EP3400324B1 - Method for producing a corrosion resistant metal substrate and corrosion resistant metal substrate provided thereby - Google Patents
Method for producing a corrosion resistant metal substrate and corrosion resistant metal substrate provided thereby Download PDFInfo
- Publication number
- EP3400324B1 EP3400324B1 EP17700205.2A EP17700205A EP3400324B1 EP 3400324 B1 EP3400324 B1 EP 3400324B1 EP 17700205 A EP17700205 A EP 17700205A EP 3400324 B1 EP3400324 B1 EP 3400324B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- nickel
- substrate
- layer
- molybdenum
- molybdenum oxide
- 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.)
- Active
Links
- 239000000758 substrate Substances 0.000 title claims description 79
- 238000005260 corrosion Methods 0.000 title claims description 27
- 230000007797 corrosion Effects 0.000 title claims description 27
- 229910052751 metal Inorganic materials 0.000 title claims description 13
- 239000002184 metal Substances 0.000 title claims description 13
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 154
- 229910052759 nickel Inorganic materials 0.000 claims description 77
- 238000000137 annealing Methods 0.000 claims description 45
- 229910000476 molybdenum oxide Inorganic materials 0.000 claims description 37
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 claims description 37
- 229910000831 Steel Inorganic materials 0.000 claims description 28
- 238000009792 diffusion process Methods 0.000 claims description 28
- 239000010959 steel Substances 0.000 claims description 28
- 239000010941 cobalt Substances 0.000 claims description 25
- 229910017052 cobalt Inorganic materials 0.000 claims description 25
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 25
- 238000000034 method Methods 0.000 claims description 25
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 20
- 239000007864 aqueous solution Substances 0.000 claims description 18
- 229910052750 molybdenum Inorganic materials 0.000 claims description 16
- 239000011733 molybdenum Substances 0.000 claims description 16
- 229910052782 aluminium Inorganic materials 0.000 claims description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 14
- 229910001220 stainless steel Inorganic materials 0.000 claims description 14
- 239000004411 aluminium Substances 0.000 claims description 13
- 238000007747 plating Methods 0.000 claims description 12
- 238000004070 electrodeposition Methods 0.000 claims description 11
- 230000008569 process Effects 0.000 claims description 9
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 8
- 230000009467 reduction Effects 0.000 claims description 8
- 229910019142 PO4 Inorganic materials 0.000 claims description 7
- AJPJDKMHJJGVTQ-UHFFFAOYSA-M sodium dihydrogen phosphate Chemical group [Na+].OP(O)([O-])=O AJPJDKMHJJGVTQ-UHFFFAOYSA-M 0.000 claims description 7
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 claims description 6
- 239000010452 phosphate Substances 0.000 claims description 6
- 229910019626 (NH4)6Mo7O24 Inorganic materials 0.000 claims description 5
- 229910001209 Low-carbon steel Inorganic materials 0.000 claims description 5
- 239000010962 carbon steel Substances 0.000 claims description 5
- 150000002751 molybdenum Chemical class 0.000 claims description 5
- 229910000162 sodium phosphate Inorganic materials 0.000 claims description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 4
- 239000001257 hydrogen Substances 0.000 claims description 4
- 229910052739 hydrogen Inorganic materials 0.000 claims description 4
- 229910000318 alkali metal phosphate Inorganic materials 0.000 claims description 2
- 235000018660 ammonium molybdate Nutrition 0.000 claims description 2
- 239000011609 ammonium molybdate Substances 0.000 claims description 2
- APUPEJJSWDHEBO-UHFFFAOYSA-P ammonium molybdate Chemical group [NH4+].[NH4+].[O-][Mo]([O-])(=O)=O APUPEJJSWDHEBO-UHFFFAOYSA-P 0.000 claims description 2
- 229940010552 ammonium molybdate Drugs 0.000 claims description 2
- 239000000446 fuel Substances 0.000 claims description 2
- 229910000403 monosodium phosphate Inorganic materials 0.000 claims 1
- 235000019799 monosodium phosphate Nutrition 0.000 claims 1
- 239000010410 layer Substances 0.000 description 88
- 239000000463 material Substances 0.000 description 10
- 239000010935 stainless steel Substances 0.000 description 10
- 229910052799 carbon Inorganic materials 0.000 description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical group [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 7
- 238000006722 reduction reaction Methods 0.000 description 7
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 6
- 239000011651 chromium Substances 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 235000021317 phosphate Nutrition 0.000 description 5
- 239000011148 porous material Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000000151 deposition Methods 0.000 description 4
- 239000003792 electrolyte Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229910000402 monopotassium phosphate Inorganic materials 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- 239000007836 KH2PO4 Substances 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- XSQUKJJJFZCRTK-UHFFFAOYSA-N Urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 239000004202 carbamide Substances 0.000 description 2
- 239000010960 cold rolled steel Substances 0.000 description 2
- 238000005097 cold rolling Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000009713 electroplating Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- GNSKLFRGEWLPPA-UHFFFAOYSA-M potassium dihydrogen phosphate Chemical compound [K+].OP(O)([O-])=O GNSKLFRGEWLPPA-UHFFFAOYSA-M 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000922 High-strength low-alloy steel Inorganic materials 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- 229910003296 Ni-Mo Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000001479 atomic absorption spectroscopy Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000000872 buffer Substances 0.000 description 1
- 239000000337 buffer salt Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010531 catalytic reduction reaction Methods 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001805 chlorine compounds Chemical group 0.000 description 1
- 229910000423 chromium oxide Inorganic materials 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- DDTIGTPWGISMKL-UHFFFAOYSA-N molybdenum nickel Chemical compound [Ni].[Mo] DDTIGTPWGISMKL-UHFFFAOYSA-N 0.000 description 1
- 235000019796 monopotassium phosphate Nutrition 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 150000003013 phosphoric acid derivatives Chemical class 0.000 description 1
- PJNZPQUBCPKICU-UHFFFAOYSA-N phosphoric acid;potassium Chemical compound [K].OP(O)(O)=O PJNZPQUBCPKICU-UHFFFAOYSA-N 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 239000011780 sodium chloride Substances 0.000 description 1
- 235000015393 sodium molybdate Nutrition 0.000 description 1
- 239000011684 sodium molybdate Substances 0.000 description 1
- TVXXNOYZHKPKGW-UHFFFAOYSA-N sodium molybdate (anhydrous) Chemical compound [Na+].[Na+].[O-][Mo]([O-])(=O)=O TVXXNOYZHKPKGW-UHFFFAOYSA-N 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/627—Electroplating characterised by the visual appearance of the layers, e.g. colour, brightness or mat appearance
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/12—Electroplating: Baths therefor from solutions of nickel or cobalt
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/36—Pretreatment of metallic surfaces to be electroplated of iron or steel
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/42—Pretreatment of metallic surfaces to be electroplated of light metals
- C25D5/44—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/48—After-treatment of electroplated surfaces
- C25D5/50—After-treatment of electroplated surfaces by heat-treatment
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/60—Electroplating characterised by the structure or texture of the layers
- C25D5/623—Porosity of the layers
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D9/00—Electrolytic coating other than with metals
- C25D9/04—Electrolytic coating other than with metals with inorganic materials
- C25D9/08—Electrolytic coating other than with metals with inorganic materials by cathodic processes
- C25D9/10—Electrolytic coating other than with metals with inorganic materials by cathodic processes on iron or steel
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D9/00—Electrolytic coating other than with metals
- C25D9/04—Electrolytic coating other than with metals with inorganic materials
- C25D9/08—Electrolytic coating other than with metals with inorganic materials by cathodic processes
- C25D9/12—Electrolytic coating other than with metals with inorganic materials by cathodic processes on light metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/16—Selection of particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2803—Construction of catalytic reactors characterised by structure, by material or by manufacturing of catalyst support
- F01N3/2807—Metal other than sintered metal
- F01N3/281—Metallic honeycomb monoliths made of stacked or rolled sheets, foils or plates
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/0011—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
- F02M37/0017—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor related to fuel pipes or their connections, e.g. joints or sealings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2510/00—Surface coverings
- F01N2510/08—Surface coverings for corrosion prevention
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2530/00—Selection of materials for tubes, chambers or housings
- F01N2530/02—Corrosion resistive metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2530/00—Selection of materials for tubes, chambers or housings
- F01N2530/02—Corrosion resistive metals
- F01N2530/04—Steel alloys, e.g. stainless steel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2530/00—Selection of materials for tubes, chambers or housings
- F01N2530/06—Aluminium or alloys thereof
Definitions
- This invention relates to a method for producing a corrosion resistant metal substrate and corrosion resistant metal substrate provided thereby.
- Materials used for exhaust piping, mufflers, and other exhaust system components consist mainly of ferrous alloys. Aluminium alloys are sometimes used as a coating on ferrous alloys to impart additional corrosion resistance.
- the choice of exhaust system materials is driven by a number of factors including cost, warranty requirements and legislated and customer demands for long service life.
- Mild carbon steel was the material of choice for exhaust systems for many decades.
- An iron oxide coating on the exhaust system protected it from atmospheric corrosion to varying degrees. However, it suffered from poor corrosion resistance when exposed to road salt and exhaust condensate. As a result, exhaust systems made from this material had a very short life if exposed to the environment experienced by many on-road vehicles.
- the corrosion resistance of carbon steel can be greatly improved through the use of a hot dipped aluminium coating. This is often referred to as aluminised steel.
- One particularly important ferrous alloy alloying element is chromium.
- stainless steel By adding sufficient chromium, stainless steel is formed. When stainless steel is heated, chromium forms a protective chromium oxide coating that delays further oxidation. A minimum of about 10.5% chromium is usually required to passivate the surface and to classify a material as stainless steel. So long as this oxide layer is stable and continuous, the metal substrate is well protected from corrosion. Since about the mid-1990s, plain carbon and low alloy steels have been replaced by stainless steel as the primary material for exhaust systems. This transition has taken place because of market demands for extended warranties, and because of demands mandated by emission standards. Technologies to meet increasingly stringent emission standards can raise exhaust temperatures which makes the task of meeting strength and durability requirements especially challenging. Emission standards also require that exhaust systems are designed in a manner that facilitates leak-free assembly, installation and operation for the full useful life of the vehicle.
- US2010/0167087 discloses a steel or aluminum substrate electroplated with a corrosion resistant alloy layer of Ni-Mo.
- One or more of the objects is reached by a method for producing a corrosion resistant metal substrate by electroplating:
- the diffusion layer contains nickel, molybdenum and optionally cobalt. There may be other components in the diffusion layer such as phosphate.
- the metal substrate which may be provided in the form of a coiled strip of steel such as (low) carbon steel or stainless steel, or in the form a coiled strip of aluminium or aluminium alloy with a suitable chemical composition for the application of the final product, is provided with a nickel layer, or a nickel-based layer, and optionally with a cobalt layer on top of the nickel or nickel-based layer to form a plated substrate.
- Nickel layers can for instance be deposited onto the substrate in a Watts nickel plating bath.
- a nickel-based layer is a layer predominantly consisting of nickel but not solely of nickel.
- a nickel alloy layer is therefore considered a nickel based layer.
- the term "nickel layer" hereinafter intends to include "nickel-based layer".
- the corrosion protection offered by the nickel layer may be insufficient for certain applications as a result of the presence of pores in the nickel layer.
- the cobalt layer is used to improve the corrosion resistance of the nickel plated substrate.
- the plated substrate is then led through the said aqueous solution in an electroplating device in which the plated substrate acts as the cathode, and provided with the molybdenum oxide layer.
- the molybdenum oxide in the molybdenum oxide layer is then reduced to molybdenum metal in a reduction annealing step and, as a consequence of the high temperature during the reduction annealing step, the molybdenum diffuses into the nickel and/or cobalt layer, thereby forming a diffusion layer comprising nickel, molybdenum and optionally cobalt.
- the reduction annealing step is also the diffusion annealing step. This is the preferable case. However, if necessary, the annealing step can be prolonged to further promote the diffusion after the reduction of the molybdenum oxide has been completed.
- the reducing atmosphere is a hydrogen containing atmosphere, such as substantially pure hydrogen or HNX.
- the diffusion layer comprising nickel and molybdenum, and optionally cobalt, is pore free, and provides an excellent protection of the substrate.
- the molybdenum salt is ammonium molybdate ((NH 4 ) 6 Mo 7 O 24 ).
- ammonium molybdate (NH 4 ) 6 Mo 7 O 24 ).
- ammonium molybdate (NH 4 ) 6 Mo 7 O 24 ).
- ammonium molybdate (NH 4 ) 6 Mo 7 O 24 ).
- Other molybdenum salts would result in deposits on the surface.
- sodium-molybdate would result in the presence of sodium on the surface which would result in an undesirable alkaline corrosion reaction.
- the phosphate is sodium dihydrogen phosphate (NaH 2 PO 4 ).
- NaH 2 PO 4 sodium dihydrogen phosphate
- This functions acts both a conducting salt in the electrolyte and as a buffer salt.
- the buffer ensures that the right pH-value of the electrolyte is maintained.
- Potassium dihydrogen phosphate (KH 2 PO 4 ) could technically also be used, alone or as a mixture with NaH 2 PO 4 , but KH 2 PO 4 is currently more expensive and therefore economically less attractive.
- the nickel layer (or nickel-based layer) provided on the substrate is between 0.5 and 5 ⁇ m in thickness. This thickness range provides sufficient thickness for the diffusion layer after the reduction annealing to be effective. It is preferable that the diffusion layer comprising of nickel, originating from the nickel or nickel-based layer, and optionally cobalt, originating from the optional cobalt layer, and molybdenum, originating from the reduced molybdenum oxide layer, has a thickness of between 10 and 200 nm. A preferable minimum thickness is 20 nm, and a preferable maximum thickness is 150 nm. Preferably the thickness of the diffusion layer is between 50 and 100 nm.
- the temperature of the aqueous solution is at least 51 °C and/or at most 69 °C.
- the plating time is preferably at most 20 seconds, whereas it is preferable that the current density for the electrodeposition of the molybdenum oxide layer is at least 6 and/or at most 22 A/dm 2 . More preferably the temperature of the aqueous solution is at least 55 °C and/or at most 65 °C.
- the maximum annealing temperature is 700 °C, preferably 650 °C and more preferably 600 °C to prevent too large an impact on the properties of the steel substrate.
- the maximum annealing temperature is 900 °C, preferably 850 °C and more preferably 800 °C to prevent too large an impact on the properties of the steel substrate.
- the lower limit of the annealing temperature is controlled largely by the lay-out of the annealing facilities and of the economy of the process. The lower the temperature, the longer it takes for a Ni-Mo-diffusion layer of a desired thickness to form.
- the allowable temperatures are lower.
- the maximum annealing temperature depends on the alloy is at most 500 and preferably at most 450 °C to prevent too large an impact on the properties of the substrate.
- a suitable temperature can be determined easily by simple trial and error. As the temperature is lower, the required diffusion time increases.
- the annealing time in the batch annealing process is between 6 and 10 hours, preferably at most 8.5 hours and more preferably at most 7.5 hours.
- the annealing time is at most 120 seconds, preferably at most 95 s, more preferably at most 75 s and even more preferably at most 40 s.
- a suitable minimum continuous annealing temperature is 5 s, preferably at least 10 s.
- This composition allows to effectively and reproducibly deposit the molybdenum oxide layer. It is noted that 30 g/l of (NH 4 ) 6 Mo 7 O 24 corresponds to 0.024 mol/l and 50 g/l of NaH 2 PO 4 to 0.42 mol/l.
- the thickness of the deposited molybdenum oxide layer is at most 100 nm, preferably at most 75, more preferably 50 nm, and even more preferably 40 nm.
- the minimum thickness is at least 10 nm.
- the pH of the aqueous solution is at least 4.5 and/or at most 6.
- the pH is at least 5.25 and/or at most 5.75.
- the cathodic current density for depositing the molybdenum oxide layer is at least 12.5 A/dm 2 and preferably at least 15 A/dm 2 .
- the steel substrate is a carbon steel, preferably a low carbon steel, extra-low carbon steel or a HSLA-steel.
- These unalloyed (LC and ELC) or micro-alloyed (HSLA) steels are relatively cheap substrates and provide good strength and formability.
- the steels are produced by means of commonly known processes such as casting, hot-rolling and cold-rolling.
- Low carbon steels typically comprise 0.05 to 0.15 wt.% C and extra low carbon steels typically comprise 0.02 to 0.05 wt.% C.
- Other elements may be present in addition to carbon in accordance with EN 10020-2000 which prescribes how much of a certain element may be present to still be considered an unalloyed steel.
- High-strength low-alloy (HSLA) steels are designed to provide better mechanical properties and/or greater resistance to atmospheric corrosion than carbon steels.
- the HSLA steels have low carbon contents (0.05-0.15% C) in order to produce adequate formability and weldability, and they have manganese contents up to 2.0%.
- Small quantities of chromium, nickel, molybdenum, copper, nitrogen, vanadium, niobium, titanium and zirconium are used in various combinations to achieve the desired properties.
- the steel substrate has been cold-rolled to its final thickness, usually between 0.15 and 1.5 mm, and the cold-rolled steel substrate may or may not have been recrystallisation or recovery annealed prior to depositing the nickel and optional cobalt layer according to the invention.
- the steel substrate is preferably supplied in the form of a coiled strip.
- the steel substrate is a ferritic stainless steel, such as an SAE 400-series, which generally are considered to have better engineering properties than austenitic stainless steel grades, but have reduced corrosion resistance, because of the lower chromium and nickel content. They are also usually less expensive. Ferritic stainless steels have a body-centered cubic crystal structure and contain between 10.5% and 27% chromium with very little nickel, if any. By means of a non-limiting example the steel SAE 430 (1.4016) proved to be a useful substrate for the method according to the invention.
- the stainless steel substrate has been cold-rolled to its final thickness, usually between 0.15 and 1.5 mm, and the cold-rolled steel substrate may or may not have been recrystallisation or recovery annealed prior to depositing the nickel and optional cobalt layer according to the invention.
- the stainless steel substrate is preferably supplied in the form of a coiled strip.
- the substrate for the method according to the invention may also be an aluminium or an aluminium alloy substrate.
- the diffusion layer comprising of nickel originating from the nickel or nickel-based layer and molybdenum originating from the molybdenum oxide layer also comprises phosphor, preferably 5 to 15 wt.% of phosphor, more preferably 6 to 13 wt.%. A suitable maximum amount is 10 wt.%. A suitable minimum amount is 7 wt.%.
- the invention is also embodied in a corrosion resistant metal substrate provided with a diffusion layer comprising nickel, molybdenum and optionally cobalt, produced according to the invention wherein the diffusion layer (i.e. the Ni-Mo- or Ni-Mo-Co-diffusion layer) has a thickness of between 10 and 200 nm.
- the diffusion layer i.e. the Ni-Mo- or Ni-Mo-Co-diffusion layer
- the thickness of the Ni-Mo-diffusion layer is between 50 and 100 nm. This thickness can be determined e.g. by means of GDOES.
- the thickness of the layer is determined by locating the halfvalue (ignoring the surface effects) of the Mo-curve.
- the invention is embodied in the use of the above corrosion resistant substrate for the production of an exhaust system or parts for an exhaust system produced from the metal substrate according to the invention.
- the metal substrate according to the invention is used in fuel lines for instance for internal combustion engines.
- An aqueous solution was prepared consisting of 30 g/l of (NH 4 ) 6 Mo 7 O 24 (0.024 mol/l) and 50 g/l of NaH 2 PO 4 (0.42 mol/l) with a pH of 5.5 and maintained at 60 °C.
- a molybdenum-oxide layer was deposited on a 2 ⁇ m matt nickel plated low-carbon steel using a current density of 20 A/dm 2 and a plating time of 15 and 10 seconds. This material was then annealed in a reducing hydrogen atmosphere for 7.3 hours in a batch annealing furnace.
- the resulting Ni-Mo-diffusion layer has a thickness of about 150 nm at the surface of the coated substrate.
- Figure 1 shows a non-limitative example of the implementation of the process according to the invention.
- the hot-rolled starting product is pickled to remove the oxides from the strip and clean the surface.
- the strip is cold-rolled.
- the various layers are electrodeposited.
- the diffusion annealing takes place.
- the cold-rolling can obviously also take place elsewhere when the cold-rolled coil is bought from a supplier of cold rolled coil.
- Figure 2 shows a GDOES-measurement of the surface after depositing the molybdenum oxide on the nickel layer.
- the X-axis gives the thickness in nm and the Y-axis gives the concentration in wt%. Note that the values for carbon and sulphur are in fact 10 times as low as presented.
- the layer of molybdenum oxide on top of the nickel layer is 2 ⁇ m (i.e. 2000 nm), whereas the molybdenum oxide layer is about 60 nm.
- Figure 3 shows a GDOES-measurement of the surface after annealing the layers of Figure 2 .
- the values for carbon and sulphur are in fact 10 times as low as presented.
- the clearly discernable layer of molybdenum oxide on top of the nickel layer has vanished, and a diffusion layer comprising nickel and molybdenum is shown.
- There is still a degree of oxygen present in the surface layers but this is believed to be associated with re-oxidation if the surface, and with the presence of the phosphates, and not with the molybdenum oxide which has reduced to metallic molybdenum.
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Description
- This invention relates to a method for producing a corrosion resistant metal substrate and corrosion resistant metal substrate provided thereby.
- Materials used for exhaust piping, mufflers, and other exhaust system components consist mainly of ferrous alloys. Aluminium alloys are sometimes used as a coating on ferrous alloys to impart additional corrosion resistance. The choice of exhaust system materials is driven by a number of factors including cost, warranty requirements and legislated and customer demands for long service life. Mild carbon steel was the material of choice for exhaust systems for many decades. An iron oxide coating on the exhaust system protected it from atmospheric corrosion to varying degrees. However, it suffered from poor corrosion resistance when exposed to road salt and exhaust condensate. As a result, exhaust systems made from this material had a very short life if exposed to the environment experienced by many on-road vehicles. The corrosion resistance of carbon steel can be greatly improved through the use of a hot dipped aluminium coating. This is often referred to as aluminised steel.
- One particularly important ferrous alloy alloying element is chromium. By adding sufficient chromium, stainless steel is formed. When stainless steel is heated, chromium forms a protective chromium oxide coating that delays further oxidation. A minimum of about 10.5% chromium is usually required to passivate the surface and to classify a material as stainless steel. So long as this oxide layer is stable and continuous, the metal substrate is well protected from corrosion. Since about the mid-1990s, plain carbon and low alloy steels have been replaced by stainless steel as the primary material for exhaust systems. This transition has taken place because of market demands for extended warranties, and because of demands mandated by emission standards. Technologies to meet increasingly stringent emission standards can raise exhaust temperatures which makes the task of meeting strength and durability requirements especially challenging. Emission standards also require that exhaust systems are designed in a manner that facilitates leak-free assembly, installation and operation for the full useful life of the vehicle.
- From the early part of the 21st century, commodities including many of the alloying elements used in stainless steel, have experienced wide and rapid price fluctuations. Emission control systems such as actively regenerated diesel particulate filters (DPFs) and urea selective catalytic reduction (SCR) have also created new demands on material properties. Active DPF regeneration can produce exhaust temperatures as high as 800°C in parts of the exhaust system that would otherwise operate at much lower temperatures. Also, some commonly used stainless steels, such as type 304, have been found to corrode after exposure to urea decomposition products in high temperature environments.
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US2010/0167087 discloses a steel or aluminum substrate electroplated with a corrosion resistant alloy layer of Ni-Mo. - It is an object of the present invention to provide a new corrosion resistant substrate.
- It is also an object of the present invention to provide a new corrosion resistant substrate for applications at high temperatures.
- It is also an object of the present invention to provide a new corrosion resistant substrate for applications at high temperatures on the basis of a low cost ferrous substrate.
- It is also an object of the present invention to provide a low cost method for producing a corrosion resistant substrate, suitable for applications at high temperatures.
- One or more of the objects is reached by a method for producing a corrosion resistant metal substrate by electroplating:
- i. a nickel or nickel-based layer on a steel or aluminium substrate, or
- ii. a nickel or nickel-based layer on a steel or aluminium substrate followed by providing a cobalt layer on the nickel or nickel-based layer,
to form a plated substrate followed by electrodepositing a molybdenum oxide layer from an aqueous solution onto the plated substrate, wherein the plated substrate acts as a cathode, wherein the aqueous solution comprises a molybdenum salt and an alkali metal phosphate and wherein the pH of the aqueous solution is adjusted to between 4.0 and 6.5, wherein the plated substrate provided with the molybdenum oxide layer is subjected to an annealing step in a reducing atmosphere to, at least partly, reduce the molybdenum oxide in the molybdenum oxide layer to molybdenum metal in a reduction annealing step and to form, simultaneously or subsequently, in the annealing step a diffusion layer which contains nickel and molybdenum, and optionally cobalt, wherein the nickel originates from the nickel or nickel-based layer, the cobalt originates from the optional cobalt layer, and the molybdenum originates from the molybdenum oxide layer. - The diffusion layer contains nickel, molybdenum and optionally cobalt. There may be other components in the diffusion layer such as phosphate.
- The metal substrate, which may be provided in the form of a coiled strip of steel such as (low) carbon steel or stainless steel, or in the form a coiled strip of aluminium or aluminium alloy with a suitable chemical composition for the application of the final product, is provided with a nickel layer, or a nickel-based layer, and optionally with a cobalt layer on top of the nickel or nickel-based layer to form a plated substrate. Nickel layers can for instance be deposited onto the substrate in a Watts nickel plating bath. A nickel-based layer is a layer predominantly consisting of nickel but not solely of nickel. A nickel alloy layer is therefore considered a nickel based layer. Unless indicated otherwise, the term "nickel layer" hereinafter intends to include "nickel-based layer". The corrosion protection offered by the nickel layer may be insufficient for certain applications as a result of the presence of pores in the nickel layer. The cobalt layer is used to improve the corrosion resistance of the nickel plated substrate. The plated substrate is then led through the said aqueous solution in an electroplating device in which the plated substrate acts as the cathode, and provided with the molybdenum oxide layer. The molybdenum oxide in the molybdenum oxide layer is then reduced to molybdenum metal in a reduction annealing step and, as a consequence of the high temperature during the reduction annealing step, the molybdenum diffuses into the nickel and/or cobalt layer, thereby forming a diffusion layer comprising nickel, molybdenum and optionally cobalt. So the reduction annealing step is also the diffusion annealing step. This is the preferable case. However, if necessary, the annealing step can be prolonged to further promote the diffusion after the reduction of the molybdenum oxide has been completed. Preferably the reducing atmosphere is a hydrogen containing atmosphere, such as substantially pure hydrogen or HNX.
- The inventors found that the diffusion layer comprising nickel and molybdenum, and optionally cobalt, is pore free, and provides an excellent protection of the substrate. The pores in the nickel or nickel-alloy layer, if present, are closed as a result of the use of the method according to the invention.
- It should be noted that after the reduction annealing step in principle all molybdenum oxide is reduced to molybdenum metal. However, after exposure of the annealed strip to the ambient atmosphere the outermost surface may reoxidise. On a 150 nm thick diffusion layer a 20 to 30 nm thick oxide layer may be present.
- In an embodiment the molybdenum salt is ammonium molybdate ((NH4)6Mo7O24). The advantage of the use of ammonium as the cation is that it decomposes during the heat treatment. Other molybdenum salts would result in deposits on the surface. E.g. sodium-molybdate would result in the presence of sodium on the surface which would result in an undesirable alkaline corrosion reaction.
- In an embodiment the phosphate is sodium dihydrogen phosphate (NaH2PO4). This functions acts both a conducting salt in the electrolyte and as a buffer salt. The buffer ensures that the right pH-value of the electrolyte is maintained. Potassium dihydrogen phosphate (KH2PO4) could technically also be used, alone or as a mixture with NaH2PO4, but KH2PO4 is currently more expensive and therefore economically less attractive.
- In further embodiments of the invention wherein the nickel layer (or nickel-based layer) provided on the substrate is between 0.5 and 5 µm in thickness. This thickness range provides sufficient thickness for the diffusion layer after the reduction annealing to be effective. It is preferable that the diffusion layer comprising of nickel, originating from the nickel or nickel-based layer, and optionally cobalt, originating from the optional cobalt layer, and molybdenum, originating from the reduced molybdenum oxide layer, has a thickness of between 10 and 200 nm. A preferable minimum thickness is 20 nm, and a preferable maximum thickness is 150 nm. Preferably the thickness of the diffusion layer is between 50 and 100 nm.
- In an embodiment
- the temperature of the aqueous solution for the electrodeposition of the molybdenum oxide layer onto the nickel plated substrate is between 40 °C and 75 °C, and/or
- the plating time for the electrodeposition of the molybdenum oxide layer onto the nickel plated substrate is between 5 and 30 seconds, and/or
- the current density for the electrodeposition of the molybdenum oxide layer onto the nickel plated substrate is between 2 and 25 A/dm2, and/or
- the maximum annealing temperature during the annealing step is between 500 and 1050 °C, and/or
- the annealing time is between 6 and 10 hours for a batch annealing process or between 10 and 120 seconds for a continuous annealing process.
- These features are independent and can be applied separately or in combination.
- Preferably the temperature of the aqueous solution is at least 51 °C and/or at most 69 °C. The plating time is preferably at most 20 seconds, whereas it is preferable that the current density for the electrodeposition of the molybdenum oxide layer is at least 6 and/or at most 22 A/dm2. More preferably the temperature of the aqueous solution is at least 55 °C and/or at most 65 °C.
- In an embodiment
- the plating time for the electrodeposition of the cobalt layer onto the nickel plated substrate is between 5 and 40 seconds, and/or
- the current density for the electrodeposition of the cobalt layer onto the nickel plated substrate is between 2 and 25 A/dm2, and/or
- In relation to the maximum annealing temperature during the annealing step a distinction can be made in dependence of the substrate. It was found that for a low-carbon steel substrate the maximum annealing temperature is 700 °C, preferably 650 °C and more preferably 600 °C to prevent too large an impact on the properties of the steel substrate. For a stainless steel substrate the maximum annealing temperature is 900 °C, preferably 850 °C and more preferably 800 °C to prevent too large an impact on the properties of the steel substrate. Both for low-carbon (LC) steel substrates as for stainless steel substrates the lower limit of the annealing temperature is controlled largely by the lay-out of the annealing facilities and of the economy of the process. The lower the temperature, the longer it takes for a Ni-Mo-diffusion layer of a desired thickness to form.
- For an aluminium or aluminium alloy substrate, the allowable temperatures are lower. For such a substrate the maximum annealing temperature depends on the alloy is at most 500 and preferably at most 450 °C to prevent too large an impact on the properties of the substrate. A suitable temperature can be determined easily by simple trial and error. As the temperature is lower, the required diffusion time increases.
- The annealing time in the batch annealing process is between 6 and 10 hours, preferably at most 8.5 hours and more preferably at most 7.5 hours. For a continuous annealing process the annealing time is at most 120 seconds, preferably at most 95 s, more preferably at most 75 s and even more preferably at most 40 s. A suitable minimum continuous annealing temperature is 5 s, preferably at least 10 s. There is a degree of interchangeability between the annealing time and the annealing temperature. It should be noted that when referring to an annealing time of 8.5 hours in a batch annealing furnace this intends to mean that the cold spot of the (coiled) material reaches the set temperature in 8.5 hours, after which the cooling starts. A total cycle of heating and cooling may therefore be considerably longer than 8.5 hours and be more than double that value.
- In an embodiment the aqueous solution for the electrodeposition of the molybdenum oxide layer onto the plated substrate comprises:
- between 10 and 50 g/l of (NH4)6Mo7O24, and/or
- between 20 and 80 g/l of NaH2PO4.
- This composition allows to effectively and reproducibly deposit the molybdenum oxide layer. It is noted that 30 g/l of (NH4)6Mo7O24 corresponds to 0.024 mol/l and 50 g/l of NaH2PO4 to 0.42 mol/l.
- In a preferable embodiment the thickness of the deposited molybdenum oxide layer is at most 100 nm, preferably at most 75, more preferably 50 nm, and even more preferably 40 nm. Preferably the minimum thickness is at least 10 nm.
- In an embodiment the pH of the aqueous solution is at least 4.5 and/or at most 6. Preferably the pH is at least 5.25 and/or at most 5.75.
- In a preferable embodiment wherein the cathodic current density for depositing the molybdenum oxide layer is at least 12.5 A/dm2 and preferably at least 15 A/dm2.
- Preferably the steel substrate is a carbon steel, preferably a low carbon steel, extra-low carbon steel or a HSLA-steel. These unalloyed (LC and ELC) or micro-alloyed (HSLA) steels are relatively cheap substrates and provide good strength and formability. The steels are produced by means of commonly known processes such as casting, hot-rolling and cold-rolling. Low carbon steels typically comprise 0.05 to 0.15 wt.% C and extra low carbon steels typically comprise 0.02 to 0.05 wt.% C. Other elements may be present in addition to carbon in accordance with EN 10020-2000 which prescribes how much of a certain element may be present to still be considered an unalloyed steel. High-strength low-alloy (HSLA) steels (aka micro-alloyed steels) are designed to provide better mechanical properties and/or greater resistance to atmospheric corrosion than carbon steels. The HSLA steels have low carbon contents (0.05-0.15% C) in order to produce adequate formability and weldability, and they have manganese contents up to 2.0%. Small quantities of chromium, nickel, molybdenum, copper, nitrogen, vanadium, niobium, titanium and zirconium are used in various combinations to achieve the desired properties. It is preferable that the steel substrate has been cold-rolled to its final thickness, usually between 0.15 and 1.5 mm, and the cold-rolled steel substrate may or may not have been recrystallisation or recovery annealed prior to depositing the nickel and optional cobalt layer according to the invention. The steel substrate is preferably supplied in the form of a coiled strip.
- In an embodiment of the invention the steel substrate is a ferritic stainless steel, such as an SAE 400-series, which generally are considered to have better engineering properties than austenitic stainless steel grades, but have reduced corrosion resistance, because of the lower chromium and nickel content. They are also usually less expensive. Ferritic stainless steels have a body-centered cubic crystal structure and contain between 10.5% and 27% chromium with very little nickel, if any. By means of a non-limiting example the steel SAE 430 (1.4016) proved to be a useful substrate for the method according to the invention. It is preferable that the stainless steel substrate has been cold-rolled to its final thickness, usually between 0.15 and 1.5 mm, and the cold-rolled steel substrate may or may not have been recrystallisation or recovery annealed prior to depositing the nickel and optional cobalt layer according to the invention. The stainless steel substrate is preferably supplied in the form of a coiled strip.
- The substrate for the method according to the invention may also be an aluminium or an aluminium alloy substrate.
- In an embodiment the diffusion layer comprising of nickel originating from the nickel or nickel-based layer and molybdenum originating from the molybdenum oxide layer also comprises phosphor, preferably 5 to 15 wt.% of phosphor, more preferably 6 to 13 wt.%. A suitable maximum amount is 10 wt.%. A suitable minimum amount is 7 wt.%. Although the oxidation state of the phosphor is not exactly known, it is believed that the phosphor originated from the phosphate in the electrolyte. It may even still be present as phosphate in the layer. It is believed that its presence contributes to the corrosion protection of the layer.
- According to a second aspect, the invention is also embodied in a corrosion resistant metal substrate provided with a diffusion layer comprising nickel, molybdenum and optionally cobalt, produced according to the invention wherein the diffusion layer (i.e. the Ni-Mo- or Ni-Mo-Co-diffusion layer) has a thickness of between 10 and 200 nm. A preferable minimum thickness is 20 nm, and a preferable maximum thickness is 150 nm. Preferably the thickness of the Ni-Mo-diffusion layer is between 50 and 100 nm. This thickness can be determined e.g. by means of GDOES. The thickness of the layer is determined by locating the halfvalue (ignoring the surface effects) of the Mo-curve. The thickness in
Figure 2 (before annealing) results in a NiMo-layer thickness of 60 nm and inFigure 3 in a Mo-alloy layer of 80 nm. It is noted thatFigure 3 shows that the tail of the Mo-signal inFigure 3 is much more pronounced than inFigure 2 as a result of the diffusion of the Mo into the nickel layer. - According to a third aspect, the invention is embodied in the use of the above corrosion resistant substrate for the production of an exhaust system or parts for an exhaust system produced from the metal substrate according to the invention. In another embodiment of the invention the metal substrate according to the invention is used in fuel lines for instance for internal combustion engines.
- The invention will now be further explained by means of the following, non-limitative examples.
- An aqueous solution was prepared consisting of 30 g/l of (NH4)6Mo7O24 (0.024 mol/l) and 50 g/l of NaH2PO4 (0.42 mol/l) with a pH of 5.5 and maintained at 60 °C. A molybdenum-oxide layer was deposited on a 2 µm matt nickel plated low-carbon steel using a current density of 20 A/dm2 and a plating time of 15 and 10 seconds. This material was then annealed in a reducing hydrogen atmosphere for 7.3 hours in a batch annealing furnace. The resulting Ni-Mo-diffusion layer has a thickness of about 150 nm at the surface of the coated substrate. These materials were subsequently tested in a salt spray test (NSS) according to ISO 9227:2012 at 5% NaCl and 35 °C and the corrosion protection for the 10 seconds plating time layer was up to 21 hrs (Ni-layer, both sides 2 µm). Also the number of pores in the Ni-Mo-diffusion layer was much reduced. The pores were determined visually on a sample which was subjected to an aqueous solution as described in the ferroxyl test in ASTM A380. The rating of samples is a qualitative rating, but quite indicative for its performance under corrosive conditions, such as in exhaust applications.
- Experiments using the conditions above result in the following linear dependence of the amount of Mo deposited on plating time (measured after annealing using Atomic Absorption Spectroscopy after dissolution of the layer of the substrate in HCl (1:1)).
Plating time A/dm2 mg (Mo) / m2 5 20 94 10 20 128 15 20 174 20 20 220 -
Figure 1 shows a non-limitative example of the implementation of the process according to the invention. The hot-rolled starting product is pickled to remove the oxides from the strip and clean the surface. After pickling the strip is cold-rolled. In the plating step the various layers are electrodeposited. In the annealing step the diffusion annealing takes place. The cold-rolling can obviously also take place elsewhere when the cold-rolled coil is bought from a supplier of cold rolled coil. -
Figure 2 shows a GDOES-measurement of the surface after depositing the molybdenum oxide on the nickel layer. The X-axis gives the thickness in nm and the Y-axis gives the concentration in wt%. Note that the values for carbon and sulphur are infact 10 times as low as presented. Clearly visible is the layer of molybdenum oxide on top of the nickel layer. The nickel layer is 2 µm (i.e. 2000 nm), whereas the molybdenum oxide layer is about 60 nm. -
Figure 3 shows a GDOES-measurement of the surface after annealing the layers ofFigure 2 . Note that the values for carbon and sulphur are infact 10 times as low as presented. The clearly discernable layer of molybdenum oxide on top of the nickel layer has vanished, and a diffusion layer comprising nickel and molybdenum is shown. There is still a degree of oxygen present in the surface layers, but this is believed to be associated with re-oxidation if the surface, and with the presence of the phosphates, and not with the molybdenum oxide which has reduced to metallic molybdenum.
Claims (15)
- A method for producing a corrosion resistant metal substrate by providing:i. a nickel or nickel-based layer on a steel or aluminium substrate, orii. a nickel or nickel-based layer on a steel or aluminium substrate followed by providing a cobalt layer on the nickel or nickel-based layer,to form a plated substrate followed by electrodepositing a molybdenum oxide layer from an aqueous solution onto the plated substrate, wherein the plated substrate acts as a cathode, wherein the aqueous solution comprises a molybdenum salt and an alkali metal phosphate and wherein the pH of the aqueous solution is adjusted to between 4.0 and 6.5, wherein the plated substrate provided with the molybdenum oxide layer is subjected to an annealing step in a reducing atmosphere to, at least partly and preferably fully, reduce the molybdenum oxide in the molybdenum oxide layer to molybdenum metal in a reduction annealing step and to form, simultaneously or subsequently, in the annealing step a diffusion layer which contains nickel and molybdenum, and optionally cobalt, wherein the nickel originates from the nickel or nickel-based layer, the cobalt originates from the optional cobalt layer, and the molybdenum originates from the molybdenum oxide layer.
- The method according to claim 1, wherein the molybdenum salt is ammonium molybdate.
- The method according to claim 1 or 2, wherein the phosphate is sodium dihydrogen phosphate.
- The method according to any one of the preceding claims, wherein the nickel or nickel-based layer provided on the substrate is between 0.5 and 5 µm in thickness, and/or wherein the diffusion layer has a thickness of between 10 and 200 nm.
- The method according to any one of the preceding claims, wherein:- the temperature of the aqueous solution for the electrodeposition of the molybdenum oxide layer onto the nickel plated steel or aluminium substrate is between 40 °C and 75 °C, and/or- the plating time for the electrodeposition of the molybdenum oxide layer onto the nickel plated steel or aluminium substrate is between 5 and 30 seconds, and/or- the current density for the electrodeposition of the molybdenum oxide layer onto the nickel plated steel or aluminium substrate is between 2 and 25 A/dm2, and/or- the maximum annealing temperature during the annealing step is between 500 and 1050 °C, and/or- the annealing time is between 6 and 10 hours for a batch annealing process and between 10 and 120 seconds for a continuous annealing process.
- The method according to any one of the preceding claims, wherein the aqueous solution for the electrodeposition of the molybdenum oxide layer onto the nickel plated steel or aluminium substrate comprises:- between 10 and 50 g/l of (NH4)6Mo7O24, and/or- between 20 and 80 g/l of NaH2PO4.
- The method according to any one of the preceding claims, wherein the aqueous solution is maintained at a temperature between 50 and 70°C and/or wherein the pH of the aqueous solution is at least 4.5 and/or at most 6.
- The method according to any one of the preceding claims, the thickness of the deposited molybdenum oxide layer is at most 50 nm.
- The method according to any one of the preceding claims, wherein the cathodic current density is at least 12.5 A/dm2 and/or at most 22.5 A/dm2.
- The method according to any one of the preceding claims, wherein the reducing atmosphere is a hydrogen containing atmosphere.
- The method according to any one of the preceding claims, wherein the substrate is a steel substrate, preferably a carbon steel, more preferably a low carbon steel.
- The method according to any one of claims 1 to 10, wherein the substrate is a ferritic stainless steel substrate.
- The method according to any one of the preceding claims, wherein the diffusion layer comprising of nickel originating from the nickel or nickel-based layer and molybdenum originating from the molybdenum oxide layer also comprises 5 to 15 wt.% of elemental phosphate.
- A corrosion resistant metal substrate provided with a diffusion layer which contains nickel and molybdenum, and optionally cobalt, on a steel or aluminium substrate, produced according to the method of any one of claims 1 to 13 wherein the diffusion layer has a thickness of between 10 and 200 nm.
- Use of the corrosion resistant metal substrate according to claim 14 for the production of an exhaust system or parts for an exhaust system or a fuel line.
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EP2016150383 | 2016-01-07 | ||
PCT/EP2017/050291 WO2017118751A1 (en) | 2016-01-07 | 2017-01-08 | Method for producing a corrosion resistant metal substrate and corrosion resistant metal substrate provided thereby |
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