US20200010946A1 - Ferrous structural component for use in fouling and corrosive environments, and method of making and using a ferrous structural component - Google Patents
Ferrous structural component for use in fouling and corrosive environments, and method of making and using a ferrous structural component Download PDFInfo
- Publication number
- US20200010946A1 US20200010946A1 US16/460,050 US201916460050A US2020010946A1 US 20200010946 A1 US20200010946 A1 US 20200010946A1 US 201916460050 A US201916460050 A US 201916460050A US 2020010946 A1 US2020010946 A1 US 2020010946A1
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- United States
- Prior art keywords
- layer
- structural component
- alloy body
- aluminized
- modified surface
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- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 title claims abstract description 55
- 238000004519 manufacturing process Methods 0.000 title description 6
- 239000010410 layer Substances 0.000 claims abstract description 84
- 238000000034 method Methods 0.000 claims abstract description 80
- 239000002344 surface layer Substances 0.000 claims abstract description 69
- 229910000640 Fe alloy Inorganic materials 0.000 claims abstract description 60
- 230000008569 process Effects 0.000 claims abstract description 52
- 239000012530 fluid Substances 0.000 claims abstract description 32
- 230000001590 oxidative effect Effects 0.000 claims abstract description 32
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims abstract description 31
- 238000005260 corrosion Methods 0.000 claims abstract description 20
- 230000007797 corrosion Effects 0.000 claims abstract description 20
- 229910021326 iron aluminide Inorganic materials 0.000 claims abstract description 15
- 229910052782 aluminium Inorganic materials 0.000 claims description 42
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 38
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 36
- 239000010959 steel Substances 0.000 claims description 26
- 229910052742 iron Inorganic materials 0.000 claims description 19
- 230000003247 decreasing effect Effects 0.000 claims description 11
- 238000010438 heat treatment Methods 0.000 claims description 10
- 238000004821 distillation Methods 0.000 claims description 8
- -1 halide salt Chemical class 0.000 claims description 8
- 229910021328 Fe2Al5 Inorganic materials 0.000 claims description 6
- 239000003921 oil Substances 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 6
- 239000003208 petroleum Substances 0.000 claims description 5
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 4
- 230000003068 static effect Effects 0.000 claims description 4
- 239000004215 Carbon black (E152) Substances 0.000 claims description 3
- 229910017372 Fe3Al Inorganic materials 0.000 claims description 3
- 229910015372 FeAl Inorganic materials 0.000 claims description 3
- 229910015370 FeAl2 Inorganic materials 0.000 claims description 3
- 229910015392 FeAl3 Inorganic materials 0.000 claims description 3
- 239000002551 biofuel Substances 0.000 claims description 3
- 229930195733 hydrocarbon Natural products 0.000 claims description 3
- 150000002430 hydrocarbons Chemical class 0.000 claims description 3
- 239000003348 petrochemical agent Substances 0.000 claims description 3
- 229910001018 Cast iron Inorganic materials 0.000 claims description 2
- 229910001208 Crucible steel Inorganic materials 0.000 claims description 2
- 229910021329 Fe4Al13 Inorganic materials 0.000 claims description 2
- 229910021327 Fe5Al8 Inorganic materials 0.000 claims description 2
- 239000003345 natural gas Substances 0.000 claims description 2
- 229910000831 Steel Inorganic materials 0.000 description 24
- 229910052799 carbon Inorganic materials 0.000 description 13
- 239000011651 chromium Substances 0.000 description 13
- 238000012360 testing method Methods 0.000 description 13
- 230000006870 function Effects 0.000 description 12
- 229910052804 chromium Inorganic materials 0.000 description 11
- 229910045601 alloy Inorganic materials 0.000 description 10
- 239000000956 alloy Substances 0.000 description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 230000008901 benefit Effects 0.000 description 7
- 238000000151 deposition Methods 0.000 description 7
- 230000008021 deposition Effects 0.000 description 7
- 238000009792 diffusion process Methods 0.000 description 7
- 238000002474 experimental method Methods 0.000 description 6
- 238000012545 processing Methods 0.000 description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 5
- 229910052786 argon Inorganic materials 0.000 description 5
- 238000007373 indentation Methods 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000000243 solution Substances 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical group N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 229910000975 Carbon steel Inorganic materials 0.000 description 4
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical group [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical group [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 4
- 230000007613 environmental effect Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 229910000041 hydrogen chloride Inorganic materials 0.000 description 4
- IXCSERBJSXMMFS-UHFFFAOYSA-N hydrogen chloride Substances Cl.Cl IXCSERBJSXMMFS-UHFFFAOYSA-N 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000001301 oxygen Chemical group 0.000 description 4
- 229910052760 oxygen Chemical group 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- 150000007944 thiolates Chemical class 0.000 description 4
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 3
- 230000015556 catabolic process Effects 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 238000003920 environmental process Methods 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 230000000116 mitigating effect Effects 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000001878 scanning electron micrograph Methods 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 230000003746 surface roughness Effects 0.000 description 3
- IMCYIKBWTTWXHH-UHFFFAOYSA-N 1-(6-pyren-1-ylsulfanylhexylsulfanyl)pyrene Chemical compound C1(=CC=C2C=CC3=CC=CC4=CC=C1C2=C34)SCCCCCCSC1=CC=C2C=CC3=CC=CC4=CC=C1C2=C34 IMCYIKBWTTWXHH-UHFFFAOYSA-N 0.000 description 2
- NLXLAEXVIDQMFP-UHFFFAOYSA-N Ammonia chloride Chemical compound [NH4+].[Cl-] NLXLAEXVIDQMFP-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- MXRIRQGCELJRSN-UHFFFAOYSA-N O.O.O.[Al] Chemical compound O.O.O.[Al] MXRIRQGCELJRSN-UHFFFAOYSA-N 0.000 description 2
- 238000002441 X-ray diffraction Methods 0.000 description 2
- 239000012190 activator Substances 0.000 description 2
- 239000008186 active pharmaceutical agent Substances 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- QRRWWGNBSQSBAM-UHFFFAOYSA-N alumane;chromium Chemical compound [AlH3].[Cr] QRRWWGNBSQSBAM-UHFFFAOYSA-N 0.000 description 2
- VSCWAEJMTAWNJL-UHFFFAOYSA-K aluminium trichloride Chemical compound Cl[Al](Cl)Cl VSCWAEJMTAWNJL-UHFFFAOYSA-K 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000002149 energy-dispersive X-ray emission spectroscopy Methods 0.000 description 2
- 238000001341 grazing-angle X-ray diffraction Methods 0.000 description 2
- 125000005842 heteroatom Chemical group 0.000 description 2
- 235000000396 iron Nutrition 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 230000036961 partial effect Effects 0.000 description 2
- 238000005498 polishing Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000002829 reductive effect Effects 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000010301 surface-oxidation reaction Methods 0.000 description 2
- 238000007725 thermal activation Methods 0.000 description 2
- 229910000619 316 stainless steel Inorganic materials 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910001141 Ductile iron Inorganic materials 0.000 description 1
- 229910017060 Fe Cr Inorganic materials 0.000 description 1
- 229910002544 Fe-Cr Inorganic materials 0.000 description 1
- MBMLMWLHJBBADN-UHFFFAOYSA-N Ferrous sulfide Chemical compound [Fe]=S MBMLMWLHJBBADN-UHFFFAOYSA-N 0.000 description 1
- 229910001060 Gray iron Inorganic materials 0.000 description 1
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910001296 Malleable iron Inorganic materials 0.000 description 1
- 239000007868 Raney catalyst Substances 0.000 description 1
- 229910000564 Raney nickel Inorganic materials 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 229910001037 White iron Inorganic materials 0.000 description 1
- UJXVAJQDLVNWPS-UHFFFAOYSA-N [Al].[Al].[Al].[Fe] Chemical compound [Al].[Al].[Al].[Fe] UJXVAJQDLVNWPS-UHFFFAOYSA-N 0.000 description 1
- DIZPMCHEQGEION-UHFFFAOYSA-H aluminium sulfate (anhydrous) Chemical compound [Al+3].[Al+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O DIZPMCHEQGEION-UHFFFAOYSA-H 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- 238000000498 ball milling Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- PBAYDYUZOSNJGU-UHFFFAOYSA-N chelidonic acid Natural products OC(=O)C1=CC(=O)C=C(C(O)=O)O1 PBAYDYUZOSNJGU-UHFFFAOYSA-N 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- UPHIPHFJVNKLMR-UHFFFAOYSA-N chromium iron Chemical compound [Cr].[Fe] UPHIPHFJVNKLMR-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010779 crude oil Substances 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000012153 distilled water Substances 0.000 description 1
- 238000009760 electrical discharge machining Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 239000013505 freshwater Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 230000035876 healing Effects 0.000 description 1
- 239000008240 homogeneous mixture Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 239000003701 inert diluent Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000001802 infusion Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000002086 nanomaterial Substances 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 1
- 238000007339 nucleophilic aromatic substitution reaction Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000002407 reforming Methods 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000000851 scanning transmission electron micrograph Methods 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
- 229910052720 vanadium Inorganic materials 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
- 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
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/28—Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
- C23C10/34—Embedding in a powder mixture, i.e. pack cementation
- C23C10/36—Embedding in a powder mixture, i.e. pack cementation only one element being diffused
- C23C10/48—Aluminising
- C23C10/50—Aluminising of ferrous surfaces
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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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/60—After-treatment
-
- 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
- C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C22/05—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
- C23C22/06—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6
- C23C22/48—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 not containing phosphates, hexavalent chromium compounds, fluorides or complex fluorides, molybdates, tungstates, vanadates or oxalates
- C23C22/56—Treatment of aluminium or alloys based thereon
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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
- C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C22/73—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process
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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
- C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C22/82—After-treatment
- C23C22/83—Chemical after-treatment
Definitions
- the present disclosure is related generally to ferrous structural components used in fouling and/or corrosive environments, and more particularly to surface modification technology to improve the fouling- and corrosion-resistance of ferrous alloys.
- Asphaltene deposition is a ubiquitous and undesirable phenomenon in the petroleum production chain. Asphaltenes are the heaviest and most surface active component within the aromatic composition group of crude oil. In addition to carbon and hydrogen, they can include heteroatoms such as sulfur, nitrogen, and oxygen. At low temperatures, asphaltenes may precipitate from process fluids and foul critical processing and refining equipment. At high temperatures, heteroatoms such as sulfur may contribute to the formation of deleterious corrosive deposits. Asphaltene precipitation on sidewalls of a pipeline can limit process fluid flow and reduce productivity. In severe cases, flow from petroleum wells may completely cease within a matter of days because of arterial clogging from asphaltene deposition.
- the modified surface includes an aluminized surface layer comprising one or more iron aluminides and a passivating layer comprising aluminum oxide on the aluminized surface layer.
- the modified surface resists corrosion and fouling as exhibited by a substantial absence of carbonaceous deposits on the iron alloy body.
- the method comprises integrating a ferrous structural component into process equipment, where the ferrous structural component comprises an iron alloy body with a modified surface.
- the modified surface includes an aluminized surface layer comprising one or more iron aluminides.
- the modified surface of the iron alloy body is exposed to an oxidative environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer.
- the modified surface of the iron alloy is also exposed to a process fluid. The exposure to the oxidative environment occurs prior to and/or upon exposure of the modified surface to the process fluid. Due to protection afforded by the passivating layer, the modified surface resists fouling and corrosion while exposed to the process fluid, as exhibited by a substantial absence of carbonaceous deposits on the iron alloy body.
- the method comprises introducing aluminum into a surface of an iron alloy body at an elevated temperature to form a modified surface of the iron alloy body, where the modified surface includes an aluminized surface layer comprising one or more iron aluminides.
- the iron alloy body comprising the modified surface is exposed to an oxidizing environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer.
- FIGS. 1A and 1B (inset image) show an exemplary ferrous structural component comprising a modified surface.
- FIG. 2A is a scanning electron microscope (SEM) image of a cross-section of an iron alloy body having a modified surface including an aluminized surface layer and an interdiffusion layer; as indicated, the iron alloy body comprises X65 steel. Indentations from nanoindentation (hardness) tests are visible in the image.
- SEM scanning electron microscope
- FIG. 2B shows a concentration profile of atomic percent (at. %) Al and Fe as a function of depth (distance from the surface) in microns as determined from an energy dispersive spectroscopy (EDS) linescan.
- EDS energy dispersive spectroscopy
- FIG. 2C identifies phases present in the aluminized surface layer as determined by grazing incidence x-ray diffraction (GIXRD).
- FIG. 3 is a schematic of an exemplary configuration for low-temperature pack aluminization with nested crucibles.
- FIG. 4 is a SEM image of a cross-section of an X65 steel sample having a modified surface as in FIG. 2A , but at a different magnification; the aluminized surface layer and the interdiffusion layer are both discernible on the X65 steel.
- FIG. 5A is a typical load versus depth plot obtained from nanoindentation experiments on cross-sections such as those shown in FIG. 2A or FIG. 4 .
- FIG. 5B shows hardness as a function of depth as determined by nanoindentation.
- FIG. 5C shows a bar plot revealing the average hardness of the aluminized surface layer and base X65 steel as determined by nanoindentation.
- FIG. 6 is a plot showing normalized mass gain for aluminized and bare (untreated) X65 steel samples.
- FIG. 7 shows a cross-sectional scanning transmission electron microscope (STEM) image taken after fouling experiments of an X65 steel sample having a modified surface, where a passivating layer comprising aluminum oxide is visible.
- STEM scanning transmission electron microscope
- FIGS. 8A-8C show cross-sectional STEM images of a pack aluminized X65 steel sample after scratching the passivating layer and then annealing, demonstrating the reformation of a thick and dense aluminum oxide layer.
- FIG. 9 shows results from corrosion tests of aluminized and untreated X65 steel samples.
- Described in this disclosure is an approach to modifying surfaces of ferrous structural components, such as oil and gas pipelines, to improve their resistance to fouling and corrosion in use. Also described are ferrous structural components having such modified surfaces, and methods of using the ferrous structural components to exploit their fouling- and corrosion-resistance in industrial and environmental processes.
- FIG. 1A is a schematic of an exemplary ferrous structural component which has undergone surface modification processing as described herein for improved performance in corrosive and/or fouling environments.
- the ferrous structural component 102 comprises an iron alloy body 104 having a modified surface 104 a , which is shown in the inset ( FIG. 1B ) to include an aluminized surface layer 106 comprising one or more iron aluminides and a passivating layer 108 on the aluminized surface layer 106 .
- the passivating layer 108 comprises aluminum oxide.
- the modified surface 104 a may also include, beneath the aluminized surface layer 106 , an interdiffusion layer 110 comprising a decreasing amount of aluminum and an increasing amount of iron in a depth direction 112 of the iron alloy body 104 .
- the depth direction 112 is shown by the arrow in FIG. 1B , and generally may be described as a direction normal to the modified surface 104 a and into the depth of the structural component 102 .
- carbonaceous deposits may refer to asphaltene deposits and/or other types of deposits (e.g., thiolate and sulfide deposits), the latter of which may be formed as a consequence of asphaltene decomposition at elevated temperatures (e.g., above 300° C.).
- substantially absence of carbonaceous deposits can be understood to mean that the iron alloy body 104 exhibits an area normalized mass gain of no greater than about 500 mg/m 2 after exposure to the process fluid for 1 hour at a temperature of 350° C. This is typically an upper bound for rough surfaces (e.g., average roughness of a few microns), where smoother surfaces may show a significantly lower mass gain. Accordingly, the phrase “substantial absence of carbonaceous deposits” may mean that the iron alloy body 104 exhibits an area normalized mass gain of no greater than about 100 mg/m 2 , or preferably no greater than about 50 mg/m 2 , after exposure to the process fluid for 1 hour at a temperature of 350° C.
- aluminum oxide-containing passivating layer 108 acts as a protective barrier, mitigating asphaltene deposition and reducing sulfidic corrosion of the ferrous structural component 102 .
- aluminum oxide has a high thermal stability and low diffusivity that can inhibit the uncontrolled formation of thiolate and sulfide deposits that commonly foul unpassivated steels.
- the modified surface 104 a of the ferrous structural component 104 may be formed in a pack bed aluminization process followed by exposure to an oxidative environment.
- the pack-bed aluminization process may be employed to modify the surface of the iron alloy body 104 (e.g., to create the aluminized surface layer 106 and the interdiffusion layer 110 ), while subsequent exposure to the oxidative environment may produce the passivating layer 108 comprising aluminum oxide. Since the pack bed aluminization process entails inert or reducing conditions, the passivating layer 108 may not be formed as a consequence of that process.
- the exposure to the oxidative environment may take place during an oxidizing heat treatment following pack bed aluminization and/or during use of the ferrous structural component 102 in an industrial or environmental process. Since the aluminized surface layer 106 is formed by diffusion of aluminum into the iron alloy body 104 and does not constitute a separate surface coating prone to delamination, the aluminized surface layer 106 may serve as a microscale aluminum “reservoir” for forming and reforming the passivating layer 108 as needed (e.g., upon damage or removal in use).
- the ferrous structural component 102 takes the form of tubing (a tube) or a pipeline; however, the size and shape of the structural component 102 are not limited by this particular example.
- the ferrous structural component 102 may comprise an expansion fitting, an orifice plate, a blind, a valve, a flange, a connector, a baffle, an agglomerator, a demister, a static mixer, a thermowell, a pitot tube, a sparger, a nozzle, a distillation or fractionating column, a component used in a distillation or fractionating column (e.g., a distillation tray or a downcomer), a heat exchanger, a component used in a heat exchanger, and/or a vessel.
- the term “iron alloy body” 104 is used without intending any limitation to the geometry or size of the ferrous structural component 102 and may be understood to refer to the mass of material that constitutes some or all of the component 102 and which includes
- the iron alloy body may comprise a ferrous alloy, such as cast iron or steel.
- the ferrous alloy may include Fe, C, and one or more other alloying elements, such as Cu, Mn, Mo, Ni, V and/or Cr.
- Exemplary steels include low alloy steels, such as low-carbon, medium-carbon, and high-carbon steels, and high alloy steels, such as tool steel (which may also be considered to be a high-carbon steel) and stainless steel, which includes at least about 11 wt. % Cr.
- Low-carbon steels typically include less than about 0.25 wt. % C; medium-carbon steels typically include between about 0.25 wt. % C and 0.60 wt. % C, and high-carbon steels typically include between about 0.60 wt.
- Exemplary cast irons include gray iron, ductile iron, white iron, and malleable iron; typically, cast irons include above about 2.1 wt. % C and may include between about 3.0 wt. % C and about 4.5 wt. % C.
- a commercially-available low-carbon steel that is investigated in this disclosure is X65 steel, which may include, in wt. %: 0.16 C, 0.45 Si, 1.65 Mn, 0.020 P, 0.010 S, 0.09 V, 0.05 Nb, and 0.06 Ti.
- the iron alloy body may comprise any of the aforementioned ferrous alloys, or others known in the art, which may benefit from enhanced corrosion- and/or fouling-resistance.
- the modified surface 104 a of the iron alloy body 104 includes an aluminized surface layer 106 comprising one or more iron aluminides, such as one or more of the following: Fe 2 Al 5 , FeAl, Fe 3 Al, Fe 5 Al 8 , FeAl 2 , FeAl 3 , and Fe 4 Al 13 . More typically, the one or more iron aluminides comprise Fe 2 Al 5 , FeAl, Fe 3 Al, FeAl 2 , and/or FeAl 3 .
- the aluminized surface layer 106 may also include an elemental iron phase, an elemental aluminum phase, and/or a solid solution phase.
- the depth to which the aluminized surface layer 106 extends may range from a few microns to tens of microns, in contrast to the passivating layer 108 , which may have a nanoscale thickness, as described below.
- the aluminized surface layer 106 may extend to a depth as large as about 10 microns, as large as about 20 microns, or as large as about 30 microns.
- the aluminized surface layer 106 extends to a depth of at least about 3 microns, at least about 5 microns, or at least about 7 microns.
- the aluminized surface layer 106 may include a decreasing amount of aluminum as a function of depth.
- the aluminized surface layer 106 may include a decreasing amount of aluminum at increasing depths into the modified surface 104 a .
- the aluminized surface layer 106 may include a substantially constant amount of aluminum as a function of depth.
- the aluminized surface layer 106 may include a substantially constant amount of aluminum at increasing depths into the modified surface. (“Substantially constant amount” may be understood to mean an amount that does not vary by more than about +/ ⁇ 15%, or by more than about +/ ⁇ 10%, from an average value.)
- the aluminized surface layer 106 may include an increasing amount of iron as a function of depth, and/or a substantially constant amount of iron as a function of depth.
- the interdiffusion layer 110 typically has a thickness (in a depth direction) in a range from about 1 micron to about 5 microns. As described above, the interdiffusion layer 110 includes a decreasing amount of aluminum and an increasing amount of iron as a function of depth. A significant rise or fall in the amount of the respective element (Fe or Al) typically occurs in the interdiffusion layer 110 . For example, a concentration change of ⁇ 50-90 wt. % may occur over a depth of just a few microns (e.g., 1-5 microns). This may be visualized with a concentration profile, as described below.
- FIG. 2A shows a scanning electron microscope (SEM) image (cross-sectional view) of an exemplary iron alloy body 104 having a modified surface 104 a .
- the iron alloy body 104 of this example is a 5 mm ⁇ 5 mm ⁇ 0.5 mm pipe steel sample comprising an X65 alloy that underwent pack aluminization as described below.
- an interdiffusion layer 110 of about 2 microns in thickness is visible between the aluminized surface layer 106 , which extends to a depth of about 7 microns, and the iron alloy body 104 .
- FIG. 2B provides a concentration profile and FIG. 2C shows an x-ray diffraction pattern obtained from the modified surface 104 b . Referring to FIG.
- the aluminized surface layer 106 of this example comprises a substantially constant amount of aluminum (about 70 wt. %) as a function of depth.
- the aluminized surface layer 106 includes a substantially constant amount of iron as a function of depth (about 30 wt. %).
- the aluminized surface layer 106 may contain an amount of aluminum in a range from about 50-90 wt. % and an amount of iron in a range from about 10-50 wt. %.
- the x-ray diffraction pattern of FIG. 2C reveals the presence of Fe 2 Al 5 and Fe in the aluminized surface layer 106 .
- the passivating layer 108 comprising aluminum oxide typically has a thickness greater than 5 nm and is continuous over an entirety of the aluminized surface layer 106 .
- the aluminum contained in the aluminized surface layer 106 may serve as a “reservoir” to regenerate the passivating layer 108 if damaged or otherwise removed, ensuring that the continuity of the passivating layer 108 can be maintained. This regeneration, if needed, may occur either in use or in a separate oxidizing heat treatment, as discussed below.
- the thickness of the passivating layer 108 may lie in the range from greater than 5 nm to about 40 nm, and is typically in the range from about 10 nm to about 30 nm.
- the passivating layer 108 exhibits a uniform thickness, with a variation in average thickness no greater than about ⁇ 10% over the layer 108 .
- the passivating layer 108 may act as a protective barrier against a corrosive environment and may mitigate the build-up of foulant from reactive species, such as sulfur and carbon; the passivating layer 108 may also prevent outward diffusion of metal species from the iron alloy body 104 .
- an aluminum sulfate layer may, in some cases, form on the passivating layer 108 in use.
- the passivating layer 108 may consist essentially of aluminum oxide, i.e., aluminum oxide and any incidental impurities only. Alternatively, the passivating layer 108 may comprise some amount of other metallic elements, such as chromium, depending on the composition of the iron alloy body 104 . However, the presence of iron is not advantageous and it is preferred that the passivating layer 108 be substantially devoid of iron. In other words, iron may not be present in the passivating layer 108 beyond parts-per-million (ppm) or incidental impurity levels.
- ppm parts-per-million
- iron aluminide phase(s) such as Fe 2 Al 5 in the aluminized surface layer 106 biases the native oxide chemistry to favor the formation of aluminum oxide (Al 2 O 3 ) instead of iron oxide (e.g., Fe 2 O 3 ).
- the aluminum oxide present in the passivating layer comprises amorphous alumina.
- Gamma ( ⁇ ) alumina is not known to be an effective diffusion barrier, and alpha ( ⁇ ) alumina may not be formed at temperatures below 1000° C., which can damage the mechanical properties of steels. Accordingly, this suggests there is a maximum temperature to which the modified surface 104 a may be exposed during processing or use (about 550° C.) to prevent the amorphous alumina, which is an effective diffusion barrier, from transforming to ⁇ alumina.
- the method comprises integrating a ferrous structural component 102 into process equipment exposed to fouling and/or corrosive process streams in use.
- the ferrous structural component 102 comprises an iron alloy body 104 with a modified surface 104 a including, as described above, an aluminized surface layer 106 comprising one or more iron aluminides.
- An interdiffusion layer 110 comprising a decreasing amount of aluminum and an increasing amount of iron in a depth direction of the iron alloy body 104 may lie beneath the aluminized surface layer 106 .
- a passivating layer 108 forms on the aluminized surface layer 106 upon exposure to an oxidative environment, which may occur prior to use of the ferrous structural component 102 and/or in use.
- the passivating layer 108 may be formed upon exposure of the aluminized surface layer 106 to an oxidizing heat treatment prior to use, or upon exposure of the modified surface to a process fluid, which may entail oxidative conditions. While a thin oxide layer may form on the aluminized surface layer 106 upon air exposure without heating, an oxidizing heat treatment is believed to be advantageous if not necessary to promote formation of a passivating layer 108 that is sufficiently thick and continuous to serve a protective function.
- the process fluid to which the modified surface 104 a of the iron alloy body 104 is exposed in use may include hydrocarbon and/or oxygenate components and/or water.
- the process fluid may comprise petroleum, natural gas, oil, one or more petrochemicals, a biofuel, and/or water (e.g., seawater, fresh water, and/or cooling water).
- the modified surface 104 a includes a passivating layer 108 comprising aluminum oxide on the aluminized surface layer 106 . Due to protection afforded by the passivating layer 108 , the modified surface 104 a resists fouling and corrosion while exposed to the process fluid, as exhibited by a substantial absence of carbonaceous deposits on the iron alloy body 104 .
- carbonaceous deposits may refer to asphaltene deposits and/or other types of deposits (e.g., thiolate and sulfide deposits), the latter of which may be formed as a consequence of asphaltene decomposition at elevated temperatures.
- substantially absence of carbonaceous deposits can be understood to mean that the iron alloy body 104 exhibits an area normalized mass gain of no greater than about 500 mg/m 2 (or no greater than about 200 mg/m 2 , or preferably no greater than about 50 mg/m 2 ) after exposure to the process fluid for 1 hour at a temperature of 350° C.
- modified surfaces 104 a exhibiting a surface roughness up to about 2.5 microns (e.g., 2.0-2.5 microns) can exhibit an area normalized mass gain of less than about 500 mg/m 2 after exposure to a process fluid (as described in the examples below) at 350° C. for 1 hour.
- the oxidative environment referred to above may be understood to be an environment in which the aluminized surface layer 106 undergoes surface oxidation to form the passivating layer 108 comprising aluminum oxide.
- the oxidative environment may comprise conditions and/or characteristics (e.g., elevated temperature, oxygenate component(s)) conducive to surface oxidation of the aluminized surface layer 106 , such that the passivating layer 108 is formed.
- An oxidizing heat treatment carried out in air or in a controlled environment (such as a furnace) at a suitable elevated temperature (e.g., from about 150° C. to about 350° C.) may provide the oxidative environment.
- exposure of the aluminized surface layer 106 to the process fluid in use in an industrial or environmental application may provide the oxidative environment.
- exposure to the process fluid may occur at an elevated temperature, such as in the range from about 150-350° C.
- the passivating layer 108 may form essentially instantaneously on the aluminized surface layer 106 upon exposure to the process fluid.
- Dissolved oxygen in the process fluid may act as a source of oxygen and the elevated temperature may accelerate oxide growth rate.
- the passivating layer 108 being formed is preferably greater than 5 nm in thickness and continuous over an entirety of the aluminized surface layer 106 to be effective in mitigating fouling and corrosion.
- the ferrous structural component 102 may be integrated into process equipment utilized in oil or gas production, oil refining, petrochemicals processing, and/or biofuels processing.
- the integration may comprise assembly and/or connection with one or more other structural components that may or may not have undergone the pack bed aluminization process.
- the ferrous structural component 102 may comprise tubing (a tube), a pipeline, an expansion fitting, an orifice plate, a blind, a valve, a flange, a connector, a baffle, an agglomerator, a demister, a static mixer, a thermowell, a pitot tube, a sparger, a nozzle, a distillation or fractionation column, a component used in a distillation or fractionating column (e.g., a distillation tray or a downcomer), a heat exchanger, a component used in a heat exchanger, and/or a vessel, for example.
- the method includes introducing aluminum into a surface of an iron alloy body at an elevated temperature to form a modified surface of the iron alloy body.
- the introduction of aluminum into the surface may be referred to as aluminization.
- the modified surface includes, as described above, an aluminized surface layer comprising one or more iron aluminides.
- An interdiffusion layer including a decreasing amount of aluminum and an increasing amount of iron in a depth direction of the iron alloy body may also be formed beneath the aluminized surface layer.
- the aluminum is introduced into the surface under inert or reducing conditions, and thus a passivating layer may not be formed during aluminization. After aluminization, the iron alloy body is exposed to an oxidative environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer.
- the exposure to the oxidative environment may occur while the ferrous structural component is in use, such as while the iron alloy body is in contact with a process fluid.
- the exposure to the oxidative environment may occur prior to use, such as during exposure to an oxidizing heat treatment following the formation of the aluminized surface layer.
- the method may entail introducing chromium instead of or in addition to aluminum into the surface, in which case the aluminized surface layer 106 may comprise iron and chromium instead of or in addition to aluminum.
- the aluminum and/or chromium may be introduced into the surface of the iron alloy body 104 via pack aluminization (or chromization) using a pack comprising an aluminum source (a chromium source), a halide salt, and aluminum oxide.
- Pack aluminization (or chromization) may be described as a halide salt activated chemical vapor deposition process in which a structural component of any size or geometry is embedded in a powder-based pack and surface-treated with aluminum (or chromium) through thermal activation.
- Pack aluminization may create a chemical gradient as a function of depth into the surface, with decreasing Al (or Cr) concentration in a depth direction of the iron alloy body (i.e., in a direction away from the surface).
- the chemical profile may be modified by altering the aluminization (chromization) conditions or by post-aluminization (chromization) annealing or heat treatment steps in inert or oxidizing conditions. Aluminization and chromization can be done simultaneously or sequentially to produce the aluminized surface layer 106 described above.
- the pack 330 and the ferrous structural component 340 to be aluminized (chromized) may be placed in a controlled environment 350 , such as in a crucible with a gas-tight seal or in a semi-open crucible placed in a furnace under vacuum conditions or inert gas (e.g., He, Ar, or N 2 ) flow.
- a reducing environment such as a forming gas flow (e.g., N 2 or Ar+H 2 ) may be employed.
- the controlled environment may comprise an environmental control furnace under gettered argon ( ⁇ 10 ⁇ 12 partial pressure of O 2 ).
- the argon may be maintained at a pressure of 1 atm and continuously purged at a flow rate in a range of 0.5-2 L/min.
- the controlled environment is substantially devoid of oxygen.
- the introduction of the aluminum (chromium) may be carried out at an elevated temperature in a range from 500° C. to 1000° C., and preferably below 900° C. to avoid having a detrimental impact on the mechanical properties of the ferrous structural component 102 .
- the elevated temperature may lie in the range from about 550° C. to about 900° C.
- pack aluminization of alloy steels including 13 wt. % Cr (“13 Cr alloys”) may be carried out at an elevated temperature of about 900° C. or less
- pack aluminization of X65 steels may be carried out at an elevated temperature of 600° C. or less.
- the elevated temperature at which aluminization (chromization) takes place may be understood to be the temperature attained by the ferrous metal component during processing.
- the elevated temperature may be maintained for 12 hours or less, for 6 hours or less, or for 3 hours or less, and typically for at least one hour to achieve aluminization (chromization).
- the aluminum source may comprise an aluminum alloy including from 50% to 99% aluminum or pure aluminum including only incidental impurities.
- the chromium source may comprise chromium (e.g., 99.5% purity).
- the halide salt may comprise NH 4 Cl or AlCl 3 , for example.
- the halide salt may serve as an activator and the aluminum oxide may act as an inert diluent. All three ingredients may take the form of a powder that can be tumbled together to form a mixture that serves as the pack. For example, the powder may be ball milled for 24-48 hours to ensure a homogeneous mixture.
- the pack may comprise the aluminum (or chromium) source at a concentration from about 5 wt.
- the relative amounts of the pack ingredients are selected so that the pack has a sufficiently high aluminum (chromium) activity to be effective at the lower temperatures desired to preserve the mechanical properties of the iron alloy body and minimize grain growth.
- low-temperature pack aluminization is applied to samples comprising API 5L X65, a high strength pipe steel that is low in alloying elements.
- BPH 1,6-bis(pyren-1-ylthio)hexane
- the ferrous alloy utilized for this study is API 5L X65.
- EDM electrical discharge machining
- the coupons After being machined down to 5 mm ⁇ 5 mm ⁇ 0.5 mm size by electrical discharge machining (EDM), the coupons are brought to a level but stochastic finish ( ⁇ 20 nm RMS roughness) by grinding with silicon carbide papers up to 1200 grit followed by polishing with a 1 ⁇ m neutral alumina solution. While the aluminization process increases the original surface roughness of the polished X65 specimens ( ⁇ 180 nm RMS roughness), the benefits of reduced asphaltene fouling are realized (see below) due to the presence of the passivating layer.
- the pack used for the aluminization process includes three ingredients: 82 wt. % inert Al 2 O 3 powder [Baikowski/US Research Nanomaterials, 99.9% pure], 3 wt. % NH 4 Cl activator [Alfa Aesar, 99.999% pure], and a 15 wt. % Raney-nickel aluminum source [Ni-50 wt. % Al, Acros, 99.99% pure].
- the relative amounts of the ingredients are selected to ensure that the pack has a sufficiently high aluminum activity to work at the lower temperatures desired to minimize grain growth and preserve the base mechanical properties of the steel.
- the X65 samples 340 are embedded in the pack 330 , as shown in FIG. 3 , and placed in an environmental control furnace 350 under 1 atmosphere of gettered argon (10 ⁇ 12 partial pressure of O 2 ) that was continuously purged at a flow rate of 1 L/min.
- gettered argon (10 ⁇ 12 partial pressure of O 2 ) that was continuously purged at a flow rate of 1 L/min.
- the embedded samples are heated to 600° C. at a ramp rate of 20° C./min and held at this temperature for 6 hrs.
- Several 5 mm ⁇ 5 mm ⁇ 0.5 mm X65 pipe steel coupons 340 are aluminized, as illustrated in FIG. 3 .
- the samples 340 are then cooled under argon for an hour, followed by a nitrogen purge until they reach room temperature.
- the model asphaltene used in this study is 1,6-bis(pyren-1-ylthio)hexane, referred to as BPH.
- BPH 1,6-bis(pyren-1-ylthio)hexane
- the BPH is synthesized through a nucleophilic aromatic substitution reaction.
- an autoclave [60 ml EZE Seal Pressure Vessel, Parker Hannifin] made from 316 stainless steel is used.
- the steel coupons are fully submerged in 5 mL of the model asphaltene solution before being air-sealed and then heated from room temperature at a rate of 10° C./min. Once the furnace reaches its final temperature of 350° C., the temperature is held for 1 hour before the furnace is naturally cooled to room temperature.
- the coupons are removed and rinsed with 1 mL of petroleum ether to remove loosely adhered deposits.
- the mass gain of the coupons is measured using a microbalance [XPE26, Mettler-Toledo] after the fouling test.
- the hardness of the aluminized coupons is measured along the depth of the cross-sectional samples using a nanoindentation system [Hysitron TI 950 Tribolndenter, Bruker Corporation] with a diamond Berkovich tip. All indentation tests are made to a maximum depth of 100 nm with a constant rate of 10 nm/s. The obtained load-displacement data are analyzed using the Oliver-Pharr method to calculate the hardness.
- Corrosion tests are performed by immersing X65 samples in a fixed pH ( ⁇ 3) HCl solution at room temperature.
- the HCl solution is composed of 1.0 M HCl and distilled water in the appropriate proportions.
- the solution is monitored daily to keep the pH value relatively constant throughout the test.
- the mass of the samples is measured every three days using a microbalance.
- the total area normalized mass loss of specimens is calculated and compared to the original mass before immersion.
- the modified surface 104 a includes an aluminized surface layer 106 overlying a smaller interdiffusion layer 110 . Beneath the interdiffusion layer 110 is the base X65 alloy, which is not altered by the aluminization.
- FIGS. 5A-5C Results from nanoindentation tests carried out on the cross-sections of aluminized X65 steel samples as described above are shown in FIGS. 5A-5C , where indentations from the tests are visible in FIG. 2A .
- the hardness of the aluminized top layer and the X65 substrate beneath is evaluated from the indentation load-depth curves.
- FIG. 5A shows the typical load-depth curves for the indents made in the aluminized surface layer and in the base X65 alloy.
- the aluminized surface lay has a much higher maximum indentation load, thus a higher hardness compared to the base X65.
- the variation of hardness as a function of depth is shown in FIG.
- the aluminized surface layer is significantly harder than both the interdiffusion layer and the base X65 alloy.
- the average hardness of the aluminized surface is 8.77 ⁇ 1.66 GPa, and it drops to 3.22 ⁇ 0.15 GPa in the base X65 region, as shown in FIG. 5C .
- the hardness data as a function of depth correlate well with the concentration profile data, discussed above and shown in FIG. 2B . Combined, these data confirm the formation of an aluminized surface layer including one or more iron aluminides.
- the high hardness in the aluminized surface layer suggests that Fe 2 Al 5 , the hardest intermetallic phase formed among Fe—Al compounds, may be present.
- Results from fouling experiments conducted on aluminized and untreated (bare) X65 coupons at 350° C. as described above are presented in FIG. 6 as area normalized mass gain.
- the difference in mass gain between the aluminized and bare X65 samples is significant.
- the average amount of deposition measured for the bare X65 samples is nearly 3000 mg/m 2 (2914 mg/m 2 ), while negligible mass gain is observed for the aluminized X65 sample.
- Optical images reveal large and numerous carbonaceous deposits on the bare X65 samples, while there is no significant foulant build-up on the aluminized X65 samples.
- FIG. 7 A detailed cross-sectional scanning transmission electron microscope (STEM) image of an aluminized X65 steel surface after fouling is shown in FIG. 7 .
- the STEM data reveal a dense and continuous film of Al 2 O 3 with a thickness of ⁇ 10 nm.
- the results show that during the fouling experiment, the existing thin Al 2 O 3 layer grows thicker.
- the alumina layer prevents the formation of thiolate species and iron sulfide at the surface.
- the passivating layer also mitigates the diffusion of other metallic species from the X65 substrate. Therefore, the aluminized surface shows no significant mass gain from the fouling deposits, in contrast to the bare X65 coupons.
- the aluminum diffuses into the X65 steel and establishes an aluminum reservoir for the formation and healing of the passivating layer, as described above.
- the aluminized surface layer undergoes polishing to remove the existing passivating layer.
- a nanoindenter scratch test is then performed along a 100 ⁇ m line with a continuously increasing load from zero to the maximal load of 150 mN in order to determine the desired depth of penetration.
- a few scratches are made at a constant load of 50 mN and a depth of ⁇ 500 nm (0.5 micron). After introducing the scratches, the sample is annealed in air at 350° C.
- FIG. 8A An STEM cross-sectional image of a representative scratch is shown in FIG. 8A .
- the high magnification images confirm the reformation of a ⁇ 10 nm thick and uniform oxide layer both at the side and tip of the scratch ( FIGS. 8B and 8C ).
- the results show that if the passivating oxide layer on the iron alloy body is damaged within the aluminized region, it can be reformed continuously from the Al reservoir.
- FIG. 9 A summary of the results of the corrosion tests is shown in FIG. 9 , where it can be observed that the average mass loss after 30 days is higher for the bare X65 sample than for the aluminized X65 sample. This indicates increased corrosion resistance for the aluminized X65 sample.
- an aluminum oxide layer may form immediately upon air exposure; this oxide layer may be very thin and discontinuous. However, exposure to higher temperatures can rapidly help it grow thick and continuous to form the passivating layer 108 , which provides protection against corrosion and deposition.
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Abstract
Description
- The present patent document claims the benefit of priority under 35 U.S.C. § 119(e) to U.S. Provisional Patent Application Ser. No. 62/694,198, filed on Jul. 5, 2018, and to U.S. Provisional Patent Application Ser. No. 62/695,353, filed on Jul. 9, 2018, both of which are hereby incorporated by reference in their entirety.
- The present disclosure is related generally to ferrous structural components used in fouling and/or corrosive environments, and more particularly to surface modification technology to improve the fouling- and corrosion-resistance of ferrous alloys.
- Degradation of structural surfaces via a variety of corrosion or fouling mechanisms in industrial and environmental process streams is a pressing challenge. Such degradation may lead to reduced efficiency or component failure. However, the complexity of the process conditions (temperature, pressure, chemistry, flow) has encumbered a comprehensive description of possible degradation mechanisms, thereby limiting the effectiveness of existing mitigation strategies.
- Asphaltene deposition is a ubiquitous and undesirable phenomenon in the petroleum production chain. Asphaltenes are the heaviest and most surface active component within the aromatic composition group of crude oil. In addition to carbon and hydrogen, they can include heteroatoms such as sulfur, nitrogen, and oxygen. At low temperatures, asphaltenes may precipitate from process fluids and foul critical processing and refining equipment. At high temperatures, heteroatoms such as sulfur may contribute to the formation of deleterious corrosive deposits. Asphaltene precipitation on sidewalls of a pipeline can limit process fluid flow and reduce productivity. In severe cases, flow from petroleum wells may completely cease within a matter of days because of arterial clogging from asphaltene deposition.
- A ferrous structural component for use in fouling and/or corrosive environments is described. The ferrous structural component comprises an iron alloy body having a modified surface. The modified surface includes an aluminized surface layer comprising one or more iron aluminides and a passivating layer comprising aluminum oxide on the aluminized surface layer. When in direct contact with a process fluid, the modified surface resists corrosion and fouling as exhibited by a substantial absence of carbonaceous deposits on the iron alloy body.
- Also described is a method of using a ferrous structural component with enhanced fouling- and corrosion-resistance. The method comprises integrating a ferrous structural component into process equipment, where the ferrous structural component comprises an iron alloy body with a modified surface. The modified surface includes an aluminized surface layer comprising one or more iron aluminides. The modified surface of the iron alloy body is exposed to an oxidative environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer. The modified surface of the iron alloy is also exposed to a process fluid. The exposure to the oxidative environment occurs prior to and/or upon exposure of the modified surface to the process fluid. Due to protection afforded by the passivating layer, the modified surface resists fouling and corrosion while exposed to the process fluid, as exhibited by a substantial absence of carbonaceous deposits on the iron alloy body.
- Finally, a method of imparting fouling- and corrosion-resistance to a ferrous structural component is described. The method comprises introducing aluminum into a surface of an iron alloy body at an elevated temperature to form a modified surface of the iron alloy body, where the modified surface includes an aluminized surface layer comprising one or more iron aluminides. The iron alloy body comprising the modified surface is exposed to an oxidizing environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer.
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FIGS. 1A and 1B (inset image) show an exemplary ferrous structural component comprising a modified surface. -
FIG. 2A is a scanning electron microscope (SEM) image of a cross-section of an iron alloy body having a modified surface including an aluminized surface layer and an interdiffusion layer; as indicated, the iron alloy body comprises X65 steel. Indentations from nanoindentation (hardness) tests are visible in the image. -
FIG. 2B shows a concentration profile of atomic percent (at. %) Al and Fe as a function of depth (distance from the surface) in microns as determined from an energy dispersive spectroscopy (EDS) linescan. -
FIG. 2C identifies phases present in the aluminized surface layer as determined by grazing incidence x-ray diffraction (GIXRD). -
FIG. 3 is a schematic of an exemplary configuration for low-temperature pack aluminization with nested crucibles. -
FIG. 4 is a SEM image of a cross-section of an X65 steel sample having a modified surface as inFIG. 2A , but at a different magnification; the aluminized surface layer and the interdiffusion layer are both discernible on the X65 steel. -
FIG. 5A is a typical load versus depth plot obtained from nanoindentation experiments on cross-sections such as those shown inFIG. 2A orFIG. 4 . -
FIG. 5B shows hardness as a function of depth as determined by nanoindentation. -
FIG. 5C shows a bar plot revealing the average hardness of the aluminized surface layer and base X65 steel as determined by nanoindentation. -
FIG. 6 is a plot showing normalized mass gain for aluminized and bare (untreated) X65 steel samples. -
FIG. 7 shows a cross-sectional scanning transmission electron microscope (STEM) image taken after fouling experiments of an X65 steel sample having a modified surface, where a passivating layer comprising aluminum oxide is visible. -
FIGS. 8A-8C show cross-sectional STEM images of a pack aluminized X65 steel sample after scratching the passivating layer and then annealing, demonstrating the reformation of a thick and dense aluminum oxide layer. -
FIG. 9 shows results from corrosion tests of aluminized and untreated X65 steel samples. - Described in this disclosure is an approach to modifying surfaces of ferrous structural components, such as oil and gas pipelines, to improve their resistance to fouling and corrosion in use. Also described are ferrous structural components having such modified surfaces, and methods of using the ferrous structural components to exploit their fouling- and corrosion-resistance in industrial and environmental processes.
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FIG. 1A is a schematic of an exemplary ferrous structural component which has undergone surface modification processing as described herein for improved performance in corrosive and/or fouling environments. The ferrousstructural component 102 comprises aniron alloy body 104 having a modifiedsurface 104 a, which is shown in the inset (FIG. 1B ) to include analuminized surface layer 106 comprising one or more iron aluminides and apassivating layer 108 on thealuminized surface layer 106. Thepassivating layer 108 comprises aluminum oxide. The modifiedsurface 104 a may also include, beneath the aluminizedsurface layer 106, aninterdiffusion layer 110 comprising a decreasing amount of aluminum and an increasing amount of iron in adepth direction 112 of theiron alloy body 104. Thedepth direction 112 is shown by the arrow inFIG. 1B , and generally may be described as a direction normal to the modifiedsurface 104 a and into the depth of thestructural component 102. - When in direct contact with a process fluid, which may comprise hydrocarbon and/or oxygenate components and/or water, the modified
surface 104 a resists fouling and corrosion—as exhibited by a substantial absence of carbonaceous deposits on theiron alloy body 104. The term “carbonaceous deposits” may refer to asphaltene deposits and/or other types of deposits (e.g., thiolate and sulfide deposits), the latter of which may be formed as a consequence of asphaltene decomposition at elevated temperatures (e.g., above 300° C.). The phrase “substantial absence of carbonaceous deposits” can be understood to mean that theiron alloy body 104 exhibits an area normalized mass gain of no greater than about 500 mg/m2 after exposure to the process fluid for 1 hour at a temperature of 350° C. This is typically an upper bound for rough surfaces (e.g., average roughness of a few microns), where smoother surfaces may show a significantly lower mass gain. Accordingly, the phrase “substantial absence of carbonaceous deposits” may mean that theiron alloy body 104 exhibits an area normalized mass gain of no greater than about 100 mg/m2, or preferably no greater than about 50 mg/m2, after exposure to the process fluid for 1 hour at a temperature of 350° C. This enhanced resistance to fouling and corrosion can be attributed to the presence of the aluminum oxide-containingpassivating layer 108, which acts as a protective barrier, mitigating asphaltene deposition and reducing sulfidic corrosion of the ferrousstructural component 102. Advantageously, aluminum oxide has a high thermal stability and low diffusivity that can inhibit the uncontrolled formation of thiolate and sulfide deposits that commonly foul unpassivated steels. - The modified
surface 104 a of the ferrousstructural component 104 may be formed in a pack bed aluminization process followed by exposure to an oxidative environment. As described below, the pack-bed aluminization process may be employed to modify the surface of the iron alloy body 104 (e.g., to create the aluminizedsurface layer 106 and the interdiffusion layer 110), while subsequent exposure to the oxidative environment may produce thepassivating layer 108 comprising aluminum oxide. Since the pack bed aluminization process entails inert or reducing conditions, thepassivating layer 108 may not be formed as a consequence of that process. The exposure to the oxidative environment may take place during an oxidizing heat treatment following pack bed aluminization and/or during use of the ferrousstructural component 102 in an industrial or environmental process. Since the aluminizedsurface layer 106 is formed by diffusion of aluminum into theiron alloy body 104 and does not constitute a separate surface coating prone to delamination, the aluminizedsurface layer 106 may serve as a microscale aluminum “reservoir” for forming and reforming thepassivating layer 108 as needed (e.g., upon damage or removal in use). - In the schematic of
FIG. 1A , the ferrousstructural component 102 takes the form of tubing (a tube) or a pipeline; however, the size and shape of thestructural component 102 are not limited by this particular example. In other examples, the ferrousstructural component 102 may comprise an expansion fitting, an orifice plate, a blind, a valve, a flange, a connector, a baffle, an agglomerator, a demister, a static mixer, a thermowell, a pitot tube, a sparger, a nozzle, a distillation or fractionating column, a component used in a distillation or fractionating column (e.g., a distillation tray or a downcomer), a heat exchanger, a component used in a heat exchanger, and/or a vessel. The term “iron alloy body” 104 is used without intending any limitation to the geometry or size of the ferrousstructural component 102 and may be understood to refer to the mass of material that constitutes some or all of thecomponent 102 and which includes the modifiedsurface 104 a. - The iron alloy body may comprise a ferrous alloy, such as cast iron or steel. The ferrous alloy may include Fe, C, and one or more other alloying elements, such as Cu, Mn, Mo, Ni, V and/or Cr. Exemplary steels include low alloy steels, such as low-carbon, medium-carbon, and high-carbon steels, and high alloy steels, such as tool steel (which may also be considered to be a high-carbon steel) and stainless steel, which includes at least about 11 wt. % Cr. Low-carbon steels typically include less than about 0.25 wt. % C; medium-carbon steels typically include between about 0.25 wt. % C and 0.60 wt. % C, and high-carbon steels typically include between about 0.60 wt. % C and about 1.4 wt. % C. Exemplary cast irons include gray iron, ductile iron, white iron, and malleable iron; typically, cast irons include above about 2.1 wt. % C and may include between about 3.0 wt. % C and about 4.5 wt. % C. A commercially-available low-carbon steel that is investigated in this disclosure is X65 steel, which may include, in wt. %: 0.16 C, 0.45 Si, 1.65 Mn, 0.020 P, 0.010 S, 0.09 V, 0.05 Nb, and 0.06 Ti. The iron alloy body may comprise any of the aforementioned ferrous alloys, or others known in the art, which may benefit from enhanced corrosion- and/or fouling-resistance.
- The modified
surface 104 a of theiron alloy body 104 is now described. As indicated above, the modifiedsurface 104 a includes an aluminizedsurface layer 106 comprising one or more iron aluminides, such as one or more of the following: Fe2Al5, FeAl, Fe3Al, Fe5Al8, FeAl2, FeAl3, and Fe4Al13. More typically, the one or more iron aluminides comprise Fe2Al5, FeAl, Fe3Al, FeAl2, and/or FeAl3. The aluminizedsurface layer 106 may also include an elemental iron phase, an elemental aluminum phase, and/or a solid solution phase. The depth to which the aluminizedsurface layer 106 extends may range from a few microns to tens of microns, in contrast to thepassivating layer 108, which may have a nanoscale thickness, as described below. For example, depending on the process conditions, the aluminizedsurface layer 106 may extend to a depth as large as about 10 microns, as large as about 20 microns, or as large as about 30 microns. Typically, the aluminizedsurface layer 106 extends to a depth of at least about 3 microns, at least about 5 microns, or at least about 7 microns. The aluminizedsurface layer 106 may include a decreasing amount of aluminum as a function of depth. In other words, the aluminizedsurface layer 106 may include a decreasing amount of aluminum at increasing depths into the modifiedsurface 104 a. Also or alternatively, the aluminizedsurface layer 106 may include a substantially constant amount of aluminum as a function of depth. In other words, the aluminizedsurface layer 106 may include a substantially constant amount of aluminum at increasing depths into the modified surface. (“Substantially constant amount” may be understood to mean an amount that does not vary by more than about +/−15%, or by more than about +/−10%, from an average value.) Similarly, the aluminizedsurface layer 106 may include an increasing amount of iron as a function of depth, and/or a substantially constant amount of iron as a function of depth. - The
interdiffusion layer 110 typically has a thickness (in a depth direction) in a range from about 1 micron to about 5 microns. As described above, theinterdiffusion layer 110 includes a decreasing amount of aluminum and an increasing amount of iron as a function of depth. A significant rise or fall in the amount of the respective element (Fe or Al) typically occurs in theinterdiffusion layer 110. For example, a concentration change of ±50-90 wt. % may occur over a depth of just a few microns (e.g., 1-5 microns). This may be visualized with a concentration profile, as described below. -
FIG. 2A shows a scanning electron microscope (SEM) image (cross-sectional view) of an exemplaryiron alloy body 104 having a modifiedsurface 104 a. Theiron alloy body 104 of this example is a 5 mm×5 mm×0.5 mm pipe steel sample comprising an X65 alloy that underwent pack aluminization as described below. Referring to the SEM image, aninterdiffusion layer 110 of about 2 microns in thickness is visible between thealuminized surface layer 106, which extends to a depth of about 7 microns, and theiron alloy body 104.FIG. 2B provides a concentration profile andFIG. 2C shows an x-ray diffraction pattern obtained from the modified surface 104 b. Referring toFIG. 2B , the aluminizedsurface layer 106 of this example comprises a substantially constant amount of aluminum (about 70 wt. %) as a function of depth. Similarly, the aluminizedsurface layer 106 includes a substantially constant amount of iron as a function of depth (about 30 wt. %). Depending on the process conditions, the aluminizedsurface layer 106 may contain an amount of aluminum in a range from about 50-90 wt. % and an amount of iron in a range from about 10-50 wt. %. The x-ray diffraction pattern ofFIG. 2C reveals the presence of Fe2Al5 and Fe in the aluminizedsurface layer 106. - To be effective in inhibiting corrosion and fouling, the
passivating layer 108 comprising aluminum oxide typically has a thickness greater than 5 nm and is continuous over an entirety of the aluminizedsurface layer 106. As indicated above, the aluminum contained in the aluminizedsurface layer 106 may serve as a “reservoir” to regenerate thepassivating layer 108 if damaged or otherwise removed, ensuring that the continuity of thepassivating layer 108 can be maintained. This regeneration, if needed, may occur either in use or in a separate oxidizing heat treatment, as discussed below. The thickness of thepassivating layer 108 may lie in the range from greater than 5 nm to about 40 nm, and is typically in the range from about 10 nm to about 30 nm. Ideally thepassivating layer 108 exhibits a uniform thickness, with a variation in average thickness no greater than about ±10% over thelayer 108. Thepassivating layer 108 may act as a protective barrier against a corrosive environment and may mitigate the build-up of foulant from reactive species, such as sulfur and carbon; thepassivating layer 108 may also prevent outward diffusion of metal species from theiron alloy body 104. In addition, there is evidence that an aluminum sulfate layer may, in some cases, form on thepassivating layer 108 in use. - The
passivating layer 108 may consist essentially of aluminum oxide, i.e., aluminum oxide and any incidental impurities only. Alternatively, thepassivating layer 108 may comprise some amount of other metallic elements, such as chromium, depending on the composition of theiron alloy body 104. However, the presence of iron is not advantageous and it is preferred that thepassivating layer 108 be substantially devoid of iron. In other words, iron may not be present in thepassivating layer 108 beyond parts-per-million (ppm) or incidental impurity levels. It is believed that the presence of iron aluminide phase(s) such as Fe2Al5 in the aluminizedsurface layer 106 biases the native oxide chemistry to favor the formation of aluminum oxide (Al2O3) instead of iron oxide (e.g., Fe2O3). It is believed that the aluminum oxide present in the passivating layer comprises amorphous alumina. Gamma (γ) alumina is not known to be an effective diffusion barrier, and alpha (α) alumina may not be formed at temperatures below 1000° C., which can damage the mechanical properties of steels. Accordingly, this suggests there is a maximum temperature to which the modifiedsurface 104 a may be exposed during processing or use (about 550° C.) to prevent the amorphous alumina, which is an effective diffusion barrier, from transforming to γ alumina. - Also described in this disclosure is a method of using the ferrous
structural component 102 in industrial or environmental applications which may benefit from resistance to fouling and corrosion. The method comprises integrating a ferrousstructural component 102 into process equipment exposed to fouling and/or corrosive process streams in use. The ferrousstructural component 102 comprises aniron alloy body 104 with a modifiedsurface 104 a including, as described above, analuminized surface layer 106 comprising one or more iron aluminides. Aninterdiffusion layer 110 comprising a decreasing amount of aluminum and an increasing amount of iron in a depth direction of theiron alloy body 104 may lie beneath the aluminizedsurface layer 106. Apassivating layer 108 forms on the aluminizedsurface layer 106 upon exposure to an oxidative environment, which may occur prior to use of the ferrousstructural component 102 and/or in use. For example, thepassivating layer 108 may be formed upon exposure of the aluminizedsurface layer 106 to an oxidizing heat treatment prior to use, or upon exposure of the modified surface to a process fluid, which may entail oxidative conditions. While a thin oxide layer may form on the aluminizedsurface layer 106 upon air exposure without heating, an oxidizing heat treatment is believed to be advantageous if not necessary to promote formation of apassivating layer 108 that is sufficiently thick and continuous to serve a protective function. - The process fluid to which the modified
surface 104 a of theiron alloy body 104 is exposed in use may include hydrocarbon and/or oxygenate components and/or water. For example, the process fluid may comprise petroleum, natural gas, oil, one or more petrochemicals, a biofuel, and/or water (e.g., seawater, fresh water, and/or cooling water). As explained above, the modifiedsurface 104 a includes apassivating layer 108 comprising aluminum oxide on the aluminizedsurface layer 106. Due to protection afforded by thepassivating layer 108, the modifiedsurface 104 a resists fouling and corrosion while exposed to the process fluid, as exhibited by a substantial absence of carbonaceous deposits on theiron alloy body 104. As described above, the term “carbonaceous deposits” may refer to asphaltene deposits and/or other types of deposits (e.g., thiolate and sulfide deposits), the latter of which may be formed as a consequence of asphaltene decomposition at elevated temperatures. The phrase “substantial absence of carbonaceous deposits” can be understood to mean that theiron alloy body 104 exhibits an area normalized mass gain of no greater than about 500 mg/m2 (or no greater than about 200 mg/m2, or preferably no greater than about 50 mg/m2) after exposure to the process fluid for 1 hour at a temperature of 350° C. - It is known that rough surfaces can provide physical entrapment sites for foulants in hydrodynamic environments. In fact, improving surface finish to reduce foulant deposition is a strategy employed in the oil and gas industry. Thus, it is notable that the protection afforded by the
passivating layer 108 reduces the negative impact of surface roughness on foulant deposition. For example, even modifiedsurfaces 104 a exhibiting a surface roughness up to about 2.5 microns (e.g., 2.0-2.5 microns) can exhibit an area normalized mass gain of less than about 500 mg/m2 after exposure to a process fluid (as described in the examples below) at 350° C. for 1 hour. - The oxidative environment referred to above may be understood to be an environment in which the aluminized
surface layer 106 undergoes surface oxidation to form thepassivating layer 108 comprising aluminum oxide. In other words, the oxidative environment may comprise conditions and/or characteristics (e.g., elevated temperature, oxygenate component(s)) conducive to surface oxidation of the aluminizedsurface layer 106, such that thepassivating layer 108 is formed. An oxidizing heat treatment carried out in air or in a controlled environment (such as a furnace) at a suitable elevated temperature (e.g., from about 150° C. to about 350° C.) may provide the oxidative environment. Also or alternatively, exposure of the aluminizedsurface layer 106 to the process fluid in use in an industrial or environmental application may provide the oxidative environment. For example, exposure to the process fluid may occur at an elevated temperature, such as in the range from about 150-350° C. In such a situation, thepassivating layer 108 may form essentially instantaneously on the aluminizedsurface layer 106 upon exposure to the process fluid. Dissolved oxygen in the process fluid may act as a source of oxygen and the elevated temperature may accelerate oxide growth rate. It is understood that thepassivating layer 108 being formed is preferably greater than 5 nm in thickness and continuous over an entirety of the aluminizedsurface layer 106 to be effective in mitigating fouling and corrosion. - The ferrous
structural component 102 may be integrated into process equipment utilized in oil or gas production, oil refining, petrochemicals processing, and/or biofuels processing. The integration may comprise assembly and/or connection with one or more other structural components that may or may not have undergone the pack bed aluminization process. As described above, the ferrousstructural component 102 may comprise tubing (a tube), a pipeline, an expansion fitting, an orifice plate, a blind, a valve, a flange, a connector, a baffle, an agglomerator, a demister, a static mixer, a thermowell, a pitot tube, a sparger, a nozzle, a distillation or fractionation column, a component used in a distillation or fractionating column (e.g., a distillation tray or a downcomer), a heat exchanger, a component used in a heat exchanger, and/or a vessel, for example. - A method of imparting fouling- and corrosion-resistance to a ferrous structural component is now described. The method includes introducing aluminum into a surface of an iron alloy body at an elevated temperature to form a modified surface of the iron alloy body. The introduction of aluminum into the surface may be referred to as aluminization. The modified surface includes, as described above, an aluminized surface layer comprising one or more iron aluminides. An interdiffusion layer including a decreasing amount of aluminum and an increasing amount of iron in a depth direction of the iron alloy body may also be formed beneath the aluminized surface layer. The aluminum is introduced into the surface under inert or reducing conditions, and thus a passivating layer may not be formed during aluminization. After aluminization, the iron alloy body is exposed to an oxidative environment, thereby forming, as part of the modified surface, a passivating layer comprising aluminum oxide on the aluminized surface layer.
- The exposure to the oxidative environment may occur while the ferrous structural component is in use, such as while the iron alloy body is in contact with a process fluid. Alternatively, the exposure to the oxidative environment may occur prior to use, such as during exposure to an oxidizing heat treatment following the formation of the aluminized surface layer.
- It is also contemplated that the method may entail introducing chromium instead of or in addition to aluminum into the surface, in which case the aluminized
surface layer 106 may comprise iron and chromium instead of or in addition to aluminum. The aluminum and/or chromium may be introduced into the surface of theiron alloy body 104 via pack aluminization (or chromization) using a pack comprising an aluminum source (a chromium source), a halide salt, and aluminum oxide. Pack aluminization (or chromization) may be described as a halide salt activated chemical vapor deposition process in which a structural component of any size or geometry is embedded in a powder-based pack and surface-treated with aluminum (or chromium) through thermal activation. Two processes may occur simultaneously during thermal activation: (1) the formation of aluminum (chromium) halide vapors and their infusion into the surface of the iron alloy body; and (2) their reduction at the surface to form a Fe—Al (Fe—Cr) diffusion couple and the consequent interdiffusion process. Pack aluminization (chromization) may create a chemical gradient as a function of depth into the surface, with decreasing Al (or Cr) concentration in a depth direction of the iron alloy body (i.e., in a direction away from the surface). The chemical profile may be modified by altering the aluminization (chromization) conditions or by post-aluminization (chromization) annealing or heat treatment steps in inert or oxidizing conditions. Aluminization and chromization can be done simultaneously or sequentially to produce thealuminized surface layer 106 described above. - Referring now to
FIG. 3 , thepack 330 and the ferrousstructural component 340 to be aluminized (chromized) may be placed in a controlledenvironment 350, such as in a crucible with a gas-tight seal or in a semi-open crucible placed in a furnace under vacuum conditions or inert gas (e.g., He, Ar, or N2) flow. Alternatively, a reducing environment, such as a forming gas flow (e.g., N2 or Ar+H2) may be employed. For example, the controlled environment may comprise an environmental control furnace under gettered argon (≤10−12 partial pressure of O2). The argon may be maintained at a pressure of 1 atm and continuously purged at a flow rate in a range of 0.5-2 L/min. Advantageously, the controlled environment is substantially devoid of oxygen. - To promote diffusion into the surface, the introduction of the aluminum (chromium) may be carried out at an elevated temperature in a range from 500° C. to 1000° C., and preferably below 900° C. to avoid having a detrimental impact on the mechanical properties of the ferrous
structural component 102. Preferably, the elevated temperature may lie in the range from about 550° C. to about 900° C. For example, pack aluminization of alloy steels including 13 wt. % Cr (“13 Cr alloys”) may be carried out at an elevated temperature of about 900° C. or less, and pack aluminization of X65 steels may be carried out at an elevated temperature of 600° C. or less. The elevated temperature at which aluminization (chromization) takes place may be understood to be the temperature attained by the ferrous metal component during processing. The elevated temperature may be maintained for 12 hours or less, for 6 hours or less, or for 3 hours or less, and typically for at least one hour to achieve aluminization (chromization). - The aluminum source may comprise an aluminum alloy including from 50% to 99% aluminum or pure aluminum including only incidental impurities. When chromization takes place, the chromium source may comprise chromium (e.g., 99.5% purity). The halide salt may comprise NH4Cl or AlCl3, for example. The halide salt may serve as an activator and the aluminum oxide may act as an inert diluent. All three ingredients may take the form of a powder that can be tumbled together to form a mixture that serves as the pack. For example, the powder may be ball milled for 24-48 hours to ensure a homogeneous mixture. The pack may comprise the aluminum (or chromium) source at a concentration from about 5 wt. % to about 40 wt. %; the halide salt at a concentration from about 1 wt. % to about 5 wt. %; and the aluminum oxide at a concentration from about 70 wt. % to about 90 wt. %. The relative amounts of the pack ingredients are selected so that the pack has a sufficiently high aluminum (chromium) activity to be effective at the lower temperatures desired to preserve the mechanical properties of the iron alloy body and minimize grain growth.
- In experiments described below, low-temperature pack aluminization is applied to samples comprising API 5L X65, a high strength pipe steel that is low in alloying elements. High-temperature and high-pressure (HPHT) autoclave fouling with a model sulfur-containing asphaltene, specifically, 1,6-bis(pyren-1-ylthio)hexane, referred to as BPH, is conducted on untreated and aluminized sample surfaces. The results suggest that using low-temperature pack aluminization can be a viable route to improve the fouling resistance of ferrous structural components, with beneficial effects on other metrics, such as mechanical properties and corrosion resistance.
- Metallographic Sample Preparation
- As indicated above, the ferrous alloy utilized for this study is API 5L X65. After being machined down to 5 mm×5 mm×0.5 mm size by electrical discharge machining (EDM), the coupons are brought to a level but stochastic finish (˜20 nm RMS roughness) by grinding with silicon carbide papers up to 1200 grit followed by polishing with a 1 μm neutral alumina solution. While the aluminization process increases the original surface roughness of the polished X65 specimens (˜180 nm RMS roughness), the benefits of reduced asphaltene fouling are realized (see below) due to the presence of the passivating layer.
- Low-Temperature Pack Aluminization
- The pack used for the aluminization process includes three ingredients: 82 wt. % inert Al2O3 powder [Baikowski/US Research Nanomaterials, 99.9% pure], 3 wt. % NH4Cl activator [Alfa Aesar, 99.999% pure], and a 15 wt. % Raney-nickel aluminum source [Ni-50 wt. % Al, Acros, 99.99% pure]. The relative amounts of the ingredients are selected to ensure that the pack has a sufficiently high aluminum activity to work at the lower temperatures desired to minimize grain growth and preserve the base mechanical properties of the steel. After the ingredients are combined, they are mixed with Al2O3 ball milling media for 48 hours to ensure homogeneous mixing. The
X65 samples 340 are embedded in thepack 330, as shown inFIG. 3 , and placed in anenvironmental control furnace 350 under 1 atmosphere of gettered argon (10−12 partial pressure of O2) that was continuously purged at a flow rate of 1 L/min. In order to produce Al chloride vapors that reduce at the surface of the metal to leave behind Al metal, the embedded samples are heated to 600° C. at a ramp rate of 20° C./min and held at this temperature for 6 hrs. Several 5 mm×5 mm×0.5 mm X65pipe steel coupons 340 are aluminized, as illustrated inFIG. 3 . Thesamples 340 are then cooled under argon for an hour, followed by a nitrogen purge until they reach room temperature. - High-Temperature Fouling Test
- The model asphaltene used in this study is 1,6-bis(pyren-1-ylthio)hexane, referred to as BPH. The BPH is synthesized through a nucleophilic aromatic substitution reaction. For the HPHT fouling test, an autoclave [60 ml EZE Seal Pressure Vessel, Parker Hannifin] made from 316 stainless steel is used. The steel coupons are fully submerged in 5 mL of the model asphaltene solution before being air-sealed and then heated from room temperature at a rate of 10° C./min. Once the furnace reaches its final temperature of 350° C., the temperature is held for 1 hour before the furnace is naturally cooled to room temperature. After the autoclave reaches room temperature, the coupons are removed and rinsed with 1 mL of petroleum ether to remove loosely adhered deposits. The mass gain of the coupons is measured using a microbalance [XPE26, Mettler-Toledo] after the fouling test.
- Mechanical Characterization
- The hardness of the aluminized coupons is measured along the depth of the cross-sectional samples using a nanoindentation system [Hysitron TI 950 Tribolndenter, Bruker Corporation] with a diamond Berkovich tip. All indentation tests are made to a maximum depth of 100 nm with a constant rate of 10 nm/s. The obtained load-displacement data are analyzed using the Oliver-Pharr method to calculate the hardness.
- Hydrogen Chloride Corrosion Test
- Corrosion tests are performed by immersing X65 samples in a fixed pH (˜3) HCl solution at room temperature. The HCl solution is composed of 1.0 M HCl and distilled water in the appropriate proportions. The solution is monitored daily to keep the pH value relatively constant throughout the test. The mass of the samples is measured every three days using a microbalance. The total area normalized mass loss of specimens is calculated and compared to the original mass before immersion.
- Results
- Cross-sectional SEM images of
X65 samples 104 after aluminization are shown at different magnifications inFIGS. 2A and 4 . The modifiedsurface 104 a includes an aluminizedsurface layer 106 overlying asmaller interdiffusion layer 110. Beneath theinterdiffusion layer 110 is the base X65 alloy, which is not altered by the aluminization. - Results from nanoindentation tests carried out on the cross-sections of aluminized X65 steel samples as described above are shown in
FIGS. 5A-5C , where indentations from the tests are visible inFIG. 2A . The hardness of the aluminized top layer and the X65 substrate beneath is evaluated from the indentation load-depth curves.FIG. 5A shows the typical load-depth curves for the indents made in the aluminized surface layer and in the base X65 alloy. The aluminized surface lay has a much higher maximum indentation load, thus a higher hardness compared to the base X65. The variation of hardness as a function of depth is shown inFIG. 5B ; the aluminized surface layer is significantly harder than both the interdiffusion layer and the base X65 alloy. The average hardness of the aluminized surface is 8.77±1.66 GPa, and it drops to 3.22±0.15 GPa in the base X65 region, as shown inFIG. 5C . The hardness data as a function of depth correlate well with the concentration profile data, discussed above and shown inFIG. 2B . Combined, these data confirm the formation of an aluminized surface layer including one or more iron aluminides. The high hardness in the aluminized surface layer suggests that Fe2Al5, the hardest intermetallic phase formed among Fe—Al compounds, may be present. - Results from fouling experiments conducted on aluminized and untreated (bare) X65 coupons at 350° C. as described above are presented in
FIG. 6 as area normalized mass gain. The difference in mass gain between the aluminized and bare X65 samples is significant. The average amount of deposition measured for the bare X65 samples is nearly 3000 mg/m2 (2914 mg/m2), while negligible mass gain is observed for the aluminized X65 sample. Optical images reveal large and numerous carbonaceous deposits on the bare X65 samples, while there is no significant foulant build-up on the aluminized X65 samples. - A detailed cross-sectional scanning transmission electron microscope (STEM) image of an aluminized X65 steel surface after fouling is shown in
FIG. 7 . The STEM data reveal a dense and continuous film of Al2O3 with a thickness of ˜10 nm. In agreement with XPS data, the results show that during the fouling experiment, the existing thin Al2O3 layer grows thicker. Thus, in contrast to the bare X65 substrate, the alumina layer prevents the formation of thiolate species and iron sulfide at the surface. The passivating layer also mitigates the diffusion of other metallic species from the X65 substrate. Therefore, the aluminized surface shows no significant mass gain from the fouling deposits, in contrast to the bare X65 coupons. - In the aluminization process, the aluminum diffuses into the X65 steel and establishes an aluminum reservoir for the formation and healing of the passivating layer, as described above. In order to examine the reformation of the passivating layer in aluminized samples, the aluminized surface layer undergoes polishing to remove the existing passivating layer. A nanoindenter scratch test is then performed along a 100 μm line with a continuously increasing load from zero to the maximal load of 150 mN in order to determine the desired depth of penetration. A few scratches are made at a constant load of 50 mN and a depth of ˜500 nm (0.5 micron). After introducing the scratches, the sample is annealed in air at 350° C. for 1 hour (similar to the fouling experiment) for further analysis. An STEM cross-sectional image of a representative scratch is shown in
FIG. 8A . The high magnification images confirm the reformation of a ˜10 nm thick and uniform oxide layer both at the side and tip of the scratch (FIGS. 8B and 8C ). The results show that if the passivating oxide layer on the iron alloy body is damaged within the aluminized region, it can be reformed continuously from the Al reservoir. - A summary of the results of the corrosion tests is shown in
FIG. 9 , where it can be observed that the average mass loss after 30 days is higher for the bare X65 sample than for the aluminized X65 sample. This indicates increased corrosion resistance for the aluminized X65 sample. As explained above, an aluminum oxide layer may form immediately upon air exposure; this oxide layer may be very thin and discontinuous. However, exposure to higher temperatures can rapidly help it grow thick and continuous to form thepassivating layer 108, which provides protection against corrosion and deposition. - Although the present invention has been described in considerable detail with reference to certain embodiments thereof, other embodiments are possible without departing from the present invention. The spirit and scope of the appended claims should not be limited, therefore, to the description of the preferred embodiments contained herein. All embodiments that come within the meaning of the claims, either literally or by equivalence, are intended to be embraced therein.
- Furthermore, the advantages described above are not necessarily the only advantages of the invention, and it is not necessarily expected that all of the described advantages will be achieved with every embodiment of the invention.
Claims (20)
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