US3679460A - Composite wear resistant material and method of making same - Google Patents
Composite wear resistant material and method of making same Download PDFInfo
- Publication number
- US3679460A US3679460A US79090A US3679460DA US3679460A US 3679460 A US3679460 A US 3679460A US 79090 A US79090 A US 79090A US 3679460D A US3679460D A US 3679460DA US 3679460 A US3679460 A US 3679460A
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- US
- United States
- Prior art keywords
- coating
- thickness
- metal oxide
- surface
- applied
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- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
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- 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
- C23C24/00—Coating starting from inorganic powder
-
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
- C23C4/11—Oxides
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24355—Continuous and nonuniform or irregular surface on layer or component [e.g., roofing, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
Abstract
Description
BEST AVAILABLE COPY u y 1972 E. D. REID 3,679,460
COMPOSITE WEAR RESISTANT MATERIAL AND METHOD OF MAKING SAME Filed O0t. a, 1970 4 Sheets-Sheet 1 IOO- (ROUGHNESS-A. A.)
l l I l l l l l l I u l I; GRIT- .001" .002" .003" .004 .005'. .006" .007" .008 .009- 0:0
BLAST (THICKNESS) INVENTOR EDV J IN DURHAM REID July 25, 1972 Filed Oc t. a. 1970 BEST AVAILABLE COPY E. ol REID 3,679,460
COMPOSITE WEAR RESISTANT MATERIAL AND METHOD OF MAKING SAME 4 Sheets-Sheet 2 I l .OOI" .002" .003" .004." .005" .006" .00?" .008" .009" .OIO"
(THICKNESS) INVENTOR EDWIN DURHAM REID ATTORNEY July 25, 1972 Filed Oct. 8, 1970 (ROUGHNESS -A.A.)
BESTAVAJLABLE COPY E. o; REID 3,679,460
COMPOSITE WEA RESISTANT MATERIAL AND METHOD OF MAKING SAME 4 Sheets-Sheet 5 Blast l l I I l I II I II I I II I ll I I I I l em- .ool" .002 .003 -.004 .005" .006 .00? .008 .009 .0|0'
(THICKNESS) 0,
INVENTOR ATTORNEY July 25, 1972 E. D. REID BEST AVAILABLE COPY Filed Oct. 8. 1970 4 Sheets-Sheet 4 l l l l l l l l l l l J l I l,,l l,,l l.lw l l l 1 GRIT- .001 .002 .003 .004 .005 .006 .007 .008 .009 .010
BLAST (THICKNESS) iNVENTQR ATTORNEY United States Patent Int. Cl. C2311 5/10 U.S. Cl. 117-931 PF 7 Claims ABSTRACT OF THE DISCLOSURE -A method of forming a metal oxide coating upon a workpiece, which coating may have a closely controlled surface roughness over a wide range of coating thicknesses. The method consists of applying a metal oxide base coating by an arc torch deposition process and thereafter applying a top surface coating of metal oxide with a detonation gun deposition process. A wear-resistant composite coating having an arc torch-applied base portion with a roughness of 100 AA. to 150 AA. combined with a detonation gun-applied top surface coating having surface roughness of 150 AA. to 450 AA. is also disclosed as a preferred textile surface.
This application is a continuation-in-part of application Ser. No. 20,582, filed Mar. 18, 1970, and now abandoned.
This invention relates to a ceramic coated workpiece and more particularly to ceramic coated workpieces for the textile industry which have closely controlled surface roughness over a wide range of coating thicknesses.
It has heretofore been proposed to coat workpieces with ceramic metal oxide materials such as chrome oxide, aluminum oxide, and the like, for increasing the wear resistance of the workpiece when the same is contacted by a moving textile fiber. In order that the textile fiber pass over the ceramic surface without being damaged, it has been necessary to closely control the roughness of the ceramic surface.
It is often desirable that a ceramic coating have not only a specified surface roughness, but that it have this roughness with a specified coating thickness.
Since it has heretofore been found that with any given process for forming the ceramic coating the surface roughness varies as a function of the thickness of the coating, it has been extremely diflicult to meet many specifications requiring certain combinations of roughness and coating thickness, i.e., it has not been possible to control the surface roughness of a ceramic coating independently of its thickness over a substantial thickness range.
One solution to overcoming this difliculty has been to utilize a metal base coating, such as nickel or aluminum, to build up the workpiece to some intermediate thickness followed by applying an arc torch coating of ceramic material on top of the base metal to the desired roughness. This procedure is not only expensive, but also prevents the easy removal of the entire coating to expose the original workpiece, i.e., grinding or turning is necessary to remove the metal undercoat after the top coating has been removed by a grit blast operation;
One object of the invention is to provide a wear-resistant textile fiber compatible ceramic coating which can have a roughness substantially independent of its thickness over a substantial coating thickness range.
Another object is to provide a ceramic coating which is compatible with a textile fiber moving in contact therewith, which coating is also totally removable by grit blasting and without the need for grinding or turning.
3,679,460 Patented July 25, 1972 Other objects and advantages of the invention will be apparent from the following disclosure and appended claims.
In the drawings:
FIG. 1 is a diagram in the nature of a graph showing the relationship of surface roughness versus coating thickness for an aluminum oxide coating applied to a workpiece with an arc torch of the type disclosed in U.S. Pat. No. 3,016,447;
FIG. 2 is a diagram in the nature of a graph showing surface roughness of an aluminum oxide coating versus coating thickness when the same is applied to a workpiece with a detonation gun as disclosed in U.S. Pat. No. 2,714,563;
FIG. 3 is a graph showing the relationship of surface roughness versus coating thickness for a chrome oxide coating applied to a workpiece with an arc torch of the type disclosed in U.S. Pat. No. 3,016,447; and
FIG. 4 is a graph showing the relationship of surface roughness versus coating thickness for a chrome oxide coating applied to a workpiece with a detonation gun as disclosed in U.S. Pat. No. 2,714,563.
Briefly, this invention is based upon the discovery that a ceramic metal oxide coating when applied with a detonation gun will adhere tenaciously to a previously formed metal oxide coating applied to a workpiece with an arc torch.
'It has also been found that the resultant composite ceramic material can be easily removed from the workpiece in a single grit blasting operation.
The surface roughness to thickness variation of a metal oxide coating applied with a detonation gun differs substantially from the same metal oxide coating when applied with an arc torch. A combination of an arc torch-applied base coating having a certain thickness with a top coating applied by the detonation gun to the same or different thickness can be used as an effective process for achieving a desired roughness over a much wider range of coating thicknesses than could be attained by either the arc torch process or the detonation gun process utilized alone.
While the arc torch-applied base coating and the detonation gun-applied top surface coating will usually have the same chemical composition, different metal oxides may also be used if necessary to obtain a desired specification of roughness and coating thickness.
More specifically, a composite wear-resistant ceramic material having a surface compatible to textile fiber may be formed according to the invention. Such material comprises in combination with a workpiece, a metal oxide base coating on the workpiece having a surface roughness of between 70 AA. and AA. and a top coating of metal oxide on top of the base coating having a surface roughness of between 150 AA. and 450 AA. The composite material is formed with a base coating thickness of .001" to 015", the top coating provided as a thickness of .001" to .010". :Preferred metal oxide materials are aluminum oxide and chrome oxide.
The surface roughness terminology and measurements as used throughout the specification and claims are in microinches and the reference A.A. refers to the arithmetical average of the same.
In practice a workpiece, for example, is one formed of aluminum or steel, which is first chemically cleaned with a suitable degreasing solvent, such as trichloroethylene. Thereafter the workpiece surface to be coated is grit blasted with a dry, free-flowing aluminum oxide blasting grain grit, e.g., #30 to #60 mesh grain size.
The workpiece is next subjected to a continuous stream of aluminum oxide or chrome oxide material which has been electrically are heated by a high temperature arc" torch device which causes the metal oxide material to be formed into a high velocity molten stream. When the molten stream from the arc torch impinges upon the surface oftheworkpiece a coating having tenacious bond is formed thereon. V v r The amount of metal oxide deposited by the arc torch is determined by first determining the thickness of the detonation gun-applied metal oxide coating which corresponds with the surface roughness required. Thereafter the thickness of coating to be applied by the arc torch is determined by subtracting from the total thickness of coating desired, the thickness of the detonation gunapplied coating necessary to attain the required roughness.
The invention will now. be illustrated by referring to the following examples.
EXAMPLE NO. 1
It is desired to form aluminum oxide coating having a surface roughness of 150 A.A. to 250 A.A. and a thickness of .0075". As shown in FIG. 1, the roughness of a .0075" thick arc torch-applied coating would be approximately 125 A.A., which is substantially less than required.
Referring to FIG. 2, a .0075 thick detonation gunapplied coating would have a roughness of about 350 A.A., which is substantially higher than the roughness required. According to the invention, a roughness of 200 A.A. (the midpoint between the 150 A.A. and 250 A.A. required) of a detonation gun-applied coating would correspond with a coating thickness of about .003". Since the total coatingthickness in this instance is .0075", the amount of base coating to be applied with an arc torch will be about .0075" minus .003" or .0045".
EXAMPLE NO. 2
It is desired to form an aluminum oxide coating having a surface roughness of 250 A.A. to 350 A.A. and a coating thickness of .015". As shown in FIG. 1, an arc torchapplied aluminum oxide coating will not offer sufficient roughness to meet the required specification. As shown in FIG. 2, however, a detonation gun-applied aluminum J oxide coating having a surface roughness of 300 (the middle between 250 A.A. and 350 A.A.) corresponds with a coating thickness of .006". In order to meet the surface roughness and thickness specification an arc torch- ,formed base coating of aluminum oxide is applied to a thickness of .015 minus .006". The top coating of alumiemployed to provide a top coating detonation gun-de- (a) spraying" an electrically arc-lheat ed continuous stream of metal oxide material onto'the surface of the workpiece to form a base coating thereon and r thereafter, I (b) spraying by detonation gun means a pulsed highvelocity stream of molten metal'oxide particles on top of said base coating to form a top coating thereon.
. 2. The method of claim 1, wherein said metal oxide is in each instance aluminum oxide. 3. The method of claim 1, wherein said metal 7 oxide is m each instance chrome oxide.
4. A method as claimed in claim 1, wherein step (a) is continued until a base coating having a thickness of 0.001 inch to 0.015 inch is formed and thereafter step (b) is continued until said top coating has a thickness of 0.001 inch to 0.010 inch. J
5. A composite wear resistant material comprising a workpiece having on its surface a metal oxide base coating 1 between 0.001 inch and 0.015 inch thick with a surface roughness between A.A. and 150 A.A., and a top coating of a metal oxide on top of said base coating between 0.001 and 0.010 inch thick with asurface roughness of between 150 A.A. and 450 A.A. 7
6. The composite material of claim 5 wherein said base coating is aluminum oxide having a surface roughness between A.A. and A.A., and wherein said top coatingis aluminum oxide having a surface roughness of between 150 A.A. and 450 A.A.
7. The composite material as in claim 5 whereinfsaid base coating is chrome oxide having a surface roughness. of between 70 A.A. and 150 A.A., and wherein said top coating is chrome oxide having a surface roughness of a between 150 A.A. and 275 A.A.
References Cited I UNITED STATES PATENTS 3,080,134 3/1963 England et al. 117-129 X 3,091,548 5/1963 Dillon 117-429 X ALFRED L. LEAVITI, Primary Examiner A J. H. NEWSOME, Assistant Examiner US. Cl. X.R. 117-1052, 129
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US7909070A true | 1970-10-08 | 1970-10-08 |
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US3679460A true US3679460A (en) | 1972-07-25 |
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US79090A Expired - Lifetime US3679460A (en) | 1970-10-08 | 1970-10-08 | Composite wear resistant material and method of making same |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3836394A (en) * | 1971-07-29 | 1974-09-17 | Alusuisse | Method of manufacture of a conductor rail |
US4311283A (en) * | 1980-07-18 | 1982-01-19 | Bounds William E | Condiment grater |
FR2577471A1 (en) * | 1985-02-15 | 1986-08-22 | Aerospatiale | layered refractory wall structure and provided with such a refractory structure |
EP0287023A2 (en) * | 1987-04-14 | 1988-10-19 | Castolin S.A. | Process for producing a sprayed surface with a particular roughness, and its use |
US20050089699A1 (en) * | 2003-10-22 | 2005-04-28 | Applied Materials, Inc. | Cleaning and refurbishing chamber components having metal coatings |
US20060105182A1 (en) * | 2004-11-16 | 2006-05-18 | Applied Materials, Inc. | Erosion resistant textured chamber surface |
US20060110620A1 (en) * | 2004-11-24 | 2006-05-25 | Applied Materials, Inc. | Process chamber component with layered coating and method |
US20070173059A1 (en) * | 2005-11-25 | 2007-07-26 | Applied Materials, Inc. | Process kit components for titanium sputtering chamber |
US20070283884A1 (en) * | 2006-05-30 | 2007-12-13 | Applied Materials, Inc. | Ring assembly for substrate processing chamber |
US7670436B2 (en) | 2004-11-03 | 2010-03-02 | Applied Materials, Inc. | Support ring assembly |
US7762114B2 (en) | 2005-09-09 | 2010-07-27 | Applied Materials, Inc. | Flow-formed chamber component having a textured surface |
US7942969B2 (en) | 2007-05-30 | 2011-05-17 | Applied Materials, Inc. | Substrate cleaning chamber and components |
US7964085B1 (en) | 2002-11-25 | 2011-06-21 | Applied Materials, Inc. | Electrochemical removal of tantalum-containing materials |
US7981262B2 (en) | 2007-01-29 | 2011-07-19 | Applied Materials, Inc. | Process kit for substrate processing chamber |
US8617672B2 (en) | 2005-07-13 | 2013-12-31 | Applied Materials, Inc. | Localized surface annealing of components for substrate processing chambers |
US9127362B2 (en) | 2005-10-31 | 2015-09-08 | Applied Materials, Inc. | Process kit and target for substrate processing chamber |
-
1970
- 1970-10-08 US US79090A patent/US3679460A/en not_active Expired - Lifetime
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3836394A (en) * | 1971-07-29 | 1974-09-17 | Alusuisse | Method of manufacture of a conductor rail |
US4311283A (en) * | 1980-07-18 | 1982-01-19 | Bounds William E | Condiment grater |
FR2577471A1 (en) * | 1985-02-15 | 1986-08-22 | Aerospatiale | layered refractory wall structure and provided with such a refractory structure |
EP0193429A1 (en) * | 1985-02-15 | 1986-09-03 | AEROSPATIALE Société Nationale Industrielle | Refractory multilayer structure and wall provided with this structure |
EP0287023A2 (en) * | 1987-04-14 | 1988-10-19 | Castolin S.A. | Process for producing a sprayed surface with a particular roughness, and its use |
EP0287023A3 (en) * | 1987-04-14 | 1990-06-20 | Castolin S.A. | Process for producing a sprayed surface with a particular roughness, and its use |
US9068273B2 (en) | 2002-11-25 | 2015-06-30 | Quantum Global Technologies LLC | Electrochemical removal of tantalum-containing materials |
US7964085B1 (en) | 2002-11-25 | 2011-06-21 | Applied Materials, Inc. | Electrochemical removal of tantalum-containing materials |
US20050089699A1 (en) * | 2003-10-22 | 2005-04-28 | Applied Materials, Inc. | Cleaning and refurbishing chamber components having metal coatings |
US7910218B2 (en) | 2003-10-22 | 2011-03-22 | Applied Materials, Inc. | Cleaning and refurbishing chamber components having metal coatings |
US7670436B2 (en) | 2004-11-03 | 2010-03-02 | Applied Materials, Inc. | Support ring assembly |
US20060105182A1 (en) * | 2004-11-16 | 2006-05-18 | Applied Materials, Inc. | Erosion resistant textured chamber surface |
US20060110620A1 (en) * | 2004-11-24 | 2006-05-25 | Applied Materials, Inc. | Process chamber component with layered coating and method |
US7579067B2 (en) | 2004-11-24 | 2009-08-25 | Applied Materials, Inc. | Process chamber component with layered coating and method |
WO2006073585A3 (en) * | 2004-11-24 | 2006-09-08 | Applied Materials Inc | Process chamber component with layered coating and method |
US20100086805A1 (en) * | 2004-11-24 | 2010-04-08 | Applied Materials, Inc. | Process chamber component with layered coating and method |
WO2006073585A2 (en) * | 2004-11-24 | 2006-07-13 | Applied Materials, Inc. | Process chamber component with layered coating and method |
CN101065510B (en) | 2004-11-24 | 2011-04-06 | 应用材料股份有限公司 | Process chamber component with layered coating and method |
US8021743B2 (en) | 2004-11-24 | 2011-09-20 | Applied Materials, Inc. | Process chamber component with layered coating and method |
US8617672B2 (en) | 2005-07-13 | 2013-12-31 | Applied Materials, Inc. | Localized surface annealing of components for substrate processing chambers |
US9481608B2 (en) | 2005-07-13 | 2016-11-01 | Applied Materials, Inc. | Surface annealing of components for substrate processing chambers |
US7762114B2 (en) | 2005-09-09 | 2010-07-27 | Applied Materials, Inc. | Flow-formed chamber component having a textured surface |
US9127362B2 (en) | 2005-10-31 | 2015-09-08 | Applied Materials, Inc. | Process kit and target for substrate processing chamber |
US20070173059A1 (en) * | 2005-11-25 | 2007-07-26 | Applied Materials, Inc. | Process kit components for titanium sputtering chamber |
US8790499B2 (en) | 2005-11-25 | 2014-07-29 | Applied Materials, Inc. | Process kit components for titanium sputtering chamber |
US20070283884A1 (en) * | 2006-05-30 | 2007-12-13 | Applied Materials, Inc. | Ring assembly for substrate processing chamber |
US7981262B2 (en) | 2007-01-29 | 2011-07-19 | Applied Materials, Inc. | Process kit for substrate processing chamber |
US8980045B2 (en) | 2007-05-30 | 2015-03-17 | Applied Materials, Inc. | Substrate cleaning chamber and components |
US7942969B2 (en) | 2007-05-30 | 2011-05-17 | Applied Materials, Inc. | Substrate cleaning chamber and components |
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