US20170333971A1 - Method for producing a component by subjecting a sheet bar of steel to a forming process - Google Patents
Method for producing a component by subjecting a sheet bar of steel to a forming process Download PDFInfo
- Publication number
- US20170333971A1 US20170333971A1 US15/523,191 US201515523191A US2017333971A1 US 20170333971 A1 US20170333971 A1 US 20170333971A1 US 201515523191 A US201515523191 A US 201515523191A US 2017333971 A1 US2017333971 A1 US 2017333971A1
- Authority
- US
- United States
- Prior art keywords
- plate
- forming
- heating
- component
- heat treatment
- 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.)
- Abandoned
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/02—Stamping using rigid devices or tools
- B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/02—Stamping using rigid devices or tools
- B21D22/04—Stamping using rigid devices or tools for dimpling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D28/00—Shaping by press-cutting; Perforating
- B21D28/02—Punching blanks or articles with or without obtaining scrap; Notching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D35/00—Combined processes according to or processes combined with methods covered by groups B21D1/00 - B21D31/00
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D35/00—Combined processes according to or processes combined with methods covered by groups B21D1/00 - B21D31/00
- B21D35/001—Shaping combined with punching, e.g. stamping and perforating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/88—Making other particular articles other parts for vehicles, e.g. cowlings, mudguards
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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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/02—Hardening articles or materials formed by forging or rolling, with no further heating beyond that required for the formation
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
-
- 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
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
-
- 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
-
- 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
- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
-
- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- 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
- C21D2221/00—Treating localised areas of an article
- C21D2221/02—Edge parts
-
- 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
- C21D2261/00—Machining or cutting being involved
Definitions
- the invention relates to a method for producing a component by forming a plate made of steel, according to the preamble of patent claim 1 , which enables a high formability of strain hardened, mechanically separated plate edges.
- component means a component made from a metal plate by forming with a forming tool at room temperature.
- Metal materials that can be used include all formable metal materials, in particular however steel.
- the metal plates can be uncoated or can be provided with a metallic and/or organic anti-corrosion coating.
- Such components are mainly used in vehicle body construction but also in the home appliance industry, machine construction or building industry.
- Raw material suppliers are trying to address the demands placed on materials by providing high-strength and ultra-high strength steels, which allows reducing wall thicknesses while at the same time offering improved component properties during manufacture and operation.
- a metal plate is first cut to size from hot or cold strip at room temperature.
- Cutting methods used for this purpose mostly include mechanical separation processes such as shearing or punching, less frequently also thermal separation processes such as laser cutting. Thermal separation methods are significantly more expensive compared to mechanical separation methods and are therefore only used in exceptional cases.
- the cut plate After being cut to size the cut plate is placed into a forming tool and the finished component, such as for example a vehicle chassis, is produced in a single- or multi-step forming process.
- the finished component such as for example a vehicle chassis
- the cut edges are subjected to particularly high stress, in particular when being bent up or upwards, for example during flanging operations in punched plates.
- the mentioned prior damages at the plate edges may lead to premature failure in subsequent forming operations or during operation of the component.
- the testing of the forming characteristics of cut plate edges with regard to their sensitivity for edge crack formation is performed with a hole expansion test according to ISO 16630.
- the measuring variable is the change of the hole diameter with respect to the starting diameter, at which hole diameter the first crack occurs at the border of the hole.
- the method is simple and cost-effective and achieves comparable and/or improved properties on one hand regarding production, in particular with regard to the formability of the cut edges, and on the other hand in the component in particular with regard to the static strength.
- this object is solved by a method for producing a component by forming a plate made of steel at room temperature, which has a high formability and reduced crack sensitivity of edges that are mechanically cut or punched on the plate, in which method the plate is cut to size beforehand from a strip or plate at room temperature, wherein depending on the situation at hand further manufacturing steps, such as for example punching or cutting operations for generating recesses or perforation on the sheet metal or the plate are performed at room temperature and subsequently the thusly prepared plate is formed in one or multiple steps into a component at room temperature, which method is characterized in that independent of the forming into a component and at an arbitrary time point after the cutting to size and possible further punching or cutting operations the edge regions of the metal plate that have been strain hardened by the cutting or punching operations and which are subjected to a subsequent cold forming during the production of the component, are heated to a temperature of at least 600° C. and the time of the heat treatment is less than 10 seconds.
- Tests have shown that for improving the hole expansion capability it is not required to perform the cutting process itself at an increased temperature of the cut edge regions, but that it is sufficient to only heat the strain hardened, shear-impacted cut edge regions for a surprisingly short period of time within the range of less than 10 seconds, usually between 0.1 and 2 seconds to a temperature of at least 600° C. According to the invention this can be performed independent of the cutting or punching process and the following production steps, at an arbitrary time point prior to the forming into a component.
- the heat influence hereby acts over the entire sheet thickness and in plane direction of the plate in a region, which corresponds at most to the sheet thickness.
- the duration of the heat influence depends on the type of the heat treatment method.
- the heating itself can be performed in any manner, for example conductively inductively via radiation heating or by means of laser processing.
- Very well suited for the heat treatment is the conductive heating for example as used in automobile manufacturing, for example in spot welding.
- a spot welding machine with a relatively short impact time is suited for holes punched in the plate, whereas for treating longer edge sections the inductive method, radiation heating or laser processing with longer impact times are useful.
- an advantageous embodiment of the invention provides to rinse these regions with inert gases, for example argon.
- inert gases for example argon.
- the rinsing with inert gas is hereby performed during the duration of the heat treatment, however if required it can also be additionally already be performed prior to the start of the heat treatment and/or within a limited period of time after the heat treatment.
- the heat treatment is carried out in a very concentrated manner in the shear-impacted cut edge regions and is therefore associated with a relatively small energy investment, in particular compared to methods in which the entire metal plate is heated or in which a stress relief annealing is used which is more time-intensive by orders of magnitude.
- the process window for the temperature to be reached in the cut edge region is very wide and includes a temperature range of above 600° C. up to the solidus temperature of about 1500° C.
- a microstructure transformation with a hardness and a strength increase usually associated therewith usually has no adverse effect on the hole expansion capability, independent of whether a less hard or less tenacious microstructure forms, so that also treatment temperatures of the cut edges up to the solidus temperature limit are possible. The important factor remains in each case that the strain hardening introduced by the cutting is eliminated to the most degree.
- the method according to the invention has the advantage that as a result of the heat treatment only the shear-impacted edge region undergoes microstructural change and the strength is hereby not reduced but increased.
- the resistance against edge cracks as manifested by a greater hole expansion capability can thus be improved by a factor of 2 or even by more than 3.
- the scrap of formed components can be lowered due to the significantly increased formability of the critically shear-impacted plate edge regions and on the other hand currently required joining operations can be dispensed with, for example as a result of the fact that flanging operations can now for example be performed during the formation of bearing sites.
- the method according to the invention thus enables as a result of the improved forming capability of the cut edge regions more complex component geometries and thus greater constructive freedom using the same material.
- dual phase microstructures such as for example dual phase microstructures the fatigue strength of the cold formed component is not decreased but increased, because even though the generated microstructure may be harder compared to the starting state it is more homogenous.
- the heat treatment of the cut edge regions that are to be cold formed can be completely performed at an arbitrary time point after the cutting or punching process and prior to the forming of the plate, or it can be performed as an intermediate step in multistep forming operations in which the plate is formed into a component, so that the process steps cutting or punching of the plate, heat treatment of the cut edges and forming of the plate into a component are completely decoupled from each other.
- the manufacture is thus significantly more flexible than is possible according to the state of the art with integration of an edge modification by heat treatment.
- the method can be integrated as intermediate manufacturing step in a serial production, which has a cycle time in the range from 0.1 to 10 seconds.
- a particularly predestined field of application is thus the manufacture of sheet metal components in the automobile field in multiple subsequent steps.
- the plate prepared in this way can advantageously be formed with the forming tools that are already present in the production because no additional heating devices such as for example furnaces for heating the plate itself are required. This also contributes to a cost-effective manufacture and as a result of the decoupling of the manufacturing steps enables a high flexibility in the production process.
- the heating of the cut edges can, however, if determined advantageous also be performed directly after the mechanical cutting or punching process or directly prior to the forming into a component in a working step that is combined with the respective manufacturing step.
- the cutting and punching devices can be provided with a downstream heat treatment device or the latter can be arranged directly upstream of the forming device for cold forming of the plate.
- the plate itself can for example be flexibly rolled with different thicknesses or can be joined from cold or hot strip of the same or different thickness and/or grade.
- the invention can be used for warm or cold rolled steel strips made of soft to high strength steels for example with yield strengths of 140 MPa to 1200 MPa which can be provided with a corrosion-resistant layer as metallic and/or organic coating.
- the metallic coating can for example be made of zinc or an alloy made of zinc or of magnesium or of aluminum and/or silicone.
- higher-strength steels all single phase steels but also multiphase steels can be used. This includes micro-alloyed, higher-strength steels as well as bainitic or martensitic steels and also dual-phase steels, complex phase steel and TRIP steels.
- FIG. 1 a schematic representation of the hole expansion test according to ISO 16630 on cut edge that have been heat treated according to the invention
- FIG. 2 a test installation for conductive heat treatment of shear-impacted cut edges
- FIG. 3 results of hole expansion tests according to ISO 16630 on uncoated samples HDT780C after conducive heat treatment of the shear-impacted cut edge
- FIG. 4 results of hole expansion tests according to ISO 16630 on hot dip coated samples HCT780CD and uncoated samples HDT780C after heat treatment of the shear-impacted cut edges by means of laser
- FIG. 5 the microstructure and hardness course on cut edges that have been heat treated according to the invention.
- FIG. 1 schematically shows a hole expansion test according to ISO 16630 on cut edges that have been heat treated according to the invention.
- the heat treatment is only performed on the shear-impacted cut edges as intermediate step after cutting the plates to size and prior to the forming of regions proximate to the cut edge.
- the test installation for conductive heat treatment of shear-impacted cut edges is shown in FIG. 2 .
- step 1 a sheet with a hole punched therein (step 1) is heat treated in the region of the shear-impacted plate edges (step 2). Thereafter in step 3 the actual hole expansion is performed by means of a die, which is then determined at the tested probe.
- the opposing spot welding electrodes have a diameter, which is greater than the punched-out hole so that the shear-impacted hole edges can be heat treated.
- the electrodes have a semicircular shape so that on one hand the plate can be easily centered and on the other hand the heat can be introduced in a concentrated manner only in the shear-impacted region.
- the shape of the contacting electrode tip should be adjusted to the respective geometric configuration of the edge regions.
- a treatment duration i.e., the duration of the current flow when heating is performed inductively and the duration of the power uptake by the laser or the exposure time to other heat sources is within a range of 20 ms up to at most 10 s, usually however advantageously between 100 ms and 2000 ms. Important in any case is that a temperature of at least 600° C. is reached at the site of the heat treatment.
- the important method parameters are the treatment duration and in the case of the inductive heating the current, which was varied between 4 and 10 kA.
- a laser power of 5 kW was first adjusted which was distributed over a circular area of about 12 mm so that approximately a ring shape with 1 mm border width of the cut circular hole of the sample with the diameter of 10 mm was heat treated.
- FIG. 5 shows in the upper portion of the image on the left hand side a schematic top view onto a hole punched into a metal plate, which was treated according to the invention in the region of the hole edge.
- the microstructures that form in the heat influenced region are schematically shown in the upper portion of the image on the right hand side.
- the microstructure In the proximate border regions of about 0.5 mm the microstructure is made of 100% martensite. As a consequence heating of above Ac 3 was performed which was followed by a fast cooling. With increasing distance to the edge the proportion of bainite increases up to a distance to the edge of about 2.5 mm beyond which 100% bainite is present. Above an edge distance of 2.5 trim the microstructure did no longer undergo transformation so that here treatment temperatures below Ac 2 (about 700° C.) were present.
- the hardness increase ( FIG. 5 , lower partial image) in the proximate region of the hole edge is typical for micro-alloyed bainitic hot strip and results from the subsequent precipitation of nanoparticles in the temperature range of about 500° C.-700° C.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Heat Treatment Of Articles (AREA)
- Laser Beam Processing (AREA)
- Metal Rolling (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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DE102014016614.7 | 2014-10-31 | ||
DE102014016614.7A DE102014016614A1 (de) | 2014-10-31 | 2014-10-31 | Verfahren zur Herstellung eines Bauteils durch Umformen einer Platine aus Stahl |
PCT/DE2015/100414 WO2016066155A1 (de) | 2014-10-31 | 2015-10-06 | Verfahren zur herstellung eines bauteils durch umformen einer platine aus stahl |
Publications (1)
Publication Number | Publication Date |
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US20170333971A1 true US20170333971A1 (en) | 2017-11-23 |
Family
ID=54359651
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US15/523,191 Abandoned US20170333971A1 (en) | 2014-10-31 | 2015-10-06 | Method for producing a component by subjecting a sheet bar of steel to a forming process |
Country Status (9)
Country | Link |
---|---|
US (1) | US20170333971A1 (de) |
EP (1) | EP3212348B1 (de) |
KR (1) | KR102469605B1 (de) |
CN (1) | CN107208170B (de) |
DE (1) | DE102014016614A1 (de) |
ES (1) | ES2701869T3 (de) |
MX (1) | MX2017005563A (de) |
RU (1) | RU2701810C2 (de) |
WO (1) | WO2016066155A1 (de) |
Cited By (6)
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EP3685933A1 (de) * | 2019-01-25 | 2020-07-29 | Toyota Jidosha Kabushiki Kaisha | Verfahren zur behandlung einer stahlplatte |
WO2020175486A1 (ja) * | 2019-02-27 | 2020-09-03 | Jfeスチール株式会社 | 冷間プレス用の鋼板の製造方法、及びプレス部品の製造方法 |
US11339479B2 (en) | 2016-04-18 | 2022-05-24 | Salzgitter Flachstahl Gmbh | Component made of press-form-hardened, aluminum-based coated steel sheet, and method for producing such a component |
US11383288B2 (en) * | 2019-01-25 | 2022-07-12 | Toyota Jidosha Kabushiki Kaisha | Method of processing steel plate and punching machine |
US11511330B2 (en) * | 2017-12-25 | 2022-11-29 | Jfe Steel Corporation | Method for manufacturing press formed product |
US11654472B2 (en) | 2021-01-13 | 2023-05-23 | Toyota Jidosha Kabushiki Kaisha | Forming and processing method |
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DE102016121905A1 (de) | 2016-11-15 | 2018-05-17 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung von Radschüsseln aus Dualphasenstahl mit verbesserter Kaltumformbarkeit |
DE102016121902A1 (de) * | 2016-11-15 | 2018-05-17 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung von Fahrwerksteilen aus mikrolegiertem Stahl mit verbesserter Kaltumformbarkeit |
DE102017103729A1 (de) | 2017-02-23 | 2018-08-23 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung eines Bauteils durch Weiterformen einer vorgeformten Kontur |
DE102017103743A1 (de) * | 2017-02-23 | 2018-08-23 | Salzgitter Flachstahl Gmbh | Verfahren zur optimierten Herstellung eines Bauteils mit zumindest einem Nebenformelement |
CN114555453B (zh) * | 2019-11-08 | 2024-06-14 | 自动工程有限公司 | 一种用于车辆框架的成形钣金部件和相应的生产方法 |
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US6143241A (en) * | 1999-02-09 | 2000-11-07 | Chrysalis Technologies, Incorporated | Method of manufacturing metallic products such as sheet by cold working and flash annealing |
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DE102011054865B4 (de) * | 2011-10-27 | 2016-05-12 | Benteler Automobiltechnik Gmbh | Verfahren zur Herstellung eines warmumgeformten und pressgehärteten Kraftfahrzeugkarosseriebauteils sowie Kraftfahrzeugkarosseriebauteil |
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2015
- 2015-10-06 RU RU2017118583A patent/RU2701810C2/ru active
- 2015-10-06 WO PCT/DE2015/100414 patent/WO2016066155A1/de active Application Filing
- 2015-10-06 EP EP15786860.5A patent/EP3212348B1/de active Active
- 2015-10-06 ES ES15786860T patent/ES2701869T3/es active Active
- 2015-10-06 US US15/523,191 patent/US20170333971A1/en not_active Abandoned
- 2015-10-06 MX MX2017005563A patent/MX2017005563A/es unknown
- 2015-10-06 CN CN201580059268.5A patent/CN107208170B/zh active Active
- 2015-10-06 KR KR1020177014382A patent/KR102469605B1/ko active IP Right Grant
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US11339479B2 (en) | 2016-04-18 | 2022-05-24 | Salzgitter Flachstahl Gmbh | Component made of press-form-hardened, aluminum-based coated steel sheet, and method for producing such a component |
US11511330B2 (en) * | 2017-12-25 | 2022-11-29 | Jfe Steel Corporation | Method for manufacturing press formed product |
EP3685933A1 (de) * | 2019-01-25 | 2020-07-29 | Toyota Jidosha Kabushiki Kaisha | Verfahren zur behandlung einer stahlplatte |
US11383288B2 (en) * | 2019-01-25 | 2022-07-12 | Toyota Jidosha Kabushiki Kaisha | Method of processing steel plate and punching machine |
US11732317B2 (en) | 2019-01-25 | 2023-08-22 | Toyota Jidosha Kabushiki Kaisha | Method for processing steel plate |
WO2020175486A1 (ja) * | 2019-02-27 | 2020-09-03 | Jfeスチール株式会社 | 冷間プレス用の鋼板の製造方法、及びプレス部品の製造方法 |
CN113474100A (zh) * | 2019-02-27 | 2021-10-01 | 杰富意钢铁株式会社 | 冷压用的钢板的制造方法及冲压部件的制造方法 |
JPWO2020175486A1 (ja) * | 2019-02-27 | 2021-12-23 | Jfeスチール株式会社 | 冷間プレス用の鋼板の製造方法、及びプレス部品の製造方法 |
JP7276428B2 (ja) | 2019-02-27 | 2023-05-18 | Jfeスチール株式会社 | 冷間プレス用の鋼板の製造方法、及びプレス部品の製造方法 |
US11654472B2 (en) | 2021-01-13 | 2023-05-23 | Toyota Jidosha Kabushiki Kaisha | Forming and processing method |
Also Published As
Publication number | Publication date |
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RU2017118583A (ru) | 2018-11-30 |
RU2701810C2 (ru) | 2019-10-01 |
EP3212348B1 (de) | 2018-09-12 |
CN107208170A (zh) | 2017-09-26 |
DE102014016614A1 (de) | 2016-05-04 |
ES2701869T3 (es) | 2019-02-26 |
EP3212348A1 (de) | 2017-09-06 |
RU2017118583A3 (de) | 2019-04-24 |
MX2017005563A (es) | 2017-12-14 |
KR102469605B1 (ko) | 2022-11-21 |
CN107208170B (zh) | 2019-06-14 |
KR20170077192A (ko) | 2017-07-05 |
WO2016066155A1 (de) | 2016-05-06 |
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