EP3715490B1 - Method of casting steel alloy component and cast component - Google Patents

Method of casting steel alloy component and cast component Download PDF

Info

Publication number
EP3715490B1
EP3715490B1 EP19166206.3A EP19166206A EP3715490B1 EP 3715490 B1 EP3715490 B1 EP 3715490B1 EP 19166206 A EP19166206 A EP 19166206A EP 3715490 B1 EP3715490 B1 EP 3715490B1
Authority
EP
European Patent Office
Prior art keywords
component
steel alloy
cast
casting
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.)
Active
Application number
EP19166206.3A
Other languages
German (de)
French (fr)
Other versions
EP3715490A1 (en
Inventor
Clemens Bergmann
Michel Millot
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bayerische Motoren Werke AG
Meita Industrial Co Ltd
Original Assignee
Bayerische Motoren Werke AG
Meita Industrial Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bayerische Motoren Werke AG, Meita Industrial Co Ltd filed Critical Bayerische Motoren Werke AG
Priority to EP19166206.3A priority Critical patent/EP3715490B1/en
Priority to PCT/EP2020/058411 priority patent/WO2020200972A1/en
Priority to US17/598,736 priority patent/US20220154316A1/en
Priority to EP20712393.6A priority patent/EP3947764A1/en
Priority to CN202080026048.3A priority patent/CN113614267A/en
Publication of EP3715490A1 publication Critical patent/EP3715490A1/en
Application granted granted Critical
Publication of EP3715490B1 publication Critical patent/EP3715490B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/08Making cast-iron alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/26Methods of annealing
    • C21D1/28Normalising
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/005Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C37/00Cast-iron alloys
    • C22C37/06Cast-iron alloys containing chromium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C37/00Cast-iron alloys
    • C22C37/06Cast-iron alloys containing chromium
    • C22C37/08Cast-iron alloys containing chromium with nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C37/00Cast-iron alloys
    • C22C37/10Cast-iron alloys containing aluminium or silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/16Ferrous alloys, e.g. steel alloys containing copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/34Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/005Ferrite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/009Pearlite

Definitions

  • the invention relates to a method of manufacturing a component, and a component.
  • a steel alloy comprises, in percent by mass, 0.17 to 0.23 carbon (C).
  • the unit or specification "percent by mass” is also referred to as “percentage by mass”, “percentage by weight”, “percent by weight”, “weight percent, “weight percentage” or “mass fraction”.
  • the percentage by mass of a substance within a mixture or an alloy such as the steel alloy is the ratio of the mass of that substance to the total mass of the mixture or the alloy respectively.
  • said substance can be an alloying element such as carbon.
  • said carbon is a substance of the steel alloy.
  • the steel alloy comprises, in percent by mass, 1.40 to 1.60 silicon (Si), 0.50 to 0.60 manganese (Mn), up to 0.020 phosphor (P), up to 0.020 sulphur (S), up to 0.30 chrome (Cr), up to 0.12 molybdenum (Mo), up to 0.80 nickel (Ni), up to 0.30 copper (Cu) and up to 0.03 vanadium (V), the remainder or balance being iron (Fe) and incidental or unavoidable impurities.
  • This means the carbon, the silicon, the manganese, the phosphor, the sulphur, the chrome, the molybdenum, the nickel, the copper and the vanadium are substances, in particular alloying elements, of the steel alloy.
  • said iron and said impurities are substances of the steel alloy.
  • said impurities can be conditional of manufacturing.
  • the steel alloy comprises at least 95 percent by mass and preferably at least 95.5 percent by mass of iron.
  • the steel alloy comprises at least 95.78 percent by mass of iron.
  • the steel alloy comprises a mass fraction of at least 95 percent, preferably at least 95.5 percent and preferably at least 95.78 percent of iron, the remainder being incidental or unavoidable or inevitable impurities.
  • the steel alloy can be cast in a particular advantageous way so that components can be made of the steel alloy in a particular advantageous, time- and cost efficient way. It has particularly been found that silicon, in particular its mass fraction or percentage by mass according to the present invention, helps create a particularly good flowability of a molten mass made from the steel alloy.
  • the mass fraction of silicon according to the present invention helps realize an advantageously low solidus temperature.
  • manganese and its mass fraction according to the present invention help avoid an excessive or unwished reactivity, in particular during processing the steel alloy.
  • the steel alloy is a steel cast alloy. It has been found that the steel alloy used in the present invention can be cast in a particular advantageous way due to said substances and their respective mass fractions. In other words, the steel alloy used in the present invention is processed particular advantageously by casting.
  • the steel alloy as cast has a Brinell hardness of at least 190 HBW 5/750 and/or a yield point (R p0,2 ) of at least 300 megapascal (N/mm 2 ).
  • the present invention relates to a method of manufacturing a component in a cast state of the steel alloy, wherein the component is made from the steel alloy by casting, i.e. by a casting method or a casting process.
  • the present invention relates to a method for manufacturing at least one component. In said method the component is manufactured or made from the steel alloy described above.
  • the component is made from the steel alloy by casting, i.e. by a casting method or a casting process.
  • the component can be made in a particular easy and time- and cost-efficient way.
  • a particularly low wall thickness of the component can be realized by manufacturing the component from the steel alloy.
  • the component is subjected to a heat treatment after the casting.
  • the component is subjected to at least or exactly one heat treatment after the casting.
  • the heat treatment comprises a normalizing of the component.
  • the heat treatment is a normalizing of the component.
  • the normalizing is carried out in a temperature range extending from 900 degrees centigrade to 980 degrees centigrade.
  • the steel alloy has a tensile strength (R m ) of at least 560 megapascal and/or a yield point (R p0,2 ) of at least 370 megapascal and/or an elongation at break (A 5,65 ) of at least 20% and/or a Vickers hardness of at least 180 HV10 and/or a viscosity or ductility (KV) of at least 27 joule, wherein the ductility has been or can be determined by an impact test.
  • R m tensile strength
  • R p0,2 yield point
  • a 5,65 elongation at break
  • KV viscosity or ductility
  • Said tensile strength, said yield point, said elongation at break, said ductility and said Vickers hardness as well as said Brinell hardness are mechanical characteristics or properties of the steel alloy or the component respectively, wherein said properties and their mentioned characteristic values have been or can be determined according to DIN EN ISO 6892-1, in particular by means of a tensile test according to DIN EN ISO 6892-1.
  • said properties and their mentioned characteristic values have been or can be determined by means of a sample or probe which can be taken or drawn according to DIN EN ISO 377.
  • the probe or sample is also referred to as a specimen. If possible, the specimen type E according to DIN 50125 should be chosen.
  • the standards, in particular the DIN EN standards mentioned herein are or have been valid on June 29 th , 2017.
  • a homogeneous perlitic-ferritic structure or micro structure is created by the heat treatment, wherein during the heat treatment, a carbonization and a decarbonisation of the component are omitted.
  • the present invention also relates to a component which is a cast component.
  • Said cast component is obtained by the method according to the invention, i.e. from the steel alloy according to the description above.
  • the component is a body component for a body in white or an integral body of a vehicle, in particular a passenger vehicle.
  • the body in white or the integral body are also referred to as a self-supporting body, body work or shell.
  • the body component is a dome such as a suspension-strut dome.
  • the dome has a particularly low wall thickness which can be realized by using the steel alloy according to the description above.
  • the present invention relates to a cast component obtained by the method defined in claims 1 or 2.
  • Figs. 1 and 2 show a component 1 for a vehicle such as a car or an automobile.
  • said vehicle is a passenger vehicle having, in its completely assembled state, a body in white which is also referred to as a body, an integral body, a self-supporting body, a bodywork or a shell.
  • the component 1 is a body component of the body in white.
  • the component 1 is a dome in a form of a suspension-strut dome of the body in white.
  • the component 1 has a particularly low wall thickness.
  • the component 1 has a rib structure 2 stiffening the component 1.
  • the component 1 is formed in one piece. In other words, the component is integrally formed. As can be seen from Figs.
  • the component 1 has a recess 3 which is, preferably, a through opening.
  • a spring and/or damper element such as a suspension-strut can be supported on the component 1 in the vertical direction of the vehicle upwardly.
  • the spring and/or damper element can be arranged partially in the recess 3.
  • the component 1 is made from a steel alloy by casting, i.e. by a casting method.
  • Said steel alloy is a steel cast alloy which can be processed by casting in a particularly easy and time- and cost-efficient way.
  • Said steel alloy comprises the following substances, given in mass fractions in the unit %:
  • the steel alloy comprises the afore-mentioned substances, in percent by mass or percentage by mass.
  • the steel alloy can be processed very well, in particular by casting.
  • the component 1 After casting the component 1, the component 1 is subjected to a heat treatment, which is a normalizing of the component 1.
  • the normalizing is also referred to as a normalization and is performed in a temperature range of 900 to 980 degrees centigrade.
  • the component 1 is normalized in an oven.
  • a temperature and an atmosphere in the oven during the normalizing should be chosen in a way that a homogeneous perlitic-ferritic grain structure of the component 1 is accomplished and neither carbonisation nor decarbonisation of the component 1 or the steel alloy respectively occurs. This can be proven by means of a grain structure analysis.
  • the component 1 or the steel alloy has a tensile strength (TS) of at least 560 megapascal and /or a yield point or yield strength (YS) of at least 370 megapascal and/or an elongation at break or a fracture elongation (A 5.65 ) of at least 20 percent and/or a tensile ductility or toughness (KV) of at least 27 joule and/or a Vickers hardness of at least 180 HV10.
  • TS tensile strength
  • YS yield point or yield strength
  • a 5.65 of at least 20 percent
  • KV tensile ductility or toughness
  • a measurement to determine said toughness is preferably carried out according to ISO 148-1:2016 which, preferably, is or has been valid on June 29 th , 2017.
  • a measurement for determining said hardness is carried out according to DIN EN ISO 6507-1.
  • Said tensile strength, said yield strength, said fracture elongation, said toughness and said Vickers hardness are mechanical properties or mechanical characteristics in normalized condition of the component 1, i.e. after said normalizing.
  • the component 1 is cleaned, preferably by centrifugal blasting.
  • the component 1 is cleaned by means of airless blast cleaning after the casting and after the heat treatment.
  • Fig. 3 shows a flow diagram illustrating a process or process sequence which is carried out after the casting and after the heat treatment and, preferably, after said cleaning of the component 1.
  • the process sequence shown in Fig. 3 is carried out in order to realize a particularly high quality of a surface of the, in particular completely manufactured, component 1.
  • a first step S1 of the process sequence the component 1 is degreased, preferably by means of an alkaline fluid.
  • the component 1 is subjected to a first purging in which, preferably, the component 1 is purged by means of deionised water.
  • the second step S2 is carried out after the first step S1.
  • a third step S3 of the process sequence the component 1 is subjected to an ultrasonically cleaning in which, preferably, the component 1 is cleaned by means of the deionised water.
  • the third step S3 is carried out after the second step S2.
  • a fourth step S4 of the process sequence the component 1 is subjected to a first chemical polishing which is preferably carried out after the third step S3.
  • the fourth step S4 at least or exactly one layer having a thickness of 10 to 15 micrometres is abased from the component 1.
  • a fifth step S5 the component 1 is subjected to a second chemical polishing.
  • the fifth step S5 is an alternative to the fourth step S4 so that either the fourth step S4 or the fifth step S5 is carried out.
  • the fifth step S5 at least or exactly one layer having a thickness of 25 to 30 micrometres is abased from the component 1.
  • the fourth or fifth step respectively is carried out after the third step.
  • a sixth step S6 which is preferably carried out after the fourth step S4 or the fifth step S5 respectively, the component 1 is subjected to a second purging in which the component 1 is purged by deionised water.
  • a seventh step S7 of the process sequence the component 1 is subjected to an ultrasonically cleaning, wherein, preferably, the seventh step S7 is carried out after the sixth step S6.
  • the seventh step S7 the component 1 is ultrasonically cleaned by means of deionised water.
  • an eighth step S8 of the process sequence the component 1 is subjected to a pickling which is also referred to as a pickeling. Preferably, by means of the pickling the component 1 is cleaned.
  • the eighth step S8 is carried out after the seventh step S7.
  • a ninth step S9 of the process sequence the component 1 is subjected to a galvanising process in which the component 1 is galvanised.
  • the ninth step S9 is carried out after the eighth step S8.
  • the component 1 is furnished or provided with at least one layer by means of galvanising.
  • Said layer is made of zinc (Zn) in order to protect the component 1 from corrosion. Since the galvanising in the ninth step S9 is carried out after the pickling carried out in the eighth step S8, the layer adheres particularly advantageously or strongly to the surface of the component 1.
  • a corrosion protection oil in particular by spraying.
  • said corrosion protection oil is sprayed on said zinc layer and, thus, on a surface formed by said layer which is a zinc layer.
  • the tenth step S10 is carried out after the ninth step S9.
  • the component 1, in particular in its completely manufactured state has a surface having a surface roughness fulfilling the following demands: Ra max.10 micrometres, Rz max. 50 micrometres and Rt max. 75 micrometres.
  • said surface roughness is determined or measured according to DIN EN ISO 4288:1997.
  • the ninth step S9 is a coating or coating process which is also referred to as a galvanic zinc coating or galvanic zinc coating process, said layer being a zinc layer is a coat or a zinc coat.
  • the zinc coat is also referred to as a sink coating which is, preferably, at every position of the component 1 and, thus, completely closed.
  • the layer has a thickness of 7 to 15 micrometres.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)

Description

  • The invention relates to a method of manufacturing a component, and a component.
  • Steel alloys such as, for example, G20Mn5 according to DIN EN 10293 are well-known from the prior art. Moreover, US 2019/0078190 A1 shows a method of manufacturing an alloyed hot-dip galvanized steel sheet. CN 101343716 B discloses a low-alloy cast steel.
  • It is an object of the present invention to provide method of manufacturing a component, as well as a component so that the component can be manufactured from said steel alloy in a particular advantageous way.
  • This object is solved by a method having the features of patent claim 1, and a component having the features of patent claim 3. Advantageous embodiments of the invention are indicated in the dependent claims.
  • Firstly, a steel alloy comprises, in percent by mass, 0.17 to 0.23 carbon (C). The unit or specification "percent by mass" is also referred to as "percentage by mass", "percentage by weight", "percent by weight", "weight percent, "weight percentage" or "mass fraction". In the context, the percentage by mass of a substance within a mixture or an alloy such as the steel alloy is the ratio of the mass of that substance to the total mass of the mixture or the alloy respectively. With respect to an alloy such as the steel alloy, said substance can be an alloying element such as carbon. In other words, said carbon is a substance of the steel alloy.
  • Furthermore, the steel alloy comprises, in percent by mass, 1.40 to 1.60 silicon (Si), 0.50 to 0.60 manganese (Mn), up to 0.020 phosphor (P), up to 0.020 sulphur (S), up to 0.30 chrome (Cr), up to 0.12 molybdenum (Mo), up to 0.80 nickel (Ni), up to 0.30 copper (Cu) and up to 0.03 vanadium (V), the remainder or balance being iron (Fe) and incidental or unavoidable impurities. This means the carbon, the silicon, the manganese, the phosphor, the sulphur, the chrome, the molybdenum, the nickel, the copper and the vanadium are substances, in particular alloying elements, of the steel alloy. Moreover, said iron and said impurities are substances of the steel alloy. Particularly, said impurities can be conditional of manufacturing. The steel alloy comprises at least 95 percent by mass and preferably at least 95.5 percent by mass of iron. Preferably, the steel alloy comprises at least 95.78 percent by mass of iron. In other words, the steel alloy comprises a mass fraction of at least 95 percent, preferably at least 95.5 percent and preferably at least 95.78 percent of iron, the remainder being incidental or unavoidable or inevitable impurities.
  • It has surprisingly been found that the steel alloy can be cast in a particular advantageous way so that components can be made of the steel alloy in a particular advantageous, time- and cost efficient way. It has particularly been found that silicon, in particular its mass fraction or percentage by mass according to the present invention, helps create a particularly good flowability of a molten mass made from the steel alloy.
  • Moreover, the mass fraction of silicon according to the present invention helps realize an advantageously low solidus temperature.
  • Furthermore, it has been found that manganese and its mass fraction according to the present invention help avoid an excessive or unwished reactivity, in particular during processing the steel alloy.
  • The steel alloy is a steel cast alloy. It has been found that the steel alloy used in the present invention can be cast in a particular advantageous way due to said substances and their respective mass fractions. In other words, the steel alloy used in the present invention is processed particular advantageously by casting.
  • In a further advantageous embodiment of the invention, the steel alloy as cast has a Brinell hardness of at least 190 HBW 5/750 and/or a yield point (Rp0,2) of at least 300 megapascal (N/mm2). Thus, particular advantageous characteristics of the steel alloy and, thus, a component made from the steel alloy can be realized.
  • The present invention relates to a method of manufacturing a component in a cast state of the steel alloy, wherein the component is made from the steel alloy by casting, i.e. by a casting method or a casting process. In other words, the present invention relates to a method for manufacturing at least one component. In said method the component is manufactured or made from the steel alloy described above.
  • In said method, the component is made from the steel alloy by casting, i.e. by a casting method or a casting process. Thus, the component can be made in a particular easy and time- and cost-efficient way. In particular, a particularly low wall thickness of the component can be realized by manufacturing the component from the steel alloy.
  • The component is subjected to a heat treatment after the casting. The component is subjected to at least or exactly one heat treatment after the casting. Thus, particular advantageous characteristics of the component can be realized.
  • The heat treatment comprises a normalizing of the component. Preferably, the heat treatment is a normalizing of the component.
  • In order to realize advantageous characteristics of the component, the normalizing is carried out in a temperature range extending from 900 degrees centigrade to 980 degrees centigrade.
  • Preferably, after the heat treatment the steel alloy has a tensile strength (Rm) of at least 560 megapascal and/or a yield point (Rp0,2) of at least 370 megapascal and/or an elongation at break (A5,65) of at least 20% and/or a Vickers hardness of at least 180 HV10 and/or a viscosity or ductility (KV) of at least 27 joule, wherein the ductility has been or can be determined by an impact test. Said tensile strength, said yield point, said elongation at break, said ductility and said Vickers hardness as well as said Brinell hardness are mechanical characteristics or properties of the steel alloy or the component respectively, wherein said properties and their mentioned characteristic values have been or can be determined according to DIN EN ISO 6892-1, in particular by means of a tensile test according to DIN EN ISO 6892-1. Particularly, said properties and their mentioned characteristic values have been or can be determined by means of a sample or probe which can be taken or drawn according to DIN EN ISO 377. The probe or sample is also referred to as a specimen. If possible, the specimen type E according to DIN 50125 should be chosen. Particularly, the standards, in particular the DIN EN standards mentioned herein are or have been valid on June 29th, 2017.
  • In order to realize particularly advantageous characteristics of the component, in an advantageous embodiment of the invention, a homogeneous perlitic-ferritic structure or micro structure is created by the heat treatment, wherein during the heat treatment, a carbonization and a decarbonisation of the component are omitted.
  • The present invention also relates to a component which is a cast component. Said cast component is obtained by the method according to the invention, i.e. from the steel alloy according to the description above.
  • Preferably, the component is a body component for a body in white or an integral body of a vehicle, in particular a passenger vehicle. The body in white or the integral body are also referred to as a self-supporting body, body work or shell. Preferably, the body component is a dome such as a suspension-strut dome. In this regard, the dome has a particularly low wall thickness which can be realized by using the steel alloy according to the description above.
  • The present invention relates to a cast component obtained by the method defined in claims 1 or 2.
  • Further details of the invention derive from the following description of preferred embodiments as well as from the drawings. The drawings show in:
  • Fig. 1
    part of a schematic and perspective view of a component according to the present invention;
    Fig. 2
    part of a further schematic and perspective view of the component; and
    Fig. 3
    a flow diagram illustrating a method for manufacturing the component.
  • In the figures the same elements or elements having the same functions are indicated by the same reference signs.
  • Figs. 1 and 2 show a component 1 for a vehicle such as a car or an automobile. In particular, said vehicle is a passenger vehicle having, in its completely assembled state, a body in white which is also referred to as a body, an integral body, a self-supporting body, a bodywork or a shell. In this regard, the component 1 is a body component of the body in white. Particularly, the component 1 is a dome in a form of a suspension-strut dome of the body in white. The component 1 has a particularly low wall thickness. Moreover, the component 1 has a rib structure 2 stiffening the component 1. Moreover, preferably, the component 1 is formed in one piece. In other words, the component is integrally formed. As can be seen from Figs. 1 and 2, the component 1 has a recess 3 which is, preferably, a through opening. For example, a spring and/or damper element such as a suspension-strut can be supported on the component 1 in the vertical direction of the vehicle upwardly. Alternatively or additionally, the spring and/or damper element can be arranged partially in the recess 3.
  • In order to manufacture the component 1 in a particular easy and time- and cost-efficient way the component 1 is made from a steel alloy by casting, i.e. by a casting method. Said steel alloy is a steel cast alloy which can be processed by casting in a particularly easy and time- and cost-efficient way. Said steel alloy comprises the following substances, given in mass fractions in the unit %:
    • 0.17 to 0.23 carbon (C)
    • 1.40 to 1.60 silicon (Si)
    • 0.50 to 0.60 manganese (Mn)
    • up to 0.020 phosphor (P)
    • up to 0.020 sulphur (S)
    • up to 0.30 chrome (Cr)
    • up to 0.12 molybdenum (Mo)
    • up to 0.80 nickel (Ni)
    • up to 0.30 copper (Cu)
    • up to 0.03 vanadium (V)
    • the remainder or balance being iron (Fe) and incidental, unavoidable or inevitable impurities.
  • This means the steel alloy comprises the afore-mentioned substances, in percent by mass or percentage by mass. In particular, due to the mass fractions of silicon and manganese respectively, the steel alloy can be processed very well, in particular by casting.
  • After casting the component 1, the component 1 is subjected to a heat treatment, which is a normalizing of the component 1. The normalizing is also referred to as a normalization and is performed in a temperature range of 900 to 980 degrees centigrade. For example, the component 1 is normalized in an oven. A temperature and an atmosphere in the oven during the normalizing should be chosen in a way that a homogeneous perlitic-ferritic grain structure of the component 1 is accomplished and neither carbonisation nor decarbonisation of the component 1 or the steel alloy respectively occurs. This can be proven by means of a grain structure analysis.
  • Preferably, in a state or condition after the heat treatment and before an optional or possible further heat treatment to which the component 1 is possibly subjected, the component 1 or the steel alloy has a tensile strength (TS) of at least 560 megapascal and /or a yield point or yield strength (YS) of at least 370 megapascal and/or an elongation at break or a fracture elongation (A5.65) of at least 20 percent and/or a tensile ductility or toughness (KV) of at least 27 joule and/or a Vickers hardness of at least 180 HV10. A measurement to determine said toughness is preferably carried out according to ISO 148-1:2016 which, preferably, is or has been valid on June 29th, 2017. Alternatively or additionally, a measurement for determining said hardness is carried out according to DIN EN ISO 6507-1. Said tensile strength, said yield strength, said fracture elongation, said toughness and said Vickers hardness are mechanical properties or mechanical characteristics in normalized condition of the component 1, i.e. after said normalizing.
  • Preferably, after the casting and after the heat treatment the component 1 is cleaned, preferably by centrifugal blasting. Preferably, the component 1 is cleaned by means of airless blast cleaning after the casting and after the heat treatment.
  • Fig. 3 shows a flow diagram illustrating a process or process sequence which is carried out after the casting and after the heat treatment and, preferably, after said cleaning of the component 1. The process sequence shown in Fig. 3 is carried out in order to realize a particularly high quality of a surface of the, in particular completely manufactured, component 1.
  • In a first step S1 of the process sequence, the component 1 is degreased, preferably by means of an alkaline fluid. In a second step S2 the component 1 is subjected to a first purging in which, preferably, the component 1 is purged by means of deionised water. Preferably, the second step S2 is carried out after the first step S1. In a third step S3 of the process sequence the component 1 is subjected to an ultrasonically cleaning in which, preferably, the component 1 is cleaned by means of the deionised water. Preferably, the third step S3 is carried out after the second step S2. In a fourth step S4 of the process sequence the component 1 is subjected to a first chemical polishing which is preferably carried out after the third step S3. In the fourth step S4 at least or exactly one layer having a thickness of 10 to 15 micrometres is abased from the component 1.
  • In a fifth step S5 the component 1 is subjected to a second chemical polishing. The fifth step S5 is an alternative to the fourth step S4 so that either the fourth step S4 or the fifth step S5 is carried out. In the fifth step S5 at least or exactly one layer having a thickness of 25 to 30 micrometres is abased from the component 1. Preferably, the fourth or fifth step respectively is carried out after the third step.
  • In a sixth step S6 which is preferably carried out after the fourth step S4 or the fifth step S5 respectively, the component 1 is subjected to a second purging in which the component 1 is purged by deionised water. In a seventh step S7 of the process sequence the component 1 is subjected to an ultrasonically cleaning, wherein, preferably, the seventh step S7 is carried out after the sixth step S6. In the seventh step S7, the component 1 is ultrasonically cleaned by means of deionised water. In an eighth step S8 of the process sequence the component 1 is subjected to a pickling which is also referred to as a pickeling. Preferably, by means of the pickling the component 1 is cleaned. Preferably, the eighth step S8 is carried out after the seventh step S7.
  • In a ninth step S9 of the process sequence the component 1 is subjected to a galvanising process in which the component 1 is galvanised. Preferably, the ninth step S9 is carried out after the eighth step S8. In the ninth step S9, the component 1 is furnished or provided with at least one layer by means of galvanising. Said layer is made of zinc (Zn) in order to protect the component 1 from corrosion. Since the galvanising in the ninth step S9 is carried out after the pickling carried out in the eighth step S8, the layer adheres particularly advantageously or strongly to the surface of the component 1. In other words, by means of the pickling carried out in the eighth step a particularly advantageous surface of the component 1 can be realized, wherein the layer created in the galvanising process carried out in the ninth step S9 can adhere very advantageously and strongly to said surface created by the pickling.
  • In a tenth step S10 of the process sequence the component 1 is provided with a corrosion protection oil, in particular by spraying. In other words, in particular and preferably, said corrosion protection oil is sprayed on said zinc layer and, thus, on a surface formed by said layer which is a zinc layer. Preferably, the tenth step S10 is carried out after the ninth step S9.
  • Preferably, the component 1, in particular in its completely manufactured state, has a surface having a surface roughness fulfilling the following demands: Ra max.10 micrometres, Rz max. 50 micrometres and Rt max. 75 micrometres. Preferably, said surface roughness is determined or measured according to DIN EN ISO 4288:1997.
  • The ninth step S9 is a coating or coating process which is also referred to as a galvanic zinc coating or galvanic zinc coating process, said layer being a zinc layer is a coat or a zinc coat. The zinc coat is also referred to as a sink coating which is, preferably, at every position of the component 1 and, thus, completely closed. Preferably, the layer has a thickness of 7 to 15 micrometres.
  • List of reference signs
  • 1
    component
    2
    rip structure
    3
    recess
    S1
    first step
    S2
    second step
    S3
    third step
    S4
    fourth step
    S5
    fifth step
    S6
    sixth step
    S7
    seventh step
    S8
    eighth step
    S9
    ninth step
    S10
    tenth step

Claims (5)

  1. A method of manufacturing a component in a cast state of a steel alloy which comprises, in percent by mass: - 0.17 to 0.23 carbon; - 1.40 to 1.60 silicon; - 0.50 to 0.60 manganese; - up to 0.020 phosphor; - up to 0.020 sulfur; - up to 0.30 chrome; - up to 0.12 molybdenum; - up to 0.80 nickel; - up to 0.30 copper; - up to 0.03 vanadium;
    the remainder being iron and incidental impurities, wherein the component (1) is made from the steel alloy by casting, wherein after the casting the component (1) is subjected to a heat treatment which comprises a normalizing of the component (1), and wherein the normalizing is carried out in a temperature range extending from 900 degrees centigrade to 980 degrees centigrade.
  2. The method according to claim 1,
    characterized in that
    by the heat treatment a homogeneous perlitic-ferritic structure is created, wherein, during the heat treatment, a carbonization and a decarbonization of the component are omitted.
  3. A cast component (1) obtained by the method according to claim 1 or 2.
  4. The cast component according to claim 3,
    characterized in that
    the component (1) is a body component for a body in white or an integral body of a vehicle.
  5. The cast component (1) according to claim 4,
    characterized in that
    the body component (1) is a dome.
EP19166206.3A 2019-03-29 2019-03-29 Method of casting steel alloy component and cast component Active EP3715490B1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP19166206.3A EP3715490B1 (en) 2019-03-29 2019-03-29 Method of casting steel alloy component and cast component
PCT/EP2020/058411 WO2020200972A1 (en) 2019-03-29 2020-03-25 Steel alloy, use of such a steel alloy, and component
US17/598,736 US20220154316A1 (en) 2019-03-29 2020-03-25 Steel Alloy, Use of Such a Steel Alloy, and Component
EP20712393.6A EP3947764A1 (en) 2019-03-29 2020-03-25 Steel alloy, use of such a steel alloy, and component
CN202080026048.3A CN113614267A (en) 2019-03-29 2020-03-25 Steel alloy, use and component of such a steel alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP19166206.3A EP3715490B1 (en) 2019-03-29 2019-03-29 Method of casting steel alloy component and cast component

Publications (2)

Publication Number Publication Date
EP3715490A1 EP3715490A1 (en) 2020-09-30
EP3715490B1 true EP3715490B1 (en) 2023-08-23

Family

ID=66041230

Family Applications (2)

Application Number Title Priority Date Filing Date
EP19166206.3A Active EP3715490B1 (en) 2019-03-29 2019-03-29 Method of casting steel alloy component and cast component
EP20712393.6A Withdrawn EP3947764A1 (en) 2019-03-29 2020-03-25 Steel alloy, use of such a steel alloy, and component

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP20712393.6A Withdrawn EP3947764A1 (en) 2019-03-29 2020-03-25 Steel alloy, use of such a steel alloy, and component

Country Status (4)

Country Link
US (1) US20220154316A1 (en)
EP (2) EP3715490B1 (en)
CN (1) CN113614267A (en)
WO (1) WO2020200972A1 (en)

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005273006A (en) * 2004-02-27 2005-10-06 Jfe Steel Kk Outer ring of constant velocity joint and manufacturing method therefor
US8025982B2 (en) * 2005-12-06 2011-09-27 Kobe Steel, Ltd. High-strength hot dip galvannealed steel sheet having high powdering resistance and method for producing the same
CN101343716B (en) * 2008-06-27 2010-12-01 南车戚墅堰机车车辆工艺研究所有限公司 Low alloy cast steel
JP5503195B2 (en) * 2009-06-18 2014-05-28 株式会社神戸製鋼所 Steel for machine structure suitable for friction welding, manufacturing method thereof, friction welding component
JP5629598B2 (en) * 2011-02-15 2014-11-19 株式会社神戸製鋼所 Manufacturing method for seamless steel pipe for high strength hollow spring
DE102011057007B4 (en) * 2011-12-23 2013-09-26 Benteler Automobiltechnik Gmbh Method for producing a motor vehicle component and motor vehicle component
CN105779893B (en) * 2012-06-28 2018-08-10 中车戚墅堰机车车辆工艺研究所有限公司 Alloy cast steel for brake disc of high-speed train and the brake disc of high-speed train that is manufactured by the alloy cast steel
JP5708884B2 (en) * 2012-11-06 2015-04-30 新日鐵住金株式会社 Alloyed hot-dip galvanized steel sheet and manufacturing method thereof
CN106834929A (en) * 2017-03-03 2017-06-13 衡水裕菖铸锻有限公司 Corrosion-resistant cast steel and its Technology for Heating Processing under a kind of environment suitable for atmospheric corrosion
JP7127999B2 (en) * 2017-03-27 2022-08-30 株式会社神戸製鋼所 Steel for forgings, forged steel crank throws and forged journals for assembled crankshafts
CN107267861A (en) * 2017-05-31 2017-10-20 舞阳钢铁有限责任公司 Continuous casting billet produces normalized high-strength S460NL steel plates and its production method

Also Published As

Publication number Publication date
US20220154316A1 (en) 2022-05-19
EP3715490A1 (en) 2020-09-30
EP3947764A1 (en) 2022-02-09
WO2020200972A1 (en) 2020-10-08
CN113614267A (en) 2021-11-05

Similar Documents

Publication Publication Date Title
TWI479030B (en) A melt-plated high strength steel sheet for extrusion processing with excellent low temperature toughness and corrosion resistance and its manufacturing method
US11530474B2 (en) Fe—Al-based plated hot-stamped member and manufacturing method of Fe—Al-based plated hot-stamped member
US20190010596A1 (en) High-strength plated steel plate for welded structural member, and method for producing the same
JP5510057B2 (en) Hot-dip galvanized steel sheet and manufacturing method thereof
KR20060096002A (en) High-yield-ratio high-strength thin steel sheet and high-yield-ratio high-strength hot-dip galvanized thin steel sheet excelling in weldability and ductility as well as high-yield-ratio high-strength alloyed hot-dip galvanized thin steel sheet and process for producing the same
KR20130025961A (en) High yield ratio high-strength hot-dip galvanized steel sheet with excellent ductility and hole expansion properties, and manufacturing method thereof
KR102130232B1 (en) Thin steel plate and plated steel sheet, and hot rolled steel sheet manufacturing method, cold rolled full hard steel sheet manufacturing method, thin steel sheet manufacturing method and plated steel sheet manufacturing method
EP3369837B1 (en) Plated steel sheet
KR20200135815A (en) Hot stamp molded body
US20180371596A1 (en) High-strength hot-dip zinc plated steel material having excellent plating properties and method for preparing same
KR20190022769A (en) Steel sheet and its manufacturing method
JP7364935B2 (en) Hot stamp molded products and steel plates for hot stamping
KR102668389B1 (en) Manufacturing methods and steel parts of steel parts
EP3715490B1 (en) Method of casting steel alloy component and cast component
KR101775816B1 (en) Large-sized forging steel and large-sized forged part
CN114945698A (en) Plated steel material
EP4332251A1 (en) Steel welded member
US20240227354A1 (en) Steel welded member
CN111936659A (en) High-strength alloyed hot-dip galvanized steel sheet and method for producing same
JP2018115379A (en) Zn-Al PLATED STEEL PLATE EXCELLENT IN PHOSPHATE CHEMICAL PROCESSABILITY, AND PRODUCTION METHOD THEREOF
CN118140000A (en) Steel plate
KR20240089216A (en) hot press member
KR20240089215A (en) hot press member
KR20240007934A (en) High-strength galvanized steel sheets and members and their manufacturing methods
CN118140004A (en) Hot-pressed component

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20210329

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20220630

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20230313

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230719

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602019035413

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20230823

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1602674

Country of ref document: AT

Kind code of ref document: T

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231226

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231123

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240325

Year of fee payment: 6

Ref country code: GB

Payment date: 20240322

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20240320

Year of fee payment: 6

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT