GB1210026A - Surface treatment of nickel- and/or cobalt-based alloys - Google Patents
Surface treatment of nickel- and/or cobalt-based alloysInfo
- Publication number
- GB1210026A GB1210026A GB34866/69A GB3486669A GB1210026A GB 1210026 A GB1210026 A GB 1210026A GB 34866/69 A GB34866/69 A GB 34866/69A GB 3486669 A GB3486669 A GB 3486669A GB 1210026 A GB1210026 A GB 1210026A
- Authority
- GB
- United Kingdom
- Prior art keywords
- less
- nickel
- pickling
- metals
- seconds
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/28—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
- C23C10/34—Embedding in a powder mixture, i.e. pack cementation
- C23C10/52—Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12875—Platinum group metal-base component
-
- 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
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12944—Ni-base component
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Electroplating Methods And Accessories (AREA)
- Electroplating And Plating Baths Therefor (AREA)
Abstract
1,210,26. Coating with metals; electrolytic plating; electrolytic pickling; nickel alloy. DEUTSCHE EDELSTAHLWERKE A.G. July 10, 1969 [Sep.14, 1968], No.34866/69. Headings C7A, C7B and C7F. Nickel or cobalt alloys, used e.g. in turbine blades, are diffusion coated with aluminium and one or more metals of the platinum group e.g. Pt, Pd or Rh. The platinum group metal may be applied first or simultaneously with the Al and the Pt may be diffused before or simultaneously with the Al. A nickel alloy is degreased in a cyanide bath 10 seconds cathodically and 30 seconds anodically followed by anodic pickling in H2 SO4 and then cathodic and anodic pickling in NaOH. Pt is then electro-plated in a bath comprising (g. /1.) 13 H2 PtCl6, 45 (NH4 )3 PO4, and 240 Na2 HPO4. The coating is heated at 400‹ C. and then packed in a 5% Al 95% Al2O3 mixture and heated at 1100‹ C. in hydrogen. The alloy base may be 0À12% carbon, less than 0À25% Si, less than 0À25% Mn, 13À5% Cr, 4À5% Mo, 6À25% Al, 2À3% Nb plus Ta, less than 1% Co, 0À9% Ti, less than 1À5% iron, traces of boron and Zr, remainder Ni.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1796175A DE1796175C2 (en) | 1968-09-14 | 1968-09-14 | High temperature corrosion and scaling resistant diffusion protection layer on objects made of high temperature alloys based on nickel and / or cobalt |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1210026A true GB1210026A (en) | 1970-10-28 |
Family
ID=5708389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34866/69A Expired GB1210026A (en) | 1968-09-14 | 1969-07-10 | Surface treatment of nickel- and/or cobalt-based alloys |
Country Status (9)
Country | Link |
---|---|
US (1) | US3677789A (en) |
AT (1) | AT285277B (en) |
BE (1) | BE736266A (en) |
CH (1) | CH518376A (en) |
DE (1) | DE1796175C2 (en) |
FR (1) | FR2018097A1 (en) |
GB (1) | GB1210026A (en) |
NL (1) | NL165223C (en) |
SE (1) | SE344766B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5482578A (en) * | 1992-04-29 | 1996-01-09 | Walbar Inc. | Diffusion coating process |
GB2310435A (en) * | 1996-02-26 | 1997-08-27 | Gen Electric | High temperature alloy article with a discrete additive protective coating produced by aluminiding |
WO1999042633A1 (en) * | 1998-02-23 | 1999-08-26 | MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH | Method for producing a slip layer which is resistant to corrosion and oxidation |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3837901A (en) * | 1970-08-21 | 1974-09-24 | Gen Electric | Diffusion-coating of nickel-base superalloy articles |
US3876456A (en) * | 1973-03-16 | 1975-04-08 | Olin Corp | Catalyst for the reduction of automobile exhaust gases |
US3961910A (en) * | 1973-05-25 | 1976-06-08 | Chromalloy American Corporation | Rhodium-containing superalloy coatings and methods of making same |
US3999956A (en) * | 1975-02-21 | 1976-12-28 | Chromalloy American Corporation | Platinum-rhodium-containing high temperature alloy coating |
US3979273A (en) * | 1975-05-27 | 1976-09-07 | United Technologies Corporation | Method of forming aluminide coatings on nickel-, cobalt-, and iron-base alloys |
US4048390A (en) * | 1976-12-20 | 1977-09-13 | Electric Power Research Institute, Inc. | Na/s cell reactant container with metal aluminide coating |
DE2809444C2 (en) * | 1978-03-04 | 1984-01-26 | Degussa Ag, 6000 Frankfurt | Process for the pretreatment of light metals before electroplating |
US4965095A (en) * | 1979-03-30 | 1990-10-23 | Alloy Surfaces Company, Inc. | Method for refurbishing used jet engine hot section airfoils |
US4439470A (en) * | 1980-11-17 | 1984-03-27 | George Kelly Sievers | Method for forming ternary alloys using precious metals and interdispersed phase |
US4352840A (en) * | 1980-11-17 | 1982-10-05 | Turbine Metal Technology, Inc. | Interdispersed phase coatings method |
US4501776A (en) * | 1982-11-01 | 1985-02-26 | Turbine Components Corporation | Methods of forming a protective diffusion layer on nickel, cobalt and iron base alloys |
FR2638174B1 (en) * | 1988-10-26 | 1991-01-18 | Onera (Off Nat Aerospatiale) | METHOD FOR PROTECTING THE SURFACE OF METAL WORKPIECES AGAINST CORROSION AT HIGH TEMPERATURE, AND WORKPIECE TREATED BY THIS PROCESS |
US5132185A (en) * | 1991-06-21 | 1992-07-21 | General Electric Company | Ceramic articles having heat-sealable metallic coatings |
GB9204791D0 (en) * | 1992-03-05 | 1992-04-22 | Rolls Royce Plc | A coated article |
US5500252A (en) * | 1992-09-05 | 1996-03-19 | Rolls-Royce Plc | High temperature corrosion resistant composite coatings |
US5902638A (en) * | 1993-03-01 | 1999-05-11 | General Electric Company | Method for producing spallation-resistant protective layer on high performance alloys |
US6495271B1 (en) | 1993-03-01 | 2002-12-17 | General Electric Company | Spallation-resistant protective layer on high performance alloys |
EP0654542B1 (en) * | 1993-11-19 | 1999-03-31 | Walbar Inc. | Improved platinum group silicide modified aluminide coating process and products |
US5650235A (en) * | 1994-02-28 | 1997-07-22 | Sermatech International, Inc. | Platinum enriched, silicon-modified corrosion resistant aluminide coating |
US5427866A (en) * | 1994-03-28 | 1995-06-27 | General Electric Company | Platinum, rhodium, or palladium protective coatings in thermal barrier coating systems |
US5658614A (en) * | 1994-10-28 | 1997-08-19 | Howmet Research Corporation | Platinum aluminide CVD coating method |
US5667663A (en) * | 1994-12-24 | 1997-09-16 | Chromalloy United Kingdom Limited | Method of applying a thermal barrier coating to a superalloy article and a thermal barrier coating |
GB9426257D0 (en) * | 1994-12-24 | 1995-03-01 | Rolls Royce Plc | Thermal barrier coating for a superalloy article and method of application |
DE69615517T2 (en) | 1995-12-22 | 2002-05-16 | General Electric Co., Schenectady | Body with high temperature protective layer and method for coating |
US6066405A (en) * | 1995-12-22 | 2000-05-23 | General Electric Company | Nickel-base superalloy having an optimized platinum-aluminide coating |
US5788823A (en) * | 1996-07-23 | 1998-08-04 | Howmet Research Corporation | Platinum modified aluminide diffusion coating and method |
FR2757181B1 (en) * | 1996-12-12 | 1999-02-12 | Snecma | PROCESS FOR PRODUCING A HIGH EFFICIENCY PROTECTIVE COATING AGAINST HIGH TEMPERATURE CORROSION FOR SUPERALLOYS, PROTECTIVE COATING OBTAINED BY THIS PROCESS AND PARTS PROTECTED BY THIS COATING |
US6458473B1 (en) | 1997-01-21 | 2002-10-01 | General Electric Company | Diffusion aluminide bond coat for a thermal barrier coating system and method therefor |
DE19820944A1 (en) * | 1998-04-30 | 1999-11-11 | Manuel Hertter | Catalyst for reducing metal oxides |
US6132520A (en) | 1998-07-30 | 2000-10-17 | Howmet Research Corporation | Removal of thermal barrier coatings |
EP1099775A1 (en) * | 1999-11-12 | 2001-05-16 | General Electric Company | Platinum aluminide coating for cobalt-based superalloys |
US6589668B1 (en) | 2000-06-21 | 2003-07-08 | Howmet Research Corporation | Graded platinum diffusion aluminide coating |
CA2440573C (en) * | 2002-12-16 | 2013-06-18 | Howmet Research Corporation | Nickel base superalloy |
US7273662B2 (en) * | 2003-05-16 | 2007-09-25 | Iowa State University Research Foundation, Inc. | High-temperature coatings with Pt metal modified γ-Ni+γ′-Ni3Al alloy compositions |
DE10336989B4 (en) * | 2003-08-12 | 2006-11-09 | Mtu Aero Engines Gmbh | Process for the preparation of hot gas corrosion protection coatings |
EP1784517B1 (en) * | 2004-08-18 | 2009-06-10 | Iowa State University Research Foundation, Inc. | HIGH-TEMPERATURE COATINGS AND BULK -Ni+ '-Ni3Al ALLOYS MODIFIED WITH PT GROUP METALS HAVING HOT-CORROSION RESISTANCE |
US7531217B2 (en) * | 2004-12-15 | 2009-05-12 | Iowa State University Research Foundation, Inc. | Methods for making high-temperature coatings having Pt metal modified γ-Ni +γ′-Ni3Al alloy compositions and a reactive element |
US7371428B2 (en) * | 2005-11-28 | 2008-05-13 | Howmet Corporation | Duplex gas phase coating |
US8123872B2 (en) | 2006-02-22 | 2012-02-28 | General Electric Company | Carburization process for stabilizing nickel-based superalloys |
ES2859572T3 (en) | 2013-04-26 | 2021-10-04 | Howmet Corp | Electrodeposition of the component of the internal wing profile |
JP6226231B2 (en) | 2013-09-18 | 2017-11-08 | 株式会社Ihi | Heat-shielding coated Ni alloy part and manufacturing method thereof |
CA2866479C (en) | 2013-12-20 | 2021-08-17 | Will N. Kirkendall | Internal turbine component electroplating |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3345197A (en) * | 1963-08-09 | 1967-10-03 | Howmet Corp | Aluminizing process and composition |
FR1369892A (en) * | 1963-09-25 | 1964-08-14 | Coast Metals | Method of applying metallic coatings |
-
1968
- 1968-09-14 DE DE1796175A patent/DE1796175C2/en not_active Expired
-
1969
- 1969-07-10 GB GB34866/69A patent/GB1210026A/en not_active Expired
- 1969-07-18 BE BE736266D patent/BE736266A/xx not_active IP Right Cessation
- 1969-07-25 CH CH1144669A patent/CH518376A/en not_active IP Right Cessation
- 1969-08-05 FR FR6926802A patent/FR2018097A1/fr active Pending
- 1969-08-05 AT AT752369A patent/AT285277B/en active
- 1969-09-08 SE SE12359/69A patent/SE344766B/xx unknown
- 1969-09-10 US US856539A patent/US3677789A/en not_active Expired - Lifetime
- 1969-09-12 NL NL6913933.A patent/NL165223C/en not_active IP Right Cessation
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5482578A (en) * | 1992-04-29 | 1996-01-09 | Walbar Inc. | Diffusion coating process |
GB2310435A (en) * | 1996-02-26 | 1997-08-27 | Gen Electric | High temperature alloy article with a discrete additive protective coating produced by aluminiding |
US5897966A (en) * | 1996-02-26 | 1999-04-27 | General Electric Company | High temperature alloy article with a discrete protective coating and method for making |
GB2310435B (en) * | 1996-02-26 | 2000-03-22 | Gen Electric | High temperature alloy article with a discrete additive protective coating and method for making |
WO1999042633A1 (en) * | 1998-02-23 | 1999-08-26 | MTU MOTOREN- UND TURBINEN-UNION MüNCHEN GMBH | Method for producing a slip layer which is resistant to corrosion and oxidation |
US6440499B1 (en) | 1998-02-23 | 2002-08-27 | Mtu Aero Engines Gmbh | Method for producing a slip layer which is resistant to corrosion and oxidation |
Also Published As
Publication number | Publication date |
---|---|
US3677789A (en) | 1972-07-18 |
BE736266A (en) | 1969-12-31 |
DE1796175C2 (en) | 1974-05-30 |
NL165223C (en) | 1981-03-16 |
AT285277B (en) | 1970-10-27 |
SE344766B (en) | 1972-05-02 |
FR2018097A1 (en) | 1970-05-29 |
NL165223B (en) | 1980-10-15 |
CH518376A (en) | 1972-01-31 |
DE1796175B1 (en) | 1971-07-01 |
NL6913933A (en) | 1970-03-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PE20 | Patent expired after termination of 20 years |