GB1258833A - - Google Patents
Info
- Publication number
- GB1258833A GB1258833A GB1258833DA GB1258833A GB 1258833 A GB1258833 A GB 1258833A GB 1258833D A GB1258833D A GB 1258833DA GB 1258833 A GB1258833 A GB 1258833A
- Authority
- GB
- United Kingdom
- Prior art keywords
- components
- pack
- aluminides
- aluminide
- superalloys
- 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
- C23C10/60—After-treatment
-
- 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
- C23C10/36—Embedding in a powder mixture, i.e. pack cementation only one element being diffused
- C23C10/48—Aluminising
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
-
- 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
- Y10T428/12937—Co- or Ni-base component next to Fe-base component
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,258,833. Pack aluminizing aluminide coated Ni superalloys. UNITED AIRCRAFT CORP. Oct. 17, 1969 [Oct. 25, 1968], No.51020/69. Heading C7F. Aluminide coated Ni superalloy components which have been subjected to oxidation erosion e.g. gas turbine components, are repaired prior to coating failure by cleaning the component surface to remove oxides without stripping the aluminide coating and then pack aluminizing the components in a pack composition such that aluminides with an Al content in excess of that of the monoaluminide is formed. The components are than heat treated to convert at least some of the aluminides to aluminides having an Al content less than that of Ni 2 Al 3 . The pack mixture contains by weight 5-20% Al, 0À5-3% NH 4 , Cl, balance Al 2 O 3 and is heated to 649-871 C. in inert atmosphere with the components embedded in the mixture. A minimum coating thickness of 76À2 microns is formed, heat treatment is then effected at 1038-1204 C. Several different examples of Ni superalloys are given.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77085368A | 1968-10-25 | 1968-10-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1258833A true GB1258833A (en) | 1971-12-30 |
Family
ID=25089896
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1258833D Expired GB1258833A (en) | 1968-10-25 | 1969-10-17 |
Country Status (8)
Country | Link |
---|---|
US (1) | US3544348A (en) |
BE (1) | BE740776A (en) |
CH (1) | CH540346A (en) |
ES (1) | ES372871A1 (en) |
FR (1) | FR2021543A1 (en) |
GB (1) | GB1258833A (en) |
NL (1) | NL153276B (en) |
SE (1) | SE344767B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2213841A (en) * | 1987-12-17 | 1989-08-23 | Mtu Muenchen Gmbh | Aluminium diffusion coating of titanium |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3647517A (en) * | 1970-06-22 | 1972-03-07 | Chromalloy American Corp | Impact resistant coatings for cobalt-base superalloys and the like |
IL36735A0 (en) * | 1970-08-19 | 1971-06-23 | Chromalloy American Corp | The coating of nickel-base and cobalt-base superalloys and the like |
US3837901A (en) * | 1970-08-21 | 1974-09-24 | Gen Electric | Diffusion-coating of nickel-base superalloy articles |
US3922474A (en) * | 1971-07-01 | 1975-11-25 | United States Borax Chem | Cold-pressed refractory materials |
US3839898A (en) * | 1972-11-22 | 1974-10-08 | United Aircraft Corp | Determination of thermal profile history of high temperature parts |
US3887731A (en) * | 1973-04-23 | 1975-06-03 | Chromalloy American Corp | Corrosion resistant coating system for ferrous metal articles having brazed joints |
US3953647A (en) * | 1973-10-05 | 1976-04-27 | United Technologies Corporation | Graphite fiber reinforced metal matrix composite |
US4128522A (en) * | 1976-07-30 | 1978-12-05 | Gulf & Western Industries, Inc. | Method and maskant composition for preventing the deposition of a coating on a substrate |
US4181758A (en) * | 1976-07-30 | 1980-01-01 | Gulf & Western Industries, Inc. | Method for preventing the deposition of a coating on a substrate |
US4729799A (en) * | 1986-06-30 | 1988-03-08 | United Technologies Corporation | Stress relief of single crystal superalloy articles |
US4944858A (en) * | 1988-12-08 | 1990-07-31 | United Technologies Corporation | Method for applying diffusion aluminide coating |
EP0496935B1 (en) * | 1991-01-31 | 1995-04-19 | General Electric Company | Aluminide processing of articles protected by a thermal barrier coating system |
US5161898A (en) * | 1991-07-05 | 1992-11-10 | Camco International Inc. | Aluminide coated bearing elements for roller cutter drill bits |
GB9116332D0 (en) * | 1991-07-29 | 1991-09-11 | Diffusion Alloys Ltd | Refurbishing of corroded superalloy or heat resistant steel parts and parts so refurbished |
GB9218859D0 (en) * | 1992-09-05 | 1992-10-21 | Rolls Royce Plc | Aluminide-silicide coatings |
US5538796A (en) * | 1992-10-13 | 1996-07-23 | General Electric Company | Thermal barrier coating system having no bond coat |
US6333121B1 (en) * | 1992-10-13 | 2001-12-25 | General Electric Company | Low-sulfur article having a platinum-aluminide protective layer and its preparation |
US6689422B1 (en) * | 1994-02-16 | 2004-02-10 | Howmet Research Corporation | CVD codeposition of A1 and one or more reactive (gettering) elements to form protective aluminide coating |
US5650235A (en) * | 1994-02-28 | 1997-07-22 | Sermatech International, Inc. | Platinum enriched, silicon-modified corrosion resistant aluminide coating |
EP0713957A1 (en) * | 1994-11-25 | 1996-05-29 | FINMECCANICA S.p.A. AZIENDA ANSALDO | Method of repairing the coating of turbine blades |
US5897966A (en) * | 1996-02-26 | 1999-04-27 | General Electric Company | High temperature alloy article with a discrete protective coating and method for making |
US6022632A (en) * | 1996-10-18 | 2000-02-08 | United Technologies | Low activity localized aluminide coating |
US5813118A (en) * | 1997-06-23 | 1998-09-29 | General Electric Company | Method for repairing an air cooled turbine engine airfoil |
US6110262A (en) * | 1998-08-31 | 2000-08-29 | Sermatech International, Inc. | Slurry compositions for diffusion coatings |
US6071622A (en) * | 1998-10-30 | 2000-06-06 | Beesabathina; Durga Prasad | Stabilized two-phase-glass diffusion barrier |
US6042880A (en) * | 1998-12-22 | 2000-03-28 | General Electric Company | Renewing a thermal barrier coating system |
US6233822B1 (en) * | 1998-12-22 | 2001-05-22 | General Electric Company | Repair of high pressure turbine shrouds |
US6203847B1 (en) | 1998-12-22 | 2001-03-20 | General Electric Company | Coating of a discrete selective surface of an article |
US6228510B1 (en) | 1998-12-22 | 2001-05-08 | General Electric Company | Coating and method for minimizing consumption of base material during high temperature service |
EP1123987A1 (en) * | 2000-02-11 | 2001-08-16 | General Electric Company | Repairable diffusion aluminide coatings |
US6482470B1 (en) * | 2000-07-18 | 2002-11-19 | General Electric Company | Diffusion aluminide coated metallic substrate including a thin diffusion portion of controlled thickness |
US6605364B1 (en) | 2000-07-18 | 2003-08-12 | General Electric Company | Coating article and method for repairing a coated surface |
US6465040B2 (en) | 2001-02-06 | 2002-10-15 | General Electric Company | Method for refurbishing a coating including a thermally grown oxide |
EP1298230A1 (en) * | 2001-10-01 | 2003-04-02 | Siemens Aktiengesellschaft | Process for removing corrosion products from metallic parts |
US20040180232A1 (en) * | 2003-03-12 | 2004-09-16 | General Electric Company | Selective region vapor phase aluminided superalloy articles |
US7163718B2 (en) * | 2003-10-15 | 2007-01-16 | General Electric Company | Method of selective region vapor phase aluminizing |
DE102004059762A1 (en) * | 2004-12-11 | 2006-06-14 | Mtu Aero Engines Gmbh | Method of repairing turbine blades |
US8038894B2 (en) * | 2006-11-29 | 2011-10-18 | General Electric Company | Method of selectively stripping an engine-run ceramic coating |
DE102008019296A1 (en) * | 2008-04-16 | 2009-10-22 | Rolls-Royce Deutschland Ltd & Co Kg | Process for producing a fire protection for titanium component bodies of an aircraft gas turbine and titanium component body for an aircraft gas turbine |
DE102012010602A1 (en) | 2012-05-30 | 2013-12-05 | Dechema-Forschungsinstitut | Process for coating a cobalt, nickel and / or iron containing substrate with a corrosion resistant layer |
US9771644B2 (en) | 2013-11-08 | 2017-09-26 | Praxair S.T. Technology, Inc. | Method and apparatus for producing diffusion aluminide coatings |
US10053779B2 (en) * | 2016-06-22 | 2018-08-21 | General Electric Company | Coating process for applying a bifurcated coating |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3129069A (en) * | 1956-10-11 | 1964-04-14 | Gen Motors Corp | Oxidation-resistant turbine blades |
US3079276A (en) * | 1960-10-14 | 1963-02-26 | Union Carbide Corp | Vapor diffusion coating process |
US3141744A (en) * | 1961-06-19 | 1964-07-21 | Dwight E Couch | Wear-resistant nickel-aluminum coatings |
US3345197A (en) * | 1963-08-09 | 1967-10-03 | Howmet Corp | Aluminizing process and composition |
US3257230A (en) * | 1964-03-24 | 1966-06-21 | Chromalloy American Corp | Diffusion coating for metals |
GB1063412A (en) * | 1966-02-23 | 1967-03-30 | Rolls Royce | Mixture for aluminising metals and a process of aluminising |
US3450512A (en) * | 1966-07-05 | 1969-06-17 | United Aircraft Corp | Coated nickel base engine alloys |
-
1968
- 1968-10-25 US US770853A patent/US3544348A/en not_active Expired - Lifetime
-
1969
- 1969-10-17 GB GB1258833D patent/GB1258833A/en not_active Expired
- 1969-10-21 CH CH1569069A patent/CH540346A/en not_active IP Right Cessation
- 1969-10-21 FR FR6936133A patent/FR2021543A1/fr active Pending
- 1969-10-21 NL NL696915857A patent/NL153276B/en not_active IP Right Cessation
- 1969-10-23 SE SE14558/69A patent/SE344767B/xx unknown
- 1969-10-24 BE BE740776D patent/BE740776A/xx not_active IP Right Cessation
- 1969-10-25 ES ES372871A patent/ES372871A1/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2213841A (en) * | 1987-12-17 | 1989-08-23 | Mtu Muenchen Gmbh | Aluminium diffusion coating of titanium |
GB2213841B (en) * | 1987-12-17 | 1992-01-15 | Mtu Muenchen Gmbh | Method for the aluminium diffusion coating of components which consist of titanium alloys |
Also Published As
Publication number | Publication date |
---|---|
US3544348A (en) | 1970-12-01 |
DE1952370B2 (en) | 1972-07-20 |
CH540346A (en) | 1973-08-15 |
NL153276B (en) | 1977-05-16 |
DE1952370A1 (en) | 1970-08-27 |
ES372871A1 (en) | 1971-11-01 |
FR2021543A1 (en) | 1970-07-24 |
BE740776A (en) | 1970-04-01 |
NL6915857A (en) | 1970-04-28 |
SE344767B (en) | 1972-05-02 |
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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 |