EP3250727B2 - Method for producing such a component made of press-form-hardened, aluminum-based coated steel sheet - Google Patents
Method for producing such a component made of press-form-hardened, aluminum-based coated steel sheet Download PDFInfo
- Publication number
- EP3250727B2 EP3250727B2 EP17721056.4A EP17721056A EP3250727B2 EP 3250727 B2 EP3250727 B2 EP 3250727B2 EP 17721056 A EP17721056 A EP 17721056A EP 3250727 B2 EP3250727 B2 EP 3250727B2
- Authority
- EP
- European Patent Office
- Prior art keywords
- treatment
- aluminum
- steel sheet
- press
- steel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 229910000831 Steel Inorganic materials 0.000 title claims description 52
- 239000010959 steel Substances 0.000 title claims description 52
- 229910052782 aluminium Inorganic materials 0.000 title claims description 30
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 29
- 238000004519 manufacturing process Methods 0.000 title claims description 8
- 238000000576 coating method Methods 0.000 claims description 52
- 239000011248 coating agent Substances 0.000 claims description 35
- 238000010438 heat treatment Methods 0.000 claims description 34
- 238000000034 method Methods 0.000 claims description 22
- 230000008569 process Effects 0.000 claims description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-M hydroxide Chemical compound [OH-] XLYOFNOQVPJJNP-UHFFFAOYSA-M 0.000 claims description 12
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 10
- 230000003647 oxidation Effects 0.000 claims description 9
- 238000007254 oxidation reaction Methods 0.000 claims description 9
- 238000010422 painting Methods 0.000 claims description 8
- 238000003466 welding Methods 0.000 claims description 8
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 claims description 7
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 5
- 239000001301 oxygen Substances 0.000 claims description 5
- 229910052760 oxygen Inorganic materials 0.000 claims description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 229910021529 ammonia Inorganic materials 0.000 claims description 3
- 238000010924 continuous production Methods 0.000 claims description 3
- 150000004679 hydroxides Chemical class 0.000 claims description 3
- 150000003139 primary aliphatic amines Chemical class 0.000 claims description 3
- 150000005619 secondary aliphatic amines Chemical class 0.000 claims description 3
- 150000003510 tertiary aliphatic amines Chemical class 0.000 claims description 3
- 229910000760 Hardened steel Inorganic materials 0.000 claims description 2
- 239000004411 aluminium Substances 0.000 claims 2
- 229910021502 aluminium hydroxide Inorganic materials 0.000 claims 1
- 229910000069 nitrogen hydride Inorganic materials 0.000 claims 1
- 238000007493 shaping process Methods 0.000 claims 1
- 239000010410 layer Substances 0.000 description 53
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 26
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 19
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 15
- 239000003973 paint Substances 0.000 description 12
- 229910052742 iron Inorganic materials 0.000 description 10
- 238000000926 separation method Methods 0.000 description 8
- 238000000137 annealing Methods 0.000 description 7
- 238000009792 diffusion process Methods 0.000 description 7
- 238000005275 alloying Methods 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 5
- 229910052710 silicon Inorganic materials 0.000 description 5
- 238000012876 topography Methods 0.000 description 5
- 229910052725 zinc Inorganic materials 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000008021 deposition Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000011148 porous material Substances 0.000 description 4
- 229910015372 FeAl Inorganic materials 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 238000002048 anodisation reaction Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000007598 dipping method Methods 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000010791 quenching Methods 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000007858 starting material Substances 0.000 description 3
- -1 zinc-aluminum-iron Chemical compound 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000011241 protective layer Substances 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 229910000712 Boron steel Inorganic materials 0.000 description 1
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910000611 Zinc aluminium Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000002318 adhesion promoter Substances 0.000 description 1
- HXFVOUUOTHJFPX-UHFFFAOYSA-N alumane;zinc Chemical compound [AlH3].[Zn] HXFVOUUOTHJFPX-UHFFFAOYSA-N 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- 229940024545 aluminum hydroxide Drugs 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- PALQHNLJJQMCIQ-UHFFFAOYSA-N boron;manganese Chemical compound [Mn]#B PALQHNLJJQMCIQ-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 230000000376 effect on fatigue Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- KFZAUHNPPZCSCR-UHFFFAOYSA-N iron zinc Chemical compound [Fe].[Zn] KFZAUHNPPZCSCR-UHFFFAOYSA-N 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- QELJHCBNGDEXLD-UHFFFAOYSA-N nickel zinc Chemical compound [Ni].[Zn] QELJHCBNGDEXLD-UHFFFAOYSA-N 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/12—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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/14—Removing excess of molten coatings; Controlling or regulating the coating thickness
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/261—After-treatment in a gas atmosphere, e.g. inert or reducing atmosphere
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
- C23C2/29—Cooling or quenching
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/34—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
- C23C2/36—Elongated material
- C23C2/40—Plates; Strips
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/324—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal matrix material layer comprising a mixture of at least two metals or metal phases or a metal-matrix material with hard embedded particles, e.g. WC-Me
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/02—Pretreatment of the material to be coated
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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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/10—Oxidising
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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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/80—After-treatment
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
Definitions
- the invention relates to a method for producing a component made of press-hardened, aluminum-based steel sheet, the coating having a coating applied by hot-dipping that contains aluminum and silicon.
- the coating relates to an aluminum-silicon coating.
- press hardening can be used to produce high-strength components that are primarily used in the bodywork area.
- Press hardening can basically be carried out using two different process variants, namely the direct or indirect process. While in the indirect process the process steps of forming and hardening take place separately from each other, in the direct process they take place together in one tool. Only the direct method is considered below.
- a steel sheet is heated above the so-called austenitization temperature (Ac3).
- the steel sheet heated in this way is then transferred to a mold and formed into the finished component in a single-stage forming step and simultaneously cooled by the cooled mold at a rate that is above the critical cooling rate of the steel, so that a hardened component is produced.
- the steel sheet itself is usually cut out of a steel strip, usually wound up as a coil, and then further processed.
- the steel sheet to be formed is often referred to as a blank.
- Well-known hot-formable steels for this area of application include the manganese-boron steel "22MnB5" and, more recently, air-hardenable steels in accordance with the European patent EP 2 449 138 B1 .
- steel sheets with anti-scaling protection are also used for press hardening (e.g. for automotive body construction). used.
- press hardening e.g. for automotive body construction.
- the advantages here are that the blanks or components do not scale in the oven, which reduces wear on the press tools caused by chipped scale and the components often do not have to be extensively blasted before further processing.
- the following (alloy) coatings applied by hot-dipping are currently known for press hardening: aluminum-silicon (AS), zinc-aluminum (Z), zinc-aluminum-iron (ZF/Galvannealed), zinc-magnesium-aluminum (ZM ), as well as electrolytically deposited coatings made of zinc-nickel or zinc, the latter being converted into an iron-zinc alloy layer before hot forming.
- AS aluminum-silicon
- Z zinc-aluminum
- ZF/Galvannealed zinc-aluminum-iron
- ZM zinc-magnesium-aluminum
- electrolytically deposited coatings made of zinc-nickel or zinc the latter being converted into an iron-zinc alloy layer before hot forming.
- These corrosion protection coatings are usually applied to the hot or cold strip in a continuous process.
- US 2011/0300407 A1 is a method of manufacturing a press-hardened steel sheet for use in the automotive industry.
- the steel sheet is provided with an aluminum-silicon (AS) coating with a layer of 20 to 80 g/m 2 , heated to temperatures above 820 ° C and the temperature is maintained for some time (approx. 3 minutes).
- AS aluminum-silicon
- Different intermetallic phases are formed in the coating, for example Fe 3 Al, FeAl or Fe-Al 2 O 3 .
- the product is cooled in the press.
- European patent application EP 2 312 011 A1 describes a process for producing metallic coatings on cast parts for use in automobile construction.
- the cast part is coated with an aluminum alloy in a melt pool and then subjected to heat treatment in an oxidizing atmosphere to produce a high-temperature-resistant aluminum oxide layer. After the heat treatment, anodic oxidation is also provided.
- German patent specification DE 198 53 285 C1 presents a process for producing a protective layer on martensitic steel. Under a protective gas atmosphere (argon with 5% H 2 ), the steel to be coated is dipped into a melt made of aluminum or an aluminum alloy, cooled and then hot isostatically pressed at the austenitizing temperature.
- the aluminum protective layer created in this way is between 100 and 200 ⁇ m thick and should contain an approx. 1 ⁇ m thick aluminum oxide layer on its surface, about the creation or maintenance of which no further information is provided.
- the advantage of aluminum-based coatings over zinc-based coatings is that, in addition to a larger process window (e.g. with regard to heating parameters), the finished components do not need to be processed before further processing need to be blasted.
- the finished components do not need to be processed before further processing need to be blasted.
- there is no risk of liquid metal embrittlement and no microcracks can form in the substrate area near the surface at the former austenite grain boundaries, which can have a negative effect on fatigue strength at depths of over 10 ⁇ m.
- the alloying of the coating with iron and the formation of a paintable surface topography require a correspondingly long residence time in the commonly used roller hearth furnace, which significantly extends the cycle times and reduces the economic efficiency of press mold hardening.
- the minimum residence time is therefore determined by the coating and not by the base material, for which only the necessary austenitization temperature would be necessary.
- the corrosion resistance is reduced by the increased alloying with iron, as the aluminum content in the alloy layer decreases with the furnace residence time and the iron content increases.
- longer ovens are usually used for AS boards in order to achieve high cycle rates despite the necessary oven dwell time. However, these are more expensive to purchase and operate and also require a lot of space.
- AS coatings Another disadvantage of AS coatings is that with very short annealing times, weldability using the spot welding process is extremely poor. This is expressed, for example, in only a very small welding area. The reason for this is, among other things, a very low contact resistance with short glow times.
- the object of the invention is therefore to provide a method for producing a component from a press-hardened, aluminum-based steel sheet, which is cost-effective and leads to a component that has excellent paintability and weldability, in particular resistance spot weldability.
- aluminum-based coatings are understood to mean metallic coatings in which aluminum is the main component (in mass percent).
- examples of possible aluminum-based coatings are aluminum-silicon (AS), aluminum-zinc-silicon (AZ), as well as the same coatings with admixtures of additional elements such as magnesium, transition metals such as manganese, titanium and rare earths.
- a coating of the steel sheet according to the invention is produced, for example, in a melt pool with an Si content of 8 to 12% by weight, an Fe content of 1 to 4% by weight, and the balance being aluminum.
- the cover layers containing aluminum oxide and/or hydroxide act as ideal adhesion promoters for subsequent painting, in particular cathodic dip painting (KTL), on the component formed by press-hardening.
- KTL cathodic dip painting
- oven time increases accordingly due to the lower heating rate of the steel material.
- the typical ones Oven temperatures between 900 and 950 °C should also be maintained here.
- oven temperatures between 930 and 950 °C are advantageous.
- the cover layer according to the invention made of aluminum oxides and/or hydroxides has an advantageous effect on the resistance spot weldability with short furnace times, since the contact resistance is increased and good resistance heating is thus achieved.
- a thickness of this cover layer of at least 0.05 ⁇ m has proven to be positive.
- the thicker the top layer containing aluminum oxide and/or hydroxide the better the paint adhesion and the less infiltration due to corrosive attack.
- this cover layer is too thick, the contact resistance during resistance spot welding is too high, which in turn would worsen the weldability. Therefore, a maximum thickness of the top layer of 5 ⁇ m should not be exceeded.
- a thickness of between 0.10 and 3 ⁇ m was found for the top layer as a good compromise between weldability and paint adhesion.
- top layers with an average thickness of between 0.15 and 1 ⁇ m are particularly advantageous.
- the term is to be understood at least in some areas in the sense of local sections of the treated steel sheet or steel strip, so that a steel sheet or steel strip is created with structures and properties that differ from one another in a targeted manner.
- the top layer is preferably applied to the surface of the coating in a continuous process.
- the treatment advantageously takes place in an atmosphere which also contains proportions of basic components, preferably ammonia (NH 3 ), primary, secondary or tertiary aliphatic amines (NH 2 R, NHR 2 ), NR 3 ).
- basic components preferably ammonia (NH 3 ), primary, secondary or tertiary aliphatic amines (NH 2 R, NHR 2 ), NR 3 ).
- a thin oxide cover layer can advantageously be achieved by anodic oxidation (thin-film anodization), plasma oxidation and a cover layer containing hydroxide by means of a hot water treatment of the aluminum-based coating at temperatures of at least 90 ° C, advantageously at least 95 ° C and / or a treatment in steam at temperatures of at least 90 °C, advantageously at least 95 °C.
- gas phase treatment of the AS surface also achieves the same goal.
- the AS surface is treated with an atmosphere which can contain at least variable proportions of oxygen, water vapor, and optionally also proportions of basic components, in particular ammonia, primary, secondary or tertiary aliphatic amines.
- This treatment leads to a time- or temperature-controlled growth of a top layer containing aluminum oxide and/or hydroxide.
- the composition of the gas phase can be used to control the growth of the layer thickness of this top layer.
- the treatment is carried out at a temperature of 40 °C to 100 °C, preferably 90 °C to 100 °C. Lower treatment temperatures extend the treatment time; treatment temperatures above 100 °C may require pressure vessels.
- Both anodization and gas phase treatment lead to a cover layer containing aluminum oxide and/or hydroxide, which has network or needle-like structures on its surface.
- the associated increase in surface area improves the adhesion of subsequent KT painting. Since longer heating times are no longer necessary to form a surface topography that can be painted, the corrosion protection of the coating is also increased. This can be explained by the fact that with only a short annealing time required in the roller hearth furnace, less diffusion of aluminum and iron takes place. This also leads, among other things, to a relatively small interdiffusion zone. This is an example for an AS layer of the starting material of 150 g/m 2 (AS150) below 7 ⁇ m.
- the thicknesses of the interdiffusion layers I according to the invention for a layer layer of the starting material result from the linear relationship according to the following formulas for various sheet thickness-dependent Heating times: I ⁇ m ⁇ 1 35 ⁇ edition bilaterally G / m 2 + 19 7 (short heating time ) I ⁇ m ⁇ 1 35 ⁇ edition bilaterally G / m 2 + 5 7 (very short heating time ) I ⁇ m ⁇ 1 35 ⁇ edition bilaterally G / m 2 ⁇ 2 7 (extremely short heating time )
- the necessary heating time in the oven depends only on the sheet thickness, since the coating according to the invention does not require any holding time in the oven to produce a surface that can be painted. Thicker sheets therefore require longer heating times than thinner sheets.
- Table 1 lists short (220 seconds), very short (180 seconds) and extremely short (150 seconds) heating times compared to usual heating times (360 seconds) in the roller hearth furnace.
- Another positive effect of the short heating time is a significantly reduced proportion of pores in the alloy layer and in the diffusion zone. Pores arise during longer annealing times, for example due to the Kirkendall effect. Tests have shown that short-term annealing can reduce the total pore content to values of less than 6% and even to values of less than 4% or 2%. Which, for example, can have a beneficial effect on the suitability for welding.
- Figure 1 shows schematically the layer structure of the coating on a press-hardened component with a coating made of AS and the usual long heating time according to the prior art to achieve alloying of the coating with iron.
- An interdiffusion zone Fe(Al,Si) with a thickness of 7 to 14 ⁇ m is formed on the martensitic steel base material, on which a zone with different intermetallic phases (e.g. Fe 2 SiAl 2 and FeAl 2 ) has formed, the individual phases being in This zone can occur in rows or clusters.
- intermetallic phases e.g. Fe 2 SiAl 2 and FeAl 2
- Figure 2 shows the layer structure of a coating according to the invention on a press-hardened component with an AS coating on which a cover layer according to the invention containing aluminum oxide and / or hydroxide of at least 0.05 ⁇ m is formed and which is produced with shortened heating times compared to the prior art became.
- an interdiffusion zone is formed in which aluminum and silicon have diffused into the steel Fe(Al, Si). Due to the very short heating time required in the oven to the austenitization temperature, this layer, for example for AS150, has an average thickness of less than 7 ⁇ m.
- a further layer with different intermetallic phases forms on this layer, whereby the individual phases in this zone can appear in rows or clusters and on which an aluminum oxide and/or -hydroxide-containing cover layer is arranged with an average thickness of at least 0.05 ⁇ m to a maximum of 5 ⁇ m.
- Figure 3 graphically shows the thickness I of the interdiffusion zone according to the invention for a layer of the starting material between 50 g/m 2 and 180 g/m 2 according to the following relationship: I ⁇ m ⁇ 1 35 ⁇ edition bilaterally G / m 2 + 19 7
- Table 1 summarizes tests on paint adhesion (phosphating treatment typical for automobiles and cathodic dip painting; testing after 72 hours of condensation water constant climate according to DIN EN ISO 6270-2:2005 CH) and weldability (resistance spot welding) of press-hardened AS150 samples at 940 °C oven temperature and various heating times.
- the sheet thickness of the samples is 1.5 mm. It can be seen that good paint adhesion and weldability are only achieved with heating times of 220 s and less a cover layer containing aluminum oxide and/or hydroxide according to the invention is present. Short heating times of 220 s and less also resulted in interdiffusion layers of less than 7 ⁇ m on the press-hardened component.
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Description
Die Erfindung betrifft ein Verfahren zur Herstellung eines Bauteils aus pressformgehärtetem, auf Basis von Aluminium beschichtetem Stahlblech, wobei die Beschichtung einen im Schmelztauchverfahren aufgebrachten Überzug aufweist, der Aluminium und Silizium enthält. Insbesondere betrifft die Beschichtung einen Aluminium-Silizium-Überzug.The invention relates to a method for producing a component made of press-hardened, aluminum-based steel sheet, the coating having a coating applied by hot-dipping that contains aluminum and silicon. In particular, the coating relates to an aluminum-silicon coating.
Es ist bekannt, dass warmumgeformte Stahlbleche insbesondere im Automobilbau immer häufiger Verwendung finden. Durch den auch als Presshärten bezeichneten Prozess können hochfeste Bauteile erzeugt werden, die vorwiegend im Bereich der Karosserie eingesetzt werden. Das Presshärten kann grundsätzlich mittels zwei verschiedener Verfahrensvarianten durchgeführt werden, nämlich mittels des direkten oder indirekten Verfahrens. Während beim indirekten Verfahren die Prozessschritte des Umformens und Härtens getrennt voneinander ablaufen, finden sie beim direkten Verfahren in einem Werkzeug gemeinsam statt. Im Folgenden wird nur das direkte Verfahren betrachtet.It is known that hot-formed steel sheets are being used more and more frequently, particularly in automobile construction. The process, also known as press hardening, can be used to produce high-strength components that are primarily used in the bodywork area. Press hardening can basically be carried out using two different process variants, namely the direct or indirect process. While in the indirect process the process steps of forming and hardening take place separately from each other, in the direct process they take place together in one tool. Only the direct method is considered below.
Beim direkten Verfahren wird ein Stahlblech über die sogenannte Austenitisierungstemperatur (Ac3) aufgeheizt. Anschließend wird das so erhitzte Stahlblech in ein Formwerkzeug überführt und in einem einstufigen Umformschritt zum fertigen Bauteil umgeformt und hierbei durch das gekühlte Formwerkzeug gleichzeitig mit einer Geschwindigkeit, die über der kritischen Abkühlgeschwindigkeit des Stahls liegt, abgekühlt, so dass ein gehärtetes Bauteil erzeugt wird. Das Stahlblech selbst wird dabei üblicherweise aus einem meist als Coil aufgewickelten Stahlband herausgeschnitten und anschließend weiterverarbeitet. Das umzuformende Stahlblech wird häufig auch als Platine bezeichnet.In the direct process, a steel sheet is heated above the so-called austenitization temperature (Ac3). The steel sheet heated in this way is then transferred to a mold and formed into the finished component in a single-stage forming step and simultaneously cooled by the cooled mold at a rate that is above the critical cooling rate of the steel, so that a hardened component is produced. The steel sheet itself is usually cut out of a steel strip, usually wound up as a coil, and then further processed. The steel sheet to be formed is often referred to as a blank.
Bekannte warmumformbare Stähle für diesen Einsatzbereich sind zum Beispiel der Mangan-Bor-Stahl "22MnB5" und neuerdings auch luftvergütbare Stähle gemäß des europäischen Patentes
Neben unbeschichteten Stahlblechen werden auch Stahlbleche mit einem Verzunderungsschutz für das Presshärten (z.B. für den automobilen Karosseriebau) eingesetzt. Die Vorteile liegen hier neben der erhöhten Korrosionsbeständigkeit des fertigen Bauteils darin, dass die Platinen oder Bauteile im Ofen nicht verzundern, wodurch der Verschleiß der Pressenwerkzeuge durch abgeplatzten Zunder reduziert wird und die Bauteile vor der Weiterverarbeitung oft nicht aufwendig gestrahlt werden müssen.In addition to uncoated steel sheets, steel sheets with anti-scaling protection are also used for press hardening (e.g. for automotive body construction). used. In addition to the increased corrosion resistance of the finished component, the advantages here are that the blanks or components do not scale in the oven, which reduces wear on the press tools caused by chipped scale and the components often do not have to be extensively blasted before further processing.
Für das Presshärten sind derzeit die folgenden, durch Schmelztauchen aufgebrachten (Legierungs-) Beschichtungen bekannt: Aluminium-Silizium (AS), Zink-Aluminium (Z), Zink-Aluminium-Eisen (ZF/ Galvannealed), Zink-Magnesium-Aluminium (ZM), sowie elektrolytisch abgeschiedene Beschichtungen aus Zink-Nickel oder Zink, wobei die letztere vor der Warmumformung in eine Eisen-Zink-Legierungsschicht umgewandelt wird. Diese Korrosionsschutzbeschichtungen werden üblicherweise in kontinuierlichen Durchlaufverfahren auf das Warm- oder Kaltband aufgebracht.The following (alloy) coatings applied by hot-dipping are currently known for press hardening: aluminum-silicon (AS), zinc-aluminum (Z), zinc-aluminum-iron (ZF/Galvannealed), zinc-magnesium-aluminum (ZM ), as well as electrolytically deposited coatings made of zinc-nickel or zinc, the latter being converted into an iron-zinc alloy layer before hot forming. These corrosion protection coatings are usually applied to the hot or cold strip in a continuous process.
Die Herstellung von Bauteilen mittels Abschrecken von Vorprodukten aus presshärtbaren Stählen durch Warmumformen in einem Umformwerkzeug ist aus dem deutschen Patent
Die Herstellung von Bauteilen mittels Abschrecken von mit einer Aluminiumlegierung beschichteten Vorprodukten aus presshärtbaren Stählen durch Warmumformen in einem Umformwerkzeug ist aus dem deutschen Patent
Aus der Offenlegungsschrift
Auch die europäische Patentanmeldung
Die deutsche Patentschrift
Aus der europäischen Patentanmeldung
Der Vorteil bei den aluminiumbasierten Überzügen gegenüber den zinkbasierten Überzügen liegt darin, dass neben einem größeren Prozessfenster (z.B. hinsichtlich der Erwärmungsparameter) die fertigen Bauteile vor der Weiterverarbeitung nicht gestrahlt werden müssen. Darüber hinaus besteht bei aluminiumbasierten Überzügen nicht die Gefahr von Flüssigmetallversprödung und es können sich keine Mikrorisse im oberflächennahen Substratbereich an den ehemaligen Austenitkorngrenzen ausbilden, die bei Tiefen über 10 µm einen negativen Effekt auf die Dauerfestigkeit haben können.The advantage of aluminum-based coatings over zinc-based coatings is that, in addition to a larger process window (e.g. with regard to heating parameters), the finished components do not need to be processed before further processing need to be blasted. In addition, with aluminum-based coatings there is no risk of liquid metal embrittlement and no microcracks can form in the substrate area near the surface at the former austenite grain boundaries, which can have a negative effect on fatigue strength at depths of over 10 µm.
Nachteilig bei der Verwendung von aluminiumbasierten Überzügen, z.B. aus Aluminium-Silizium (AS), ist jedoch die mangelhafte Lackhaftung des umgeformten Bauteils bei der automobiltypischen kathodischen Tauchlackierung (KTL), wenn eine zu kurze Erwärmungszeit beim Presshärten verwendet wurde. Bei kurzen Erwärmungszeiten weist die Oberfläche eine zu geringe Rauheit auf, so dass keine ausreichende Lackhaftung erreicht wird.However, the disadvantage of using aluminum-based coatings, e.g. made of aluminum-silicon (AS), is the inadequate paint adhesion of the formed component in cathodic dip painting (KTL), which is typical for automobiles, if too short a heating time was used during press hardening. If the heating times are short, the surface has too little roughness so that sufficient paint adhesion is not achieved.
Im Gegensatz zu den zinkbasierten Überzügen lassen sich aluminiumbasierte Überzüge nicht oder nur unzureichend phosphatieren und somit kann durch den Phosphatierschritt keine Verbesserung der Lackhaftung erzielt werden. Aus diesen Gründen müssen bisher bei der Verarbeitung von Platinen mit aluminiumbasierten Überzügen Mindesterwärmzeiten eingehalten werden, wodurch der Überzug mit Eisen durchlegiert und sich eine raue Oberflächentopografie ausbildet, die eine ausreichende Lackhaftung beim Lackieren des umgeformten Bauteils bewirkt.In contrast to zinc-based coatings, aluminum-based coatings cannot be phosphated or only insufficiently phosphated and therefore the phosphating step cannot achieve any improvement in paint adhesion. For these reasons, minimum heating times have previously had to be adhered to when processing circuit boards with aluminum-based coatings, which causes the coating to alloy with iron and form a rough surface topography, which ensures sufficient paint adhesion when painting the formed component.
Das Durchlegieren des Überzugs mit Eisen und die Ausbildung einer lackierfähigen Oberflächentopografie erfordern allerdings eine entsprechend lange Verweildauer im üblicherweise verwendeten Rollenherdofen, was die Taktzeiten deutlich verlängert und die Wirtschaftlichkeit des Pressformhärtens reduziert. Die Mindestverweildauer wird somit durch den Überzug bestimmt und nicht durch das Grundmaterial, für das lediglich die Erreichung der notwendigen Austenitisierungstemperatur notwendig wäre. Zudem wird die Korrosionsbeständigkeit durch das stärkere Auflegieren mit Eisen verringert, da der Aluminiumgehalt in der Legierungsschicht mit der Ofenverweilzeit abnimmt und der Eisengehalt ansteigt. Für AS-Platinen werden üblicherweise angepasste, längere Öfen eingesetzt, um trotz der notwendigen Ofenverweilzeit hohe Taktraten zu erzielen. Diese sind jedoch teurer in der Anschaffung und im Betrieb und haben zudem einen sehr großen Platzbedarf. Ein weiterer Nachteil von AS-Überzügen besteht darin, dass bei sehr kurzen Glühzeiten die Schweißbarkeit im Punktschweißverfahren äußerst schlecht ist. Dies drückt sich z.B. in einem nur sehr kleinen Schweißbereich aus. Ursächlich hierfür ist unter anderem ein sehr geringer Übergangswiderstand bei kurzen Glühzeiten.However, the alloying of the coating with iron and the formation of a paintable surface topography require a correspondingly long residence time in the commonly used roller hearth furnace, which significantly extends the cycle times and reduces the economic efficiency of press mold hardening. The minimum residence time is therefore determined by the coating and not by the base material, for which only the necessary austenitization temperature would be necessary. In addition, the corrosion resistance is reduced by the increased alloying with iron, as the aluminum content in the alloy layer decreases with the furnace residence time and the iron content increases. Adapted, longer ovens are usually used for AS boards in order to achieve high cycle rates despite the necessary oven dwell time. However, these are more expensive to purchase and operate and also require a lot of space. Another disadvantage of AS coatings is that with very short annealing times, weldability using the spot welding process is extremely poor. This is expressed, for example, in only a very small welding area. The reason for this is, among other things, a very low contact resistance with short glow times.
Aufgabe der Erfindung ist es deshalb, ein Verfahren zur Herstellung eines Bauteils aus einem pressformgehärteten auf Basis von Aluminium beschichteten Stahlblech anzugeben, welches kostengünstig ist und zu einem Bauteil führt, dass eine hervorragende Lackierbarkeit und Schweißbarkeit, insbesondere Widerstandspunktschweißbarkeit, aufweist.The object of the invention is therefore to provide a method for producing a component from a press-hardened, aluminum-based steel sheet, which is cost-effective and leads to a component that has excellent paintability and weldability, in particular resistance spot weldability.
Erfindungsgemäß umfasst die Erfindung ein Verfahren zur Herstellung eines Bauteils, aus pressformgehärtetem, auf Basis von Aluminium beschichtetem Stahlblech mit besonderer Eignung zum Lackieren und Widerstandspunktschweißen, wobei als Beschichtung ein aluminiumbasierter Überzug im Schmelztauchverfahren auf das Stahlblech aufgebracht wird, welches dadurch gekennzeichnet ist,
- dass das Stahlblech oder Stahlband mit dem Überzug nach dem Schmelztauchprozess und vor dem Umformprozess einer Behandlung durch anodische Oxidation und/oder einer Plasmaoxidation und/oder einer Heißwasserbehandlung und/oder einer Behandlung in einer Atmosphäre, die mindestens variable Anteile von Sauerstoff, Wasserdampf unterzogen wird
- dass die Heißwasserbehandlung oder die Behandlung unter Wasserdampf bei Temperaturen von wenigstens 90 °C, vorteilhaft wenigstens 95 °C, erfolgt
- dass im Zuge der Behandlung auf der Oberfläche des Überzugs unter Ausbildung von Oxiden oder Hydroxiden eine Aluminiumoxid und/oder - hydroxid enthaltene Deckschicht mit einer Dicke von mindestens 0,05 µm bis höchstens 5µm ausgebildet wird
- dass das Stahlblech oder Stahlband zumindest bereichsweise auf eine Temperatur oberhalb der Austenitisierungstemperatur erwärmt wird
- dass das erwärmte Stahlblech oder Stahlband anschließend umgeformt und danach mit einer Geschwindigkeit abgekühlt wird, die zumindest bereichsweise oberhalb der kritischen Abkühlgeschwindigkeit liegt,
- that the steel sheet or steel strip with the coating is subjected to a treatment by anodic oxidation and/or a plasma oxidation and/or a hot water treatment and/or a treatment in an atmosphere containing at least variable proportions of oxygen and water vapor after the hot-dipping process and before the forming process
- that the hot water treatment or the treatment under steam takes place at temperatures of at least 90 ° C, advantageously at least 95 ° C
- that in the course of the treatment, a cover layer containing aluminum oxide and/or hydroxide with a thickness of at least 0.05 µm to a maximum of 5 µm is formed on the surface of the coating with the formation of oxides or hydroxides
- that the steel sheet or steel strip is heated at least in some areas to a temperature above the austenitization temperature
- that the heated steel sheet or steel strip is then formed and then cooled at a speed which is at least partially above the critical cooling speed,
Als aluminiumbasierte Überzüge werden nachfolgend metallische Überzüge verstanden, bei denen Aluminium der Hauptbestandteil (in Massenprozent) ist. Beispiele für mögliche aluminiumbasierte Überzüge sind Aluminium-Silizium (AS), Aluminium-Zink-Silizium (AZ), sowie dieselben Überzüge mit Beimischungen zusätzlicher Elemente, wie z.B. Magnesium, Übergangsmetallen wie Mangan, Titan und seltenen Erden. Ein erfindungsgemäßer Überzug des Stahlbleches wird beispielsweise in einem Schmelzbad mit einem Si-Gehalt von 8 bis 12 Gewichts-%, einem Fe-Gehalt von 1 bis 4 Gewichts-%, Rest Aluminium erzeugt.In the following, aluminum-based coatings are understood to mean metallic coatings in which aluminum is the main component (in mass percent). Examples of possible aluminum-based coatings are aluminum-silicon (AS), aluminum-zinc-silicon (AZ), as well as the same coatings with admixtures of additional elements such as magnesium, transition metals such as manganese, titanium and rare earths. A coating of the steel sheet according to the invention is produced, for example, in a melt pool with an Si content of 8 to 12% by weight, an Fe content of 1 to 4% by weight, and the balance being aluminum.
Durch die Ausbildung einer definierten Aluminiumoxid und/oder -hydroxid enthaltenden Deckschicht auf der aluminiumbasierten Beschichtung des Stahlbleches oder des Stahlbandes, können die vorgenannten negativen Aspekte von aluminiumbasierten Beschichtungen deutlich reduziert oder sogar ganz verhindert werden.By forming a defined cover layer containing aluminum oxide and/or hydroxide on the aluminum-based coating of the steel sheet or steel strip, the aforementioned negative aspects of aluminum-based coatings can be significantly reduced or even completely prevented.
Die Aluminiumoxid und/oder -hydroxid enthaltenen Deckschichten wirken auf dem durch Pressformhärten umgeformten Bauteil auf Grund ihrer netzartigen Struktur als ideale Haftvermittler für eine anschließende Lackierung, insbesondere der kathodischen Tauchlackierung (KTL). Ein langwieriges Durchlegieren der aluminiumbasierten Beschichtung im Ofen mit Eisen ist damit nicht mehr erforderlich, so dass sich die Durchlaufzeiten im Ofen zum Aufheizen des Stahlblechs auf Umformtemperatur drastisch verkürzen lassen. Während bislang beispielsweise bei Blechdicken von 1,5 mm Glühzeiten im Rollenherdofen von mindestens 4 Minuten bei 950 °C Ofentemperatur für das Durchlegieren der Beschichtung mit Eisen und die Ausbildung einer lackierfähigen Oberflächentopografie erforderlich sind, werden beim erfindungsgemäßen Verfahren bei einer Blechdicke von 1,5 mm Glühzeiten von nur noch 2 - 3 Minuten benötigt, die Glühzeit wird somit signifikant reduziert. Die maximal möglichen Ofenzeiten ändern sich durch die Aluminiumoxid und/oder -hydroxid enthaltene Deckschicht nicht. Somit wird das Prozessfenster der Erwärmung hin zu kürzeren Ofenzeiten stark erweitert.Due to their network-like structure, the cover layers containing aluminum oxide and/or hydroxide act as ideal adhesion promoters for subsequent painting, in particular cathodic dip painting (KTL), on the component formed by press-hardening. A lengthy alloying of the aluminum-based coating with iron in the furnace is no longer necessary, so that the throughput times in the furnace for heating the steel sheet to the forming temperature can be drastically shortened. While previously, for example, for sheet thicknesses of 1.5 mm, annealing times in the roller hearth furnace of at least 4 minutes at a furnace temperature of 950 ° C were required for the alloying of the coating with iron and the formation of a paintable surface topography, in the method according to the invention, for a sheet thickness of 1.5 mm Annealing times of only 2 - 3 minutes are required, which means the annealing time is significantly reduced. The maximum possible oven times do not change due to the top layer containing aluminum oxide and/or hydroxide. This means that the heating process window is greatly expanded towards shorter oven times.
Für dickere Bleche verlängert sich die Ofenzeit bedingt durch die geringere Aufheizgeschwindigkeit des Stahlwerkstoffes entsprechend. Die typischen Ofentemperaturen zwischen 900 und 950 °C sollten auch hier eingehalten werden. Für hohe Taktzeiten sind Ofentemperaturen zwischen 930 und 950 °C vorteilhaft.For thicker sheets, the oven time increases accordingly due to the lower heating rate of the steel material. The typical ones Oven temperatures between 900 and 950 °C should also be maintained here. For high cycle times, oven temperatures between 930 and 950 °C are advantageous.
Zudem wirkt sich die erfindungsgemäße Deckschicht aus Aluminiumoxiden und/oder - hydroxiden vorteilhaft auf die Widerstandpunktschweißbarkeit bei kurzen Ofenzeiten aus, da der Übergangswiderstand erhöht wird und so eine gute Widerstandserwärmung erreicht wird. Für eine gute Schweißbarkeit nach kurzen Erwärmzeiten hat sich daher eine Dicke dieser Deckschicht von mindestens 0,05 µm als positiv herausgestellt.In addition, the cover layer according to the invention made of aluminum oxides and/or hydroxides has an advantageous effect on the resistance spot weldability with short furnace times, since the contact resistance is increased and good resistance heating is thus achieved. For good weldability after short heating times, a thickness of this cover layer of at least 0.05 µm has proven to be positive.
Bei Versuchen wurde festgestellt, dass die Lackhaftung besser bzw. die Unterwanderung infolge eines korrosiven Angriffs umso geringer wird, je dicker die Aluminiumoxid und/oder -hydroxid enthaltende Deckschicht ist. Andererseits ist bei zu großer Dicke dieser Deckschicht der Übergangswiderstand beim Widerstandspunktschweißen zu hoch, wodurch sich die Schweißbarkeit wiederum verschlechtern würde. Daher sollte eine maximale Dicke der Deckschicht von 5 µm nicht überschritten werden.During tests it was found that the thicker the top layer containing aluminum oxide and/or hydroxide, the better the paint adhesion and the less infiltration due to corrosive attack. On the other hand, if this cover layer is too thick, the contact resistance during resistance spot welding is too high, which in turn would worsen the weldability. Therefore, a maximum thickness of the top layer of 5 µm should not be exceeded.
Als guter Kompromiss zwischen Schweißeignung und Lackhaftung wurde für die Deckschicht eine Dicke zwischen 0,10 und 3 µm gefunden.A thickness of between 0.10 and 3 µm was found for the top layer as a good compromise between weldability and paint adhesion.
Für eine hervorragende Schweißeignung bei guter Lackhaftung sind Deckschichten mit einer mittleren Dicke zwischen 0,15 und 1 µm besonders vorteilhaft.For excellent weldability with good paint adhesion, top layers with an average thickness of between 0.15 and 1 µm are particularly advantageous.
Im Zusammenhang mit der Erfindung ist der Begriff zumindest bereichsweise im Sinne von örtlichen Abschnitten des behandelten Stahlblechs oder Stahlbandes zu verstehen, so dass ein Stahlblech oder Stahlband mit gezielt örtlich voneinander abweichenden Gefügen und Eigenschaften entstehen.In connection with the invention, the term is to be understood at least in some areas in the sense of local sections of the treated steel sheet or steel strip, so that a steel sheet or steel strip is created with structures and properties that differ from one another in a targeted manner.
Bevorzugt wird die Deckschicht in einem kontinuierlichen Prozess auf die Oberfläche des Überzugs aufgebracht.The top layer is preferably applied to the surface of the coating in a continuous process.
Vorteilhafter Weise findet die Behandlung in einer Atmosphäre statt, die auch Anteile basischer Komponenten, vorzugsweise Ammoniak (NH3), primäre, sekundäre oder tertiäre aliphatische Amine (NH2R, NHR2), NR3) enthält.The treatment advantageously takes place in an atmosphere which also contains proportions of basic components, preferably ammonia (NH 3 ), primary, secondary or tertiary aliphatic amines (NH 2 R, NHR 2 ), NR 3 ).
Verfahrenstechnisch kann eine dünne oxidische Deckschicht vorteilhaft durch anodische Oxidation (Dünnschichteloxieren), Plasmaoxidation und eine Hydroxid enthaltene Deckschicht mittels einer Heißwasserbehandlung der aluminiumbasierten Beschichtung bei Temperaturen von mindestens 90 °C, vorteilhaft mindestens 95 °C und/oder einer Behandlung in Wasserdampf bei Temperaturen von mindestens 90 °C, vorteilhaft mindestens 95 °C hergestellt werden.In terms of process technology, a thin oxide cover layer can advantageously be achieved by anodic oxidation (thin-film anodization), plasma oxidation and a cover layer containing hydroxide by means of a hot water treatment of the aluminum-based coating at temperatures of at least 90 ° C, advantageously at least 95 ° C and / or a treatment in steam at temperatures of at least 90 °C, advantageously at least 95 °C.
Alternativ zur Anodisierung führt auch eine Gasphasenbehandlung der AS-Oberfläche zum gleichen Ziel. Hierzu wird die AS-Oberfläche mit einer Atmosphäre behandelt, die mindestens variable Anteile von Sauerstoff, Wasserdampf, optional auch Anteile basischer Komponenten, insbesondere Ammoniak, primären, sekundären oder tertiären aliphatischen Aminen enthalten kann. Diese Behandlung führt zu einem zeit- bzw. temperaturgesteuerten Wachstum einer Aluminiumoxid und/oder -hydroxid enthaltenen Deckschicht. Weiterhin lässt sich die Zusammensetzung der Gasphase zur Steuerung des Schichtdickenwachstums dieser Deckschicht nutzen. Die Behandlung wird bei einer Temperatur von 40 °C bis 100 °C, vorzugsweise 90 °C bis 100 °C durchgeführt. Niedrigere Behandlungstemperaturen verlängern die Behandlungsdauer, Behandlungstemperaturen über 100 °C erfordern ggf. Druckbehälter.As an alternative to anodization, gas phase treatment of the AS surface also achieves the same goal. For this purpose, the AS surface is treated with an atmosphere which can contain at least variable proportions of oxygen, water vapor, and optionally also proportions of basic components, in particular ammonia, primary, secondary or tertiary aliphatic amines. This treatment leads to a time- or temperature-controlled growth of a top layer containing aluminum oxide and/or hydroxide. Furthermore, the composition of the gas phase can be used to control the growth of the layer thickness of this top layer. The treatment is carried out at a temperature of 40 °C to 100 °C, preferably 90 °C to 100 °C. Lower treatment temperatures extend the treatment time; treatment temperatures above 100 °C may require pressure vessels.
Sowohl Anodisierung als auch Gasphasenbehandlung führen zu einer Aluminiumoxid und/oder -hydroxid enthaltenen Deckschicht, die an ihrer Oberfläche netz- oder nadelartige Strukturen aufweist. Die damit verbundene Oberflächenvergrößerung verbessert die Haftung einer nachfolgenden KT-Lackierung.
Da längere Erwärmungszeiten zur Ausbildung einer lackierfähigen Oberflächentopografie nicht mehr erforderlich sind, wird zudem der Korrosionsschutz der Beschichtung erhöht. Dies ist damit zu erklären, dass bei einer nur kurzen erforderlichen Glühzeit im Rollenherdofen weniger Diffusion von Aluminium und Eisen stattfindet. Dies führt unter anderem auch zu einer relativ gering ausgebildeten Interdiffusionszone. Beispielhaft ist diese für eine AS-Auflage des Ausgangsmaterials von 150 g/m2 (AS150) unterhalb von 7 µm.Both anodization and gas phase treatment lead to a cover layer containing aluminum oxide and/or hydroxide, which has network or needle-like structures on its surface. The associated increase in surface area improves the adhesion of subsequent KT painting.
Since longer heating times are no longer necessary to form a surface topography that can be painted, the corrosion protection of the coating is also increased. This can be explained by the fact that with only a short annealing time required in the roller hearth furnace, less diffusion of aluminum and iron takes place. This also leads, among other things, to a relatively small interdiffusion zone. This is an example for an AS layer of the starting material of 150 g/m 2 (AS150) below 7 µm.
In Versuchen wurden je nach Ofenverweildauer bei Verwendung von Platinen mit einer AS-Auflage von 150 g/m2 auch Dicken der Diffusionszone von unterhalb 5 µm, und sogar unterhalb 4 µm am fertigen Bauteil erzielt.In tests, depending on the length of time in the oven when using boards with an AS layer of 150 g/m 2 , thicknesses of the diffusion zone were also found to be below 5 µm, and even achieved below 4 µm on the finished component.
Bei Verwendung von Platinen mit einer AS-Auflage von 80 g/m2 (AS80) ist bekannt, dass sich hier die Ofenzeit auch bei nicht erfindungsgemäßem Überzug geringfügig reduzieren lässt und auch dadurch dünnere Diffusionsschichten von z.B. 5 µm resultieren. Versuche haben gezeigt, dass sich mit der erfindungsgemäßen Lösung die Ofenzeiten auch in diesem Fall noch weiter reduzieren lassen und hierdurch Dicken der Diffusionsschichten von unterhalb 5 µm am fertigen Bauteil erzielt werden können. In weiteren Versuchen konnten durch eine weitere Verkürzung der Erwärmzeit im Ofen auch noch geringere Dicken der Diffusionsschichten von unterhalb 3 µm, und sogar unterhalb von 2 µm am fertigen Bauteil erzielt werden.When using boards with an AS coating of 80 g/m 2 (AS80), it is known that the oven time can be reduced slightly even with a coating not according to the invention and this also results in thinner diffusion layers of, for example, 5 µm. Tests have shown that with the solution according to the invention, the oven times can be reduced even further in this case and that thicknesses of the diffusion layers of less than 5 µm can be achieved on the finished component. In further experiments, even smaller thicknesses of the diffusion layers of below 3 µm and even below 2 µm could be achieved on the finished component by further shortening the heating time in the oven.
Bei Einsatz von Platinen mit einer Schichtauflage zwischen AS80 und AS150 und bei Schichtauflagen die kleiner als AS80 sind oder größer als AS150 ergeben sich nach dem Presshärten die Dicken der erfindungsgemäßen Interdiffusionschichten I für eine Schichtauflage des Ausgangsmaterials aus dem linearen Zusammenhang gemäß den folgenden Formeln für verschiedene blechdickenabhängige Erwärmzeiten:
Die notwendige Erwärmzeit im Ofen richtet sich erfindungsgemäß nur nach der Blechdicke, da der erfindungsgemäße Überzug keine Haltezeit im Ofen zur Erzeugung einer lackierfähigen Oberfläche erfordert. Dickere Bleche erfordern für die Erwärmung daher längere Erwärmzeiten als dünnere Bleche.According to the invention, the necessary heating time in the oven depends only on the sheet thickness, since the coating according to the invention does not require any holding time in the oven to produce a surface that can be painted. Thicker sheets therefore require longer heating times than thinner sheets.
Beispielhaft für Bleche mit 1,5 mm Dicke sind in Tabelle 1 kurze (220 Sekunden), sehr kurze (180 Sekunden) und äußerst kurze (150 Sekunden) Erwärmzeiten im Vergleich zu üblichen Erwärmzeiten (360 Sekunden) im Rollenherdofen aufgeführt.As an example for sheets with a thickness of 1.5 mm, Table 1 lists short (220 seconds), very short (180 seconds) and extremely short (150 seconds) heating times compared to usual heating times (360 seconds) in the roller hearth furnace.
Ein weiterer positiver Effekt der kurzen Erwärmzeit ist ein deutlich verringerter Porenanteil in der Legierungsschicht sowie in der Diffusionszone. Poren entstehen bei längeren Glühzeiten z.B. durch den Kirkendall-Effekt. Bei Versuchen wurde festgestellt, dass sich durch die Kurzzeitglühung der Gesamtporenanteil auf Werte von weniger als 6 % und sogar auf Werte von unter 4 % bzw. 2 % reduzieren lässt. Was sich z.B. vorteilhaft auf die Schweißeignung auswirken kann.Another positive effect of the short heating time is a significantly reduced proportion of pores in the alloy layer and in the diffusion zone. Pores arise during longer annealing times, for example due to the Kirkendall effect. Tests have shown that short-term annealing can reduce the total pore content to values of less than 6% and even to values of less than 4% or 2%. Which, for example, can have a beneficial effect on the suitability for welding.
Für das Pressformhärten von Platinen mit einer Aluminium-Silizium Beschichtung ist es nun nicht mehr erforderlich, lange Verweilzeiten des Stahlbleches im Ofen einzuhalten. Das Stahlblech muss nur noch auf die erforderliche Umformtemperatur aufgeheizt werden und kann bei Erreichen der Umformtemperatur sofort der Umformpresse zugeführt, umgeformt und abgeschreckt werden.For the press-hardening of circuit boards with an aluminum-silicon coating, it is no longer necessary to maintain long residence times for the steel sheet in the oven. The steel sheet only needs to be heated to the required forming temperature and can be immediately fed to the forming press, formed and quenched when the forming temperature is reached.
Dadurch können auch vorteilhaft kürzere Rollenherdöfen als die bislang eingesetzten verwendet werden. Darüber hinaus ist die Verwendung von anderen Ofentypen beispielsweise zur induktiven oder konduktiven Schnellerwärmung möglich, ohne dass die erwärmten Platinen zur Ausbildung einer lackierfähigen Oberflächentopografie auf Temperatur gehalten werden müssen.This means that shorter roller hearth ovens than those previously used can also be advantageously used. In addition, the use of other types of ovens, for example for inductive or conductive rapid heating, is possible without the heated boards having to be kept at temperature to form a surface topography that can be painted.
Weiter ist es nun möglich, Platinen nur partiell zu erwärmen und zu härten, wodurch auch in den Bereichen mit geringem Wärmeeinfluss eine gute Punktschweißbarkeit und KT-Lackhaftung gegeben ist.Furthermore, it is now possible to only partially heat and harden circuit boards, which ensures good spot weldability and KT paint adhesion even in areas with little heat influence.
Nachfolgend wird anhand der dargestellten Figuren die Erfindung näher beschrieben.The invention is described in more detail below with reference to the figures shown.
Durch die Oxidation im Ofen sowie beim Transfer in die Presse hat sich eine nur sehr dünne Aluminiumoxidschicht mit einer Dicke von weniger als 0,05 µm gebildet. Zu erkennen sind ebenfalls Poren, die sich in den verschiedenen Zonen gebildet haben.Due to the oxidation in the oven and during transfer into the press, a very thin layer of aluminum oxide with a thickness of less than 0.05 µm was formed. Pores that have formed in the different zones can also be seen.
Tabelle 1 fasst Versuche zur Lackhaftung (automobiltypische Phosphatierungsbehandlung und kathodische Tauchlackierung; Prüfung nach 72 Stunden Kondenswasser-Konstantklima gemäß DIN EN ISO 6270-2:2005 CH) und Schweißeignung (Widerstandspunktschweißen) pressgehärteter AS150-Proben bei 940 °C Ofentemperatur und verschiedenen Erwärmzeiten zusammen. Die Blechdicke der Proben beträgt 1,5 mm. Zu erkennen ist, dass sich nur eine gute Lackhaftung und Schweißeignung bei Erwärmzeiten von 220 s und weniger ergibt, wenn eineerfindungsgemäße Aluminiumoxid und/oder -hydroxid enthaltene Deckschicht vorhanden ist. Bei kurzen Erwärmzeiten von 220 s und weniger ergaben sich darüber hinaus Interdiffusionsschichten von weniger als 7 µm am pressgehärteten Bauteil. Bei den nicht erfindungsgemäßen langen Erwärmzeiten von 360 s nach dem Stand der Technik, ist hingegen auf Grund der Durchlegierung des Überzugs mit Eisen auch bei den Proben ohne die erfindungsgemäße Aluminiumoxid und/oder -hydroxid enthaltene Deckschicht eine gute Lackhaftung und Schweißeignung gegeben. Die Dicke der Interdiffusionsschichten liegt nach 360 s Erwärmzeit deutlich über 7 µm.
Claims (3)
- Method for producing a component from press-form-hardened steel sheet or steel strip coated on the basis of aluminium, with particular suitability for painting and resistance spot welding, with an aluminium-based overcoat being applied to the steel sheet or steel strip as a coating by a hot-dip process, characterised in that- the steel sheet or steel strip having the overcoat is subjected, after the hot-dip process and before the shaping process, to treatment by anodic oxidation and/or plasma oxidation and/or hot water treatment and/or treatment in an atmosphere containing at least variable proportions of oxygen and water vapour,- the hot water treatment or the treatment under water vapour takes place at temperatures of at least 90 °C, advantageously at least 95 °C,- in the course of the treatment, a cover layer containing aluminium oxide and/or hydroxide and having a thickness of at least 0.05 µm to at most 5 µm is formed on the surface of the overcoat with the formation of oxides or hydroxides- the steel sheet or steel strip is heated at least in some regions to a temperature above the austenitisation temperature- the heated sheet steel or steel strip is then shaped and then cooled at a rate that is above the critical cooling rate at least in some regions,wherein the heating time and dwell time during the press form hardening are selected to be short enough that the thickness of the interdiffusion zone I obeys the following formula
- Method according to claim 1, characterised in that the cover layer is applied to the surface of the overcoat in a continuous process.
- Method according to either claim 1 or claim 2, characterised in that the treatment takes place in an atmosphere which also contains proportions of basic components, preferably ammonia (NH3), primary, secondary or tertiary aliphatic amines (NH2R, NHR2).
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DE102016107152A1 (en) | 2017-10-19 |
EP3250727B1 (en) | 2021-07-07 |
CN109477197B (en) | 2021-10-26 |
RU2704339C1 (en) | 2019-10-28 |
KR20190003502A (en) | 2019-01-09 |
EP3250727A1 (en) | 2017-12-06 |
KR102189424B1 (en) | 2020-12-11 |
CN109477197A (en) | 2019-03-15 |
WO2017182382A1 (en) | 2017-10-26 |
US11339479B2 (en) | 2022-05-24 |
DE102016107152B4 (en) | 2017-11-09 |
US20200308708A1 (en) | 2020-10-01 |
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