AU2002358833B2 - Coating precursor and method for coating a substrate with a refractory layer - Google Patents

Coating precursor and method for coating a substrate with a refractory layer Download PDF

Info

Publication number
AU2002358833B2
AU2002358833B2 AU2002358833A AU2002358833A AU2002358833B2 AU 2002358833 B2 AU2002358833 B2 AU 2002358833B2 AU 2002358833 A AU2002358833 A AU 2002358833A AU 2002358833 A AU2002358833 A AU 2002358833A AU 2002358833 B2 AU2002358833 B2 AU 2002358833B2
Authority
AU
Australia
Prior art keywords
precursor
coating
refractory
proportion
weight
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.)
Ceased
Application number
AU2002358833A
Other versions
AU2002358833A1 (en
AU2002358833B9 (en
Inventor
Christian Barthelemy
Airy-Pierre Lamaze
Robert Rey-Flandrin
Thomas Spadone
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rio Tinto France SAS
Constellium Issoire SAS
Original Assignee
Aluminium Pechiney SA
Pechiney Rhenalu SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from FR0113267A external-priority patent/FR2830857B1/en
Priority claimed from PCT/FR2002/003485 external-priority patent/WO2003033767A2/en
Application filed by Aluminium Pechiney SA, Pechiney Rhenalu SAS filed Critical Aluminium Pechiney SA
Publication of AU2002358833A1 publication Critical patent/AU2002358833A1/en
Application granted granted Critical
Publication of AU2002358833B2 publication Critical patent/AU2002358833B2/en
Publication of AU2002358833B9 publication Critical patent/AU2002358833B9/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/62222Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining ceramic coatings
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/622Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/626Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
    • C04B35/63Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B using additives specially adapted for forming the products, e.g.. binder binders
    • C04B35/632Organic additives
    • C04B35/634Polymers
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/50Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
    • C04B41/5022Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials with vitreous materials
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/50Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
    • C04B41/5025Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials with ceramic materials
    • C04B41/5037Clay, Kaolin
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81Coating or impregnation
    • C04B41/85Coating or impregnation with inorganic materials
    • C04B41/86Glazes; Cold glazes
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81Coating or impregnation
    • C04B41/85Coating or impregnation with inorganic materials
    • C04B41/87Ceramics
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L83/00Compositions of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon only; Compositions of derivatives of such polymers
    • C08L83/04Polysiloxanes
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09DCOATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D183/00Coating compositions based on macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing silicon, with or without sulfur, nitrogen, oxygen, or carbon only; Coating compositions based on derivatives of such polymers
    • C09D183/04Polysiloxanes
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C18/00Chemical 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
    • C23C18/02Chemical 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 thermal decomposition
    • C23C18/12Chemical 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 thermal decomposition characterised by the deposition of inorganic material other than metallic material
    • C23C18/1204Chemical 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 thermal decomposition characterised by the deposition of inorganic material other than metallic material inorganic material, e.g. non-oxide and non-metallic such as sulfides, nitrides based compounds
    • C23C18/1208Oxides, e.g. ceramics
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C18/00Chemical 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
    • C23C18/02Chemical 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 thermal decomposition
    • C23C18/12Chemical 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 thermal decomposition characterised by the deposition of inorganic material other than metallic material
    • C23C18/1225Deposition of multilayers of inorganic material
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C18/00Chemical 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
    • C23C18/02Chemical 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 thermal decomposition
    • C23C18/12Chemical 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 thermal decomposition characterised by the deposition of inorganic material other than metallic material
    • C23C18/125Process of deposition of the inorganic material
    • C23C18/1275Process of deposition of the inorganic material performed under inert atmosphere
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/00474Uses not provided for elsewhere in C04B2111/00
    • C04B2111/0087Uses not provided for elsewhere in C04B2111/00 for metallurgical applications
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2111/00Mortars, concrete or artificial stone or mixtures to prepare them, characterised by specific function, property or use
    • C04B2111/00474Uses not provided for elsewhere in C04B2111/00
    • C04B2111/0087Uses not provided for elsewhere in C04B2111/00 for metallurgical applications
    • C04B2111/00879Non-ferrous metallurgy
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G77/00Macromolecular compounds obtained by reactions forming a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon in the main chain of the macromolecule
    • C08G77/04Polysiloxanes
    • C08G77/14Polysiloxanes containing silicon bound to oxygen-containing groups
    • C08G77/16Polysiloxanes containing silicon bound to oxygen-containing groups to hydroxyl groups
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/01Use of inorganic substances as compounding ingredients characterized by their specific function
    • C08K3/013Fillers, pigments or reinforcing additives

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Structural Engineering (AREA)
  • Metallurgy (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • General Chemical & Material Sciences (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Health & Medical Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Paints Or Removers (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Description

ABSTRACT
COATING PRECURSOR AND METHOD FOR COATING A SUBSTRATE WITH A REFRACTORY LAYER The purpose of the invention is a coating precursor comprising a silicone resin, a mineral filler and an organic solvent capable of dissolving the said resin and putting the said mineral filler into suspension, the said silicone resin and the said mineral filler being capable of chemically reacting so as to produce a solid layer on a substrate after the organic solvent has evaporated and a cohesive refractory layer after a calcination operation.
Another purpose of the invention is a method for coating a given surface of a substrate with at least one refractory layer containing silicon in which the substrate is coated with a coating precursor according to the invention so as to form a green layer and a heat treatment is carried out to calcine the said green layer and to form a cohesive refractory layer. The invention is a means of obtaining a protective coating capable of resisting oxidising environments, liquid metal and solid or molten salt.
N, liquid aluminium alloys satisfactorily under the most demanding conditions and a applications.
Description of the Invention
INO
C An object of the invention is a coating precursor to be used for the formation of a protective layer on a substrate. The said precursor comprises a silicone resin and a Cc mineral filler capable of reacting chemically with the said resin so as to produce a 00 cohesive refractory layer after a calcination operation of the layer.
More precisely, an object of the invention is a coating precursor comprising a silicone resin (or organosiloxane), a mineral filler and an organic solvent capable of dissolving the said resin and putting the said mineral filler into suspension, the said silicone resin and the said mineral filler being capable of chemically reacting so as to produce a solid layer on a substrate after the organic solvent has evaporated and a cohesive refractory layer after a calcination operation.
Accordingly, in a first embodiment the invention relates to a coating precursor comprising a silicone resin, a mineral filler and an organic solvent capable of dissolving the said resin and putting the mineral filler into suspension, the silicone resin and the mineral filler being intended to chemically react so as to produce a solid layer on a substrate after the organic solvent has evaporated and a cohesive refractory layer after a calcination operation, the silicone resin being a polymethylsiloxane or a polymethylsilsesquioxane, or a mixture thereof, comprising a proportion of OH groups substituted for methyl groups comprised between about 0.5% and about 2%.
In a second embodiment the invention relates to a method for coating a given surface of a substrate with at least one refractory layer containing silicon wherein: the said surface is coated with a coating precursor according to the first embodiment of the invention, so as to form a green layer; a heat treatment called calcination treatment is carried out to eliminate volatile materials, to calcine the said green layer and to form a cohesive refractory layer.
In a third embodiment the invention relates to a method for coating a given surface of a substrate with at least one refractory layer containing silicon, wherein: the said surface is coated with a coating precursor according to the first embodiment of the invention, wherein the precursor is in the form of a paste, so as to form a green layer, a heat treatment called calcination treatment is carried out to eliminate volatile materials, to calcine the said green layer and to form a cohesive refractory layer.
0 2a C In a fourth embodiment the invention relates to the use of the precursor according to the first embodiment of the invention or of the method according to the second or third
C
1 embodiment of the invention for the protection of a material and/or a piece of equipment I that will be exposed to an oxidising environment, or liquid metal and/or a solid or molten salt.
SIn a fifth embodiment of the invention there is provided a substrate characterised in 00 00 that at least part of the surface comprises at least one refractory layer obtained using a t precursor according to the first embodiment of the invention or using the method according to the second or third embodiment of the invention.
S 10 The said precursor is preferably homogeneous.
The silicone resin is a polysiloxane preferably comprising a proportion of OH groups, such as a polymethylsiloxane, a polydimethylsiloxane, a polymethylsilsesquioxane, or a mixture thereof, comprising a proportion of OH groups substituted for methyl groups. The applicant has noted that the proportion of OH groups is preferably between about 0.5% and about If the proportion of OH groups is too low, there will not be sufficient propension to
I
If 3 form a solid layer after the solvent has evaporated and with good cohesiveness after calcination. A very high proportion of OH groups may make the polysiloxane difficult to produce at an acceptable cost. The silanol (Si-OH) groups are preferably stable so that the resin can be stored. These OH groups may be grafted to a polysiloxane by hydrolysis. The siloxanic patterns of the polysiloxane according to the invention are advantageously wholly or partly trifunctional or quadrifunctional.
The organic solvent is typically an apolar solvent such as a xylene or a toluene. The xylene may be a mixture of different types of xylene, such as o and p.
The mineral filler is typically chosen from among metal borides, carbides, nitrides and oxides, or from among non-metal borides, carbides and nitrides (such as boron nitrides) or a combination or a mixture thereof.
The said mineral filler is advantageously chosen from among metal compounds such as metal oxides, metal carbides, metal borides and metal nitrides, or a combination or a mixture thereof. The mineral filler is preferably capable of chemically reacting with the silicone resin so as to produce a solid layer after the organic solvent has evaporated and a refractory layer with good cohesiveness after calcination of the said green layer. The mineral filler may be chosen as a function of the physicochemical characteristics expected from the coating (such as wettability or nonwettability by a liquid metal).
The metal compound is advantageously alumina, Zr02, ZrB 2 TiB 2 or TiO 2 or a combination or a mixture thereof. The alumina is preferably a reactive calcined alpha alumina called a technical alumina, with a very low hydration ratio (typically less than or even less than The mineral filler is preferably in the form of a fine powder, which can give a fluid precursor and a uniform coating. It is typically added to the silicone resin organic solvent mixture after a fine grinding operation. The size grading of the mineral filler powder is typically such that the size of the grains is between 0.05 im and 50 im.
The physical properties of the coating, such as its mechanical properties, can sometimes be adapted by adjusting the proportion of the mineral filler and /or its size grading.
According to one preferred embodiment of the invention, the precursor is typically in the form of a slurry or a slip. It is typically obtained by mixing the resin, the mineral filler and the organic solvent.
In this embodiment, the proportion of silicone resin in the precursor is typically between 5 and by weight, and preferably between 7.5 and 20% by weight, to enable satisfactory ceramisation of the coating during calcination. Apart from the solvent, the proportion of silicone resin in the precursor is typically between 15 and 40% by weight.
The proportion of organic solvent in the precursor is then typically between 7.5% and 60% by weight, and preferably between 15 and 30% byweight. The solvent quantity is preferably such that all the silicone resin is dissolved and the mineral filler can be put into suspension in the solution obtained.
The proportion of the mineral filler in the precursor is typically between 30% and 75% by weight, and preferably between 45 and 70% by weight. If the proportion is too low, the deposition will be too thin and consequently it will be necessary to deposit a large number of layers in succession. If the proportion is too large, the precursor will be difficult to spread.
According to another preferred embodiment of the invention, the precursor is typically in the form of a paste.
In this embodiment, the proportion of silicone resin in the precursor is then typically between and 20% by weight, and preferably between 10 and 17.5% by weight, to enable satisfactory ceramisation of the coating during calcination.
The proportion of organic solvent in the precursor is typically between 2.5% and 10% by weight.
The proportion of mineral filler in the precursor is typically between 70% and 95% by weight, and preferably between 75% and 90% by weight.
In this embodiment, the coating precursor advantageously includes an additive capable of reducing the viscosity of the precursor. The said additive typically comprises a dispersing agent such as stearic acid. The proportion of the said additive in the precursor is typically less than 2% by weight, and more typically between 0.1 and 1%.
t 6 The precursor is typically obtained by mixing the resin, the mineral filler and the additive, and if necessary grinding the mixture.
Another object of the invention is a method for coating a given surface of a substrate with at least one refractory layer containing silicon wherein: the substrate is coated with a coating precursor according to the invention so as to form a green layer; a heat treatment called calcination treatment is carried out to eliminate volatile materials, to calcine the said green layer and to form a cohesive refractory layer.
The applicant has observed that the method according to the invention can give a strong thin layer bonding strongly to the substrate that has good resistance to liquid metal and that has good cohesiveness.
The coating precursor may be prepared in at least two operations: a silicone resin is dissolved in an organic solvent so as to obtain a solution of silicone resin; the mineral filler is added into the solution of silicone resin thus obtained.
The substrate may be coated (typically including the deposition and spreading of the said precursor on the substrate) by any known means. For example, the coating may be deposited by brushing (typically using a brush and or a roller), by dipping, by atomisation or by spraying (typically using a spray gun). Brushing, dipping and atomisation are particularly adapted to the deposition of precursors in the form of a slurry or
L
slip. Spraying is particularly adapted to the deposition of precursors in the form of a paste. The temperature of the substrate may possibly be increased above the ambient temperature before coating in order to facilitate the formation of a homogeneous deposit and bonding of the deposition by melting of the resin.
The method according to the invention may also comprise complementary operations such as preparation of the parts of the substrate surface to be coated and or drying of the green coating before the heat treatment. The said drying treatment serves in particular to evaporate the said organic solvent and, at least partially, to solidify the green layer (so that the substrate can be handled without damaging the layer). The preparation of the substrate surface typically includes cleaning and or degreasing (for example using acetone).
In some applications, it may be advantageous to use a coating precursor also containing a wetting agent capable of facilitating the formation of a thin layer.
This is the case particularly for some screen filters for which it is required to coat the wires of the metal mesh without blocking the openings. The said wetting agent is preferably a silane polyether, which encourages spreading of the coating on the substrate without preventing ceramisation of the refractory coating during the heat treatment. The chemical formula of the said silane polyether is typically:
/O-R
CH3 0 (CH 2
CH
2 0 10 CH2 CH 2
CH
2 Si O R
\O-R
where R is an alkyl group and typically a methyl.
Advantageously, the wetting agent also prevents or significantly delays the precursor caking.
The proportion of wetting agent in the precursor is typically between about 1 and 5% by weight, and is preferably between 2 and 4% by weight for precursors in the form of a slip or a slurry and between 2 and 5% by weight for precursors in the form of a paste.
The so-called calcination heat treatment comprises at least one step at a high temperature, typically between 650 and 1300 0 C, and more typically between 800 and 13000C, capable of transforming the green layer into a refractory ceramic, that is advantageously in the vitreous state. The composition of the vitreous phase typically comprises between 5 and 25% by weight of silica obtained from the resin (the remainder, typically 75 to 95% by weight, consists essentially of the mineral filler). The calcination temperature also depends on the substrate; for example, in the case of a metallic substrate, it is advantageously less than the softening temperature of the substrate.
Furthermore, it is also preferable to use a calcination temperature greater than the working temperature of the coated substrate. The heat treatment may include an intermediate step at a temperature of between 200 and 6000C (typically between 200 and 2500C). This intermediate step is preferably capable of causing crosslinking of the resin, and possibly decomposition of the resin, before "ceramisation" (or final calcination) of the coating. In this case, it is possible, according to an advantageous variant of the invention, to continue in situ calcination heat treatment, in other words when using the substrate at high temperature (advantageously higher than 650 0
C).
The duration of the heat treatment is advantageously such that it enables complete ceramisation of the precursor. The temperature increase is preferably sufficiently slow to prevent the coating from cracking.
During the heat treatment, the organic compounds are eliminated (by evaporation and or by decomposition) leaving a refractory solid on a surface of the substrate. For example, this solid may be formed from metal originating from the metal compound and silicon originating from the silicone resin. In the case of alumina, silanol groups Si-OH of the polysiloxane seem to create covalent links with the OH groups of alumina, the said links seem to transform into Si-O-Al links with release of water, during the heat treatment to form an aluminosilicate, which is advantageously in the vitreous state. A similar mechanism may occur with metal compounds other than alumina.
The ambient atmosphere during the calcination treatment is advantageously non-oxidizing, particularly to prevent oxidation of the substrate at the substratecoating interface that could cause decohesion between the substrate and the coating, or possibly destruction of the substrate (for example when the substrate is made of graphite).
The final coating may comprise two or more successive layers that may be applied by coatings and successive heat treatments, i.e. by successive coating heat treatment sequences. In other words, the layer coating and calcination treatment operations are repeated for each elementary layer in the final coating. The successive layers may have a different composition, such that they have different chemical and mechanical properties. This variant provides a means of adapting each layer to a local function, such as bond to the substrate for the first layer, mechanical strength for intermediate layers and chemical resistance for the surface layer.
Another object of the invention is a substrate in which at least part of the surface comprises at least one refractory layer obtained using the said precursor or using the said coating method, the said refractory layer being advantageously in the vitreous state, with or without a gradient of the composition in the direction perpendicular to the surface of the substrate.
Another object of the invention is the use of the said precursor or the said coating method for the protection of a substrate, particularly for the protection of a material and or a piece of equipment that will be exposed to an oxidising environment, or liquid metal (particularly aluminium, an aluminium alloy, magnesium or a magnesium alloy, in the liquid state) and or a solid or molten salt.
The term "substrate" must be understood in the broad sense: the substrate may be made of metal (such as an iron nickel chromium based alloy (typically a steel or inconel) or a refractory material or a carbonaceous material (such as graphite), or a mixture or a combination thereof; it may be a particular object (typically a piece of equipment, such as a metallic or refractory component of a casting unit, a nozzle, a liquid metal distributor in a sump, a screen made of steel (particularly stainless steel) or a refractory or ceramic material, a metallic or refractory filter, a liquid metal or gas bubbles injector, a rotor, a scraper, a pouring spout, an ultrasound sensor, a measurement sensor (ultrasound, temperature, etc.) designed to be immersed in liquid metal, parts made of carbonaceous materials, bricks made of graphite, etc.), or a material, particularly a coating material (such as a brick made of a refractory material or a carbonaceous material (such as graphite) The substrate may be porous or non-porous.
Tests Several tests have been carried out on different substrates. These tests were carried out using the following components: *Mineral fillers: a calcined alpha alumina powder (technical alumina ref. P172SB made by the Aluminium Pechiney company) with a D50 of 0.5 pm and a BET specific surface area of 6 to 8 m 2 The alumina was finely ground (size grading typically between 0.2 pum and In); a Zr02 powder (Saint Gobain reference CS02) with a D50 of 0.8 iun and a BET of 5.5 m 2 /g; 1- 12 a TiO 2 powder (Kemira reference UV Titan P 370), with a grain size of 0.06 pm; a TiB 2 powder (reference Metabap 143) with a of 1.7 pm; *Silicone resin: a MK polymethylsiloxane made by the Wacker company, which is a trifunctional resin with about 1% of OH groups. This resin was composed of about 80% of silica equivalent and 20% of methyl groups, which dissociate at a temperature of the order of 450 0
C;
*Organic solvent: xylene; *Wetting agent: a Dynasylan® 4140 polysilane made by the D6gussa-HUls company (about 3% by weight compared with the quantity of metal compound in all cases).
Series of tests with slip Several slip compositions were tested. They had the compositions given in table I by weight). The proportions were such that the refractory coating obtained comprised about 80% by metal compound equivalent weight (or mixture of metal compounds) and by silica equivalent weight. The concentration of silicone resin in the xylene was about 250 g/l.
Table I Component No. 1 No. 2 No. 3 No. 4 No. 5 No. 6 Alumina 44.9 35.9 (Al 2 0 3 Zirconia 44.9 (ZrO 2 Titanium 30.2 oxide (TiO 2 Titanium 9 44.9 66.0 diboride (TiB 2 Silicone 14 14 9.4 14 14 11.2 resin Organic 39.8 39.8 59.4 39.8 39.8 22.8 solvent_ Wetting 1.35 1.35 0.9 1.35 1.35 agent Xylene was mixed so as to obtain a homogeneous mixture. The silicone resin was dissolved at ambient temperature in this organic solvent until a homogeneous solution was obtained. If necessary, the wetting agent was then added to this solution. After a 10 minute ageing time, the filler was added to this solution and mixed (by stirring) so as to obtain a homogeneous slurry.
Several tests were carried out on a 304 L stainless steel grid, as a substrate. The diameter of the wires on this grid was 100 um and the mesh size was 200 pm.
The substrate was previously cleaned using a solvent capable of degreasing surfaces, particularly acetone. In some tests, the grid was also dipped in a caustic soda solution (for example 60 g/l at ambient temperature).
The slip was deposited in a thin layer on the substrate by painting (using a brush and a roller so as to open up the meshes). The coated substrate was then left in the open air for a few minutes so that the solvent could evaporate. It was then found that the layer dried quickly and that the deposition bonded firmly to the substrate (the deposition was very hard and uniform, and the grid could easily be handled).
The percent of blocked meshes was small (typically less than After the drying operation, the substrate coated with slip was heat treated for one hour at a temperature of 900 0
C.
Typically, the coating was obtained by deposition and baking of four thin and successive uniform layers.
Excess precursors in each deposition were removed so as to prevent the occurrence of bond defects. The final thickness of the coating was typically of the order of lm. This coating was very uniform and strong (with good cohesiveness and non-powdering) and did not block up the grid openings (the mesh size was reduced only to about 100 jim).
The grids thus coated were dipped in liquid aluminium for two hours at a temperature of between 700 and 800 0 C. This test did not show up any deterioration to the coating.
Grids thus coated were used to filter liquid aluminium. This test showed that these grids enable circulation of liquid aluminium without any excessive pressure loss and without damage to the coating. The results obtained for initial flows on an area of the order of 13 cm 2 are shown in table II.
I
These results show that the metal flow is high with all tested slips.
Table II Slip No. 1 No. 2 No. 3 No. 4 No. Initial flow 0.011 0.017 0.045 0.05 0.19 (kg/s) The few tests carried out with a slip similar to slip No. 5, but without a wetting agent, gave results similar to those obtained with slip No. 5. Slip No. 6 gave flows similar to those obtained with slips No. 1 to Series of tests with paste A paste composition was tested. Its composition was by weight): 82% of mineral filler (alumina), 13.9% of silicone resin and 4.1% of organic solvent.
The proportions were such that the refractory coating obtained comprised about 80% of metal compound equivalent weight (or a mixture of metal compounds) and by silica equivalent weight. The compositions did not include any wetting agent.
The paste obtained was deposited on a metallic substrate (a thin strip) made of 304 L stainless steel using a spatula.
After the drying operation, the coated substrate was cross-linked at a temperature of 2400C for one hour and was then baked at a temperature of 8000C.
The final thickness of the coating was typically of the order of 200 to 300 pm. This coating was very uniform and strong (with good cohesiveness and nonpowdering).

Claims (42)

  1. 2. Coating precursor according to claim 1, characterised in that the siloxanic patterns of the silicone resin include trifunctional or quadrifunctional patterns.
  2. 3. Coating precursor according to any one of claims 1 or 2, characterised in that the said organic solvent is apolar.
  3. 4. Precursor according to claim 3, characterised in that the apolar organic solvent is a xylene or a toluene.
  4. 5. Coating precursor according to any one of claims 1 to 4, characterised in that the mineral filler is chosen from among metal oxides, metal and non-metal carbides, metal and non-metal borides and metal and non-metal nitrides, or a combination or a mixture thereof.
  5. 6. Coating precursor according to claim characterised in that the mineral filler comprises a calcined alpha alumina.
  6. 7. Coating precursor according to claim 5 or 6, characterised in that the mineral filler is chosen from the group comprising ZrO 2 ZrB 2 TiB 2 TiO 2 boron nitride, and a mixture or a combination thereof.
  7. 8. Coating precursor according to any one of claims 1 to 7, characterised in that the mineral filler is in the form of a powder with the size of the grains between 0.05 pm and 50 pm.
  8. 9. Coating precursor according to any one of claims 1 to 8, characterised in that the said coating precursor also contains a wetting agent capable of facilitating the formation of a thin layer.
  9. 10. Coating precursor according to claim 9, characterised in that the said wetting agent is a silane polyether.
  10. 11. Coating precursor according to either claim 9 or 10, characterised in that the proportion of wetting agent in the precursor is between 1 and by weight.
  11. 12. Precursor according to any one of claims 1 to 11, characterised in that it is in the form ofa slurry or a slip.
  12. 13. Precursor according to claim 12, characterised in that the proportion of solvent in the precursor is between 7.5% and 60% by weight.
  13. 14. Precursor according to claim 12, characterised in that the proportion of solvent in the precursor is between 15% and 30% by weight. Coating precursor according to any one of claims 12 to 14, characterised in that the proportion of silicone resin in the precursor is between 5 and 30% by weight.
  14. 16. Coating precursor according to any one of claims 12 to 14, characterised in that the proportion of silicone resin in the precursor is between 7.5 and 20% by weight.
  15. 17. Precursor according to any one of claims 12 to 16, characterised in that the proportion of mineral filler in the precursor is between 30% and by weight.
  16. 18. Precursor according to any one of claims 12 to 16, characterised in that the proportion of mineral filler in the precursor is between 45% and by weight.
  17. 19. Precursor according to any one of claims 1 to 11, characterised in that it is in the form of a paste. Precursor according to claim 19, characterised in that the proportion of solvent in the precursor is between 2.5% and 10% by weight.
  18. 21. Precursor according to claim 19, characterised in that the proportion of solvent in the precursor is between 10% and 17.5% by weight.
  19. 22. Coating precursor according to any one of claims 19 to 21, characterised in that the proportion of silicone resin in the precursor is between 7.5 and 20% by weight.
  20. 23. Coating precursor according to any one of claims 19 to 21, characterised in that the proportion of silicone resin in the precursor is between 10 and 17.5% by weight.
  21. 24. Precursor according to any one of claims 19 to 23, characterised in that the proportion of mineral filler in the precursor is between 70% and by weight. Precursor according to any one of claims 19 to 23, characterised in that the proportion of mineral filler in the precursor is between 75% and by weight.
  22. 26. Precursor according to any one of claims 19 to 23, characterised in that it also includes an additive capable of reducing the viscosity of the precursor.
  23. 27. Precursor according to claim 26, characterised in that the additive comprises a dispersing agent such as a stearic acid.
  24. 28. Precursor according to claim 26 or 27, characterised in that the proportion of additive in the precursor is less than 2% by weight.
  25. 29. Precursor according to claim 27 or 28, characterised in that the proportion of additive in the precursor is between 0.1 and 1% by weight. Method for coating a given surface of a substrate with at least one refractory layer containing silicon wherein: the said surface is coated with a coating precursor according to any one of claims 1 to 18, so as to form a green layer; a heat treatment called calcination treatment is carried out to eliminate volatile materials, to calcine the said green layer and to form a cohesive refractory layer.
  26. 31. Method according to claim 30, wherein coating is deposited by brushing, by dipping or by atomisation.
  27. 32. Method for coating a given surface of a substrate with at least one refractory layer containing silicon wherein: the said surface is coated with a coating precursor according to any one of claims 19 to 29, so as to form a green layer; a heat treatment called calcination treatment is carried out to eliminate volatile materials, to calcine the said green layer and to form a cohesive refractory layer.
  28. 33. Method according to claim 32, wherein coating is deposited by spraying.
  29. 34. Method according to any one of claims 30 to 33, wherein the temperature of the substrate is increased above the ambient temperature before coating.
  30. 35. Method according to any one of claims 30 to 34, wherein the said calcination treatment comprises at least one step at a temperature of between 650 and 1300 0 C capable of transforming the green layer into a refractory ceramic.
  31. 36. Method according to any one of claims 30 to 35, wherein the said heat treatment comprises an intermediate step at a temperature of between 200 and 600'C.
  32. 37. Method according to any one of claims 30 to 36, wherein the said calcination treatment is carried out in a non-oxidising atmosphere.
  33. 38. Method according to any one of claims 30 to 37, wherein the said refractory layer is formed from several successive layers.
  34. 39. Method according to any one of claims 30 to 38, characterised in that the said substrate is made of metal, a refractory material or a carbonaceous material, or a mixture or a combination thereof. Method according to claim 39, characterised in that the said metal is an iron nickel chromium based alloy.
  35. 41. Method according to any one of claims 30 to 38, wherein the said substrate is chosen from the group comprising metallic or refractory components of a casting unit, nozzles, liquid metal distributors in a sump, screens made of steel, stainless steel, a refractory material or ceramic, metallic filters, refractory filters, liquid metal injectors, gas bubble injectors, rotors, scrapers, pouring spouts, ultrasound sensors, measurement sensors designed to be immersed in liquid metal, bricks made of refractory material, parts made of carbonaceous materials and bricks made of graphite.
  36. 42. Use of the precursor according to any one of claims 1 to 29 or of the method according to any one of claims 30 to 41 for the protection of a material and or a piece of equipment that will be exposed to an oxidising environment, or liquid metal and or a solid or molten salt.
  37. 43. Use according to claim 42, characterised in that the said material is a metal, a refractory or a carbonaceous material, or a mixture or a combination thereof.
  38. 44. Use according to claim 43, characterised in that the said metal is an iron nickel chromium based alloy. Use according to claim 42, characterised in that the said part is chosen from the group comprising metallic or refractory components of a casting unit, nozzles, liquid metal distributors in a sump, screens made of steel, stainless steel, a refractory material or ceramic, metallic filters, refractory filters, liquid metal injectors, gas bubble injectors, rotors, scrapers, pouring spouts, ultrasound sensors, measurement sensors designed to be immersed in liquid metal, bricks made of refractory material, parts made of carbonaceous materials and bricks made of graphite.
  39. 46. Substrate characterised in that at least part of the surface comprises at least one refractory layer obtained using a precursor 1 24 according to any one of claims 1 to 29 or using the method according to any one of claims 30 to 41.
  40. 47. Substrate according to claim 46, characterised in that it is made of metal, a refractory material or a carbonaceous material, or a mixture or a combination thereof.
  41. 48. Substrate according to claim 47, characterised in that the said metal is an iron nickel chromium based alloy.
  42. 49. Substrate according to claim 46, characterised in that it is chosen from among the group comprising metallic or refractory components of a casting unit, nozzles, liquid metal distributors in a sump, screens made of steel, stainless steel, a refractory material or ceramic, metallic filters, refractory filters, liquid metal injectors, gas bubble injectors, rotors, scrapers, pouring spouts, ultrasound sensors, measurement sensors designed to be immersed in liquid metal, bricks made of refractory material, parts made of carbonaceous materials and bricks made of graphite.
AU2002358833A 2001-10-15 2002-10-14 Coating precursor and method for coating a substrate with a refractory layer Ceased AU2002358833B9 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FR01/13267 2001-10-15
FR0113267A FR2830857B1 (en) 2001-10-15 2001-10-15 COATING PRECURSOR AND METHOD FOR COATING A SUBSTRATE WITH A REFRACTORY LAYER
PCT/FR2002/003485 WO2003033767A2 (en) 2001-10-15 2002-10-11 Coating precursor and method for coating a substrate with a refractory layer
AUPCT/FR2002/003485 2002-10-11
PCT/FR2002/003515 WO2003033435A2 (en) 2001-10-15 2002-10-14 Coating precursor and method for coating a substrate with a refractory layer

Publications (3)

Publication Number Publication Date
AU2002358833A1 AU2002358833A1 (en) 2003-07-03
AU2002358833B2 true AU2002358833B2 (en) 2007-10-25
AU2002358833B9 AU2002358833B9 (en) 2008-05-22

Family

ID=26213219

Family Applications (2)

Application Number Title Priority Date Filing Date
AU2002362826A Ceased AU2002362826B2 (en) 2001-10-15 2002-10-14 Coating precursor and method for coating a substrate with a refractory layer
AU2002358833A Ceased AU2002358833B9 (en) 2001-10-15 2002-10-14 Coating precursor and method for coating a substrate with a refractory layer

Family Applications Before (1)

Application Number Title Priority Date Filing Date
AU2002362826A Ceased AU2002362826B2 (en) 2001-10-15 2002-10-14 Coating precursor and method for coating a substrate with a refractory layer

Country Status (4)

Country Link
EP (2) EP1436240A2 (en)
AU (2) AU2002362826B2 (en)
CA (2) CA2464340A1 (en)
WO (2) WO2003033435A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115667423A (en) * 2020-04-22 2023-01-31 达涅利机械设备股份公司 Coating compositions for metal products and related methods

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2855774B1 (en) * 2003-06-05 2005-07-08 Pechiney Rhenalu METHOD FOR SEPARATING THE FALL LAYERS OF PLATED BANDS BY COLAMINING
DE102008044396A1 (en) * 2008-12-05 2010-06-10 Wacker Chemie Ag Highly hydrophobic coatings
FR2997616A1 (en) * 2012-11-06 2014-05-09 Seb Sa COOKING DEVICE HAVING A COOKING SURFACE HAVING NON-OXIDE OR AT LEAST PARTIALLY NON-OXIDE CERAMIC ANTI-ADHESIVE COATING, AND CULINARY ARTICLE OR HOME APPLIANCE COMPRISING SUCH A COOKING DEVICE
WO2021214802A1 (en) * 2020-04-22 2021-10-28 Danieli & C. Officine Meccaniche S.P.A. Coated metallic product

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0601317A2 (en) * 1992-12-04 1994-06-15 Nitto Denko Corporation Label substrate, ink, and label

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5536074B2 (en) * 1973-10-05 1980-09-18
US3928668A (en) * 1974-05-06 1975-12-23 Ferro Corp Electrostatic deposition of dry ceramic powders
US4292345A (en) * 1980-02-04 1981-09-29 Kolesnik Mikhail I Method of protecting carbon-containing component parts of metallurgical units from oxidation
US4496469A (en) * 1982-01-12 1985-01-29 Otsuka Kagaku Yakuhin Kabushiki Kaisha Heat-insulating refractory material consisting alkali titanate and silicon resin
DE3439007A1 (en) * 1984-10-25 1986-04-30 Bayer Ag, 5090 Leverkusen METHOD FOR ELECTROSTATIC SPRAYING INORGANIC POWDER
DE3638937A1 (en) * 1986-11-14 1988-05-26 Sigri Gmbh Cathode for a molten-salt electrolysis cell
DE3700702C1 (en) * 1987-01-13 1988-02-11 Bayer Ag Enamel powder coated with organopolysiloxanes for electrostatic powder application and process for their production
US5215801A (en) * 1990-08-22 1993-06-01 At&T Bell Laboratories Silicone resin electronic device encapsulant
JPH04300251A (en) * 1991-03-28 1992-10-23 Shin Etsu Chem Co Ltd Production of sintered material of titanium boride
DE4122764A1 (en) * 1991-07-10 1993-01-14 Bayer Ag Thermoplastic moulding materials contg. e.g. sinterable ceramic - can be shaped using thermoplastic processing techniques and sintered to yield ceramic or metal bodies
US5310476A (en) * 1992-04-01 1994-05-10 Moltech Invent S.A. Application of refractory protective coatings, particularly on the surface of electrolytic cell components
JPH06212115A (en) * 1992-05-29 1994-08-02 Ube Ind Ltd Heat-resistant coating material
US5399441A (en) * 1994-04-12 1995-03-21 Dow Corning Corporation Method of applying opaque coatings
FR2730227B1 (en) * 1995-02-03 1997-03-14 Pechiney Recherche COMPOSITION FOR COATING CARBON PRODUCTS AND COATING
US6210791B1 (en) * 1995-11-30 2001-04-03 General Electric Company Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation
US5776235A (en) * 1996-10-04 1998-07-07 Dow Corning Corporation Thick opaque ceramic coatings
DE19833063A1 (en) * 1998-07-22 2000-02-03 Reinz Dichtungs Gmbh Solvent-free, applicable, thermosetting coating material
JP2000119595A (en) * 1998-10-14 2000-04-25 Shin Etsu Chem Co Ltd Organopolysiloxane composition for forming fired coat
RU2149168C1 (en) * 1998-12-15 2000-05-20 Открытое акционерное общество "Северсталь" Insulating heat-resistant composite formulation
US6294261B1 (en) * 1999-10-01 2001-09-25 General Electric Company Method for smoothing the surface of a protective coating
US6413578B1 (en) * 2000-10-12 2002-07-02 General Electric Company Method for repairing a thermal barrier coating and repaired coating formed thereby

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0601317A2 (en) * 1992-12-04 1994-06-15 Nitto Denko Corporation Label substrate, ink, and label

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115667423A (en) * 2020-04-22 2023-01-31 达涅利机械设备股份公司 Coating compositions for metal products and related methods

Also Published As

Publication number Publication date
EP1436240A2 (en) 2004-07-14
WO2003033436A3 (en) 2003-09-25
WO2003033435A2 (en) 2003-04-24
AU2002358833B9 (en) 2008-05-22
CA2463568A1 (en) 2003-04-24
WO2003033435A3 (en) 2003-09-25
AU2002362826B2 (en) 2007-10-18
CA2464340A1 (en) 2003-04-24
WO2003033436A2 (en) 2003-04-24
EP1438271A2 (en) 2004-07-21

Similar Documents

Publication Publication Date Title
US7256232B2 (en) Coating precursor and method for coating a substrate with a refractory layer
EP0791029B1 (en) Protective compositions and methods of making same
US7951459B2 (en) Oxidation resistant coatings, processes for coating articles, and their coated articles
US8012252B2 (en) Durable hard coating containing silicon nitride
US6632762B1 (en) Oxidation resistant coating for carbon
US20220411912A1 (en) Oxidation resistant bond coat layers, processes for coating articles, and their coated articles
CN104136138B (en) The method repaired and/or protect surface in reactor
KR101276506B1 (en) Surface-treated ceramic member, method for producing same, and vacuum processing device
WO2007089666A2 (en) Aluminosilicate-based oxide composite coating and bond coat for silicon-based ceramic substrates
RU2293797C2 (en) Precursor of the coating and the method of deposition of the refractory layer on the substrate
AU2002358833B2 (en) Coating precursor and method for coating a substrate with a refractory layer
HRP950604A2 (en) ANTI-OXIDATIVE, ABRASION-RESISTANT PROTECTIVE COATING FOR SiC BODIES
DE19516790C2 (en) Process for minimizing corrosion of ceramic components
KR20110111754A (en) Process for silicon carbide coating on graphite
EP1156024A1 (en) Composite ceramic precursors and layers
JP2950612B2 (en) Method for producing zircon-based coating composition and zircon-based oxide-coated graphite molded article
JPS6048550B2 (en) Corrosion-resistant paint for high-temperature molten metals
JP2950598B2 (en) Method for producing zircon-based coating composition and zircon-based oxide-coated graphite molded article
RU2266880C1 (en) Method of passivation of contact surface of refractory reservoir made from mullite and slip used for realization of this method
EP0404410A1 (en) Method for producing a thin oxidation resistant SiC coating on carbonaceous substrates
CA1100366A (en) Coated silicon-based ceramic composites and method for making same
JP2950610B2 (en) Method for producing zircon-based coating composition and zircon-based oxide-coated graphite molded article
JPH0733302B2 (en) Zircon coating composition and method for producing zircon oxide-coated graphite compact
JPS63258683A (en) Preparation of film

Legal Events

Date Code Title Description
FGA Letters patent sealed or granted (standard patent)
SREP Specification republished
MK14 Patent ceased section 143(a) (annual fees not paid) or expired