EP0897018B1 - Duplexstahl mit hoher Festigkeit und Korrosionsbeständigkeit - Google Patents
Duplexstahl mit hoher Festigkeit und Korrosionsbeständigkeit Download PDFInfo
- Publication number
- EP0897018B1 EP0897018B1 EP19980890210 EP98890210A EP0897018B1 EP 0897018 B1 EP0897018 B1 EP 0897018B1 EP 19980890210 EP19980890210 EP 19980890210 EP 98890210 A EP98890210 A EP 98890210A EP 0897018 B1 EP0897018 B1 EP 0897018B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- max
- duplex
- content
- alloy according
- austenite
- 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.)
- Expired - Lifetime
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- 238000005260 corrosion Methods 0.000 title claims description 24
- 230000007797 corrosion Effects 0.000 title claims description 24
- 229910001039 duplex stainless steel Inorganic materials 0.000 title description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 34
- 229910045601 alloy Inorganic materials 0.000 claims description 33
- 239000000956 alloy Substances 0.000 claims description 33
- 239000000463 material Substances 0.000 claims description 29
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 20
- 229910052757 nitrogen Inorganic materials 0.000 claims description 20
- 229910001566 austenite Inorganic materials 0.000 claims description 19
- 229910000859 α-Fe Inorganic materials 0.000 claims description 16
- 239000011651 chromium Substances 0.000 claims description 15
- 239000011572 manganese Substances 0.000 claims description 15
- 229910052804 chromium Inorganic materials 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 10
- 229910052750 molybdenum Inorganic materials 0.000 claims description 10
- 229910052748 manganese Inorganic materials 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 9
- 239000000126 substance Substances 0.000 claims description 9
- 229910052721 tungsten Inorganic materials 0.000 claims description 9
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- 150000004767 nitrides Chemical class 0.000 claims description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 7
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 6
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 239000010937 tungsten Substances 0.000 claims description 6
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 5
- 238000000137 annealing Methods 0.000 claims description 5
- 239000011733 molybdenum Substances 0.000 claims description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 4
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 239000010949 copper Substances 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 239000004411 aluminium Substances 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 239000010955 niobium Substances 0.000 claims description 3
- 229910052698 phosphorus Inorganic materials 0.000 claims description 3
- 239000011574 phosphorus Substances 0.000 claims description 3
- 230000009467 reduction Effects 0.000 claims description 3
- 150000001247 metal acetylides Chemical class 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000005864 Sulphur Substances 0.000 claims 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims 1
- 229910052796 boron Inorganic materials 0.000 claims 1
- 239000011575 calcium Substances 0.000 claims 1
- 229910052791 calcium Inorganic materials 0.000 claims 1
- 239000011777 magnesium Substances 0.000 claims 1
- 229910052749 magnesium Inorganic materials 0.000 claims 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims 1
- 229910052715 tantalum Inorganic materials 0.000 claims 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims 1
- 230000000694 effects Effects 0.000 description 7
- 230000015572 biosynthetic process Effects 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 238000009826 distribution Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000029142 excretion Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- SJKRCWUQJZIWQB-UHFFFAOYSA-N azane;chromium Chemical compound N.[Cr] SJKRCWUQJZIWQB-UHFFFAOYSA-N 0.000 description 1
- CXOWYMLTGOFURZ-UHFFFAOYSA-N azanylidynechromium Chemical compound [Cr]#N CXOWYMLTGOFURZ-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 125000004433 nitrogen atom Chemical group N* 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- 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
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
Definitions
- the invention relates to a duplex alloy for components subject to complex stress high corrosion resistance and high strength, which is essentially a heat-treated one Sigma-phase and nitride-free microstructure and a material strength RM of greater than 800 MPa, a 0.2 proof stress of at least 600 MPa and one Charpy V toughness greater than 125 joules
- Duplex alloys are materials for complex components, which high mechanical values regarding the strength and toughness of the material have and a toughness transition temperature of below - 20 ° C if possible should have. Furthermore, the corrosion resistance of the duplex alloys of great importance because these, abbreviated to DSS (Duplex-Stainless-Steels), in corrosive media in the chemical industry and especially in the OFFSHORE TECHNOLOGY can be used for system components. A good Weldability while avoiding any cracks and maintaining the Corrosion resistance in the zone affected by welding are further requirements for such materials.
- SDSS super duplex stainless steel
- EP-455625-B An improved both in terms of corrosion behavior and in the mechanical and welding properties increased duplex alloy, a So-called SDSS (super duplex stainless steel) is disclosed in EP-455625-B. at an alloy composition of max. 0.04 C, 0.15-0.55 Si, 2.0-2.9 Mn, max. 0.025 P, max. 0.005 S, 23.0-27.0 Cr, 3.0-5.0 Mo, 5.6-8.0 Ni, 0.5-1.0 W, 0-0.5 Cu, 0.2-0.35 N, 0.04-0.25 V, 0-0.20 Nb / Ta, 0-0.04 Ca, 0-0.02 Mg, max, 0.06 Al. Rest Fe and accompanying elements and setting a Ni to Mn ratio value determined within limits and a structural phase factor, the properties are improved overall.
- the invention is based on this prior art (EP-455 625-9) the task of creating a duplex alloy which can be used both in the corrosion and welding properties are improved - as well as higher mechanical material values and a material strength RM of greater than 800 MPa, a 0.2 proof stress of at least 600 MPa and one Charpy V toughness of higher than 125 joules.
- a raw or component made from this alloy has one Heat treatment by solution annealing in the temperature range between 1180 ° C and 850 ° C with subsequent forced cooling a microstructure with one austenite content exceeding the ferrite content.
- the advantages of the duplex alloy according to the invention are in particular that this improved corrosion resistance and increased mechanical Has properties of the material at the same time. Furthermore, the Temperature range for solution annealing before the increased cooling of raw or components expanded so that the heat treatment to adjust the desired austenite-ferrite structure in the structure less accuracy in their Execution requires or the generation security is significantly improved. It is namely with this new alloy through the total effect of the intended Elements in a wide solution annealing temperature range essentially constant and desired ratio of ferrite to austenite in this form Material before, which is an advantageous margin regarding the temperature control in the heat treatment. This gives another advantage to one Use of the alloy according to the invention that also with thick-walled parts a microstructure which is substantially uniform over the cross section are.
- the composition of the duplex material according to the invention in each case within narrow limits.
- Chromium, molybdenum, tungsten and nitrogen generally improve with increasing levels of corrosion resistance of the material, but indicate in their effect and mutual influence of the structural morphology pronounced limits.
- the demanding Limits of 26.0, 5.0, 1.00 and 0.39 in% by weight for the above Elements have been found to promote the formation of the sigma phase and Nitrides excreted. As a result or exacerbate these excretions not only the mechanical properties and the weldability of the Material leaps and bounds, the corrosion resistance of it is also affected by a so-called phase limit depletion adversely affected.
- Concentrations below 24.0 wt% Cr, 4.0 wt% Mo, 0.51 wt% W and The corrosion resistance is reduced in particular below 0.351% by weight of N. and especially the strength of the alloy.
- a comparatively high nitrogen content within narrow limits from 0.351 to 0.39 % By weight is important in the material according to the invention, because thereby how could surprisingly be found, an advantageously homogeneous Distribution of elements between austenite and ferrite in the structure is achieved with
- chrome, tungsten and molybdenum are made by the high Compensating nitrogen contents from the usually alloyed ferrite in the alloyed austenite, which is a significant increase in Corrosion resistance and the tendency to excrete the SIGMA phase largely suppressed.
- manganese in one Concentration range of 2.50 to 3.50 wt .-% is present because manganese on the one hand Nitrogen solubility increased and on the other hand has an austenite-forming function.
- Mn Contents of more than 3.50% by weight of Mn increase the austenite content in the structure, however, reduce the corrosion resistance, and may also have an effect disadvantageous in terms of the achievable material strength and in particular safe setting of a desired ratio of ferrite to austenite in the Heat treatment of parts. Increase manganese contents lower than 2.50% by weight however, the activity of nitrogen in the steel and therefore the risk of Nitride deposits and also change the phase distribution of the structure in disadvantageously.
- Ni contents higher than 7.50% by weight have an extraordinary effect in the alloy stabilizing, resulting in long thermal treatment times and unevenly high Austenite contents depending on the temperature, with lower ones Concentrations than 6.51 wt .-% of nickel higher ferrite contents with the result cause excretions.
- Tungsten fractions of 0.51 to 1.00 wt .-% increase the corrosion resistance and reduce the tendency to form intermetallic phases in the Heat treatment of the material. At W contents below 0.51% by weight, these are mechanical material properties deteriorated, whereas the limit of W values exceeding 1.00% by weight can cause production disadvantages.
- the alloy component vanadium as a strong nitride former is in the intended Limits in terms of fine microstructure and high homogeneity meaningful of the material. Vanadium contents higher than 0.202% by weight mask nitrogen and form harmful, especially row-shaped Nitrides, whereas lower levels of vanadium are no longer effective are, so that Grobkom can arise disadvantageously. This also applies to the in this regard, partially substitutable elements Ti and Nb / Ta.
- Silicon contents in the range between 0.21 and 0.82 wt .-% are with regard to the Material quality is important. Lower concentrations of Si can increase Oxygen levels and a poor degree of purity of the material cause. High values above a content of 0.82% by weight influence due to the ferrite-forming and nitride-forming effects of Si Phase formation disadvantageous. Another disadvantage of higher Si contents is that these favor the formation of intermetallic phases or precipitations
- Aluminum contents of 0.003 to 0.062% by weight are provided in the alloy. Higher Al contents again promote nitride formation and thereby Reduction of the proportion of dissolved nitrogen with all of the above Disadvantages and smaller aluminum values increase the tendency to form coarse grains.
- the austenite is compared to the ferrite Phase with the lower hardness and strength, it is for components from the alloy according to the invention important that the volume fraction of austenite is greater than that of the ferrite is present in the structure. On the one hand, this increases the tendency formation of chromium nitride, which worsens the Usage properties of the part causes, reduced, on the other hand, the Austenite phase due to the dissolved nitrogen with regard to the mechanical Properties improved.
- the new duplex steel according to the invention in specialist circles HDSS (Hyper-Duplex-Stainless- Steel) connects the lowest differences in corrosion potential between alpha and gamma or maximum corrosion resistance and optimal Phase formation kinetics with largely homogeneous distribution of elements between Ferrite and austenite and is therefore concerning the chemical attack that Weldability and the strength properties of the generic Superior materials according to the state of the art.
- HDSS Hydro-Duplex-Stainless- Steel
- the PREN factor calculated from the current alloy composition a value between 44.6 and 49.5, preferably between 45.5 and 48.0, exhibits the highest corrosion resistance of the duplex material become.
- the heat treatment uses a ratio of ferrite to austenite in the structure between 0 , 42 and 0.8, preferably between 0.60 and 0.69, is set, the proportion of the sigma phase and the nitride proportion and the proportion of carbides being less than 5% by weight, preferably less than 0.5% by weight is.
- the good weldability of the material is further improved, with practically none in particular in the zones of the base material which are affected by the heat Impairment of the properties are caused.
- Tab. 1 shows the chemical composition and the PREN factor achieved of examined melts or samples.
- Table 2 shows the heat treatment and the test results.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Description
Beeinträchtigung der Eigenschaften bewirkt sind.
| Chemische Zusammensetzung in Gew.-% | ||||||||||||||||
| Probe | C | Si | Mn | P | S | Cr | Mo | Ni | W | Cu | N | V | Nb+Ta | Ca | Mg | Al |
| A | 0.021 | 0.43 | 1.37 | 0.032 | 0.017 | 22.7 | 3.18 | 5.65 | 0.08 | 0.10 | 0.184 | 0.05 | 0.06 | 0.0003 | 0.000 | < 0.001 |
| B | 0.026 | 0.59 | 1.23 | 0.020 | 0.012 | 21.4 | 3.24 | 5.90 | 0.21 | 0.31 | 0.190 | 0.04 | 0.08 | NB | NB | NB |
| C | 0.029 | 0.78 | 4.9 | 0.022 | 0.004 | 27.6 | 2.4 | 4.51 | 0.8 | 0.43 | 0.312 | 0.06 | 0.09 | 0.0016 | 0.000 | 0.021 |
| D | 0.028 | 0.68 | 5.74 | 0.027 | 0.005 | 26.3 | 2.17 | 4.10 | 0.52 | NB | 0.353 | 0.009 | NB | 0.0011 | NB | 0.002 |
| E | 0.031 | 0.38 | 2.16 | 0.020 | 0.003 | 24.8 | 4.01 | 6.23 | 0.63 | 0.38 | 0.29 | 0.014 | 0.04 | 0.0012 | 0.000 | 0.001 |
| F | 0.028 | 0.50 | 0.66 | 0.009 | 0.001 | 25.9 | 3.83 | 7.15 | 0.64 | 0.61 | 0.236 | 0.021 | NB | NB | NB | 0.005 |
| G | 0.030 | 0.68 | 3.41 | 0.007 | 0.001 | 24.6 | 4.33 | 6.58 | 0.82 | 0.14 | 0.382 | 0.11 | 0.01 | NB | NB | 0.011 |
| H | 0.021 | 0.51 | 3.13 | 0.009 | 0.003 | 25.8 | 4.24 | 7.28 | 0.56 | 0.09 | 0.358 | 0.06 | NB | 0.006 | 0.005 | 0.007 |
| I | 0.027 | 0.38 | 3.04 | 0.010 | 0.002 | 25.1 | 4.53 | 7.16 | 0.62 | 0.28 | 0.371 | 0.08 | 0.04 | 0.002 | NB | 0.019 |
| NB = NICHT BESTIMMT |
| Probe | PREN-Faktor (% Cr+3,3xMo+20xN) | Lösungsglüh-Temp. [°C] | RM [MPa] | RP 0,2 [MPa] | AV (iso-v) [Joule] | FATT [°C] |
| A | 36.9 | 1100 | 730 | 498 | > 300 | -30 |
| B | 35.9 | 1110 | 744 | 506 | 296 | -25 |
| C | 41.7 | 1100 | 758 | 572 | 134 | +/- 0 |
| D | 40.6 | 1120 | 774 | 594 | 128 | -5 |
| E | 43.8 | 1100 | 782 | 586 | 261 | -23 |
| F | 43.2 | 1100 | 760 | 571 | 287 | -20 |
| G | 46.5 | 1060 | 929 | 660 | 202 | -22 |
| H | 47.0 | 1070 | 901 | 631 | 210 | -25 |
| I | 47.5 | 1100 | 912 | 642 | 218 | -22 |
| G,H,I erfindungsgemäße Duplexlegierung |
Claims (6)
- Duplexlegierung für komplex beanspruchte Bauteile mit hoher
Korrosionsbeständigkeit und hoher Festigkeit, welche eine chemische Zusammensetzung in Gew.-% vonEisen Rest und herstellungsbedingte Verunreinigungen besitzt, wobei derKohlenstoff max. 0,04Silizium 0,21 bis 0,82Mangan 2,50 bis 3,50Phosphor max. 0,03Schwefel max. 0,005Chrom 24,0 bis 26,0Molybdän 4,0 bis 5,0Nickel 6,51 bis 7,50Wolfram 0,51 bis 1,00Kupfer max. 0,8Stickstoff 0,351 bis 0,39Vanadin 0,021 bis 0,202Niob/Tantal 0 bis 0,1Calzium 0 bis 0,05Magnesium 0 bis 0,025Aluminium 0,003 bis 0,062Bor max. 0,003
PREN-Faktor der Legierung, gebildet aus ( % Cr + 3,3 x %Mo + 20 x%N), einen Wert zwischen 44,5 und 50 aufweist und diese in wärmebehandeltem Zustand ein im wesentlichen sigmaphasen- und nitridfreies Mischgefüge und eine Materialfestigkeit RM von größer als 800 MPa, eine 0,2 Dehngrenze RP 0,2 von mindestens 600 MPa und eine Charpy-V-Zähigkeit von höher als 125 Joule besitzt. - Duplexlegierung nach Anspruch 1, dadurch gekennzeichnet, daß diese nach einer Wärmebehandlung durch ein Lösungsglühen im Temperaturbereich zwischen 1180°C und 850°C mit anschließender forcierter Abkühlung eine Mikrostruktur mit einem den Ferritanteil übersteigenden Austenitgehalt hat.
- Duplexlegierung nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß diese eine chemische Zusammensetzung in Gew.-% vonEisen Rest und herstellungsbedingte Verunreinigungen besitzt.Kohlenstoff max. 0,028Silizium 0,30 bis 0,62Mangan 2,92 bis 3,38Phosphor max. 0,028Schwefel max. 0,004Chrom 24,8 bis 25,8Molybdän 4,1 bis 4,7Nickel 6,9 bis 7,4Wolfram 0,6 bis 0,8Kupfer max. 0,5Stickstoff 0,352 bis 0,385Vanadin 0,05 bis 0,1Aluminium 0,005 bis 0,009
- Duplexlegierung gemäß einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß der errechnete PREN-Faktor einen Wert zwischen 44,5 und 49,5 , vorzugweise zwischen 45,5 und 48,0 aufweist.
- Duplexlegierung gemäß einem der Ansprüche 1 bis 4. dadurch gekennzeichnet, daß mittels der Wärmebehandlung ein Verhältniswert von Ferrit zu Austenit im Gefüge zwischen 0,42 und 0,8, vorzugsweise zwischen 0,60 und 0,69 eingestellt ist, wobei der Anteil der Sigmaphase und der Nitridanteil und der Anteil an Karbiden unter 5 Gew.-%, vorzugsweise unter 0,5 Gew.-%, ausgebildet ist.
- Duplexlegierung gemäß einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß ein daraus gebildeter Formteil einen Verformungsgrad von mindestens 2,5fach, insbesondere von mindestens 3,8fach, aufweist, wobei der Verformungsgrad als Summe der Reduktion der Querschnittsfläche zu verstehen ist.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT136597 | 1997-08-13 | ||
| AT1365/97 | 1997-08-13 | ||
| AT136597A AT405297B (de) | 1997-08-13 | 1997-08-13 | Duplexlegierung für komplex beanspruchte bauteile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0897018A1 EP0897018A1 (de) | 1999-02-17 |
| EP0897018B1 true EP0897018B1 (de) | 2003-09-03 |
Family
ID=3512308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19980890210 Expired - Lifetime EP0897018B1 (de) | 1997-08-13 | 1998-07-17 | Duplexstahl mit hoher Festigkeit und Korrosionsbeständigkeit |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0897018B1 (de) |
| AT (1) | AT405297B (de) |
| DE (1) | DE59809467D1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2735179C2 (ru) * | 2015-01-20 | 2020-10-28 | Нуово Пиньоне Текнолоджи С.Р.Л. | Коррозионностойкое изделие и способ его изготовления |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6187045B1 (en) | 1999-02-10 | 2001-02-13 | Thomas K. Fehring | Enhanced biocompatible implants and alloys |
| SE524952C2 (sv) * | 2001-09-02 | 2004-10-26 | Sandvik Ab | Duplex rostfri stållegering |
| SE524951C2 (sv) * | 2001-09-02 | 2004-10-26 | Sandvik Ab | Användning av en duplex rostfri stållegering |
| SE527175C2 (sv) | 2003-03-02 | 2006-01-17 | Sandvik Intellectual Property | Duplex rostfri ställegering och dess användning |
| SE527178C2 (sv) * | 2003-03-02 | 2006-01-17 | Sandvik Intellectual Property | Användning av en duplex rostfri stållegering |
| WO2014112445A1 (ja) * | 2013-01-15 | 2014-07-24 | 株式会社神戸製鋼所 | 二相ステンレス鋼材および二相ステンレス鋼管 |
| CN113584377A (zh) * | 2021-06-22 | 2021-11-02 | 济源市瑞麦特金属材料有限公司 | 一种含氮不锈钢及制备方法 |
| CN118253937A (zh) * | 2024-03-25 | 2024-06-28 | 中国第一汽车股份有限公司 | 金属零件及其制备方法和发动机 |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AT397515B (de) * | 1990-05-03 | 1994-04-25 | Boehler Edelstahl | Hochfeste korrosionsbeständige duplex-legierung |
| JP2500162B2 (ja) * | 1991-11-11 | 1996-05-29 | 住友金属工業株式会社 | 耐食性に優れた高強度二相ステンレス鋼 |
| SE501321C2 (sv) * | 1993-06-21 | 1995-01-16 | Sandvik Ab | Ferrit-austenitiskt rostfritt stål samt användning av stålet |
| DE69518354T2 (de) * | 1994-05-21 | 2001-04-26 | Yong Soo Park | Rostfreier Duplex-Stahl mit hoher Korrosionsbeständigkeit |
-
1997
- 1997-08-13 AT AT136597A patent/AT405297B/de not_active IP Right Cessation
-
1998
- 1998-07-17 DE DE59809467T patent/DE59809467D1/de not_active Expired - Lifetime
- 1998-07-17 EP EP19980890210 patent/EP0897018B1/de not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2735179C2 (ru) * | 2015-01-20 | 2020-10-28 | Нуово Пиньоне Текнолоджи С.Р.Л. | Коррозионностойкое изделие и способ его изготовления |
Also Published As
| Publication number | Publication date |
|---|---|
| AT405297B (de) | 1999-06-25 |
| EP0897018A1 (de) | 1999-02-17 |
| DE59809467D1 (de) | 2003-10-09 |
| ATA136597A (de) | 1998-11-15 |
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