GB2323855A - Depositing a coating on a conductive substrate using positive bias and electron bombardment - Google Patents

Depositing a coating on a conductive substrate using positive bias and electron bombardment Download PDF

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Publication number
GB2323855A
GB2323855A GB9706538A GB9706538A GB2323855A GB 2323855 A GB2323855 A GB 2323855A GB 9706538 A GB9706538 A GB 9706538A GB 9706538 A GB9706538 A GB 9706538A GB 2323855 A GB2323855 A GB 2323855A
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United Kingdom
Prior art keywords
coating
conductive substrate
substrate
depositing
bias
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.)
Granted
Application number
GB9706538A
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GB2323855B (en
GB9706538D0 (en
Inventor
Allan Matthews
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ION COAT Ltd
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ION COAT Ltd
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Filing date
Publication date
Application filed by ION COAT Ltd filed Critical ION COAT Ltd
Priority to GB9706538A priority Critical patent/GB2323855B/en
Publication of GB9706538D0 publication Critical patent/GB9706538D0/en
Publication of GB2323855A publication Critical patent/GB2323855A/en
Application granted granted Critical
Publication of GB2323855B publication Critical patent/GB2323855B/en
Anticipated expiration legal-status Critical
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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/54Controlling or regulating the coating process
    • C23C14/541Heating or cooling of the substrates
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02Pretreatment of the material to be coated
    • C23C14/021Cleaning or etching treatments
    • C23C14/022Cleaning or etching treatments by means of bombardment with energetic particles or radiation
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/08Oxides
    • C23C14/083Oxides of refractory metals or yttrium
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2237/00Discharge tubes exposing object to beam, e.g. for analysis treatment, etching, imaging
    • H01J2237/30Electron or ion beam tubes for processing objects
    • H01J2237/31Processing objects on a macro-scale
    • H01J2237/3132Evaporating

Abstract

Depositing a coating on a conductive substrate includes applying a positive d.c. bias to the conductive substrate and subjecting the substrate to electron bombardment before and/or during deposition of the coating. The coating may be applied by physical vapour deposition and is preferably zirconia. In one embodiment the positive d.c. bias and a negative d.c. bias are applied alternately to the substrate. Sputter cleaning can also be carried out prior to deposition.

Description

METHOD AND APPARATUS FOR DEPOSITING A COATING ON A CORIJCTIW SUBSTRATE This invention relates to methods and apparatus for depositing a coating on a conductive substrate. The invention has considerable, though not exclusive, relevance to the deposition of metallic oxides onto conductive substrates, in particular, the metallic oxide zirconia. Whilst normally electrically insulating, zirconia becomes conducting at higher temperatures. The exact temperature will depend on the purity and structure of the coating material, but typically temperatures greater than 7000C are needed to achieve appreciable electrical conductivity.
Zirconia is an interesting material for many technological applications, especially because of its low thermal conductivity and thus its excellent thermal insulation properties. These properties are useful, for example, in the regions of gas turbine engines where combustion takes place, to protect components such as turbine blades from thermal degradation.
In order to ensure coating purity and effectively control the deposition species, a number of vacuum-based coating processes are in current use. These fall into two groups. The first employs substrate heating, by means such as radiant heaters in the coating chamber, to raise the substrate temperature; this ensures that the resulting coating, after being deposited onto the heated substrate, has improved adhesion and has a denser structure than a coating formed at near-ambient temperatures.
Also, since the deposition temperature is nearer to the operating temperature of the turbine, any in-service thermally induced stresses in the coating, caused by differential expansion or contraction of the coating relative to the substrate, will be reduced. Usually, electron beam evaporation is used to produce the coating.
There are several disadvantages of this system. One is that the adhesion of the coating (whilst improved) may still not be adequate; a second is that the heating arrangement can limit the space available within the deposition chamber, and can be inefficient in terms of electrical power consumption.
The second group of vacuum-based coating processes, in which there has been much recent research interest, employs plasmaassistance in the deposition process. This involves ionising a proportion of the depositing species, such that they are accelerated to the substrate being coated which is biased negatively, either by a direct current or radio frequency supply. This can improve the adhesion and the structure of the coatings. However, for optimal effect, additional heating means are still needed.
According to one aspect of the invention there is provided a method of depositing a coating on a conductive substrate including applying a positive d.c. bias to the conductive substrate and subjecting the substrate to energetic electron bombardment before and/or during deposition of the coating.
According to another aspect of the invention there is provided an apparatus for depositing a coating on a conductive substrate comprising means for applying a positive d.c. bias to the conductive substrate and means for subjecting the substrate to energetic electron bombardment before and/or during deposition of the coating on the conductive substrate.
A distinguishing feature of the apparatus and method of the invention is the requirement for the substrate to be held at a positive d.c. bias before and/or during deposition. Direct heating of the substrate is then accomplished with great efficiency by energetic electron bombardment which also ensures that the condition at the substrate surface is suitable for the growth of well adhered films with an excellent micro-structural morphology.
This arrangement may be combined with a plasma-assisted method such as that described in GB2261226B to produce a sequential process. However, the electron bombardment method and apparatus defined in accordance with this invention is preferably used alone, in a single stage process. Indeed, one of the advantages of the electrical bombardment method and apparatus is its relative simplicity, and low cost, by virtue of the reduction in the number of power supplies used, compared to currently available plasma processes.
A method and apparatus according to the invention are now described, by way of example only, with reference to the sole figure which is a schematic diagram of the apparatus.
Referring to the figure, the apparatus comprises a vacuum chamber 1 having a pumping port 2 which in use of the apparatus is connected to a vacuum pumping system (not shown), and a gas inlet 3. Within the chamber 1 there is provided a crucible 4 containing the source material 5 for evaporation, for example zirconia, adjacent to an electron beam arrangement 6, such as an electron beam gun, connected to a power supply 7. Also arranged within the chamber 1 is a support 8 which carries the conductive substrates 9, i.e. components, to be coated. The support 8 is connected to a d.c. power supply 10 arranged to maintain the support 8 at a positive d.c.
potential.
Between the crucible 4 and the support 8 there is provided a thermionic emitter comprising a filament 11 provided with a filament heater power supply 12 and a bias supply 13 which applies a negative d.c. bias to the filament. The filament 11 may be of any of the usual forms which will be evident to a person skilled in the art of the deposition of materials, for example a tungsten or tantalum filament.
In use, the vacuum chamber 1 is first pumped down via pumping port 2 to a pressure of less than lO-STorr. The next stage may involve increasing the chamber pressure to around l0mTorr by admitting argon gas to the chamber 1 via gas inlet 3, and then negatively biasing the substrates to several hundred volts, whereby a glow discharge or plasma will be initiated which then sputter-cleans the substrates by bombarding them with ions. This bombardment (so called "sputter-cleaning") can be intensified by heating the filament 11 and (preferably) at the same time biasing it negatively. This sputter-cleaning stage normally lasts for about twenty minutes, but is not a necessary prerequisite for the process, provided that satisfactory chemical precleaning of the substrates 9 is carried out prior to placing them in the vacuum chamber 1.
If the sputter-cleaning stage is not utilised, then the deposition process can proceed without raising the chamber pressure. Thus with a chamber pressure of about 10.STorr the substrates 9 are biased positively by supply 10 to between 50 and 500 volts At the same time, the filament 11 is heated, by passing a current through it. Electrons thus emitted are accelerated to the substrates 9 which are directly heated by the resultant energetic electron bombardment to a temperature typically greater than 7000C. The electron beam gun 6 is then activated to commence evaporation of zirconia, which ideally has an additional phase, such as yttria (typically 8 to 20 percent by weight) which stabilises the higher temperature tetragonal or cubic phases, and therefore reduces the possibility of changes in the phase composition of the coating during in-service temperature cycling.
The coating progresses in this mode for a sufficient duration to build-up an adequate coating thickness, typically 300-400 micrometers. The thickness is determined by the required inservice temperature 'drop' across the coating, i.e. the thicker the coating the greater the thermal insulation provided and thus the lower the maximum temperature attained by the component during use.
It will be appreciated that the heated filament 11 need not be negatively biassed. Alternatively, the filament could be maintained at earth potential and, in this case, the bias supply 13 could be omitted.
However, a negatively biassed filament can be advantageous in that it enables other surfaces in the earthed chamber 1 to be heated by electron bombardment. In a specific implementation of this, shields 14 are provided inside the chamber and are thermally insulated from the chamber wall. The shields 14 can be held at earth potential (like the chamber wall), and are thereby heated by bombardment with energetic electrons which are accelerated away from the negatively biassed heated filament 11. If the filament is at earth potential then this effect can be achieved by biassing the shields 14 positively.
The shields, thus provided, are effective to maintain the substrates 9 at a relatively high temperature by reducing radiative heat loss to the exterior.
It has been found that energetic electron bombardment will take place much more effectively if the atmosphere between the heated filament 11 and the substrates 9 is electrically conducting. To this end, a small amount of an ionisable gas, e.g. argon, is preferably introduced into the chamber, via inlet 3, such that the chamber pressure is slightly higher, e.g.3 x 10.STorr, to encourage the creation of a thermionically supported discharge between the filament 11 and the substrates 9. This discharge provides an electrically conducting path between the filament 9 and the substrates 11 and so enhances electron transport. Once deposition has commenced the ionisable species can also be derived from the coating material itself.
The foregoing processes can be further modified by using a pulsed power supply which alternates a positive then negative.
then positive (etc.) bias. This allows heating by energetic electron bombardment whilst the sample is positive and ion bombardment of the growing films during the negative bias periods provided the chamber pressure is sufficiently high to create a plasma. This offers additional control over the coating microstructure. However, for elements which can form negative ions (such as oxygen) the ion bombardment effect can occur when a positive bias is applied to the substrates. In this respect it can be beneficial to raise the chamber pressure to several mTorr to initiate a plasma during the process. This, however, can create certain disadvantages caused by ion bombardment of the filament (made typically of tungsten), as this may lead to incorporation of tungsten in the growing film. The effects of this can be mitigated by shielding the filament from the substrates, so that the whole of the filament is not in direct line-of-sight of the substrates. However, if a plasma is initiated with the substrates in the positively biased mode, the chamber walls will be cathodic in the resulting plasma or glow discharge, and there is then the danger of coating contamination by material from the walls. This can be mitigated by depositing the coating material onto the walls prior to the process.
However, for a material which is electrically insulating at lower temperatures this can create plasma instabilities, especially if no conducting cathode surface is available.
Thus, although the above-described sequential process may be advantageous in some applications, it is generally preferable to deposit the entire coating at low pressure (approx.10-5Torr) on a positively biased component or components which is subjected to energetic electron bombardment before and/or during deposition of the coating Since this preferred embodiment is essentially a line-of-sight process, component rotation and traversal relative to the vapour source is usually needed to ensure adequate thickness uniformity over the component surface.

Claims (20)

1. A method of depositing a coating on a conductive
substrate including applying a positive d.c. bias to the conductive substrate and subjecting the substrate to energetic electron bombardment before and/or during deposition of the coating.
2. A method as claimed in claim 1, wherein said electron bombardment is such as to heat the conductive substrate to a temperature greater than 7000C.
3. A method as claimed in claim 1 or claim 2, including applying said positive d.c. voltage in the range 50 volts to 500 volts.
4. A method as claimed in any one of claims 1 to 3, wherein said deposition takes place at a chamber pressure no greater than 3 x lO-STorr.
5. A method as claimed in any one of claims 1 to 4, including evaporating a source of the coating material so that the resultant vapour is deposited on the substrate to form the coating.
6. A method as claimed in any one of claims 1 to 5, for depositing a coating of a metal oxide.
7. A method as claimed in claim 6, for depositing a coating of zirconia.
8. A method as claimed in any one of claims 1 to 7, including sputter-cleaning the conductive substrate before the coating is deposited.
9. A method as claimed in any one of claims 1 to 8, including depositing part of the coating by a plasma-assisted physical vapour deposition technique.
10. A method as claimed in claim 9, including alternatively applying said positive d.c. bias and a negative d.c. bias to the conductive substrate whereby deposition by application of said plasma-assisted physical vapour deposition technique takes place while said negative d.c. bias is being applied.
11. An apparatus for depositing a coating on a conductive substrate comprising means for applying a positive d.c. bias to the conductive substrate and means for subjecting the substrate to energetic electron bombardment before and/or during deposition of the coating on the conductive substrate.
12. An apparatus as claimed in claim 11, including means for evaporating a source of the coating material such that the resultant vapour is deposited on the conductive substrate to form the coating.
13. An apparatus as claimed in claim 11 or claim 12, wherein the electron bombardment means is effective to heat the conductive substrate to a temperature greater than 7000C.
14. An apparatus as claimed in claim 13, wherein the electron bombardment means is a heated filament.
15. An apparatus as claimed in claim 14, wherein said heated filament is negatively biassed relative to the deposition chamber wall.
16. An apparatus as claimed in claim 15, wherein the negatively biassed heated filament causes heating of internal shield means by energetic electronic bombardment to reduce radiative cooling of the substrate.
17. An apparatus as claimed in claim 16 wherein the internal shielding means is either held at earth potential or is positively biassed.
18. An apparatus as claimed in claim 12, wherein the evaporation means is an electron beam gun.
19. A method substantially as herein described, with reference to the accompanying drawing.
20. An apparatus substantially as herein described with reference to the accompanying drawing.
GB9706538A 1997-04-01 1997-04-01 Method and apparatus for depositing a coating on a conductive substrate Expired - Lifetime GB2323855B (en)

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Application Number Priority Date Filing Date Title
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GB9706538D0 GB9706538D0 (en) 1997-05-21
GB2323855A true GB2323855A (en) 1998-10-07
GB2323855B GB2323855B (en) 2002-06-05

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000023634A1 (en) * 1998-10-21 2000-04-27 Siemens Aktiengesellschaft Method and device for cleaning a product
EP1136584A1 (en) * 2000-03-21 2001-09-26 Buechel-Pappas Trust Apparatus and method for coating prosthetic components
WO2005100631A1 (en) * 2004-04-15 2005-10-27 Bestcoating S.A.R.L. Method for coating a base body, device for carrying out said method, and coated base body
EP2369036A1 (en) * 2010-03-12 2011-09-28 United Technologies Corporation Coating apparatus and method
RU2451770C2 (en) * 2010-05-21 2012-05-27 Открытое акционерное общество "Научно-производственное объединение Энергомаш имени академика В.П. Глушко" Method for vacuum ion-plasma coating application
EP2597172A1 (en) * 2011-11-25 2013-05-29 Kabushiki Kaisha Kobe Seiko Sho Ion bombardment apparatus and method for cleaning of surface of base material using the same

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WO1989005361A1 (en) * 1987-12-04 1989-06-15 National Research Development Corporation Deposition of materials in a desired pattern on to substrates
US4941430A (en) * 1987-05-01 1990-07-17 Nihon Sinku Gijutsu Kabusiki Kaisha Apparatus for forming reactive deposition film
EP0387904A2 (en) * 1989-03-17 1990-09-19 Matsushita Electric Industrial Co., Ltd. Method of producing thin film
GB2261226A (en) * 1991-11-08 1993-05-12 Univ Hull Deposition of non-conductive material using D.C. biased, thermionically enhanced, plasma assisted PVD
US5436035A (en) * 1991-12-05 1995-07-25 Alusuisse-Lonza Services Ltd. Coating a substrate surface with a permeation barrier
US5487922A (en) * 1992-08-14 1996-01-30 Hughes Aircraft Company Surface preparation and deposition method for titanium nitride onto carbon-containing materials
EP0725161A1 (en) * 1995-01-06 1996-08-07 METAPLAS IONON Oberflächenveredelungstechnik GmbH Method for plasma treating of worked articles
WO1996024703A1 (en) * 1995-02-10 1996-08-15 Jet Process Corporation An electron jet vapor deposition system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4269137A (en) * 1979-03-19 1981-05-26 Xerox Corporation Pretreatment of substrates prior to thin film deposition
US4941430A (en) * 1987-05-01 1990-07-17 Nihon Sinku Gijutsu Kabusiki Kaisha Apparatus for forming reactive deposition film
WO1989005361A1 (en) * 1987-12-04 1989-06-15 National Research Development Corporation Deposition of materials in a desired pattern on to substrates
EP0387904A2 (en) * 1989-03-17 1990-09-19 Matsushita Electric Industrial Co., Ltd. Method of producing thin film
GB2261226A (en) * 1991-11-08 1993-05-12 Univ Hull Deposition of non-conductive material using D.C. biased, thermionically enhanced, plasma assisted PVD
US5436035A (en) * 1991-12-05 1995-07-25 Alusuisse-Lonza Services Ltd. Coating a substrate surface with a permeation barrier
US5487922A (en) * 1992-08-14 1996-01-30 Hughes Aircraft Company Surface preparation and deposition method for titanium nitride onto carbon-containing materials
EP0725161A1 (en) * 1995-01-06 1996-08-07 METAPLAS IONON Oberflächenveredelungstechnik GmbH Method for plasma treating of worked articles
WO1996024703A1 (en) * 1995-02-10 1996-08-15 Jet Process Corporation An electron jet vapor deposition system

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6602542B2 (en) 1998-10-21 2003-08-05 Siemens Aktiengesellschaft Device for cleaning an article
WO2000023634A1 (en) * 1998-10-21 2000-04-27 Siemens Aktiengesellschaft Method and device for cleaning a product
EP1136584A1 (en) * 2000-03-21 2001-09-26 Buechel-Pappas Trust Apparatus and method for coating prosthetic components
US6548104B2 (en) 2000-03-21 2003-04-15 Michael J. Pappas Apparatus and method for coating prosthetic components
WO2005100631A1 (en) * 2004-04-15 2005-10-27 Bestcoating S.A.R.L. Method for coating a base body, device for carrying out said method, and coated base body
US8328945B2 (en) 2010-03-12 2012-12-11 United Technologies Corporation Coating apparatus and method with indirect thermal stabilization
EP2369036A1 (en) * 2010-03-12 2011-09-28 United Technologies Corporation Coating apparatus and method
RU2451770C2 (en) * 2010-05-21 2012-05-27 Открытое акционерное общество "Научно-производственное объединение Энергомаш имени академика В.П. Глушко" Method for vacuum ion-plasma coating application
EP2597172A1 (en) * 2011-11-25 2013-05-29 Kabushiki Kaisha Kobe Seiko Sho Ion bombardment apparatus and method for cleaning of surface of base material using the same
US20130133690A1 (en) * 2011-11-25 2013-05-30 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Ion bombardment apparatus and method for cleaning of surface of base material using the same
CN103132013A (en) * 2011-11-25 2013-06-05 株式会社神户制钢所 Ion bombardment apparatus and method for cleaning of surface of base material using the same
CN103132013B (en) * 2011-11-25 2015-10-28 株式会社神户制钢所 Ion bombardment device and utilize the cleaning method of substrate material surface of this device
US9911576B2 (en) 2011-11-25 2018-03-06 Kobe Steel, Ltd. Ion bombardment apparatus and method for cleaning of surface of base material using the same

Also Published As

Publication number Publication date
GB2323855B (en) 2002-06-05
GB9706538D0 (en) 1997-05-21

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Expiry date: 20170331