EP3105358B1 - Verfahren zur herstellung einer titanfreien legierung - Google Patents

Verfahren zur herstellung einer titanfreien legierung Download PDF

Info

Publication number
EP3105358B1
EP3105358B1 EP15716712.3A EP15716712A EP3105358B1 EP 3105358 B1 EP3105358 B1 EP 3105358B1 EP 15716712 A EP15716712 A EP 15716712A EP 3105358 B1 EP3105358 B1 EP 3105358B1
Authority
EP
European Patent Office
Prior art keywords
max
alloy
titanium
weight
producing
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
EP15716712.3A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP3105358A1 (de
Inventor
Julia Rosenberg
Jutta KLÖWER
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.)
VDM Metals International GmbH
Original Assignee
VDM Metals International GmbH
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
Priority claimed from DE102014002402.4A external-priority patent/DE102014002402A1/de
Priority claimed from DE102014002693.0A external-priority patent/DE102014002693A1/de
Application filed by VDM Metals International GmbH filed Critical VDM Metals International GmbH
Publication of EP3105358A1 publication Critical patent/EP3105358A1/de
Application granted granted Critical
Publication of EP3105358B1 publication Critical patent/EP3105358B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • 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
    • 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • 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
    • 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
    • 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
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/021Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular fabrication or treatment of ingot or slab
    • 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
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • 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
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
    • 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
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • 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
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0263Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
    • 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
    • C21D8/10Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of tubular bodies
    • C21D8/105Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of tubular bodies of ferrous alloys
    • 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0081Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for slabs; for billets
    • 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/08Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tubular bodies or pipes
    • 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • C22C30/02Alloys containing less than 50% by weight of each constituent 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
    • C22C38/002Ferrous 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
    • C22C38/004Very low carbon steels, i.e. having a carbon content of less than 0,01%
    • 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
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • 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
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • 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
    • C22C38/20Ferrous alloys, e.g. steel alloys containing chromium 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
    • C22C38/22Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
    • 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
    • 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
    • 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
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • 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
    • C22C38/52Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
    • 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
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon

Definitions

  • the invention relates to a method for producing a titanium-free alloy with high pitting and crevice corrosion resistance and high yield strength and strength in the work-hardened state.
  • the highly corrosion-resistant alloy Alloy 825 is mainly used in the chemical industry and offshore technology. It is marketed under the material number 2.4858 and has the following chemical composition: C ⁇ 0.025%, S ⁇ 0.015%, Cr 19.5-23.5%, Ni 28-46%, Mn ⁇ 1%, Si ⁇ 0.5% , Mo 2.5-3.5%, Ti 0.6-1.2%, Cu 1.5-3%, Al ⁇ 0.2%, Co ⁇ 1%, Fe balance.
  • the alloy Alloy 825 is a titanium-stabilized material.
  • titanium can cause problems, especially in continuous casting, since it reacts with the SiO 2 of the casting powder (Problem 3). It would be desirable to avoid the element titanium, but this leads to a significant increase in the edge crack tendency.
  • the JP 61288041 A1 refers to an alloy of the following composition: C ⁇ 0,045%, S ⁇ 0,03%, N 0,005 - 0,2%, Cr 14 - 26%, Mn ⁇ 1%, Si ⁇ 1%, Mo ⁇ 8%, Cu ⁇ 2 %, Fe ⁇ 25%, Al ⁇ 2%, B 0.001 - 0.1%, Mg 0.005 - 0.5%, remainder Ni.
  • the content of Nb is generated by a formula.
  • at least one of the elements Ti, Al, Zr, W, Ta, V, Hf may be contained in contents ⁇ 2.
  • the US 2,777,766 discloses an alloy of the following composition: C ⁇ 0.25%, Cr 18-25%, Ni 35-50%, Mo 2-12%, Nb 0.1-5%, Cu up to 2.5%, W up to 5% , Fe remainder (at least 15%).
  • GB 2123031 A is an austenitic high nickel-containing alloy of the following composition: ⁇ 0.05% C, ⁇ 0.04 N, ⁇ 1.0% Si, ⁇ 1.0% Mn, 35-45% Ni, 20-30% Cr, 4 - 7% Mo, balance iron and unavoidable impurities, where Cr + 3 Mo is at least 40%.
  • an austenitic stainless steel which has the following composition (in% by weight):> 0.05-0.15% C, ⁇ 2% Si, 0.1-3% Mn, ⁇ 0.04% P, ⁇ 0.01% S,> 20 - ⁇ 28% Cr,> 15 - 55% Ni,> 2 to 6% Cu, 0.1 - 0.8% Nb, 0.02 - 1.5% V, 0.001 - 0.1% Al,> 0.05 - 0.3% N, ⁇ 0.006% O, balance iron and impurities.
  • the EP 2163655 A1 describes a method for producing a high alloy steel pipe.
  • the following alloy is to be formed into a tube by multi-stage hot and cold forming processes: ⁇ 0.03% C, ⁇ 1.0% Si, 0.05 - 1.5% Mn, ⁇ 0.03% P, ⁇ 0.03 % S,> 22 - ⁇ 40% Ni, 20 - 30% Cr,> 0.01 - ⁇ 4.0% Mo, 0 - 4% Cu, 0.001 - 0.3% Al,> 0.05 - ⁇ 0 , 3% N, ⁇ 0.01% O, balance iron and impurities.
  • a suitable embodiment of the alloy has the following composition (in% by weight) C Max. 0.015% S Max. 0.005% N Max. 0.02% Cr 21.0 - ⁇ 23% Ni > 39.0 - ⁇ 43.0% Mn 0,5 - 0,9% Si 0.2 - ⁇ 0.5% Not a word > 4.5-6.5% Nb Max. 0.15% Cu > 1.6 - ⁇ 2.3% al 0.06 - ⁇ 0.25% Co Max. 0.5% B 0.002 - 0.004% mg 0.006 - 0.015% Fe Remainder as well as smelting-related impurities
  • the chromium content can be modified as follows: Cr > 21.5 - ⁇ 23% Cr 22.0 - ⁇ 23%
  • the molybdenum content can be modified as follows: Not a word > 5 - ⁇ 6.5% Not a word > 5 - ⁇ 6.2%
  • the content of copper can, if necessary, still be set as follows: Cu > 1.6 - ⁇ 2.0%
  • the alloy may still contain the element V in contents (in wt.) V > 0 - 1.0% V 0.2 - 0.7% be added.
  • the iron content in the alloy according to the invention should be> 22%.
  • the PRE total in terms of corrosion resistance of Alloy 825 is PRE 33 and is very low compared to other alloys.
  • Table 2 shows the active quantities PRE according to the prior art. Table 2: Sum of PRE for various prior art alloys Alloy Ni Fe Cr Not a word Other PRE Duplex 2205 5.5 rest 22 3 0.15 N 37 825 40 31 23 3.2 33 28 31 35 27 3.5 1.3 Cu 38 926 25 rest 19 6 0.16 N 47
  • Table 3 shows the results of various pitting corrosion studies.
  • the reduced titanium content has no negative influence on the pitting corrosion temperature.
  • the increased molybdenum content has positive effects.
  • Table 3 Critical pitting corrosion temperature in 6% FeCl 3 3 /% + 1% HCL, over 72 hours (ASTM G-48 Method C).
  • Figures 1 and 2 below show results of tensile tests on the one hand of the reference alloy Alloy 825 and on the other hand of alternative alloys.
  • Molybdenum has a positive effect on yield strength and strength.
  • Figures 3 and 4 illustrate the positive influence of Molydbän.
  • the alloy can also be produced by ESR / VAR remelting.
  • the inventive method is intended to be used for the production of a component in the oil and gas industry.
  • Table 6 contrasts Alloy 825 (standard) with two alloys of the present invention.

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)
  • Manufacturing & Machinery (AREA)
  • Heat Treatment Of Steel (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Arc Welding In General (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP15716712.3A 2014-02-13 2015-02-10 Verfahren zur herstellung einer titanfreien legierung Active EP3105358B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102014002402.4A DE102014002402A1 (de) 2014-02-13 2014-02-13 Titanfreie Legierung
DE102014002693.0A DE102014002693A1 (de) 2014-02-28 2014-02-28 Titanfreie Legierung
PCT/DE2015/000053 WO2015120832A1 (de) 2014-02-13 2015-02-10 Titanfreie legierung

Publications (2)

Publication Number Publication Date
EP3105358A1 EP3105358A1 (de) 2016-12-21
EP3105358B1 true EP3105358B1 (de) 2018-06-13

Family

ID=52875351

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15716712.3A Active EP3105358B1 (de) 2014-02-13 2015-02-10 Verfahren zur herstellung einer titanfreien legierung

Country Status (7)

Country Link
US (1) US10174397B2 (pt)
EP (1) EP3105358B1 (pt)
JP (1) JP6300941B2 (pt)
KR (1) KR101865406B1 (pt)
CN (2) CN114000032A (pt)
BR (1) BR112016012184B1 (pt)
WO (1) WO2015120832A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106391747B (zh) * 2016-11-28 2018-03-16 西安诺博尔稀贵金属材料有限公司 以一般工业用铌条为原料制备核燃料用高纯铌丝的方法
JP2023516503A (ja) * 2020-03-09 2023-04-19 エイティーアイ インコーポレイテッド 耐食性ニッケル基合金
CN114058903B (zh) * 2020-07-30 2022-06-14 宝武特种冶金有限公司 一种镍铁基合金大口径厚壁管及其制造方法
JP2024505366A (ja) * 2021-02-04 2024-02-06 ファオデーエム メタルズ インターナショナル ゲゼルシャフト ミット ベシュレンクテル ハフツング チタン不含のニッケル-クロム-鉄-モリブデン合金の使用
CN113528895B (zh) * 2021-07-19 2022-05-27 江苏图南合金股份有限公司 一种气阀用高硬度3j40合金棒材及其制造方法
CN115747576B (zh) * 2022-10-26 2024-03-22 中国科学院金属研究所 一种高压氢气压缩机临氢膜片用耐氢脆耐疲劳板材的制备方法

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2777766A (en) 1952-06-04 1957-01-15 Union Carbide & Carbon Corp Corrosion resistant alloys
JPS57210940A (en) 1981-06-19 1982-12-24 Sumitomo Metal Ind Ltd Alloy for high-strength oil well pipe with superior stress corrosion cracking resistance
JPS58199851A (ja) 1982-05-17 1983-11-21 Kobe Steel Ltd 酸性油井用高ニツケル合金
JPS58199852A (ja) 1982-12-22 1983-11-21 Kobe Steel Ltd 酸性油井用高ニツケル合金
NO831752L (no) * 1982-05-17 1983-11-18 Kobe Steel Ltd Austenittiske legeringer med hoeyt nikkelinnhold.
JPS61288041A (ja) 1985-06-14 1986-12-18 Babcock Hitachi Kk 耐粒界型応力腐食割れ性、耐孔食性に優れたNi基合金
DE3716665A1 (de) * 1987-05-19 1988-12-08 Vdm Nickel Tech Korrosionsbestaendige legierung
JP3470418B2 (ja) * 1994-11-09 2003-11-25 住友金属工業株式会社 耐海水腐食性と耐硫化水素腐食性に優れた高強度オーステナイト合金
JP3838216B2 (ja) 2003-04-25 2006-10-25 住友金属工業株式会社 オーステナイト系ステンレス鋼
AU2005258506B2 (en) * 2004-06-30 2008-11-20 Nippon Steel Corporation Raw pipe of Fe-Ni alloy and method for production thereof
JP2006023846A (ja) 2004-07-06 2006-01-26 Sony Corp データ出力装置、データ出力方法、コンピュータプログラム及び記録媒体
JP4506958B2 (ja) * 2004-08-02 2010-07-21 住友金属工業株式会社 溶接継手およびその溶接材料
JP5208354B2 (ja) * 2005-04-11 2013-06-12 新日鐵住金株式会社 オーステナイト系ステンレス鋼
WO2007099949A1 (ja) * 2006-03-02 2007-09-07 Sumitomo Metal Industries, Ltd. 耐水蒸気酸化性に優れた鋼管およびその製造方法
DE102007005605B4 (de) * 2007-01-31 2010-02-04 Thyssenkrupp Vdm Gmbh Eisen-Nickel-Chrom-Silizium-Legierung
JP5176561B2 (ja) * 2007-07-02 2013-04-03 新日鐵住金株式会社 高合金管の製造方法
DE102013004365B4 (de) * 2013-03-14 2015-09-24 VDM Metals GmbH Nickelbasislegierung mit Silizium, Aluminium und Chrom

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
BR112016012184B1 (pt) 2021-04-27
JP2017510704A (ja) 2017-04-13
BR112016012184A2 (pt) 2017-09-26
CN105745345A (zh) 2016-07-06
US10174397B2 (en) 2019-01-08
EP3105358A1 (de) 2016-12-21
KR20160135168A (ko) 2016-11-25
JP6300941B2 (ja) 2018-03-28
KR101865406B1 (ko) 2018-06-07
US20170002437A1 (en) 2017-01-05
CN114000032A (zh) 2022-02-01
CN105745345A8 (zh) 2016-08-10
WO2015120832A1 (de) 2015-08-20

Similar Documents

Publication Publication Date Title
EP3105358B1 (de) Verfahren zur herstellung einer titanfreien legierung
EP2855723B1 (de) Nickel-chrom-aluminium-legierung mit guter verarbeitbarkeit, kriechfestigkeit und korrosionsbeständigkeit
EP2855724B1 (de) Nickel-chrom-legierung mit guter verarbeitbarkeit, kriechfestigkeit und korrosionsbeständigkeit
DE602004000140T2 (de) Rostfreier austenitischer Stahl
DE60004737T2 (de) Hitzebeständige Nickelbasislegierung
EP2956562B1 (de) Nickel-kobalt-legierung
EP2882881B1 (de) Verwendung einer nickel-chrom-eisen-aluminium-legierung mit guter verarbeitbarkeit
EP2632628B1 (de) Ni-fe-cr-mo-legierung
EP2678458B1 (de) Nickel-chrom-eisen-aluminium-legierung mit guter verarbeitbarkeit
EP2547804B1 (de) Nickel-chrom-kobalt-molybdän-legierung
EP3228724A1 (de) Verfahren zur einstellung der wärmeleitfähigkeit eines stahls, werkzeugstahl, insbesondere warmarbeitsstahl, und stahlgegenstand
EP3508602A1 (en) Austenitic stainless steel
DE102015008322A1 (de) Verfahren zur Herstellung einer Nickel-Eisen-Chrom-Aluminium-Knetlegierung mit einer erhöhten Dehnung im Zugversuch
DE69802602T2 (de) Schweisszusatzwerkstoff für hochzähem ferritischem Stahl mit niedrigem Chromgehalt
EP1420077B1 (de) Reaktionsträger Werkstoff mit erhöhter Härte für thermisch beanspruchte Bauteile
EP2535430B1 (de) Werkzeugstahl für höher beanspruchte Warmumformungswerkzeuge sowie dessen Herstellungsprozess
DE112016004410T5 (de) Superlegierung mit geringer thermischer ausdehnung und herstellungsverfahren dafür
DE102018133255A1 (de) Superaustenitischer Werkstoff
DE102014002402A1 (de) Titanfreie Legierung
EP1748088B1 (de) Verfahren zur Herstellung eines Halbzeugs oder Bauteils von Fahrwerk- oder Strukturanwendungen im Kraftfahrzeug
DE112021004006T5 (de) Hoch korrosionsbeständige Ni-Cr-Mo-N-Legierung mit überlegener Phasenstabilität
EP1529853B1 (de) Verwendung eines Stahls für Rohrbauteile und Rohrbauteile für Rohr-Wärmetauscher
DE102014002693A1 (de) Titanfreie Legierung
DE102015007929A1 (de) Aluminium-Gusslegierung, Verfahren zum Herstellen eines Bauteils aus einer Aluminium-Gusslegierung und Verwendung einer Aluminium-Gusslegierung
EP3797013B1 (en) An austenitic nickel-base alloy

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: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20160722

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

RIN1 Information on inventor provided before grant (corrected)

Inventor name: KLOEWER, JUTTA

Inventor name: ROSENBERG, JULIA

DAX Request for extension of the european patent (deleted)
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: 20170927

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 502015004668

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: C22C0019050000

Ipc: C21D0006000000

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

RIC1 Information provided on ipc code assigned before grant

Ipc: C21D 9/52 20060101ALI20180206BHEP

Ipc: C22C 38/52 20060101ALI20180206BHEP

Ipc: C21D 6/00 20060101AFI20180206BHEP

Ipc: C22C 38/20 20060101ALI20180206BHEP

Ipc: C21D 1/26 20060101ALI20180206BHEP

Ipc: C21D 9/08 20060101ALI20180206BHEP

Ipc: C22C 38/40 20060101ALI20180206BHEP

Ipc: C21D 9/00 20060101ALI20180206BHEP

Ipc: C21D 8/00 20060101ALI20180206BHEP

Ipc: C22C 38/44 20060101ALI20180206BHEP

Ipc: C21D 8/02 20060101ALI20180206BHEP

Ipc: C21D 9/46 20060101ALI20180206BHEP

Ipc: C22C 38/54 20060101ALI20180206BHEP

Ipc: C22C 38/18 20060101ALI20180206BHEP

Ipc: C22C 38/22 20060101ALI20180206BHEP

Ipc: C22C 38/08 20060101ALI20180206BHEP

Ipc: C22C 30/00 20060101ALI20180206BHEP

Ipc: C22C 1/02 20060101ALI20180206BHEP

Ipc: C22C 38/42 20060101ALI20180206BHEP

Ipc: C21D 8/10 20060101ALI20180206BHEP

INTG Intention to grant announced

Effective date: 20180309

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

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 1008577

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180615

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502015004668

Country of ref document: DE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180613

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

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

Ref country code: CY

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: 20180613

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: 20180913

Ref country code: BG

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: 20180913

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: 20180613

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: 20180613

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

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: 20180613

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: 20180613

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: 20180914

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: 20180613

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

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: 20180613

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: 20180613

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: 20181013

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: 20180613

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: 20180613

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: 20180613

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: 20180613

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: 20180613

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502015004668

Country of ref document: DE

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

26N No opposition filed

Effective date: 20190314

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

Ref country code: SI

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: 20180613

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: 20180613

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190210

Ref country code: MC

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: 20180613

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190228

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

Ref country code: AL

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: 20180613

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

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190228

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190228

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

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190210

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

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190228

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

Ref country code: TR

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: 20180613

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

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: 20181015

Ref country code: MT

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: 20180613

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

Ref country code: HU

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

Effective date: 20150210

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

Ref country code: MK

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: 20180613

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

Ref country code: AT

Payment date: 20240220

Year of fee payment: 10

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

Ref country code: FI

Payment date: 20240219

Year of fee payment: 10

Ref country code: DE

Payment date: 20240219

Year of fee payment: 10

Ref country code: GB

Payment date: 20240219

Year of fee payment: 10

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

Ref country code: SE

Payment date: 20240219

Year of fee payment: 10

Ref country code: IT

Payment date: 20240228

Year of fee payment: 10

Ref country code: FR

Payment date: 20240221

Year of fee payment: 10