EP0748877B1 - Procédé de réalisation d'une bande de tôle d'acier laminée à chaud à très haute limite d'élasticité et tôle d'acier obtenue - Google Patents
Procédé de réalisation d'une bande de tôle d'acier laminée à chaud à très haute limite d'élasticité et tôle d'acier obtenue Download PDFInfo
- Publication number
- EP0748877B1 EP0748877B1 EP96401263A EP96401263A EP0748877B1 EP 0748877 B1 EP0748877 B1 EP 0748877B1 EP 96401263 A EP96401263 A EP 96401263A EP 96401263 A EP96401263 A EP 96401263A EP 0748877 B1 EP0748877 B1 EP 0748877B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sheet
- steel sheet
- niobium
- temperature
- thickness
- 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
Links
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 35
- 239000010959 steel Substances 0.000 title claims abstract description 35
- 238000004519 manufacturing process Methods 0.000 title claims description 12
- 238000000034 method Methods 0.000 title claims description 11
- 238000005098 hot rolling Methods 0.000 claims abstract description 13
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 11
- 238000001816 cooling Methods 0.000 claims description 20
- 230000007704 transition Effects 0.000 claims description 16
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 11
- 229910052758 niobium Inorganic materials 0.000 claims description 11
- 239000010955 niobium Substances 0.000 claims description 11
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 11
- 238000005452 bending Methods 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 9
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 9
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 9
- 238000001556 precipitation Methods 0.000 claims description 9
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 8
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 8
- 239000010936 titanium Substances 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910052748 manganese Inorganic materials 0.000 claims description 6
- 239000011572 manganese Substances 0.000 claims description 6
- 229910052750 molybdenum Inorganic materials 0.000 claims description 6
- 239000011733 molybdenum Substances 0.000 claims description 6
- 239000004411 aluminium Substances 0.000 claims description 5
- 229910001563 bainite Inorganic materials 0.000 claims description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims description 5
- 239000011574 phosphorus Substances 0.000 claims description 5
- 238000007493 shaping process Methods 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- 229910052717 sulfur Inorganic materials 0.000 claims description 5
- 239000011593 sulfur Substances 0.000 claims description 5
- 229910000859 α-Fe Inorganic materials 0.000 claims description 5
- 229910001275 Niobium-titanium Inorganic materials 0.000 claims description 4
- RJSRQTFBFAJJIL-UHFFFAOYSA-N niobium titanium Chemical compound [Ti].[Nb] RJSRQTFBFAJJIL-UHFFFAOYSA-N 0.000 claims description 4
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 230000007547 defect Effects 0.000 description 4
- 239000000047 product Substances 0.000 description 3
- 238000007792 addition Methods 0.000 description 2
- 229910000742 Microalloyed steel Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000010438 granite Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
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
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- 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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
Definitions
- the invention relates to a method for producing a sheet metal strip. hot rolled steel with very high yield strength, particularly for the shaping of parts and having a brittle / ductile transition to a temperature below -50 ° C.
- Controlled rolling keeps sheet steel in a low equivalent carbon level and obtain mechanical properties wanted by refining of the ferritic structure grain and coherent precipitation niobium carbonitride, niobium can be combined with titanium or vanadium.
- a product such as a ULCB steel sheet (bainitic structure low carbon) has a higher yield strength at 700 MPa and a brittle / ductile transition temperature of approximately - 60 ° C.
- flawless 180 ° bending of the steel sheet is limited to internal bending diameters greater than 2.5 times the thickness of the sheet in the rolling direction and greater than 3 times the thickness of the sheet in the cross direction of rolling.
- a product such as a micro-alloy steel sheet has a yield strength greater than 700 MPa and can be bent 180 ° without generating a defect for a bending diameter less than twice the thickness of the sheet but this steel has the disadvantage of having a temperature of ductile / brittle transition between -20 ° C and -40 ° C.
- the object of the invention is to present a method for producing a strip of hot-rolled steel sheet with very high yield strength especially for the shaping of parts and presenting a possibility faultless 180 ° bending under a bending diameter of less than twice sheet thickness and brittle / ductile transition at a lower temperature at -50 ° C.
- the invention also relates to a steel sheet as defined in claim 4.
- Figure 1 is a curve showing schematic, according to the method of the invention, the variation of temperature as a function of time, imposed on the strip of hot-rolled sheet steel.
- Figure 2 shows transition curves brittle / ductile for a 5 mm thick steel sheet, brittle / ductile transition measured in the direction long and crosswise of the rolled sheet strip hot.
- the basic composition provides a ferrite microstructure and hardened granular bainite by precipitation of niobium-titanium microalloy elements.
- the rolling process according to the invention aims to obtain a good recrystallization of the austenitic grains at the exit of the rolling mill stands thus allowing obtaining an equiaxed structure.
- Steel structure of sheet metal strip allows high elongations greater than 15 % up to 20% and bending at 180 ° without defect with smaller inside bending diameters twice the thickness of the sheet.
- the temperature at the end of rolling is greater than 850 ° C, and preferably 900 ° C in order to limit the precipitation of micro-alloying elements induced by hot rolling and secondly, to make the most of their effect hardening during controlled cooling.
- Controlled cooling is imposed on the belt hot-rolled sheet after a time interval less than 10 seconds between the end of hot rolling and the start of controlled cooling.
- the time interval is of the order of 1.5 seconds, this which ensures a very fine grain size and a limit high elasticity.
- the controlled cooling rates are chosen between 20 ° C per second and 100 ° C per second in depending on the thickness of the sheet strip to be treated.
- the controlled cooling rate is, on average 40 ° C per second for a strip of sheet metal about 5 mm thick. Under these conditions, there are hardening precipitation of microalloy elements, which provides an upper yield strength at 700 MPa, or 740 MPa.
- End of controlled cooling temperature is between 550 ° C and 750 ° C and preferably 650 ° C, which ensures hardening precipitation of microalloy elements.
- Figure 1 is a diagrammatic curve, according to the process of the invention, the temperature variation in time function imposed on the sheet steel strip after hot rolling. After rolling to a temperature greater than 850 ° C represented by the portion of curve "a”, a period of less than 10 seconds, represented by the portion of curve "b", is requested before controlled cooling of the rolled sheet strip hot which is represented by the portion of curve "c".
- Figure 2 shows two transition curves A and B brittle / ductile, i.e. curves giving the breaking energy of a test piece taken from a sheet metal as a function of temperature.
- Curves A and B relate to a steel sheet 5 mm thick and the brittle / ductile transition is measured respectively in the long direction and in the cross direction of the sheet hot rolled.
- the sheet steel strip according to the invention does not have a brittle / ductile transition in the temperature range between + 20 ° C and -80 ° C. All the ruptures are therefore ductile up to -80 ° C.
- the brittle / ductile transition temperature is therefore less than -80 ° C.
- the method according to the invention allows the realization thick hot-rolled steel sheet between 2.5 and 10 mm, sheet of which the steel has an elastic limit greater than 700 MPa.
- Prison steel can be subjected to a 180 ° bend without defects, the inside diameter of the folding can be less than twice the thickness of the sheet.
- Titanium participates in precipitation hardening in the form of TiC.
- Molybdenum allows after precipitation microalloy elements in the form of carbide, limit carbon diffusion at high temperatures thus ensuring obtaining fine precipitates in the ferritic matrix and lowering the temperature of fragile / ductile transition at a temperature always located below -50 ° C in the case of a steel according to the composition defining the invention.
- the hot-rolled sheet strip according to the invention can be used for parts manufacturing folded profiled or stamped with reduced thickness for their lightening and / or pieces having better mechanical characteristics in fatigue.
- the low temperature of brittle / ductile transition offers the possibility operation of pieces of equipment, entering through example in the construction of cranes, in a field of very low temperature without risk of fragile breakage.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Strip Materials And Filament Materials (AREA)
Description
- carbone ≤ 0,1%,
- 1 % ≤ manganèse ≤ 1,5 %
- silicium ≤ 0,3 %
- phosphore ≤ 0,03 %,
- soufre ≤ 0,01 %,
- 0,01 % ≤ aluminium ≤ 0,1 %,
- 0,04 % ≤ niobium ≤ 0,06 %,
- 0,1 % ≤ titane ≤ 0,15%,
- 0,1 %≤ molybdène ≤ 0,2 %,
est, après laminage à chaud, soumis à un refroidissement contrôlé à une vitesse de refroidissement comprise entre 20°C par seconde et 100°C par seconde jusqu'à une température de fin de refroidissement comprise entre 550°C et 750°C, de façon à obtenir une microstructure de ferrite et bainite granulaire durcie par la précipitation des éléments de micro-alliage niobium-titane.
- la température de fin de laminage à chaud est de préférence supérieure à 850°C ou même 900°C ;
- le temps séparant la fin du laminage à chaud et le début du refroidissement contrôlé est de préférence inférieur à 10 secondes et par exemple de l'ordre de 1,5 seconde.
- carbone ≤ 0,1 %,
- 1 % ≤ manganèse ≤ 1,5 %,
- silicium ≤ 0,3 %,
- phosphore ≤ 0,03 %,
- soufre ≤ 0,01 %,
- 0,01 % ≤ aluminium ≤ 0,1 %,
- 0,04 % ≤ niobium ≤ 0,06 %,
- 0,1 % ≤ titane ≤ 0,15 %,
- 0,1 % ≤ molybdène ≤ 0,2 %.
- 0,06 % ≤ carbone ≤ 0,08 %,
- 1,4 % ≤ manganèse ≤ 1,5 %,
- 0,2 % ≤ silicium ≤ 0.26 %,
- phosphore ≤ 0,02 %,
- soufre ≤ 0,005 %,
- 0,02 % ≤ aluminium ≤ 0,06 %,
- 0,055 % ≤ niobium ≤ 0,06 %,
- 0,110 % ≤ titane ≤ 0,14 %,
- 0,130 % ≤ molybdène ≤ 0,170 %.
Claims (4)
- Procédé de réalisation d'une bande de tôle d'acier laminée à chaud d'épaisseur comprise entre 2,5 mm et 10 mm, dont la limite d'élasticité est supérieure à 700 MPa et qui peut être pliée à 180° sans défaut sous un diamètre intérieur de pliage inférieur à deux fois l'épaisseur de la tôle, utilisable notamment pour la mise en forme de pièces et présentant une transition fragile/ductile à une température inférieure à -50°C, caractérisé en ce que l'acier de composition pondérale suivante :carbone ≤ 0,1%,1 % ≤ manganèse ≤ 1,5 %silicium ≤ 0,3 %phosphore ≤ 0,03 %,soufre ≤ 0,01 %,0,01 % ≤ aluminium ≤ 0,1 %,0,04 % ≤ niobium ≤ 0,06 %,0,1 % ≤ titane ≤ 0,15%,0,1 %≤ molybdène ≤ 0,2 %,
est, après laminage à chaud, soumis à un refroidissement contrôlé à une vitesse de refroidissement comprise entre 20°C par seconde et 100°C par seconde jusqu'à une température de fin de refroidissement comprise entre 550°C et 750°C, de façon à obtenir une microstructure de ferrite et bainite granulaire durcie par la précipitation des éléments de micro-alliage niobium-titane. - Procédé selon la revendication 1, caractérisé en ce que la température de fin de laminage à chaud est supérieure à 850°C.
- Procédé selon les revendications 1 e 2, caractérisé en ce que le temps séparant la fin du laminage à chaud et le début du refroidissement contrôlé est inférieur à 10 secondes.
- Tôle d'acier laminée à chaud d'une épaisseur comprise entre 2,5 mm et 10 mm ayant une limite d'élasticité supérieure à 700 MPa et qui peut être pliée à 180° sans défaut sous un diamètre intérieur de pliage inférieur à deux fois l'épaisseur de la tôle, utilisable notamment pour la mise en forme de pièces et présentant une transition fragile/ductile à une température inférieure à -50°C, tôle obtenue par le procédé selon les revendications 1 à 3, caractérisée en ce que la composition pondérale suivante :carbone ≤ 0,1%,1 % ≤ manganèse ≤ 1,5 %silicium ≤ 0,3 %phosphore ≤ 0,03 %,soufre ≤ 0,01 %,0,01 % ≤ aluminium ≤ 0,1 %,0,04 % ≤ niobium ≤ 0,06 %,0,1 % ≤ titane ≤ 0,15%,0,1 %≤ molybdène ≤ 0,2 %,
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9507122 | 1995-06-15 | ||
FR9507122A FR2735498B1 (fr) | 1995-06-15 | 1995-06-15 | Procede de realisation d'une bande de tole d'acier laminee a chaud a haute limite d'elasticite utlisable notamment pour la mise en forme |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0748877A1 EP0748877A1 (fr) | 1996-12-18 |
EP0748877B1 true EP0748877B1 (fr) | 2001-03-07 |
Family
ID=9480017
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96401263A Expired - Lifetime EP0748877B1 (fr) | 1995-06-15 | 1996-06-11 | Procédé de réalisation d'une bande de tôle d'acier laminée à chaud à très haute limite d'élasticité et tôle d'acier obtenue |
Country Status (6)
Country | Link |
---|---|
US (1) | US5716464A (fr) |
EP (1) | EP0748877B1 (fr) |
AT (1) | ATE199575T1 (fr) |
DE (1) | DE69611950T2 (fr) |
ES (1) | ES2156985T3 (fr) |
FR (1) | FR2735498B1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3417878B2 (ja) * | 1999-07-02 | 2003-06-16 | 株式会社神戸製鋼所 | 伸びフランジ性および疲労特性に優れた高強度熱延鋼板およびその製法 |
WO2001023624A1 (fr) * | 1999-09-29 | 2001-04-05 | Nkk Corporation | Tole d'acier et son procede de fabrication |
FR2801061B1 (fr) | 1999-11-12 | 2001-12-14 | Lorraine Laminage | Procede de realisation d'une bande de tole laminere a chaud a tres haute resistance, utilisable pour la mise en forme et notamment pour l'emboutissage |
JP6252291B2 (ja) * | 2014-03-26 | 2017-12-27 | 新日鐵住金株式会社 | 鋼板及びその製造方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3795506A (en) * | 1971-04-20 | 1974-03-05 | Nippon Kokan Kk | Nonthermal refining type high tension steel exhibiting excellent cold-work-ability |
US3976514A (en) * | 1975-02-10 | 1976-08-24 | Nippon Steel Corporation | Method for producing a high toughness and high tensil steel |
DE2517164A1 (de) * | 1975-04-18 | 1976-10-21 | Rheinstahl Giesserei Ag | Verwendung einer schweissbaren, hoeherfesten stahllegierung fuer dickwandige stahlgusserzeugnisse |
JPS6220821A (ja) * | 1985-07-17 | 1987-01-29 | Nippon Steel Corp | 高強度厚鋼板の製造法 |
JP3031485B2 (ja) * | 1990-11-28 | 2000-04-10 | 川崎製鉄株式会社 | 降伏伸びに優れた高強度鉄筋の製造方法 |
EP0535238A4 (en) * | 1991-03-13 | 1993-08-04 | Kawasaki Steel Corporation | High-strength steel sheet for forming and production thereof |
KR0165151B1 (ko) * | 1994-03-29 | 1999-01-15 | 다나카 미노루 | 취성균열전파정지특성과 저온인성이 우수한 후강판과 그 제조방법 |
-
1995
- 1995-06-15 FR FR9507122A patent/FR2735498B1/fr not_active Expired - Fee Related
-
1996
- 1996-06-11 AT AT96401263T patent/ATE199575T1/de not_active IP Right Cessation
- 1996-06-11 ES ES96401263T patent/ES2156985T3/es not_active Expired - Lifetime
- 1996-06-11 DE DE69611950T patent/DE69611950T2/de not_active Expired - Fee Related
- 1996-06-11 EP EP96401263A patent/EP0748877B1/fr not_active Expired - Lifetime
- 1996-06-13 US US08/663,529 patent/US5716464A/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
H. Berns, Stahlkunde für Ingenieure, 2. ed. juillet 1993, Springer Verlag, Berlin, p. 109-111 * |
Also Published As
Publication number | Publication date |
---|---|
DE69611950D1 (de) | 2001-04-12 |
EP0748877A1 (fr) | 1996-12-18 |
FR2735498B1 (fr) | 1997-07-11 |
ATE199575T1 (de) | 2001-03-15 |
FR2735498A1 (fr) | 1996-12-20 |
US5716464A (en) | 1998-02-10 |
DE69611950T2 (de) | 2001-06-21 |
ES2156985T3 (es) | 2001-08-01 |
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