EP0481575B1 - Procédé de fabrication de tôles soudables à haute résistance mécanique et leur application - Google Patents
Procédé de fabrication de tôles soudables à haute résistance mécanique et leur application Download PDFInfo
- Publication number
- EP0481575B1 EP0481575B1 EP91250279A EP91250279A EP0481575B1 EP 0481575 B1 EP0481575 B1 EP 0481575B1 EP 91250279 A EP91250279 A EP 91250279A EP 91250279 A EP91250279 A EP 91250279A EP 0481575 B1 EP0481575 B1 EP 0481575B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- max
- sheet
- cooled
- air
- less
- 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 30
- 239000010959 steel Substances 0.000 title claims abstract description 30
- 238000000034 method Methods 0.000 title claims abstract description 7
- 238000004519 manufacturing process Methods 0.000 title abstract description 6
- 238000005096 rolling process Methods 0.000 claims abstract description 16
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 8
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 8
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 7
- 229910052742 iron Inorganic materials 0.000 claims abstract description 6
- 239000000203 mixture Substances 0.000 claims abstract description 6
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 6
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 6
- 229910052802 copper Inorganic materials 0.000 claims abstract description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 5
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 5
- 239000012535 impurity Substances 0.000 claims abstract 4
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract 4
- 238000005496 tempering Methods 0.000 claims description 17
- 238000003466 welding Methods 0.000 claims description 15
- 238000011282 treatment Methods 0.000 claims description 8
- 239000000463 material Substances 0.000 claims description 7
- 238000010276 construction Methods 0.000 claims description 2
- 230000003068 static effect Effects 0.000 claims 3
- 238000010438 heat treatment Methods 0.000 abstract description 3
- 238000009749 continuous casting Methods 0.000 abstract 1
- 239000000523 sample Substances 0.000 description 11
- 238000001816 cooling Methods 0.000 description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 238000000137 annealing Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 230000007704 transition Effects 0.000 description 3
- 241001136792 Alle Species 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 239000000654 additive Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 229910001562 pearlite Inorganic materials 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000000161 steel melt Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910000859 α-Fe Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 238000007545 Vickers hardness test Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 229910001563 bainite Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
Classifications
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/021—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular fabrication or treatment of ingot or slab
-
- 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
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- 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
-
- 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
- C21D2211/009—Pearlite
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
Definitions
- the invention relates to a method for producing a high-strength weldable sheet and its use according to the preambles of claims 1 and 4.
- Such steels are used for all types of welded structures.
- Thermomechanically rolled, easily weldable steels which can also have a ferritic-pearlitic structure and a yield strength of up to 500 N / mm2, for example grade StE 480.7 TM, have the following composition (in% by weight) according to DE standard DIN 17172: 0 , 04-0.16% C; 0.55% Si; 1.10 to 1.90% Mn; Max. 0.035% P; Max. 0.025% S; Max. 0.20% V and Nb, balance iron.
- Thick-walled sheets made of known steels with yield strength values above 500 N / mm2 receive their good ones Strength properties apart from the alloy additives, in particular Cr, Mo and higher Ni additions, by accelerated cooling with water directly at the rolling heat (Stahlrohr Handbuch, 10th edition, pp. 79-80, plates XLVII, XLVIII).
- the invention is therefore based on the problem of proposing a method for producing a thick-walled sheet from high-strength weldable steel which makes it possible to use the advantages of a ferritic-pearlitic structure of the steel and in which water cooling can be dispensed with and a suitable advantageous one Specify use.
- a steel produced by this special thermomechanical treatment and hardening at temperatures below the transition point A1 has Yield strengths of more than 500 N / mm2 and at the same time ferritic-pearlitic structure. This fine structure gives the steel unexpectedly high toughness values. In extensive tests, it was surprisingly found that it is possible to raise structural steels of this type without accelerated cooling with water by appropriate hardening to yield strength values of up to about 750 N / mm2.
- the slab can be heated both from room temperature and after hot use to the metallurgically favorable temperature of greater than 1200 ° C. known to the person skilled in the art.
- Ti is limited to 0.04% in order to positively influence the fine grain structure of the structure in the heat affected zone of welded component edges.
- the Cu content is deliberately driven above the usual addition amounts in order to activate the strength-increasing effect of Cu by tempering treatment.
- the potential strength of the steel produced according to the invention is thus exploited as far as possible.
- the manufacturing process can also be used for steels with yield strengths of approximately 420-500 N / mm2.
- the alloy additives can be reduced accordingly.
- weldable structural steels of this strength are known, the method according to the invention saves the use of expensive annealing or cooling treatments.
- the preferred tempering temperature is 560-600 ° C. In this area, the effect of Cu on the strength values of the steel is optimized. In addition, components in this temperature range usually become low-voltage after welding annealed so that stress relieving cannot adversely affect the metallurgical effect according to the invention.
- the sheets produced according to the invention in particular with thicknesses of greater than 15 mm to 50 mm and higher, can advantageously be used for offshore structures such as oil platforms, pipes and the like, since the high impact strength combined with a high yield strength and a relatively homogeneous hardness curve over the welding zone of components meet the extreme requirements for the swell strength of steels for such structures.
- the sheets can also be used in commercial vehicle construction such as B. used in mobile cranes or in mining for support purposes.
- a strip of 500 mm width was cut from each of the 2 sheets, divided into 5 sections and annealed in electrically heated laboratory annealing furnaces in the temperature range between 440 and 620 ° C. The individual examinations for the two sheet thicknesses will be discussed below.
- the sheet A 1 was divided into 5 sections Q, R, S, T, U with the dimensions 500 x 400 mm and annealed at 5 tempering temperatures from 480 to 620 ° C. All tempering treatments required an annealing time of 1.5 hours.
- tempering temperatures of 600 ° C approximately the same yield strength and tensile strength values can be determined. It is remarkable that in the above-mentioned tempering temperature range up to 600 ° C the very high yield strengths with values between 600 and 650 N / mm2 for the transverse samples are still associated with good elongation at break values over 24% and very good indentation values over 70%.
- the notched impact strength-temperature profiles are shown in Table 4, lower area, as a function of the tempering temperature.
- values for the transverse samples are still above 200 J / cm2 even at -40 ° C.
- the samples left at 480 ° C are at the lower limit of a scattering band 620 ° C samples annealed as expected at the upper limit.
- Ground specimens (not shown) were taken over the entire sheet thickness. They consistently showed the appearance of grain lines with coarser grains for all heat treatment conditions. While most of the structure was made up of extremely fine-grained crystallites of sizes 12 to 13, there were occasional lines with grain sizes 7 to 8. The structure consisted largely of acicular ferrite and pearlite.
- the notched bar impact specimens also showed extremely high notched bar impact strengths, which were between 239 and 321 J / cm2 at the test temperature of -40 ° C. Even at -80 ° C at least 130 J / cm2 were measured.
- a steel sheet B 1 of 40 mm thickness was produced from a steel melt B (Table 5) in the same way as in Example 1.
- the yield strength was 736 N / mm2, the tensile strength 882 N / mm2 with an elongation at break of 20.2%.
- the melt B showed random traces of Cr and Mo.
- the sheet C 1 not produced according to the invention has only half the thickness of the sheet B 1, its values for the impact energy (Table 6) on the ISO-V cross-sample are about 20 to 40% lower than for sheet B 1. This shows clearly the effect of the invention.
- sample sections were cut to length from the sheet A 2 produced according to the invention and these were welded to one another by manual arc welding and UP tandem welding after a V-seam preparation.
- the samples were subjected to a Vickers hardness test across the weld seam, without first being stress-relieved.
- Table 7 shows the hardness values for sample A 21.
- the measured hardness values HV 10 are plotted on the ordinate for the measuring zones of base material (GW), heat affected zone (WEZ) and weld metal.
- the upper curve in the table shows the Hardness curve at the top of the seam, the lower curve shows the hardness curve at the seam root.
- the weld seam was created with manual arc welding.
- Tables 8 and 10 show in an analogous manner the course of hardness over samples A 22, A 23, which, however, were generated by UP tandem welding.
- Typical of the sheets produced according to the invention are unexpectedly small increases in hardness and decreases in hardness in the heat affected zone.
- the hardening was a maximum of 20% compared to the hardness in the base material (sample A 23, seam root).
- HZ heat affected zone
- Table 11 shows the notched impact energy measured in the welding area for the three samples A 21, A 22, A 23 at the test temperatures + 20 ° C, -10 ° C, -40 ° C.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
Claims (5)
- Procédé de fabrication d'une tôle d'acier à paroi épaisse, ayant une structure ferritique-perlitique, une limite d'étirage supérieure à 500 N/mm² avec en même temps une ténacité élevée et une bonne aptitude au soudage, à partir d'une brame coulée en continu ayant la composition en % en poids :
0,04 à 0,10 % de C
0,25 à 0,50 % de Si
1,40 à 2,00 % de Mn
max. 0,02 % de P
max. 0,01 % de S
0,015 à 0,08 % d'Al
max. 0,01 % de N
0,60 à 1,60 % de Ni
0,60 à 1,60 % de Cu
0,06 à 0,10 % de V
0,03 à 0,05 % de Nb
0,01 à 0,04 % de Ti
le reste étant constitué par du fer et les impuretés inévitables, dans lequel la brame est chauffée à des températures supérieures à 1200°C, refroidie dans l'air à moins de 1000°C de température de surface, puis laminée thermomécaniquement sans pause de laminage avec une température de fin de laminage d'environ 750 à 650°C, la tôle étant ensuite refroidie dans l'air immobile ou en empilement jusqu'à une température inférieure à 200°C, puis, après un réchauffage à environ 420 à 610°C, à nouveau refroidie dans l'air jusqu'à la température ambiante. - Procédé de fabrication d'une tôle d'acier à paroi épaisse, ayant une structure ferritique-perlitique, une limite d'étirage de 420 à 500 N/mm² avec en même temps une ténacité élevée et une bonne aptitude au soudage, à partir d'une brame coulée en continu ayant la composition en % en poids :
0,02 à 0,05 % de C
0,05 à 0,30 % de Si
1,00 à 1,40 % de Mn
max. 0,02 % de P
max. 0,01 % de S
0,015 à 0,08 % d'Al
max. 0,01 % de N
0,30 à 0,60 % de Ni
0,20 à 0,60 % de Cu
0,04 à 0,06 % de V
0,01 à 0,03 % de Nb
0,01 à 0,04 % de Ti
le reste étant constitué par du fer et les impuretés inévitables,
dans lequel la brame est chauffée à des températures supérieures à 1200°C, refroidie dans l'air à moins de 1000°C de température de surface, puis laminée thermomécaniquement sans pause de laminage avec une température de fin de laminage d'environ 750 à 650°C, la tôle étant ensuite refroidie dans l'air immobile ou en empilement jusqu'à une température inférieure à 200°C, puis, après un réchauffage à environ 420 à 610°C, à nouveau refroidie dans l'air jusqu'à la température ambiante. - Procédé selon la revendication 1 ou 2, caractérisé par un traitement de revenu avec un chauffage de la tôle à une température de 560 à 600°C.
- Utilisation d'une tôle obtenue conformément à l'une des revendications 1 à 3, ayant une épaisseur de plus de 15 mm pour des constructions soudées de résistance élevée pour bâtiments en mer et constructions de véhicules utilitaires.
- Elément de construction obtenu par soudage à l'arc, en tôles ayant une épaisseur supérieure à 15 mm, se composant d'acier ayant une structure ferritique-perlitique, une ténacité élevée et une bonne aptitude au soudage, et réalisées à partir d'une brame coulée en continu avec la composition (en % en poids) :
0,02 à 0,10 % de C
0,05 à 0,50 % de Si
1,00 à 2,00 % de Mn
max. 0,02 % de P
max. 0,01 % de S
0,015 à 0,08 % d'Al
max. 0,01 % de N
0,30 à 1,60 % de Ni
0,20 à 1,60 % de Cu
0,04 à 0,10 % de V
0,01 à 0,05 % de Nb
0,01 à 0,04 % de Ti
le reste étant constitué par du fer et les impuretés inévitables, brame qui est chauffée à des températures supérieures à 1200°C, refroidie dans l'air à moins de 1000°C de température de surface, puis laminée thermomécaniquement sans pause de laminage avec une température de fin de laminage d'environ 750 à 650°C, la tôle étant ensuite refroidie dans l'air immobile ou en empilement jusqu'à une température inférieure à 200°C, puis, après un réchauffage à environ 420 à 610°C, à nouveau refroidie dans l'air jusqu'à la température ambiance, l'élément de construction présentant un profil de dureté transversalement au cordon de soudure de métal de base à métal de base avec des valeurs de dureté dont les minima et les maxima diffèrent entre eux de moins de 20 %.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4033700 | 1990-10-19 | ||
DE4033700A DE4033700C1 (fr) | 1990-10-19 | 1990-10-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0481575A2 EP0481575A2 (fr) | 1992-04-22 |
EP0481575A3 EP0481575A3 (en) | 1992-08-26 |
EP0481575B1 true EP0481575B1 (fr) | 1995-06-28 |
Family
ID=6416886
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP91250279A Expired - Lifetime EP0481575B1 (fr) | 1990-10-19 | 1991-10-11 | Procédé de fabrication de tôles soudables à haute résistance mécanique et leur application |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0481575B1 (fr) |
AT (1) | ATE124464T1 (fr) |
DE (2) | DE4033700C1 (fr) |
ES (1) | ES2074651T3 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU2003222211A1 (en) | 2002-02-12 | 2003-09-04 | The Timken Company | Low carbon microalloyed steel |
CN105132805B (zh) * | 2015-09-15 | 2017-03-15 | 攀钢集团攀枝花钢铁研究院有限公司 | 一种含钒焊接结构用钢及其制备方法 |
DE102018132816A1 (de) * | 2018-12-19 | 2020-06-25 | Voestalpine Stahl Gmbh | Verfahren zur Herstellung von thermo-mechanisch hergestellten profilierten Warmbanderzeugnissen |
DE102018132908A1 (de) * | 2018-12-19 | 2020-06-25 | Voestalpine Stahl Gmbh | Verfahren zur Herstellung von thermo-mechanisch hergestellten Warmbanderzeugnissen |
CN114438415A (zh) * | 2022-01-26 | 2022-05-06 | 宝武集团鄂城钢铁有限公司 | 一种36kg级特厚低温高韧性船板钢及其生产方法 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0030309B1 (fr) * | 1979-12-06 | 1985-02-13 | Preussag Stahl Aktiengesellschaft | Feuillard à chaud ou tôle forte en acier dénitruré et procédé pour sa fabrication |
CS330783A2 (en) * | 1982-07-09 | 1984-06-18 | Mannesmann Ag | Zpusob vyroby plechu s jemnozrnnou strukturou z nizce legovane oceli pro vyrobu trub velkeho prumeru |
CA1207639A (fr) * | 1983-03-17 | 1986-07-15 | Rodney J. Jesseman | Tole epaisse en alliage d'acier, et sa fabrication |
DE3818879C1 (fr) * | 1988-06-01 | 1989-11-16 | Mannesmann Ag, 4000 Duesseldorf, De | |
JPH0794687B2 (ja) * | 1989-03-29 | 1995-10-11 | 新日本製鐵株式会社 | 高溶接性、耐応力腐食割れ性および低温靭性にすぐれたht80鋼の製造方法 |
-
1990
- 1990-10-19 DE DE4033700A patent/DE4033700C1/de not_active Expired - Lifetime
-
1991
- 1991-10-11 DE DE59105852T patent/DE59105852D1/de not_active Expired - Fee Related
- 1991-10-11 EP EP91250279A patent/EP0481575B1/fr not_active Expired - Lifetime
- 1991-10-11 AT AT91250279T patent/ATE124464T1/de not_active IP Right Cessation
- 1991-10-11 ES ES91250279T patent/ES2074651T3/es not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0481575A3 (en) | 1992-08-26 |
ES2074651T3 (es) | 1995-09-16 |
DE4033700C1 (fr) | 1992-02-06 |
EP0481575A2 (fr) | 1992-04-22 |
DE59105852D1 (de) | 1995-08-03 |
ATE124464T1 (de) | 1995-07-15 |
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