US20180371601A1 - KINETICALLY APPLIED GRADATED Zr-Al-C OR Ti-Al-C CERAMIC OR AMORPHOUS OR SEMI-AMORPHOUS STAINLESS STEEL WITH NUCLEAR GRADE ZIRCONIUM ALLOY METAL STRUCTURE - Google Patents
KINETICALLY APPLIED GRADATED Zr-Al-C OR Ti-Al-C CERAMIC OR AMORPHOUS OR SEMI-AMORPHOUS STAINLESS STEEL WITH NUCLEAR GRADE ZIRCONIUM ALLOY METAL STRUCTURE Download PDFInfo
- Publication number
- US20180371601A1 US20180371601A1 US16/008,439 US201816008439A US2018371601A1 US 20180371601 A1 US20180371601 A1 US 20180371601A1 US 201816008439 A US201816008439 A US 201816008439A US 2018371601 A1 US2018371601 A1 US 2018371601A1
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- United States
- Prior art keywords
- coating
- component
- ceramic
- cladding
- zirconium
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- 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
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- 229910001093 Zr alloy Inorganic materials 0.000 title claims abstract description 68
- 239000000919 ceramic Substances 0.000 title claims abstract description 37
- 239000010935 stainless steel Substances 0.000 title claims abstract description 8
- 229910001220 stainless steel Inorganic materials 0.000 title claims abstract description 8
- 229910052751 metal Inorganic materials 0.000 title description 6
- 239000002184 metal Substances 0.000 title description 6
- 238000000576 coating method Methods 0.000 claims abstract description 88
- 239000011248 coating agent Substances 0.000 claims abstract description 86
- 238000005253 cladding Methods 0.000 claims abstract description 80
- 239000008199 coating composition Substances 0.000 claims abstract description 58
- 238000000151 deposition Methods 0.000 claims abstract description 32
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910001928 zirconium oxide Inorganic materials 0.000 claims abstract description 23
- 239000000203 mixture Substances 0.000 claims abstract description 20
- 230000007423 decrease Effects 0.000 claims abstract description 15
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 13
- 229910009818 Ti3AlC2 Inorganic materials 0.000 claims abstract description 12
- WEAMLHXSIBDPGN-UHFFFAOYSA-N (4-hydroxy-3-methylphenyl) thiocyanate Chemical compound CC1=CC(SC#N)=CC=C1O WEAMLHXSIBDPGN-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910021355 zirconium silicide Inorganic materials 0.000 claims abstract description 7
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052593 corundum Inorganic materials 0.000 claims abstract description 6
- 229910001845 yogo sapphire Inorganic materials 0.000 claims abstract description 6
- 230000008021 deposition Effects 0.000 claims description 9
- 238000000034 method Methods 0.000 abstract description 20
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 14
- 239000010410 layer Substances 0.000 description 29
- 230000003647 oxidation Effects 0.000 description 27
- 238000007254 oxidation reaction Methods 0.000 description 27
- 239000000758 substrate Substances 0.000 description 15
- 239000011247 coating layer Substances 0.000 description 14
- 229940043774 zirconium oxide Drugs 0.000 description 13
- 239000000463 material Substances 0.000 description 7
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 239000003758 nuclear fuel Substances 0.000 description 4
- 230000005855 radiation Effects 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- 230000010354 integration Effects 0.000 description 3
- 230000001464 adherent effect Effects 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000009835 boiling Methods 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000002826 coolant Substances 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 230000008961 swelling Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000011236 particulate material Substances 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 238000009718 spray deposition Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
- 150000003755 zirconium compounds Chemical class 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
- C23C4/11—Oxides
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/48—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/62222—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining ceramic coatings
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C24/00—Coating starting from inorganic powder
- C23C24/02—Coating starting from inorganic powder by application of pressure only
- C23C24/04—Impact or kinetic deposition of particles
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
- C23C28/042—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/04—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
- C23C28/048—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material with layers graded in composition or physical properties
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/322—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/324—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal matrix material layer comprising a mixture of at least two metals or metal phases or a metal-matrix material with hard embedded particles, e.g. WC-Me
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/341—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one carbide layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
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- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21C—NUCLEAR REACTORS
- G21C3/00—Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
- G21C3/02—Fuel elements
- G21C3/04—Constructional details
- G21C3/06—Casings; Jackets
- G21C3/07—Casings; Jackets characterised by their material, e.g. alloys
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
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- Y02E30/40—
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Definitions
- This invention relates to coating compositions and methods of coating zirconium alloy nuclear fuel cladding to reduce oxidation corrosion of the cladding which is exposed to light water nuclear reactor under normal or accident conditions.
- the exposure of zirconium alloy cladding to the high temperature and pressure water environment in a nuclear reactor can result in corrosion (oxidation) of the cladding surface, and may ultimately lead to metal embrittlement. This weakening of the metal may adversely affect the performance, life-time, and safety margin of the nuclear fuel core.
- the inclusion of an oxidation resistant coating on the zirconium alloy cladding surface can in theory protect the zirconium alloy substrate from the reactor environment.
- problems associated with this solution For example, achieving strong adherence of the coating to the zirconium alloy substrate is problematic due to a fine oxidation layer that inherently exists on top of the zirconium alloy cladding surface.
- FIG. 1 shows a coated zirconium alloy cladding 10 in accordance with the prior art.
- the zirconium alloy cladding 10 has an oxidation layer 12 resulting from the immediate oxidation of the substrate 10 , and a further oxidation portion 14 added as the zirconium is exposed to air, water or other oxidizing media.
- a coating layer 16 is applied to the oxidation portion 14 .
- the zirconium alloy cladding 10 is simply coated with the coating layer 16 . Since the coating layer 16 is merely deposited on top of the oxidation layer 14 , this process often results in the coating, peeling or spalling of the coating layer 16 when exposed to reactor conditions.
- thermal and radiation induced stresses are typically introduced in any coating during operation that can cause the coating layer 16 to peel off the zirconium alloy cladding 10 .
- the zirconium alloy material of which the cladding is constructed is composed of zirconium (Zr) with up to about 2 wt. % of other metals, such as niobium (Nb), tin (Sn), iron (Fe), chromium (Cr) and mixtures thereof.
- Zr zirconium
- Such zirconium alloy cladding tubes are taught, for example, by Biancheria et al., Kapil, and Lahoda (see U.S. Pat. Nos. 3,427,222; 5,075,075; and 7,139,360 respectively).
- These fuel rods/cladding have an end cap at each end and a hold device such as a metal spring to keep the enclosed stack of nuclear fuel pellets in place.
- Mazzoccoli et al. discloses a method of coating zirconium alloy cladding tubes with an adherent mass of oxidation resistant material, using high velocity thermal application for a Zr—Al—C ceramic or Ti—Al—C ceramic or an iron based alloy, Nanosteel or Zr—Al alloy.
- a Zr—Al—C ceramic or Ti—Al—C ceramic or an iron based alloy, Nanosteel or Zr—Al alloy There are disadvantages associated with this method, such as the inability of the coating to adhere to the base Zr alloy during thermal cycles.
- the above needs are met and objects accomplished by a method of depositing a coating composition onto an exterior surface of a zirconium alloy cladding of a light water nuclear reactor to form a coating which at least partially adheres to said exterior surface.
- the method includes providing the zirconium alloy cladding which inherently has a zirconium oxide-containing layer at least partially formed on the exterior surface with an adherent coating of a graded composition.
- the graded coating composition includes a first component and a second component.
- the first component is selected from the group consisting of zirconium, zirconium oxide and mixtures thereof.
- the second component is selected from the group consisting of Zr 2 AlC ceramic, Ti 2 AlC ceramic, Ti 3 AlC 2 ceramic, Al 2 O 3 , aluminum, zirconium silicide, amorphous and semi-amorphous alloyed stainless steel, and mixtures of Zr 2 AlC ceramic, Ti 2 AlC ceramic and Ti 3 AlC 2 ceramic.
- the method further includes kinetically depositing the coating composition onto the exterior surface of the cladding to form the coating.
- the coating has a gradient emanating from the surface of the cladding toward an exposed outer surface of the coating such that percent by weight of the first component decreases from the exterior surface of the cladding toward the exposed outer surface of the coating and percent by weight of the second component increases from the exterior surface of the cladding to the exposed outer surface of the coating, based on total weight of the coating composition.
- the kinetic deposition of the coating composition can be conducted by employing a technique wherein a propellant is heated.
- the kinetic deposition technique may be effective to at least partially penetrate the zirconium oxide-containing layer formed on the exterior surface of the cladding.
- the coating may be applied by one or more passes of the kinetic deposition technique.
- a first pass may include depositing the coating composition to form a first layer which includes from about 75% to about 100% by weight of the first component and from about 0% to about 25% by weight of the second component based on total weight of the coating composition.
- a final pass may include depositing the coating composition to form the exposed outer surface which comprises from about 75% to about 100% by weight of the second component and from about 0% to about 25% by weight of the first component based on total weight of the coating composition.
- a portion of the coating composition kinetically deposited adjacent to or near the exterior surface of the cladding mixes with the zirconium oxide-containing layer to form an integrated layer.
- the zirconium alloy cladding is positioned in a light water nuclear reactor selected from the group consisting of a pressurized water reactor and a boiling water reactor.
- the invention provides a coating composition for kinetic deposition on an exterior surface of a zirconium alloy cladding of a light water nuclear reactor to form a coating which at least partially adheres to said exterior surface.
- the zirconium alloy cladding inherently has a zirconium oxide-containing layer at least partially formed on said exterior surface.
- the coating composition includes a first component and a second component.
- the first component is selected from the group consisting of zirconium, zirconium oxide, and mixtures thereof.
- the second component is selected from the group consisting of Zr 2 AlC ceramic, Ti 2 AlC ceramic, Ti 3 AlC 2 ceramic, Al 2 O 3 , aluminum, zirconium silicide, amorphous or semi-amorphous alloyed stainless steel, and mixtures of Zr 2 AlC ceramic, Ti 2 AlC ceramic and Ti 3 AlC 2 ceramic.
- the coating formed by the coating composition has a gradient emanating from the exterior surface of the cladding, which serves as the coating substrate, towards an exposed outer surface of the coating such that percent by weight of the first component decreases from the exterior surface of the cladding toward the exposed outer surface of the coating and percent by weight of the second component increases from the exterior surface of the cladding to the exposed outer surface of the coating, based on total weight percent of the coating composition.
- FIG. 1 is a cross-section view of a coated zirconium alloy substrate in accordance with the prior art
- FIG. 2 is a cross-section view of a coated zirconium alloy substrate in accordance with certain embodiments of the invention.
- FIG. 3 is a block diagram of a method of applying a coating material employing a kinetic deposition technique in accordance with certain embodiments of the invention.
- the invention provides a coating composition which includes a zirconium compound and a compound which protects the cladding surface from bulk oxidation.
- the coating composition is deposited on an exterior surface of a zirconium alloy cladding, e.g., tube.
- the deposition can be performed using various conventional techniques, such as a kinetic deposition technique (referred to as “cold spray”).
- the zirconium alloy cladding tube typically has a zirconium-oxide layer inherently formed on at least a portion of its exterior surface. Deposition of the coating composition results in a coating being formed on at least a portion of the exterior surface of the zirconium alloy cladding tube.
- the zirconium alloy cladding is positioned in the core of a light water nuclear reactor, such as a pressurized water reactor (PWR) or a boiling water reactor (BWR).
- a light water nuclear reactor such as a pressurized water reactor (PWR) or a boiling water reactor (BWR).
- PWR pressurized water reactor
- BWR boiling water reactor
- the coating composition of the invention includes a first component and a second component.
- the first component includes zirconium, zirconium oxide or mixtures thereof.
- the second component includes Zr 2 AlC ceramic, Ti 2 AlC ceramic, Ti 3 AlC 2 ceramic, Al 2 O 3 , aluminum, zirconium silicide (ZrSi 2 ), amorphous or semi-amorphous alloyed stainless steel, or mixtures of Zr 2 AlC, Ti 2 AlC and Ti 3 AlC 2 .
- the coating composition is actually deposited on and adhered to this zirconium oxide-containing layer.
- Deposition of the coating composition of the invention results in a gradient coating or matrix that emanates from the exterior surface of the zirconium alloy cladding to an outer exposed surface of the coating.
- This gradient coating is effective to eliminate bulk oxidation of the zirconium alloy cladding upon exposure to PWR or BWR conditions, e.g., coolant that circulates in the reactor core.
- the gradient of the coating is such that the amount or weight percent (based on total weight of the coating composition) of each of the first and second components increases or decreases as the coating thickness emanates from the surface of the coating which is adjacent to or near the zirconium alloy cladding surface toward the exposed outer surface of the coating.
- the amount of the first component decreases as the coating thickness emanates from the surface adjacent to or near the zirconium alloy cladding surface toward the exposed outer coating surface
- the amount of the second component increases as the coating thickness emanates from the surface adjacent to or near the zirconium alloy cladding surface toward the exposed outer coating surface.
- the decrease in the amount of the first component may correspond to the increase in the amount of the second component.
- the weight percent of the first component decreases from about 75% by weight at the surface of the coating adjacent to or near the cladding surface to about 10% by weight at the exposed outer surface
- the weight percent of the second component correspondingly increases from about 25% by weight at the surface of the coating adjacent to or near the cladding surface to about 90% by weight at the exposed outer surface of the coating.
- the weight percent of each of the first and second components may decrease and increase, respectively, such that the first component is present on the exposed outer surface of the coating in an amount of about 0% by weight and the second component is present on the exposed outer surface of the coating in an amount of about 100% by weight.
- the coating composition may be deposited onto the exterior surface of the zirconium alloy cladding to form the gradient coating by employing various coating techniques known in the art.
- the coating composition is deposited using a conventional kinetic deposition technique which generally includes directing particulate material by a gas stream toward a substrate.
- the coating composition is propelled by a propulsive gas stream toward the zirconium alloy cladding.
- the first and second components of the coating composition may each be propelled separately or they may be propelled together, e.g., in a blend or mixture.
- the coating composition may be propelled at room temperature or may be pre-heated to an elevated temperature, e.g., at or above the melting temperature of the first and second components.
- this method of kinetic deposition is capable of at least partially disrupting the zirconium-oxide layer which is inherently formed on the zirconium alloy cladding such that the resulting coating is firmly bonded, e.g., atom-to-atom, to the cladding surface.
- the gradient coating may be formed in several passes or in a single pass.
- the first pass includes an excess amount of the first component. That is, the first component is present in greater than about 50% by weight based on total weight of the coating composition. In other embodiments, the first component in the first pass may be present in about 75% by weight or greater based on total weight of the coating composition. The remainder of the coating composition being composed of the second component.
- the first pass includes about 100% by weight of the first component and about 0% by weight of the second component based on total weight of the coating composition. In each subsequent pass, the amount of the first component decreases and the amount of the second component increases. In certain embodiments, the amount by which the first component decreases is equal to the amount by which the second component increases.
- a single pass technique is employed.
- the amount (e.g., percent by weight) of each of the first and second components in the coating composition is continually varied to produce the gradient coating.
- the kinetic deposition methodology of the invention produces an integrated gradient coating that is richer in the first component, e.g., the zirconium or zirconium oxide, in the portion of the coating that is closer to the substrate, e.g., zirconium alloy cladding, and richer in the second component, e.g., the oxidation resistant material, in the portion of the coating that is nearer the exposed surface of the coating.
- the first component is present in excess (e.g., as compared to the second component) near the zirconium alloy cladding surface and the presence of the first component decreases throughout the coating thickness such that the exposed surface of the coating has an excess of the second component.
- the increased presence of the first component adjacent to or near the cladding tube surface enhances incorporation of the gradient coating onto and into the surface, as the coating composition is chemically similar to the zirconium alloy cladding composition and, gradually changes the thermal expansion and radiation swelling characteristics to minimize thermal and radiation stresses during operation.
- the gradient coating of the invention is created by kinetically depositing a first layer of the coating composition which includes from about 50% to about 100% or from greater than about 50% to about 100% or from about 75% to about 95% by weight of the first component, and from about 0% to about 50% or from about 0% to less than about 50% or from about 5% to about 25% by weight of the second component, based on total weight of the coating composition.
- the first component is zirconium alloy.
- additional layers of the coating composition may be deposited on the first layer. In certain embodiments, in each of the additional layers, the amount of the first component will successively decrease and the amount of the second component will successively increase.
- the exposed outer surface of the coating is composed of an excess of the second component such that it retains the oxidation resistant behavior of the second component while a base is present (e.g., underlying layers) that is rich in zirconium, i.e., the first component.
- a base e.g., underlying layers
- the method of the invention is generally directed to depositing an oxidation resistant material into a zirconium oxide layer, such that the oxidation resistant material ultimately penetrates into the zirconium substrate resulting in strong adhesion, and the oxidation resistant material deposited on the exposed outer coating surface provides a dense oxidation resistant surface that protects the underlying substrate from the nuclear reactor environment.
- FIG. 2 shows an integrated gradient coating deposited on a zirconium alloy substrate 10 in accordance with certain embodiments of the invention.
- a coating layer 20 containing zirconium alloy e.g., the first component is applied to the zirconium alloy substrate 10 .
- the zirconium alloy substrate 10 includes an oxidation layer 12 thereon.
- the coating layer 20 is adjacent to the oxidation layer 12 .
- Within the coating layer 20 is an integration layer 22 . Without intending to be bound by any particular theory, it is believed that a portion of the coating layer 20 mixes together or integrates with a portion of the oxidation layer 12 , to form the integration layer 22 adjacent to the oxidation layer 12 , which may penetrate within the zirconium alloy substrate 10 .
- the zirconium (e.g., the first component) content of the coating layer 20 increases toward the zirconium alloy substrate 10 as shown by arrow 24 and the non-zirconium species (e.g., the second component) content increases toward the outside surface 26 as shown by arrow 28 .
- the gradient coating layer 20 is deposited and the integration layer 22 formed as a result of several passes of the kinetic deposition technique described herein. Each successive deposition increases in the non-zirconium alloy species, e.g., the second component, and decreases in zirconium alloy, e.g., the first component, content. In certain embodiments, a single pass deposition technique may be employed where the coating composition itself is altered in a continuous manner such that multiple passes are not required.
- the thickness of the coating layer 20 may vary and in certain embodiments is less than or equal to about 100 micrometers thick, or more preferably from about 5 to about 100 micrometers thick, or from about 5 to about 50 micrometers thick.
- the gradient coating of the invention provides numerous benefits over known corrosion resistant coatings.
- known coatings may be applied on top of, e.g., overlay, the oxidation layer resulting in poor adhesion and failure.
- the gradient coating provides oxidation resistant material directly into the oxidation layer which ultimately penetrates into the zirconium alloy cladding resulting in strong adhesion and a dense oxidation resistant surface that protects the underlying cladding from the reactor environment.
- FIG. 3 shows a method of depositing a coating composition, e.g., the first and second components, in accordance with certain embodiments of this invention.
- a zirconium alloy tube 30 is supplied.
- a coating composition 32 is supplied to a Kinetic Cold Spray or Thermal Spray Deposition Process (KCS/TSDP) 34 .
- KCS/TSDP Kinetic Cold Spray or Thermal Spray Deposition Process
- the KCS/TSDP provides or deposits the coating composition 32 to form a gradient coating 36 .
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Abstract
Description
- This is a divisional application and claims priority to U.S. patent application Ser. No. 14/205,799, filed Mar. 12, 2014, and to U.S. Provisional Patent Application Ser. No. 61/827,792 filed May 28, 2013, entitled “A Kinetically Applied Gradated Ti—Al—C Ceramic or Amorphous or Semi-Amorphous Stainless Steel With Nuclear Grade Zirconium Alloy Metal Structure”, and incorporated herein by reference.
- This invention relates to coating compositions and methods of coating zirconium alloy nuclear fuel cladding to reduce oxidation corrosion of the cladding which is exposed to light water nuclear reactor under normal or accident conditions.
- The exposure of zirconium alloy cladding to the high temperature and pressure water environment in a nuclear reactor can result in corrosion (oxidation) of the cladding surface, and may ultimately lead to metal embrittlement. This weakening of the metal may adversely affect the performance, life-time, and safety margin of the nuclear fuel core. The inclusion of an oxidation resistant coating on the zirconium alloy cladding surface can in theory protect the zirconium alloy substrate from the reactor environment. However, there are problems associated with this solution. For example, achieving strong adherence of the coating to the zirconium alloy substrate is problematic due to a fine oxidation layer that inherently exists on top of the zirconium alloy cladding surface.
FIG. 1 shows a coated zirconium alloy cladding 10 in accordance with the prior art. As shown inFIG. 1 , the zirconium alloy cladding 10 has anoxidation layer 12 resulting from the immediate oxidation of thesubstrate 10, and afurther oxidation portion 14 added as the zirconium is exposed to air, water or other oxidizing media. Acoating layer 16 is applied to theoxidation portion 14. Thus, there are four distinct, separate layers that exist when the zirconium alloy cladding 10 is simply coated with thecoating layer 16. Since thecoating layer 16 is merely deposited on top of theoxidation layer 14, this process often results in the coating, peeling or spalling of thecoating layer 16 when exposed to reactor conditions. In addition, thermal and radiation induced stresses are typically introduced in any coating during operation that can cause thecoating layer 16 to peel off the zirconium alloy cladding 10. - The zirconium alloy material of which the cladding is constructed is composed of zirconium (Zr) with up to about 2 wt. % of other metals, such as niobium (Nb), tin (Sn), iron (Fe), chromium (Cr) and mixtures thereof. Such zirconium alloy cladding tubes are taught, for example, by Biancheria et al., Kapil, and Lahoda (see U.S. Pat. Nos. 3,427,222; 5,075,075; and 7,139,360 respectively). These fuel rods/cladding have an end cap at each end and a hold device such as a metal spring to keep the enclosed stack of nuclear fuel pellets in place.
- Various methods of coating nuclear fuel cladding tubes are known in the art. For example, such methods are taught by Knight et al., Bryan et al., Van Swam, and Lahoda et al. (see U.S. Pat. Nos. 6,231,969; 5,171,520; 6,005,906 and 7,815,964; respectively).
- Further, Mazzoccoli et al. (see U.S. patent application Ser. No. 13/670,808 filed on Nov. 7, 2012) discloses a method of coating zirconium alloy cladding tubes with an adherent mass of oxidation resistant material, using high velocity thermal application for a Zr—Al—C ceramic or Ti—Al—C ceramic or an iron based alloy, Nanosteel or Zr—Al alloy. There are disadvantages associated with this method, such as the inability of the coating to adhere to the base Zr alloy during thermal cycles.
- Thus, there is a need in the art to develop a coating composition and method of depositing the composition to form a protective coating on a zirconium alloy cladding such that the coating sufficiently adheres to the cladding surface and is effective to reduce or prevent oxidation of the surface of the cladding due to its exposure to nuclear reactor coolant water.
- In one aspect, the above needs are met and objects accomplished by a method of depositing a coating composition onto an exterior surface of a zirconium alloy cladding of a light water nuclear reactor to form a coating which at least partially adheres to said exterior surface. The method includes providing the zirconium alloy cladding which inherently has a zirconium oxide-containing layer at least partially formed on the exterior surface with an adherent coating of a graded composition. The graded coating composition includes a first component and a second component. The first component is selected from the group consisting of zirconium, zirconium oxide and mixtures thereof. The second component is selected from the group consisting of Zr2AlC ceramic, Ti2AlC ceramic, Ti3AlC2 ceramic, Al2O3, aluminum, zirconium silicide, amorphous and semi-amorphous alloyed stainless steel, and mixtures of Zr2AlC ceramic, Ti2AlC ceramic and Ti3AlC2 ceramic. The method further includes kinetically depositing the coating composition onto the exterior surface of the cladding to form the coating. The coating has a gradient emanating from the surface of the cladding toward an exposed outer surface of the coating such that percent by weight of the first component decreases from the exterior surface of the cladding toward the exposed outer surface of the coating and percent by weight of the second component increases from the exterior surface of the cladding to the exposed outer surface of the coating, based on total weight of the coating composition.
- The kinetic deposition of the coating composition can be conducted by employing a technique wherein a propellant is heated. The kinetic deposition technique may be effective to at least partially penetrate the zirconium oxide-containing layer formed on the exterior surface of the cladding. The coating may be applied by one or more passes of the kinetic deposition technique. A first pass may include depositing the coating composition to form a first layer which includes from about 75% to about 100% by weight of the first component and from about 0% to about 25% by weight of the second component based on total weight of the coating composition. A final pass may include depositing the coating composition to form the exposed outer surface which comprises from about 75% to about 100% by weight of the second component and from about 0% to about 25% by weight of the first component based on total weight of the coating composition.
- In certain embodiments, a portion of the coating composition kinetically deposited adjacent to or near the exterior surface of the cladding mixes with the zirconium oxide-containing layer to form an integrated layer.
- In certain embodiments, the zirconium alloy cladding is positioned in a light water nuclear reactor selected from the group consisting of a pressurized water reactor and a boiling water reactor.
- In another aspect, the invention provides a coating composition for kinetic deposition on an exterior surface of a zirconium alloy cladding of a light water nuclear reactor to form a coating which at least partially adheres to said exterior surface. The zirconium alloy cladding inherently has a zirconium oxide-containing layer at least partially formed on said exterior surface. The coating composition includes a first component and a second component. The first component is selected from the group consisting of zirconium, zirconium oxide, and mixtures thereof. The second component is selected from the group consisting of Zr2AlC ceramic, Ti2AlC ceramic, Ti3AlC2 ceramic, Al2O3, aluminum, zirconium silicide, amorphous or semi-amorphous alloyed stainless steel, and mixtures of Zr2AlC ceramic, Ti2AlC ceramic and Ti3AlC2 ceramic. The coating formed by the coating composition has a gradient emanating from the exterior surface of the cladding, which serves as the coating substrate, towards an exposed outer surface of the coating such that percent by weight of the first component decreases from the exterior surface of the cladding toward the exposed outer surface of the coating and percent by weight of the second component increases from the exterior surface of the cladding to the exposed outer surface of the coating, based on total weight percent of the coating composition.
- A further understanding of the invention can be gained from the following description of the preferred embodiments when read in conjunction with the accompanying drawings in which:
-
FIG. 1 is a cross-section view of a coated zirconium alloy substrate in accordance with the prior art; -
FIG. 2 is a cross-section view of a coated zirconium alloy substrate in accordance with certain embodiments of the invention; and -
FIG. 3 is a block diagram of a method of applying a coating material employing a kinetic deposition technique in accordance with certain embodiments of the invention. - The invention provides a coating composition which includes a zirconium compound and a compound which protects the cladding surface from bulk oxidation. The coating composition is deposited on an exterior surface of a zirconium alloy cladding, e.g., tube. The deposition can be performed using various conventional techniques, such as a kinetic deposition technique (referred to as “cold spray”). The zirconium alloy cladding tube typically has a zirconium-oxide layer inherently formed on at least a portion of its exterior surface. Deposition of the coating composition results in a coating being formed on at least a portion of the exterior surface of the zirconium alloy cladding tube.
- The zirconium alloy cladding is positioned in the core of a light water nuclear reactor, such as a pressurized water reactor (PWR) or a boiling water reactor (BWR). Thus, the cladding is exposed to a high temperature and pressure water environment.
- The coating composition of the invention includes a first component and a second component. The first component includes zirconium, zirconium oxide or mixtures thereof. The second component includes Zr2AlC ceramic, Ti2AlC ceramic, Ti3AlC2 ceramic, Al2O3, aluminum, zirconium silicide (ZrSi2), amorphous or semi-amorphous alloyed stainless steel, or mixtures of Zr2AlC, Ti2AlC and Ti3AlC2.
- Since the zirconium alloy cladding inherently has at least partially formed on its exterior surface a zirconium oxide-containing layer or film, the coating composition is actually deposited on and adhered to this zirconium oxide-containing layer. Deposition of the coating composition of the invention results in a gradient coating or matrix that emanates from the exterior surface of the zirconium alloy cladding to an outer exposed surface of the coating. This gradient coating is effective to eliminate bulk oxidation of the zirconium alloy cladding upon exposure to PWR or BWR conditions, e.g., coolant that circulates in the reactor core. The gradient of the coating is such that the amount or weight percent (based on total weight of the coating composition) of each of the first and second components increases or decreases as the coating thickness emanates from the surface of the coating which is adjacent to or near the zirconium alloy cladding surface toward the exposed outer surface of the coating. In certain embodiments, the amount of the first component decreases as the coating thickness emanates from the surface adjacent to or near the zirconium alloy cladding surface toward the exposed outer coating surface, and the amount of the second component increases as the coating thickness emanates from the surface adjacent to or near the zirconium alloy cladding surface toward the exposed outer coating surface. Further, the decrease in the amount of the first component may correspond to the increase in the amount of the second component. For example, when the weight percent of the first component decreases from about 75% by weight at the surface of the coating adjacent to or near the cladding surface to about 10% by weight at the exposed outer surface, the weight percent of the second component correspondingly increases from about 25% by weight at the surface of the coating adjacent to or near the cladding surface to about 90% by weight at the exposed outer surface of the coating. In certain embodiments, the weight percent of each of the first and second components may decrease and increase, respectively, such that the first component is present on the exposed outer surface of the coating in an amount of about 0% by weight and the second component is present on the exposed outer surface of the coating in an amount of about 100% by weight.
- The coating composition may be deposited onto the exterior surface of the zirconium alloy cladding to form the gradient coating by employing various coating techniques known in the art. In certain embodiments, the coating composition is deposited using a conventional kinetic deposition technique which generally includes directing particulate material by a gas stream toward a substrate. In accordance with the invention, typically, the coating composition is propelled by a propulsive gas stream toward the zirconium alloy cladding. The first and second components of the coating composition may each be propelled separately or they may be propelled together, e.g., in a blend or mixture. The coating composition may be propelled at room temperature or may be pre-heated to an elevated temperature, e.g., at or above the melting temperature of the first and second components. Without intending to be bound by any particular theory, it is believed that this method of kinetic deposition is capable of at least partially disrupting the zirconium-oxide layer which is inherently formed on the zirconium alloy cladding such that the resulting coating is firmly bonded, e.g., atom-to-atom, to the cladding surface.
- The gradient coating may be formed in several passes or in a single pass. In certain embodiments wherein several passes are employed, the first pass includes an excess amount of the first component. That is, the first component is present in greater than about 50% by weight based on total weight of the coating composition. In other embodiments, the first component in the first pass may be present in about 75% by weight or greater based on total weight of the coating composition. The remainder of the coating composition being composed of the second component. In certain embodiments, the first pass includes about 100% by weight of the first component and about 0% by weight of the second component based on total weight of the coating composition. In each subsequent pass, the amount of the first component decreases and the amount of the second component increases. In certain embodiments, the amount by which the first component decreases is equal to the amount by which the second component increases.
- In alternate embodiments, a single pass technique is employed. In these embodiments, the amount (e.g., percent by weight) of each of the first and second components in the coating composition is continually varied to produce the gradient coating.
- The kinetic deposition methodology of the invention produces an integrated gradient coating that is richer in the first component, e.g., the zirconium or zirconium oxide, in the portion of the coating that is closer to the substrate, e.g., zirconium alloy cladding, and richer in the second component, e.g., the oxidation resistant material, in the portion of the coating that is nearer the exposed surface of the coating. In certain embodiments in accordance with the invention, the first component is present in excess (e.g., as compared to the second component) near the zirconium alloy cladding surface and the presence of the first component decreases throughout the coating thickness such that the exposed surface of the coating has an excess of the second component. Without intending to be bound by any particular theory, it is believed that the increased presence of the first component adjacent to or near the cladding tube surface enhances incorporation of the gradient coating onto and into the surface, as the coating composition is chemically similar to the zirconium alloy cladding composition and, gradually changes the thermal expansion and radiation swelling characteristics to minimize thermal and radiation stresses during operation.
- In certain embodiments of the invention, the gradient coating of the invention is created by kinetically depositing a first layer of the coating composition which includes from about 50% to about 100% or from greater than about 50% to about 100% or from about 75% to about 95% by weight of the first component, and from about 0% to about 50% or from about 0% to less than about 50% or from about 5% to about 25% by weight of the second component, based on total weight of the coating composition. In certain embodiments, the first component is zirconium alloy. Subsequently, additional layers of the coating composition may be deposited on the first layer. In certain embodiments, in each of the additional layers, the amount of the first component will successively decrease and the amount of the second component will successively increase. As a result, the exposed outer surface of the coating is composed of an excess of the second component such that it retains the oxidation resistant behavior of the second component while a base is present (e.g., underlying layers) that is rich in zirconium, i.e., the first component.
- The method of the invention is generally directed to depositing an oxidation resistant material into a zirconium oxide layer, such that the oxidation resistant material ultimately penetrates into the zirconium substrate resulting in strong adhesion, and the oxidation resistant material deposited on the exposed outer coating surface provides a dense oxidation resistant surface that protects the underlying substrate from the nuclear reactor environment.
-
FIG. 2 shows an integrated gradient coating deposited on azirconium alloy substrate 10 in accordance with certain embodiments of the invention. InFIG. 2 , acoating layer 20 containing zirconium alloy, e.g., the first component is applied to thezirconium alloy substrate 10. Thezirconium alloy substrate 10 includes anoxidation layer 12 thereon. Thecoating layer 20 is adjacent to theoxidation layer 12. Within thecoating layer 20 is anintegration layer 22. Without intending to be bound by any particular theory, it is believed that a portion of thecoating layer 20 mixes together or integrates with a portion of theoxidation layer 12, to form theintegration layer 22 adjacent to theoxidation layer 12, which may penetrate within thezirconium alloy substrate 10. The zirconium (e.g., the first component) content of thecoating layer 20 increases toward thezirconium alloy substrate 10 as shown byarrow 24 and the non-zirconium species (e.g., the second component) content increases toward theoutside surface 26 as shown by arrow 28. - Typically, the
gradient coating layer 20 is deposited and theintegration layer 22 formed as a result of several passes of the kinetic deposition technique described herein. Each successive deposition increases in the non-zirconium alloy species, e.g., the second component, and decreases in zirconium alloy, e.g., the first component, content. In certain embodiments, a single pass deposition technique may be employed where the coating composition itself is altered in a continuous manner such that multiple passes are not required. The thickness of thecoating layer 20 may vary and in certain embodiments is less than or equal to about 100 micrometers thick, or more preferably from about 5 to about 100 micrometers thick, or from about 5 to about 50 micrometers thick. - The higher concentration of zirconium alloy, e.g., the first component, near the base of the
coating layer 20, e.g., its presence in excess as compared to the second (non-zirconium) component, and its presence in general, reduces thermal stresses incorporated by the kinetic deposition technique and in operation, reduces thermal coefficient and radiation swelling mismatches between the corrosion resistant additive, e.g., the second component, and the zirconium alloy cladding, thus increasing the propensity of thecoating layer 20 to adhere to thezirconium alloy cladding 10. - The gradient coating of the invention provides numerous benefits over known corrosion resistant coatings. For example, known coatings may be applied on top of, e.g., overlay, the oxidation layer resulting in poor adhesion and failure. In the invention as shown in
FIG. 2 , the gradient coating provides oxidation resistant material directly into the oxidation layer which ultimately penetrates into the zirconium alloy cladding resulting in strong adhesion and a dense oxidation resistant surface that protects the underlying cladding from the reactor environment. -
FIG. 3 shows a method of depositing a coating composition, e.g., the first and second components, in accordance with certain embodiments of this invention. Azirconium alloy tube 30 is supplied. Acoating composition 32 is supplied to a Kinetic Cold Spray or Thermal Spray Deposition Process (KCS/TSDP) 34. The KCS/TSDP provides or deposits thecoating composition 32 to form agradient coating 36. - While specific embodiments of the invention have been described in detail, it will be appreciated by those skilled in the art that various modifications and alternatives to those details could be developed in light of the overall teachings of the disclosure. Accordingly, the particular embodiments disclosed are meant to be illustrative only and not limiting as to the scope of the invention which is to be given the full breadth of the appended claims and any and all equivalents thereof.
Claims (16)
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|---|---|---|---|
| US16/008,439 US20180371601A1 (en) | 2013-05-28 | 2018-06-14 | KINETICALLY APPLIED GRADATED Zr-Al-C OR Ti-Al-C CERAMIC OR AMORPHOUS OR SEMI-AMORPHOUS STAINLESS STEEL WITH NUCLEAR GRADE ZIRCONIUM ALLOY METAL STRUCTURE |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201361827792P | 2013-05-28 | 2013-05-28 | |
| US14/205,799 US10060018B2 (en) | 2013-05-28 | 2014-03-12 | Kinetically applied gradated Zr-Al-C ceramic or Ti-Al-C ceramic or amorphous or semi-amorphous stainless steel with nuclear grade zirconium alloy metal structure |
| US16/008,439 US20180371601A1 (en) | 2013-05-28 | 2018-06-14 | KINETICALLY APPLIED GRADATED Zr-Al-C OR Ti-Al-C CERAMIC OR AMORPHOUS OR SEMI-AMORPHOUS STAINLESS STEEL WITH NUCLEAR GRADE ZIRCONIUM ALLOY METAL STRUCTURE |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| US14/205,799 Division US10060018B2 (en) | 2013-05-28 | 2014-03-12 | Kinetically applied gradated Zr-Al-C ceramic or Ti-Al-C ceramic or amorphous or semi-amorphous stainless steel with nuclear grade zirconium alloy metal structure |
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| US20180371601A1 true US20180371601A1 (en) | 2018-12-27 |
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| US14/205,799 Expired - Fee Related US10060018B2 (en) | 2013-05-28 | 2014-03-12 | Kinetically applied gradated Zr-Al-C ceramic or Ti-Al-C ceramic or amorphous or semi-amorphous stainless steel with nuclear grade zirconium alloy metal structure |
| US16/008,439 Abandoned US20180371601A1 (en) | 2013-05-28 | 2018-06-14 | KINETICALLY APPLIED GRADATED Zr-Al-C OR Ti-Al-C CERAMIC OR AMORPHOUS OR SEMI-AMORPHOUS STAINLESS STEEL WITH NUCLEAR GRADE ZIRCONIUM ALLOY METAL STRUCTURE |
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| US14/205,799 Expired - Fee Related US10060018B2 (en) | 2013-05-28 | 2014-03-12 | Kinetically applied gradated Zr-Al-C ceramic or Ti-Al-C ceramic or amorphous or semi-amorphous stainless steel with nuclear grade zirconium alloy metal structure |
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| Country | Link |
|---|---|
| US (2) | US10060018B2 (en) |
| EP (1) | EP3004420B1 (en) |
| JP (1) | JP6385015B2 (en) |
| KR (1) | KR20160016900A (en) |
| CN (1) | CN105189820B (en) |
| ES (1) | ES2741832T3 (en) |
| WO (1) | WO2014193549A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112775428A (en) * | 2020-12-25 | 2021-05-11 | 北京交通大学 | Ti generated on the surface of a titanium substrate in situ2AlC ceramic layer and preparation method thereof |
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| US9844923B2 (en) * | 2015-08-14 | 2017-12-19 | Westinghouse Electric Company Llc | Corrosion and wear resistant coating on zirconium alloy cladding |
| US10872701B2 (en) * | 2016-06-10 | 2020-12-22 | Westinghouse Electric Company Llc | Zirconium-coated silicon carbide fuel cladding for accident tolerant fuel application |
| JP6517981B2 (en) * | 2017-07-31 | 2019-05-22 | 株式会社東芝 | Method of repairing fuel assembly, method of manufacturing fuel assembly |
| ES2894683T3 (en) * | 2017-07-31 | 2022-02-15 | Toshiba Kk | Fuel assembly repair method, fuel assembly production method and fuel assembly |
| CN107805071B (en) * | 2017-10-26 | 2020-12-18 | 西南交通大学 | A kind of preparation method of low glass wettability titanium trialuminum carbon two/mullite composite ceramics |
| CN109207786B (en) * | 2018-11-01 | 2020-08-07 | 西北工业大学 | Zr3Al3C5-ZrAlxSiyMethod for preparing composite material |
| US11530485B2 (en) * | 2018-12-29 | 2022-12-20 | Kunming University Of Science And Technology | Ultralimit alloy and preparation method therefor |
| EP3680917B1 (en) * | 2019-01-14 | 2023-10-04 | Westinghouse Electric Sweden AB | A cladding tube for a fuel rod for nuclear reactors |
| CN110205567B (en) * | 2019-06-18 | 2021-05-04 | 河海大学 | A kind of iron-based amorphous/MAX phase composite material for piston ring and its preparation method and application |
| FR3100545B1 (en) * | 2019-09-06 | 2021-08-06 | Safran | COATED PART INCLUDING A PROTECTIVE COATING BASED ON MAX PHASES |
| EP3933067A1 (en) * | 2020-07-03 | 2022-01-05 | Flender GmbH | Coating, a component with a coating and method for producing a coating |
| CN111690892B (en) * | 2020-07-09 | 2022-03-22 | 长沙理工大学 | Preparation method of MAX phase-based coating |
| CN112921299B (en) * | 2021-01-20 | 2022-03-25 | 哈尔滨工业大学 | Preparation method of composite film on surface of zirconium cladding |
| CN116285468B (en) * | 2023-03-09 | 2024-06-11 | 北京交通大学 | Al (aluminum) alloy2O3And Ti is2AlC composite wave-absorbing coating and preparation method thereof |
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- 2014-04-14 CN CN201480025399.7A patent/CN105189820B/en not_active Expired - Fee Related
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Also Published As
| Publication number | Publication date |
|---|---|
| US20180179624A1 (en) | 2018-06-28 |
| JP6385015B2 (en) | 2018-09-05 |
| EP3004420B1 (en) | 2019-05-15 |
| JP2016540882A (en) | 2016-12-28 |
| EP3004420A1 (en) | 2016-04-13 |
| ES2741832T3 (en) | 2020-02-12 |
| EP3004420A4 (en) | 2017-01-11 |
| WO2014193549A1 (en) | 2014-12-04 |
| US10060018B2 (en) | 2018-08-28 |
| KR20160016900A (en) | 2016-02-15 |
| CN105189820A (en) | 2015-12-23 |
| CN105189820B (en) | 2017-09-26 |
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