EP0455625B1 - Alliage à structure duplex, à haute résistance mécanique et résistant à la corrosion - Google Patents
Alliage à structure duplex, à haute résistance mécanique et résistant à la corrosion Download PDFInfo
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- EP0455625B1 EP0455625B1 EP91890088A EP91890088A EP0455625B1 EP 0455625 B1 EP0455625 B1 EP 0455625B1 EP 91890088 A EP91890088 A EP 91890088A EP 91890088 A EP91890088 A EP 91890088A EP 0455625 B1 EP0455625 B1 EP 0455625B1
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 55
- 239000000956 alloy Substances 0.000 title claims abstract description 55
- 230000007797 corrosion Effects 0.000 title claims abstract description 51
- 238000005260 corrosion Methods 0.000 title claims abstract description 51
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 44
- 239000011572 manganese Substances 0.000 claims abstract description 34
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 27
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 25
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 19
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 16
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 15
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 15
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 13
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 13
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 9
- 238000001816 cooling Methods 0.000 claims abstract description 6
- 229910052742 iron Inorganic materials 0.000 claims abstract description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 38
- 239000000463 material Substances 0.000 claims description 29
- 239000011651 chromium Substances 0.000 claims description 16
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 9
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 9
- 229910052791 calcium Inorganic materials 0.000 claims description 9
- 239000011733 molybdenum Substances 0.000 claims description 9
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 8
- 239000011575 calcium Substances 0.000 claims description 8
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 229910052720 vanadium Inorganic materials 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 7
- 238000003754 machining Methods 0.000 claims description 7
- 239000010703 silicon Substances 0.000 claims description 7
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 6
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 6
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 5
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 5
- 239000011777 magnesium Substances 0.000 claims description 5
- 229910052749 magnesium Inorganic materials 0.000 claims description 5
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 5
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 5
- 239000010937 tungsten Substances 0.000 claims description 5
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 4
- 239000004411 aluminium Substances 0.000 claims description 4
- 229910052758 niobium Inorganic materials 0.000 claims description 4
- 239000010955 niobium Substances 0.000 claims description 4
- 229910052715 tantalum Inorganic materials 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 3
- 229910052698 phosphorus Inorganic materials 0.000 claims description 3
- 239000011574 phosphorus Substances 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 2
- 239000005864 Sulphur Substances 0.000 claims 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims 1
- 229910052739 hydrogen Inorganic materials 0.000 claims 1
- 239000001257 hydrogen Substances 0.000 claims 1
- 239000011261 inert gas Substances 0.000 claims 1
- 229960004838 phosphoric acid Drugs 0.000 claims 1
- 235000011007 phosphoric acid Nutrition 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 239000012071 phase Substances 0.000 description 11
- 238000000137 annealing Methods 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 6
- 229910052717 sulfur Inorganic materials 0.000 description 6
- 239000011593 sulfur Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 230000000875 corresponding effect Effects 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 239000013535 sea water Substances 0.000 description 3
- 230000002411 adverse Effects 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000005553 drilling Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000005272 metallurgy Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003345 natural gas Substances 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000003856 thermoforming Methods 0.000 description 2
- 229910001262 Ferralium Inorganic materials 0.000 description 1
- 229910000593 SAF 2205 Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001669 calcium Chemical class 0.000 description 1
- 230000015271 coagulation Effects 0.000 description 1
- 238000005345 coagulation Methods 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000012669 compression test Methods 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 230000029142 excretion Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- VCTOKJRTAUILIH-UHFFFAOYSA-N manganese(2+);sulfide Chemical class [S-2].[Mn+2] VCTOKJRTAUILIH-UHFFFAOYSA-N 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000010310 metallurgical process Methods 0.000 description 1
- ZLANVVMKMCTKMT-UHFFFAOYSA-N methanidylidynevanadium(1+) Chemical class [V+]#[C-] ZLANVVMKMCTKMT-UHFFFAOYSA-N 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 231100000989 no adverse effect Toxicity 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000003209 petroleum derivative Substances 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 230000002250 progressing effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 238000007514 turning Methods 0.000 description 1
Images
Classifications
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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
- C22C38/58—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 high-strength, easily weldable, essentially containing the alloy components C, Si, Mn, Cr, Mo, Ni, W, N and V duplex alloy with excellent resistance to corrosion, in particular general or surface-removing corrosion, pitting and Crevice corrosion as well as stress and vibration crack corrosion, in media containing chloride and phosphoric acid and in heat-treated condition with a material strength RM of at least 750 MPa, a 0.2 proof stress RP 0.2 of at least 550 MPa and a Charpy-V toughness of at least 100 joules with good Machining properties.
- Alloys of this type are required for mechanically highly stressed system parts in corrosive media in the chemical industry and especially in the OFF-SHORE TECHNOLOGY in the search for or production and distribution of oil and natural gas. It is necessary that these materials are easy to weld and easy to work with, can withstand high mechanical loads and have above-average toughness properties even at temperatures below 0 ° C.
- the materials must have excellent resistance to all types of corrosion, because chloride-containing and phosphoric acid-containing media in plant parts, pipes and the like, which may be exposed to mechanical direct voltages or mechanical alternating voltages, usually alongside general surface-removing corrosion, rapidly progressing pitting and intercrystalline crevice corrosion and cause stress and vibration crack corrosion.
- a known nitrogen-containing duplex alloy with high corrosion resistance (EP-A2-0220141) is composed in such a way that it has a ferrite content of 30 to 55%, the corrosion resistance being increased by Cr, Mo and N and reduced by manganese and sulfur.
- the contents of the elements tungsten and in particular manganese are capped at 0.5% by weight and 1.2% by weight with regard to the resistance in chloride-containing media.
- EP-A1-0107489 discloses a corrosion-resistant duplex alloy which, in order to improve the mechanical properties and the resistance to pitting corrosion and stress corrosion cracking in seawater, has in particular high manganese contents of 3.5 to 5.0% in order to increase the amount of nitrogen in solution hold and raise the tensile strength and yield strength.
- the disadvantage here is that sigma phase is formed at slower cooling speeds of such materials and the toughness is significantly deteriorated.
- Mn contents of 5 to 7% by weight, nitrogen contents of up to 0.4% by weight and to improve the corrosion resistance, copper contents of 1.1 to 3.0% by weight are used in a duplex alloy containing chromium plus 3x molybdenum of greater than 32% by weight according to WO 85/05129.
- a duplex alloy containing chromium plus 3x molybdenum of greater than 32% by weight according to WO 85/05129.
- EP-A1-0320548 discloses a duplex alloy with improved mechanical properties with better toughness values than FERRALIUM alloy 255 or SAF 2205.
- a characteristic of this alloy is the setting of a ratio of Cr equivalent and Ni equivalent within narrow limits, with nickel contents of 8.0 to 11.0% by weight being maintained due to manganese concentrations of up to 2.0.
- pore formation can occur in the casting and it can also be difficult to carry out the hot deformation, so that it is preferably used to manufacture forged or, in particular, cast parts.
- DE-B2-26 16 599 discloses an alloy with a composition within wide limits for the production of pipes and pipe connections, which parts are used for the transport and further processing of acid gas. To increase the yield strength, these parts must be subjected to cold working after solution annealing, which causes considerable manufacturing disadvantages, particularly in the case of complicated shapes.
- the object of the invention is to create a duplex alloy, in particular for the OFF-SHORE application in the petroleum and natural gas sector and for the chemical industry, which can be produced and processed economically and with a high level of production reliability and which has good thermoforming properties, whereby the parts made from it are easy to weld and process or machinable and the material has high mechanical properties has excellent resistance to all types of corrosion.
- it is therefore essential that the combination of properties of high material strength, high yield strength, good toughness and resistance to surface-removing corrosion, pitting and crevice corrosion as well as stress and vibration crack corrosion is optimized.
- the remainder contains iron and production-related impurities with the proviso that the ratio G of the nickel content in% by weight to the manganese content in% by weight is more than 2.0 but less than 4.0 and the structure phase factor P is formed [2.9x (% Cr) + 2.9x (% Mo) + 1.4x (% W) + 4.4x (% Si) -2.1 (% Ni) -1.0x (% Mn) -62 , 5x (% N)] has a value greater than 40 but less than 65.
- Duplex alloys are cooled from a solution annealing temperature at which the proportion of austenite and ferrite is set depending on the temperature. Increasing proportions of ferrite increase the strength of the material, however the toughness and corrosion resistance are adversely affected. With a share of 40 to 60% of ferrite in the structure, sufficiently high toughness values are achieved with high strength of the material. It is important for the setting of the microstructure that the solution annealing temperature is from 1020 ° to 1150 ° C., preferably from 1050 ° C. to 1100 ° C.
- Carbon is a strong austenite former, but reacts with carbide-forming elements to form carbides that impair toughness and, in particular, corrosion resistance.
- Silicon is a strong ferrite former and is required by melt metallurgy to deoxidize the liquid steel. High levels of silicon impair machinability and promote Sigma phase formation, which reduces toughness. Silicon contents of 0.15 to 0.55, preferably 0.2 to 0.5, are therefore essential.
- Manganese is an austenite former and increases the nitrogen solubility of the melt, but in higher concentrations it favors the toughness-reducing excretion of sigma phase. Low manganese levels cause problems in the melt metallurgy and casting technology with reduced nitrogen solubility and possibly deterioration of the hot formability.
- manganese binds the sulfur with the formation of sulfide, which sulfide inclusions particularly favor pitting and crevice corrosion. It is therefore essential to the invention that the manganese content of the alloy is present within narrow limits, specifically with a concentration of 2.0 to 2.9, preferably 2.1 to 2.7,% by weight and that the sulfur content is less than 0.005% by weight. -% is.
- Chromium is important for establishing a passive state in relation to a corrosion medium and has a ferrite-forming effect. Good corrosion resistance is brought about in the range from 23 to 27, preferably 24 to 26,% by weight of chromium of the alloy.
- Molybdenum is particularly effective against pitting and crevice corrosion, especially in chloride-containing media.
- high molybdenum contents can form molybdenum-rich phases, which adversely affect the corrosion resistance of the material.
- a molybdenum content of the alloy of 3.0 to 5.0, preferably 3.5 to 4.5,% by weight is also important for achieving good weldability.
- Nickel is an important austenite former and is required to adjust the duplex structure with concentrations of 5.6 to 8.0, preferably 6.2 to 7.4,% by weight.
- Tungsten in the content limits of 0.5 to 1.0, preferably 0.55 to 0.9,% by weight decisively improves the hot-formability of the alloy and is also essential for increasing the resistance of the alloy to pitting and crevice corrosion.
- Copper-containing phases deteriorate the pitting and crevice corrosion resistance in chloride-containing media, so that the copper content is at most 0.5, preferably at most 0.35,% by weight.
- Nitrogen is an extremely important alloying element because nitrogen, as an austenite former, solidifies the austenite phase without loss of toughness. Nitrogen also inhibits the precipitation of intermetallic phases and promotes the chromium distribution between austenite and ferrite. Nitrogen levels of 0.2 to 0.35% by weight are particularly effective.
- Vanadium forms fine vanadium carbides, in particular vanadium carbonitrides, in a concentration range from 0.04 to 0.25, preferably from 0.05 to 0.15,% by weight, as a result of which grain refinement and solidification of the material result in improved weldability and thermal structural stability becomes.
- Lower vanadium contents can lead to coarse grain formation, higher concentrations can lead to a coagulation of the carbonitrides and nitrides which is disadvantageous for the material properties.
- An aluminum content of the alloy cannot be absolutely prevented in most of the melt-metallurgical processes, but must be limited to a maximum of 0.06, preferably to a maximum of 0.04,% by weight because of the aluminum nitride formation, which significantly reduces the toughness.
- Niobium / tantalum enhances the beneficial effect of vanadium and can contain up to 0.2, preferably up to 0.1,% by weight in the alloy be provided.
- Calcium is a particularly effective deoxidation element and a strong sulfide former and improves the purity and the properties, in particular the machinability, of the alloy at concentrations of up to 0.04% by weight. Calcium with a content of 0.001 to 0.015% by weight largely prevents the formation of harmful manganese sulfides, calcium inclusions having a positive effect on the machining.
- Magnesium contents of up to 0.02% by weight favor the thermoforming properties and can increase the degree of purity of the material.
- Essential to the invention for a high level of properties of the mechanical and corrosion-chemical-metallurgical characteristic values of the material corresponding to the complex requirements of the alloy are a ratio value G of the nickel content to the manganese content and a structural factor P which reflects the different and differently strong effects of the individual elements on the phase distribution heat treatment.
- the hot formability determined by duplex alloys is compared with the respective nickel to manganese ratio value G by compression tests.
- a hot upsetting test cylindrical samples with a diameter of 12 mm and a height of 18 mm at a temperature of 1150 C were compressed in a press or hammer mechanism to a third of the initial height and the side surface formed by free spreading was examined for cracks. In these experiments, mesh-like cracks usually develop on poorly deformable materials.
- the hot-formability of the material drops sharply from a ratio G of 4, that is to say above the range according to the invention.
- Fig. 3 shows the influence of the sulfur and manganese content of duplex alloys on the pitting corrosion potential in synthetic sea water, aerated at a temperature of 80 ° C. It can be seen from the diagram that, according to the invention, sulfur contents of less than 0.005% by weight are required to achieve a high resistance of the material to pitting corrosion, the manganese content essentially increasing the nitrogen solubility of the melt or the nitrogen content of the alloy, thereby improving the corrosion resistance is effected.
- FIG. 4 shows the corrosion behavior of duplex alloys according to the invention in phosphoric acid as a function of the temperature on the basis of isocorrosion lines a, b and c.
- the machining behavior of ferrite-austenite materials is shown in the diagram in FIG. 5.
- a machining behavior is checked by drilling when measuring the total drilling depth and / or by turning when determining the machined volume.
- Alloys according to the invention with a ratio G (nickel content to manganese content) of 2 to 4 and a calcium content of approx. 0.006% by weight have good machining behavior, whereas comparison alloys, in particular those with low manganese concentrations or high G values, are difficult to machine.
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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)
- Manufacture And Refinement Of Metals (AREA)
- Chemically Coating (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
- Heat Treatment Of Articles (AREA)
- Secondary Cells (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Claims (7)
- Alliage duplex, à haute résistance et se soudant bien, contenant essentiellement les composants d'alliage C, Si, Mn, Cr, Mo, Ni, W, N et V, qui possède une résistance excellente à la corrosion, notamment la corrosion générale ou la corrosion d'attaque superficielle, la corrosion en trous ou en fentes, la corrosion en criques sous des contraintes et sous des efforts alternés, dans des milieux contenant des chlorures et des milieux contenant de l'acide phosphorique et à l'état traité à chaud, une résistance mécanique du matériau RM au moins égale à 750 MPa, une limite d'élasticité 0,2 RP0,2 au moins égale à 550 MPa et une résilience Charpy sur encoche en V au moins égale à 100 Joules dans le cas de bonnes propriétés d'usinage, cet alliage, qui, après un traitement thermique et au moyen d'un refroidissement forcé à partir d'une température comprise entre 1020 °C et 1 150 °C, comporte de la ferrite et de l'austénite dans un rapport de 40 à 60 %, contenant, en % en poids :Carbone max 0,04Silicium 0,15 à 0,55Manganèse 2,0 à 2,9Phosphore max 0,025Soufre max 0,005Chrome 23,0 à 27,0Molybdène 3,0 à 5,0Nickel 5,6 à 8,0Tungstène 0,5 à 1,0Cuivre max 0,5Azote 0,2 à 0,35Vanadium 0,04 à 0,25Niobium/tantale 0 à 0,20Calcium 0 à 0,04Magnésium 0 à 0,02Aluminium max 0,06,avec un complément constitué de fer et d'impuretés dues à la fabrication, sous la réserve que la valeur de rapport G de la teneur en nickel en % en poids à la teneur en manganèse en % en poids soit supérieure à 2,0, mais inférieure à 4,0 et que le facteur de phases de structure P, constitué par:
[2,9.(%Cr) + 2,9.(%Mo) + 1,4.(%W) + 4,4.(%Si) - 2,1.(%Ni) - 1,0.(%Mn) - 62,5.(%N)], ait une valeur supérieure à 40, mais inférieure à 65. - Alliage duplex selon la revendication 1, caractérisé en ce qu'il contient, en % en poids :Carbone max 0,03Silicium 0,2 à 0,5Manganèse 2,1 à 2,7Phosphore max 0,025Soufre max 0,005Chrome 24,0 à 26,0Molybdène 3,5 à 4,5Nickel 6,2 à 7,4Tungstène 0,55 à 0,9Cuivre max 0,35Azote 0,20 à 0,30Vanadium 0,05 à 0,15Niobium/tantale jusqu'à 0,1Calcium jusqu'à 0,02Magnésium jusqu'à 0,02Aluminium max 0,04.
- Alliage duplex selon l'une des revendications 1 et 2, caractérisé en ce qu'il contient, en % en poids :Calcium 0,01 à 0,015.
- Alliage duplex selon l'une des revendications 1 à 3, caractérisé en ce qu'il contient, en % en poids :Aluminium max 0,025.
- Alliage duplex selon l'une des revendications 1 à 4, caractérisé en ce que la valeur de rapport G est supérieure à 2,2, mais inférieure à 3,5.
- Alliage duplex selon l'une des revendications 1 à 5, caractérisé en ce que le facteur de phases de structure P a une valeur supérieure à 45, mais inférieure à 59.
- Alliage duplex selon l'une des revendications 1 à 6, caractérisé en ce qu'il est soumis à un traitement thermique par refroidissement à partir d'une température comprise entre 1 050 °C et 1 100 °C et en utilisant de l'eau ou un gaz inerte, par exemple de l'hydrogène.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT1007/90 | 1990-05-03 | ||
AT0100790A AT397515B (de) | 1990-05-03 | 1990-05-03 | Hochfeste korrosionsbeständige duplex-legierung |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0455625A1 EP0455625A1 (fr) | 1991-11-06 |
EP0455625B1 true EP0455625B1 (fr) | 1994-07-06 |
Family
ID=3504787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP91890088A Revoked EP0455625B1 (fr) | 1990-05-03 | 1991-04-25 | Alliage à structure duplex, à haute résistance mécanique et résistant à la corrosion |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0455625B1 (fr) |
AT (2) | AT397515B (fr) |
DE (1) | DE59102100D1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT405297B (de) * | 1997-08-13 | 1999-06-25 | Boehler Edelstahl | Duplexlegierung für komplex beanspruchte bauteile |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU703877B2 (en) * | 1995-09-27 | 1999-04-01 | Nippon Steel & Sumitomo Metal Corporation | Welded high-strength steel structure with excellent corrosion resistance |
SE519589C2 (sv) * | 1998-02-18 | 2003-03-18 | Sandvik Ab | Användning av höghållfast rostfritt stål i apparatur för framställning av kaustiksoda |
SE524951C2 (sv) * | 2001-09-02 | 2004-10-26 | Sandvik Ab | Användning av en duplex rostfri stållegering |
SE524952C2 (sv) * | 2001-09-02 | 2004-10-26 | Sandvik Ab | Duplex rostfri stållegering |
SE527178C2 (sv) * | 2003-03-02 | 2006-01-17 | Sandvik Intellectual Property | Användning av en duplex rostfri stållegering |
SE527175C2 (sv) | 2003-03-02 | 2006-01-17 | Sandvik Intellectual Property | Duplex rostfri ställegering och dess användning |
SE531593C2 (sv) * | 2007-10-26 | 2009-06-02 | Sandvik Intellectual Property | Värmeväxlare för fosforsyramiljö |
EP3693121B8 (fr) | 2011-01-27 | 2022-04-13 | NIPPON STEEL Stainless Steel Corporation | Tôle d'acier plaquée en acier inoxydable duplex en tant que matériau de placage et son procédé de production |
JP5868206B2 (ja) | 2011-03-09 | 2016-02-24 | 新日鐵住金ステンレス株式会社 | 溶接部耐食性に優れた二相ステンレス鋼 |
KR101702252B1 (ko) * | 2013-01-15 | 2017-02-03 | 가부시키가이샤 고베 세이코쇼 | 2상 스테인리스강재 및 2상 스테인리스강관 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2815439C3 (de) * | 1978-04-10 | 1980-10-09 | Vereinigte Edelstahlwerke Ag (Vew), Wien Niederlassung Vereinigte Edelstahlwerke Ag (Vew) Verkaufsniederlassung Buederich, 4005 Meerbusch | Verwendung eines ferritisch-austenitischen Chrom-Nickel-Stahles |
JPS58197260A (ja) * | 1982-05-13 | 1983-11-16 | Kobe Steel Ltd | 酸性油井用2相系ステンレス鋼 |
GB2128632A (en) * | 1982-10-23 | 1984-05-02 | Mather & Platt Ltd | Stainless steel |
CA1242095A (fr) * | 1984-02-07 | 1988-09-20 | Akira Yoshitake | Acier inoxydable duplex ferritique-austenitique |
EP0179117A1 (fr) * | 1984-04-27 | 1986-04-30 | Bonar Langley Alloys Limited | Acier inox duplex a haute teneur en chrome |
JPS61564A (ja) * | 1984-06-13 | 1986-01-06 | Nippon Kokan Kk <Nkk> | 衝撃特性の優れた2相ステンレス鋼 |
SE453838B (sv) * | 1985-09-05 | 1988-03-07 | Santrade Ltd | Hogkvevehaltigt ferrit-austenitiskt rostfritt stal |
EP0320548B1 (fr) * | 1987-12-17 | 1992-08-12 | Esco Corporation | Procédé de fabrication d'un acier inoxydable duplex et produit en acier inoxydable duplex, présentant des caractéristiques mécaniques améliorées |
US4816085A (en) * | 1987-08-14 | 1989-03-28 | Haynes International, Inc. | Tough weldable duplex stainless steel wire |
-
1990
- 1990-05-03 AT AT0100790A patent/AT397515B/de not_active IP Right Cessation
-
1991
- 1991-04-25 AT AT91890088T patent/ATE108220T1/de not_active IP Right Cessation
- 1991-04-25 DE DE59102100T patent/DE59102100D1/de not_active Revoked
- 1991-04-25 EP EP91890088A patent/EP0455625B1/fr not_active Revoked
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT405297B (de) * | 1997-08-13 | 1999-06-25 | Boehler Edelstahl | Duplexlegierung für komplex beanspruchte bauteile |
Also Published As
Publication number | Publication date |
---|---|
EP0455625A1 (fr) | 1991-11-06 |
ATE108220T1 (de) | 1994-07-15 |
AT397515B (de) | 1994-04-25 |
DE59102100D1 (de) | 1994-08-11 |
ATA100790A (de) | 1993-09-15 |
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