US20160334049A1 - Multi-layer anti-corrosive coating - Google Patents
Multi-layer anti-corrosive coating Download PDFInfo
- Publication number
- US20160334049A1 US20160334049A1 US15/218,814 US201615218814A US2016334049A1 US 20160334049 A1 US20160334049 A1 US 20160334049A1 US 201615218814 A US201615218814 A US 201615218814A US 2016334049 A1 US2016334049 A1 US 2016334049A1
- Authority
- US
- United States
- Prior art keywords
- alloy
- coating layer
- approximately
- microns
- zinc
- 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.)
- Abandoned
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 49
- 239000011248 coating agent Substances 0.000 title claims abstract description 44
- 239000011247 coating layer Substances 0.000 claims abstract description 122
- 239000000463 material Substances 0.000 claims abstract description 80
- 229910052751 metal Inorganic materials 0.000 claims abstract description 57
- 239000002184 metal Substances 0.000 claims abstract description 57
- 239000000758 substrate Substances 0.000 claims abstract description 39
- 238000000034 method Methods 0.000 claims abstract description 31
- 239000000203 mixture Substances 0.000 claims abstract description 11
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 229910045601 alloy Inorganic materials 0.000 claims description 105
- 239000000956 alloy Substances 0.000 claims description 105
- 229910052733 gallium Inorganic materials 0.000 claims description 28
- -1 polyethylene Polymers 0.000 claims description 28
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 26
- 239000007921 spray Substances 0.000 claims description 23
- 229910052714 tellurium Inorganic materials 0.000 claims description 21
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 19
- 230000007797 corrosion Effects 0.000 claims description 19
- 238000005260 corrosion Methods 0.000 claims description 19
- 229910052725 zinc Inorganic materials 0.000 claims description 19
- 239000011701 zinc Substances 0.000 claims description 19
- 229920001343 polytetrafluoroethylene Polymers 0.000 claims description 16
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 14
- 229920001187 thermosetting polymer Polymers 0.000 claims description 14
- 239000002023 wood Substances 0.000 claims description 14
- 229910000831 Steel Inorganic materials 0.000 claims description 13
- 229910052782 aluminium Inorganic materials 0.000 claims description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 13
- 229910052742 iron Inorganic materials 0.000 claims description 13
- 239000010959 steel Substances 0.000 claims description 13
- 239000004698 Polyethylene Substances 0.000 claims description 10
- 239000004743 Polypropylene Substances 0.000 claims description 10
- 229920000573 polyethylene Polymers 0.000 claims description 10
- 229920001155 polypropylene Polymers 0.000 claims description 10
- 239000004593 Epoxy Substances 0.000 claims description 9
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 8
- 239000004677 Nylon Substances 0.000 claims description 8
- 239000002253 acid Substances 0.000 claims description 8
- 239000004567 concrete Substances 0.000 claims description 8
- 229920001577 copolymer Polymers 0.000 claims description 8
- STVZJERGLQHEKB-UHFFFAOYSA-N ethylene glycol dimethacrylate Chemical compound CC(=C)C(=O)OCCOC(=O)C(C)=C STVZJERGLQHEKB-UHFFFAOYSA-N 0.000 claims description 8
- 230000004927 fusion Effects 0.000 claims description 8
- 239000011777 magnesium Substances 0.000 claims description 8
- 229920001778 nylon Polymers 0.000 claims description 8
- 239000012815 thermoplastic material Substances 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 7
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 claims description 7
- 229910000611 Zinc aluminium Inorganic materials 0.000 claims description 7
- JHYLKGDXMUDNEO-UHFFFAOYSA-N [Mg].[In] Chemical compound [Mg].[In] JHYLKGDXMUDNEO-UHFFFAOYSA-N 0.000 claims description 7
- PGTXKIZLOWULDJ-UHFFFAOYSA-N [Mg].[Zn] Chemical compound [Mg].[Zn] PGTXKIZLOWULDJ-UHFFFAOYSA-N 0.000 claims description 7
- HXFVOUUOTHJFPX-UHFFFAOYSA-N alumane;zinc Chemical compound [AlH3].[Zn] HXFVOUUOTHJFPX-UHFFFAOYSA-N 0.000 claims description 7
- RNQKDQAVIXDKAG-UHFFFAOYSA-N aluminum gallium Chemical compound [Al].[Ga] RNQKDQAVIXDKAG-UHFFFAOYSA-N 0.000 claims description 7
- AJGDITRVXRPLBY-UHFFFAOYSA-N aluminum indium Chemical compound [Al].[In] AJGDITRVXRPLBY-UHFFFAOYSA-N 0.000 claims description 7
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 claims description 7
- 239000000919 ceramic Substances 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 239000011152 fibreglass Substances 0.000 claims description 7
- 229910052738 indium Inorganic materials 0.000 claims description 7
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 claims description 7
- NJWNEWQMQCGRDO-UHFFFAOYSA-N indium zinc Chemical compound [Zn].[In] NJWNEWQMQCGRDO-UHFFFAOYSA-N 0.000 claims description 7
- 229910052749 magnesium Inorganic materials 0.000 claims description 7
- 229910052759 nickel Inorganic materials 0.000 claims description 7
- 239000004033 plastic Substances 0.000 claims description 7
- 229920003023 plastic Polymers 0.000 claims description 7
- 239000000047 product Substances 0.000 claims description 7
- OFIYHXOOOISSDN-UHFFFAOYSA-N tellanylidenegallium Chemical compound [Te]=[Ga] OFIYHXOOOISSDN-UHFFFAOYSA-N 0.000 claims description 7
- ZTBJFXYWWZPTFM-UHFFFAOYSA-N tellanylidenemagnesium Chemical compound [Te]=[Mg] ZTBJFXYWWZPTFM-UHFFFAOYSA-N 0.000 claims description 7
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 claims description 7
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 6
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 6
- 229910000640 Fe alloy Inorganic materials 0.000 claims description 4
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 claims description 3
- 239000007769 metal material Substances 0.000 claims description 3
- 239000010410 layer Substances 0.000 description 6
- 238000004210 cathodic protection Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000005246 galvanizing Methods 0.000 description 2
- 238000010286 high velocity air fuel Methods 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000010405 anode material Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L58/00—Protection of pipes or pipe fittings against corrosion or incrustation
- F16L58/02—Protection of pipes or pipe fittings against corrosion or incrustation by means of internal or external coatings
- F16L58/04—Coatings characterised by the materials used
- F16L58/10—Coatings characterised by the materials used by rubber or plastics
- F16L58/1054—Coatings characterised by the materials used by rubber or plastics the coating being placed outside the pipe
- F16L58/1072—Coatings characterised by the materials used by rubber or plastics the coating being placed outside the pipe the coating being a sprayed layer
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING 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
- C09D5/00—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes
- C09D5/08—Anti-corrosive paints
-
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- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/02—Coating starting from inorganic powder by application of pressure only
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- 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
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- 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
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- C23F13/02—Inhibiting corrosion of metals by anodic or cathodic protection cathodic; Selection of conditions, parameters or procedures for cathodic protection, e.g. of electrical conditions
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- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
- Y10T428/24967—Absolute thicknesses specified
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- the invention relates generally to apparatus and methods relating to the application of coatings, and more particularly to a multilayer anti-corrosive coating for a metallic substrate such as an iron pipe.
- Iron-based pipes have been used in transporting water from different sources for many years. Over time, these pipes exhibit corrosion and, depending on their use, may require frequent replacement. Replacing iron-based pipes is costly for the material, the labor, and the down-time to the consumer.
- Cathodic protection is one technique used to control corrosion of a metal surface. This is done by making the surface to be protected the cathode of an electrochemical, or galvanic cell. This is most commonly done using alloys of zinc, magnesium and aluminum. These galvanic anodes are designed and selected to have a greater negative electrochemical potential than the metal they are protecting, which is typically steel. As the galvanic anode electrode corrodes, the anode material is consumed until it must be replaced.
- Galvanizing or more specifically hot-dip galvanizing is the process whereby steel is coated with a layer of metallic zinc.
- Galvanized coatings are extremely durable in most environments because of their barrier properties and cathodic protection. If, or when, the zinc coating is breached or scratched, exposing the steel surface, the zinc coating acts as an anode to form a galvanic cell, thereby protecting the steel from corrosion. This is also known as localized cathodic protection.
- Coatings to iron-based pipes have also been developed utilizing epoxy compositions that result in good corrosion resistance.
- thermoset polymers are widely used to protect steel pipes, concrete reinforcing bars (rebar), pipe connections, valves and the like from corrosion.
- the most commonly used thermoset polymer for this type of application is fusion bonded epoxy.
- Fusion bonded epoxy is typically applied to a steel pipe that is preheated to the application temperature where the fusion bonded epoxy transforms to a liquid.
- the liquid fusion bonded epoxy flows and solidifies on the pipe, pipe joint, and the like.
- Coating thickness of the fusion bonded epoxy is around 250 to 500 microns. However, the thickness of these coatings vary, are difficult to apply especially at the joints, and different coatings are required depending on the environmental exposure of the iron-based pipes.
- a multilayer coating that is corrosion resistant has a first coating layer on a substrate; a second coating layer deposited on the first coating layer; and a third coating layer deposited on the second coating layer; wherein the first coating layer is substantially a metal, the second coating layer is a mixture of the metal and a polymeric material, and the third coating layer is substantially the polymeric material.
- Embodiments are directed to a method of providing a multilayer coating that includes applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate; applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer; applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer; and at least one of: heating the substrate to approximately the fusing temperature of the metal when applying the first coating layer; and heating the substrate to approximately the fusing temperature of the polymeric material when applying the third coating layer.
- a first coating layer which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate
- a second coating layer which is a mixture of the metal and
- the substrate can include at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
- the metal may include at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
- the polymeric material can include at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material;
- Embodiments are directed to a multilayer corrosion resistant coating that includes a first coating layer, which is substantially a metal, deposited directly on and in contact with a substrate; a second coating layer, which is a mixture of the metal and a polymeric material, deposited directly on and in contact with the first coating layer; and a third coating layer, which is substantially the polymeric material, deposited directly on and in contact with the second coating layer.
- the substrate includes at least one of steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic;
- the metal includes at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium; and the polymeric material includes comprises at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
- a thickness of the first coating layer is approximately 25
- the metal can include at least 99% zinc.
- the metal can include aluminum and zinc having an aluminum-zinc ratio of about 85% aluminum to about 15% zinc.
- the substrate may be a metallic material, and the metal may be anodic to the substrate.
- thermoset material when the polymeric material includes thermoset material, can be a fusion bonded epoxy.
- the first coating layer may be approximately 50-100 microns
- the second coating layer may be approximately 5-100 microns
- the third coating layer may be approximately 50-150 microns.
- the first coating layer can be approximately 70-80 microns
- the second coating layer can be approximately 20-30 microns
- the third coating layer can be approximately 95-105 microns.
- Embodiments are directed to a method of providing a multilayer coating that includes applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate, wherein the first coating layer is applied at a fusing temperature of the metal; applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer, wherein the second coating layer is applied at a fusing temperature of the polymeric material; and applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer, wherein the third coating layer is applied at the fusing temperature of the polymeric material.
- a first coating layer which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate, wherein the
- the first coating layer, the second coating layer and the third coating layer can be applied sequentially using at least one of cold spray, thermal spray and plasma spray.
- the method can also include at least one of: heating the substrate to approximately a fusing temperature of the metal when applying the first coating layer; and heating the substrate to approximately a fusing temperature of the polymeric material when applying the third coating layer.
- the applying of the second coating layer can include: applying the polymeric material onto an outer surface of the first coating layer; and embedding the metal into the polymeric material on the outer surface of the first coating layer.
- the applying of the second coating layer may include at least one of: mixing the polymeric material and the metal together prior to being applied as the second coating layer; and mixing the polymeric material and metal together upon impact at an outer surface on which the second coating layer is applied.
- the substrate can include at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
- the metal can include at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
- the polymeric material may include at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
- the multilayer coating can form a corrosion resistant coating for the substrate.
- FIG. 1 is a cross section of a pipe with a multilayer coating.
- FIG. 1 shows a cross-sectional view of a substrate 10 having a multilayer corrosion resistant coating 12 .
- the substrate 10 may be any of iron, iron pipe, steel, copper, nickel, concrete, wood, wood products, fiberglass, ceramic, plastic, and any other metal or non-metal material that can be used as a substrate.
- the corrosion resistant coating 12 is made up of three distinct coating layers 20 , 30 , 40 .
- the first coating layer 20 is substantially a metal layer that is applied using cold spray or thermal spray techniques. It is understood that thermal spray includes the use of various techniques, including, but not limited to, combustion flame, combustion wire, high velocity oxygen fuel (HVOF), high velocity liquid fuel (HVLF), high velocity air-fuel (HVAF), and plasma.
- thermal spray includes the use of various techniques, including, but not limited to, combustion flame, combustion wire, high velocity oxygen fuel (HVOF), high velocity liquid fuel (HVLF), high velocity air-fuel (HVAF), and plasma.
- the metal 22 is typically at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy if indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium. Other metals may also be considered.
- the substrate 10 is iron pipe and the first coating layer 20 is a metal 22 that is anodic to the substrate 10 .
- the metal 22 is preferably one of 99% zinc and aluminum-zinc having a ratio of about 85% aluminum to about 15% zinc, and the thickness 24 of the first coating layer is approximately 25 microns to approximately 200 microns. In another embodiment the thickness 24 of the first coating layer is approximately 70-80 microns.
- the first coating layer 20 is applied utilizing thermal spray techniques, where the metal 22 is fed as a powder or a wire.
- the metal 22 is preferably applied at the fusing temperature of the anode, that is, for example, if the substrate 10 is an iron pipe and the metal 22 is zinc, the fusing temperature is approximately 850° F.
- the second coating layer 30 is a mixture of the metal 22 and a polymeric material 32 .
- the polymeric material 32 may be applied using thermal spray or cold spray techniques.
- the polymeric material 32 is at least one of polyethylene, polypropylene, polyester, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
- PTFE polytetrafluorethylene
- EMA ethylene methacrylate acid copolymer
- the thickness 34 of the second coating layer 30 is approximately 5 microns to approximately 200 microns. In another embodiment, the thickness 34 of the second coating layer 30 is approximately 20-30 microns.
- the second coating layer 30 is preferably applied utilizing thermal spray techniques, where the polymeric material 32 is powder fed through a hopper.
- the polymeric material 32 is preferably applied at the fusing temperature of the polymeric material 32 , that is, for example, at a temperature of approximately 450° F.
- the metal 22 and the polymeric material 32 are applied substantially simultaneously from two or more applicator guns, the mixing occurring at the deposition site.
- the third coating layer 40 is made up essentially of the polymeric material 32 .
- the polymeric material 32 may be applied using thermal spray or cold spray techniques.
- the polymeric material 32 is at least one of polyethylene, polypropylene, polyester, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
- PTFE polytetrafluorethylene
- EMA ethylene methacrylate acid copolymer
- the polymeric material 32 is at least one of polyethylene and polypropylene.
- the thickness 44 of the third coating layer 40 is approximately 5 microns to approximately 200 microns. In the preferred embodiment, the third thickness 44 of the third coating layer is approximately 95-105 microns.
- the third coating layer 40 is preferably applied utilizing thermal spray techniques, where the polymeric material 32 is powder fed through a hopper.
- the polymeric material 32 is preferably applied at the fusing temperature of the polymeric material 32 , that is, for example, at a temperature of approximately 450° F. This is similar to the application of the polymeric material as part of the second layer.
- the multi-layer coating 12 is applied to the substrate 10 by first applying the first coating layer 20 onto the substrate 10 . This is followed by applying the second coating layer 30 onto the first coating layer.
- the second coating layer 30 is applied by spraying a mixture of the metal 22 used in the first layer 20 with a polymeric material 32 .
- the second coating layer 30 can be applied to the first coating layer 20 utilizing a single spray gun or a multiple spray gun method.
- a two spray gun method the metal 22 is sprayed from a first spray gun towards the outer surface of the first coating layer 20 while the polymeric material 32 is sprayed from a second spray gun towards the outer surface of the first coating layer 20 .
- Mixing of the coating materials 22 , 32 takes place, for example, prior to the coating material reaching the outer surface of the first coating layer 20 by firing the spray guns substantially simultaneously, or upon impact at the outer surface of the first coating layer 20 .
- the polymeric coating material 32 is applied first to the outer layer of the first coating layer 20 , and the metal coating material 22 embeds into the polymeric material 32 forming the second coating layer 30 .
- the multiple spray guns release the coating materials 22 , 32 substantially simultaneously to form the second coating layer 30 .
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Abstract
Method of providing a multilayer coating. The method includes applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate; applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer; applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer; and at least one of: heating the substrate to approximately the fusing temperature of the metal when applying the first coating layer; and heating the substrate to approximately the fusing temperature of the polymeric material when applying the third coating layer.
Description
- This application is a Continuation of U.S. application Ser. No. 12/746,114, which is U.S. National Stage of International Application No. PCT/US08/85396 filed Dec. 3, 2008, which claims the benefit under 35 U.S.C. §119(e) of U.S. Provisional Application No. 60/992,143 filed Dec. 4, 2007, the disclosures of which are expressly incorporated by reference in their entireties.
- Not applicable.
- Not applicable.
- 1. Field of the Invention
- The invention relates generally to apparatus and methods relating to the application of coatings, and more particularly to a multilayer anti-corrosive coating for a metallic substrate such as an iron pipe.
- 2. Description of Related Art
- Iron-based pipes have been used in transporting water from different sources for many years. Over time, these pipes exhibit corrosion and, depending on their use, may require frequent replacement. Replacing iron-based pipes is costly for the material, the labor, and the down-time to the consumer.
- Cathodic protection is one technique used to control corrosion of a metal surface. This is done by making the surface to be protected the cathode of an electrochemical, or galvanic cell. This is most commonly done using alloys of zinc, magnesium and aluminum. These galvanic anodes are designed and selected to have a greater negative electrochemical potential than the metal they are protecting, which is typically steel. As the galvanic anode electrode corrodes, the anode material is consumed until it must be replaced.
- Galvanizing, or more specifically hot-dip galvanizing is the process whereby steel is coated with a layer of metallic zinc. Galvanized coatings are extremely durable in most environments because of their barrier properties and cathodic protection. If, or when, the zinc coating is breached or scratched, exposing the steel surface, the zinc coating acts as an anode to form a galvanic cell, thereby protecting the steel from corrosion. This is also known as localized cathodic protection.
- Coatings to iron-based pipes have also been developed utilizing epoxy compositions that result in good corrosion resistance. For example, thermoset polymers are widely used to protect steel pipes, concrete reinforcing bars (rebar), pipe connections, valves and the like from corrosion. The most commonly used thermoset polymer for this type of application is fusion bonded epoxy. Fusion bonded epoxy is typically applied to a steel pipe that is preheated to the application temperature where the fusion bonded epoxy transforms to a liquid. The liquid fusion bonded epoxy flows and solidifies on the pipe, pipe joint, and the like. Coating thickness of the fusion bonded epoxy is around 250 to 500 microns. However, the thickness of these coatings vary, are difficult to apply especially at the joints, and different coatings are required depending on the environmental exposure of the iron-based pipes.
- With fusion bonded epoxy, any breach in the coating will result in corrosion of the coated material.
- A multilayer coating that is corrosion resistant has a first coating layer on a substrate; a second coating layer deposited on the first coating layer; and a third coating layer deposited on the second coating layer; wherein the first coating layer is substantially a metal, the second coating layer is a mixture of the metal and a polymeric material, and the third coating layer is substantially the polymeric material.
- Embodiments are directed to a method of providing a multilayer coating that includes applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate; applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer; applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer; and at least one of: heating the substrate to approximately the fusing temperature of the metal when applying the first coating layer; and heating the substrate to approximately the fusing temperature of the polymeric material when applying the third coating layer.
- In embodiments, the substrate can include at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
- In accordance with embodiments, the metal may include at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
- According to other embodiments, the polymeric material can include at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material;
- Embodiments are directed to a multilayer corrosion resistant coating that includes a first coating layer, which is substantially a metal, deposited directly on and in contact with a substrate; a second coating layer, which is a mixture of the metal and a polymeric material, deposited directly on and in contact with the first coating layer; and a third coating layer, which is substantially the polymeric material, deposited directly on and in contact with the second coating layer. The substrate includes at least one of steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic; the metal includes at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium; and the polymeric material includes comprises at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material. A thickness of the first coating layer is approximately 25 microns to approximately 200 microns; a thickness of the second coating layer is approximately 5 microns to approximately 200 microns; and a thickness of the third coating layer is approximately 5 microns to approximately 200 microns.
- According to embodiments, the metal can include at least 99% zinc.
- In accordance with embodiments, the metal can include aluminum and zinc having an aluminum-zinc ratio of about 85% aluminum to about 15% zinc.
- In other embodiments the substrate may be a metallic material, and the metal may be anodic to the substrate.
- According to other embodiments, when the polymeric material includes thermoset material, the thermoset material can be a fusion bonded epoxy.
- In accordance with still other embodiments, the first coating layer may be approximately 50-100 microns, the second coating layer may be approximately 5-100 microns, and the third coating layer may be approximately 50-150 microns.
- In still other embodiments, the first coating layer can be approximately 70-80 microns, the second coating layer can be approximately 20-30 microns, and the third coating layer can be approximately 95-105 microns.
- Embodiments are directed to a method of providing a multilayer coating that includes applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate, wherein the first coating layer is applied at a fusing temperature of the metal; applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer, wherein the second coating layer is applied at a fusing temperature of the polymeric material; and applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer, wherein the third coating layer is applied at the fusing temperature of the polymeric material.
- According to embodiments, the first coating layer, the second coating layer and the third coating layer can be applied sequentially using at least one of cold spray, thermal spray and plasma spray.
- In accordance with other embodiments, the method can also include at least one of: heating the substrate to approximately a fusing temperature of the metal when applying the first coating layer; and heating the substrate to approximately a fusing temperature of the polymeric material when applying the third coating layer.
- In other embodiments, the applying of the second coating layer can include: applying the polymeric material onto an outer surface of the first coating layer; and embedding the metal into the polymeric material on the outer surface of the first coating layer.
- According to still other embodiments, the applying of the second coating layer may include at least one of: mixing the polymeric material and the metal together prior to being applied as the second coating layer; and mixing the polymeric material and metal together upon impact at an outer surface on which the second coating layer is applied.
- In accordance with still other embodiments, the substrate can include at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
- In other embodiments, the metal can include at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
- In still other embodiments, the polymeric material may include at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
- In accordance with still yet other embodiments of the present invention, the multilayer coating can form a corrosion resistant coating for the substrate.
- Other exemplary embodiments and advantages of the present invention may be ascertained by reviewing the present disclosure and the accompanying drawing.
- The present invention is further described in the detailed description which follows, in reference to the noted drawing by way of a non-limiting example of an exemplary embodiment of the present invention, and wherein:
-
FIG. 1 is a cross section of a pipe with a multilayer coating. - The particulars shown herein are by way of example and for purposes of illustrative discussion of the embodiments of the present invention only and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the present invention. In this regard, no attempt is made to show structural details of the present invention in more detail than is necessary for the fundamental understanding of the present invention, the description taken with the drawings making apparent to those skilled in the art how the several forms of the present invention may be embodied in practice.
-
FIG. 1 shows a cross-sectional view of asubstrate 10 having a multilayer corrosionresistant coating 12. Thesubstrate 10 may be any of iron, iron pipe, steel, copper, nickel, concrete, wood, wood products, fiberglass, ceramic, plastic, and any other metal or non-metal material that can be used as a substrate. The corrosionresistant coating 12 is made up of three distinct coating layers 20, 30, 40. - The
first coating layer 20 is substantially a metal layer that is applied using cold spray or thermal spray techniques. It is understood that thermal spray includes the use of various techniques, including, but not limited to, combustion flame, combustion wire, high velocity oxygen fuel (HVOF), high velocity liquid fuel (HVLF), high velocity air-fuel (HVAF), and plasma. - The
metal 22 is typically at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy if indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium. Other metals may also be considered. In one embodiment, thesubstrate 10 is iron pipe and thefirst coating layer 20 is ametal 22 that is anodic to thesubstrate 10. When this is the configuration, themetal 22 is preferably one of 99% zinc and aluminum-zinc having a ratio of about 85% aluminum to about 15% zinc, and thethickness 24 of the first coating layer is approximately 25 microns to approximately 200 microns. In another embodiment thethickness 24 of the first coating layer is approximately 70-80 microns. - In one embodiment the
first coating layer 20 is applied utilizing thermal spray techniques, where themetal 22 is fed as a powder or a wire. Themetal 22 is preferably applied at the fusing temperature of the anode, that is, for example, if thesubstrate 10 is an iron pipe and themetal 22 is zinc, the fusing temperature is approximately 850° F. - The
second coating layer 30 is a mixture of themetal 22 and apolymeric material 32. Thepolymeric material 32 may be applied using thermal spray or cold spray techniques. Thepolymeric material 32 is at least one of polyethylene, polypropylene, polyester, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material. In one embodiment thepolymeric material 32 is at least one of polyethylene and polypropylene. Thethickness 34 of thesecond coating layer 30 is approximately 5 microns to approximately 200 microns. In another embodiment, thethickness 34 of thesecond coating layer 30 is approximately 20-30 microns. - The
second coating layer 30 is preferably applied utilizing thermal spray techniques, where thepolymeric material 32 is powder fed through a hopper. Thepolymeric material 32 is preferably applied at the fusing temperature of thepolymeric material 32, that is, for example, at a temperature of approximately 450° F. - In one embodiment, the
metal 22 and thepolymeric material 32 are applied substantially simultaneously from two or more applicator guns, the mixing occurring at the deposition site. - The
third coating layer 40 is made up essentially of thepolymeric material 32. Thepolymeric material 32 may be applied using thermal spray or cold spray techniques. Thepolymeric material 32 is at least one of polyethylene, polypropylene, polyester, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material. In the preferred embodiment thepolymeric material 32 is at least one of polyethylene and polypropylene. Thethickness 44 of thethird coating layer 40 is approximately 5 microns to approximately 200 microns. In the preferred embodiment, thethird thickness 44 of the third coating layer is approximately 95-105 microns. - The
third coating layer 40 is preferably applied utilizing thermal spray techniques, where thepolymeric material 32 is powder fed through a hopper. Thepolymeric material 32 is preferably applied at the fusing temperature of thepolymeric material 32, that is, for example, at a temperature of approximately 450° F. This is similar to the application of the polymeric material as part of the second layer. - The
multi-layer coating 12 is applied to thesubstrate 10 by first applying thefirst coating layer 20 onto thesubstrate 10. This is followed by applying thesecond coating layer 30 onto the first coating layer. Thesecond coating layer 30 is applied by spraying a mixture of themetal 22 used in thefirst layer 20 with apolymeric material 32. - It should be noted that the
second coating layer 30 can be applied to thefirst coating layer 20 utilizing a single spray gun or a multiple spray gun method. When a two spray gun method is used, themetal 22 is sprayed from a first spray gun towards the outer surface of thefirst coating layer 20 while thepolymeric material 32 is sprayed from a second spray gun towards the outer surface of thefirst coating layer 20. Mixing of the 22, 32 takes place, for example, prior to the coating material reaching the outer surface of thecoating materials first coating layer 20 by firing the spray guns substantially simultaneously, or upon impact at the outer surface of thefirst coating layer 20. - In one embodiment, the
polymeric coating material 32 is applied first to the outer layer of thefirst coating layer 20, and themetal coating material 22 embeds into thepolymeric material 32 forming thesecond coating layer 30. - In another embodiment, the multiple spray guns release the
22, 32 substantially simultaneously to form thecoating materials second coating layer 30. - It is noted that the foregoing examples have been provided merely for the purpose of explanation and are in no way to be construed as limiting of the present invention. While the present invention has been described with reference to an exemplary embodiment, it is understood that the words which have been used herein are words of description and illustration, rather than words of limitation. Changes may be made, within the purview of the appended claims, as presently stated and as amended, without departing from the scope and spirit of the present invention in its aspects. Although the present invention has been described herein with reference to particular means, materials and embodiments, the present invention is not intended to be limited to the particulars disclosed herein; rather, the present invention extends to all functionally equivalent structures, methods and uses, such as are within the scope of the appended claims.
Claims (20)
1. A method of providing a multilayer coating comprising:
applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate;
applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer;
applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer; and
at least one of:
heating the substrate to approximately the fusing temperature of the metal when applying the first coating layer; and
heating the substrate to approximately the fusing temperature of the polymeric material when applying the third coating layer.
2. A method of providing a multilayer coating according to claim 1 , wherein the substrate comprises at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
3. A method of providing a multilayer coating according to claim 1 , wherein the metal comprises at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
4. A method of providing a multilayer coating according to claim 1 , wherein the polymeric material comprises at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material;
5. A multilayer corrosion resistant coating comprising:
a first coating layer, which is substantially a metal, deposited directly on and in contact with a substrate;
a second coating layer, which is a mixture of the metal and a polymeric material, deposited directly on and in contact with the first coating layer; and
a third coating layer, which is substantially the polymeric material, deposited directly on and in contact with the second coating layer;
wherein the substrate comprises at least one of steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic;
wherein the metal comprises at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium;
wherein the polymeric material comprises at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material;
wherein a thickness of the first coating layer is approximately 25 microns to approximately 200 microns;
wherein a thickness of the second coating layer is approximately 5 microns to approximately 200 microns; and
wherein a thickness of the third coating layer is approximately 5 microns to approximately 200 microns.
6. The multilayer corrosion resistant coating of claim 5 , wherein the metal comprises at least 99% zinc.
7. The multilayer corrosion resistant coating of claim 5 , wherein the metal comprises aluminum and zinc having an aluminum-zinc ratio of about 85% aluminum to about 15% zinc.
8. The multilayer corrosion resistant coating of claim 5 , wherein the substrate is a metallic material, and wherein the metal is anodic to the substrate.
9. The multilayer corrosion resistant coating of claim 5 , wherein, when the polymeric material comprises thermoset material, the thermoset material is a fusion bonded epoxy.
10. The multilayer corrosion resistant coating of claim 5 , wherein the first coating layer is approximately 50-100 microns, the second coating layer is approximately 5-100 microns, and the third coating layer is approximately 50-150 microns.
11. The multilayer corrosion resistant coating of claim 5 , wherein the first coating layer is approximately 70-80 microns, the second coating layer is approximately 20-30 microns, and the third coating layer is approximately 95-105 microns.
12. A method of providing a multilayer coating comprising:
applying a first coating layer, which is substantially a metal, having a thickness of approximately 25 microns to approximately 200 microns directly on and in contact with a substrate, wherein the first coating layer is applied at a fusing temperature of the metal;
applying a second coating layer, which is a mixture of the metal and a polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the first coating layer, wherein the second coating layer is applied at a fusing temperature of the polymeric material; and
applying a third coating layer, which is substantially the polymeric material, having a thickness of approximately 5 microns to approximately 200 microns directly on and in contact with the second coating layer, wherein the third coating layer is applied at the fusing temperature of the polymeric material.
13. The method of providing the multilayer coating of claim 12 , wherein the first coating layer, the second coating layer and the third coating layer are applied sequentially using at least one of cold spray, thermal spray and plasma spray.
14. The method of providing the multilayer coating of claim 12 , further comprising at least one of:
heating the substrate to approximately a fusing temperature of the metal when applying the first coating layer; and
heating the substrate to approximately a fusing temperature of the polymeric material when applying the third coating layer.
15. The method of providing the multilayer coating of claim 12 , wherein the applying of the second coating layer comprises:
applying the polymeric material onto an outer surface of the first coating layer; and
embedding the metal into the polymeric material on the outer surface of the first coating layer.
16. The method of providing the multilayer coating of claim 12 , wherein the applying of the second coating layer comprises at least one of:
mixing the polymeric material and the metal together prior to being applied as the second coating layer; and
mixing the polymeric material and metal together upon impact at an outer surface on which the second coating layer is applied.
17. The method of providing a multilayer coating according to claim 12 , wherein the substrate comprises at least one of iron, iron alloy, steel, copper, alloys of copper, nickel, alloys of nickel, concrete, wood, wood products, fiberglass, ceramic and plastic.
18. The method of providing a multilayer coating according to claim 12 , wherein the metal comprises at least one of zinc, aluminum, alloy of zinc-aluminum, magnesium, alloy of zinc-magnesium, alloy of aluminum-magnesium, indium, alloy of zinc-indium, alloy of aluminum-indium, alloy of magnesium-indium, gallium, alloy of zinc-gallium, alloy of aluminum-gallium, alloy of magnesium-gallium, alloy of indium-gallium, tellurium, alloy of zinc-tellurian, alloy of aluminum-tellurium, alloy of magnesium-tellurium, alloy of indium-tellurium, and alloy of gallium-tellurium.
19. The method of providing a multilayer coating according to claim 12 , wherein the polymeric material comprises at least one of polyethylene, polypropylene, nylon, polytetrafluorethylene (PTFE), ethylene methacrylate acid copolymer (EMAA), a thermoplastic material and a thermoset material.
20. The method of providing a multilayer coating according to claim 12 , wherein the multilayer coating forms a corrosion resistant coating for the substrate.
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| US15/218,814 US20160334049A1 (en) | 2007-12-04 | 2016-07-25 | Multi-layer anti-corrosive coating |
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| US99214307P | 2007-12-04 | 2007-12-04 | |
| PCT/US2008/085396 WO2009073716A1 (en) | 2007-12-04 | 2008-12-03 | Multi-layer anti-corrosive coating |
| US74611410A | 2010-09-14 | 2010-09-14 | |
| US15/218,814 US20160334049A1 (en) | 2007-12-04 | 2016-07-25 | Multi-layer anti-corrosive coating |
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| PCT/US2008/085396 Continuation WO2009073716A1 (en) | 2007-12-04 | 2008-12-03 | Multi-layer anti-corrosive coating |
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| US12/315,529 Active 2029-03-19 US8293378B2 (en) | 2007-12-04 | 2008-12-04 | Anti-corrosive coating for metal surfaces |
| US15/218,814 Abandoned US20160334049A1 (en) | 2007-12-04 | 2016-07-25 | Multi-layer anti-corrosive coating |
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| US12/315,529 Active 2029-03-19 US8293378B2 (en) | 2007-12-04 | 2008-12-04 | Anti-corrosive coating for metal surfaces |
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| EP (1) | EP2229241B1 (en) |
| CA (1) | CA2702638C (en) |
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| WO (2) | WO2009073716A1 (en) |
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- 2008-12-03 EP EP08858275.4A patent/EP2229241B1/en not_active Not-in-force
- 2008-12-03 WO PCT/US2008/085396 patent/WO2009073716A1/en not_active Ceased
- 2008-12-04 MX MX2010006082A patent/MX2010006082A/en active IP Right Grant
- 2008-12-04 US US12/315,529 patent/US8293378B2/en active Active
- 2008-12-04 CA CA2702638A patent/CA2702638C/en active Active
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| US11898986B2 (en) | 2012-10-10 | 2024-02-13 | Westinghouse Electric Company Llc | Systems and methods for steam generator tube analysis for detection of tube degradation |
| US11935662B2 (en) | 2019-07-02 | 2024-03-19 | Westinghouse Electric Company Llc | Elongate SiC fuel elements |
| US11662300B2 (en) | 2019-09-19 | 2023-05-30 | Westinghouse Electric Company Llc | Apparatus for performing in-situ adhesion test of cold spray deposits and method of employing |
| WO2023000024A1 (en) * | 2021-07-19 | 2023-01-26 | Fortescue Future Industries Pty Ltd | Cryogenic liquid transfer using pipe-in-pipe system |
| WO2023000026A1 (en) * | 2021-07-19 | 2023-01-26 | Fortescue Future Industries Pty Ltd | Cryogenic hydrogen pipe-in-pipe system with microporous insulation |
| WO2023000027A1 (en) * | 2021-07-19 | 2023-01-26 | Fortescue Future Industries Pty Ltd | Apparatus and method for transfer of cryogenic fluids – dual use vapour return and liquid circulation line |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2229241B1 (en) | 2019-06-05 |
| CA2702638A1 (en) | 2009-06-11 |
| MX2010006082A (en) | 2010-06-23 |
| EP2229241A4 (en) | 2011-08-03 |
| EP2229241A1 (en) | 2010-09-22 |
| WO2009073196A1 (en) | 2009-06-11 |
| US20110003165A1 (en) | 2011-01-06 |
| WO2009073716A1 (en) | 2009-06-11 |
| US8293378B2 (en) | 2012-10-23 |
| CA2702638C (en) | 2014-09-02 |
| US20090252986A1 (en) | 2009-10-08 |
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