WO2003100110A2 - Verfahren zur entfernung von zumindest einem teilbereich eines bauteils aus metall oder einer metallverbindung - Google Patents
Verfahren zur entfernung von zumindest einem teilbereich eines bauteils aus metall oder einer metallverbindung Download PDFInfo
- Publication number
- WO2003100110A2 WO2003100110A2 PCT/EP2003/005573 EP0305573W WO03100110A2 WO 2003100110 A2 WO2003100110 A2 WO 2003100110A2 EP 0305573 W EP0305573 W EP 0305573W WO 03100110 A2 WO03100110 A2 WO 03100110A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- component
- layer
- partial area
- metal
- diffusion
- Prior art date
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
- C23C10/02—Pretreatment of the material to be coated
-
- 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F4/00—Processes for removing metallic material from surfaces, not provided for in group C23F1/00 or C23F3/00
-
- 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
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G5/00—Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents
Definitions
- the invention relates to a method for removing a partial area, in particular a layer area of a component consisting of metal or a metal compound, whereby the partial area can be removed or removed more easily after application of the method.
- thermal insulation layers have been developed that are applied to thermally stressed components, such as superalloys, that alone could no longer withstand the high inlet temperatures in the long run.
- the ceramic thermal barrier coating offers the advantage of a high temperature resistance due to its ceramic properties and the metallic substrate offers the advantage of the good mechanical properties in this composite or layer system.
- An adhesion-promoting layer of the composite is typically between the substrate and the ceramic thermal barrier coating.
- composition of these MCrAlY layers can vary, but all MCrAlY layers are subject to corrosion or degradation due to oxidation, sulfidation, nitridation, diffusion or other chemical and / or mechanical attacks, in spite of the overlying ceramic layer.
- the MCrAlY layer often degrades to a greater extent than the metallic substrate, i.e.
- the lifespan of the composite system of substrate and layer is determined by the lifespan of the MCrAlY layer.
- the MCrAlY intermediate layer is only partially functional after a long period of use, however, the substrate can still be fully functional.
- the invention overcomes the disadvantages described by a method as described in claim 1.
- the diffusion agent can be obtained by simple known coating processes such as plasma spraying, evaporation, CVD, packing. drive (component in powder bed) or other processes (paste application).
- FIG. 1 shows a corroded metallic component
- FIG. 2 shows a component in which the diffusion agent is applied
- FIG. 3 shows the component according to FIG. 2 after a heat treatment
- FIG. 4 components which are subjected to an acid treatment
- FIGS. 5 and 6 components after an acid treatment for a method according to the invention and according to the prior art.
- FIG. 1 shows a component 1 made of metal, a metal alloy or a metal compound, which has corrosion products 4 on a surface 13 and / or in the interior of the component 1 in at least one partial area, which are present, for example, in areas formed separately from one another.
- the corrosion products 4 can also be present continuously or on / under the entire surface 13, that is to say also form a corrosion layer 4.
- a partial area 28 is represented, for example, by the area with a dashed border.
- the component 1 can be solid or a layer or an area of a composite or layer system 14.
- a substrate 7 made of metal or ceramic is present, on which the metallic layer 10, for example an MCrAlY layer, is applied, where M means that a metal made of nickel, chromium or iron is used.
- the partial area 28 can also be a partial area of the layer 10 or represent the entire layer 10 of the layer system 14 and / or part of the metallic substrate 7.
- the corrosion products 4 have formed during the use of the component 1 and are undesirable for the further use of the component and must be removed. This is often done by treatment in an acid bath.
- the material of the component 1 below or above the layer 10 degraded areas and / or the corrosion products 4 have a different reactivity in an acid bath, i.e. are more resistant to erosion.
- the different solution behavior in the acid bath is caused by the different solution behavior of the corrosion products 4 or because an original composition of the material of the component 1 or the layer 10 has changed, e.g. because the corrosion product 4 extracts a component from an area of the component 1 in the area around the corrosion product 4 and creates a depletion area there. Therefore, there is an uneven removal or no removal of the corrosion products 4 or the material in the depletion area.
- the method according to the invention makes it possible to
- a first process step for example, rough removal of the corrosion products 4 or other areas by mechanical processes, such as e.g. Sandblasting and / or chemical agents such as e.g. Acid bath take place.
- mechanical processes such as e.g. Sandblasting and / or chemical agents such as e.g. Acid bath take place.
- a multi-component diffusion agent 16 is applied onto the corroded component 1 onto the surface 13, in particular in the area with the Corrosion products 4 or, for example, applied to the corrosion layer 4 or at least one component of the diffusion agent 16 diffuses directly from the gas phase into the component 1, the corrosion products 4 in this example representing the more resistant areas.
- the diffusion agent 16 contains, for example, two components, both of which diffuse through a heat treatment into the layer 10 or the component 1 and change the chemical composition and materials there. By diffusing in and the heat treatment, new phases can also be formed, which can be removed more easily by means of an acid bath 19 (FIG. 4).
- FIG. 3 shows a component according to FIG. 2, in which the diffusion means 16 is completely based on the layer 10 due to a heat treatment at a temperature T.
- Layer 10 represents the partial area 28 to be removed, which does not only consist of more resistant areas.
- the diffusion means 16 is at least two-component. At least one component of the diffusion agent 16 is, for example, metallic, e.g. Aluminum. Another metallic component is, for example, cobalt. Other components can be silicon or carbon.
- the method works particularly well if cobalt and aluminum as components of the diffusion agent 16 diffuse into the partial region 28.
- FIG. 4 shows two components which are arranged in an acid bath 19 or are exposed to an acid attack.
- FIG. 5 shows the component 22 after the acid treatment.
- the component 22 still has acid-resistant regions 25 which were not or only slightly removed during the acid attack, so that a layer region of the component 22 was removed non-uniformly.
- FIG. 6 shows a component 1 or layer system 14 in which a layer region of component 1 or layer 10 has been removed evenly.
- the partial area 28 can also have become so brittle that the partial area 28 can be removed by mechanical treatment (sandblasting, ultrasound, dry ice blasting).
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- ing And Chemical Polishing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/516,085 US20060112976A1 (en) | 2002-05-29 | 2003-05-27 | Method for removing at least one partial area of a component made of metal or a metallic compound |
EP03735475A EP1507882A2 (de) | 2002-05-29 | 2003-05-27 | Verfahren zur entfernung von zumindest einem teilbereich eines bauteils aus metall oder einer metallverbindung |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02011965A EP1367144A1 (de) | 2002-05-29 | 2002-05-29 | Verfahren zur Entfernung von zumindest einem Teilbereich eines Bauteils aus Metall oder einer Metallverbindung |
EP02011965.7 | 2002-05-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2003100110A2 true WO2003100110A2 (de) | 2003-12-04 |
WO2003100110A3 WO2003100110A3 (de) | 2004-03-04 |
Family
ID=29414719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2003/005573 WO2003100110A2 (de) | 2002-05-29 | 2003-05-27 | Verfahren zur entfernung von zumindest einem teilbereich eines bauteils aus metall oder einer metallverbindung |
Country Status (3)
Country | Link |
---|---|
US (1) | US20060112976A1 (de) |
EP (2) | EP1367144A1 (de) |
WO (1) | WO2003100110A2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008068070A1 (de) * | 2006-12-05 | 2008-06-12 | Siemens Aktiengesellschaft | Verfahren zum beschichten eines mit öffnungen versehenen bauteils |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150370882A1 (en) * | 2014-06-20 | 2015-12-24 | Amazon Technologies, Inc. | Use of dependency graphs to dynamically update n-dimensional cubes |
US10769175B1 (en) | 2014-06-20 | 2020-09-08 | Amazon Technologies, Inc. | Real-time hosted system analytics |
US11868372B1 (en) | 2014-06-20 | 2024-01-09 | Amazon Technologies, Inc. | Automated hierarchy detection for cloud-based analytics |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB980727A (en) * | 1963-09-23 | 1965-01-20 | Coast Metals Inc | Method of applying metallic coatings |
US6036995A (en) * | 1997-01-31 | 2000-03-14 | Sermatech International, Inc. | Method for removal of surface layers of metallic coatings |
EP1043424A1 (de) * | 1999-04-07 | 2000-10-11 | General Electric Company | Verfahren zum lokalen Entfernen von Oxidations- und Korrosionsprodukten von Oberflächen von Turbinenmotorkomponenten |
EP1199377A2 (de) * | 2000-10-20 | 2002-04-24 | General Electric Company | Schutz der Oberfläche eines Gegenstands auf Nickel-Basis mit einer korrosionsbeständigen Schicht aus einer Aluminiumlegierung |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3184292A (en) * | 1964-07-08 | 1965-05-18 | Du Pont | Process and composition for diffusion coating refractory metals and product produced thereby |
US4117179A (en) * | 1976-11-04 | 1978-09-26 | General Electric Company | Oxidation corrosion resistant superalloys and coatings |
US4965095A (en) * | 1979-03-30 | 1990-10-23 | Alloy Surfaces Company, Inc. | Method for refurbishing used jet engine hot section airfoils |
GB2167773A (en) * | 1984-11-29 | 1986-06-04 | Secr Defence | Improvements in or relating to coating processes |
GB9116332D0 (en) * | 1991-07-29 | 1991-09-11 | Diffusion Alloys Ltd | Refurbishing of corroded superalloy or heat resistant steel parts and parts so refurbished |
EP0861927A1 (de) * | 1997-02-24 | 1998-09-02 | Sulzer Innotec Ag | Verfahren zum Herstellen von einkristallinen Strukturen |
US6042879A (en) * | 1997-07-02 | 2000-03-28 | United Technologies Corporation | Method for preparing an apertured article to be recoated |
US6010746A (en) * | 1998-02-03 | 2000-01-04 | United Technologies Corporation | In-situ repair method for a turbomachinery component |
EP1162284A1 (de) * | 2000-06-05 | 2001-12-12 | Alstom (Switzerland) Ltd | Verfahren zum Reparieren einer beschichteten Komponenten |
EP1298230A1 (de) * | 2001-10-01 | 2003-04-02 | Siemens Aktiengesellschaft | Verfahren zur Entfernung von Schichtbereichen eines Bauteils aus Metall |
-
2002
- 2002-05-29 EP EP02011965A patent/EP1367144A1/de not_active Withdrawn
-
2003
- 2003-05-27 US US10/516,085 patent/US20060112976A1/en not_active Abandoned
- 2003-05-27 EP EP03735475A patent/EP1507882A2/de not_active Withdrawn
- 2003-05-27 WO PCT/EP2003/005573 patent/WO2003100110A2/de not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB980727A (en) * | 1963-09-23 | 1965-01-20 | Coast Metals Inc | Method of applying metallic coatings |
US6036995A (en) * | 1997-01-31 | 2000-03-14 | Sermatech International, Inc. | Method for removal of surface layers of metallic coatings |
EP1043424A1 (de) * | 1999-04-07 | 2000-10-11 | General Electric Company | Verfahren zum lokalen Entfernen von Oxidations- und Korrosionsprodukten von Oberflächen von Turbinenmotorkomponenten |
EP1199377A2 (de) * | 2000-10-20 | 2002-04-24 | General Electric Company | Schutz der Oberfläche eines Gegenstands auf Nickel-Basis mit einer korrosionsbeständigen Schicht aus einer Aluminiumlegierung |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008068070A1 (de) * | 2006-12-05 | 2008-06-12 | Siemens Aktiengesellschaft | Verfahren zum beschichten eines mit öffnungen versehenen bauteils |
EP1932954A1 (de) * | 2006-12-05 | 2008-06-18 | Siemens Aktiengesellschaft, A German Corporation | Verfahren zum Beschichten eines mit Öffnungen versehenen Bauteils |
Also Published As
Publication number | Publication date |
---|---|
EP1507882A2 (de) | 2005-02-23 |
EP1367144A1 (de) | 2003-12-03 |
WO2003100110A3 (de) | 2004-03-04 |
US20060112976A1 (en) | 2006-06-01 |
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