EP3899063B1 - Superaustenitischer werkstoff - Google Patents
Superaustenitischer werkstoff Download PDFInfo
- Publication number
- EP3899063B1 EP3899063B1 EP19829563.6A EP19829563A EP3899063B1 EP 3899063 B1 EP3899063 B1 EP 3899063B1 EP 19829563 A EP19829563 A EP 19829563A EP 3899063 B1 EP3899063 B1 EP 3899063B1
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- EP
- European Patent Office
- Prior art keywords
- superaustenitic
- material according
- detection limit
- nitrogen
- weight
- Prior art date
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- 239000000463 material Substances 0.000 title claims description 40
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 82
- 229910052757 nitrogen Inorganic materials 0.000 claims description 44
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 42
- 229910045601 alloy Inorganic materials 0.000 claims description 39
- 239000000956 alloy Substances 0.000 claims description 39
- 239000011651 chromium Substances 0.000 claims description 28
- 239000011572 manganese Substances 0.000 claims description 27
- 238000001514 detection method Methods 0.000 claims description 23
- 229910052804 chromium Inorganic materials 0.000 claims description 21
- 229910052750 molybdenum Inorganic materials 0.000 claims description 21
- 229910052748 manganese Inorganic materials 0.000 claims description 20
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 18
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 18
- 239000010949 copper Substances 0.000 claims description 18
- 239000011733 molybdenum Substances 0.000 claims description 18
- 229910052759 nickel Inorganic materials 0.000 claims description 18
- 239000010955 niobium Substances 0.000 claims description 18
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 17
- 229910052799 carbon Inorganic materials 0.000 claims description 15
- 239000010936 titanium Substances 0.000 claims description 15
- 238000000034 method Methods 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 13
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 11
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 229910052758 niobium Inorganic materials 0.000 claims description 11
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 11
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 10
- 239000010941 cobalt Substances 0.000 claims description 10
- 229910017052 cobalt Inorganic materials 0.000 claims description 10
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 10
- 229910052710 silicon Inorganic materials 0.000 claims description 10
- 239000010703 silicon Substances 0.000 claims description 10
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 10
- 229910052721 tungsten Inorganic materials 0.000 claims description 10
- 239000010937 tungsten Substances 0.000 claims description 10
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 9
- 239000012535 impurity Substances 0.000 claims description 9
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 8
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- 229910052796 boron Inorganic materials 0.000 claims description 8
- 229910052698 phosphorus Inorganic materials 0.000 claims description 8
- 239000011574 phosphorus Substances 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 7
- 238000010276 construction Methods 0.000 claims description 5
- 239000000126 substance Substances 0.000 claims description 4
- 238000000137 annealing Methods 0.000 claims description 3
- 239000013535 sea water Substances 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000005864 Sulphur Substances 0.000 claims 7
- 239000004411 aluminium Substances 0.000 claims 6
- 238000003856 thermoforming Methods 0.000 claims 6
- 229910000734 martensite Inorganic materials 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 20
- 238000005260 corrosion Methods 0.000 description 20
- 230000007797 corrosion Effects 0.000 description 20
- 239000010959 steel Substances 0.000 description 20
- 238000005482 strain hardening Methods 0.000 description 7
- 239000000203 mixture Substances 0.000 description 5
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 4
- 229910001566 austenite Inorganic materials 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- GJPVPJBNBCITNZ-UHFFFAOYSA-N [N].[Mn].[Cr] Chemical compound [N].[Mn].[Cr] GJPVPJBNBCITNZ-UHFFFAOYSA-N 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- OGSYQYXYGXIQFH-UHFFFAOYSA-N chromium molybdenum nickel Chemical compound [Cr].[Ni].[Mo] OGSYQYXYGXIQFH-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000005291 magnetic effect Effects 0.000 description 3
- 238000005204 segregation Methods 0.000 description 3
- 230000002195 synergetic effect Effects 0.000 description 3
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000005272 metallurgy Methods 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 230000005298 paramagnetic effect Effects 0.000 description 2
- 230000035699 permeability Effects 0.000 description 2
- 230000008092 positive effect Effects 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910019932 CrNiMo Inorganic materials 0.000 description 1
- 241001295925 Gegenes Species 0.000 description 1
- 229910001199 N alloy Inorganic materials 0.000 description 1
- JXMHJWIFEMFZDH-UHFFFAOYSA-N [Mn].[Mo].[Cr] Chemical compound [Mn].[Mo].[Cr] JXMHJWIFEMFZDH-UHFFFAOYSA-N 0.000 description 1
- MPQIMOMLTNCGNB-UHFFFAOYSA-N [N].[Mn].[Ni].[Cr] Chemical compound [N].[Mn].[Ni].[Cr] MPQIMOMLTNCGNB-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- SJKRCWUQJZIWQB-UHFFFAOYSA-N azane;chromium Chemical compound N.[Cr] SJKRCWUQJZIWQB-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- -1 chromium nitrides Chemical class 0.000 description 1
- 238000004836 empirical method Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- 238000005491 wire drawing Methods 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
- C21D7/10—Modifying the physical properties of iron or steel by deformation by cold working of the whole cross-section, e.g. of concrete reinforcing bars
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- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/13—Modifying the physical properties of iron or steel by deformation by hot working
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- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
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- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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- C21D8/0236—Cold rolling
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- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
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- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
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- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0285—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
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- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
Definitions
- the invention relates to a super-austenitic material and a method for its production.
- Such materials are z. B. used in chemical plant construction or in oil field or gas field technology.
- a requirement for such materials is that they withstand corrosive attack, in particular attack in media with high chloride concentrations.
- Such materials are, for example, from the CN 107876562A , the CN 104195446A or DE 43 42 188 known.
- WO 02/02837 A1 is a corrosion-resistant material for use in media with a high chloride concentration in oil field technology. This is a chromium-nickel-molybdenum superaustenite that has a comparatively low nitrogen content but very high chromium and very high nickel contents.
- the JP 2005 179733 A discloses a super austenitic material.
- chromium-nickel-molybdenum steels usually have improved corrosion behavior compared to the previously mentioned chromium-manganese-nitrogen steels.
- chromium manganese nitrogen steels are a more economical alloy composition that nonetheless offers an excellent combination of strength, toughness and corrosion resistance.
- the chromium-nickel-molybdenum steels mentioned achieve significantly higher corrosion resistance than chromium manganese nitrogen steels, but are associated with significantly higher costs due to the very high nickel content.
- PREN 16 % Cr + 3.3 x % Mo + 16 x % N.
- MARC % Cr + 3.3 x % Mo + 20 x % N + 20 x % C - 0.25 x % Ni - 0.5 x % Mn.
- Comparable steel grades are also known for use as shipbuilding steels for submarines, these being chromium-nickel manganese nitrogen steels which are also alloyed with niobium to stabilize the carbon, but this degrades the impact strength. These steels are generally low in manganese and therefore have relatively good corrosion resistance, but do not achieve the strength of drill collar grades.
- the object of the invention is to create a super-austenitic, high-strength and tough material that can be produced in a comparatively simple and cost-effective manner.
- the material is to be used, in particular in the measuring device industry and especially in the watchmaking industry, in particular as a housing for highly sensitive measuring devices and for screw support axle drives, pumps, flexible pipes, wire guides, chemical apparatus construction and seawater treatment plants. It should have a completely austenitic structure even after an optional cold forming after strain hardening the yield point should be R p0.2 >1000 MPa.
- the alloy according to the invention has the following composition: elements preferred more preferred carbon (C) 0.01 - 0.20 0.01 - 0.1 Silicon (Si) ⁇ 0.5 ⁇ 0.5 Manganese (Mn) 4.0 - 7.0 5.0 - 6.0 Phosphorus (P) ⁇ 0.05 ⁇ 0.05 Sulfur (S) ⁇ 0.005 ⁇ 0.005 iron (Fe) rest rest Chromium (Cr) 24.0 - 28.0 26.0 - 28.0 Molybdenum (Mo) 2.5 - 3.5 2.5 - 3.5 Nickel (Ni) 12.0 - 15.5 13.0 - 15.0 vanadium (V) ⁇ 0.3 Below detection limit Tungsten (W) ⁇ 0.1 Below detection limit copper (Cu) ⁇ 0.15 Below detection limit cobalt (Co) ⁇ 0.5 Below detection limit Titanium (Ti) ⁇ 0.05 Below detection limit Aluminum (Al) ⁇ 0.1 ⁇ 0.1 niobium (Nb) ⁇ 0.025 Below detection limit boron
- the steel according to the invention should be free of precipitation, since precipitation has a negative impact on toughness and corrosion resistance.
- the yield point is R p0.2 >450 MPa and can easily reach values >500 MPa, with the impact work at 20°C being greater than 350 J and values of up to 440 J being reached.
- the yield point is definitely R p0.2 >1000 MPa and values of up to 1100 MPa are achieved in practice, with strain hardened the impact work at 20°C being certainly greater than 80J, with values of 200 J being achieved in practice .
- the notch impact work was determined according to DIN EN ISO 148-1.
- values for the product of tensile strength Rm with notched impact strength KV of more than 100,000 MPa J, preferably >200,000 MPa J, particularly preferably >300,000 MPa J, can be achieved.
- Carbon is contained in contents from 0.01 up to 0.25%. Carbon is an austenite former and has a favorable effect in terms of high mechanical parameters. With a view to avoiding carbidic precipitations, the carbon content should be set to between 0.01 and 0.20% by weight, in particular between 0.01 and 0.10% by weight.
- silicon are ⁇ 0.5% by weight and are mainly used for deoxidizing the steel.
- the specified upper limit reliably avoids the formation of intermetallic phases. Since silicon is also a ferrite former, the upper limit is also selected with a safety range in this regard. In particular, silicon can be provided in contents of 0.1-0.3% by weight.
- Manganese is contained in amounts of 3.0 - 8.0% by weight. This is an extremely low value compared to materials according to the prior art. Up to now it has been assumed that manganese contents of more than 19% by weight, if possible more than 20% by weight, are necessary for high nitrogen solubility. Surprisingly, it has been found with the present alloy that even with the low manganese contents according to the invention, a nitrogen solubility is achieved which is above what is possible according to the prevailing expert opinion. In addition, it was previously assumed that good corrosion resistance goes hand in hand with very high manganese contents, but it has been found according to the invention that this is apparently not necessary due to unexplained synergistic effects in the present alloy.
- the lower limit for manganese can be chosen at 3.5 or 4.0 or 4.5 or 5.0%.
- the upper limit for manganese can be chosen at 6.0 or 6.5 or 7.0 or 7.5%.
- Chromium levels of 17% by weight or more are found to be necessary for higher corrosion resistance. According to the invention, at least 24.0% and at most 30% chromium are included. Up to now it was assumed that contents higher than 24% by weight have an adverse effect on the magnetic permeability, because chromium is one of the ferrite-stabilizing elements. On the other hand, it was found with the alloy according to the invention that even very high chromium contents above 23% do not negatively affect the magnetic permeability in the present alloy, but the resistance to pitting and stress corrosion cracking is known to be optimally influenced.
- the lower limit for chromium can be chosen at 25 or 26%.
- the upper limit for chromium can be chosen at 28 or 29%.
- Molybdenum is an element which contributes significantly to corrosion resistance in general and pitting corrosion resistance in particular, the effect of molybdenum being enhanced by nickel. According to the invention, 2.0 to 4% by weight of molybdenum are added. The lower limit for molybdenum can be chosen at 2.1 or 2.2 or 2.3 or 2.4 or 2.5%. The upper limit for molybdenum can be chosen at 3.5 or 3.6 or 3.7 or 3.8 or 3.9%. Higher molybdenum contents make an ESR treatment absolutely necessary in order to rule out segregation. Remelting processes are very complex and expensive. Therefore, according to the invention, DESU or ESU routes should be avoided.
- tungsten is present in amounts below 0.5% and contributes to the increase in corrosion resistance.
- the upper limit for tungsten can be chosen at 0.4 or 0.3 or 0.2 or 0.1% or below the detection limit (i.e. without any deliberate addition).
- nickel is present in contents of 10 to 16%, as a result of which a high resistance to stress corrosion cracking is achieved in media containing chloride.
- the lower limit for nickel can be chosen at 11 or 12 or 13%.
- the upper limit for nickel can be chosen at 15 or 15.5%.
- the alloying of copper is described as advantageous for the resistance in sulfuric acid, it is found according to the invention that copper at values >0.5% increases the tendency to precipitate chromium nitrides, which has a negative effect on the corrosion properties.
- the upper limit value for copper was set at ⁇ 0.5%, preferably below 0.15%, most preferably below the detection limit.
- Cobalt can be provided in amounts of up to 5% by weight, in particular to replace nickel.
- the upper limit for cobalt can be chosen at 5 or 3 or 1 or 0.5 or 0.4 or 0.3 or 0.2 or 0.1% or below the detection limit (i.e. without any intentional addition).
- Nitrogen is included at levels of 0.50 to 0.90% by weight to ensure high strength. Furthermore, nitrogen contributes to corrosion resistance and is a strong austenite former, which is why higher contents than 0.50% by weight, in particular higher than 0.52% by weight, are favorable. In order to avoid nitrogen-containing precipitates, in particular chromium nitride, the upper limit of nitrogen is limited to 0.90% by weight. It has been shown that despite the very low manganese content, in contrast to known alloys, these high nitrogen contents can be achieved in the alloy . Due to the good nitrogen solubility on the one hand and the disadvantages that are obtained with higher nitrogen contents, in particular over 0.90%, any pressure increase is even out of the question as part of a DESU route.
- the ratio of nitrogen to carbon is greater than 15.
- the lower limit for nitrogen can be chosen at 0.52 or 0.54 or 0.60 or 0.65%.
- the upper limit for nitrogen can be selected at 0.80 or 0.85%.
- boron, aluminum and sulfur can be included as further alloy components, but only optionally.
- the alloy components vanadium and titanium are not necessarily contained in the present steel alloy. Although these elements contribute positively to the solubility of nitrogen, the high nitrogen solubility of the present invention can be provided even in their absence.
- the alloy according to the invention should not contain niobium, since it can form precipitates which reduce toughness. Historically, niobium has only been used to bind carbon, which is not necessary in the alloy of the present invention. The niobium content is still tolerable up to 0.1%, but should not exceed the content of unavoidable impurities.
- the components are melted under atmospheric conditions and then further treated with secondary metallurgy. Blocks are then cast, which are immediately hot-formed.
- ESR Electroslag remelting
- DESU pressure electroslag remelting
- MARC opt 40 ⁇ wt%Cr + 3.3 x wt%Mo + 20 x wt%C + 20 x wt%N - 0.5 x wt%Mn
- MARC formula is optimized by finding that the otherwise usual deduction of nickel does not apply to the system according to the invention and the limit value of 40 is necessary.
- FIG 2 the possible process routes for the production of the alloy composition according to the invention are shown as examples.
- a possible one is now used as an example Route described.
- VID vacuum induction melting unit
- melted material is simultaneously melted and treated for secondary metallurgy.
- the melt is then poured into molds (ingot) and solidifies there into blocks.
- molds ingot
- These are then hot-formed in several steps. For example, pre-forged on the rotary forging machine and brought to final dimensions in the multi-line rolling mill.
- a heat treatment step can also be carried out.
- the cold forming step can be carried out by means of wire drawing.
- a super-austenitic material according to the invention can not only have the described (and in particular in figure 2 illustrated) production routes are produced, the advantageous properties of the alloy according to the invention can also be achieved by a powder-metallurgical production route.
- figure 4 are the three alloys made figure 3 produced by a method according to the invention and subjected to strain hardening.
- R p0.2 was around 1000 MPa for all three materials and the tensile strength Rm was between 1100 MPa and 1250 MPa.
- the impact energy was excellent at 270 J to even over 300 J (alloy C - 329.5 J).
- the advantage of the invention is that an austenitic, high-strength material with increased corrosion resistance and a low nickel content is created, which at the same time shows high strength and paramagnetic behavior.
- a completely austenitic structure is also present after cold forming, so that it has been possible to combine the positive properties of a cost-effective CrMnNi steel with the outstanding technical properties of a CrNiMo steel.
- a special feature of the invention is that, due to the high nitrogen content, the work hardening rate is higher than with other super austenites in order to be able to achieve tensile strengths (R m ) of 2500 MPa.
- R m tensile strengths
- Typical areas of application for the materials according to the invention are shipbuilding and here in particular submarine construction, chemical apparatus construction, seawater treatment plants, the paper industry, screws and bolts, flexible pipes, so-called wirelines, completion tools, springs, valves, umbilicals, axle drives, pumps. Depending on the area of application, there may be minor alloy adjustments which figure 5 are shown.
- the strength can be further increased by cold forming, as already described.
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DE102018133255.6A DE102018133255A1 (de) | 2018-12-20 | 2018-12-20 | Superaustenitischer Werkstoff |
PCT/EP2019/086384 WO2020127788A1 (de) | 2018-12-20 | 2019-12-19 | Superaustenitischer werkstoff |
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DE (1) | DE102018133255A1 (es) |
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CN116121667A (zh) * | 2021-11-14 | 2023-05-16 | 重庆三爱海陵实业有限责任公司 | 气门及其耐高温合金 |
CN115261718B (zh) * | 2022-03-28 | 2023-06-06 | 江西宝顺昌特种合金制造有限公司 | 一种超级奥氏体不锈钢s34565板材及其制备方法 |
CN115992330B (zh) * | 2023-02-17 | 2024-04-19 | 东北大学 | 一种高氮低钼超级奥氏体不锈钢及其合金成分优化设计方法 |
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ES2957403T3 (es) | 2024-01-19 |
DE102018133255A1 (de) | 2020-06-25 |
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EP3899064A1 (de) | 2021-10-27 |
BR112021011849A2 (pt) | 2021-09-08 |
US20220145436A1 (en) | 2022-05-12 |
PL3899064T3 (pl) | 2023-11-20 |
EP3899064B1 (de) | 2023-08-30 |
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JP2022522092A (ja) | 2022-04-14 |
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CA3124189C (en) | 2023-10-31 |
CN113544294A (zh) | 2021-10-22 |
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JP2022514920A (ja) | 2022-02-16 |
US20240052469A2 (en) | 2024-02-15 |
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US20230332282A1 (en) | 2023-10-19 |
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