WO2002027056A1 - Ferritic-austenitic stainless steel - Google Patents
Ferritic-austenitic stainless steel Download PDFInfo
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- WO2002027056A1 WO2002027056A1 PCT/SE2001/001986 SE0101986W WO0227056A1 WO 2002027056 A1 WO2002027056 A1 WO 2002027056A1 SE 0101986 W SE0101986 W SE 0101986W WO 0227056 A1 WO0227056 A1 WO 0227056A1
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- ferrite
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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
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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
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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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
- C22C38/002—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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- 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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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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
- 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
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
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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
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
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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
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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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
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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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
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
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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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
Definitions
- the invention relates to a ferritic-austenitic stainless steel having a microstructure which essentially consists of 35-65 vol- % ferrite and 35-65 vol- % austenite.
- the ferritic-austenitic stainless steels - the duplex steels - combine a high mechanical strength and toughness with good corrosion resistance, particularly as far as stress corrosion is concerned.
- austenite and ferrite are well balanced.
- the duplex steels to an increased extent compete with traditional austenitic stainless steels within offshore, paper and pulp industry, chemical industry, and other fields where high strength and corrosion resistance are required.
- the duplex steels which so far are commercially available are, however, too expensive to find wider use, in spite of the fact that the duplex steels generally contain lower contents of the expensive alloy element nickel than comparable austenitic stainless steels.
- Most of the fields where duplex steels are used today are conceivable and suitable fields of use, i.e. for applications within offshore, paper and pulp industry, chemical industry etc., but above all for applications where the corrosion conditions are milder than where duplex steels are employed today, but where high strength and/or good resistance against stress corrosion is a benefit.
- the combination of mechanical strength and corrosion resistance also makes the material suitable for light, maintenance-free constructions within the transportation-, building-, and construction fields.
- a microstructure which contains 35-65 % ferrite and 35-65 % austenite, preferably 35-55 % ferrite and 45-65 % austenite,
- the steel has a chemical composition which contains in weight- %:
- carbon has a very small solubility in the ferrite, which means that the carbon content of the steel substantially is collected in the austenitic phase.
- the carbon content therefore shall be restricted to max 0.07 %, preferably to max 0.05 %, and suitably to max 0.04 %.
- Silicon can be used as a reduction agent at the manufacturing of the steel and exists as a residue from the manufacturing of the steel in an amount of at least 0.1 %. Silicon has favourable features in the steel to the effect that it strengthens the high temperature strength of the ferrite, which has a significant importance at the manufacturing. Silicon also is a strong ferrite former and participates as such in the stabilisation of the duplex structure and should from these reasons exist in an amount of at least 0.2 %, preferably in an amount of at least 0.35 %. Silicon, also have some unfavourable features because it pronouncedly reduces the solubility for nitrogen, which shall exist in high amounts, and if the content of silicon is high also the risk of precipitation of undesired intermetallic phases is increased.
- the silicon content therefore is limited to max 2.0 %, preferably to max 1.5 %, and suitably to max 1.0 %.
- An optimal silicon content is 0.35- 0.80 %.
- Manganese is an important austenite former and increases the solubility for nitrogen in the steel and shall therefore exist in an amount of at least 3 %, preferably at least 4 %, suitably at least 4.5 %.
- Manganese reduces the corrosion resistance of the steel.
- the steel therefore should not contain more than 8 % manganese, preferably max 6 % manganese.
- An optimal content is 4.5-5.5 % manganese.
- Chromium is the most important element for the achievement of a desired corrosion resistance of the steel. Chromium also is the most important ferrite former of the steel and gives in combination with other ferrite formers and with a balanced content of the austenite formers of the steel a desired duplex character of the steel. If the chromium content is low, there is a risk that the steel will contain martensite and if the chromium content is high, there is a risk of impaired stability against precipitation of intermetallic phases and so called 475°-embrittlement, and an unbalanced phase composition of the steel.
- the chromium content shall be at least 19 %, preferably at least 20 %, and suitably at least 20.5 %, and max 24 %, preferably max 23 %, suitably max 22.5 %.
- a suitable chromium content is 21.0-22.0 %, nominally 21.2-21.8 %.
- Nickel is a strong austenite former and has a favourable effect on the ductility of the steel and shall therefore exist in an amount of at least 0.5 %.
- nickel should exist in an amount of at least 0.8 %, suitably at least 1.1%.
- the raw material price of nickel often is high and fluctuates, wherefore nickel, according to an aspect of the invention, is substituted by other alloy elements as far as is possible.
- An optimal nickel content therefore is 1.35-1.70 %Ni.
- Molybdenum is an element which can be omitted according to a wide aspect of the composition of the steel, i.e. molybdenum is an optional element in the steel of the invention. Molybdenum, however, together with nitrogen has a favourable synergy effect on the corrosion resistance. In view of the high nitrogen content of the steel, the steel therefore should contain at least 0.1 % molybdenum, preferably at least 0.15 %. Molybdenum, however, is a strong ferrite former, it can stabilize sigma-phase in the microstructure of the steel, and it also has a tendency to segregate. Further, molybdenum is an expensive alloy element.
- molybdenum content is limited to max 1.0 %, preferably to max 0.8 %, suitably to max 0.65 %.
- An optimal molybdenum content is 0.15-0.54 %.
- Molybdenum can partly be replaced by the double amount of tungsten, which has properties similar to those of molybdenum. However, at least half of the total amount of Mo + W/2 should consist of molybdenum. In a preferred composition the steel, however, the steel does not contain more than max 0.3 tungsten.
- Copper is also an optional element, which can be omitted according to the widest aspect on this element.
- copper is a valuable austenite former and can have a favourable influence on the corrosion resistance in some environments, especially in some acid media, and should therefore exist in an amount of at least 0.1 %.
- the copper content should be maximized to 1.0 %, preferably to max 0.7 %.
- the copper content should be at least 0.15, preferably at least 0.25 and max 0.54 % in order to balance the favourable and possibly unfavourable effects of copper with reference to the features of the steel.
- Nitrogen has a fundamental importance because it is the dominating austenite former of the steel. Nitrogen also contributes to the strength and corrosion resistance of the steel and shall therefore exist in a minimum amount of 0.15 %, preferably at least 0.18 %. The solubility of nitrogen in the steel, however, is limited. In case of a too high nitrogen content there is a risk of formation of flaws when the steel solidifies, and a risk of formation of pores in connection with welding of the steel. The steel therefore should not contain more than 0.30 % nitrogen, preferably max 0.26 % nitrogen. An optimal content is 0.20-0.24 %.
- Boron can optionally exist in the steel as a micro alloying addition up to max 0.005 % (50 ppm) in order to improve the hot ductility of the steel. If boron exists as an intentionally added element, it should exist in an amount of at least 0.001 % (10 ppm) in order to provide the desired effect with reference to improved hot ductility of the steel.
- cerium and/or calcium optionally may exist in the steel in amounts of max 0.03 % of each of said elements in order to improve the hot ductility of the steel.
- the steel does not essentially contain any further intentionally added elements, but only impurities and iron.
- Phosphorus is, as in most steels, a non-desired impurity and should preferably not exist in an amount higher than max 0.035 %.
- Sulphur also should be kept at as low as is possible from an economically manufacturing point of view, preferably in an amount of max 0.10 %, suitably lower, e.g. max 0.002 % in order not to impair the hot ductility of the steel and hence its reliability, which can be a general problem in connection with the duplex steels.
- the contents of ferrite formers and austenite formers shall be balanced according to the conditions which have been mentioned in the foregoing, in order that the steel shall get a desired, stabile duplex character.
- the nickel equivalent, Ni eq should be at least 10.5 and the chromium equivalent at least 21, most advantageously at least 22. Upwards, the nickel equivalent, Ni eq , should be limited to max 15, preferably to max 14. Further the chromium equivalent, Cr eq , should be at least 21, preferably at least 21.5 and most advantageously at least 22, but can be limited to max 23.5.
- a steel with chromium- and nickel equivalents related to one another according to the said criteria has a balanced content of ferrite and austenite within above mentioned content rage.
- the steel because of its alloy composition should contain less or even much less than 35 volume- % ferrite, but measurements carried out through image analyses of the microstructures instead have shown that the steel as a matter of fact contains a stabile content of at least 35 vol- % ferrite and, for several of the tested steels according to the invention, about 50 % ferrite.
- Fig. 1 shows microstructures and a Schaeffler diagram, illustrating the theoretical chromium- and nickel equivalents according to the invention
- Fig. 2 is a bar chart which illustrates the real ferrite and austenite contents which have been measured in examined steels according to the invention
- Fig. 3 is a bar chart illustrating the resistance to pitting corrosion of examined steels in the form of measured critical pitting temperatures, CPT,
- Fig. 4 is a diagram illustrating the resistance to stress corrosion versus time to fracture at drop evaporation testing of a number of examined alloys
- Fig. 5 is a bar charge illustrating the weldability of a number of examined alloys in terms of ferrite content in the heat effected zone (HAZ) and in the welding seam itself.
- the laboratory heats were rolled to the shape of 3 mm thick, narrow plates, which were used for the mechanical tests.
- the 0.2 yield strength lies at a 80-100 MPa lower level than for materials which have been manufactured at a full production scale.
- the 0.2- and 1.0 yield strengths, the ultimate strength (Rm), the elongation in tensile test (A5) and the Brinell hardness were examined at room temperature, 20 °C, and at 150 °C. Representative measurements are given in Table 2.
- the critical pitting temperature, CPT was determined according to the standardized method which is known by the designation ASTM G 150. The results are represented by the chart diagram in Fig. 3. The test shows that the steels V251, V258, and V260 manufactured at a laboratory scale have a significantly better corrosion resistance than V254 and also essentially better than the reference steels Ref. A, ASTM 304 and ASTM 201, but the steels of the invention manufactured at a laboratory scale do not reach the level of ASTM 316 L or UNS S 32304, which however, have a higher content of expensive alloy metals.
- the resistance to stress corrosion was studied according to the drop evaporation test (DEI) described e.g. in MTI manual No. 3, method MTA-5.
- DEI drop evaporation test
- a mono-axially loaded, resistance heated test specimen was exposed to a dripping sodium chloride solution.
- the time to fracture was determined at different load levels, defined as a certain proportion of Rp02 at 200 °C.
- the results for the experimental heats V260 and V254 are shown in Fig. 4 together with data for the austemtic steel ASTM 316L.
- the experimental heats exhibited an essentially higher resistance to stress corrosion than standardized austenitic steels, such as ASTM 316L, V260 appears to be more resistant that V254.
- the weldability of the test alloys was comparable to that of the reference material Ref. A and UNS S 31803. Non destructive testing with x-ray controls could not detect any high porosity levels.
- the material of the invention had a high degree of austenite reformation in the heat affected zone, HAZ, and in the weld in comparison with the reference material Ref. A and UNS S 31803.
- the ferrite content in the case of manual TIG welding a steel of type UNS S 31803, the reference steel Ref. A, and the steel V258 of the invention with a filler metal of type AWS ER2209 is shown in the bar chart in Fig. 5. When subjected to tensile testing, all the welds were fractured in the parent material and not in the welds.
- a strand was made through continuous casting of the molten steel.
- the strand was cut into slabs.
- Some slabs were hot rolled to the shape of plates having thicknesses of 8 mm and 15 mm respectively, while other slabs were hot-rolled to the form of coils having a thickness of 4 mm.
- Some of the hot-rolled coils were further cold rolled to thicknesses of 3 mm, 1.5 mm and 1.0 mm, respectively.
- Test specimens were taken from different parts of the plates and coils respectively.
- the mechanical properties of the hot rolled, 4 mm thick coil were tested at 20 °C. The results of the tests (mean values) are given in Table 4.
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- Heat Treatment Of Sheet Steel (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
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Abstract
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Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2001288179A AU2001288179A1 (en) | 2000-09-27 | 2001-09-18 | Ferritic-austenitic stainless steel |
DE60117276T DE60117276T3 (en) | 2000-09-27 | 2001-09-18 | FERRITISH-AUSTENISTIC STAINLESS STEEL |
EP01967896A EP1327008B2 (en) | 2000-09-27 | 2001-09-18 | Ferritic-austenitic stainless steel |
US12/654,593 US20100172785A1 (en) | 2000-09-27 | 2009-12-23 | Ferritic-austenitic stainless steel |
US14/725,713 US9856551B2 (en) | 2000-09-27 | 2015-05-29 | Ferritic-austenitic stainless steel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0003448-8 | 2000-09-27 | ||
SE0003448A SE517449C2 (en) | 2000-09-27 | 2000-09-27 | Ferrite-austenitic stainless steel |
Related Child Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/381,673 A-371-Of-International US20030172999A1 (en) | 2000-09-27 | 2001-09-18 | Ferritic-austenitic stainless steel |
US10381673 A-371-Of-International | 2001-09-18 | ||
US12/654,593 Continuation US20100172785A1 (en) | 2000-09-27 | 2009-12-23 | Ferritic-austenitic stainless steel |
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WO2002027056A1 true WO2002027056A1 (en) | 2002-04-04 |
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PCT/SE2001/001986 WO2002027056A1 (en) | 2000-09-27 | 2001-09-18 | Ferritic-austenitic stainless steel |
Country Status (9)
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US (3) | US20030172999A1 (en) |
EP (1) | EP1327008B2 (en) |
AT (1) | ATE317919T1 (en) |
AU (1) | AU2001288179A1 (en) |
DE (1) | DE60117276T3 (en) |
ES (1) | ES2258546T5 (en) |
SE (1) | SE517449C2 (en) |
WO (1) | WO2002027056A1 (en) |
ZA (1) | ZA200302011B (en) |
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Also Published As
Publication number | Publication date |
---|---|
DE60117276D1 (en) | 2006-04-20 |
ZA200302011B (en) | 2004-02-16 |
SE0003448L (en) | 2002-03-28 |
DE60117276T3 (en) | 2012-01-19 |
US9856551B2 (en) | 2018-01-02 |
US20150259772A1 (en) | 2015-09-17 |
EP1327008B2 (en) | 2011-07-13 |
SE0003448D0 (en) | 2000-09-27 |
AU2001288179A1 (en) | 2002-04-08 |
ES2258546T3 (en) | 2006-09-01 |
DE60117276T2 (en) | 2006-11-09 |
ATE317919T1 (en) | 2006-03-15 |
SE517449C2 (en) | 2002-06-04 |
EP1327008B1 (en) | 2006-02-15 |
US20100172785A1 (en) | 2010-07-08 |
ES2258546T5 (en) | 2011-12-05 |
EP1327008A1 (en) | 2003-07-16 |
US20030172999A1 (en) | 2003-09-18 |
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