Bainitic steel of high strength and high elongation and method to manufacture said bainitic steel
11345983 · 2022-05-31
Assignee
Inventors
Cpc classification
C21D9/52
CHEMISTRY; METALLURGY
International classification
C21D8/00
CHEMISTRY; METALLURGY
C21D1/20
CHEMISTRY; METALLURGY
C21D9/52
CHEMISTRY; METALLURGY
Abstract
The invention relates to a bainite steel consisting of the following elements in weight %: C: 0.25-0.55 Si: 0.5-1.8 Mn: 0.8-3.8 Cr: 0.2-2.0 Ti: 0.0-0.1 Cu: 0.0-1.2 V: 0.0-0.5 Nb: 0.0-0.06 Al: 0.0-2.75 N: <0.004 P: <0.025 S: <0.025 and a method for manufacturing a bainite steel strip that comprises the step of cooling the coiled strip of such composition to ambient temperature, during which the bainite transformation takes place.
Claims
1. A bainite steel comprising the following elements in weight %: C: 0.30-0.50 Si: 1.0-1.8 Mn: 1.0-2.5 Cr: 0.7-1.5 Ti: 0.0-0.08 Cu: 0.0-1.2 V: 0.0-0.5 Nb: 0.0-0.06 Al: 0.0-1.50 N: <0.004 P: <0.025 S: <0.025 the balance being iron and unavoidable impurities, wherein the bainite steel comprises no added alloying Ni or Mo, wherein the bainite has a microstructure with bainite plates with a thickness of less than 100 nm, and wherein the steel has an ultimate tensile strength of at least 1350 MPa, wherein the bainite steel is formed by: casting a slab from a liquid steel of the composition; cooling the slab; reheating the cooled slab to 1250° C.; hot rolling a cast slab into a strip at a temperature of 850° C.; and coiling the strip of steel at a temperature above the bainite start temperature in the range of 350° C.-500° C., and continuously cooling the coiled strip by natural cooling, and wherein no further heat is applied during the step of continuously cooling the coiled strip such that the slab transforms to bainite steel during the cooling the coiled strip.
2. The bainite steel according to claim 1, wherein one or more of the following elements are present in weight %: C: 0.30-0.40 Si: 1.2-1.7 Mn: 1.6-2.1 Cr: 0.9-1.2 Ti: 0.0-0.07 Al: 0.0-0.2.
3. The bainite steel according to claim 1, wherein the steel has a hardness of at least 415 VHN.
4. The bainite steel according to claim 1, wherein the steel has at least a total elongation of 20%.
5. The bainite steel according to claim 1, wherein the steel has a microstructure with 15-30% of retained austenite.
6. The bainite steel according to claim 1, wherein the bainite steel is 70-85% carbide-free bainite.
7. The bainite steel according to claim 1, wherein the bainite steel comprises 70-80% nano-structured bainite.
8. The bainite steel according to claim 1, wherein the Ti and N react to form TiN which in turn forms fine TiCN precipitates.
9. The bainite steel according to claim 1, wherein the steel has a dislocation density in the range of 4-6×10.sup.6.
10. The bainite steel according to claim 1, wherein N is present in a weight % of 0.001-0.004.
11. The bainite steel according to claim 1, further comprising, prior to coiling the strip, cooling the strip formed from the slab to a temperature above the bainite start temperature in the range of 400-550° C.
12. The bainite steel according to claim 1, wherein Cu is present in a weight % of 0.1-1.2.
13. The bainite steel according to claim 1, wherein V is present in a weight % of 0.1-0.5.
Description
BRIEF DESCRIPTION OF THE FIGURES
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DESCRIPTION OF THE INVENTION
(11) In
(12) TABLE-US-00001 TABLE 1 Range of compositions C Si Mn Cr Ti Cu V Nb Al N Min 0.25 0.5 0.8 0.2 0.0 0.0 0.0 0.0 0.01 0.001 Max 0.55 1.8 3.8 2.0 0.1 1.2 0.5 0.06 2.75 0.004
(13) In the diagram B.sub.s and M.sub.s stand for respectively bainite start temperature and martensite start temperature. It can be seen from this figure that a minimal cooling rate 20° C. sec.sup.−1, which is typical of any hot rolling mill, is capable enough to avoid the diffusional bay and in turn avoid the chance of formation of high temperature products like ferrite. The difference between B.sub.s and M.sub.s temperatures provides a reasonably wide processing window to carry out the method for producing bainite.
(14) The M.sub.s will further be suppressed by the formation of bainite where due to the rejection of C from bainitic ferrite, adjacent austenite gets enriched with C, as denoted by the T.sub.0 curve presented in
(15) From
(16) During the progress of bainitic transformation, the whole of the austenite grain does not transform instantaneously to bainite. It is a gradual process; when the first plate of bainite forms, it rejects its excess carbon which it can not accommodate into the adjacent austenite. Further advancement of transformation therefore is associated with a lowering of free energy due to the higher carbon content of austenite from which bainite forms. Finally a time is reached when the free energies of both residual austenite and bainitic ferrite of the same composition becomes identical and therefore any further transformation becomes thermodynamically impossible. T.sub.0 represents the locus of all the points, on a temperature versus carbon concentration plot, where the stress-free austenite and ferrite of identical composition have the same free energy. The bainitic transformation can progress by successive nucleation of subunits of bainitic ferrite till the carbon concentration in the remaining austenite reaches to its limit which is defined by the T.sub.0 curve. The maximum amount of bainite which can be produced at any given transformation temperature is restricted by the retained austenite carbon concentration which can not exceed the limit given by the T.sub.0 curve.
(17) In this approach, bainitic transformation is made to occur at such a temperature where the diffusion of any elements except carbon is extremely negligible. Hence it can be considered that during bainitic transformation no other diffusional reaction interacts with it and the temperature is high enough for restricting other diffusionless transformation product. The carbon enrichment in austenite from adjacent bainitic-ferrite plates makes it thermally stable at room temperature and it will only transform to martensite during deformation exhibiting a TRansformation Induced Plasticity (TRIP) effect.
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(19) It can also be found from
(20) TABLE-US-00002 TABLE 2 Composition in wt % for the 4 casts Heat number C Mn Si Cr S P Al Ti Ni Mo Co 1 0.37 1.84 1.65 0.92 0.01 0.03 0.054 0.068 0.014 0.024 0.005 2 0.345 1.97 1.29 1.03 0.007 0.015 0.036 0.017 0.01 0.01 0.001 3 0.355 2.01 1.46 1.04 0.007 0.016 0.038 0.017 0.01 <0.005 0.001 4 0.32 1.94 1.55 1.01 0.01 0.03 0.01 0.04 0.01 0.01 0.001
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(22) Four 40 kg heats were made in vacuum induction furnace. The chemical compositions of these four casts are given in Table 2 below.
(23) Subsequently, the cast steels were forged to 40 mm thickness and homogenized at 1100° C. for 48 hours after which the steels were cooled along with the furnace. All the experiments were carried out with this homogenized steel.
(24) Small pieces of samples (150 mm×100 mm×20 mm) were cut for hot rolling in an experimental rolling mill. The soaking was done at 1200° for 3 hours. The rolling operation was completed within 6-7 passes, keeping the final rolling temperature at about 850-900° C. Throughout the experiments, temperature was monitored with laser radiation pyrometer. After the hot rolling, the samples were kept on run-out table where water jet cooling was applied till a temperature of 400-550° C. is reached and finally the samples were kept inside a programmable furnace where very slow cooling rate was applied to simulate the actual coil cooling situation. The cooling rate of a coil after coiling in downcoiler in hot strip mill was first measured with radiation pyrometer over a long period of time and similar cooling rate was simulated in furnace for the simulation purpose. The temperature of the furnace for coiling simulation was kept within 350-500° C. Schematic diagram of the entire hot rolling process is shown in
(25) Samples for metallographic observation were cut from the rolling plane of one end of the heat treated samples. The samples were polished using standard procedure, etched with nital and the microstructures are reproduced here in
(26) The volume fraction and the lattice parameter of retained austenite were calculated from the X-ray data by using commercial software, X'Pert High Score Plus. The X-Ray Diffraction analysis results are shown in Table 3 below.
(27) TABLE-US-00003 TABLE 3 Volume fraction of different phases along with C in austenite C in austenite C in austenite Austenite/ (from XRD)/ (from T.sub.0)/ Ferrite/ wt % wt % wt % wt % 22 ± 1.4 1.07 ± 0.06 0.99 79 ± 2.1
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(29) After continuous cooling to room temperature, hardness measurement was to carried out in Vicker's Hardness tester using 30 kg load. The hardness value turned out to be 425±9 VHN which is an averaged out value of 100 readings from four different hot rolled and continuously cooled samples. See Table 4 below for all the mechanical properties (hardness, YS, UTS, uniform elongation, total elongation). The ultimate tensile strength is even more than 1350 MPa.
(30) TABLE-US-00004 TABLE 4 Mechanical properties of the 4 casts Hardness/ YS/ UTS/ YS/ Uniform Total VHN MPa MPa UTS elongation/% elongation/% 425 ± 9 864 ± 28 1366 ± 4 0.63 13.6 ± 0.5 22 ± 0.7
(31) Standard tensile samples were prepared from the steel following the ASTM procedure [ASTM E8] for standard samples of 50 mm gauge length and tested in Instron tensile testing machine (Model number: 5582).