EP0702375B1 - Overhead contact wire of high speed electrical railways and process for manufacturing the same - Google Patents

Overhead contact wire of high speed electrical railways and process for manufacturing the same Download PDF

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Publication number
EP0702375B1
EP0702375B1 EP95113311A EP95113311A EP0702375B1 EP 0702375 B1 EP0702375 B1 EP 0702375B1 EP 95113311 A EP95113311 A EP 95113311A EP 95113311 A EP95113311 A EP 95113311A EP 0702375 B1 EP0702375 B1 EP 0702375B1
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Prior art keywords
wire
cold working
alloy
component
cooling
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EP0702375A2 (en
EP0702375A3 (en
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Christian Dr. Kuhrt
Arno Fink
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Siemens AG
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Siemens AG
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/02Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
    • H01B1/026Alloys based on copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper

Definitions

  • the invention relates to a catenary wire of a high-speed electrical railway line with a tensile strength (R m ) of the wire of at least 550 MPa and an electrical conductivity ( ⁇ ) of at least 65%, based on that of annealed pure copper according to the International Annealed Copper Standard (IACS) .
  • the invention further relates to a method for producing such an overhead line wire.
  • Such an overhead line wire and a corresponding manufacturing method can be found in EP 0 569 036 A.
  • the contact wire material is therefore subject to the highest demands with regard to its mechanical tensile strength R m with high electrical conductivity ⁇ at the same time.
  • a CuAg alloy with an Ag content of 0.1% by weight Ag content is currently used for the contact wire of the Re250 control overhead line from Deutsche Bahn AG with a grooved profile and 120 mm 2 diameter.
  • This alloy has a tensile strength R m of about 350 MPa (N / mm 2 ) with a conductivity ⁇ of about 95%, based on that of annealed pure Cu according to IACS (International Annealed Copper Standard).
  • the contact wire is designed for regular operation at speeds of up to 250 km / h. Taking into account an unavoidable wear, it is prestressed at 125 MPa, ie with about 36% of its tensile strength ⁇ or a safety margin against breakage of about 2.8 (cf.
  • Such a high minimum tensile strength can e.g. with from the mentioned copper alloys can be achieved.
  • the selected composition of the alloy requires that one of the melted components obtained casting strand after hot rolling to an output wire either by immersion in a water or oil bath must be cooled very quickly or after a slower one Air cooling then an additional heat treatment (Solution annealing) with rapid cooling got to.
  • the preform obtained in this way then undergoes several cold deformations subjected to being interrupted by excretion annealing are. Because of the generally necessary rapid cooling of the preliminary product from the solution temperature (860 - 1000 ° C) the known method is relatively expensive and therefore not very suitable for commercial wire production.
  • An electrical wire is also made from US Pat. No. 4,755,235 a precipitation hardened Cu alloy with Cr (0.05 to 1.5 wt%), Zr (0.05 to 0.5 wt%) and Mg (0.005 to 0.1% by weight).
  • an alloy melt is said be cooled rapidly (within 1 to 2 minutes from about 1200 ° C to room temperature).
  • the object of the present invention is to provide a catenary wire made of a material which on the one hand meets the minimum requirements mentioned with regard to the mechanical tensile strength R m and the electrical conductivity K and which on the other hand enables the wire to be produced in a simplified manner compared to the known methods.
  • the catenary wire consists of an at least 5-component, hardenable Cu a Cr b Zr c Mg d X e alloy, where X is an element from the group of elements Al, P, S, Fe, Ni , Zn, Ag, Cd, In, Sn, Sb and Bi and should apply to the components (each in percent by weight): 0.2 ⁇ b ⁇ 0.8, 0.02 ⁇ c ⁇ 0.4, 0.01 ⁇ d ⁇ 0.2, 0.01 ⁇ e ⁇ 0.4, With a + b + c + d + e ⁇ 100 including unavoidable pollution elements.
  • the invention is based on the knowledge that with the Choice of the Mg component in combination with the proportions mentioned the other components advantageous to a special one Treatment of the wire intermediate in the form of rapid cooling waived from the melting or solution temperature can be.
  • a melted from the alloy according to the invention then normal in the usual way, e.g. from 1200 ° C to room temperature in 5 to 10 min, cooled and optionally still pre-deformed, for example, by hot rolling Starting product or wire intermediate product therefore only needs to be cold worked and outsourced to using a wire to get the desired properties.
  • the materials to be selected for the X component (5th component) advantageously increase the yield strength of the Cu alloy and improve the formability of the wire intermediate. These properties are particularly important when the production of the wire only a single cold forming to be provided.
  • the wire according to the invention has a Si-free Cu alloy. Because by avoiding it of an Si portion can be an undesirable reduction exclude the electrical conductivity ⁇ (cf. e.g. the book “Materials in Electrical Engineering", Page 172).
  • the manufacturing method according to the invention is characterized in that that a wire intermediate is first created, whereby the Cu alloy melted and then opposed a rapid cooling cooled comparatively more slowly is then the wire intermediate by means of at least one Cold working is converted into a wire intermediate, then the intermediate wire product of at least one age heat treatment is subjected and if necessary the Cold forming and / or aging steps can be repeated at least once, with the last cold deformation the final shape of the wire is generated.
  • the intermediate wire product can be produced directly from the melt of the Cu alloy. But it is also possible an initial product formed from the slowly solidified melt by means of at least one pre-deformation in the To transfer wire intermediate.
  • the melt with a comparatively lower cooling rate especially with at most 20 ° C / s in the important temperature range from Melting temperature to about 700 ° C, are cooled. Below of 700 ° C the cooling rate can be significantly lower and for example at 5 ° C / s. Let such cooling rates realize themselves without much effort, so that the invention
  • the method is correspondingly simple to carry out is.
  • the aging heat treatment is in itself known manner at elevated temperature and above such Period carried out that the hardening of the Precipitation of the material required with the cold forming trained dislocation structures.
  • the material from the individual components preferably in a protective gas atmosphere such as melted under Ar.
  • a protective gas atmosphere such as melted under Ar.
  • Oxygen content in the melt should be as possible be low and preferably below 100 ppm.
  • the melt is then with a Cooling rate or rate (in ° C / min) cooled, the in the for the formation of the precipitation hardened material important temperature range between the melting temperature and about 700 ° C well below that for a quick Cooling characteristic cooling rates of at least about 100 ° C / s.
  • Such cooling rates can be achieved, for example, by a simple one Pour into a water-cooled mold under air or in a protective gas atmosphere. On a scare So in a water or oil bath can be beneficial to be dispensed with.
  • the direct pouring of the melt into one Pre-wire with e.g. 20 to 30 mm diameter by pulling the melt through a water-cooled, horizontally stored Chill mold is particularly suitable here.
  • the one, if necessary, cast into blocks or bars Melting mass can then be remelted to get out of it a wire preliminary product more suitable with regard to the wire shape to accomplish.
  • the cooled melt mass can by hot rolling to a wire intermediate as one Process pre-wire. Hot rolling can also be done in one continuous step, a so-called casting roll, immediately connect to the melting of the Cu alloy.
  • the pre-wire cross-section should be set this way be that in the subsequent at least a cold forming a cross-sectional reduction of 50 to 99%, preferably from 60 to 95%, is done so as to achieve the desired one Obtain the final cross-section of the catenary wire.
  • the pre-wire (or the pre-wire) is then undergo a first cold working.
  • Such cold deformation can e.g. by pressing or rolling or hammering, especially by pulling.
  • the degree of deformation is generally between 20 and 80%, preferably between 40 and 70%.
  • the first cold-forming step is then followed by a first one Age heat treatment of the wire intermediate which is advantageous at a temperature between 350 ° C and 600 ° C, preferably between 450 ° C and 500 ° C, performed becomes.
  • This heat treatment will harden the material due to excretions on those with cold forming generated dislocation structures achieved.
  • the duration this heat treatment is generally between 10 minutes and 10 hours. Large batches are significant Heating and cooling times must be taken into account.
  • the processing steps of cold forming and / or hardening by heat treatment are advantageously repeated, advantageously completed with a cold working the desired end product of the catenary wire in the to get hard drawn condition. If this last cold working should be done in just one step, then should not exceed the cross-sectional reduction to be chosen here 20% to 22%. Of course, everyone can Cold forming, in particular also the last cold forming, Assemble from several cold forming steps.
  • An at least 5-component Cu alloy of the composition Cu a Cr b Zr c Mg d X e is provided for the catenary wire to be produced in this way.
  • This proportion ⁇ of impurity elements is generally less than 100 ppm per impurity element.
  • the following table shows the tensile strength R m , the microhardness HV, the conductivity ⁇ and the elongation at break ⁇ B for some wires made of Cu alloys according to the invention in comparison to the known CuAg0.1 alloy for different processing states.
  • the microhardness HV 50 was determined on cross sections perpendicular to the longitudinal direction of the wire.
  • the electrical conductivity ⁇ was measured with 0.2 to 1 A alternating current in lock-in technology at 370 Hz using a four-point method.
  • the conductivity values determined apply to a temperature of 20 ° C.
  • the specified properties are the same for corresponding catenary wires.
  • the 5-component alloy according to the invention represents only a basic alloy for a catenary wire for high speed electric railways to which if necessary, at least one other element proportionate to one small proportion of less than 0.1 wt .-% added can be.
  • additional elements are particularly selected from the elements provided for the X component.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)
  • Contacts (AREA)
  • Manufacturing Of Electric Cables (AREA)
  • Electric Cable Installation (AREA)
  • Organic Insulating Materials (AREA)
  • Manufacture Of Switches (AREA)

Abstract

The conductor wire is made of a Cu alloy of formula CuaCrbZrcMgdXe (I), where X is one from Al, P, S, Fe, Ni, Zn, Ag, Cd, In, Sn, Sb and Bi. b is 0.2-0.8, c is 0.02-0.04, d is 0.01-0.2 and e is 0.01-0.4. a + b + c + d + e = 100.

Description

Die Erfindung bezieht sich auf einen Oberleitungsdraht einer elektrischen Hochgeschwindigkeitsbahnstrecke mit einer Zugfestigkeit (Rm) des Drahtes von mindestens 550 MPa und einer elektrischen Leitfähigkeit (κ) von mindestens 65 %, bezogen auf die von geglühtem reinen Kupfer gemäß International Annealed Copper Standard (IACS). Die Erfindung betrifft ferner ein Verfahren zur Herstellung eines solchen Oberleitungsdrahtes.Ein derartiger Oberleitungsdraht und ein entsprechendes Herstellungsverfahren gehen aus der EP 0 569 036 A hervor.The invention relates to a catenary wire of a high-speed electrical railway line with a tensile strength (R m ) of the wire of at least 550 MPa and an electrical conductivity (κ) of at least 65%, based on that of annealed pure copper according to the International Annealed Copper Standard (IACS) . The invention further relates to a method for producing such an overhead line wire. Such an overhead line wire and a corresponding manufacturing method can be found in EP 0 569 036 A.

Auf Hochgeschwindigkeitsbahnstrecken ist für eine sichere Energiezufuhr über ein Oberleitungssystem eine hohe mechanische Vorspannung des Fahrdrahtes eine unverzichtbare Voraussetzung. An den Fahrdrahtwerkstoff werden somit höchste Anforderungen bezüglich seiner mechanischen Zugfestigkeit Rm bei gleichzeitig hoher elektrischer Leitfähigkeit κ gestellt.On high-speed rail lines, high mechanical pretensioning of the contact wire is an indispensable prerequisite for the safe supply of energy via an overhead line system. The contact wire material is therefore subject to the highest demands with regard to its mechanical tensile strength R m with high electrical conductivity κ at the same time.

Gegenwärtig wird für den Fahrdraht der Regeloberleitung Re250 der Deutschen Bahn AG mit Rillenprofil und 120 mm2 Durchmesser eine CuAg-Legierung mit einem Ag-Anteil von 0,1 Gew.-% Ag-Anteil verwendet. Diese Legierung weist eine Zugfestigkeit Rm von etwa 350 MPa(N/mm2) auf bei einer Leitfähigkeit κ von etwa 95 %, bezogen auf die von geglühtem reinen Cu gemäß IACS (International Annealed Copper Standard). Der Fahrdraht ist für einen Regelbetrieb mit Fahrgeschwindigkeiten von höchstens 250 km/h ausgelegt. Er ist unter Berücksichtigung einer unvermeidbaren Abnutzung mit 125 MPa vorgespannt, d.h. mit etwa 36 % seiner Zugfestigkeit κ bzw. einer Sicherheitsmarge gegen Bruch von etwa 2,8 (vgl. "Elektrische Bahnen", 80. Jg., 1982, H. 4, Seiten 119 bis 125 oder "Eisenbahntechnische Rundschau", Bd. 35, H. 9, Sept. 1986, Seiten 593 bis 599). Diese Vorspannung wurde für eine Hochgeschwindigkeitsfahrt mit über 400 km/h kurzfristig auf 175 MPa erhöht ("Elektrische Bahnen", 86. Jg., 1988, H. 9, Seiten 268 bis 289).A CuAg alloy with an Ag content of 0.1% by weight Ag content is currently used for the contact wire of the Re250 control overhead line from Deutsche Bahn AG with a grooved profile and 120 mm 2 diameter. This alloy has a tensile strength R m of about 350 MPa (N / mm 2 ) with a conductivity κ of about 95%, based on that of annealed pure Cu according to IACS (International Annealed Copper Standard). The contact wire is designed for regular operation at speeds of up to 250 km / h. Taking into account an unavoidable wear, it is prestressed at 125 MPa, ie with about 36% of its tensile strength κ or a safety margin against breakage of about 2.8 (cf. "Electrical Railways", 80th year, 1982, p. 4, Pages 119 to 125 or "Eisenbahntechnische Rundschau", vol. 35, H. 9, Sept. 1986, pages 593 to 599). This pretension was briefly increased to 175 MPa for a high-speed drive at over 400 km / h ("Electric Railways", 86th vol., 1988, No. 9, pages 268 to 289).

Zur Auslegung der Oberleitung für einen Regelbetrieb mit Hochgeschwindigkeiten von über 300 km/h wird eine Fahrdrahtvorspannung von bis zu 200 MPa gefordert. Dies bedingt unter Zugrundelegung der vorgenannten Sicherheitsmarge eine Fahrdraht legierung mit einer Mindestzugfestigkeit κ von etwa 550 MPa. Die Zugfestigkeit wird dabei durch Zugversuche nach DIN 50145/46 bestimmt (vgl. das Buch "Werkstoffe in der Elektrotechnik" von H. Fischer, 3. Auflage, G. Hanser Verlag München Wien, 1987, Seiten 113 bis 121).To design the overhead line for regular operation with High speed of over 300 km / h becomes a contact wire pretension of up to 200 MPa. This requires under On the basis of the aforementioned safety margin a contact wire alloy with a minimum tensile strength κ of approx 550 MPa. The tensile strength is determined by tensile tests DIN 50145/46 determines (cf. the book "Materials in electrical engineering" by H. Fischer, 3rd edition, G. Hanser Verlag Munich Vienna, 1987, pages 113 to 121).

Eine derart hohe Mindestzugfestigkeit kann z.B. mit aus der genannten EP-A zu entnehmenden Cu-Legierungen erreicht werden. Gemäß einem speziellen Ausführungsbeispiel setzt sich eine dieser Legierungen aus den Komponenten Cr (0,1 bis 1 %), Zr (0,01 bis 0,3 %), Mg (0,001 bis 0,05 %), O (maximal 10 ppm) und Cu (Rest) unter Einschluß unvermeidbarer Verunreinigungen zusammen. Die gewählte Zusammensetzung der Legierung bedingt dabei, daß ein aus den erschmolzenen Komponenten gewonnener Gießstrang nach einem Warmwalzen zu einem Ausgangsdraht entweder durch Eintauchen in ein Wasser- oder Ölbad sehr rasch abgekühlt werden muß oder nach einer langsameren Luftabkühlung anschließend einer zusätzlichen Wärmebehandlung (Lösungsglühung) mit Raschabkühlung unterzogen werden muß. Der so gewonnene Vorkörper wird dann mehreren Kaltverformungen unterzogen, die von Ausscheidungsglühungen unterbrochen sind. Wegen der generell notwendigen raschen Abkühlung des Vorprodukts von der Lösungstemperatur (860 - 1000°C) ist das bekannte Verfahren verhältnismäßig aufwendig und deshalb für eine kommerzielle Drahtfertigung wenig geeignet. Such a high minimum tensile strength can e.g. with from the mentioned copper alloys can be achieved. According to a special embodiment, sits down one of these alloys from the components Cr (0.1 to 1%), Zr (0.01 to 0.3%), Mg (0.001 to 0.05%), O (maximum 10 ppm) and Cu (rest) including unavoidable impurities together. The selected composition of the alloy requires that one of the melted components obtained casting strand after hot rolling to an output wire either by immersion in a water or oil bath must be cooled very quickly or after a slower one Air cooling then an additional heat treatment (Solution annealing) with rapid cooling got to. The preform obtained in this way then undergoes several cold deformations subjected to being interrupted by excretion annealing are. Because of the generally necessary rapid cooling of the preliminary product from the solution temperature (860 - 1000 ° C) the known method is relatively expensive and therefore not very suitable for commercial wire production.

Aus der US-PS 4,755,235 ist ferner ein elektrischer Draht aus einer ausscheidungsgehärteten Cu-Legierung mit Cr (0,05 bis 1,5 Gew.-%), Zr (0,05 bis 0,5 Gew.-%) und Mg (0,005 bis 0,1 Gew.-%) zu entnehmen. Auch hier soll eine Legierungsschmelze rasch abgekühlt werden (innerhalb 1 bis 2 Minuten von etwa 1200°C auf Raumtemperatur).An electrical wire is also made from US Pat. No. 4,755,235 a precipitation hardened Cu alloy with Cr (0.05 to 1.5 wt%), Zr (0.05 to 0.5 wt%) and Mg (0.005 to 0.1% by weight). Here too an alloy melt is said be cooled rapidly (within 1 to 2 minutes from about 1200 ° C to room temperature).

Aufgabe der vorliegenden Erfindung ist es, einen Oberleitungsdraht aus einem Material anzugeben, das einerseits die genannten Mindestanforderungen bezüglich der mechanischen Zugfestigkeit Rm und der elektrischen Leitfähigkeit K erfüllt und das andererseits eine gegenüber den bekannten Verfahren vereinfachte Herstellung des Drahtes ermöglicht.The object of the present invention is to provide a catenary wire made of a material which on the one hand meets the minimum requirements mentioned with regard to the mechanical tensile strength R m and the electrical conductivity K and which on the other hand enables the wire to be produced in a simplified manner compared to the known methods.

Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß der Oberleitungsdraht aus einer wenigstens 5-komponentigen, aushärtbaren CuaCrbZrcMgdXe-Legierung besteht, wobei X ein Element aus der Gruppe der Elemente Al, P, S, Fe, Ni, Zn, Ag, Cd, In, Sn, Sb und Bi ist und für die Komponenten gelten soll (jeweils in Gewichtsprozent): 0,2 ≤ b ≤ 0,8, 0,02 ≤ c ≤ 0,4, 0,01 ≤ d ≤ 0,2, 0,01 ≤ e ≤ 0,4, mit a + b + c + d + e ≅ 100 unter Einschluß unvermeidbarer Verunreinigungselemente.This object is achieved in that the catenary wire consists of an at least 5-component, hardenable Cu a Cr b Zr c Mg d X e alloy, where X is an element from the group of elements Al, P, S, Fe, Ni , Zn, Ag, Cd, In, Sn, Sb and Bi and should apply to the components (each in percent by weight): 0.2 ≤ b ≤ 0.8, 0.02 ≤ c ≤ 0.4, 0.01 ≤ d ≤ 0.2, 0.01 ≤ e ≤ 0.4, With a + b + c + d + e ≅ 100 including unavoidable pollution elements.

Die Erfindung geht dabei von der Erkennntnis aus, daß mit der Wahl der Mg-Komponente in Kombination mit den genannten Anteilen der übrigen Komponenten vorteilhaft auf eine besondere Behandlung des Draht-Vorproduktes in Form einer raschen Abkühlung von der Schmelz- bzw. Lösungstemperatur verzichtet werden kann. Ein aus der erfindungsgemäßen Legierung erschmolzenes, dann in üblicher Weise normal, z.B. von 1200°C auf Raumtemperatur in 5 bis 10 min, abgekühltes und gegebenenfalls noch beispielsweise durch Warmwalzen vorverformtes Ausgangsprodukt bzw. Drahtvorprodukt braucht also nur noch kaltverformt und ausgelagert zu werden, um einen Draht mit den gewünschten Eigenschaften zu erhalten. Es wurde erkannt, daß die für die X-Komponente (5. Komponente) zu wählenden Materialien vorteilhaft die Streckgrenze der Cu-Legierung erhöhen und die Umformbarkeit des Drahtvorproduktes verbessern. Diese Eigenschaften sind insbesondere von Bedeutung, wenn bei der Herstellung des Drahtes nur ein einmaliges Kaltverformen vorgesehen werden soll.The invention is based on the knowledge that with the Choice of the Mg component in combination with the proportions mentioned the other components advantageous to a special one Treatment of the wire intermediate in the form of rapid cooling waived from the melting or solution temperature can be. A melted from the alloy according to the invention, then normal in the usual way, e.g. from 1200 ° C to room temperature in 5 to 10 min, cooled and optionally still pre-deformed, for example, by hot rolling Starting product or wire intermediate product therefore only needs to be cold worked and outsourced to using a wire to get the desired properties. It was recognized that the materials to be selected for the X component (5th component) advantageously increase the yield strength of the Cu alloy and improve the formability of the wire intermediate. These properties are particularly important when the production of the wire only a single cold forming to be provided.

Besonders vorteilhaft wird als X-Komponente Al oder In gewählt. Die entsprechende Cu-Legierung zeichnet sich durch verhältnismäßig hohe Zugfestigkeitswerte Rm und verhältnismäßig hohe Werte der 0,01 %-Dehnungsgrenze (= technische Elastizitätsgrenze) aus.Al or In is particularly advantageously selected as the X component. The corresponding Cu alloy is characterized by relatively high tensile strength values R m and relatively high values of the 0.01% elongation limit (= technical elastic limit).

Außerdem ist es vorteilhaft, wenn der erfindungsgemäße Draht eine Si-freie Cu-Legierung aufweist. Denn durch die Vermeidung eines Si-Anteils läßt sich so eine unerwünschte Verminderung der elektrischen Leitfähigkeit κ ausschließen (vgl. z.B. das genannte Buch "Werkstoffe in der Elektrotechnik", Seite 172).It is also advantageous if the wire according to the invention has a Si-free Cu alloy. Because by avoiding it of an Si portion can be an undesirable reduction exclude the electrical conductivity κ (cf. e.g. the book "Materials in Electrical Engineering", Page 172).

Das erfindungsgemäße Herstellungsverfahren ist dadurch gekennzeichnet, daß zunächst ein Drahtvorprodukt erstellt wird, wobei die Cu-Legierung erschmolzen und anschließend gegenüber einer Raschabkühlung vergleichsweise langsamer abgekühlt wird, darauf das Drahtvorprodukt mittels mindestens einer Kaltverformung in ein Drahtzwischenprodukt überführt wird, dann das Drahtzwischenprodukt mindestens einer Auslagerungswärmebehandlung unterzogen wird und gegebenenfalls die Schritte der Kaltverformung und/oder der Auslagerungsbehandlung mindestens noch einmal wiederholt werden, wobei mit der letzten Kaltverformung die Endform des Drahtes erzeugt wird. Dabei kann das Drahtvorprodukt unmittelbar aus der Schmelze der Cu-Legierung gegossen werden. Es ist aber auch möglich, ein aus der langsam erstarrten Schmelze ausgebildetes Ausgangsprodukt mittels mindestens einer Vorverformung in das Drahtvorprodukt zu überführen. Da die für eine Raschabkühlung charakteristischen Abkühlraten bei etwa 100°C/s und höher liegen, soll bei dem erfindungsgemäßen Verfahren die Schmelze mit vergleichsweise kleinerer Abkühlrate, insbesondere mit höchstens 20°C/s in dem wichtigen Temperaturbereich von der Schmelztemperatur auf etwa 700°C, abgekühlt werden. Unterhalb von 700°C kann die Abkühlrate noch deutlich geringer sein und beispielsweise bei 5°C/s liegen. Solche Abkühlraten lassen sich ohne größeren Aufwand realisieren, so daß das erfindungsgemäße Verfahren vorteilhaft entsprechend einfach durchzuführen ist. Die Auslagerungswärmebehandlung wird in an sich bekannter Weise bei erhöhter Temperatur und über einen solchen Zeitraum durchgeführt, daß sich die für eine Härtung des Materials erforderlichen Ausscheidungen an den mit der Kaltverformung erzeugten Versetzungsstrukturen ausbilden.The manufacturing method according to the invention is characterized in that that a wire intermediate is first created, whereby the Cu alloy melted and then opposed a rapid cooling cooled comparatively more slowly is then the wire intermediate by means of at least one Cold working is converted into a wire intermediate, then the intermediate wire product of at least one age heat treatment is subjected and if necessary the Cold forming and / or aging steps can be repeated at least once, with the last cold deformation the final shape of the wire is generated. The intermediate wire product can be produced directly from the melt of the Cu alloy. But it is also possible an initial product formed from the slowly solidified melt by means of at least one pre-deformation in the To transfer wire intermediate. Because for rapid cooling characteristic cooling rates at about 100 ° C / s and higher should lie in the process of the invention, the melt with a comparatively lower cooling rate, especially with at most 20 ° C / s in the important temperature range from Melting temperature to about 700 ° C, are cooled. Below of 700 ° C the cooling rate can be significantly lower and for example at 5 ° C / s. Let such cooling rates realize themselves without much effort, so that the invention Advantageously, the method is correspondingly simple to carry out is. The aging heat treatment is in itself known manner at elevated temperature and above such Period carried out that the hardening of the Precipitation of the material required with the cold forming trained dislocation structures.

Vorteilhafte Weiterbildungen des Oberleitungsdrahtes und des Verfahrens zu seiner Herstellung gehen aus den jeweils abhängigen Ansprüchen hervor.Advantageous further developments of the catenary wire and Processes for its manufacture go from the respective dependent ones Claims.

Die Erfindung wird nachfolgend anhand von Ausführungsbeispielen noch weiter erläutert.The invention is described below using exemplary embodiments explained further.

Zur Herstellung eines Oberleitungsdrahtes aus einer Cu-Legierung mit der erfindungsgemäßen Zusammensetzung wird zunächst das Material aus den einzelnen Komponenten vorzugsweise in einer Schutzgasatmosphäre wie z.B. unter Ar erschmolzen. Der Sauerstoffgehalt in der Schmelze sollte nämlich möglichst niedrig sein und vorzugsweise unter 100 ppm liegen. Um eine gute Homogenität der Schmelze zu gewährleisten, muß über den Schmelzpunkt von Cu (1084°C), insbesondere auf mindestens 1200°C erhitzt werden. Gegebenenfalls kommen noch höhere Temperaturen in Frage. Deswegen wird vorteilhaft ein Induktionsschmelzen vorgesehen. Die Schmelze wird dann mit einer Abkühlgeschwindigkeit bzw. -rate (in °C/min) abgekühlt, die in dem für die Ausbildung des ausscheidungsgehärteten Materials wichtigen Temperaturbereich zwischen der Schmelztemperatur und etwa 700°C deutlich unterhalb der für eine rasche Abkühlung charakteristischen Abkühlraten von mindestens etwa 100°C/s liegt. So kommen insbesondere Abkühlraten von höchstens 20°C/s in dem genannten Temperaturbereich in Frage. Solche Abkühlraten lassen sich beispielsweise durch ein einfaches Abgießen in eine wassergekühlte Kokille unter Luft oder in einer Schutzgasatmosphäre realisieren. Auf ein Abschrecken in einem Wasser- oder Ölbad kann also vorteilhaft verzichtet werden. Das direkte Abgießen der Schmelze zu einem Vordraht mit z.B. 20 bis 30 mm Durchmesser mittels Abziehens der Schmelze durch eine wassergekühlte, horizontal gelagerte Kokille ist hier besonders geeignet.For the production of a catenary wire from a Cu alloy with the composition according to the invention the material from the individual components preferably in a protective gas atmosphere such as melted under Ar. Of the Oxygen content in the melt should be as possible be low and preferably below 100 ppm. To one To ensure good homogeneity of the melt, must over the Melting point of Cu (1084 ° C), especially at least 1200 ° C to be heated. If necessary, even higher temperatures come in question. This is why induction melting is advantageous intended. The melt is then with a Cooling rate or rate (in ° C / min) cooled, the in the for the formation of the precipitation hardened material important temperature range between the melting temperature and about 700 ° C well below that for a quick Cooling characteristic cooling rates of at least about 100 ° C / s. In particular, cooling rates of at most come 20 ° C / s in the temperature range mentioned in question. Such cooling rates can be achieved, for example, by a simple one Pour into a water-cooled mold under air or in a protective gas atmosphere. On a scare So in a water or oil bath can be beneficial to be dispensed with. The direct pouring of the melt into one Pre-wire with e.g. 20 to 30 mm diameter by pulling the melt through a water-cooled, horizontally stored Chill mold is particularly suitable here.

Die gegebenenfalls zu Blöcken oder Barren abgegossene Schmelzmasse kann dann noch umgeschmolzen werden, um daraus ein hinsichtlich der Drahtform geeigneteres Drahtvorprodukt zu schaffen. Darüber hinaus läßt sich die abgekühlte Schmelzmasse durch ein Warmwalzen zu einem Drahtvorprodukt als ein Vordraht verarbeiten. Das Warmwalzen kann sich auch in einem kontinuierlichen Schritt, einem sogenannten Gießwalzen, unmittelbar an das Erschmelzen der Cu-Legierung anschließen. Ferner ist auch ein Umschmelzen der abgekühlten Schmelzmasse zu einem Barren möglich, der z.B. durch Strangpressen zu einem Vordraht verarbeitet wird. Aus einem entsprechenden Barren können auch stiftartige Körper herausgearbeitet werden, die dann z.B. durch Rundhämmern zu einem Vordraht verformt werden. Der Vordrahtquerschnitt sollte dabei so eingestellt werden, daß bei der sich anschließenden mindestens einen Kaltverformung eine Querschnittsreduktion von 50 bis 99 %, vorzugsweise von 60 bis 95 %, erfolgt, um so den gewünschten Endquerschnitt des Oberleitungsdrahtes zu erhalten. The one, if necessary, cast into blocks or bars Melting mass can then be remelted to get out of it a wire preliminary product more suitable with regard to the wire shape to accomplish. In addition, the cooled melt mass can by hot rolling to a wire intermediate as one Process pre-wire. Hot rolling can also be done in one continuous step, a so-called casting roll, immediately connect to the melting of the Cu alloy. Furthermore, there is also a remelting of the cooled melt mass into an ingot possible, e.g. by extrusion a pre-wire is processed. From a corresponding one Ingots can also be worked out in pencil-like bodies, which then e.g. deformed into a pre-wire by round hammering will. The pre-wire cross-section should be set this way be that in the subsequent at least a cold forming a cross-sectional reduction of 50 to 99%, preferably from 60 to 95%, is done so as to achieve the desired one Obtain the final cross-section of the catenary wire.

Das Drahtvorprodukt (bzw. der Vordraht) wird anschließend einer ersten Kaltverformung unterzogen. Eine solche Kaltverformung kann z.B. durch Pressen oder Walzen oder Hämmern, insbesondere durch Ziehen, vorgenommen werden. Der Verformungsgrad liegt dabei im allgemeinen zwischen 20 und 80 %, vorzugsweise zwischen 40 und 70 %. Beispielsweise werden drei Ziehschritte mit einer Querschnittsreduktion von 38 % bis 34 % (1. Schritt) bzw. von 34 % bis 30 % (2. Schritt) bzw. von 26 % bis 24 % (3. Schritt) gewählt. Mit dieser Kaltverformung werden in dem so zu erhaltenden Drahtzwischenprodukt in bekannter Weise Versetzungsstrukturen erzeugt, die Voraussetzung für eine hinreichende Härtung des Materials sind.The pre-wire (or the pre-wire) is then undergo a first cold working. Such cold deformation can e.g. by pressing or rolling or hammering, especially by pulling. The degree of deformation is generally between 20 and 80%, preferably between 40 and 70%. For example, three Drawing steps with a cross section reduction from 38% to 34% (1st step) or from 34% to 30% (2nd step) or from 26% to 24% (3rd step) selected. With this cold deformation in the wire intermediate product to be obtained in this way Generated dislocation structures in a known manner, the prerequisite for sufficient hardening of the material.

Dem ersten Kaltverformungsschritt schließt sich dann eine erste Auslagerungswärmebehandlung des Drahtzwischenproduktes an, die vorteilhaft bei einer Temperatur zwischen 350°C und 600°C, vorzugsweise zwischen 450°C und 500°C, durchgeführt wird. Mit dieser Wärmebehandlung wird eine Härtung des Materials aufgrund von Ausscheidungen an den mit der Kaltverformung erzeugten Versetzungsstrukturen erreicht. Die Dauer dieser Wärmebehandlung liegt im allgemeinen zwischen 10 Minuten und 10 Stunden. Bei großen Chargen sind dabei erhebliche Aufheiz- und Abkühlzeiten zu berücksichtigen.The first cold-forming step is then followed by a first one Age heat treatment of the wire intermediate which is advantageous at a temperature between 350 ° C and 600 ° C, preferably between 450 ° C and 500 ° C, performed becomes. This heat treatment will harden the material due to excretions on those with cold forming generated dislocation structures achieved. The duration this heat treatment is generally between 10 minutes and 10 hours. Large batches are significant Heating and cooling times must be taken into account.

Die Verarbeitungsschritte der Kaltverformung und/oder Härtung durch Wärmebehandlung werden zweckmäßigerweise wiederholt, wobei vorteilhaft mit einer Kaltverformung abgeschlossen wird, um das gewünschte Endprodukt des Oberleitungsdrahtes im hartgezogenen Zustand zu erhalten. Wenn diese letzte Kaltverformung in nur einem Schritt vorgenommen werden soll, dann sollte die hier zu wählende Querschnittsreduktion nicht über 20 % bis 22 % betragen. Selbstverständlich kann sich aber jede Kaltverformung, also insbesondere auch die letzte Kaltverformung, aus mehreren Kaltverformungsschritten zusammensetzen. The processing steps of cold forming and / or hardening by heat treatment are advantageously repeated, advantageously completed with a cold working the desired end product of the catenary wire in the to get hard drawn condition. If this last cold working should be done in just one step, then should not exceed the cross-sectional reduction to be chosen here 20% to 22%. Of course, everyone can Cold forming, in particular also the last cold forming, Assemble from several cold forming steps.

Hinsichtlich einer möglichst einfachen Herstellung des Oberleitungsdrahtes kann man gegebenenfalls auch eine nur einstufige Kaltverformung vorsehen. Der Verformungsgrad liegt hier natürlich höher.With regard to making the catenary wire as simple as possible if necessary, you can also use a one-step only Provide cold working. The degree of deformation is higher here, of course.

Für den so herzustellenden Oberleitungsdraht wird eine mindestens 5-komponentige Cu-Legierung der Zusammensetzung CuaCrbZrcMgdXe vorgesehen. Um eine Mindestfestigkeit Rm von 550 MPa und eine elektrische Leitfähigkeit κ von mindestens 65 % IACS gewährleisten zu können, werden für die einzelnen Komponenten erfindungsgemäß folgende Anteile (jeweils in Gew.-%) gewählt: 0,2 ≤ b ≤ 0,8, 0,02 ≤ c ≤ 0,4, 0,01 ≤ d ≤ 0,2, 0,01 ≤ e ≤ 0,4 und a + b + c + d + e = 100 - δ, wobei δ durch den Einschluß unvermeidbarer Verunreinigungselemente in der Legierung bestimmt ist. Dieser Anteil δ an Verunreinigungselementen liegt im allgemeinen unter 100 ppm pro Verunreinigungselement.An at least 5-component Cu alloy of the composition Cu a Cr b Zr c Mg d X e is provided for the catenary wire to be produced in this way. In order to be able to guarantee a minimum strength R m of 550 MPa and an electrical conductivity κ of at least 65% IACS, the following proportions (each in% by weight) are selected for the individual components: 0.2 ≤ b ≤ 0.8, 0.02 ≤ c ≤ 0.4, 0.01 ≤ d ≤ 0.2, 0.01 ≤ e ≤ 0.4 and a + b + c + d + e = 100 - δ, where δ is determined by the inclusion of inevitable impurity elements in the alloy. This proportion δ of impurity elements is generally less than 100 ppm per impurity element.

Im Hinblick auf die geforderten Materialeigenschaften und die verhältnismäßig einfache Verarbeitungsmöglichkeit zu einem Oberleitungsdraht ist es als besonders vorteilhaft anzusehen, wenn der Anteil d der Mg-Komponente mindestens 0,05 Gew.-% beträgt. Offenbar hält dann der Mg-Zusatz auch die beiden anderen Komponenten Cr und Zr während der verhältnismäßig langsamen Abkühlungsphase der Schmelze in Lösung. Zugleich wird vorteilhaft ein Anteil b der Cr-Komponente gewählt, der mindestens 0,3 Gew.-% beträgt und vorteilhaft unter 0,6 Gew.-% liegt. Ferner sollte der Anteil c der Zr-Komponente mindestens 0,15 Gew.-% betragen. Darüber hinaus soll die Cu-Legierung des erfindungsgemäßen Oberleitungsdrahtes zumindest eines der Elemente aus der Gruppe Al, P, S, Fe, Ni, Zn, Ag, Cd, In, Sn, Sb und Bi mit einem Anteil zwischen 0,01 und 0,4 Gew.-% enthalten. Diese Elemente, die im wesentlichen auch nach der Wärmebehandlung im Cu gelöst bleiben, sind insbesondere unter den folgenden zwei Gesichtspunkten von Vorteil:

  • 1) Das Material besitzt gegenüber der nur 4-komponentigen CuCrZrMg-Legierung eine verbesserte Kaltumformbarkeit.
  • 2) Der Kaltverfestigungsgrad während der abschließenden Kaltumformung ist vergleichsweise höher, so daß eine gegenüber der 4-komponentigen Legierung erhöhte Elastizitätsgrenze erreicht wird. Diese Vorteile kommen insbesondere bei einer nur einstufigen Kaltverformung zum Tragen.
  • In view of the required material properties and the relatively simple processing possibility to form an overhead line wire, it is to be regarded as particularly advantageous if the proportion d of the Mg component is at least 0.05% by weight. The Mg addition then apparently also keeps the two other components Cr and Zr in solution during the relatively slow cooling phase of the melt. At the same time, a proportion b of the Cr component is advantageously selected which is at least 0.3% by weight and is advantageously less than 0.6% by weight. Furthermore, the proportion c of the Zr component should be at least 0.15% by weight. In addition, the Cu alloy of the catenary wire according to the invention is said to contain at least one of the elements from the group Al, P, S, Fe, Ni, Zn, Ag, Cd, In, Sn, Sb and Bi in a proportion between 0.01 and 0, 4 wt .-% included. These elements, which remain essentially dissolved in the Cu even after the heat treatment, are particularly advantageous from the following two points of view:
  • 1) The material has improved cold formability compared to the only 4-component CuCrZrMg alloy.
  • 2) The degree of work hardening during the final cold forming is comparatively higher, so that a higher elastic limit than the 4-component alloy is reached. These advantages come into play particularly in the case of only one-step cold forming.
  • Die genannten Anteile der einzelnen Komponenten gewährleisten eine gute Aushärtbarkeit und somit Zugfestigkeit der Legierung bei einer hinreichenden Leitfähigkeit und einer genügenden Bruchdehnung des Materials.Ensure the stated proportions of the individual components good hardenability and thus tensile strength of the alloy with sufficient conductivity and sufficient Elongation at break of the material.

    Die nachfolgende Tabelle zeigt die Zugfestigkeit Rm, die Mikrohärte HV, die Leitfähigkeit κ und die Bruchdehnung εB für einige Drähte aus erfindungsgemäßen Cu-Legierungen im Vergleich zu der bekannten CuAg0.1-Legierung für verschiedene Verarbeitungszustände. Zur mechanischen Charakterisierung wurden standardmäßig die Zugfestigkeit Rm, die sogenannte 0,01 %-Dehngrenze (= technische Elastizitätsgrenze) Rp0,01 und die Bruchdehnung εB ≅ A100 bei Raumtemperatur bestimmt. Dies geschah in Zerreißversuchen an 100 mm langen Drahtstücken mit meist 1 mm  bei einer Dehngeschwindigkeit von 1 mm/min entsprechend 1,7 x 10-4 s-1. An Querschliffen senkrecht zur Draht längsrichtung wurde die Mikrohärte HV50 bestimmt. Die elektrische Leitfähigkeit κ wurde mit 0,2 bis 1 A Wechselstrom in Lock-in-Technik bei 370 Hz mit Hilfe einer Vierpunktmethode gemessen. Die ermittelten Leitfähigkeitswerte gelten für eine Temperatur von 20°C. Die angegebenen Eigenschaften sind bei entsprechenden Oberleitungsdrähten dieselben.

    Figure 00100001
    The following table shows the tensile strength R m , the microhardness HV, the conductivity κ and the elongation at break ε B for some wires made of Cu alloys according to the invention in comparison to the known CuAg0.1 alloy for different processing states. For mechanical characterization, the tensile strength R m , the so-called 0.01% proof stress (= technical elastic limit) R p0.01 and the elongation at break ε B ≅ A 100 at room temperature were determined as standard. This was done in tensile tests on 100 mm long pieces of wire with mostly 1 mm  at a stretching speed of 1 mm / min corresponding to 1.7 x 10 -4 s -1 . The microhardness HV 50 was determined on cross sections perpendicular to the longitudinal direction of the wire. The electrical conductivity κ was measured with 0.2 to 1 A alternating current in lock-in technology at 370 Hz using a four-point method. The conductivity values determined apply to a temperature of 20 ° C. The specified properties are the same for corresponding catenary wires.
    Figure 00100001

    Zur Herstellung der in der Tabelle aufgeführten Legierungen wurde von hochreinen Elementen (99,99 %) der Komponenten ausgegangen. Mit den Elementen wurden in einer Ar-Schutzgasatmosphäre zylindrische Reguli (ca. 60 g) in einem MgO-Tiegel induktiv erschmolzen und anschließend in einem Lichtbogenofen zu Barren (Länge ca. 10 bis 15 cm) umgeschmolzen. Aus den Barren wurden funkenerosiv und durch Drehen Stifte mit kreisförmigem Querschnitt (typisch 3 mm Durchmesser ) herausgeschnitten, wobei der beim Schmelzen gebildete Schlackesack entfernt wurde. Die Stifte wurden zunächst auf ca. 2 mm  rundgehämmert und anschließend auf ca. 1,5 mm  gezogen. Die Kaltumformung wurde mit kleinen Stichabnahmen von 0,1 bis 0,05 mm durchgeführt. Eine relative Querschnittsreduktion beim Kaltziehen von ca. 75 %, entsprechend einer Längung von l/l0 = 44, d.h. einem Umformungsgrad ϕ = ln (l/l0)von 1,39, konnte bei allen untersuchten Legierungen aufgrund eines hohen Kaltverformungsvermögens ohne Materialfehler erzielt werden. Die Wärmebehandlungen wurden in einem Quarzrohr unter Ar-Atmosphäre durchgeführt. Nach Auslagerungsglühungen (450 bis 500°C) wurde das Material im Quarzrohr außerhalb des Ofens relativ langsam abgekühlt.High-purity elements (99.99%) of the components were used to manufacture the alloys listed in the table. Cylindrical reguli (approx. 60 g) were inductively melted with the elements in an Ar protective gas atmosphere in a MgO crucible and then remelted into bars (length approx. 10 to 15 cm) in an arc furnace. Pins with a circular cross-section (typically 3 mm in diameter ) were cut out of the ingots by spark erosion and by turning, the slag bag formed during the melting being removed. The pins were first hammered to about 2 mm  and then pulled to about 1.5 mm . The cold forming was carried out with small passes from 0.1 to 0.05 mm. A relative reduction in cross-section during cold drawing of approx. 75%, corresponding to an elongation of l / l 0 = 44, ie a degree of deformation ϕ = ln (l / l 0 ) of 1.39, could be achieved in all alloys investigated due to their high cold-forming capacity without material defects be achieved. The heat treatments were carried out in a quartz tube under an Ar atmosphere. After aging annealing (450 to 500 ° C) the material in the quartz tube was cooled relatively slowly outside the furnace.

    Abweichend von den in der Tabelle aufgeführten Cu-Legierungen sind insbesondere auch mit den folgenden erfindungsgemäßen Legierungen die genannten Zugfestigkeits- und Leitfähigkeitsbedingungen zu erfüllen (Angaben jeweils in Gew.-%): CuCr 0,3 Zr 0,2 Mg 0,1 In 0,1 CuCr 0,3 Zr 0,1 Mg 0,1 Al 0,05 CuCr 0,3 Zr 0,05 Mg 0,05 In 0,15 CuCr 0,3 Zr 0,2 Mg 0,05 Al 0,085 CuCr 0,55 Zr 0,2 Mg 0,2 Sn 0,05 CuCr 0,55 Zr 0,1 Mg 0,1 Zn 0,15 CuCr 0,55 Zr 0,05 Mg 0,05 Ni 0,2 CuCr 0,55 Zr 0,05 Mg 0,2 Cd 0,05 CuCr 0,5 Zr 0,18 Mg 0,06 Ag 0,15 CuCr 0,6 Zr 0,15 Mg 0,05 Bi 0,15 CuCr 0,3 Zr 0,1 Mg 0,05 Fe 0,03 CuCr 0,4 Zr 0,1 Mg 0,08 P 0,04 CuCr 0,3 Zr 0,05 Mg 0,1 S 0,05 CuCr 0,5 Zr 0,18 Mg 0,05 Sb 0,1 Deviating from the Cu alloys listed in the table, the specified tensile strength and conductivity conditions must also be met with the following alloys according to the invention (details in% by weight): CuCr 0.3 Zr 0.2 Mg 0.1 In 0.1 CuCr 0.3 Zr 0.1 Mg 0.1 Al 0.05 CuCr 0.3 Zr 0.05 Mg 0.05 In 0.15 CuCr 0.3 Zr 0.2 Mg 0.05 Al 0.085 CuCr 0.55 Zr 0.2 Mg 0.2 Sn 0.05 CuCr 0.55 Zr 0.1 Mg 0.1 Zn 0.15 CuCr 0.55 Zr 0.05 Mg 0.05 Ni 0.2 CuCr 0.55 Zr 0.05 Mg 0.2 CD 0.05 CuCr 0.5 Zr 0.18 Mg 0.06 Ag 0.15 CuCr 0.6 Zr 0.15 Mg 0.05 Bi 0.15 CuCr 0.3 Zr 0.1 Mg 0.05 Fe 0.03 CuCr 0.4 Zr 0.1 Mg 0.08 P 0.04 CuCr 0.3 Zr 0.05 Mg 0.1 S 0.05 CuCr 0.5 Zr 0.18 Mg 0.05 Sb 0.1

    Die erfindungsgemäße 5-komponentige Legierung stellt selbstverständlich nur eine Basislegierung für einen Oberleitungsdraht für elektrische Hochgeschwindigkeitsbahnen dar, zu der gegebenenfalls mindestens ein weiteres Element zu einem verhältnismäßig geringen Anteil von unter 0,1 Gew.-% hinzulegiert sein kann. Solche Zusatzelemente werden insbesondere aus den für die X-Komponente vorgesehenen Elementen ausgewählt.The 5-component alloy according to the invention, of course, represents only a basic alloy for a catenary wire for high speed electric railways to which if necessary, at least one other element proportionate to one small proportion of less than 0.1 wt .-% added can be. Such additional elements are particularly selected from the elements provided for the X component.

    Claims (24)

    1. Overhead conductor wire for a high speed electric railway line having a tensile strength (Rm ) of 550 MPa and an electrical conductivity (K) relative to that of annealed pure Cu (International Annealed Copper Standard) of at least 65%, consisting of an at least 5-component age-hardenable Cu alloy of the composition CuaCrbZrcMgdXe, wherein X is an element selected from the group of elements Al, P, S, Fe, Ni, Zn, Ag, Cd, In, Sn, Sb, and Bi, with the proviso that for the components (in each case in weight percent) : 0.2 ≤ b ≤ 0.8, 0.02 ≤ c ≤ 0.4, 0.01 ≤ d ≤ 0.2, 0.01 ≤ e ≤ 0.4, with
      a + b + c + d + e ≅ 100, including unavoidable impurity elements.
    2. Wire according to claim 1, characterised in that for the Xe component: 0.02 ≤ e ≤ 0.2.
    3. Wire according to claim 1 or claim 2, characterised in that for the Mgd component: d ≥ 0.05% by wt.
    4. Wire according to any one of claims 1 to 3, characterised in that for the Zrc component: c ≤ 0.2% by wt.
    5. Wire according to any one of claims 1 to 4, characterised in that for the Crb component: 0.3% by wt. ≤ b ≤ 0.6% by wt.
    6. Wire according to any one of claims 1 to 5, characterised in that at least one further element from the group of the X elements is included in the Cu alloy in an amount less than 0.1% by wt.
    7. Wire according to any one of claims 1 to 6, characterised in that the Cu alloy is practically free from Si.
    8. Wire according to any one of claims 1 to 6, characterised in that the Cu alloy contains as a further component Si in an amount of at most 0.1% by wt.
    9. Method for manufacturing the overhead conductor wire according to any one of claims 1 to 8, characterised by the following steps:
      a) a wire bar is made by first melting the Cu alloy and then cooling relatively slowly compared with a rapid cooling,
      b) the wire bar is then converted into an intermediate wire product by means of at least one cold working,
      c) the intermediate wire product is then subjected to at least one ageing heat treatment,
      d) if desired the steps b) and/or c) are repeated at least once more,
      the final form of the wire being produced by the last cold working.
    10. Method according to claim 9, characterised in that the wire bar is formed by first making a starting product from the elements of the Cu alloy by means of melting and subsequent cooling and then converting the starting product into the wire bar by at least one preforming.
    11. Method according to claim 10, characterised in that the at least one preforming is undertaken at elevated temperature.
    12. Method according to claim 10 or claim 11, characterised in that the at least one preforming is undertaken by means of pressing and/or rolling and/or swaging.
    13. Method according to any one of claims 10 to 12, characterised in that by means of the at least one preforming of the starting product a wire bar is formed the section of which makes a reduction in area by at least one subsequent cold working of 50 to 99%, preferably of 60 to 95%, necessary in order to obtain the desired final section of the wire.
    14. Method according to claim 9, characterised in that the wire bar is cast from the Cu alloy melt.
    15. Method according to any one of claims 9 to 14, characterised in that a cooling of the melt in step a) takes place in the temperature range between the melting temperature and 700°C at a cooling rate of less than 100°C/s, preferably of at most 20°C/s.
    16. Method according to any one of claims 9 to 15, characterised in that the melting in step a) is undertaken at a temperature of at least 1200°C.
    17. Method according to any one of claims 9 to 16, characterised in that at least two cold workings are performed, with a relatively small reduction in area taking place in the last cold working.
    18. Method according to claim 17, characterised in that by the first cold working a reduction in area between 60 and 80% and by the last cold working a reduction in area between 10 and 30% is brought about.
    19. Method according to any one of claims 9 to 18, characterised in that by the last cold working the end product of the wire is obtained.
    20. Method according to any one of claims 9 to 16, characterised in that by a single cold working of the wire bar the final form of the wire is produced.
    21. Method according to any one of claims 9 to 20, characterised in that at least one cold working comprises several working steps.
    22. Method according to claim 21, characterised in that the last cold working comprises several working steps.
    23. Method according to any one of claims 9 to 22, characterised in that the at least one cold working is effected by means of pressing and/or rolling and/or swaging and/or drawing
    24. Method according to any one of claims 9 to 23, characterised in that the at least one ageing heat treatment takes place at a temperature between 350°C and 600°C.
    EP95113311A 1994-09-15 1995-08-23 Overhead contact wire of high speed electrical railways and process for manufacturing the same Revoked EP0702375B1 (en)

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    DE4321921A1 (en) * 1993-07-01 1995-01-12 Abb Patent Gmbh Overhead wire (contact wire) and a method for its production

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    Publication number Publication date
    DE59504054D1 (en) 1998-12-03
    EP0702375A2 (en) 1996-03-20
    EP0702375A3 (en) 1996-09-11
    ATE172814T1 (en) 1998-11-15
    DE19530673A1 (en) 1996-03-21
    ES2123883T3 (en) 1999-01-16

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