US20160160374A1 - Methods of forming an article using electrophoretic deposition, and related article - Google Patents

Methods of forming an article using electrophoretic deposition, and related article Download PDF

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US20160160374A1
US20160160374A1 US14/563,257 US201414563257A US2016160374A1 US 20160160374 A1 US20160160374 A1 US 20160160374A1 US 201414563257 A US201414563257 A US 201414563257A US 2016160374 A1 US2016160374 A1 US 2016160374A1
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Prior art keywords
barrier coating
electrically conductive
coating
disposing
combinations
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US14/563,257
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English (en)
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Nicholas Edward Antolino
Don Mark Lipkin
Stephen Francis Rutkowski
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General Electric Co
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General Electric Co
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Priority to US14/563,257 priority Critical patent/US20160160374A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: RUTKOWSKI, STEPHEN FRANCIS, ANTOLINO, NICHOLAS EDWARD, LIPKIN, DON MARK
Priority to CA2913436A priority patent/CA2913436A1/en
Priority to BR102015029666A priority patent/BR102015029666A2/pt
Priority to EP15196863.3A priority patent/EP3031957A1/de
Priority to JP2015234387A priority patent/JP2016108666A/ja
Priority to CN201510892914.8A priority patent/CN105671619A/zh
Publication of US20160160374A1 publication Critical patent/US20160160374A1/en
Abandoned legal-status Critical Current

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    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D13/00—Electrophoretic coating characterised by the process
    • C25D13/22—Servicing or operating apparatus or multistep processes
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81—Coating or impregnation
    • C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D13/00—Electrophoretic coating characterised by the process
    • C25D13/02—Electrophoretic coating characterised by the process with inorganic material
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D13/00—Electrophoretic coating characterised by the process
    • C25D13/12—Electrophoretic coating characterised by the process characterised by the article coated
    • 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
    • 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
    • C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
    • C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
    • C23C18/1601—Process or apparatus
    • C23C18/1633—Process of electroless plating
    • C23C18/1646—Characteristics of the product obtained
    • C23C18/165—Multilayered product
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition

Definitions

  • the present technology generally relates to methods of forming an article using electrophoretic deposition. More particularly, the present technology relates to methods of forming an article by disposing one or more barrier layers using electrophoretic deposition.
  • Monolithic ceramics, ceramic matrix composites (CMCs), and refractory metal silicides offer increased temperature capability over iron, nickel and cobalt-based superalloys.
  • CMCs are a class of materials that include a ceramic reinforcing material surrounded by a ceramic matrix phase. Such materials, along with certain monolithic ceramics (i.e. ceramic materials without a reinforcing material), provide a desirable combination of high-temperature strength and low density compared to metallic superalloys.
  • CMCs, monolithic ceramic components, and refractory metal silicides may be coated with environmental barrier coatings (EBCs) to protect them from the harsh environment of high temperature engine sections.
  • EBCs can protect the substrate from heat and corrosive gases in the combustion environment.
  • EBCs can protect silicon-containing substrates from volatilization in high temperature steam.
  • plasma spray the standard, industrial coating processes currently used to apply the EBCs (such as plasma spray) may have some drawbacks.
  • One such drawback is the difficulty in applying hermetic coatings onto components with non-line-of-sight features and regions of high convex and concave curvature.
  • a method for forming an article includes disposing an electrically conductive coating on a substrate.
  • the method further includes disposing a layer stack on the electrically conductive coating by (i) disposing a first barrier coating by electrophoretic deposition; (ii) heat treating the first barrier coating; (iii) disposing an electrically conductive layer on the first barrier coating; and (iv) optionally repeating steps (i) to (iii).
  • the method further includes disposing a second barrier coating on an outermost electrically conductive layer in the layer stack by electrophoretic deposition; and heat treating the second barrier coating.
  • a method for forming an article includes disposing an electrically conductive coating on a substrate.
  • the method further includes disposing a layer stack on the electrically conductive coating by (i) disposing a first barrier coating by electrophoretic deposition, wherein the first barrier coating includes a rare earth disilicate; (ii) heat treating the first barrier coating; (iii) disposing an electrically conductive layer on the first barrier coating; and (iv) optionally repeating steps (i) to (iii).
  • the method further includes disposing a second barrier coating on an outermost electrically conductive layer in the layer stack by electrophoretic deposition, wherein the second barrier coating includes a rare earth monosilicate; and heat treating the second barrier coating.
  • FIG. 1 a is an illustration of a method step according to an example of the present technology
  • FIG. 1 b is an illustration of a method step according to an example of the present technology
  • FIG. 1 c is an illustration of a method step according to an example of the present technology.
  • FIG. 2 is an illustration of a method according to an example of the present technology.
  • Approximating language may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about”, and “substantially” is not to be limited to the precise value specified. In some instances, the approximating language may correspond to the precision of an instrument for measuring the value. Similarly, “free” may be used in combination with a term, and may include an insubstantial number, or trace amounts, while still being considered free of the modified term.
  • range limitations may be combined and/or interchanged, such ranges are identified and include all the sub-ranges contained therein unless context or language indicates otherwise.
  • the term “layer” refers to a material disposed on at least a portion of an underlying surface in a continuous or discontinuous manner. Further, the term “layer” does not necessarily mean a uniform thickness of the disposed material.
  • the term “coating” refers to a material disposed on at least a portion of an underlying surface in a continuous or discontinuous manner. Further, the term “coating” does not necessarily mean a uniform thickness of the disposed material, and the disposed material.
  • the term “coating” may refer to a single layer of the coating material or may refer to a plurality of layers of the coating material. The coating material may be the same or different in the plurality of layers.
  • the term “disposed on” refers to layers or coatings disposed directly in contact with each other or indirectly by having intervening layers there between, unless otherwise specifically indicated.
  • adjacent as used herein means that at least a portion of the two layers or coatings are disposed contiguously and are in direct contact with each other.
  • FIGS. 1 and 2 illustrate a method 10 in accordance with an example of the present technology.
  • the method 10 includes, at step 11 , disposing an electrically conductive coating 120 on a substrate 110 .
  • the method further includes, at step 12 , forming a layer stack 150 on the electrically conductive coating 120 by: (i) disposing a first barrier coating 130 by electrophoretic deposition; (ii) heat treating the first barrier coating 130 ; (ii) disposing an electrically conductive layer 140 on the first barrier coating; and optionally repeating steps (i) to (iii).
  • the method further includes ( FIGS. 1 c and 2 ), at step 13 , disposing a second barrier coating 160 on an outermost electrically conductive layer 140 in the layer stack 150 by electrophoretic deposition.
  • the method further includes at step 14 , heat treating the second barrier coating 160 .
  • the substrate 110 may include a silicon-containing material.
  • suitable silicon-containing materials include silicon carbide, silicon nitride, silicide (for example, a refractory metal or transition metal silicide), elemental silicon, or combinations thereof.
  • the silicon containing material may be present in the substrate as one or both of the matrix and a second phase.
  • examples of substrate 110 include ceramic matrix composites (CMCs) or monolithic ceramics.
  • CMCs ceramic matrix composites
  • monolithic ceramics refers to ceramic materials without reinforcing materials, for example, fibers or whiskers.
  • CMCs refers to materials including ceramic fibers incorporated in a ceramic matrix, thus forming a ceramic fiber reinforced ceramic.
  • Suitable CMCs include silicon-containing CMCs and oxide-based CMCs, such as oxide-oxide CMCs.
  • one or both of the matrix and the reinforcing fiber may include a silicon-containing material, such as silicon, silicon carbide, silicon nitride, silicon oxycarbide, silicon oxynitride, or combinations thereof.
  • suitable CMCs include CMCs including silicon carbide matrix and silicon carbide fiber; CMCs including silicon nitride matrix and silicon carbide fiber; and CMCs including silicon carbide/silicon nitride matrix mixture and silicon carbide fiber.
  • one or both of the matrix and reinforcing fiber may include an oxide, such as aluminum oxide (Al 2 O 3 ), silicon dioxide (SiO 2 ), aluminosilicate, or combinations thereof.
  • Aluminosilicates may include crystalline materials such as mullite (3Al 2 O 3 .2SiO 2 ) as well as glassy aluminosilicates.
  • the electrically conductive coating 120 may include elemental silicon, metal silicide, silicon carbide, or combinations thereof.
  • suitable metal silicides include rare earth silicides, chromium silicide (e.g. CrSi 2 ), niobium silicide (e.g. NbSi 2 , Nb 5 Si 3 ), molybdenum silicide (e.g. MoSi 2 , Mo 5 Si 3 ), tantalum silicide (e.g. TaSi 2 ), titanium silicide (e.g. TiSi 2 ), tungsten silicide (e.g. WSi 2 , W 5 Si 3 ), zirconium silicide (e.g. ZrSi 2 ), hafnium silicide (e.g. HfSi 2 ), or combinations thereof.
  • the electrically conductive coating 120 includes elemental silicon.
  • the thickness of the electrically conductive coating 120 may be in a range from about 10 microns to about 150 microns.
  • the electrically conductive coating 120 may be disposed on the substrate 110 by plasma spray, combustion thermal spray, chemical vapor deposition, electron beam physical vapor deposition, molten silicon dipping, sputtering, powder-based application and sintering, and other conventional application processes known to those skilled in the art.
  • the electrically conductive properties of the coating 120 allows for deposition of the first barrier coating 130 by electrophoretic deposition.
  • the electrically conductive coating 120 may further function as a bond coating between the substrate and the overlying first barrier coating 130 .
  • the term “bond coating” as used herein refers to a coating that provides for improved adhesion between a substrate and an overlying coating.
  • the electrically conductive coating 120 may also serve as an oxidation barrier to prevent oxidation of the substrate 110 .
  • the method may further include a step of disposing an additional bond coating (not shown in Figures) on the substrate prior to the step of disposing the electrically conductive coating.
  • the method further includes forming a layer stack 150 .
  • the layer stack 150 may include a single first barrier coating 130 and a single electrically conductive layer 140 , as illustrated in FIG. 1 .
  • the first barrier coating 130 is disposed on the electrically conductive coating 120 by electrophoretic deposition followed by heat treatment and deposition of the electrically conductive layer 140 to form a layer stack 150 .
  • the second barrier coating 160 is then disposed on the electrically conductive layer 140 by electrophoretic deposition.
  • the method further includes heat treating the second barrier coating 160 .
  • the method further includes at least partial densification of the first barrier coating and the second barrier coating during the heat treatment steps.
  • the layer stack 150 may include a plurality of first barrier coatings 130 and a plurality of electrically conductive layers 140 .
  • the plurality of first barrier coatings 130 and the plurality of electrically conductive layers 140 are disposed in an alternating manner (not shown in Figures).
  • the method includes first disposing a first barrier coating 130 on the electrically conductive coating 120 by electrophoretic deposition, heat treating the first barrier coating 130 , disposing an electrically conductive layer 140 on the first barrier coating 130 , disposing a first barrier coating 130 on the electrically conductive layer 140 by electrophoretic deposition, heat treating the first barrier coating 130 , disposing an electrically conductive layer 140 on the first barrier coating 130 by electrophoretic deposition, and so on to form the layer stack 150 .
  • the first barrier coating 130 is deposited by electrophoretic disposition. Accordingly, in instances requiring a plurality of first barrier coatings 130 (for example, to build thickness while maintaining coating hermeticity and uniformity), application of an electrically conductive layer 140 prior to the deposition of the first barrier coating 130 facilitates electrophoretic deposition of the barrier coating material. Without the electrically conductive layers 140 , electrophoretic deposition of successive first barrier coatings 130 may not be possible as the first barrier coatings 130 are inherently electrically insulative.
  • barrier coating refers to a coating that may function as an environmental barrier coating, a thermal barrier coating, a chemical barrier coating, or combinations thereof.
  • a barrier coating may thus perform one or more of the following functions: inhibiting formation of volatile silicon hydroxide (for example, Si(OH) 4 ) products; inhibiting water vapor ingress to the oxidizing surface; inhibiting the ingress of chemical contaminants to the substrate; and reducing the amount of heat flux into the substrate.
  • a barrier coating may further exhibit one or more of the following properties: a coefficient of thermal expansion (CTE) compatible with the Si-containing substrate material, low permeability for oxidants, low thermal conductivity, low silica chemical activity, and chemical compatibility with the underlying Si-containing material and thermally grown silica.
  • the barrier coating is typically an electrically insulating material.
  • the first barrier coating 130 may include a material suitable for use on ceramic substrate components found in high temperature environments (e.g., operating temperatures greater than 1140° C.), such as those present in gas turbine engines.
  • the first barrier coating 130 includes a rare earth silicate.
  • the first barrier coating 130 includes a rare earth disilicate, a rare earth monosilicate, or combinations thereof.
  • Non-limiting examples of suitable rare earth metals include scandium, yttrium, lanthanum, cerium, gadolinium, praseodymium, neodymium, promethium, samarium, europium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or combinations thereof.
  • the first barrier coating 130 includes a rare earth disilicate, wherein the rare earth elements comprise ytterbium, yttrium, or combinations thereof.
  • the first barrier coating 130 may also include one or more additional constituents such as dopants, sintering aids and the like.
  • the first barrier coating 130 may further include rare earth monosilicates, wherein the rare earth elements comprise ytterbium, yttrium, or combinations thereof, as well as oxides of iron, aluminum, silicon or boron.
  • Each first barrier coating 130 may have a thickness in a range from about 5 microns to about 200 microns. In instances wherein the method includes disposing a plurality of first barrier coatings 130 , each first barrier coating 130 in the layer stack 150 may have the same composition as the other first barrier coatings 130 , or alternately may have a different composition. Further, the thickness of the first barrier coatings 130 in the layer stack 150 may be the same or different.
  • the electrically conductive layer 140 in the layer stack 150 allow for deposition of the subsequent barrier coating (first barrier coating 130 or second barrier coating 160 ) by electrophoretic deposition.
  • the electrically conductive layer 140 may include a material and a thickness capable of providing the desired conductive properties without significantly compromising the functionality or properties of the first barrier coating 130 and the second barrier coating 160 .
  • the electrically conductive layer 140 may include a metal, an intermetallic, a metalloid, carbon, a conductive polymer, or combinations thereof.
  • the electrically conductive layer 140 includes gold, silver, nickel, a conductive polymer, carbon, palladium, platinum, copper, iron, cobalt, boron, or combinations thereof.
  • the electrically conductive layer may include nanoparticles of an electrically conductive material in some instances.
  • the particle size may be in a range from 1 nanometer to about 10 nanometers.
  • the nanoparticles may be deposited on the first barrier coating 130 in a powder form or as a paste.
  • Each electrically conductive layer 140 may have a thickness in a range from about 10 nanometers to about 5 microns. In instances wherein the method includes disposing a plurality of electrically conductive layers 140 , each electrically conductive layer 140 in the layer stack 150 may have the same composition as the other electrically conductive layer 140 , or alternately may have a different composition. Further, the thickness of the electrically conductive layers 140 in the layer stack 150 may be the same or different.
  • the electrically conductive layer may be disposed by electroless (auto-catalytic) plating, spraying, dip coating or combinations thereof.
  • the method further includes disposing a second barrier coating 160 , as illustrated in FIGS. 1 and 2 .
  • the second barrier coating 160 may include a rare earth silicate.
  • the second barrier coating 160 may include a rare earth disilicate, a rare earth monosilicate, or combinations thereof.
  • suitable rare earth metals include scandium, yttrium, lanthanum, cerium, gadolinium, praseodymium, neodymium, promethium, samarium, europium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or combinations thereof.
  • the second barrier coating 160 includes a rare earth monosilicate selected from the group consisting of yttrium monosilicate, ytterbium monosilicate, and combinations thereof.
  • the second bather coating 160 may also include one or more additional constituents such as dopants, sintering aids and the like.
  • the second barrier coating 160 may further include rare earth disilicates, wherein the rare earth elements comprise ytterbium, yttrium, or combinations thereof, as well as oxides of iron, aluminum, silicon or boron.
  • the second barrier coating 160 may also have a thickness in a range from about 5 microns to about 300 microns.
  • the second bather coating 160 is deposited on the outermost electrically conductive layer 140 in the layer stack 150 by electrophoretic deposition.
  • the method further includes heat treating the second barrier coating.
  • Some of the example methods in accordance with the present technology allow for fabrication of articles by depositing one or more layers by electrophoretic deposition.
  • a first barrier coating is disposed over an electrically conductive coating and heat treated to at least partially densify it.
  • a thin electrically conductive layer is disposed over the underlying first barrier coating, allowing for deposition of a subsequent first barrier coating by electrophoretic deposition. This sequence is optionally repeated to build up a stack of first barrier layers. Further, disposing an outermost thin electrically conductive layer on the layer stack allows for deposition of the second barrier coating by electrophoretic deposition.
  • An article formed by the method described herein is also presented.
  • the present technology is generally applicable to components that operate within environments characterized by high temperatures, thermal cycling, thermal and mechanical stresses, and oxidation.
  • components include high and low pressure turbine vanes (nozzles) and blades (buckets), shrouds, combustor components (e.g., liners), heat shields, augmentor hardware, and other hot section components of turbine engines, though the technology has application to other components.
  • a turbine engine component including the article as described herein is also presented.
  • a silicon coated ceramic matrix composite was provided such that its surface was electrically conductive.
  • a layer of ytterbium disilicate was deposited by electrophoretic deposition from a bath consisting of 28 percent by mass ytterbium disilicate, 0.25 percent by mass iron (IIM) oxide, 0.05 percent by mass aluminum oxide, 0.05 percent by mass polyethylenimine, and 71.65 percent by mass ethanol using a voltage of 60 volts at 2 cm standoff for 15 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • the coating was then placed into a commercially available electroless gold bath (angelgilding.com) for 40 minutes according to the manufacturer's instructions.
  • yttrium monosilicate was deposited by electrophoretic deposition from a bath consisting of 22.72 percent by mass yttrium monosilicate, 0.67 percent by mass iron (IIM) oxide, 0.05 percent by mass polyethylenimine, and 76.56 percent by mass ethanol using a voltage of 30 volts at 1.7 cm standoff for 10 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • a silicon-coated ceramic matrix composite was provided such that its surface was electrically conductive.
  • a layer of ytterbium disilicate was deposited by electrophoretic deposition from a bath consisting of 28 percent by mass ytterbium disilicate, 0.25 percent by mass iron (IIM) oxide, 0.05 percent by mass aluminum oxide, 0.05 percent by mass polyethylenimine, and 71.65 percent by mass ethanol using a voltage of 60 volts at 2 cm standoff for 15 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • a fine aerosol of silver nanoparticles (Harima NPS-J Nano Paste®) was applied to the coating and heat treated at 220 degrees Celsius in air for 1 hour.
  • a second layer of ytterbium disilicate was deposited by electrophoretic deposition from a bath consisting of 28 percent by mass ytterbium disilicate, 0.25 percent by mass iron (IIM) oxide, 0.05 percent by mass aluminum oxide, 0.05 percent by mass polyethylenimine, and 71.65 percent by mass ethanol using a voltage of 60 volts at 2 cm standoff for 15 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • another layer of fine aerosol of silver nanoparticles was applied to the coating and heat treated at 220 degrees Celsius in air for 1 hour.
  • yttrium monosilicate was deposited by electrophoretic deposition from a bath consisting of 22.72 percent by mass yttrium monosilicate, 0.67 percent by mass iron (IIM) oxide, 0.05 percent by mass polyethylenimine, and 76.56 percent by mass ethanol using a voltage of 30 volts at 1.7 cm standoff for 10 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • a silicon-coated ceramic matrix composite was provided such that its surface is electrically conductive.
  • a layer of ytterbium disilicate was deposited by electrophoretic deposition from a bath consisting of 28 percent by mass ytterbium disilicate, 0.25 percent by mass iron (II,II) oxide, 0.05 percent by mass aluminum oxide, 0.05 percent by mass polyethylenimine, and 71.65 percent by mass ethanol using a voltage of 60 volts at 2 cm standoff for 15 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.
  • the coating was then dipped into a bath of Plexcore® OC RG-1110 conductive polymer and withdrawn to leave a thin coating.
  • the conductive coating was cured at 150 degrees Celsius in air for 1 hr.
  • a layer of yttrium monosilicate was deposited by electrophoretic deposition from a bath consisting of 22.72 percent by mass yttrium monosilicate, 0.67 percent by mass iron (II,II) oxide, 0.05 percent by mass polyethylenimine, 76.56 percent by mass ethanol using a voltage of 30 volts at 1.7 cm standoff for 10 seconds.
  • the coating was air dried and heat treated in air at 1345 degrees Celsius for 10 hours.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Electrochemistry (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Structural Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
US14/563,257 2014-12-08 2014-12-08 Methods of forming an article using electrophoretic deposition, and related article Abandoned US20160160374A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US14/563,257 US20160160374A1 (en) 2014-12-08 2014-12-08 Methods of forming an article using electrophoretic deposition, and related article
CA2913436A CA2913436A1 (en) 2014-12-08 2015-11-25 Methods of forming an article using electrophoretic deposition, and related article
BR102015029666A BR102015029666A2 (pt) 2014-12-08 2015-11-26 métodos para formar um artigo, artigo e componente de motor de turbina
EP15196863.3A EP3031957A1 (de) 2014-12-08 2015-11-27 Verfahren zur herstellung eines artikels mit elektrophoretischer abscheidung und entsprechende artikel
JP2015234387A JP2016108666A (ja) 2014-12-08 2015-12-01 電気泳動堆積法を用いた物品の形成方法並びに関連物品
CN201510892914.8A CN105671619A (zh) 2014-12-08 2015-12-08 使用电泳沉积形成制品的方法及相关的制品

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US14/563,257 US20160160374A1 (en) 2014-12-08 2014-12-08 Methods of forming an article using electrophoretic deposition, and related article

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CN109627014B (zh) * 2019-01-14 2021-07-13 中国科学院上海硅酸盐研究所 一种高强度、高导热性的Si3N4陶瓷材料及其制备方法

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Cited By (3)

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Publication number Priority date Publication date Assignee Title
US11479873B2 (en) * 2017-11-21 2022-10-25 Safran Helicopter Engines Method for producing a thermal barrier on a part of a turbomachine
US20210143006A1 (en) * 2019-10-04 2021-05-13 Commissariat A L'energie Atomique Et Aux Energies Alternatives Method of manufacturing an electronic device
US11682553B2 (en) * 2019-10-04 2023-06-20 Commissariat A L'energie Atomique Et Aux Energies Alternatives Method of manufacturing an electronic device

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