EP3414072B1 - Procédé et dispositif de fabrication de pièces en acier trempé - Google Patents
Procédé et dispositif de fabrication de pièces en acier trempé Download PDFInfo
- Publication number
- EP3414072B1 EP3414072B1 EP17707480.4A EP17707480A EP3414072B1 EP 3414072 B1 EP3414072 B1 EP 3414072B1 EP 17707480 A EP17707480 A EP 17707480A EP 3414072 B1 EP3414072 B1 EP 3414072B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- oxygen
- free
- blade
- positive
- moulding tool
- 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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- 238000000034 method Methods 0.000 title claims description 27
- 229910000760 Hardened steel Inorganic materials 0.000 title description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 27
- 239000010959 steel Substances 0.000 claims description 27
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 24
- 229910052760 oxygen Inorganic materials 0.000 claims description 24
- 239000001301 oxygen Substances 0.000 claims description 24
- 239000012530 fluid Substances 0.000 claims description 21
- 238000000465 moulding Methods 0.000 claims description 7
- 238000010791 quenching Methods 0.000 claims description 4
- 238000007493 shaping process Methods 0.000 claims description 3
- 230000000171 quenching effect Effects 0.000 claims 3
- 229910000851 Alloy steel Inorganic materials 0.000 claims 1
- 239000000463 material Substances 0.000 description 12
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 11
- 239000011701 zinc Substances 0.000 description 11
- 229910052725 zinc Inorganic materials 0.000 description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000011651 chromium Substances 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 238000009966 trimming Methods 0.000 description 4
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- KFZAUHNPPZCSCR-UHFFFAOYSA-N iron zinc Chemical compound [Fe].[Zn] KFZAUHNPPZCSCR-UHFFFAOYSA-N 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000010309 melting process Methods 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000975 Carbon steel Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- QFGIVKNKFPCKAW-UHFFFAOYSA-N [Mn].[C] Chemical compound [Mn].[C] QFGIVKNKFPCKAW-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910001335 Galvanized steel Inorganic materials 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- PALQHNLJJQMCIQ-UHFFFAOYSA-N boron;manganese Chemical compound [Mn]#B PALQHNLJJQMCIQ-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010924 continuous production Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000008397 galvanized steel Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011344 liquid material Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 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
- 229910000734 martensite Inorganic materials 0.000 description 1
- 229910052756 noble gas Inorganic materials 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Images
Classifications
-
- 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
Definitions
- the invention relates to a method and a device for producing hardened steel components.
- Hardened steel components have the advantage, particularly in the body shop of motor vehicles, that their outstanding mechanical properties make it possible to create a particularly stable passenger cell without having to use components that are much more massive and therefore heavier with normal strengths.
- types of steel which can be hardened by quench hardening are used.
- types of steel are, for example, boron-alloyed manganese carbon steels, the most widely used here being 22MnB5.
- other boron-alloyed manganese carbon steels are also used for this purpose.
- the steel material In order to produce components hardened from these types of steel, the steel material must be heated to the austenitizing temperature (> AC 3 ) and wait until the steel material is austenitized. Depending on the required degree of hardness, partial or full austenitization can be achieved here.
- a sheet steel blank is separated from a steel strip, e.g. cut or punched and then deep-drawn into the finished component in a conventional, for example five-step deep-drawing process.
- This finished component is dimensioned slightly smaller in order to compensate for a subsequent thermal expansion during austenitizing.
- the component produced in this way is then austenitized and then placed in a form hardening tool, in which it is pressed, but not or only very slightly deformed, and the heat flows from the component into the pressing tool as a result of the compression, at a rate that is above the critical hardening speed Speed.
- the further method is the so-called press hardening, in which a plate is separated from a sheet steel strip, bsp. is cut or punched, then the blank is austenitized and the hot blank is formed at a temperature below 782 ° C in a preferably one-stage step and at the same time cooled at a rate above the critical hardening speed.
- metallic corrosion protection layers can be used, e.g. plates provided with zinc or an alloy based on zinc can be used.
- Press hardening is also known as an indirect process and press hardening as a direct process. The advantage of the indirect process is that more complex workpiece geometries can be implemented.
- the advantage of the direct process is that a higher degree of material utilization can be achieved. However that is achievable component complexity is lower, especially in the one-step forming process.
- First-order micro-cracks are attributed to the so-called liquid metal embrittlement. It is believed that liquid zinc phases during forming, i.e. While tensile stresses are applied to the material, they interact with the remaining austenite phases, as a result of which microcracks with depths of up to several 100 ⁇ m are generated in the material.
- the applicant has succeeded in preventing these first-order microcracks by actively or passively cooling the material between removal from the heating furnace and before the start of the hot forming process to temperatures at which there are no longer any liquid zinc phases. This means that the hot forming takes place at temperatures below approx. 750 ° C.
- the second-order microcracks have so far not been manageable in hot forming despite pre-cooling and also arise at hot forming temperatures below 600 ° C.
- the crack depths here are up to a few 10 ⁇ m.
- a method and forming tool for hot forming press hardening of workpieces made of sheet steel is known, and in particular of galvanized workpieces made of sheet steel.
- the die used for hot forming and press hardening should be coated with a liquid material in its drawing edge area defined by a positive drawing radius or provided with an insert that has a thermal conductivity that is at least 10 W / (mx K) lower than the thermal conductivity of the section of the die adjacent to the drawing edge area, which comes into contact with the workpiece during hot forming and press hardening.
- the surface of the material applied in the drawing edge area or the arranged insert part facing the workpiece should have a transverse dimension extending over the drawing edge that is in the range of 1.6 to 10 times the positive drawing radius of the die. This is intended to improve the flow properties of workpieces made of sheet steel during hot forming and thus considerably reduce the risk of cracks occurring during hot forming of workpieces made of sheet steel, preferably galvanized steel blanks. With such a tool, however, microcracks of the second type cannot be avoided.
- a tool for a press hardening tool is known, the shaping surface of the tool being microstructured in some areas by two micro-depressions made in the mold surface.
- the effective contact area for the deformation of a blank between the mold surface with a blank on the Area portions located between the depressions are limited to four. This is intended to reduce friction.
- a method and a device for producing a partially hardened molded part comprising the following steps: heating a semifinished product to a hardening temperature, hot forming of the heated semifinished product in a combined hot forging cutting device to form a three-dimensional molded part, trimming of the molded part in the combined Hot forming cutting device and partial press hardening of the molded part.
- molded parts can be hot formed, trimmed and partially hardened in one step.
- a post-processing a separate trimming process in a separate trimming tool can be omitted. In this way, undesired changes in terms of shape and structure of the molded parts can be minimized.
- the object of the invention is to avoid microcracks of the second type in directly hot-formed, ie press-hardened, components.
- VME vapor metal embrittlement
- second order microcracks are to be avoided, with the largest possible working window in terms of material and temperature being retained and the implementation being inexpensive. With at least the same throughput time, there should be no increase in cycle time or throughput reduction in component production.
- the zinc vapor occurring in the tensile stressed areas is either discharged or blown off by gas flows (convection) or is sufficiently diluted.
- zinc can be rapidly converted into a stable compound such as zinc oxide or ZnJ2 through the admission of fluids.
- the steel can also be protected against second-order microcracks by producing a protective layer such as an oxide layer by supplying a fluid. All the measures described have shown that microcracks are significantly reduced.
- gaseous oxygen-containing fluids such as air or oxygen, for example, since these cannot contaminate the tool excessively or also any undesired massive cooling effect such as by ex.
- Water can be more easily regulated by controlling the temperature of the fluid.
- the avoidance of the second-order microcracks is ensured by the fact that in the area of the positive radii, i.e. in the area of the drawing edges of the die and / or the male part in the drawing direction, there is a recess adjacent to the drawing edge or other contact areas outside the positive radii / drawing edge, which is dimensioned so that on the one hand the deep drawing is not impaired or the board or the workpiece becomes wavy and on the other hand is dimensioned so that the heat flow, which is necessary for the hardening, is also not significantly impaired.
- the clearances are dimensioned in such a way that they represent a reservoir for oxygen in such a way that sufficient oxygen reaches the pulling plate or the material to supply the released zinc phases or zinc iron phases with oxygen for oxidation.
- the recess acts as a fluid reservoir in particular for oxygen, but this reservoir can also contain other fluids, such as water or nitrogen. If these are filled with a noble gas or, in particular, are also continuously flushed with it, they do not act through oxidation but rather through dilution or removal of the zinc vapor that occurs.
- the recesses on the tool side are advantageously continuously fed with fluids containing oxygen during the forming process, for example through suitable access openings, whereby a flow cushion can advantageously be formed.
- the tool cavity can be rinsed with a fluid, in particular an oxygen-containing fluid, which is then present in the recesses.
- an oxygen-containing fluid are air as well as water i.e. these can be supplied in liquid or gaseous form.
- the drawing edge region 1 or region of a positive radius 1 is arranged on a molding tool and has two workpiece-side surfaces 3, 4 which meet in the region of a drawing edge or a positive radius 2.
- a recess 5 according to the invention is arranged in a surface 4 following the drawing edge 2 in the drawing direction.
- the recess 5 is dimensioned in such a way that the remaining thickness of the drawing edge 2 between the surface 3 and the recess 5 approximately corresponds to its radius in order to offer a sufficient support effect for the material to be drawn.
- the recess 5 has a height between the drawing edge 2 and the surface 4 which is approximately 25 to 35 mm, with a depth of 5 to 9 mm.
- Figure 2 is instead of a larger recess 5 adjacent to Drawing edge 2, and leaving this in the thickness already described, introduced a groove 6 into surface 4.
- the groove 6 has a height between the surface 4 and the drawing edge 2, which is approximately 8 to 12 mm, with a depth of 5 to 9 mm.
- the grooves 7 or slots 7 instead of a continuous recess 5 in the area of the wall 4 adjacent to the drawing edge 2, there is a plurality of grooves 7 running in the drawing direction, the grooves 7 or slots 7, for example, having a slot width of 4 to 8 mm and a slot spacing of 7 up to 11 mm, so that the remaining webs have a width of 1 to 5 mm.
- the grooves 7 or slots 7 here also have a depth of 5 to 9 mm.
- the recesses 5, the groove 6, the slots 7 can be on the rear side, i.e. be supplied with an oxygen-containing fluid from the tool, by means of feeds and correspondingly drilled lines, in order, if necessary, to further increase the oxygen partial pressure in the area of the recesses 5, grooves 6 and slots 7.
- the mold cavity can also be flushed with an oxygen-containing fluid so that there is always enough oxygen reservoir in the clearances 5, grooves 6 and slots 7 is.
- the 20MnB8, 22MnB8 and other manganese-boron steels are also used - especially in the direct press hardening process.
- the remainder is iron and impurities caused by the melting process, the alloy elements boron, manganese, carbon and optionally chromium and molybdenum being used as conversion retarders in such steels.
- the remainder is iron and impurities from the melting process.
- the remainder is iron and impurities from the melting process.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Heat Treatment Of Articles (AREA)
Claims (8)
- Procédé pour produire des composants en tôle d'acier trempés sous presse, une platine étant détachée d'un feuillard d'acier en alliage d'acier durcissable et la platine étant ensuite austénitisée en la chauffant à une température supérieure à Ac3 puis en la déposant dans un outil de façonnage et en la façonnant dans l'outil de façonnage et en la refroidissant lors du façonnage à une vitesse supérieure à la vitesse de trempe critique, caractérisé en ce que, pour éviter des microfissures de second type sur les platines en tôle à façonner pendant l'opération de trempe et de façonnage, un réservoir à liquide contenant de l'oxygène est présent- adjacent aux rayons positifs et/ou aux bords d'emboutissage et/ou- à d'autres zones de contact en dehors des rayons positifs et/ou des bords d'emboutissage, des évidements côté outil de formage étant alimentés en liquides ou oxygène ou en liquides contenant de l'oxygène.
- Procédé selon la revendication 1, caractérisé en ce que l'entrée en oxygène s'effectue par des évidements prévus dans l'outil de formage adjacent aux bords d'emboutissage et/ou aux rayons positifs, évidements étant dimensionnés de telles manière que l'emboutissage n'est pas entravé et l'évidement forme un réservoir pour du liquide contenant de l'oxygène ou du liquide contenant de l'oxygène peut être alimenté par cet évidement.
- Procédé selon l'une des revendications précédentes, caractérisé en ce que l'entrée de liquide contenant de l'oxygène est assurée par l'air contenu dans les évidements.
- Procédé selon l'une des revendications précédentes, caractérisé en ce que l'aspiration se fait par les évidements.
- Procédé selon la revendication 1, caractérisé en ce que le liquide contenant de l'oxygène est alimenté en permanence.
- Dispositif pour la mise en œuvre du procédé selon l'une des revendications précédentes, avec deux moitiés d'outil de formage, les deux moitiés d'outil de formage formant une platine à interaction par emboutissage et pouvant être commandées l'une vers l'autre et s'éloigner l'une de l'autre, au moins un rayon positif (1) ou une zone de bord d'emboutissage (1) étant prévu avec un bord d'emboutissage (2) selon un contour de façonnage souhaité, un évidement (5) étant prévu- dans une surface (4) suivant le bord d'emboutissage (2) ou le rayon positif (1) dans le sens d'emboutissage et/ou- à d'autres zones de contact en dehors des rayons positifs (1) et/ou des bords d'emboutissage (2), les évidements (5), les rainures (6) ou les fentes (7) pouvant être alimentés en liquide contenant de l'oxygène à l'arrière, c.-à-d. à partir de l'outil, au moyen d'amenées et des conduites percées en conséquence.
- Dispositif selon la revendication 6, caractérisé en ce que l'évidement (5) est dimensionné de telle manière que l'épaisseur restante du bord d'emboutissage (2) entre une surface délimitant le bord d'emboutissage (2) et l'évidement (5) correspond approximativement à son rayon.
- Dispositif selon la revendication 6 ou 7, caractérisé en ce que l'évidement (5) entre le bord d'emboutissage (2) et une surface d'outil de formage (4) présente une hauteur d'environ 25 à 35 mm avec une profondeur de 5 à 9 mm ou est formé comme une rainure (6) qui présente une hauteur d'environ 8 à 12 mm avec une profondeur de 5 à 9 mm entre la surface (4) et le bord d'emboutissage (2) ou en ce qu'une multitude de rainures (7) s'étendant dans le sens d'emboutissage sont présentes comme des évidements dans la zone de la paroi (4) adjacente au bord d'emboutissage (2), les rainures (7) ou fentes (7) présentant une largeur de fente de 4 à 8 mm et un écart entre les fentes de 7 à 11 mm, de telle sorte que les nervures restantes présentent une largeur de 1 à 5 mm.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102016102322.1A DE102016102322B4 (de) | 2016-02-10 | 2016-02-10 | Verfahren und Vorrichtung zum Erzeugen gehärteter Stahlbauteile |
PCT/EP2017/052603 WO2017137377A1 (fr) | 2016-02-10 | 2017-02-07 | Procédé et dispositif de fabrication de pièces en acier trempé |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3414072A1 EP3414072A1 (fr) | 2018-12-19 |
EP3414072B1 true EP3414072B1 (fr) | 2020-09-09 |
Family
ID=58185488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17707480.4A Active EP3414072B1 (fr) | 2016-02-10 | 2017-02-07 | Procédé et dispositif de fabrication de pièces en acier trempé |
Country Status (8)
Country | Link |
---|---|
US (1) | US20190048432A1 (fr) |
EP (1) | EP3414072B1 (fr) |
JP (1) | JP6744416B2 (fr) |
KR (1) | KR102224343B1 (fr) |
CN (1) | CN109070396B (fr) |
DE (1) | DE102016102322B4 (fr) |
ES (1) | ES2820362T3 (fr) |
WO (1) | WO2017137377A1 (fr) |
Family Cites Families (23)
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KR100834555B1 (ko) * | 2003-07-29 | 2008-06-02 | 뵈스트알파인 스탈 게엠베하 | 경화 강판 부품의 제조 방법 |
JP3863874B2 (ja) * | 2003-10-02 | 2006-12-27 | 新日本製鐵株式会社 | 金属板材の熱間プレス成形装置及び熱間プレス成形方法 |
DE102004038626B3 (de) | 2004-08-09 | 2006-02-02 | Voestalpine Motion Gmbh | Verfahren zum Herstellen von gehärteten Bauteilen aus Stahlblech |
JP2007098459A (ja) * | 2005-10-07 | 2007-04-19 | Nippon Steel Corp | 亜鉛系めっき鋼板の高速ガスシールドアーク溶接方法 |
DE102008063985B4 (de) * | 2008-12-19 | 2015-10-29 | Voestalpine Metal Forming Gmbh | Verfahren und Vorrichtung zum Erzeugen partiell gehärteter Stahlblechbauteile |
JP5515304B2 (ja) * | 2009-01-30 | 2014-06-11 | 新日鐵住金株式会社 | 鋼板の熱間プレス成形方法及び熱間プレス成形装置 |
JP5477016B2 (ja) * | 2009-02-03 | 2014-04-23 | 新日鐵住金株式会社 | 亜鉛系めっき熱処理鋼材の製造方法 |
DE102009050533A1 (de) * | 2009-10-23 | 2011-04-28 | Thyssenkrupp Sofedit S.A.S | Verfahren und Warmumformanlage zur Herstellung eines gehärteten, warm umgeformten Werkstücks |
WO2011081043A1 (fr) * | 2009-12-28 | 2011-07-07 | 住友金属工業株式会社 | Procédé pour la fabrication d'un organe forgé par pression à chaud |
KR101449222B1 (ko) * | 2010-02-26 | 2014-10-08 | 신닛테츠스미킨 카부시키카이샤 | 열처리 강재와 그 제조 방법 및 그 소재 강재 |
DE102010012579B3 (de) * | 2010-03-23 | 2011-07-07 | Benteler Automobiltechnik GmbH, 33102 | Verfahren und Vorrichtung zur Herstellung von gehärteten Formbauteilen |
DE102010037534A1 (de) * | 2010-09-14 | 2012-03-15 | Thyssenkrupp Steel Europe Ag | Vorrichtung und Verfahren zur Herstellung von zumindest teilweise geschlossenen Hohlprofilen mit drehbaren Gesenkhälften und geringer Taktzeit |
ES2858225T3 (es) * | 2010-12-24 | 2021-09-29 | Voestalpine Stahl Gmbh | Procedimiento para producir elementos estructurales templados |
RU2552819C1 (ru) * | 2011-05-23 | 2015-06-10 | Ниппон Стил Энд Сумитомо Метал Корпорейшн | Способ горячего прессования и форма для горячего прессового формования |
CN103608134B (zh) * | 2011-06-29 | 2016-08-24 | 丰田自动车株式会社 | 热压装置 |
DE102011052773A1 (de) | 2011-08-17 | 2013-02-21 | Kirchhoff Automotive Deutschland Gmbh | Werkzeug für ein Presshärtwerkzeug |
EP2752257B1 (fr) * | 2011-09-01 | 2016-07-27 | Kabushiki Kaisha Kobe Seiko Sho | Pièce mise en forme par matriçage à chaud et procédé pour sa fabrication |
DE102011055643A1 (de) | 2011-11-23 | 2013-05-23 | Thyssenkrupp Steel Europe Ag | Verfahren und Umformwerkzeug zum Warmumformen und Presshärten von Werkstücken aus Stahlblech, insbesondere verzinkten Werkstücken aus Stahlblech |
DE102012012518A1 (de) * | 2012-06-22 | 2013-12-24 | GEDIA Gebrüder Dingerkus GmbH | Warmumformwerkzeug zur Herstellung von Formteilen |
JP6075304B2 (ja) * | 2013-03-28 | 2017-02-08 | 株式会社豊田中央研究所 | 熱間プレス成形方法および熱間プレス成形装置 |
JP5830056B2 (ja) * | 2013-06-05 | 2015-12-09 | トヨタ自動車株式会社 | プレス装置及び噴射ノズル |
JP6414387B2 (ja) * | 2014-04-09 | 2018-10-31 | 新日鐵住金株式会社 | 自動車部材の製造方法 |
EP3072980B1 (fr) * | 2015-03-26 | 2018-02-14 | weba Werkzeugbau Betriebs GmbH | Procédé et dispositif de fabrication d'un élément de formage partiellement durci |
-
2016
- 2016-02-10 DE DE102016102322.1A patent/DE102016102322B4/de active Active
-
2017
- 2017-02-07 KR KR1020187025952A patent/KR102224343B1/ko active IP Right Grant
- 2017-02-07 EP EP17707480.4A patent/EP3414072B1/fr active Active
- 2017-02-07 CN CN201780010624.3A patent/CN109070396B/zh active Active
- 2017-02-07 ES ES17707480T patent/ES2820362T3/es active Active
- 2017-02-07 WO PCT/EP2017/052603 patent/WO2017137377A1/fr active Application Filing
- 2017-02-07 US US16/076,923 patent/US20190048432A1/en not_active Abandoned
- 2017-02-07 JP JP2018541163A patent/JP6744416B2/ja active Active
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DE102016102322B4 (de) | 2017-10-12 |
JP6744416B2 (ja) | 2020-08-19 |
ES2820362T3 (es) | 2021-04-20 |
DE102016102322A1 (de) | 2017-08-10 |
KR20180112820A (ko) | 2018-10-12 |
KR102224343B1 (ko) | 2021-03-09 |
US20190048432A1 (en) | 2019-02-14 |
CN109070396B (zh) | 2021-10-15 |
EP3414072A1 (fr) | 2018-12-19 |
CN109070396A (zh) | 2018-12-21 |
JP2019504771A (ja) | 2019-02-21 |
WO2017137377A1 (fr) | 2017-08-17 |
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