EP3585531A1 - Method for producing a component by further forming of a preformed contour - Google Patents
Method for producing a component by further forming of a preformed contourInfo
- Publication number
- EP3585531A1 EP3585531A1 EP18702238.9A EP18702238A EP3585531A1 EP 3585531 A1 EP3585531 A1 EP 3585531A1 EP 18702238 A EP18702238 A EP 18702238A EP 3585531 A1 EP3585531 A1 EP 3585531A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- temperature
- subjected
- forming
- seconds
- edge
- 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.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 28
- 238000005520 cutting process Methods 0.000 claims abstract description 35
- 238000000034 method Methods 0.000 claims description 43
- 238000010438 heat treatment Methods 0.000 claims description 32
- 238000011282 treatment Methods 0.000 claims description 20
- 229910000831 Steel Inorganic materials 0.000 claims description 18
- 239000010959 steel Substances 0.000 claims description 18
- 238000004080 punching Methods 0.000 claims description 14
- 230000009466 transformation Effects 0.000 claims description 13
- 229910052751 metal Inorganic materials 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 5
- 238000000576 coating method Methods 0.000 claims description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 4
- 238000000465 moulding Methods 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims description 4
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 239000011261 inert gas Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000012535 impurity Substances 0.000 claims description 2
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 238000002844 melting Methods 0.000 claims description 2
- 230000008018 melting Effects 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 229910052759 nickel Inorganic materials 0.000 claims description 2
- 230000003647 oxidation Effects 0.000 claims description 2
- 238000007254 oxidation reaction Methods 0.000 claims description 2
- 238000000844 transformation Methods 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- 229910052725 zinc Inorganic materials 0.000 claims description 2
- 230000007704 transition Effects 0.000 claims 1
- 238000007493 shaping process Methods 0.000 abstract 5
- 238000007669 thermal treatment Methods 0.000 abstract 2
- 239000000463 material Substances 0.000 description 18
- 238000005482 strain hardening Methods 0.000 description 10
- 230000008569 process Effects 0.000 description 6
- 230000002829 reductive effect Effects 0.000 description 6
- 238000000926 separation method Methods 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000035945 sensitivity Effects 0.000 description 4
- 238000012545 processing Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 230000002401 inhibitory effect Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000012876 topography Methods 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000010960 cold rolled steel Substances 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Classifications
-
- 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
-
- 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
- B21D19/00—Flanging or other edge treatment, e.g. of tubes
- B21D19/08—Flanging or other edge treatment, e.g. of tubes by single or successive action of pressing tools, e.g. vice jaws
-
- 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
- B21D19/00—Flanging or other edge treatment, e.g. of tubes
- B21D19/08—Flanging or other edge treatment, e.g. of tubes by single or successive action of pressing tools, e.g. vice jaws
- B21D19/088—Flanging or other edge treatment, e.g. of tubes by single or successive action of pressing tools, e.g. vice jaws for flanging holes
-
- 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
- B21D37/00—Tools as parts of machines covered by this subclass
- B21D37/16—Heating or cooling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26D—CUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
- B26D7/00—Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
- B26D7/08—Means for treating work or cutting member to facilitate cutting
- B26D7/10—Means for treating work or cutting member to facilitate cutting by heating
-
- 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
- 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
- C21D8/0278—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
-
- 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 present invention relates to a method for producing a component by further molding a preformed contour of a circuit board according to the preamble of patent claim 1.
- the method according to the invention is characterized in
- a blank or sheet metal blank is understood to mean a blank of a sheet metal, in particular a sheet steel.
- the metal sheets can be
- a component is understood to be a component produced from a sheet metal blank by deformation by means of a forming tool at ambient temperature.
- all sheet metal materials come into consideration as sheet materials, but especially steel.
- Such components are mainly used in automobile construction, but also in the home appliance industry, in mechanical engineering or construction or in the field of the same offer applications.
- the cut board After cutting the cut board is placed in a forming tool and in single or multi-stage forming steps the finished component, such as. a chassis carrier generated.
- the cut edges especially when raised or raised, e.g. in collar operations in perforated boards, particularly stressed.
- Topography of the cut surface is created.
- the testing of the forming behavior of cut sheet edges with regard to their edge crack sensitivity is carried out with a hole expansion test according to ISO 16630.
- a hole expansion test according to ISO 16630.
- DE 10 2014 016 614 A1 describes a method for producing a component by forming a blank made of steel, in which a cut board after optional punching and / or cutting operations in the areas of
- Seconds at least 600 ° C is subjected.
- the heat treated edges are then cold formed at any time after being heated.
- Manufacturing steps such as Punching or cutting operations to achieve recesses or openings, in selected, by the punching or
- Cutting operations cold-strengthened edge regions, to obtain a preformed contour of a first deformation at ambient temperature is subjected, which is characterized in that optionally already provided for forming edge portions but at least the edge portions already subjected to the first deformation for a period of up to 10 seconds to a temperature vo n at least 600 ° C are heated and the edge areas at any time after the heat treatment of a second transformation or further transformations at ambient temperature, each with upstream again
- both the room temperature, for example 20 ° C, and the temperature of the forming tool are considered.
- the temperature of the forming tool can be well above the room temperature.
- Tempering the edge portions of the preformed contour not only eliminates unwanted strain hardening but it will
- the desired component can now be obtained.
- each of the further forming steps also a further temperature treatment of the edge regions at least 600 ° C for the Duration of a maximum of 10 seconds, in particular for 0.02 to 10 or 0.1 to 2 seconds, precedes.
- a component can be produced in a multi-step process in which the undesired material properties resulting from work hardening, in particular the increased susceptibility to cracking, are adjusted in the material first in each forming step, but are adjusted by the following
- the individual forming and temperature treatment steps of the process according to the invention can be carried out at any time, i. temporally decoupled, done.
- the inventive method is particularly applicable to any sheared material edges, in particular punched holes and edges with any contour. Due to the inventively increased Umfor mbarkeit it is possible to produce complex geometries, for which it requires, for example, several forming steps. Demanding components can also be produced in one piece, eliminating the need for additional joining operations.
- the heat treatment is preferably carried out over the entire thickness of the board and in the plane direction of the board in a range which corresponds at most to their thickness.
- the duration of the heat depends on the type of heat treatment process.
- the heating itself can take place in any desired manner, for example, conductively, inductively via radiation heating or by means of laser processing.
- Excellent for the heat treatment is the conductive heating, as it is often used in the automotive industry for example on the example of spot welds.
- the process window for the temperature to be reached in the cutting edge area is also very large and covers a temperature range from above 600 ° C up to the solidus temperature of approx. 1500 ° C.
- the heat treatment is carried out above Ad, it is converted into so-called metastable phases after treatment in the course of rapid cooling due to the surrounding cold material in the case of convertible steels.
- the resulting structure then has at least the same or an increased hardness compared to the non-heat treated area.
- the Vickers hardness increases by up to 1000 HV.
- an advantageous development of the invention provides for rinsing these areas with inert gases, for example argon or nitrogen.
- inert gases for example argon or nitrogen.
- the inert gas purging takes place during the duration of the heat treatment, but can also, if necessary, even shortly before the start and / or in a limited period of time still carried out after the heat treatment.
- the forming steps of the method according to the invention can advantageously be carried out with the forming tools already in production, e.g.
- Temperature treatment steps of the method according to the invention in the industrial application of the method is a particularly high flexibility in
- the heating of the cut edges can also take place immediately after the first forming step or immediately after an optional further forming step.
- a heat treatment device of a forming device for cold forming of the board can be connected directly downstream.
- the board itself may e.g. be rolled flexibly with different thicknesses or joined from cold or hot strip of the same or different thickness and / or quality.
- the invention is applicable to hot or cold rolled steel strip from soft to high strength steels, which may be provided with a corrosion inhibiting layer as a metallic and / or organic coating.
- the metallic coating may, for example, contain or consist of zinc, magnesium, aluminum and / or silicon.
- corrosion-inhibiting layer is not or only insignificantly influenced.
- higher-strength steels all single-phase as well as multi-phase steel grades are used. These include microalloyed, higher-strength steel grades as well as bainitic, ferritic or martensitic grades as well as dual phases,
- the Committee can be lowered on formed components and on the other hand, previously necessary joining operations, for example, by now feasible collar operations in the formation of e.g. Saved from storage locations.
- the inventive method also allows due to the improved formability of the cut edges areas more complex component geometries and thus greater design freedom when using the same materials.
- the fatigue strength of the cold-formed component is expected due to the setting, although possibly compared to
- the inventive method can be integrated in a series production, which specifies a clocking in the range of 0.1 to 10 seconds, as insects ungsuze.
- a series production which specifies a clocking in the range of 0.1 to 10 seconds, as
- the invention further relates to the use of a steel circuit board for the production of a component, wherein the previously cut at room temperature from a strip or a sheet metal plate after optional further at
- Edge regions for receiving a preformed contour of a first deformation at room temperature is subjected, and wherein the first deformation
- edge regions for a maximum of 10 seconds, preferably from 0.02 to 10 seconds or from 0.1 to 2 seconds, to a temperature of at least 600 ° C are heated and the edge portions at any time after the heat treatment of a second transformation at
- the band or sheet, from which the board used for the production of the component is cut preformed in a pre-treatment step and then cut from the already preformed band or sheet, the board, if this makes sense in terms of manufacturing technology.
- the preforming can also be done only on the already cut board.
- the cutting takes place by shear cutting, wherein the term shear cutting includes both open and closed cuts, ie both cutting and punching operations.
- the left-hand image of FIG. 1 shows the optional preforming of a circuit board already cut by shear cutting.
- the second image from the left in FIG. 1 shows the punching of a hole in the board (step 1).
- the cut edges of the hole are then optionally subjected to a heating according to the invention (step 1a).
- the method according to the invention furthermore includes the
- preformed contour for example, to an incomplete collar (step 2).
- Edge regions has a high strain hardening, which in further
- edge areas are then used to eliminate or reduce the edge areas
- step 4 Due to the temperature treatment, the component is also in the claimed edge areas to a considerable extent its formability back, so that in the next step, a new, further transformation can take place (step 4).
- the material stresses generated by the second deformation can be at least partially eliminated by a subsequent temperature treatment of at least 600 ° C. for a maximum of 10 seconds, after which a third Forming step can take place. Should the desired result not be reached as a result of the third forming step, the steps of the temperature treatment of at least 600 ° C for a maximum of 10 seconds, followed by a subsequent forming step at room temperature, as often as may be repeated.
- Embodiments be essential.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Thermal Sciences (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Crystallography & Structural Chemistry (AREA)
- Optics & Photonics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Forests & Forestry (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Ceramic Capacitors (AREA)
- Soft Magnetic Materials (AREA)
- Fixed Capacitors And Capacitor Manufacturing Machines (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102017103729.2A DE102017103729A1 (en) | 2017-02-23 | 2017-02-23 | Method for producing a component by further shaping a preformed contour |
PCT/EP2018/051978 WO2018153615A1 (en) | 2017-02-23 | 2018-01-26 | Method for producing a component by further forming of a preformed contour |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3585531A1 true EP3585531A1 (en) | 2020-01-01 |
EP3585531B1 EP3585531B1 (en) | 2022-10-05 |
Family
ID=61094510
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18702238.9A Active EP3585531B1 (en) | 2017-02-23 | 2018-01-26 | Method for producing a component by further forming of a preformed contour |
Country Status (7)
Country | Link |
---|---|
US (1) | US20200038933A1 (en) |
EP (1) | EP3585531B1 (en) |
KR (1) | KR102386137B1 (en) |
DE (1) | DE102017103729A1 (en) |
ES (1) | ES2930811T3 (en) |
RU (1) | RU2743046C1 (en) |
WO (1) | WO2018153615A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3932579A4 (en) * | 2019-02-27 | 2022-05-11 | JFE Steel Corporation | Method for manufacturing steel sheet for cold press and method for manufacturing press component |
EP4201578A1 (en) * | 2021-12-24 | 2023-06-28 | Fundación Azterlan | Apparatus and method of forming countersinks and/or mouse holes in a stamped high strength aluminium sheet |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2859510A (en) * | 1955-01-13 | 1958-11-11 | Wheeling Steel Corp | Method of forming a boiler head or the like |
SU795631A2 (en) * | 1978-11-24 | 1981-01-15 | Предприятие П/Я Р-6543 | Beading method |
RU2105626C1 (en) * | 1993-06-15 | 1998-02-27 | Комсомольское-на-Амуре авиационное производственное объединение | Opening flanging method |
DE102009016027A1 (en) * | 2009-04-02 | 2010-10-07 | Volkswagen Ag | Method for producing a component, in particular a body part, and production line for carrying out the method |
DE102009049155B4 (en) | 2009-10-12 | 2017-01-05 | Bayerische Motoren Werke Aktiengesellschaft | Method for determining the edge crack sensitivity of a sheet metal material and apparatus for producing a test piece from this sheet metal material |
DE102011121904A1 (en) | 2011-12-21 | 2013-06-27 | Volkswagen Aktiengesellschaft | Method for manufacturing recess in metal sheets for motor car wheel suspension, involves introducing target contour of recess to extend sectional contour such that recess is introduced in the metal sheet |
EP2679692A1 (en) * | 2012-06-29 | 2014-01-01 | GEDIA Gebrüder Dingerkus GmbH | Method for manufacturing a press hardened formed component made of sheet steel |
DE102012014258A1 (en) * | 2012-07-12 | 2014-01-16 | Salzgitter Flachstahl Gmbh | Method for manufacturing engine carrier from steel for body construction in automobile industry, involves carrying out shaping of sheet metal blank to component in temperature range using stamping process, and ending shaping of blank |
KR101477375B1 (en) * | 2013-02-27 | 2014-12-30 | 현대제철 주식회사 | Steel sheet and manufacturing method of the same |
US20140261919A1 (en) | 2013-03-14 | 2014-09-18 | Thyssenkrupp Steel Usa, Llc | Low carbon-high manganese steel and manufacturing process thereof |
DE102014016614A1 (en) | 2014-10-31 | 2016-05-04 | Salzgitter Flachstahl Gmbh | Process for producing a component by forming a steel circuit board |
DE102014116017A1 (en) * | 2014-11-04 | 2016-05-04 | Lissmac Maschinenbau Gmbh | Device with a turning unit for turning a workpiece and a machining device |
-
2017
- 2017-02-23 DE DE102017103729.2A patent/DE102017103729A1/en active Pending
-
2018
- 2018-01-26 EP EP18702238.9A patent/EP3585531B1/en active Active
- 2018-01-26 US US16/488,143 patent/US20200038933A1/en not_active Abandoned
- 2018-01-26 ES ES18702238T patent/ES2930811T3/en active Active
- 2018-01-26 RU RU2019129532A patent/RU2743046C1/en active
- 2018-01-26 WO PCT/EP2018/051978 patent/WO2018153615A1/en unknown
- 2018-01-26 KR KR1020197024438A patent/KR102386137B1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
KR102386137B1 (en) | 2022-04-12 |
US20200038933A1 (en) | 2020-02-06 |
RU2743046C1 (en) | 2021-02-12 |
DE102017103729A1 (en) | 2018-08-23 |
WO2018153615A1 (en) | 2018-08-30 |
KR20190120205A (en) | 2019-10-23 |
ES2930811T3 (en) | 2022-12-22 |
EP3585531B1 (en) | 2022-10-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
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