EP1548156A2 - Process for removing adherent oxide particles from an aluminized surface - Google Patents
Process for removing adherent oxide particles from an aluminized surface Download PDFInfo
- Publication number
- EP1548156A2 EP1548156A2 EP04257665A EP04257665A EP1548156A2 EP 1548156 A2 EP1548156 A2 EP 1548156A2 EP 04257665 A EP04257665 A EP 04257665A EP 04257665 A EP04257665 A EP 04257665A EP 1548156 A2 EP1548156 A2 EP 1548156A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- particles
- process according
- solution
- aluminized
- aluminized surface
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 40
- 239000002245 particle Substances 0.000 title claims abstract description 37
- 230000001464 adherent effect Effects 0.000 title claims abstract description 13
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 15
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 15
- 239000002002 slurry Substances 0.000 claims abstract description 10
- 239000003518 caustics Substances 0.000 claims abstract description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-M hydroxide Chemical compound [OH-] XLYOFNOQVPJJNP-UHFFFAOYSA-M 0.000 claims abstract description 5
- KWYUFKZDYYNOTN-UHFFFAOYSA-M Potassium hydroxide Chemical compound [OH-].[K+] KWYUFKZDYYNOTN-UHFFFAOYSA-M 0.000 claims description 20
- 238000001816 cooling Methods 0.000 claims description 13
- 238000005269 aluminizing Methods 0.000 claims description 8
- 239000013528 metallic particle Substances 0.000 claims description 6
- 239000008367 deionised water Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 4
- 239000007788 liquid Substances 0.000 claims description 3
- 230000003647 oxidation Effects 0.000 abstract description 6
- 238000007254 oxidation reaction Methods 0.000 abstract description 6
- 239000000843 powder Substances 0.000 abstract description 6
- 238000005245 sintering Methods 0.000 abstract description 5
- 238000000576 coating method Methods 0.000 description 21
- 239000000243 solution Substances 0.000 description 20
- 239000011248 coating agent Substances 0.000 description 12
- 229910000951 Aluminide Inorganic materials 0.000 description 10
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 6
- 239000012720 thermal barrier coating Substances 0.000 description 5
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 4
- 229920003229 poly(methyl methacrylate) Polymers 0.000 description 4
- -1 CrAl Inorganic materials 0.000 description 3
- 229920000180 alkyd Polymers 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 239000002270 dispersing agent Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- RSWGJHLUYNHPMX-UHFFFAOYSA-N Abietic-Saeure Natural products C12CCC(C(C)C)=CC2=CCC2C1(C)CCCC2(C)C(O)=O RSWGJHLUYNHPMX-UHFFFAOYSA-N 0.000 description 2
- SOGAXMICEFXMKE-UHFFFAOYSA-N Butylmethacrylate Chemical compound CCCCOC(=O)C(C)=C SOGAXMICEFXMKE-UHFFFAOYSA-N 0.000 description 2
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- 239000012190 activator Substances 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000011010 flushing procedure Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
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- 230000002459 sustained effect Effects 0.000 description 2
- KHPCPRHQVVSZAH-UHFFFAOYSA-N trans-cinnamyl beta-D-glucopyranoside Natural products OC1C(O)C(O)C(CO)OC1OCC=CC1=CC=CC=C1 KHPCPRHQVVSZAH-UHFFFAOYSA-N 0.000 description 2
- 238000011179 visual inspection Methods 0.000 description 2
- 239000004923 Acrylic lacquer Substances 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910002515 CoAl Inorganic materials 0.000 description 1
- 229910015372 FeAl Inorganic materials 0.000 description 1
- 235000010469 Glycine max Nutrition 0.000 description 1
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- 229920001800 Shellac Polymers 0.000 description 1
- 229910010038 TiAl Inorganic materials 0.000 description 1
- 229920006397 acrylic thermoplastic Polymers 0.000 description 1
- 238000013019 agitation Methods 0.000 description 1
- 229910001508 alkali metal halide Inorganic materials 0.000 description 1
- 150000008045 alkali metal halides Chemical class 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000001913 cellulose Substances 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 150000002118 epoxides Chemical class 0.000 description 1
- SUPCQIBBMFXVTL-UHFFFAOYSA-N ethyl 2-methylprop-2-enoate Chemical compound CCOC(=O)C(C)=C SUPCQIBBMFXVTL-UHFFFAOYSA-N 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 235000010985 glycerol esters of wood rosin Nutrition 0.000 description 1
- KWLMIXQRALPRBC-UHFFFAOYSA-L hectorite Chemical group [Li+].[OH-].[OH-].[Na+].[Mg+2].O1[Si]2([O-])O[Si]1([O-])O[Si]([O-])(O1)O[Si]1([O-])O2 KWLMIXQRALPRBC-UHFFFAOYSA-L 0.000 description 1
- 229910000271 hectorite Inorganic materials 0.000 description 1
- 150000004679 hydroxides Chemical class 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 229920000609 methyl cellulose Polymers 0.000 description 1
- 239000001923 methylcellulose Substances 0.000 description 1
- 235000010981 methylcellulose Nutrition 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000002952 polymeric resin Substances 0.000 description 1
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- 229920002635 polyurethane Polymers 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000006254 rheological additive Substances 0.000 description 1
- ZLGIYFNHBLSMPS-ATJNOEHPSA-N shellac Chemical compound OCCCCCC(O)C(O)CCCCCCCC(O)=O.C1C23[C@H](C(O)=O)CCC2[C@](C)(CO)[C@@H]1C(C(O)=O)=C[C@@H]3O ZLGIYFNHBLSMPS-ATJNOEHPSA-N 0.000 description 1
- 239000004208 shellac Substances 0.000 description 1
- 229940113147 shellac Drugs 0.000 description 1
- 235000013874 shellac Nutrition 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000008399 tap water Substances 0.000 description 1
- 235000020679 tap water Nutrition 0.000 description 1
- ISXSCDLOGDJUNJ-UHFFFAOYSA-N tert-butyl prop-2-enoate Chemical compound CC(C)(C)OC(=O)C=C ISXSCDLOGDJUNJ-UHFFFAOYSA-N 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000004506 ultrasonic cleaning Methods 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
- 229910001845 yogo sapphire Inorganic materials 0.000 description 1
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
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
-
- 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
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
- C23G1/14—Cleaning or pickling metallic material with solutions or molten salts with alkaline solutions
- C23G1/22—Light metals
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/002—Cleaning of turbomachines
Definitions
- the present invention generally relates to aluminizing processes. More particularly, this invention relates to a process for removing oxide particles adhered to a surface following aluminizing.
- the operating environment within a gas turbine engine is both thermally and chemically hostile, particularly within the turbine, combustor and augmentor sections.
- a common practice is to protect the surfaces of gas turbine engine components with an environmental coating that is resistant to oxidation and hot corrosion, and optionally a thermal barrier coating (TBC) that provides thermal-insulating protection for the component exterior.
- TBC thermal barrier coating
- Environmental coatings that have found wide use include diffusion aluminide coatings and overlay coatings such as MCrAlY. During high temperature exposure in air, these coatings form a protective aluminum oxide (alumina) scale that inhibits oxidation of the coating and the underlying substrate.
- Diffusion aluminide coatings are particularly useful for providing environmental protection to components equipped with internal cooling passages, such as high pressure turbine blades, because aluminide coatings are able to provide environmental protection without significantly reducing the cross-sections of the cooling passages.
- An aluminizing process capable of selectively coating the internal cooling passages of a turbine blade involves injecting a slurry into the passages.
- the slurry aluminizing process relies on aluminiding vapors that react at exposed surfaces to form a diffusion aluminide coating.
- the slurry process makes us of a coating powder comprising a metallic aluminum source (such as aluminum or an aluminum alloy, e.g., CrAl, CoAl, FeAl, and TiAl), a carrier or activator (such as an alkali metal halide), and an inert oxide dispersant (such as alumina (Al 2 O 3 ) or zirconia (ZrO 2 )).
- a metallic aluminum source such as aluminum or an aluminum alloy, e.g., CrAl, CoAl, FeAl, and TiAl
- a carrier or activator such as an alkali metal halide
- an inert oxide dispersant such as alumina (Al 2 O 3 ) or zirconia (ZrO 2 )
- An example of a suitable inorganic binder is hectorite clay in water
- examples of particularly suitable organic binders include acrylics such as polymethylmethacrylate (PMMA), butyl methacrylate resin, ethyl methacrylate resin, methyl methacrylate resin and methacrylate co-polymer resin.
- Other organic binders that may be used include methyl cellulose, acrylic lacquer, alkyd resins such as phenolic-modified alkyd and phenolic-modified soybean alkyd, shellac, rosin, rosin derivatives, ester gum, vinyls, styrenics, polyesters, epoxides, polyurethanes, cellulose derivatives, and mixtures thereof.
- the liquid is removed by drying, after which the component containing the dried coating media is heated in an inert or reducing atmosphere to a temperature of 1700°F (about 930°C) or more.
- the activator vaporizes and reacts with the aluminum source to form a volatile aluminum halide, which then reacts at the surfaces of the passages to form the aluminide coating.
- the present invention provides a process for removing particles that become adherently sintered to an aluminized surface during an aluminiding process.
- An important example is the internal cooling passages of gas turbine engine components, such as components within the turbine, combustor or augmentor sections of a gas turbine engine.
- the method is particularly suited for the removal of oxidized particles that form as a result of oxidation of the aluminum source powder used in slurry aluminiding processes, wherein the oxidized powder particles become attached by sintering to the aluminized surface.
- the method also serves to remove other particles that may be sintered to the aluminized surface following the aluminiding process, such as oxide particles that were mixed with the aluminum source powder as an inert dispersant.
- the processing steps of this invention include contacting the aluminized surface with an aqueous caustic hydroxide solution until these adherent particles are removed therefrom.
- an aqueous potassium hydroxide solution at moderate elevated temperatures and atmospheric pressures has been shown to facilitate removal of adherent residual coating materials, particularly if accompanied by agitation with ultrasonic energy.
- adherent oxidized and oxide particles can be completely removed from the aluminized surfaces of an internal cavity, such as the internal cooling passages of a gas turbine engine component so that cooling air flow through the passages is not reduced.
- aqueous caustic hydroxide solutions of this invention are compatible with aluminide coatings, so as not to attack such coatings during removal of the adherent oxide particles.
- the present invention is directed to the removal of particles that form by oxidation of metal particles contacting a surface undergoing aluminizing, such that the particles adhere to the aluminized surface through a sintering mechanism.
- the particles of concern to this invention are distinguishable from dirt and contaminants that collect within internal cooling passages of air-cooled gas turbine engine components during engine operation.
- the particles are distinguishable from ceramic coatings formed of metal oxides that are deposited as thermal barrier coatings (TBC) on gas turbine engine components. While the advantages of this invention will be described with reference to turbine blades, the teachings of this invention are generally applicable to any component having internal surfaces that benefit from protection by aluminide coating.
- gas turbine engine components that benefit from the present invention include air-cooled high and low pressure turbine nozzles and blades, shrouds, combustor liners and augmentor.
- air-cooled components whose interior surfaces are protected by a diffusion aluminide coating deposited by a non-line-of-sight technique, such as a slurry aluminiding process in which metallic particles of an aluminum source can directly contact the surface being aluminized.
- a slurry aluminiding process in which metallic particles of an aluminum source can directly contact the surface being aluminized.
- particles of the aluminum source may oxidize and subsequently become adhered by sintering to the internal aluminized surface.
- a slurry aluminiding process that uses particles of a Cr-44Al (wt.%) alloy as the aluminum source can result in the oxidation of at least the outer surfaces of these particles, resulting in the formation of oxidized particles that adhere to the aluminized surface.
- An additional source of particles that may sinter to an aluminized surface as a result of an aluminiding process is the oxide particles that are conventionally mixed with aluminum source particles to act as an inert dispersant during the aluminiding process.
- the process of this invention entails treating the aluminized surface with an aqueous caustic hydroxide solution, a suitable example of which contains at least 100 grams/liter of potassium hydroxide (KOH).
- KOH potassium hydroxide
- a more preferred solution contains about 175 to about 225 grams/liter of KOH, with the balance de-ionized water.
- other caustic hydroxides such as sodium hydroxide (NaOH) can be used in combination with or in place of potassium hydroxide in the solution.
- the internal aluminized surfaces are contacted with the solution at a moderate elevated temperature, such as about 150 to about 190°F (about 66 to about 88°C) and preferably about 160 to about 170°F (about 71 to about 77°C).
- This operation is carried out to ensure that all internal aluminized surfaces are contacted by the solution, such as by immersing the entire component in a bath of the solution, and preferably flushing the internal cavities with the solution while the component is immersed to ensure complete filling with the solution.
- Contact with the solution is preferable maintained for a duration of at least two hours, such as about two to about eight hours and more preferably about four hours.
- the solution is preferably agitated with ultrasonic energy.
- the solution may be held in a commercially-available ultrasonic cleaning tank employing magnetostrictive or piezoelectric transducers.
- Suitable frequencies are about 20 kHz to about 40 kHz and suitable power levels are about 20 to about 120 watts per gallon (about 80 to about 450 watts per liter) of solution, preferably about 50 to about 100 watts per gallon (about 190 to about 380 watts per liter) of solution.
- the component is rinsed and its internal cavities flushed with water for a minimum of about five minutes to remove the solution, after which the component is dried.
- One of the blades was cleaned by submersion, blade tips down, in an aqueous solution containing about 40 to about 50 weight percent KOH for about four hours.
- the solution was maintained at a temperature of about 170°F (about 77°C), and agitated by ultrasonic energy at a frequency of about 25 kHz and a power level of about 100 watts per gallon (about 380 watts per liter) of solution.
- the internal cavities of the blade were flushed with tap water and dried. Visual inspection of the cavities evidenced that the adherent oxidized particles had been completely removed from the internal cavities of the blade. The cleaning procedure was then repeated on an additional four blades with the same results.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Powder Metallurgy (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)
- Compounds Of Alkaline-Earth Elements, Aluminum Or Rare-Earth Metals (AREA)
Abstract
Description
- The present invention generally relates to aluminizing processes. More particularly, this invention relates to a process for removing oxide particles adhered to a surface following aluminizing.
- The operating environment within a gas turbine engine is both thermally and chemically hostile, particularly within the turbine, combustor and augmentor sections. A common practice is to protect the surfaces of gas turbine engine components with an environmental coating that is resistant to oxidation and hot corrosion, and optionally a thermal barrier coating (TBC) that provides thermal-insulating protection for the component exterior. Environmental coatings that have found wide use include diffusion aluminide coatings and overlay coatings such as MCrAlY. During high temperature exposure in air, these coatings form a protective aluminum oxide (alumina) scale that inhibits oxidation of the coating and the underlying substrate. Diffusion aluminide coatings are particularly useful for providing environmental protection to components equipped with internal cooling passages, such as high pressure turbine blades, because aluminide coatings are able to provide environmental protection without significantly reducing the cross-sections of the cooling passages.
- An aluminizing process capable of selectively coating the internal cooling passages of a turbine blade involves injecting a slurry into the passages. As with other types of processes employed to form aluminide coatings, the slurry aluminizing process relies on aluminiding vapors that react at exposed surfaces to form a diffusion aluminide coating. More particularly, the slurry process makes us of a coating powder comprising a metallic aluminum source (such as aluminum or an aluminum alloy, e.g., CrAl, CoAl, FeAl, and TiAl), a carrier or activator (such as an alkali metal halide), and an inert oxide dispersant (such as alumina (Al2O3) or zirconia (ZrO2)). These solid particulate components are mixed with an organic or inorganic liquid, whose role is a rheological additive to facilitate the injection of the coating powder into the often complex system of internal cooling passages present in a turbine blade. An example of a suitable inorganic binder is hectorite clay in water, while examples of particularly suitable organic binders include acrylics such as polymethylmethacrylate (PMMA), butyl methacrylate resin, ethyl methacrylate resin, methyl methacrylate resin and methacrylate co-polymer resin. Other organic binders that may be used include methyl cellulose, acrylic lacquer, alkyd resins such as phenolic-modified alkyd and phenolic-modified soybean alkyd, shellac, rosin, rosin derivatives, ester gum, vinyls, styrenics, polyesters, epoxides, polyurethanes, cellulose derivatives, and mixtures thereof. Once the mixture is injected, the liquid is removed by drying, after which the component containing the dried coating media is heated in an inert or reducing atmosphere to a temperature of 1700°F (about 930°C) or more. At the elevated temperature, the activator vaporizes and reacts with the aluminum source to form a volatile aluminum halide, which then reacts at the surfaces of the passages to form the aluminide coating.
- Following aluminiding, remnants of the solid components of the slurry must be removed so as not to inhibit the flow of cooling air through the passages. In practice, there is a tendency for particles of the aluminum source to oxidize and sinter to the aluminized surfaces as a result of the high temperatures sustained during the aluminiding process. In that these adherent particles are sintered to the aluminized surfaces, they have proven to be very difficult to remove. Mechanical cleaning techniques such as high-pressure water jets and flushing have been used with limited success. Other approaches that employ caustic compounds at high temperatures and pressures (e.g., performed in an autoclave) to strip TBC from exterior surfaces or remove dirt and contamination from internal passages of gas turbine engine components are undesirable in view of the cost of autoclaving operations. Therefore, in order to maximize air flow through aluminized cooling passages of an air-cooled component, a need exists for a reliable method of removing adherent sintered oxide particles.
- The present invention provides a process for removing particles that become adherently sintered to an aluminized surface during an aluminiding process. An important example is the internal cooling passages of gas turbine engine components, such as components within the turbine, combustor or augmentor sections of a gas turbine engine. The method is particularly suited for the removal of oxidized particles that form as a result of oxidation of the aluminum source powder used in slurry aluminiding processes, wherein the oxidized powder particles become attached by sintering to the aluminized surface. The method also serves to remove other particles that may be sintered to the aluminized surface following the aluminiding process, such as oxide particles that were mixed with the aluminum source powder as an inert dispersant. The processing steps of this invention include contacting the aluminized surface with an aqueous caustic hydroxide solution until these adherent particles are removed therefrom.
- According to the invention, an aqueous potassium hydroxide solution at moderate elevated temperatures and atmospheric pressures (i.e., without autoclaving) has been shown to facilitate removal of adherent residual coating materials, particularly if accompanied by agitation with ultrasonic energy. In this manner, adherent oxidized and oxide particles can be completely removed from the aluminized surfaces of an internal cavity, such as the internal cooling passages of a gas turbine engine component so that cooling air flow through the passages is not reduced. Finally, aqueous caustic hydroxide solutions of this invention are compatible with aluminide coatings, so as not to attack such coatings during removal of the adherent oxide particles.
- Other objects and advantages of this invention will be better appreciated from the following detailed description.
- The present invention is directed to the removal of particles that form by oxidation of metal particles contacting a surface undergoing aluminizing, such that the particles adhere to the aluminized surface through a sintering mechanism. As such, the particles of concern to this invention are distinguishable from dirt and contaminants that collect within internal cooling passages of air-cooled gas turbine engine components during engine operation. Furthermore, the particles are distinguishable from ceramic coatings formed of metal oxides that are deposited as thermal barrier coatings (TBC) on gas turbine engine components. While the advantages of this invention will be described with reference to turbine blades, the teachings of this invention are generally applicable to any component having internal surfaces that benefit from protection by aluminide coating.
- Notable examples of gas turbine engine components that benefit from the present invention include air-cooled high and low pressure turbine nozzles and blades, shrouds, combustor liners and augmentor. Of particular interest are air-cooled components whose interior surfaces are protected by a diffusion aluminide coating deposited by a non-line-of-sight technique, such as a slurry aluminiding process in which metallic particles of an aluminum source can directly contact the surface being aluminized. At the elevated temperatures necessary to transfer aluminum from the aluminum source to the internal surface being aluminized, particles of the aluminum source may oxidize and subsequently become adhered by sintering to the internal aluminized surface. For example, a slurry aluminiding process that uses particles of a Cr-44Al (wt.%) alloy as the aluminum source can result in the oxidation of at least the outer surfaces of these particles, resulting in the formation of oxidized particles that adhere to the aluminized surface. An additional source of particles that may sinter to an aluminized surface as a result of an aluminiding process is the oxide particles that are conventionally mixed with aluminum source particles to act as an inert dispersant during the aluminiding process.
- The process of this invention entails treating the aluminized surface with an aqueous caustic hydroxide solution, a suitable example of which contains at least 100 grams/liter of potassium hydroxide (KOH). A more preferred solution contains about 175 to about 225 grams/liter of KOH, with the balance de-ionized water. It is believed that other caustic hydroxides such as sodium hydroxide (NaOH) can be used in combination with or in place of potassium hydroxide in the solution. The internal aluminized surfaces are contacted with the solution at a moderate elevated temperature, such as about 150 to about 190°F (about 66 to about 88°C) and preferably about 160 to about 170°F (about 71 to about 77°C). This operation is carried out to ensure that all internal aluminized surfaces are contacted by the solution, such as by immersing the entire component in a bath of the solution, and preferably flushing the internal cavities with the solution while the component is immersed to ensure complete filling with the solution. Contact with the solution is preferable maintained for a duration of at least two hours, such as about two to about eight hours and more preferably about four hours. During this step, the solution is preferably agitated with ultrasonic energy. For example, the solution may be held in a commercially-available ultrasonic cleaning tank employing magnetostrictive or piezoelectric transducers. Suitable frequencies are about 20 kHz to about 40 kHz and suitable power levels are about 20 to about 120 watts per gallon (about 80 to about 450 watts per liter) of solution, preferably about 50 to about 100 watts per gallon (about 190 to about 380 watts per liter) of solution. Following treatment with the solution, the component is rinsed and its internal cavities flushed with water for a minimum of about five minutes to remove the solution, after which the component is dried.
- During an investigation leading to this invention, high pressure turbine blades were obtained whose internal cooling passages had been selectively aluminized by a slurry aluminiding technique in which metallic particles of Cr-44AI were used as the aluminum source material. Visual inspection of the cooling passages showed that particles were adhered to the aluminized internal surfaces. These particles, generally about 10 to about 100 micrometers in diameter, were concluded to have been formed by some of the Cr-44Al particles that had oxidized and become attached to the aluminide coating as a result of sintering at the high temperature (about 970°C) sustained during the aluminizing process. One of the blades was cleaned by submersion, blade tips down, in an aqueous solution containing about 40 to about 50 weight percent KOH for about four hours. The solution was maintained at a temperature of about 170°F (about 77°C), and agitated by ultrasonic energy at a frequency of about 25 kHz and a power level of about 100 watts per gallon (about 380 watts per liter) of solution. On removal from the solution, the internal cavities of the blade were flushed with tap water and dried. Visual inspection of the cavities evidenced that the adherent oxidized particles had been completely removed from the internal cavities of the blade. The cleaning procedure was then repeated on an additional four blades with the same results.
Claims (10)
- A process comprising the steps of:forming an aluminized surface within an internal cavity of a component by placing within the internal cavity a material comprising metallic particles of an aluminum source, wherein some of the metallic particles oxidize to form adherent particles that are sintered to the aluminized surface; and thencontacting the aluminized surface with an aqueous caustic hydroxide solution until the adherent particles are removed from the surface.
- The process according to claim 1, characterized in that the solution contains at least 100 grams/liter of potassium hydroxide and the balance essentially de-ionized water.
- The process according to claim 1, characterized in that the solution contains about 175 to about 225 grams/liter of potassium hydroxide and the balance essentially de-ionized water.
- The process according to claim 1, characterized in that the solution consists of about 175 to about 225 grams/liter of potassium hydroxide and the balance de-ionized water.
- The process according to any one of claims 1 through 4, characterized in that the aluminizing step comprises a slurry aluminizing process in which the material comprises the metallic particles suspended in a liquid vehicle.
- The process according to any one of claims 1 through 5, characterized in that the adherent particles comprise metallic particles whose outer surfaces are oxidized.
- The process according to any one of claims 1 through 6 characterized in that the forming step results in oxide particles being sintered to the aluminized surface, and the oxide particles are removed from the aluminized surface by the contacting step.
- The process according to any one of claims 1 through 7 characterized in that the contacting step is performed at a temperature of about 66□C to about 88□C and at atmospheric pressure.
- The process according to any one of claims 1 through 8, further comprising the step of agitating the solution while the solution contacts the surface.
- The process according to any one of claims 1 through 9, characterized in that the component is a gas turbine engine component and the internal cavity is a cooling passage.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US707465 | 2000-11-07 | ||
US10/707,465 US20050127039A1 (en) | 2003-12-16 | 2003-12-16 | Process for removing adherent oxide particles from an aluminized surface |
Publications (3)
Publication Number | Publication Date |
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EP1548156A2 true EP1548156A2 (en) | 2005-06-29 |
EP1548156A3 EP1548156A3 (en) | 2010-01-13 |
EP1548156B1 EP1548156B1 (en) | 2011-03-23 |
Family
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Application Number | Title | Priority Date | Filing Date |
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EP04257665A Expired - Fee Related EP1548156B1 (en) | 2003-12-16 | 2004-12-09 | Process for removing adherent oxide particles from an aluminized surface |
Country Status (6)
Country | Link |
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US (1) | US20050127039A1 (en) |
EP (1) | EP1548156B1 (en) |
BR (1) | BRPI0405921A (en) |
CA (1) | CA2490014C (en) |
DE (1) | DE602004031920D1 (en) |
SG (2) | SG133599A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1779936A2 (en) * | 2005-09-29 | 2007-05-02 | United Technologies Corporation | Squirter jet ultrasonic cleaning |
EP3269840A1 (en) * | 2016-07-12 | 2018-01-17 | United Technologies Corporation | Method of chromizing an article including internal passages of the article |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7332024B2 (en) * | 2004-04-29 | 2008-02-19 | General Electric Company | Aluminizing composition and method for application within internal passages |
US8038894B2 (en) * | 2006-11-29 | 2011-10-18 | General Electric Company | Method of selectively stripping an engine-run ceramic coating |
US20140051028A1 (en) * | 2012-08-16 | 2014-02-20 | Daniel Edward Matejczyk | Propellant compatible component for combustion device |
GB201903484D0 (en) * | 2019-03-14 | 2019-05-01 | Rolls Royce Plc | A method of removing a ceramic coating from a ceramic coated metallic article |
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US5366765A (en) * | 1993-05-17 | 1994-11-22 | United Technologies Corporation | Aqueous slurry coating system for aluminide coatings |
EP1010776A1 (en) * | 1998-12-14 | 2000-06-21 | General Electric Company | Caustic process for replacing thermal barrier coatings |
EP1076107A1 (en) * | 1999-08-09 | 2001-02-14 | ABB Alstom Power (Schweiz) AG | Process of plugging cooling holes of a gas turbine component |
US6544346B1 (en) * | 1997-07-01 | 2003-04-08 | General Electric Company | Method for repairing a thermal barrier coating |
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WO1996015863A1 (en) * | 1994-11-22 | 1996-05-30 | United Technologies Corporation | Cleaning method for turbine airfoils by ultrasonics |
US5643474A (en) * | 1995-12-26 | 1997-07-01 | General Electric Company | Thermal barrier coating removal on flat and contoured surfaces |
US6210488B1 (en) * | 1998-12-30 | 2001-04-03 | General Electric Company | Method of removing a thermal barrier coating |
US6274078B1 (en) * | 1999-01-27 | 2001-08-14 | General Electric Company | Method of removing cores from ceramic matrix composite articles |
US6475289B2 (en) * | 2000-12-19 | 2002-11-05 | Howmet Research Corporation | Cleaning of internal passages of airfoils |
US20050035086A1 (en) * | 2003-08-11 | 2005-02-17 | Chen Keng Nam | Upgrading aluminide coating on used turbine engine component |
-
2003
- 2003-12-16 US US10/707,465 patent/US20050127039A1/en not_active Abandoned
-
2004
- 2004-12-09 CA CA2490014A patent/CA2490014C/en not_active Expired - Fee Related
- 2004-12-09 DE DE602004031920T patent/DE602004031920D1/en not_active Expired - Lifetime
- 2004-12-09 EP EP04257665A patent/EP1548156B1/en not_active Expired - Fee Related
- 2004-12-16 SG SG200704440-7A patent/SG133599A1/en unknown
- 2004-12-16 SG SG200407463A patent/SG112984A1/en unknown
- 2004-12-16 BR BR0405921-2A patent/BRPI0405921A/en not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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US5366765A (en) * | 1993-05-17 | 1994-11-22 | United Technologies Corporation | Aqueous slurry coating system for aluminide coatings |
US6544346B1 (en) * | 1997-07-01 | 2003-04-08 | General Electric Company | Method for repairing a thermal barrier coating |
EP1010776A1 (en) * | 1998-12-14 | 2000-06-21 | General Electric Company | Caustic process for replacing thermal barrier coatings |
EP1076107A1 (en) * | 1999-08-09 | 2001-02-14 | ABB Alstom Power (Schweiz) AG | Process of plugging cooling holes of a gas turbine component |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
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EP1779936A2 (en) * | 2005-09-29 | 2007-05-02 | United Technologies Corporation | Squirter jet ultrasonic cleaning |
EP1779936A3 (en) * | 2005-09-29 | 2009-05-27 | United Technologies Corporation | Squirter jet ultrasonic cleaning |
EP3269840A1 (en) * | 2016-07-12 | 2018-01-17 | United Technologies Corporation | Method of chromizing an article including internal passages of the article |
Also Published As
Publication number | Publication date |
---|---|
CA2490014A1 (en) | 2005-06-16 |
US20050127039A1 (en) | 2005-06-16 |
BRPI0405921A (en) | 2005-09-06 |
CA2490014C (en) | 2013-02-12 |
EP1548156A3 (en) | 2010-01-13 |
SG133599A1 (en) | 2007-07-30 |
EP1548156B1 (en) | 2011-03-23 |
DE602004031920D1 (en) | 2011-05-05 |
SG112984A1 (en) | 2005-07-28 |
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