EP2655675B1 - Method for producing hardened structural elements - Google Patents
Method for producing hardened structural elements Download PDFInfo
- Publication number
- EP2655675B1 EP2655675B1 EP11811025.3A EP11811025A EP2655675B1 EP 2655675 B1 EP2655675 B1 EP 2655675B1 EP 11811025 A EP11811025 A EP 11811025A EP 2655675 B1 EP2655675 B1 EP 2655675B1
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- EP
- European Patent Office
- Prior art keywords
- cooling
- temperature
- zinc
- blank
- steel
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- 238000004519 manufacturing process Methods 0.000 title description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 43
- 239000010959 steel Substances 0.000 claims description 43
- 238000001816 cooling Methods 0.000 claims description 30
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 29
- 238000000034 method Methods 0.000 claims description 29
- 229910052725 zinc Inorganic materials 0.000 claims description 29
- 239000011701 zinc Substances 0.000 claims description 29
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 21
- 238000000576 coating method Methods 0.000 claims description 18
- 239000011248 coating agent Substances 0.000 claims description 16
- 239000000463 material Substances 0.000 claims description 13
- 239000011651 chromium Substances 0.000 claims description 10
- 229910052742 iron Inorganic materials 0.000 claims description 10
- 239000011572 manganese Substances 0.000 claims description 9
- 238000010791 quenching Methods 0.000 claims description 9
- 239000010936 titanium Substances 0.000 claims description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 8
- 229910001566 austenite Inorganic materials 0.000 claims description 8
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 7
- KFZAUHNPPZCSCR-UHFFFAOYSA-N iron zinc Chemical compound [Fe].[Zn] KFZAUHNPPZCSCR-UHFFFAOYSA-N 0.000 claims description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 5
- 229910052796 boron Inorganic materials 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 238000006243 chemical reaction Methods 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 5
- 229910052750 molybdenum Inorganic materials 0.000 claims description 5
- 239000011733 molybdenum Substances 0.000 claims description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 229910052748 manganese Inorganic materials 0.000 claims description 4
- 229910000734 martensite Inorganic materials 0.000 claims description 4
- 229910052757 nitrogen Inorganic materials 0.000 claims description 4
- 229910052698 phosphorus Inorganic materials 0.000 claims description 4
- 239000011574 phosphorus Substances 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 229910000760 Hardened steel Inorganic materials 0.000 claims description 3
- 238000007664 blowing Methods 0.000 claims description 3
- 230000003111 delayed effect Effects 0.000 claims description 2
- 238000005507 spraying Methods 0.000 claims description 2
- 239000005864 Sulphur Substances 0.000 claims 2
- 239000004411 aluminium Substances 0.000 claims 2
- 239000012809 cooling fluid Substances 0.000 claims 2
- 238000002844 melting Methods 0.000 claims 2
- 230000008018 melting Effects 0.000 claims 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 2
- 239000007789 gas Substances 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 238000005260 corrosion Methods 0.000 description 14
- 230000008569 process Effects 0.000 description 13
- 230000007797 corrosion Effects 0.000 description 11
- 239000012071 phase Substances 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 7
- 238000000465 moulding Methods 0.000 description 7
- PALQHNLJJQMCIQ-UHFFFAOYSA-N boron;manganese Chemical compound [Mn]#B PALQHNLJJQMCIQ-UHFFFAOYSA-N 0.000 description 5
- 239000007788 liquid Substances 0.000 description 5
- 229910000617 Mangalloy Inorganic materials 0.000 description 4
- 229910001338 liquidmetal Inorganic materials 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 238000010309 melting process Methods 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 238000009966 trimming Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910000712 Boron steel Inorganic materials 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- 229910001563 bainite Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000037396 body weight Effects 0.000 description 1
- 238000004210 cathodic protection Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000007791 liquid phase Substances 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
- 238000010587 phase diagram Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
- C21D9/48—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals deep-drawing sheets
-
- 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
- C23C2/06—Zinc or cadmium or alloys based thereon
-
- 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
-
- 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
Definitions
- the invention relates to a method for producing hardened corrosion-protected components with the features of claim 1.
- press-hardened components made of sheet steel are used in automobiles in particular.
- These press-hardened components made of sheet steel are high-strength components that are used in particular as safety components in the bodywork area.
- a sheet steel blank is heated above the so-called austenitizing temperature and, if necessary, kept at this temperature until a desired degree of austenitizing is reached.
- This heated blank is then transferred to a molding tool and in this molding tool it is formed into the finished component in a single-stage forming step, and in the process through the cooled one Mold simultaneously cooled at a rate that is above the critical hardening rate. The hardened component is thus produced.
- the component is first formed almost completely, if necessary in a multi-stage forming process. This formed component is then likewise heated to a temperature above the austenitizing temperature and, if necessary, kept at this temperature for a required time.
- This heated component is then transferred and inserted into a molding tool which already has the dimensions of the component or the final dimensions of the component, possibly taking into account the thermal expansion of the preformed component. After the particularly cooled tool has been closed, the preformed component is therefore only cooled in this tool at a speed above the critical hardening speed and thereby hardened.
- the direct method is somewhat easier to implement here, but only enables shapes that can actually be created with a single forming step, i.e. relatively simple profile shapes.
- the indirect method is a bit more complex, but it is also able to produce more complex shapes.
- Zinc has the advantage that zinc not only provides a barrier protection layer like aluminum, but also a cathodic protection against corrosion.
- zinc-coated press-hardened components fit better into the overall corrosion protection concept of the vehicle body, as these are fully galvanized in today's common construction. In this respect, contact corrosion can be reduced or excluded.
- microcracks can also occur in the coating, which are also undesirable, but not nearly as pronounced.
- the zinc-iron phase diagram shows that above 782 ° C. there is a large area in which liquid zinc-iron phases occur as long as the iron content is low, in particular less than 60%. However, this is also the temperature range in which the austenitized steel is hot worked. However, it is also pointed out that if the deformation takes place above 782 ° C, there is a great risk of stress corrosion due to liquid zinc, which presumably penetrates the grain boundaries of the base steel, which leads to macro cracks in the base steel. In addition, with iron contents less than 30% in the coating, the maximum temperature for forming a safe product without macro cracks is lower than 782 ° C. This is the reason why this is not a direct forming process, but an indirect forming process. This is intended to circumvent the problem described.
- a method for hot forming a coated steel product wherein the steel material has a zinc or zinc alloy coating which is formed on the surface of the steel material and the steel base material with the coating is heated to a temperature of 700 ° C to 1000 ° C and hot worked wherein the coating has an oxide layer consisting mainly of zinc oxide before the steel base material with the zinc or zinc alloy layer is heated in order to then prevent the zinc from evaporating when heated.
- a special procedure is provided for this.
- a method for hot forming a steel in which a component made of a given boron-manganese steel is heated to a temperature at Ac 3 point or higher, is kept at this temperature and then the heated steel sheet is formed into the finished component, wherein the molded component is quenched by cooling from the molding temperature during molding or after molding in such a way that the cooling rate to the MS point is at least equal to the critical cooling rate and that the average cooling rate of the molded component from the MS point at 200 ° C is in the range of 25 ° C / s to 150 ° C / s.
- an oxide skin is formed on the surface of the anti-corrosion coating from the elements with an affinity for oxygen during heating, which protects the cathodic anti-corrosion layer, in particular the zinc layer.
- the method takes into account the thermal expansion of the component due to the scaling down of the component in relation to its final geometry, so that neither calibration nor reshaping is necessary during hot-stamping.
- WO 2010/109012 A1 From the WO 2010/109012 A1 the applicant is known a method for producing partially hardened steel components, wherein a blank made of a hardenable steel sheet is subjected to a temperature increase which is sufficient for quench hardening and the blank is transferred to a forming tool after reaching a desired temperature and possibly a desired holding time by the The blank is formed into a component and quenched hardened at the same time, or the blank is cold formed and the component obtained by the cold forming is then subjected to a temperature increase, the temperature increase being carried out so that a temperature of the component is reached that is necessary for quench hardening is necessary and the component is then transferred to a tool, in which the heated component is cooled and thereby quenched and hardened, with during the heating of the board or the component for the purpose of increasing the temperature to one for hardening necessary temperature in the areas that should have a lower hardness and / or a higher ductility, absorption masses are applied or are spaced with a small gap,
- the object of the invention is to create a method for producing sheet steel components provided with an anti-corrosion layer, in which the formation of cracks is reduced or eliminated and, nevertheless, adequate protection against corrosion is achieved.
- the invention takes a more favorable route by using the direct method in which a plate coated with zinc or a zinc alloy is heated and is reshaped and quench hardened after heating.
- the composition of the steel alloy is set within the scope of the usual composition of a manganese-boron steel (22MnB5) so that quench hardening is carried out, and the presence of austenite also in the case of the delayed conversion of austenite into martensite Lower temperature below 780 ° C or lower is reached, so that at the moment in which mechanical stress is introduced into the steel by deformation, which in connection with a zinc melt and austenite would lead to "liquid metal embrittlement", just none or only very few liquid zinc phases are still present. It is thus possible to achieve sufficient quench hardening by means of a boron-manganese steel adjusted according to the alloying elements without provoking excessive or damaging crack formation.
- the cooling can take place with air nozzles, whereby the control of air nozzles for blowing can take place via pyrometers, which, for example, are available outside the press and the furnace in a separate system as well as the corresponding nozzles.
- the cooling options are not limited to air nozzles, cooled tables can also be used on which the circuit boards are positioned accordingly, so that the circuit boards come to rest on cooled areas of the table and are brought into thermally conductive contact, for example by pressing or sucking.
- a conventional boron-manganese steel (e.g. 22MnB5) for use as a press-hardening steel material is adjusted with regard to the transformation of the austenite into other phases in such a way that the transformation shifts to deeper areas and martensite can be formed.
- the alloying elements boron, manganese, carbon and optionally chromium and molybdenum are used as conversion retarders in such steels.
- quench hardening i. H. rapid cooling with a cooling rate above the critical hardening rate can be safely achieved even below 780 ° C.
- work is carried out below the peritectic of the zinc-iron system, i.e. H. mechanical tension is only applied below the peritectic. This also means that at the moment when mechanical stress is applied, there are no longer any liquid zinc phases that can come into contact with the austenite.
- a holding phase can be provided in the temperature range of the peritectic, so that the solidification of the zinc coating is promoted and promoted before it is subsequently reshaped.
- Figure 1 one recognizes a favorable temperature profile for an austenitized steel sheet, whereby it can be seen that after the heating to a temperature above the austenitizing temperature, a certain cooling already takes place by the corresponding placing in a cooling device. This is followed by a rapid intermediate cooling step.
- the intermediate cooling step is advantageously carried out at cooling rates of at least 15 K / s, preferably at least 30 K / s, more preferably at least 50 K / s.
- the blank is then transferred to the press and reshaped and hardened.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Crystallography & Structural Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Heat Treatment Of Articles (AREA)
- Coating With Molten Metal (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Description
Die Erfindung betrifft ein Verfahren zum Herstellen gehärteter korrosionsgeschützter Bauteile mit den Merkmalen des Anspruchs 1.The invention relates to a method for producing hardened corrosion-protected components with the features of
Es ist bekannt, dass insbesondere in Automobilen sogenannte pressgehärtete Bauteile aus Stahlblech eingesetzt werden. Diese pressgehärteten Bauteile aus Stahlblech sind hochfeste Bauteile, die insbesondere als Sicherheitsbauteile des Karosseriebereichs verwendet werden. Hierbei ist es durch die Verwendung dieser hochfesten Stahlbauteile möglich, die Materialdicke gegenüber einem normalfesten Stahl zu reduzieren und somit geringe Karosseriegewichte zu erzielen.It is known that so-called press-hardened components made of sheet steel are used in automobiles in particular. These press-hardened components made of sheet steel are high-strength components that are used in particular as safety components in the bodywork area. By using these high-strength steel components, it is possible to reduce the material thickness compared to normal-strength steel and thus achieve low body weights.
Beim Presshärten gibt es grundsätzlich zwei verschiedene Möglichkeiten zur Herstellung derartiger Bauteile. Unterschieden wird in das sogenannte direkte und indirekte Verfahren.In press hardening, there are basically two different ways of producing such components. A distinction is made between the so-called direct and indirect method.
Beim direkten Verfahren wird eine Stahlblechplatine über die sogenannten Austenitisierungstemperatur aufgeheizt und gegebenenfalls so lange auf dieser Temperatur gehalten, bis ein gewünschter Austenitisierungsgrad erreicht ist. Anschließend wird diese erhitzte Platine in ein Formwerkzeug überführt und in diesem Formwerkzeug in einem einstufigen Umformschritt zum fertigen Bauteil umgeformt und hierbei durch das gekühlte Formwerkzeug gleichzeitig mit einer Geschwindigkeit, die über der kritischen Härtegeschwindigkeit liegt, abgekühlt. Somit wird das gehärtete Bauteil erzeugt.In the direct method, a sheet steel blank is heated above the so-called austenitizing temperature and, if necessary, kept at this temperature until a desired degree of austenitizing is reached. This heated blank is then transferred to a molding tool and in this molding tool it is formed into the finished component in a single-stage forming step, and in the process through the cooled one Mold simultaneously cooled at a rate that is above the critical hardening rate. The hardened component is thus produced.
Beim indirekten Verfahren wird zunächst, gegebenenfalls in einem mehrstufigen Umformprozess, das Bauteil fast vollständig fertig umgeformt. Dieses umgeformte Bauteil wird anschließend ebenfalls auf eine Temperatur über die Austenitisierungstemperatur erhitzt und gegebenenfalls für eine gewünschte erforderliche Zeit auf dieser Temperatur gehalten.In the case of the indirect process, the component is first formed almost completely, if necessary in a multi-stage forming process. This formed component is then likewise heated to a temperature above the austenitizing temperature and, if necessary, kept at this temperature for a required time.
Anschließend wird dieses erhitzte Bauteil in ein Formwerkzeug überführt und eingelegt, welches schon die Abmessungen des Bauteils bzw. die Endabmessungen des Bauteils gegebenenfalls unter Berücksichtigung der Wärmedehnung des vorgeformten Bauteils besitzt. Nach dem Schließen des insbesondere gekühlten Werkzeuges wird somit das vorgeformte Bauteil lediglich in diesem Werkzeug mit einer Geschwindigkeit über der kritischen Härtegeschwindigkeit abgekühlt und dadurch gehärtet.This heated component is then transferred and inserted into a molding tool which already has the dimensions of the component or the final dimensions of the component, possibly taking into account the thermal expansion of the preformed component. After the particularly cooled tool has been closed, the preformed component is therefore only cooled in this tool at a speed above the critical hardening speed and thereby hardened.
Das direkte Verfahren ist hierbei etwas einfacher zu realisieren, ermöglicht jedoch nur Formen, die tatsächlich mit einem einzigen Umformschritt zu realisieren sind, d.h. relativ einfache Profilformen.The direct method is somewhat easier to implement here, but only enables shapes that can actually be created with a single forming step, i.e. relatively simple profile shapes.
Das indirekte Verfahren ist etwas aufwendiger, dafür aber in der Lage auch komplexere Formen zu realisieren.The indirect method is a bit more complex, but it is also able to produce more complex shapes.
Zusätzlich zum Bedarf an pressgehärteten Bauteilen entstand der Bedarf, derartige Bauteile nicht aus unbeschichtetem Stahlblech zu erzeugen, sondern derartige Bauteile mit einer Korrosionsschutzschicht zu versehen.In addition to the need for press-hardened components, the need arose not to produce such components from uncoated sheet steel, but to provide such components with a corrosion protection layer.
Als Korrosionsschutzschicht kommen im Automobilbau lediglich das eher in geringem Maße verwendete Aluminium oder Aluminiumlegierungen in Frage oder aber die erheblich häufiger verlangten Beschichtungen auf der Basis von Zink. Zink hat hierbei den Vorteil, dass Zink nicht nur eine Barriereschutzschicht wie Aluminium leistet, sondern einen kathodischen Korrosionsschutz. Zudem passen sich zinkbeschichtete pressgehärtete Bauteile besser in das Gesamtkorrosionsschutzkonzept der Fahrzeugkarosserien ein, da diese in heute gängiger Bauweise voll verzinkt sind. Insofern kann Kontaktkorrosion vermindert oder ausgeschlossen werden.Only aluminum or aluminum alloys, which are used to a lesser extent, or the much more frequently required zinc-based coatings are suitable as a corrosion protection layer in automobile construction. Zinc has the advantage that zinc not only provides a barrier protection layer like aluminum, but also a cathodic protection against corrosion. In addition, zinc-coated press-hardened components fit better into the overall corrosion protection concept of the vehicle body, as these are fully galvanized in today's common construction. In this respect, contact corrosion can be reduced or excluded.
Bei beiden Verfahren konnten jedoch Nachteile aufgefunden werden, die auch im Stand der Technik diskutiert werden. Bei dem direkten Verfahren, d.h. der Warmumformung von presshärtenden Stählen mit Zinkbeschichtung kommt es zu Mikro- (10 µm bis 100 µm) oder sogar Makrorissen im Material, wobei die Mikrorisse in der Beschichtung erscheinen und die Makrorisse sogar durch den vollständigen Blechquerschnitt reichen. Derartige Bauteile mit Makrorissen sind für die weitere Verwendung ungeeignet.In both processes, however, disadvantages could be found which are also discussed in the prior art. In the direct process, i.e. the hot forming of press-hardening steels with zinc coating, micro (10 µm to 100 µm) or even macro cracks occur in the material, whereby the micro cracks appear in the coating and the macro cracks even extend through the entire sheet metal cross-section. Such components with macro cracks are unsuitable for further use.
Beim indirekten Prozess, d.h. der Kaltumformung mit einer anschließenden Härtung und Restformung kann es ebenfalls zu Mikrorissen in der Beschichtung kommen, welche ebenfalls unerwünscht sind, aber bei weitem nicht so ausgeprägt.In the indirect process, i.e. cold forming with subsequent hardening and residual forming, microcracks can also occur in the coating, which are also undesirable, but not nearly as pronounced.
Zinkbeschichtete Stähle werden bislang - bis auf ein Bauteil im asiatischen Raum - im direkten Verfahren, d.h. der Warmumformung, nicht eingesetzt. Hier werden vielmehr Stähle mit einer Aluminium-Silizium-Beschichtung eingesetzt.Up to now, zinc-coated steels have not been used in the direct process, i.e. hot forming, with the exception of one component in Asia. Rather, steels with an aluminum-silicon coating are used here.
Einen Überblick erhält man in der Veröffentlichung "Corrosion resistance of different metallic coatings on press hardened steels for automotive", Arcelor Mittal Maiziere Automotive Product Research Center F-57283 Maiziere-Les-Mez. In dieser Veröffentlichung wird ausgeführt, dass es für den Warmumformprozess einen aluminierten Bor-Mangan-Stahl gibt, der unter dem Namen Usibor 1500P kommerziell vertrieben wird. Zudem werden zum Zwecke des kathodischen Korrosionsschutzes zinkvorbeschichtete Stähle für das Warmumformverfahren vertrieben, nämlich der verzinkte Usibor GI mit einer Zinkbeschichtung, die geringe Anteile von Aluminium enthält und ein sogenannter galvanealed beschichteter Usibor GA, der eine Zinkschicht mit 10 % Eisen enthält.An overview can be found in the publication "Corrosion resistance of different metallic coatings on press hardened steels for automotive", Arcelor Mittal Maiziere Automotive Product Research Center F-57283 Maiziere-Les-Mez. In this publication it is stated that there is an aluminized boron-manganese steel for the hot forming process, which is sold commercially under the name Usibor 1500P. In addition, for the purpose of cathodic corrosion protection, steels precoated with zinc are sold for the hot forming process, namely the galvanized Usibor GI with a zinc coating that contains a small amount of aluminum and a so-called galvanealed coated Usibor GA, which contains a zinc layer with 10% iron.
Es wird darauf hingewiesen, dass das Zink-Eisen-Phasendiagramm zeigt, dass oberhalb von 782°C ein großer Bereich entsteht, in dem flüssige Zink-Eisen-Phasen auftreten, solange der Eisengehalt gering, insbesondere geringer als 60 % ist. Dies ist jedoch auch der Temperaturbereich, in dem der austenitisierte Stahl warm umgeformt wird. Es wird aber auch darauf hingewiesen, dass, wenn die Umformung oberhalb von 782°C stattfindet, ein großes Risiko der Spannungskorrosion durch flüssiges Zink besteht, welches vermutlich in die Korngrenzen des Basisstahls eindringt, welche zu Makrorissen im Basisstahl führt. Darüber hinaus ist bei Eisengehalten geringer als 30 % in der Beschichtung die Maximaltemperatur zum Umformen eines sicheren Produkts ohne Makrorisse niedriger als 782°C. Dies ist der Grund, warum hiermit kein direktes Umformverfahren betrieben wird, sondern dass indirekte Umformverfahren. Hiermit soll das geschilderte Problem umgangen werden.It should be noted that the zinc-iron phase diagram shows that above 782 ° C. there is a large area in which liquid zinc-iron phases occur as long as the iron content is low, in particular less than 60%. However, this is also the temperature range in which the austenitized steel is hot worked. However, it is also pointed out that if the deformation takes place above 782 ° C, there is a great risk of stress corrosion due to liquid zinc, which presumably penetrates the grain boundaries of the base steel, which leads to macro cracks in the base steel. In addition, with iron contents less than 30% in the coating, the maximum temperature for forming a safe product without macro cracks is lower than 782 ° C. This is the reason why this is not a direct forming process, but an indirect forming process. This is intended to circumvent the problem described.
Eine weitere Möglichkeit dieses Problem zu umgehen, soll darin liegen, galvannealed beschichteten Stahl zu verwenden, was daran liegt, dass der zu Beginn schon bestehende Eisengehalt von 10 % und die Abwesenheit einer Fe2Al5-Sperrschicht zu einer homogeneren Ausbildung des Beschichtung von überwiegend eisenreichen Phasen führt. Dies resultiert in einer Verringerung oder Vermeidung von zinkreichen, flüssigen Phasen.Another possibility to circumvent this problem is to use galvannealed coated steel, which is due to the fact that the iron content of 10% already existing at the beginning and the absence of an Fe 2 Al 5 barrier layer lead to a more homogeneous formation of the coating of predominantly rich in iron Phases leads. This results in a reduction or avoidance of zinc-rich, liquid phases.
In "
Aus der
Aus der
Aus der
Aus der
Aus der
Aufgabe der Erfindung ist es, ein Verfahren zum Herstellen von mit einer Korrosionsschutzschicht versehenen Stahlblechbauteilen zu schaffen, bei dem die Rissbildung vermindert oder beseitigt wird und dennoch ein ausreichender Korrosionsschutz erzielt wird.The object of the invention is to create a method for producing sheet steel components provided with an anti-corrosion layer, in which the formation of cracks is reduced or eliminated and, nevertheless, adequate protection against corrosion is achieved.
Die Aufgabe wird mit den Merkmalen des Anspruchs 1 gelöst.The object is achieved with the features of
Vorteilhafte Weiterbildungen sind in Unteransprüchen gekennzeichnet.Advantageous further developments are characterized in the subclaims.
Der vorbeschriebene Effekt der Rissbildung durch flüssiges Zink, welches den Stahl im Bereich der Korngrenzen penetriert, ist auch als sogenanntes "liquid metal embrittlement" oder "liquid metal assisted cracking" bekannt.The above-described effect of crack formation by liquid zinc, which penetrates the steel in the area of the grain boundaries, is also known as so-called "liquid metal embrittlement" or "liquid metal assisted cracking".
Im Gegensatz zur im Stand der Technik eingeschlagenen Richtung, wegen des "liquid metal embrittlements" das indirekte Verfahren auch bei einfachen Geometrien vorzusehen, geht die Erfindung einen günstigeren Weg indem das direkte Verfahren Anwendung findet, bei dem eine mit Zink oder einer Zinklegierung beschichtete Platine aufgeheizt wird und nach dem Aufheizen umgeformt und abschreckgehärtet wird.In contrast to the direction taken in the prior art of providing the indirect method even with simple geometries because of the "liquid metal embrittlements", the invention takes a more favorable route by using the direct method in which a plate coated with zinc or a zinc alloy is heated and is reshaped and quench hardened after heating.
Wie erfindungsgemäß erkannt wurde darf möglichst keine Zinkschmelze mit Austenit während der Umformphase, also dem Eintrag von Spannung, in Berührung kommen. Erfindungsgemäß wird daher vorgesehen, die Umformung unter der peritektischen Temperatur des Systems Eisen-Zink (Schmelze, Ferrit, Gamma-Phase) durchzuführen. Um hierbei eine Abschreckhärtung noch gewährleisten zu können wird die Zusammensetzung der Stahllegierung im Rahmen der üblichen Zusammensetzung eines Mangan-Borstahles (22MnB5) so eingestellt, dass eine Abschreckhärtung durchgeführt, und dabei durch eine verzögerte Umwandlung des Austenits in Martensit das Vorhandensein von Austenit auch bei der tieferen Temperatur unterhalb von 780°C oder tiefer erreicht wird, so dass in dem Moment in dem mechanische Spannung durch Umformung auf den Stahl eingebracht wird, welche in Verbindung mit einer Zinkschmelze und Austenit zum "liquid metal embrittlement" führen würde, eben keine oder nur noch sehr wenige flüssige Zinkphasen vorhanden sind. Somit gelingt es mittels eines entsprechend der Legierungselemente eingestellten Bor-Manganstahls eine ausreichende Abschreckhärtung zu erzielen ohne eine übermäßige oder schädigende Rissbildung zu provozieren.As was recognized according to the invention, as far as possible no zinc melt should come into contact with austenite during the forming phase, that is to say when stress is introduced. According to the invention It is therefore intended to carry out the forming under the peritectic temperature of the iron-zinc system (melt, ferrite, gamma phase). In order to still be able to guarantee quench hardening, the composition of the steel alloy is set within the scope of the usual composition of a manganese-boron steel (22MnB5) so that quench hardening is carried out, and the presence of austenite also in the case of the delayed conversion of austenite into martensite Lower temperature below 780 ° C or lower is reached, so that at the moment in which mechanical stress is introduced into the steel by deformation, which in connection with a zinc melt and austenite would lead to "liquid metal embrittlement", just none or only very few liquid zinc phases are still present. It is thus possible to achieve sufficient quench hardening by means of a boron-manganese steel adjusted according to the alloying elements without provoking excessive or damaging crack formation.
Insbesondere kann die Kühlung mit Luftdüsen erfolgen, wobei die Steuerung von Luftdüsen zum Anblasen über Pyrometer erfolgen kann, die beispielsweise außerhalb der Presse und des Ofens in einer gesonderten Anlage ebenso wie die entsprechenden Düsen vorhanden sind.In particular, the cooling can take place with air nozzles, whereby the control of air nozzles for blowing can take place via pyrometers, which, for example, are available outside the press and the furnace in a separate system as well as the corresponding nozzles.
Die Kühlmöglichkeiten sind hierbei nicht auf Luftdüsen beschränkt, es können auch gekühlte Tische verwendet werden auf denen die Platinen entsprechend positioniert werden, so dass die Platinen auf abgekühlten Bereichen des Tisches zu liegen kommen und beispielsweise durch Aufdrücken oder Ansaugen in wärmeleitenden Kontakt gebracht werden.The cooling options are not limited to air nozzles, cooled tables can also be used on which the circuit boards are positioned accordingly, so that the circuit boards come to rest on cooled areas of the table and are brought into thermally conductive contact, for example by pressing or sucking.
Auch der Einsatz einer Kühlpresse ist denkbar, bei der die Pressengeometrie durch die ebenen Platinen denkbar einfach und günstig ist, wobei die Bereiche des Werkzeugs in denen die Platine abgekühlt werden soll entsprechend flüssig gekühlt sind. Vollflächig aufgeheizte Platinen können in entsprechenden Einrichtungen somit vollflächig abgekühlt werden, wobei die vollflächige Abkühlung sowohl über die beschriebenen Tische als auch über die beschriebenen Zwischenpressen als auch über einfaches Ansprühen, Anblasen oder Eintauchen erfolgen kann.The use of a cooling press is also conceivable, in which the press geometry is very simple and easy thanks to the flat plates is favorable, the areas of the tool in which the board is to be cooled are correspondingly liquid-cooled. Blanks that have been heated over the entire surface can thus be cooled over the entire surface in corresponding devices, with the entire surface cooling being able to take place both via the described tables and via the intermediate presses described as well as simply by spraying, blowing or dipping.
Die Erfindung wird anhand einer Zeichnung erläutert, es zeigen dabei:
- Figur 1:
- die Zeit-Temperaturkurve bei der Abkühlung zwischen Ofen und Umformung;
- Figur 2:
- das Zink-Eisen-Diagramm;
- Figur 3:
- Querschnittschliffdarstellungen der Oberfläche von Proben mit und ohne Zwischenkühlung;
- Figur 4:
- ZTU-Schaubild mit vereinfachter Darstellung des Abkühlverlaufs.
- Figure 1:
- the time-temperature curve during cooling between furnace and forming;
- Figure 2:
- the zinc-iron diagram;
- Figure 3:
- Cross-sectional views of the surface of samples with and without intermediate cooling;
- Figure 4:
- ZTU diagram with a simplified representation of the cooling process.
Erfindungsgemäß wird ein üblicher Bor-Manganstahl (z.B. 22MnB5) zur Verwendung als presshärtender Stahlwerkstoff bezüglich der Umwandlung des Austenits in andere Phasen so eingestellt, dass sich die Umwandlung in tiefere Bereiche verschiebt und Martensit gebildet werden kann.According to the invention, a conventional boron-manganese steel (e.g. 22MnB5) for use as a press-hardening steel material is adjusted with regard to the transformation of the austenite into other phases in such a way that the transformation shifts to deeper areas and martensite can be formed.
Für die Erfindung sind somit Stähle dieser Legierungszusammensetzung geeignet (alle Angaben in Masse-%):
Wobei als Umwandlungsverzögerer in derartigen Stählen insbesondere die Legierungselemente Bor, Mangan, Kohlenstoff und optional Chrom und Molybdän verwendet werden.The alloying elements boron, manganese, carbon and optionally chromium and molybdenum are used as conversion retarders in such steels.
Für die Erfindung sind auch Stähle der allgemeinen Legierungszusammensetzung geeignet (alle Angaben in Masse-%):
Insbesondere als geeignet erwiesen haben sich Stahlanordnungen wie folgt (alle Angaben in Masse-%):
Durch die Einstellung der als Umwandlungsverzögerer wirkenden Legierungselemente wird eine Abschreckhärtung, d. h. eine rasche Abkühlung mit einer über der kritischen Härtegeschwindigkeit liegenden Abkühlgeschwindigkeit auch noch unter 780°C sicher erreicht. Dies bedeutet, dass in diesem Fall unterhalb des Peritektikums des Systems Zink-Eisen gearbeitet wird, d. h. erst unterhalb des Peritektikums mechanische Spannung aufgebracht wird. Dies bedeutet ferner, dass in dem Moment in dem mechanische Spannung aufgebracht wird, keine flüssigen Zinkphasen mehr vorhanden sind welche mit dem Austenit in Kontakt kommen können.By adjusting the alloying elements that act as conversion retarders, quench hardening, i. H. rapid cooling with a cooling rate above the critical hardening rate can be safely achieved even below 780 ° C. This means that in this case work is carried out below the peritectic of the zinc-iron system, i.e. H. mechanical tension is only applied below the peritectic. This also means that at the moment when mechanical stress is applied, there are no longer any liquid zinc phases that can come into contact with the austenite.
Zudem kann nach dem Aufheizen der Platine erfindungsgemäß im Temperaturbereich des Peritektikums eine Haltephase vorgesehen sein, so dass die Erstarrung der Zinkbeschichtung gefördert und vorangetrieben wird bevor anschließend umgeformt wird.In addition, according to the invention, after the blank has been heated, a holding phase can be provided in the temperature range of the peritectic, so that the solidification of the zinc coating is promoted and promoted before it is subsequently reshaped.
In
In
Mit der Erfindung gelingt es somit, zuverlässig ein kostengünstiges Warmumformverfahren für mit Zink oder Zinklegierungen beschichteter Stahlbleche zu erreichen bei dem einerseits eine Abschreckhärtung herbeigeführt wird und andererseits Mikro- und Makrorissbildung, die zu Bauteilschäden führt, vermindert oder vermieden wird.With the invention it is thus possible to reliably achieve a cost-effective hot forming process for steel sheets coated with zinc or zinc alloys in which, on the one hand, quench hardening is brought about and, on the other hand, micro and macro cracking, which leads to component damage, is reduced or avoided.
Claims (5)
- Method of producing a hardened steel component with a coating of zinc or of a zinc alloy, wherein a blank is stamped out of a sheet coated with the zinc or zinc alloy, the stamped out blank is heated to a temperature ≥Ac3 and, if necessary, held at this temperature for a predetermined time to allow austenite to form, after which the heated blank is transferred into a forming tool, is formed in the forming tool at a speed which exceeds the critical hardening speed, is cooled down and is hardened thereby, in which the steel material is delayed in its conversion such that, at a forming temperature in the range of 450°C to 700°C and below the peritectic temperature of the zinc-iron system, quench hardening to convert the austenite into martensite takes place, upon which, after heating and before the conversion, active cooling takes place wherein the blank or parts of the blank is/are cooled down at a cooling speed >15K/sec wherein a steel material is used with the following analysis (all data in % by mass):
Carbon (C) 0.08-0.6 Manganese (Mn) 0.8-3.0 Aluminium (Al) 0.01-0.07 Silicon (Si) 0.01-0.5 Chromium (Cr) 0.02-0.6 Titanium (Ti) 0.01-0.08 Nitrogen (N) < 0.02 Boron (B) 0.002-0.02 Phosphorus (P) < 0.01 Sulphur (S) <0.01 Molybdenum (Mo) < 1 - Method according to claim 1 characterised in that a steel material with the following analysis is used (all data on % by mass):
Carbon (C) 0.08-0.30 Manganese (Mn) 1.00-3.00 Aluminium (Al) 0.03-0.06 Silicon (Si) 0.01-0.20 Chromium (Cr) 0.02-0.3 Titanium (Ti) 0.03-0.04 Nitrogen (N) < 0.007 Boron (B) 0.002-0.006 Phosphorus (P) < 0.01 Sulphur (S) <0.01 Molybdenum (Mo) < 1 - Method according to any one of the preceding claims, characterised in that the active cooling is performed such that the cooling down rate is >30 K/sec.
- Method according to claim 3, characterised in that the active cooling is performed such that the cooling takes place at a rate greater than 50 K/sec.
- Method according to any one of the preceding claims, characterised in that the active cooling is executed by blowing with air or gas, spraying with water or with other cooling fluids, immersing in water or in other cooling fluids or the active cooling is achieved by placing cooler solid bodies on the blank.
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DE102010056264.5A DE102010056264C5 (en) | 2010-12-24 | 2010-12-24 | Process for producing hardened components |
DE102010056265.3A DE102010056265C5 (en) | 2010-12-24 | 2010-12-24 | Process for producing hardened components |
DE102011053941.7A DE102011053941B4 (en) | 2011-09-26 | 2011-09-26 | Method for producing hardened components with regions of different hardness and / or ductility |
DE102011053939.5A DE102011053939B4 (en) | 2011-09-26 | 2011-09-26 | Method for producing hardened components |
PCT/EP2011/073880 WO2012085247A2 (en) | 2010-12-24 | 2011-12-22 | Method for producing hardened structural elements |
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EP11808645.3A Active EP2655674B1 (en) | 2010-12-24 | 2011-12-22 | Method for forming and hardening coated steel sheets |
EP11811026.1A Active EP2656187B1 (en) | 2010-12-24 | 2011-12-22 | Method for producing hardened structural elements |
EP11808211.4A Active EP2655673B1 (en) | 2010-12-24 | 2011-12-22 | Method for producing hardened structural elements |
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