EP1340564B1 - Use of a hardenable copper alloy - Google Patents
Use of a hardenable copper alloy Download PDFInfo
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- EP1340564B1 EP1340564B1 EP03001084A EP03001084A EP1340564B1 EP 1340564 B1 EP1340564 B1 EP 1340564B1 EP 03001084 A EP03001084 A EP 03001084A EP 03001084 A EP03001084 A EP 03001084A EP 1340564 B1 EP1340564 B1 EP 1340564B1
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- copper alloy
- tensile strength
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- cobalt
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- 229910000881 Cu alloy Inorganic materials 0.000 title claims abstract description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 10
- 239000010949 copper Substances 0.000 claims abstract description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 7
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052790 beryllium Inorganic materials 0.000 claims abstract description 7
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052802 copper Inorganic materials 0.000 claims abstract description 7
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 6
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- 239000011651 chromium Substances 0.000 claims abstract description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 3
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 3
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 3
- 239000010941 cobalt Substances 0.000 claims abstract 6
- 229910017052 cobalt Inorganic materials 0.000 claims abstract 6
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract 6
- 229910052749 magnesium Inorganic materials 0.000 claims abstract 4
- 239000011777 magnesium Substances 0.000 claims abstract 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract 3
- 229910052684 Cerium Inorganic materials 0.000 claims abstract 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims abstract 2
- 229910052735 hafnium Inorganic materials 0.000 claims abstract 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims abstract 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims abstract 2
- 229910052758 niobium Inorganic materials 0.000 claims abstract 2
- 239000010955 niobium Substances 0.000 claims abstract 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract 2
- 229910052715 tantalum Inorganic materials 0.000 claims abstract 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000010936 titanium Substances 0.000 claims abstract 2
- 229910052719 titanium Inorganic materials 0.000 claims abstract 2
- 229910052720 vanadium Inorganic materials 0.000 claims abstract 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract 2
- 238000005266 casting Methods 0.000 claims description 20
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 230000032683 aging Effects 0.000 claims description 4
- 238000000137 annealing Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- 229910045601 alloy Inorganic materials 0.000 description 18
- 239000000956 alloy Substances 0.000 description 18
- 239000000463 material Substances 0.000 description 14
- 230000035939 shock Effects 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 238000005336 cracking Methods 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 230000008646 thermal stress Effects 0.000 description 3
- 238000013461 design Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000002028 premature Effects 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000007542 hardness measurement Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 210000003041 ligament Anatomy 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000003856 thermoforming Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0637—Accessories therefor
- B22D11/0648—Casting surfaces
- B22D11/066—Side dams
Definitions
- the invention relates to the use of a curable copper alloy as a material for the production of blocks for the side dams of strip casting plants.
- the side dams consist in the example of the U.S. Patent 3,865,176 known strip casting from metallic form or Soendammblöcken with T-groove, which on a flexible endless belt, z. As steel, are lined up and move in synchronism with the casting belts in the longitudinal direction. The side dam blocks (dam blocks) thereby limit the mold cavity formed by the casting belts.
- EP 0 346 645 B1 describes a curable copper-based alloy consisting of 1.6 to 2.4% nickel, 0.5 to 0.8% silicon, 0.01 to 0.2% zirconium, optionally up to 0.4% chromium and / or bis to 0.2% iron, balance copper including manufacturing impurities.
- This known copper alloy basically meets the requirements for a long service life, if it is used as a material for the production of standard shaped blocks for the side dams of strip casting plants.
- CuNiSiZr alloy described disadvantageously tends at very high mechanical and thermal stresses in the casting operation of a strip casting plant for premature wear of the side edges and casting surfaces. This wear is - as research results have shown - due to a material softening of the casting edges and surfaces to a value below 160 HV.
- the thermal shock resistance of the known CuNiSiZr alloy when used as a side dam block with tongue and groove is not always sufficient to effectively prevent cracking in the T-slot in the casting insert.
- EP 0 548 636 A and US 4 179 314 A disclose other Cu alloys and their use for molds
- composition of alloy D is a known CuNiSi base alloy, while E and F are standardized CuCo2Be and CuCoNiBe materials, respectively.
- All copper alloys were melted in an induction crucible furnace and cast in a continuous casting process into round blocks with a diameter of 280 mm.
- the round blocks of the example alloys A, B and C were extruded on an extruder at a temperature above 900 ° C to flat bars of dimension 79 x 59 mm and then drawn with a cross-sectional decrease of 12% to the dimension 75 x 55 mm.
- the blocks of the comparative alloys D, E and F were extruded directly at the same temperature to the dimension 75 x 55 mm and subjected to no additional cold working.
- the CuCoBe or CuCoNiBe materials were then solution-annealed at 900 to 950 ° C and cured in the temperature range between 450 and 550 ° C for 0.5 to 16 hours.
- the CuNiSi-based alloy was solution-annealed at 800 to 850 ° C and cured under the same conditions. When cured, tensile strength Rm, Vickers hardness HV10, electrical conductivity (as a substitute for thermal conductivity), ASTM E112 grain size, Rm heat resistance at 500 ° C and softening resistance via Vickers hardness measurement (HV10) after aging at 500 ° C determined after a period of 500 hours.
- thermoforming blocks (1) measuring 70 x 50 x 40mm and shaped blocks (2) with tongue and groove measuring 70 x 50 x 47mm the thermal shock behavior was finally tested.
- the mold blocks were first annealed for two hours at 500 ° C and then quenched in water at 20 to 25 ° C.
- the T-slot of the blocks was then examined for cracks with the naked eye and a microscope at 10x magnification.
- Table 2 alloy Rm MPa HV 10 Guide% IACS Grain size ⁇ m Rm (500 ° C) MPa Hardness HV 10 after aging at 500 ° C over 500h Behavior after thermal shock test Block (1)
- Block (2) A 801 254 50 30-90 523 173 crack-free crack-free B 804 245 51.5 45-90 464 175 crack-free crack-free C 812 255 49.5 45 -90 485 167 crack-free crack-free D 652 205 43 45 -90 387 118 crack-free cracked e 786 260 50.5 up to 5000 423 150 cracked cracked cracked F 807 248 48.5 up to 3000 434 152 cracked cracked cracked
- the copper alloy disclosed in claim 1 is therefore eminently suitable as a material for the production of all mold blocks for the side dams of strip casting plants subject to the casting process of a typical alternating temperature stress. These are both the previously used mold blocks and the mold blocks in the design with tongue and groove according to EP 0 974 413 A1 ,
Abstract
Description
Die Erfindung betrifft die Verwendung einer aushärtbaren Kupferlegierung als Werkstoff zur Herstellung von Blöcken für die Seitendämme von Bandgießanlagen.The invention relates to the use of a curable copper alloy as a material for the production of blocks for the side dams of strip casting plants.
Das weltweite Ziel, insbesondere der Stahl- und Kupferindustrie, Halbzeug möglichst endabmessungsnah zu gießen, um Warm- und/oder Kaltverformungsschritte einzusparen, hat schon vor 1970 zu der Entwicklung der sogenannten Hazelett-Bandgießanlagen geführt, bei denen die Metallschmelze im Spalt von zwei parallel geführten Bändern erstarrt. Die Seitendämme bestehen bei der beispielsweise aus der
Weiterhin sind aus der
Von ganz entscheidender Bedeutung ist schließlich ein optimales Ermüdungsverhalten des Werkstoffs, welches sicherstellt, daß nach dem Verlassen der Gießstrecke die beim Rückkühlen der Blöcke auftretenden thermischen Spannungen nicht zum Reißen der Blöcke in den Ecken der für die Aufnahme des Stahlbandes eingearbeiteten T-Nut führt. Besonders hohe thermische Spannungen sind dabei - bedingt durch die ungünstigere Geometrie und Massenverteilung - bei Seitendammblöcken in der Ausführung mit Nut und Feder zu erwarten.Of crucial importance is, finally, an optimal fatigue behavior of the material, which ensures that after leaving the casting line, the thermal stresses occurring during the cooling of the blocks does not lead to tearing of the blocks in the corners of the incorporated for receiving the steel strip T-groove. Particularly high thermal stresses are expected - due to the less favorable geometry and mass distribution - in side dam blocks in the design with tongue and groove.
Treten derartige durch Thermoschock hervorgerufene Risse auf, fällt schon nach kurzer Zeit der betreffende Formblock aus der Seitendammkette der Bandgießmaschine heraus, wobei schmelzflüssiges Metall aus dem Gießformhohlraum unkontrolliert auslaufen und Anlagenteile beschädigen kann. Für das Auswechseln der schadhaften Formblöcke muß die gesamte Bandgießanlage angehalten und der Gießvorgang unterbrochen werden.Occur such caused by thermal shock cracks, falls after a short time of the block in question from the Seitendammkette the strip casting machine out molten metal from the mold cavity leak out uncontrolled and can damage equipment parts. For the replacement of the defective mold blocks, the entire strip caster must be stopped and the casting process must be interrupted.
Zur Überprüfung der Rißneigung hat sich eine Testmethode bewährt, bei der die Formblöcke einer zweistündigen Wärmebehandlung bei 500°C unterzogen und anschließend in Wasser von 20 bis 25°C abgeschreckt werden. Auch bei mehrfacher Wiederholung dieser Thermoschockprüfung dürfen bei einem geeigneten Material keine Risse in der T-Nutfläche auftreten.To test the tendency of cracking, a test method has proven in which the mold blocks are subjected to a heat treatment at 500 ° C for two hours and then quenched in water at 20 to 25 ° C. Even if this thermal shock test is repeated several times, no cracks in the T-slot surface may occur with a suitable material.
In der
Beim Thermoschocktest treten keine Risse auf. Ein Vorteil gegenüber Beryllium-haltigen Kupferbasislegierungen besteht in der Möglichkeit, die Formblöcke manuell trocken nachschleifen zu können, da kein Beryllium im Schleifstaub enthalten ist. Die Nachbearbeitung eingesetzter Seitendammblöcke mit Nut und Feder ist erheblich aufwendiger und erfordert in der Regel eine maschinelle (Naß)-Reinigung der T-Nut und der Gießflächen (z. B. in geschlossenen Kammern), wodurch die Freisetzung von Schleifstäuben unterbunden wird. Ein Einsatz Beryllium-haltiger Legierungen wäre unter diesen Bedingungen somit grundsätzlich möglich.There are no cracks during the thermal shock test. An advantage over beryllium-containing copper-base alloys is the possibility of manually regrinding the mold blocks manually, since no beryllium is contained in the grinding dust. The post-processing of inserted side dam blocks with tongue and groove is considerably more complicated and usually requires a mechanical (wet) cleaning of the T-slot and the casting surfaces (eg in closed chambers), whereby the release of abrasive dust is prevented. A use of beryllium-containing alloys would thus be possible under these conditions.
Ein Seitendammblock aus der in der
Durch die Verwendung gemäß der Ansprüche kann einerseits eine ausreichende Aushärtbarkeit des Werkstoffs zur Erzielung einer hohen Festigkeit, Härte und Leitfähigkeit sichergestellt werden. Andererseits ist nur eine relativ geringe Kaltverformung von 5% bis zu maximal 30% erforderlich, um ein feinkörniges Gefüge mit ausreichender Plastizität einzustellen. Durch den gezielt abgestuften Zirkoniumgehalt werden sowohl die Ermüdungsfestigkeit als auch die Warmfestigkeitseigenschaften verbessert.By the use according to the claims on the one hand sufficient hardenability of the material to achieve high strength, hardness and conductivity can be ensured. On the other hand, only a relatively small cold deformation of 5% to a maximum of 30% is required to set a fine-grained structure with sufficient plasticity. The targeted graded zirconium content improves both the fatigue strength and the heat resistance properties.
Mit der Abfolge der in Anspruch 1 angegebenen Verfahrensstufen gelingt es in darüber hinaus in überraschend einfacher Weise, das von den bekannten CuCoBe-Legierungen beobachtete schlechte Rekristallisationsverhalten bei der Warmformgebung und Lösungsglühbehandlung zu beseitigen. Das schlechte Rekristallisationsverhalten führt bei der Herstellung von Formblöcken aus CuCoBe-Legierungen im warmumgeformten, lösungsgeglühten und ausgehärteten Zustand zu einer für den Verwendungszweck nicht akzeptablen grobkörnigen Gefügestruktur mit Korngrößen bis über 1 mm. Wird der Werkstoff jedoch zwischen der Warmumformung und der Lösungsglühbehandlung einer Kaltverformung von 5% bis zu maximal 30 %, vorzugsweise bis zu maximal 15 %, unterworfen, so führt dieser zusätzliche Verarbeitungsschritt zu einer erheblich feinkörnigeren Gefügestruktur. Entsprechende Untersuchungsreihen haben bestätigt, daß Werkstoffe für Formblöcke für die Seitendämme von Bandgießmaschinen, die unterhalb der Rekristallisationstemperatur kaltverformt und anschließend lösungsgeglüht werden eine deutlich feinere Gefügestruktur mit Korngrößen unterhalb 0,5 mm aufweisen, während höhere Kaltumformgrade oberhalb von etwa 40 % beim nachfolgenden Lösungsglühen zu einer Kornvergröberung durch sekundäre Rekristallisation mit Korngrößen über 1 mm führen.With the sequence of the process steps specified in claim 1, it is also possible in a surprisingly simple manner to eliminate the poor recrystallization behavior observed in the hot forming and solution annealing treatment observed by the known CuCoBe alloys. The poor recrystallization behavior results in the production of blocks of CuCoBe alloys in the hot-formed, solution-annealed and cured state to a non-acceptable for the intended use coarse-grained microstructure with grain sizes up to 1 mm. However, if the material is subjected to cold working of 5% to a maximum of 30%, preferably up to a maximum of 15%, between the hot working and the solution annealing treatment, this additional processing step leads to a considerably finer grain structure. Corresponding series of tests have confirmed that materials for mold blocks for the side ram of strip casters, cold worked below the recrystallization and then solution annealed have a much finer microstructure with grain sizes below 0.5 mm, while higher degrees of cold work above about 40% in the subsequent solution annealing to a Grain coarsening by secondary recrystallization with grain sizes above 1 mm lead.
Anhand von Ausführungsbeispielen wird die Erfindung im folgenden noch näher erläutert. An drei erfindungsgemäßen Beispiel-(Legierungen A, B und C) und drei Vergleichsbeispiel-(Legierungen Vergleichsbeispiel- (D, E und F) werden die Vorteile der Erfindung aufgezeigt. Die Zusammensetzung der Kupferlegierungen in Gewichtsprozenten ist in der nachfolgenden Tabelle 1 angegeben:
Bei der Zusammensetzung der Legierung D handelt es sich um eine bekannte CuNiSi-Basislegierung, während E und F genormte CuCo2Be- bzw. CuCoNiBe-Werkstoffe sind.The composition of alloy D is a known CuNiSi base alloy, while E and F are standardized CuCo2Be and CuCoNiBe materials, respectively.
Sämtliche Kupferlegierungen wurden in einem Induktionstiegelofen erschmolzen und im Stranggießverfahren zu Rundblöcken mit einem Durchmesser von 280 mm vergossen. Die Rundblöcke der Beispiellegierungen A, B und C wurden auf einer Strangpresse bei einer Temperatur oberhalb 900 °C zu Flachstangen der Abmessung 79 x 59 mm stranggepreßt und anschließend mit einer Querschnittsabnahme von 12 % auf die Abmessung 75 x 55 mm gezogen. Die Blöcke der Vergleichslegierungen D, E und F wurden bei gleicher Temperatur direkt auf die Abmessung 75 x 55 mm stranggepreßt und keiner zusätzlichen Kaltumformung unterworfen. Die CuCoBe- bzw. CuCoNiBe-Werkstoffe wurden anschließend bei 900 bis 950 °C lösungsgeglüht und im Temperaturbereich zwischen 450 und 550 °C für 0,5 bis 16 Stunden lang ausgehärtet.All copper alloys were melted in an induction crucible furnace and cast in a continuous casting process into round blocks with a diameter of 280 mm. The round blocks of the example alloys A, B and C were extruded on an extruder at a temperature above 900 ° C to flat bars of dimension 79 x 59 mm and then drawn with a cross-sectional decrease of 12% to the dimension 75 x 55 mm. The blocks of the comparative alloys D, E and F were extruded directly at the same temperature to the dimension 75 x 55 mm and subjected to no additional cold working. The CuCoBe or CuCoNiBe materials were then solution-annealed at 900 to 950 ° C and cured in the temperature range between 450 and 550 ° C for 0.5 to 16 hours.
Die CuNiSi-Basislegierung wurde bei 800 bis 850 °C lösungsgeglüht und unter gleichen Bedingungen ausgehärtet. Im ausgehärteten Zustand wurden die Zugfestigkeit Rm, die Vickershärte HV10, die elektrische Leitfähigkeit (als Ersatzgröße für die Wärmeleitfähigkeit), die Korngröße nach ASTM E112, die Warmfestigkeit Rm bei 500 °C und die Erweichungsbeständigkeit über Vickershärtemessung (HV10) nach Auslagerung bei 500 °C nach einer Dauer von 500 Stunden ermittelt.The CuNiSi-based alloy was solution-annealed at 800 to 850 ° C and cured under the same conditions. When cured, tensile strength Rm, Vickers hardness HV10, electrical conductivity (as a substitute for thermal conductivity), ASTM E112 grain size, Rm heat resistance at 500 ° C and softening resistance via Vickers hardness measurement (HV10) after aging at 500 ° C determined after a period of 500 hours.
An Formblöcken (1) der Abmessung 70 x 50 x 40mm und Formblöcken (2) mit Nut und Feder der Abmessung 70 x 50 x 47mm wurde schließlich das Thermoschockverhalten geprüft. Hierzu wurden die Formblöcke zunächst zwei Stunden bei 500 °C geglüht und dann in Wasser von 20 bis 25 °C abgeschreckt. Die T-Nut der Blöcke wurde dann mit bloßem Auge und mit einem Mikroskop bei 10-facher Vergrößerung auf Risse untersucht.On thermoforming blocks (1) measuring 70 x 50 x 40mm and shaped blocks (2) with tongue and groove measuring 70 x 50 x 47mm, the thermal shock behavior was finally tested. For this purpose, the mold blocks were first annealed for two hours at 500 ° C and then quenched in water at 20 to 25 ° C. The T-slot of the blocks was then examined for cracks with the naked eye and a microscope at 10x magnification.
Sämtliche Untersuchungsergebnisse sind in nachstehenden Tabelle 2 zusammengefaßt.
Die Ausdehnung festgestellter Risse in der T-Nut lag bei den mit als "rissig" klassifizierten Formblöcken bei 2 bis 5 mm, in Einzelfällen betrug die Rißlänge bis zu 10 mm. Der Gegenüberstellung ist zu entnehmen, daß im Vergleich zu den Werkstoffen E und F nur die erfindungsgemäßen Beispiele bei optimalen Eigenschaften ein überraschenderweise gleichmäßiges und feinkörniges Gefüge und die notwendige Resistenz gegen Rißbildung bei Einsatz als Formblock mit Nut und Feder aufweisen. Auch bei Verwendung als üblicher Formblock weisen die erfindungsgemäßen Beispiele eine deutlich bessere Erweichungsbeständigkeit gegenüber der bekannten CuNiSi-Legierung D und eine etwas bessere Erweichungsbeständigkeit gegenüber den Legierungen E und F auf.The extent of observed cracks in the T-slot was 2 to 5 mm in the blocks classified as "cracked", in some cases the crack length was up to 10 mm. The comparison can be seen that compared to the materials E and F, only the examples of the invention with optimum properties have a surprisingly uniform and fine-grained structure and the necessary resistance to cracking when used as a mold block with tongue and groove. Even when used as a conventional molding block, the inventive examples have a significantly better resistance to softening compared to the known CuNiSi alloy D and a slightly better resistance to softening compared to the alloys E and F.
Die in Anspruch 1 offenbarte Kupferlegierung eignet sich daher hervorragend als Werkstoff zur Herstellung von sämtlichen beim Gießvorgang einer typischen wechselnden Temperaturbeanspruchung unterliegenden Formblöcken für die Seitendämme von Bandgießanlagen. Dies sind sowohl die bisher verwendeten Formblöcke als auch die Formblöcke in der Ausführung mit Nut und Feder gemäß
Claims (2)
- Use of a hardenable copper alloy for casting moulds - in particular for side dams for strip-casting installations, in that a hardenable copper alloy in accordance with the following composition:• 1.2 to 2.7% cobalt, wherein up to 80% of the cobalt content can be replaced by nickel• 0.01% to 0.5% zirconium• 0.3 to 0.7% beryllium• optionally 0.005 to 0.2% magnesium and/or iron• optionally up to a maximum of 0.15% of at least one element from the group comprising niobium, tantalum, vanadium, hafnium, chromium, manganese, titanium and cerium• remainder copper including impurities caused by productionis subjected to the method steps• cold forming of the hot-formed cast blank by between 5 and a maximum of 30%• solution annealing of the blank which has been cold formed by 5 to 30% in the temperature range of 850 to 970°C• 0.5 to 16 hours of hardening of the solution annealed blank at 400 to 550°C and in the hardened state has• a tensile strength of at least 650 MPa• Vickers hardness of at least 210 HV• electrical conductivity of at least 40% IACS• hot tensile strength at 500°C of at least 400 MPa• minimum hardness of 160 HV after 500 hours of ageing at 500°C• and a maximum grain size determined according to ASTM E112 of 0.5 mm.
- Use of a copper alloy according to claim 1, which contains 1.8 to 2.4% cobalt, 0.45 to 0.65% beryllium, 0.15 to 0.3% zirconium, up to 0.5% Mg, up to 0.1% iron, remainder copper including impurities caused by production, is subjected to the method steps according to claim 1 with a cold forming of 10 to 15% after the hot forming and has, in the hardened state, a• tensile strength of 700 to 900 MPa• Vickers hardness of 230 to 280 HV• electrical conductivity of 45 to 60% IACS• hot tensile strength at 500°C of at least 450 MPa• minimum hardness of 160 HV after 500 hours of ageing at 500°C• a grain size determined according to ASTM E112 of between 30 and 90 µm.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10206597 | 2002-02-15 | ||
DE10206597A DE10206597A1 (en) | 2002-02-15 | 2002-02-15 | Hardenable copper alloy used as a material for blocks for the sides of strip casting mills contains alloying additions of cobalt, beryllium, zirconium, and magnesium and/or iron |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1340564A2 EP1340564A2 (en) | 2003-09-03 |
EP1340564A3 EP1340564A3 (en) | 2005-04-27 |
EP1340564B1 true EP1340564B1 (en) | 2007-07-18 |
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EP03001084A Expired - Lifetime EP1340564B1 (en) | 2002-02-15 | 2003-01-18 | Use of a hardenable copper alloy |
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US (2) | US20030159763A1 (en) |
EP (1) | EP1340564B1 (en) |
JP (1) | JP4472933B2 (en) |
KR (1) | KR100967864B1 (en) |
CN (1) | CN1271228C (en) |
AT (1) | ATE367229T1 (en) |
BR (1) | BR0300445B1 (en) |
CA (1) | CA2417546C (en) |
DE (2) | DE10206597A1 (en) |
DK (1) | DK1340564T3 (en) |
ES (1) | ES2288572T3 (en) |
MX (1) | MXPA03000218A (en) |
PL (1) | PL198565B1 (en) |
PT (1) | PT1340564E (en) |
RU (1) | RU2301844C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016083023A1 (en) | 2014-11-27 | 2016-06-02 | Sms Group Gmbh | Device for the strip casting of metal products |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
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US20060086437A1 (en) * | 2004-10-22 | 2006-04-27 | Russell Nippert | Method for manufacturing copper alloys |
JP2008151270A (en) * | 2006-12-18 | 2008-07-03 | Kitz Sct:Kk | Metal diaphragm valve |
CN101333609B (en) * | 2007-06-28 | 2011-03-16 | 周水军 | Low copper beryllium mold material for gravitation and low-pressure casting and production process thereof |
DE102008015096A1 (en) * | 2008-03-19 | 2009-09-24 | Kme Germany Ag & Co. Kg | Process for producing molded parts and molded parts produced by the process |
CN101643867B (en) * | 2009-08-28 | 2011-11-23 | 镇江汇通金属成型有限公司 | High performance copper casting alloy and preparation method thereof |
JP2011081764A (en) * | 2009-09-14 | 2011-04-21 | Panasonic Corp | Content receiver, content reproducer, content reproducing system, content writing method, expiration date determining method, program, and recording medium |
DE102016006824A1 (en) * | 2016-06-03 | 2017-12-07 | Wieland-Werke Ag | Copper alloy and its uses |
RU2625193C1 (en) * | 2016-10-10 | 2017-07-12 | Юлия Алексеевна Щепочкина | Copper-based alloy |
KR101810925B1 (en) | 2017-10-18 | 2017-12-20 | 주식회사 풍산 | Copper alloy strips having high heat resistance and thermal dissipation properties |
CN112210692B (en) * | 2020-09-10 | 2021-12-17 | 新余市长城铜产品开发有限公司 | Beryllium bronze long guide rail and manufacturing method thereof |
CN115233032B (en) * | 2022-08-01 | 2023-06-27 | 河南云锦空天特导新材料有限公司 | Copper alloy wire and preparation method and application thereof |
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US3865176A (en) * | 1973-09-28 | 1975-02-11 | Hazelett Strip Casting Corp | Casting method for twin-belt continuous metal casting machines |
US4179314A (en) * | 1978-12-11 | 1979-12-18 | Kawecki Berylco Industries, Inc. | Treatment of beryllium-copper alloy and articles made therefrom |
US4377424A (en) * | 1980-05-26 | 1983-03-22 | Chuetsu Metal Works Co., Ltd. | Mold of precipitation hardenable copper alloy for continuous casting mold |
JPS6260879A (en) * | 1985-09-10 | 1987-03-17 | Ngk Insulators Ltd | Wear resistant copper alloy member |
US4749548A (en) * | 1985-09-13 | 1988-06-07 | Mitsubishi Kinzoku Kabushiki Kaisha | Copper alloy lead material for use in semiconductor device |
EP0271991B1 (en) * | 1986-11-13 | 1991-10-02 | Ngk Insulators, Ltd. | Production of copper-beryllium alloys |
JP2869076B2 (en) * | 1988-12-19 | 1999-03-10 | 中越合金鋳工株式会社 | Precipitation hardening mold material for continuous casting |
DE4142941A1 (en) * | 1991-12-24 | 1993-07-01 | Kabelmetal Ag | USE OF A CURABLE copper alloy |
US6059905A (en) * | 1993-08-26 | 2000-05-09 | Ngk Metals Corporation | Process for treating a copper-beryllium alloy |
EP0854200A1 (en) * | 1996-10-28 | 1998-07-22 | BRUSH WELLMAN Inc. | Copper-beryllium alloy |
DE10156925A1 (en) * | 2001-11-21 | 2003-05-28 | Km Europa Metal Ag | Hardenable copper alloy as a material for the production of casting molds |
-
2002
- 2002-02-15 DE DE10206597A patent/DE10206597A1/en not_active Withdrawn
-
2003
- 2003-01-08 MX MXPA03000218A patent/MXPA03000218A/en active IP Right Grant
- 2003-01-18 DE DE50307676T patent/DE50307676D1/en not_active Expired - Lifetime
- 2003-01-18 EP EP03001084A patent/EP1340564B1/en not_active Expired - Lifetime
- 2003-01-18 DK DK03001084T patent/DK1340564T3/en active
- 2003-01-18 AT AT03001084T patent/ATE367229T1/en active
- 2003-01-18 PT PT03001084T patent/PT1340564E/en unknown
- 2003-01-18 ES ES03001084T patent/ES2288572T3/en not_active Expired - Lifetime
- 2003-01-22 CN CNB031033067A patent/CN1271228C/en not_active Expired - Fee Related
- 2003-01-28 CA CA2417546A patent/CA2417546C/en not_active Expired - Fee Related
- 2003-02-10 US US10/361,660 patent/US20030159763A1/en not_active Abandoned
- 2003-02-11 PL PL358681A patent/PL198565B1/en unknown
- 2003-02-12 JP JP2003033937A patent/JP4472933B2/en not_active Expired - Fee Related
- 2003-02-13 KR KR1020030008977A patent/KR100967864B1/en not_active IP Right Cessation
- 2003-02-13 BR BRPI0300445-7A patent/BR0300445B1/en not_active IP Right Cessation
- 2003-02-14 RU RU2003104534/02A patent/RU2301844C2/en not_active IP Right Cessation
-
2008
- 2008-06-02 US US12/156,604 patent/US20080240974A1/en not_active Abandoned
Non-Patent Citations (1)
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016083023A1 (en) | 2014-11-27 | 2016-06-02 | Sms Group Gmbh | Device for the strip casting of metal products |
DE102014224236A1 (en) | 2014-11-27 | 2016-06-02 | Sms Group Gmbh | Device for strip casting of metallic products |
Also Published As
Publication number | Publication date |
---|---|
US20030159763A1 (en) | 2003-08-28 |
MXPA03000218A (en) | 2004-10-29 |
BR0300445B1 (en) | 2011-07-26 |
EP1340564A3 (en) | 2005-04-27 |
RU2301844C2 (en) | 2007-06-27 |
DK1340564T3 (en) | 2007-11-19 |
PL198565B1 (en) | 2008-06-30 |
PL358681A1 (en) | 2003-08-25 |
DE50307676D1 (en) | 2007-08-30 |
BR0300445A (en) | 2004-08-17 |
CN1271228C (en) | 2006-08-23 |
KR20030069066A (en) | 2003-08-25 |
CA2417546C (en) | 2015-03-31 |
EP1340564A2 (en) | 2003-09-03 |
JP4472933B2 (en) | 2010-06-02 |
US20080240974A1 (en) | 2008-10-02 |
JP2004002967A (en) | 2004-01-08 |
PT1340564E (en) | 2007-09-03 |
ATE367229T1 (en) | 2007-08-15 |
CN1442500A (en) | 2003-09-17 |
KR100967864B1 (en) | 2010-07-05 |
ES2288572T3 (en) | 2008-01-16 |
CA2417546A1 (en) | 2003-08-15 |
DE10206597A1 (en) | 2003-08-28 |
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