrificing the advantages provided by the basic emission line monitoring techniques that are so imple-i mented. The same techniques are used with other gases and even with a plasma that is part of a thin film ' sputtering system. In a sputtering system with a titan-ium target, the intensity of a 399.9 nanometer emission j line of titanium and a 301.3 nanometer emission line of i titanium-nitride are measured, for example. A ratio of the intensities of ~hese lines is used in the same manner as the hydrogen alpha to helium ratio discussed above.
Two line intensities from argon can be used to calculate the average electron temperature in this sputtering example, corresponding to the hydrogen alpha line to hydrogen beta line intensity ratio discussed above for the PECVD example.
Plasma input variables of power of the supply 17 and pressure within the chamber 29 are not included in the algorithm of Figure 7 as quantities that are adjusted automatically. It has been found satisfactory to main-'! tain those quantities fixed for at least a large :! processing batch. This is preferably accomplished by setting the control system 25 to the desired power and /
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pressure. The control system 25 is provided with astandard capability of monitoring those quantities and adjusting them, if necessary~ to maintain the constant levels that have been set.
The spectra of the plasma 51, an example being given in Fig. 3, is dependent upon the position within the plasma which is observed. That is, the intensities of the three emission peaks 81, 83 and 85, both absolutely and relatively, are different depending upon where the end of the optical fiber 23 is positioned with respect to the quartz window 24 (Fig. 1) of the reaction chamber 11.
So long as this position remains fixed and the intensity distribution across the plasma 51 does not change, the techniques of controlling that process described above optimizes it. But if it is desired to use that same process control on a different piece of equipment, for example, it is likely that the plasma will be viewed at a location with a different emission spectrum. Thus, the control system which has been optimized for one plasma emission spectrum may have to be recalibrated to operate with a spectrum having different relative intensities of peaks of interest than in the plasma for which the control system was optimized. Also, even in a single machine, the spectrum can change across the plasma due to a change in the substrate being coated, primarily in its thick-ness, any change of gases, gas flow rates, a pumping rate change, some relative change in the electrical power being delivered to the system, and similar matters.
Therefore, to further optimize the control of the plasma deposition process, a technique illustrated with respect to Figs. 8-10 maintains an end of the optical fiber medium 23 to gather light from the same relative position in the plasma, regardless of any such changes.
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As a preferred location, since it is relatively easy to locate for any plasma, the optical fiber 23 is positioned to view the plasma at the location where l:he ratio of the intensities of emission into relevant narrow band-widths is a maximum. In the example being descr.ibed, that ratio is preferred to be the intensity of the hydrogen alpha line divided by the intensity of the helium line of emission.
Referring to Figs. 8 and 9, a mechanism will be described for moving the optical fiber cable 23 with respect to the transparent window 24 of the reaction chamber in order to maintain this ratio at a maximum. The optical fiber cable 23 is preferably terminated in a long, small diameter cylindrical tube 301. The cable prefer-ably contains dozens of individual optical fibersO The purpose of the tube 301 is to limit the natural cone angle of acceptance of light of the optical fiber end so that it accepts substantially collimated light rays emitted from an area of the plasma 51 that is substantially the same size as the size of the opening of the tube 301 at an end adjacent the quartz window 24. The inside of the tube 301 is made to be highly reflective.
The light-guiding tube 301 is attached to a support block 303 that is carried with respect to the reaction chamber 11 in a manner that allows it to be moved in both X and Y directions. Appropriate control motors are u~ed to provide such movement. An example is the use of separate X and Y direction drive motors 305 and 307~
respectively, that drive the support block 303 through respective mechanical connections 309 and 311 to move the block 303 in those two directions. The motors 305 and 307 are controlled by position control circuits 313 which are in turn connected to the system computer control 25 (Fig.
1) by an appropriate circuit 315.
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A number of specific ways of determining the desired location may alternatively be implemented by the mechanism o~ Figs. 8 and 9. One way is to scan the fiber cable tube 301 in some raster pattern across the window 24, while the computer control system 25 calculates a desired ratio from information obtained at several locations of each raster scan line. The location of the . ~
block 303 where the ratio is maximized is then determined and the block returned to that position for monitoring the plasma.
~ Another one of many ways of determining the ; maximum intensity ratio location is illustrated in Fig.
`i, 10. As a first step, the tube 301 is located at four l spaced apart positions indicated at 317, 319, 321, and 1 323. The ratio of intensities is calculated for each of those locations and the maximum determined. Assuming that maximum in this example was obtained at the location 321, then the tube 301 is positioned at four ! other locations spaced around the position 321, such as positions 325, 327, 329 and 331. The maximum intensity ratio for each of these four locations is noted J and ~ another four locations tested around that location, and '`J~ SO forth.
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Although the various aspects of the present invention have been described with respect to its preferred embodiments, it will be understood that the invention is entitled to protection within the full scope of the appended claims.
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Background of the Invention This invention relates generally to plasma diagnostics and process control in depositing thin films on substrates, particularly ~hose processes utilizing sputtering, plasma enhanced chemical vapor deposition (PECVD) and plasma polymerization.
As is well known, a thin film depositing plasma is formed in a chamber by introducing at least one gas into a region of a controlled electrical field. Many such plasma processes operate at low pressure with magnetic confinement. Most plasma processes involve a control of at least the internal pressure level, the electrical field characteristics, and the composition and proportional flow rates of individual gases into the plasma. Selection of these variables, in turn, affects the properties of a resulting thin film. Such properties can include the film's hardness, its adhesion to the substrate, its permeability to certain liquids or gases, optical characteristics of translucence and refractive index, and its general composition. The property or properties of the resulting film that are important depend upon the purpose and application of the resulting product. For example, if a scratch resistant coating is being applied to glass, the film's hardness, adhesion to glass and degree of optical clarity are the most important properties. In another example, wherein a coating is desired to prevent the permeation of oxygen, that property of the thin film is most important~
It is, of course, desired to control the plasma variables in order to produce a product with the desired film properties. ~eretofore, most process control has ,, '' , . .
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been manual, based upon some but incomplete measurement of the resulting plasma characteristics. One such tech-nique is to measure the electron temperature (T ) of the plasma, which is a measure of the average electron energy in the plasma, by the use of available Langmuir ~electro-static) probe(s) positioned in the plasma. The plasma variables are then manually adjusted until the average ,~
electron temperature corresponds to that which has been determined to be necessary for obtaining the desired film .
, properties or rate of deposition of the film on the - substrate. However, since the Langmuir probe(s) must be ; positioned in the plasma, they quickly become coated with the film being deposited and its readings then are subject to considerable error. Also, such an average electron temperature measurement provides only a partial picture 't,' of the plasma's characteristics which, in some thin film processes, is inadequate.
It is still the practice in large-scale commer-., cial thin film deposition processes to adjust the plasma variables to a combination that is believed by the operator to be optimum for a particular application, and then to run and test a sample. Only when the plasma variables have been readjusted in response to many such test cycles is the plasma process adjusted for commercial runs.
Therefore, it is a primary object of the present invention to provide improved monitoring and control of the plasma process in order to provide a higher yield of coated product having films with uniform and repeatable properties.
It is another ob]ect of the present invention to provide a plasma thin film deposition process that is suitable for continuous commercial use in the coating of large substrates such as automobile and architectural glass.
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Summary of the Invention These and additional objects are accomplished by the various aspects of the present invention wherein, briefly and generally, characteristics of the emission of electromagnetic radiation in the visible and near visible regions of the plasma are moni~ored, such as by use of a spectrometer, and input variables to the plasma process are controlled in response to this moni~oring. The purpose of this monitoring and control is to maintain the monitored aspects of the plasma emission at a level that has been determined to relate to certain desired proper-ties of the thin film that is being deposited. Such properties may be resistance to scratching or optical clarity of the film, as examples. Certain aspects of the plasma emission found to correlate with a high film deposition rate can also be controlled. These plasma characteristics are controlled in real time by automa-tically making any adiustments to the plasma input variables that are necessary to maintain the monitored plas~a emission characteristics within close limits.
This results in the thin film coating being uniform and the process being repeatable. The necessity for inde-pendent test depositions and subsequent analysis of the film properties is minimized. A high yield process for commercially coating large substrates is made practical by this diagnostic and control technique.
According to a particular aspect of the present invention, described in detail hereinafter, the intensity of each of a plurality of lines of emission of the plasma is measured and compared. It has been found that the average electron temperature (T ) in the plasma is proportional to a ratio of the intensities of two lines of emissions from a single species in the plasma. Since ' .
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such a species has been excited to emission by absorbing energy from colliding electrons, the intensity of the lines is proportional to such an average energy. By comparing emission line intensities, the distribution of those energies can be estimated and T calculated. The average electron temperature of the plasma af~ects the film deposition rate and properties of the resul~ing film, so it is an important piece of information to have in a real time plasma control system. As an alternative to calculating the average electron temperature, the ratio of intensities of the emission lines in the single species may be controlled directly by adjusting the plasma input variables until a predetermined value of the ratio is obtained, the predetermined value having been earlier determined to provide a film having the desired properties.
By taking another ratio of two emission lines, one produced by a species that necessarily absorbs a high energy from electron collisions with it and another from a species having a probability of having absorbed much lower energy from electron collisions with it to give the measured emission, a declining "tail" of an electron energy (temperature) distribution within the plasma can be monitored and controlled. It has been found that high energy electrons in the plasma can inadvertently be suppressed in the course of optimizing other variables.
Thereforep a separate high energy electron density measurement reveals whether this is happening or not and allows an adjustment to be made in real time to maintain a sufficient proportion of high energy electrons in the plasma. An adequate supply of high energy electrons is important to the hardness of the resulting film.
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Additional objects, advantages and features of the various aspects of the present invention will ~ecome apparent from the following description of its preferred embodiments, such description being given in conjunction . with the accompanying drawings.
. Brief Descri~tion of the Drawings '~ Figure 1 is a general schematic diagram illus-~ trating a plasma system utilizing the various aspects of `. the present invention;
. Figure 2 schematically illustrates a side ~ sectional view of the plasma deposition chamber and its ,` associated equipment;
Figure 3 is an example spectrum of the emission of plasma;
Figures 4A, 4B and 4C illustrate the bonding of components of a molecule of a gas used in an example plasma enhanced chemical vapor deposition process;
Figure 5 includes a series of curves that illustrate the electron energy distribution in an example plasma;
Figure 6 is an example energy level diagram for a single species in a plasma;
Figure 7 is a flow diagram for a computer program that controls plasma process input variables in response to the measured plasma spectra;
Figure 8 shows additional elements added to the plasma system of Figs. 1 and 2 Figure 9 is a partial sectional view of Fig. 8, i taken at section 9-9 thereof; and Figure 10 illustrates one aspect of the opera-tion of the elements shown in Figs. 8 and 9.
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Description of the Preferred Embodiments General System , Referring initially to Figure 1, a system is schematically illustrated that includes an enclosed reac~ion chamber 11 in which a plasma is formed and in which a substrate, such as substrate 13, is placed for depositing a thin film of material on it. The substrate 13 can be any vacuum compatible material, such as metal, glass, some plastics and coated substrates. One or more gases are supplied to the reaction chamber by a gas supply system 15. An electric field is created by a power supply 17, and a low pressure is maintained by a pressure control system 19. An optical emission spectrometer 21 is connected through an optical fiber light transmission medium 23 to the reaction chamber in some appropriate manner to couple the visible and near visible emission (especially the ultraviolet wavelengths) of the plasma to the spectrometer. A quartz window 24 in a side wall of the reaction chamber can be used to optically couple the plasma emission with the external fiber medium 23.
general system control 25, including a computer control portion, is connected to each of the other components of the system in a manner to receive status information from them and send controlling commands to them.
The reaction chamber 11 can, in the system of Figure 1, be of an appropriate type to perform any of the sputtering, plasma~enhanced chemical vapor depo$ition (PECVD), plasma polymerization processes or other vacuum thin film deposition processes. A more detailed explana tion of certain components of the system of Figure 1 is given with respect to Figure 2, an example of the PECVD or , ~
plasma polymerization process being given. The reaction chamber 11 is divided into a load lock compartment 27 and :`
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The pressure control system 19 includes a mechanical pump ,.
33 connected to the load lock chamber 27 by a valve 35.
The pressure control system also includes diffusion pumps 37 and 39, and an associated mechanical pump 41. The diffusion pump 37 is connected to the load lock chamber 27 through an isolation gate valve 43 and an adjustable baffle 45. Similarly, the diffusion pump 39 is connected to the process chamber 29 through an isolation gate valve 47 and an adjustable baffle 49. The baffle 49 is ., controlled by the system control 25, while a coating process is being carried out, in order to maintain the internal pressure at a desired value.
A substrate to be coated is first loaded into the load lock compartment 27 with the valve 31 closed.
The mechanical pump 33 then reduces the pressure most of the way to the high vacuum region. The diffusion pu~p 37 ~:! iS then operated to reduce the pressure further, to about 5 x 10 Torr. The operating pressure is typically in the neighborhood of 46 microns for a PECVD or plasma polymerization process and is achieved by flowing the process gases into the reaction chamber and throttling i the diffusion pump 39 by use of the baffle 49. During '! loading and unloading operations, the diffusion pump 39 maintains the deposition chamber 29 at the operating pressure. Once the load lock chamber 27 is reduced to ` base pressure, the valve 31 is opened and the substrate 13 moved into the deposition chamber 29.
~ Provision is made for moving the substrate 13 -~ back and forth through a region 51 where a plasma is ~i formed. In the example system being described, this is -' accomplished by a plurality of rollers 53, preferably made of aluminium with substrate supporting, electrically ,' '. ' .
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insulative O-ring spacers attached around outside sur-faces. The rollers are driven by a motor source ~not shown) to rotate about their axes at controllable speeds and thus move the substrate 13. A typical deposition process involves passing the substrate 13 back and forth through the plasma 51 a number of times in order that the thin film deposited on the top of the substrate 13 has a desired uniform thickness.
A magnetron is positioned within the chamber 29, formed of a magnetic structure 55 and a cathode 57.
The power supply 17 has its output connected between the cathode 57 and a metallic body of the reaction chamber 29.
The magnetron creates an appropriate combination of magnetic and electrical fields in the region 51 in order to create a plasma there when the proper gases are introduced into the reaction chamber 29. The substrate 13 is maintained electrically isolated and is passed directly through the plasma region 51.
The gaseous components necessary for the plasma to form in the region 51 are introduced into the deposition chamber 29 by a conduit 59. A tube (not shown) having a plurality of gas supply nozzles along its length is positioned across the width of the chamber 29 (in a direction into the paper of Figure 2) at the position where the conduit 59 enters the chamber. That gas flows within the deposition chamber 29 generally from the supply tube to the diffusion pump 3~, as shown in dotted outline in Figure 2. It has been found preferable to introduce the gas on the side of the plasma region 51 that is closest to the pump 39. A pair of baffles 61 and 63 on either side of the magnetron also helps to confine the gas flow to the plasma region 51.
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g ., A particular gas supply system 15 that is connected to the conduit 59 depends, of course, on how many gases are being combined and their nature. In the example of Figure 2, two separate sources 65 and 67 of gases under high pressure are utilizedr fewer or addi-tional such gas sources being necessary for other processes. Also, in this particular example, a source 69 of a liquid material to be vaporized is provided. A
vaporizing apparatus 71 provides a desired controlled flow of vapor into the input condui~ 59, in accordance with a control signal from the system control 25 that operates upon a flow meter that is part of the apparatus 71. Similarly, the high pressure gases 65 and 67 are delivered through individually controlled flow meters 73 and 75, respectively. An important control of the plasma 51, and thus of the resulting film deposited on the substrate 13, is provided by the ability to adjust the proportions of each gaseous component that is flowing through the inlet tube 59 and into the deposition chamber 29. Each of the flow meters 73 and 75, and that in the apparatus 71, supply the system control 25 with an electrical signal proportional to the flow rate of gas through it, and also responds to a signal from the system control 25 to adjust and control that flow rate.
In some applications, particularly in large-scale commercial plasma coating systems, steps are desirably taken to assure a sufficient supply of ! gases from the supply system 15. In a commercial coater, it is desired that the highest possible deposition rate be achieved without degrading the quality of the deposited thin film. In order to assure that the deposition rate is not limited by the amount of gas that is made available within the reaction chamber 29, the gas supply system 15 .
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The pressure control system 19 needs to have its mechanical pump 41 and dif~usion pump 39 large enough to enable a flow of gases through the reaction chamber 11 sufficient that enough unreacted gas is always available in it. Alternatively, additional such pumps can be added to provide such a flow. To increase the effect of the pump shown in Fig. 2, the baffle 49 at the inlet of the diffusion pump 39 can be removed entirely, thereby causing the diffusion pump 39 to operate unimpeded. The diffusion pump 39 can even be eliminated en~irely, and a larger mechanical pump 41 provided, as another alter-native to providing the ability to reduce the pressure within the reaction chamber 290 Of course, in order to take advantage of a given large pumping capability in the pressure control system 19, the gas supply system 15 must be adequately sized.
The balance between the pumping ability and source gas supply is chosen to result in the desired operating pressure within the chamber 29, and to assure that the thin film deposition process is not limited in any way by a lack of supply of a reactant gas component. The provision of a plurality of gas inlets to the reaction chamber 11 also allows an increased gas flow rate, as well as a good distribution of fresh gas thoughout the chamber.
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~ Plasma Diagnostics and Control ~., A primary goal of the system and procedures to be described in this section is to adapt the system described with respect to Figures 1 and 2 for use in a ; continuous, commercially feasible process that repeat-~, ably produces thin films having uniform characteristics.
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A specific example of such a system is described with respect to Figures 3-7 herein. In this illustrative example, the liquid 69 is an organosilicon, and the pressurized gases 65 and 67 are oxygen and helium, respectively. The particular organosilicon chosen for illustration is hexamethyldisiloxane (~MDSO), its struc-ture being illustrated in Figure 4A. The result of this example PECVD process is a thin film that is very hard, scratch resistant, optically clear and adheres well to substrates. Useful applications of this particular thin film include the coating of automobile or architectural glass substrates, either directly on the glass or on top of one or more other thin films such as a sputter deposited low emissivity coating. As will be recognized, this class of substrates is physically large so the process must be able to form a film having uniform characteristics over the entire surface area of each item. However, the diagnoses and control techniques about to be described with respect to such an example have a wide and general application to numerous other specific . .
plasma processes and starting gaseous materials in thin film deposition processes.
Figure 3 is an example optical emission spec-~;
trum obtained by the spectrometer 21 of Figure 1 from a ` plasma formed in the process chamber 29 from such a combination of gases. The intensities of three strong emission lines are measured and used to diagno$e the characteristic of the plasma and then to make any adiustments to the relative proportion of the gaseous constituents that are required to maintain the plasma in a desired condition. These lines are the hydrogen alpha line 81, at about 657.1 nanometers wavelength, the hydrogen beta line B8, at about 486.1 nanometers wave-~ . ' , ~ .
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length, and a helium emission line 85, at about 501.8 nanometers wavelenqth. Since these three emission peaks are very strong relative to the intensity of the surrounding portion of the spectra, and are very narrow in bandwidth, the spectrometer 21 need have a resolution capability of only 0.5 nanometers, which is well within the resolving power of commercially available instru-ments.
In order to eliminate the effects of unknown variables and undesired optical signal noise, ratios of these intensity levels are utilized to diagnose the plasma and control the process. In this example, the ratio of the intensity of the hydrogen alpha line 81 to the intensity of the helium line 85 is used to control the rate of flow of the silicon source material vapor through the flow meter 71. This material is the source of hydrogen whose emission is being monitored. When that ratio exceeds a reference value, the computer control system 25 causes the flow meter within the apparatus 71 to decrease the rate of flow of the silicon material vapor, without affecting the flow rates of the other ga~es.
Also, if that ratio falls below the reference value, the flow meter 71 is opened to increase the flow of the silicon source material vapor.
A second ratio that is utilized is of the intensities of two emission lines of a single atomic or molecular species in the plasma. In this specific example, the intensities of the hydrogen alpha line 81 and the hydrogen beta line 83 are used. As explained below, this ratio is proportional to the average electron energy (average electron temperature T ) of the plasma. If this ratio, or the T calculated from it, exceeds a reference v=lue, the computer control 25 caoses the flow meter 73 to , , ~ :
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1 329 1 ~16 ; 13 increase the flow of oxygen without affecting the rate of ~; flow of the silicon source vapor or helium. If the ` intensity ratio, or the T calculated from it, falls below a reference value, the rate of oxygen flow is caused to decrease. A higher proportion of oxygen is believed to cause the average electron energy to decrease by combina-tion with atomic hydroqen which is a primary source of electrons in this gaseous mixture.
The nature of our example plasma will now be explored, and the relationship of the emission line intensity ratios to it will be explained. Figure 4A
illustrates a molecule of the silicon source vapor. It is desired that the portion Si-O-Si be deposited on the substrate. As noted in Figure 4A, the bond energy between the silicon and oxygen atoms is significantly higher than that of the other bonds in the molecule. That bond strength is 8.31 electron volts (eV). The bond energy between the silicon atom and the methyl group CH3 is 4.53 electron volts. Figure 4B shows the methyl group with a carbon~hydrogen bond energy of 3.51 electron - volts. Therefore, in a plasma having a distribution of high energy electrons colliding wi~h the silicon source molecules, there is a high probability that a collision of an electron with the molecule will cause a methyl group or hydrogen to be fractured away from the rest of the molecule without affecting the Si-O-Si component. The oxygen introduced into the plasma is believed to combine with the hydrogen and the carbon to form various gas and vapor compounds that are exhausted out of the deposition chamber 29 through the diffusion pump 39. This is another benefit of the oxygen component of the plasma gas.
In this example, it is desired to minimize, or completely eliminate, any carbon from the deposited film. An inorganic thin film is the goal.
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It can be seen from Figure 5 that the proper position for the electron energy distribution curve is where the density of electrons with energy sufficient to break the Si-C bond is much greater than the density of electrons having an energy great enough to undesirably break the Si-O bond. It can be seen from the shape of the curves of Figure 5 that this does indeed occur, keeping in mind that the vertical electron density scale is a logarithmic one. Indeed, it has been found that the distribution represented by the solid line 87 is approxi-mately optimum in the example being described, a T of slightly over 1.0 being desired.
It will also be noted from Figure 5 that the three emission lines discussed with respect to Figure 3 are also represented. The excitation energy that results in the hydrogen alpha line 93 is positioned at about 12 electron volts, that for the hydrogen beta line 95 at about 12~7 electron volts, and that for the helium line 97 at about 23 electron volts. These energies represent that which the hydrogen or helium atom must absorb from a collision with a free electron in order to emit the monitored wavelength of radiation when the a~om relaxes from its excited state.
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Figure 6 shows an energy diagram from the hydrogen ato~ that illustrates this. A collision with an electron of more than 12.07 electron volts can cause the atom to become excited with its electron being moved from a ground energy quantum level n=l ~o a higher energy quantum level n=3. When that excited electron falls to the next lower energy ~uantum level n=2, a hydrogen alpha wavelength photon is emitted. Similarly, a hydro-gen beta wavelength photon is emitted when an excited hydrogen atom having collided with an electron of energy greater than 12.73 electron volts relaxes from its excited n=4 quantum energy level back to the n=2 energy quantum level. As a result, the intensities of these hydrogen emission lines is related to the density of electrons in the plasma having those energy levels~ The ratio of the intensities of these hydrogen emission lines then provides a ratio of those densities. This allows a Maxwellian electron density curve to effectively be fit to those two points~ from which the average electron temperature T may be determined.
e However, the high energy "tail" of the electron energy curve of Figure 5 is desirably separately mea-sured. The hydrogen line intensity ratio is suitable for defining the rest of the curve since the electron densities represented by it are at energy levels in the main part of the energy distribution curve. But the density distribution at higher energy levels can at the same time drop off to very low levels. This is believed due to ineffective energy coupling. Therefore, a separ-ate measurement at a high energy level is also performed.
In this example, a helium line of emission is chosen, and :, ~'~ that is ratioed with one of the hydrogen lines, preferably the hydrogen alpha line, as a reference. This desired ,. ;i~
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A quantity of high energy electrons, repre-sented by the "tail" of the curve of Figure 5, is generally desirable for directly impinging upon the substrate since it is known that this improves the hardness of the resulting deposited film through a higher degree of film cross-linking. Stress in the film also decreases, resulting in better adhesion of the film to the substrate. A low ratio in the plasma emission of the ~ hydrogen alpha line intensity to that of helium predicts ; these beneficial results.
Use of the helium emission line in forming this second ratio is also advantageous since helium is inert.
il The gas does not combine with other gas components of the plasma. Any inert gas has this advantage, as well as providing an emission line in the "tail" portion of the curve. An inert gas is used in this example primarily for facilitating an initial source of electrons when the plasma is initiated by establishing the electric field.
~'~i But it has this additional diagnostic use, as well.
Once it is determined from the measured inten-sities and ratios that the electron energy distribution curve of Figure 5 needs to be altered for a process being ~;j performed, it can be done in any of a number of ways.
-' Increasing the excitation frequency of the power supply 17 tends to increase the average energy of the electrons, .
at least up to a point where the electrons can no longer `~l follow the rapidly changing electric field. The power of the supply 17 may affect the electron energy distri-butionr depending upon the precise geometry of the deposition chamber, an increase in power increasing the , .
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, -electron energy. Another variable that may be ad~usted is the total gas flow which changes the residence time of molecules within the plasma and increases the chance of collision. The pressure in the chamber 29 also affects molecular energy, within limits. The technique used in this specific example, however, keeps these variables at a constant level and instead changes the ratio of the flow rate of the individual gases into the reaction chamber 29.
The determination of average electron tempera-ture T from the ratio of the alpha and beta hydrogen emission line intensities is very significant. Others have suggested that the determination of electron tem-perature of a plasma from its emission spectra is very difficult, if not impossible. The mathematical rela-tionships between electron temperature and the intensity of a particular emission line have long been known.
However, these mathematical relationships also include additional unknowns such as molecular and electron densities in the plasma. With so many unknowns, it is impossible to use these equations directly to accurately determine electron temperature from an intensity of an emission line. However, if the intensities of two such emission lines from a single species within the plasma are ratioed, as is the case with the ratio of the hydrogen alpha and beta lines, these other variables are mathema-tically canceled out and no longer affect the result.
This calculation assumes a "cold" plasma, one where the average ion energy is very low when compared to the average electron energy.
Referring to Figure 7, a flow chart is provided of a controlling computer program that monitors the intensities of the three emission lines and make adjust-ments in the individual gaseous component flow rates as 1 32q 1 66 ., required to maintain the electron temperature distri-bution within acceptable limits. The process of Figure 7 can best be described as several functional modules. A
first module 101 requires information of both the desired plasma parameters and those that actually exist. It is preferable to enter a desired average electron tempera-ture T and then calculate what exists in the plasma, ase shown in Figure 7, since this permits the process operator to deal with known quantities. However, since T is proportional to the ratio of the hydrogen alpha and hydrogen beta emission lines, that ratio itself could more simply be substituted in the flow diagram of Figure 7 where T appears. It would then be that line intensity ratio to which the process is adjusted.
Once the actual and desired quantities are in the system, a next module 105 of the processing algorithm looks at the intensity ratio between the hydrogen alpha and the helium emission lines. A first step 107 compares the actual and desired ratios. If they are within range, then the processing component 105 is omitted completely by jumping to a step 109 in the next module 117. However, if the desired and actual ratios are not equal, a step 111 causes the flow meter 71 to be adjusted to change the flow . ~
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~>lA step 113 of the module 105 checks to make sure that the calculated voltage is within the range ~f the flow meter 71. If it is, the processing proceeds to a :1 step 109. If not, the process loop of module 105 is performed again. If the second calculation also results in a voltage that is not within the range of the flow meter 71, then the processing is stopped and an error message displayed for the operator, as indicated at 115.
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Once the silicon source vapor flow rate is adjusted, the next module 117 of the processing adjusts the flow of oxygen to the plasma in response to comparing the desired and actual T . If those quantities are equal within an acceptable tolerance, then the processing loops back to the beginning module 101 and performs the data acquisition and comparison functions once again, and then steps through the remainder of the program. This con-stant monitoring of the plasma characteristics allows real time control of the plasma for uniform film results and repeatability of film properties from substrate to substrate.
The program module 117 operates quite similarly to that of 105. If the newly calculated voltage for the oxygen supply flow meter is not within the range of that flow meter, as determined by the step 119, the calculation is made once more in case some error occurred. If the voltage is not within the range the second time, the processing is s~opped and an error message displayed.
Assuming, however, that the new oxygen flow meter valve control voltage is within its range, the processing is looped back to the beginning module 101 and repeated until the processing modules 101, 105 and 117 have been performed for a total of four times. After the fourth time, and if the last calculation loop resulted in a further adjustment to the oxygen flow meter, a next module 121 of processing is undertaken. After four ~imes through the silicon source and oxygen flow rate adjust-ments, it is concluded that some other adjustment must be made. Of course, the precise number of processing cycles that are allowed before going to the next calculation module 121 can vary.
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The module 121 also looks at T, but in this case adjusts the helium gas flow to the plasma chamber.
An increase of the inert gas supply provides more electrons, and a decrease in the gas fewer electrons.
The same check on the calculated voltage for the helium <, flow meter is made in the module 121 as in the modules 1~5 and 117, in step 123. Once a proper adjustment to the helium flow is made, the processing again loops back to the beginning module 101 to start the cycle over again.
Of course, there are many variations in the ; details of the process being described that can be changed without sacrificing the advantages provided by the basic emission line monitoring techniques that are so imple-i mented. The same techniques are used with other gases and even with a plasma that is part of a thin film ' sputtering system. In a sputtering system with a titan-ium target, the intensity of a 399.9 nanometer emission j line of titanium and a 301.3 nanometer emission line of i titanium-nitride are measured, for example. A ratio of the intensities of ~hese lines is used in the same manner as the hydrogen alpha to helium ratio discussed above.
Two line intensities from argon can be used to calculate the average electron temperature in this sputtering example, corresponding to the hydrogen alpha line to hydrogen beta line intensity ratio discussed above for the PECVD example.
Plasma input variables of power of the supply 17 and pressure within the chamber 29 are not included in the algorithm of Figure 7 as quantities that are adjusted automatically. It has been found satisfactory to main-'! tain those quantities fixed for at least a large :! processing batch. This is preferably accomplished by setting the control system 25 to the desired power and /
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pressure. The control system 25 is provided with astandard capability of monitoring those quantities and adjusting them, if necessary~ to maintain the constant levels that have been set.
The spectra of the plasma 51, an example being given in Fig. 3, is dependent upon the position within the plasma which is observed. That is, the intensities of the three emission peaks 81, 83 and 85, both absolutely and relatively, are different depending upon where the end of the optical fiber 23 is positioned with respect to the quartz window 24 (Fig. 1) of the reaction chamber 11.
So long as this position remains fixed and the intensity distribution across the plasma 51 does not change, the techniques of controlling that process described above optimizes it. But if it is desired to use that same process control on a different piece of equipment, for example, it is likely that the plasma will be viewed at a location with a different emission spectrum. Thus, the control system which has been optimized for one plasma emission spectrum may have to be recalibrated to operate with a spectrum having different relative intensities of peaks of interest than in the plasma for which the control system was optimized. Also, even in a single machine, the spectrum can change across the plasma due to a change in the substrate being coated, primarily in its thick-ness, any change of gases, gas flow rates, a pumping rate change, some relative change in the electrical power being delivered to the system, and similar matters.
Therefore, to further optimize the control of the plasma deposition process, a technique illustrated with respect to Figs. 8-10 maintains an end of the optical fiber medium 23 to gather light from the same relative position in the plasma, regardless of any such changes.
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As a preferred location, since it is relatively easy to locate for any plasma, the optical fiber 23 is positioned to view the plasma at the location where l:he ratio of the intensities of emission into relevant narrow band-widths is a maximum. In the example being descr.ibed, that ratio is preferred to be the intensity of the hydrogen alpha line divided by the intensity of the helium line of emission.
Referring to Figs. 8 and 9, a mechanism will be described for moving the optical fiber cable 23 with respect to the transparent window 24 of the reaction chamber in order to maintain this ratio at a maximum. The optical fiber cable 23 is preferably terminated in a long, small diameter cylindrical tube 301. The cable prefer-ably contains dozens of individual optical fibersO The purpose of the tube 301 is to limit the natural cone angle of acceptance of light of the optical fiber end so that it accepts substantially collimated light rays emitted from an area of the plasma 51 that is substantially the same size as the size of the opening of the tube 301 at an end adjacent the quartz window 24. The inside of the tube 301 is made to be highly reflective.
The light-guiding tube 301 is attached to a support block 303 that is carried with respect to the reaction chamber 11 in a manner that allows it to be moved in both X and Y directions. Appropriate control motors are u~ed to provide such movement. An example is the use of separate X and Y direction drive motors 305 and 307~
respectively, that drive the support block 303 through respective mechanical connections 309 and 311 to move the block 303 in those two directions. The motors 305 and 307 are controlled by position control circuits 313 which are in turn connected to the system computer control 25 (Fig.
1) by an appropriate circuit 315.
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A number of specific ways of determining the desired location may alternatively be implemented by the mechanism o~ Figs. 8 and 9. One way is to scan the fiber cable tube 301 in some raster pattern across the window 24, while the computer control system 25 calculates a desired ratio from information obtained at several locations of each raster scan line. The location of the . ~
block 303 where the ratio is maximized is then determined and the block returned to that position for monitoring the plasma.
~ Another one of many ways of determining the ; maximum intensity ratio location is illustrated in Fig.
`i, 10. As a first step, the tube 301 is located at four l spaced apart positions indicated at 317, 319, 321, and 1 323. The ratio of intensities is calculated for each of those locations and the maximum determined. Assuming that maximum in this example was obtained at the location 321, then the tube 301 is positioned at four ! other locations spaced around the position 321, such as positions 325, 327, 329 and 331. The maximum intensity ratio for each of these four locations is noted J and ~ another four locations tested around that location, and '`J~ SO forth.
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Although the various aspects of the present invention have been described with respect to its preferred embodiments, it will be understood that the invention is entitled to protection within the full scope of the appended claims.
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Claims (21)
1. In a process of depositing a thin film of material on a substrate in a chamber wherein a plasma is formed with a plurality of controllable process para-meters, said plasma containing a plurality of atomic and/or molecular species which each have an observable emission of electromagnetic radiation within a visible or near visible wavelength range whose nature changes upon changing said controllable process parameters, a method of controlling the process, comprising the steps of:
detecting two characteristics of the radiation emission of a single species in the plasma, electronically comparing said two character-istics, and causing one or more of said process parameters to automatically be changed in order to adjust the two detected single species radiation emission character istics to have a predetermined desired relationship.
detecting two characteristics of the radiation emission of a single species in the plasma, electronically comparing said two character-istics, and causing one or more of said process parameters to automatically be changed in order to adjust the two detected single species radiation emission character istics to have a predetermined desired relationship.
2. The method according to claim 1 wherein the detecting step includes detecting the intensities of the single species' emission in two different bandwidth regions as said two characteristics.
3. The method according to claim 2 wherein the comparing step includes electronically ratioing the intensities of the two bandwidth emissions, and wherein the automatic adjustment step includes comparing that ratio with a desired quantity.
4. A method according to claim 2 which com-prises an additional step of detecting an intensity of a defined bandwidth of emission of another species in the plasma.
5. A method according to claim 1 wherein the radiation emission detecting step includes detecting said emission at a physical location with respect to the plasma wherein a ratio of intensities within two specific narrow bandwidths of said emission is substantially maximized.
6. In a process of depositing a thin film of material on a substrate in a chamber wherein a plasma is formed with a plurality of controllable process para-meters that include pressure, individual rates of flow of two or more gases into the chamber, and an electric field, a method of controlling the process, comprising the steps of:
detecting an intensity of each of two narrow bandwidth lines of visible or near visible electro-magnetic radiation emission from a single species of the plasma, electronically calculating a ratio of said wavelength band intensities, electronically comparing said ratio with a desired ratio to be maintained during the deposition process, and causing one or more of said process parameters to automatically be changed in order to adjust the calculated ratio to reduce any difference between it and said desired ratio.
detecting an intensity of each of two narrow bandwidth lines of visible or near visible electro-magnetic radiation emission from a single species of the plasma, electronically calculating a ratio of said wavelength band intensities, electronically comparing said ratio with a desired ratio to be maintained during the deposition process, and causing one or more of said process parameters to automatically be changed in order to adjust the calculated ratio to reduce any difference between it and said desired ratio.
7. A method according to claim 6 which addi-tionally comprises the steps of:
detecting an intensity of a narrow bandwidth line of visible or near visible electromagnetic radiation emission from another species that results from an energy level that is significantly higher than that of the detected lines of said single species, electronically calculating a second ratio of emission line intensities, said second ratio being between the intensity of one of the two lines of emission from said single species and the intensity of the emission line of said another species, electronically comparing the second calculated ratio and a second desired ratio to be maintained during the deposition process, and causing one or more of said process parameters to automatically be changed in order to adjust the second calculated ratio to reduce any difference between it and the second desired ratio.
detecting an intensity of a narrow bandwidth line of visible or near visible electromagnetic radiation emission from another species that results from an energy level that is significantly higher than that of the detected lines of said single species, electronically calculating a second ratio of emission line intensities, said second ratio being between the intensity of one of the two lines of emission from said single species and the intensity of the emission line of said another species, electronically comparing the second calculated ratio and a second desired ratio to be maintained during the deposition process, and causing one or more of said process parameters to automatically be changed in order to adjust the second calculated ratio to reduce any difference between it and the second desired ratio.
8. A method according to claim 7 wherein said another species consists of an inert gas.
9. A method according to claim 6 wherein the adjusting step includes the step of automatically chang-ing the rate of flow of at least one of said gases into the chamber.
10. A method according to claim 7 wherein the second ratio adjusting step includes the step of automa-tically changing the rate of flow of at least one of said gases into the chamber.
11. A method according to claim 6 wherein the comparing step includes the step of calculating from the intensity ratio the average electron temperature of the plasma.
12. A process of depositing a thin film of material on a substrate in a chamber wherein a plasma is formed in a region of magnetic and electric fields as the result of flowing at least first and second gases into said chamber, comprising the steps of:
detecting first and second intensity levels of each of two narrow bandwidth lines of visible or near visible electromagnetic radiation emission from a single species of the plasma, detecting a third intensity level of a narrow bandwidth line of visible or near visible electromagnetic radiation emission from another species that results from an energy level that is significantly higher than that of the detected lines of said single species, electronically obtaining a first ratio of said first and second intensity levels, electronically obtaining a second ratio of said first and third intensity levels, adjusting the rate of flow of the first gas into said chamber in a manner to cause said first ratio to be maintained at a first predetermined level, and adjusting the rate of flow of the second gas into said chamber in a manner to cause said second ratio to be maintained at a second predetermined level.
detecting first and second intensity levels of each of two narrow bandwidth lines of visible or near visible electromagnetic radiation emission from a single species of the plasma, detecting a third intensity level of a narrow bandwidth line of visible or near visible electromagnetic radiation emission from another species that results from an energy level that is significantly higher than that of the detected lines of said single species, electronically obtaining a first ratio of said first and second intensity levels, electronically obtaining a second ratio of said first and third intensity levels, adjusting the rate of flow of the first gas into said chamber in a manner to cause said first ratio to be maintained at a first predetermined level, and adjusting the rate of flow of the second gas into said chamber in a manner to cause said second ratio to be maintained at a second predetermined level.
13. The process according to claim 12 wherein said second gas is characterized by having molecules in which said single species is contained in a manner that is fractionalized therefrom in the plasma, said another species is characterized by being inert, and said first gas is characterized by altering an average energy of electrons in the plasma.
14. The process according to claim 12 wherein said second gas includes oxygen.
15. The process according to claim 12 wherein said first gas includes oxygen.
16. A method according to claim 12 wherein the intensity level detecting steps detect the plasma emission intensity from a region of the plasma wherein said second intensity ratio is substantially maximized.
17. A method of determining the level of electron temperature in a plasma, comprising the steps of:
detecting an intensity of each of two narrow bandwidth lines of visible or near visible electromagnetic radiation emission from a single species of the plasma, electronically calculating a ratio of said wavelength band intensities, and electronically calculating an estimate of the average electron temperature of the plasma from said ratio.
detecting an intensity of each of two narrow bandwidth lines of visible or near visible electromagnetic radiation emission from a single species of the plasma, electronically calculating a ratio of said wavelength band intensities, and electronically calculating an estimate of the average electron temperature of the plasma from said ratio.
18. In a system wherein a thin film of material is deposited on a substrate positioned within a chamber wherein a plasma is formed according to a plurality of controllable process parameters, apparatus for controlling the deposition process, comprising:
mean optically communicating with the plasma for measuring a ratio of the intensity of at least two wavelength bands of emission therefrom, means receiving said ratio for comparing it to a predetermined desired value, and means responsive to said comparing means for adjusting at least on of said controllable process parameters in order to maintain said ratio substantially equal to said predetermined desired value.
mean optically communicating with the plasma for measuring a ratio of the intensity of at least two wavelength bands of emission therefrom, means receiving said ratio for comparing it to a predetermined desired value, and means responsive to said comparing means for adjusting at least on of said controllable process parameters in order to maintain said ratio substantially equal to said predetermined desired value.
19. The process according to claim 13 wherein said first gas includes oxygen, and said second gas includes an organosilicon vapour.
20. The method according to claim 19 wherein said first and second intensity levels are the hydrogen alpha hydrogen beta emissions and said third intensity level is a helium emission.
21. The method according to claim 20 wherein said second gas includes hexamethyldisiloxane.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US7392887A | 1987-07-15 | 1987-07-15 | |
US073,928 | 1987-07-15 | ||
US07/191,448 US4888199A (en) | 1987-07-15 | 1988-05-09 | Plasma thin film deposition process |
US191,448 | 1988-05-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1329166C true CA1329166C (en) | 1994-05-03 |
Family
ID=26755049
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA000571973A Expired - Fee Related CA1329166C (en) | 1987-07-15 | 1988-07-14 | Plasma thin film deposition process control |
Country Status (13)
Country | Link |
---|---|
US (1) | US4888199A (en) |
EP (1) | EP0299752B1 (en) |
JP (1) | JP2539000B2 (en) |
KR (1) | KR910009981B1 (en) |
CN (1) | CN1024814C (en) |
AT (1) | ATE110794T1 (en) |
AU (1) | AU616894B2 (en) |
CA (1) | CA1329166C (en) |
DE (1) | DE3851281T2 (en) |
ES (1) | ES2059523T3 (en) |
MX (1) | MX171506B (en) |
RU (1) | RU1797628C (en) |
UA (1) | UA18259A (en) |
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-
1988
- 1988-05-09 US US07/191,448 patent/US4888199A/en not_active Expired - Fee Related
- 1988-07-11 MX MX1222388A patent/MX171506B/en unknown
- 1988-07-13 ES ES88306431T patent/ES2059523T3/en not_active Expired - Lifetime
- 1988-07-13 EP EP88306431A patent/EP0299752B1/en not_active Expired - Lifetime
- 1988-07-13 AT AT88306431T patent/ATE110794T1/en not_active IP Right Cessation
- 1988-07-13 AU AU19012/88A patent/AU616894B2/en not_active Ceased
- 1988-07-13 DE DE3851281T patent/DE3851281T2/en not_active Expired - Fee Related
- 1988-07-14 CA CA000571973A patent/CA1329166C/en not_active Expired - Fee Related
- 1988-07-14 RU SU884356339A patent/RU1797628C/en active
- 1988-07-14 KR KR1019880008852A patent/KR910009981B1/en not_active IP Right Cessation
- 1988-07-14 UA UA4356339A patent/UA18259A/en unknown
- 1988-07-15 JP JP63176851A patent/JP2539000B2/en not_active Expired - Lifetime
- 1988-07-15 CN CN88104424A patent/CN1024814C/en not_active Expired - Fee Related
Also Published As
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EP0299752B1 (en) | 1994-08-31 |
DE3851281T2 (en) | 1995-04-13 |
MX171506B (en) | 1993-11-03 |
JP2539000B2 (en) | 1996-10-02 |
CN1024814C (en) | 1994-06-01 |
US4888199A (en) | 1989-12-19 |
RU1797628C (en) | 1993-02-23 |
UA18259A (en) | 1997-12-25 |
EP0299752A3 (en) | 1990-04-11 |
EP0299752A2 (en) | 1989-01-18 |
AU616894B2 (en) | 1991-11-14 |
KR890002287A (en) | 1989-04-10 |
ATE110794T1 (en) | 1994-09-15 |
CN1030615A (en) | 1989-01-25 |
ES2059523T3 (en) | 1994-11-16 |
JPS6487777A (en) | 1989-03-31 |
DE3851281D1 (en) | 1994-10-06 |
KR910009981B1 (en) | 1991-12-09 |
AU1901288A (en) | 1989-01-19 |
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