EP1264906A1 - Use of spray compacted copper-nickel-manganese alloy - Google Patents

Use of spray compacted copper-nickel-manganese alloy Download PDF

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Publication number
EP1264906A1
EP1264906A1 EP01109660A EP01109660A EP1264906A1 EP 1264906 A1 EP1264906 A1 EP 1264906A1 EP 01109660 A EP01109660 A EP 01109660A EP 01109660 A EP01109660 A EP 01109660A EP 1264906 A1 EP1264906 A1 EP 1264906A1
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EP
European Patent Office
Prior art keywords
spray
nickel
manganese
copper
compacted copper
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.)
Granted
Application number
EP01109660A
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German (de)
French (fr)
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EP1264906B1 (en
Inventor
Andreas Dr. Bögel
Klaus Dr. Ohla
Hilmar R. Dr. Müller
Frank Michael Keppeler
John Dr. Hendrik
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Wieland Werke AG
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Wieland Werke AG
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Publication date
Application filed by Wieland Werke AG filed Critical Wieland Werke AG
Priority to DE50106520T priority Critical patent/DE50106520D1/en
Priority to AT01109660T priority patent/ATE298007T1/en
Priority to EP01109660A priority patent/EP1264906B1/en
Priority to NO20021709A priority patent/NO20021709L/en
Priority to CA002381911A priority patent/CA2381911C/en
Priority to US10/125,291 priority patent/US6866818B2/en
Publication of EP1264906A1 publication Critical patent/EP1264906A1/en
Application granted granted Critical
Publication of EP1264906B1 publication Critical patent/EP1264906B1/en
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/05Alloys based on copper with manganese as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent

Abstract

A method for the manufacture of tools and components for the offshore field and the mining industry, in particular, for drilling installations, using a spray formed Cu-Ni-Mn alloy of 10 to 25% Ni, 10 to 25% Mn, the remainder being copper and common impurities. Due to the favorable characteristics of the combination, the alloy is suitable as a replacement material for Be-containing copper materials.

Description

Die Erfindung betrifft die Verwendung einer sprühkompaktierten Kupfer-Nickel-Mangan-Legierung als Werkstoff zur Herstellung von Werkzeugen und Komponenten für den Offshore-Bereich und den Bergbau, insbes. für Bohranlagen.The invention relates to the use of a spray-compacted copper-nickel-manganese alloy as a material for the manufacture of tools and components for offshore and mining, especially for drilling rigs.

In der Offshore-Technik werden für hohe Beanspruchungen mechanische Komponenten (wie etwa Bohrgestänge, Verschraubungen, Bolzen, etc.) verlangt, die u. a. hohe Belastbarkeit aufweisen und sehr gute Korrosionseigenschaften haben müssen sowie weder ferromagnetisch sein dürfen noch beim Aufeinanderprallen durch pyrophore Reaktionen wegspritzender Splitter Explosionen oder Feuer auslösen dürfen.
Für die in diesem Einsatzgebiet verwendeten Werkstoffe werden folgende, spezifische Eigenschaften gefordert. Hierzu zählen:

  • 1. Magnetische Eigenschaften: Um meßtechnische Anforderungen des Bohrstrangs im Bereich von Kompaßmeßsystemen zu erfüllen (Messung des Erdmagnetfelds und der daraus ableitbaren Richtungsinformation) müssen Bohrstrangkomponenten in diesem Bereich unmagnetisch sein, da in Anwesenheit von magnetischen Werkstoffen Fehlmessungen durch Beeinflussung des Magnetfeldes erfolgen. Die magnetische Suszeptibilität χ sollte dementsprechend 20.10-6 nicht überschreiten. (Dabei gibt χ nach der GI. M = µo . χ . H das Verhältnis der Magnetisierung M [ Vs / m 2] zur magnetischen Feldstärke H [ A / m] an, mit µo = 4 π . 10-7 = 1,256 . 10-6 [ Vs / Am] als magnetischer Feldkonstante.)
  • 2. Streckgrenze/Härte: Der Bohrstrang unterliegt hohen mechanischen und physikaiisch/chemischen Beanspruchungen. Die einzelnen Strangelemente werden durch Gewindeverbindungen miteinander verbunden. Wegen der hohen Kräfte, die im Bohrloch auftreten, werden die einzelnen Strangelemente unter Aufbringung hoher Drehmomente miteinander verschraubt. Um plastische Verformungen der Gewinde zu vermeiden, muß der Werkstoff eine hohe Streckgrenze haben.Die Bohrstrangoberflächen werden durch Abrasion und Erosion beansprucht. Der Verschleiß wird durch eine möglichst hohe Materialhärte auf ein Minimum reduziert.
  • 3. Zähigkeit: Die genauen Belastungskollektive sind in der Regel unbekannt. Untersuchungen an aufgetretenen Schäden haben jedoch gezeigt, daß sehr hohe schwingende aber auch schlagartige Belastungen auftreten können. Die Zähigkeit der eingesetzten Werkstoffe spielt daher für das sichere Funktionieren eine entscheidende Rolle. Die Zähigkeit der eingesetzten Kupferlegierung sollte deshalb für ein Festigkeitsniveau maximiert und möglichst gleichmäßig über den Querschnitt sein.
  • 4. Korrosionsbeständigkeit: Auf der Sohle des Bohrlochs werden die Felsformationen mechanisch zertrümmert und mit einer sogenannten Bohrspülung an die Oberfläche gepumpt. Erhöhte Temperatur und der chemische bzw. physikalisch-chemische Angriff durch die Spülflüssigkeit erfordern eine hohe Korrosionsbeständigkeit der verwendeten Werkstoffe. Insbesondere muß der Werkstoff in schwefelhaltigen Medien resistent gegen Spannungsrißkorrosion sein.
  • 5. Freßverhalten: Die Verschraubung der einzelnen Bohrstrangelemente unter hohem Drehmoment darf zu keiner Kaltverschweißung ("Fressen") führen. Daher sollten möglichst artfremde Materialien (z. B. Stahl mit NE-Metall) miteinander verbunden werden.Bei Gewindeverbindungen von Bohrstrangkomponenten aus austenitischen, nichtmagnetisierbaren Stählen werden deshalb oftmals Zwischenstücke aus einer hochfesten Kupferlegierung dazwischengeschraubt. Als geeigneter Kupferwerkstoff wurde bisher beispielsweise Kupfer-Beryllium (UNS C 17200) eingesetzt.
  • In offshore technology, mechanical components (such as drill rods, screw connections, bolts, etc.) are required for high loads, which, among other things, have a high load capacity and must have very good corrosion properties and must not be ferromagnetic or explosions when they collide due to pyrophoric reactions of splinters spraying away or may start a fire.
    The following specific properties are required for the materials used in this application. Which includes:
  • 1. Magnetic properties: In order to meet the measurement requirements of the drill string in the area of compass measurement systems (measurement of the earth's magnetic field and the directional information derived from it), drill string components in this area must be non-magnetic, since in the presence of magnetic materials, incorrect measurements are made due to the influence of the magnetic field. Accordingly, the magnetic susceptibility χ should not exceed 20.10 -6 . (Here gibt according to the GI. M = µ o . χ. H the ratio of magnetization M [ V s / m 2 ] to the magnetic field strength H [ A / m ], with µ o = 4 π. 10 -7 = 1.256. 10 -6 [ V s / Am ] as magnetic field constant.)
  • 2. Yield strength / hardness: The drill string is subject to high mechanical and physical / chemical stresses. The individual strand elements are connected to one another by threaded connections. Because of the high forces that occur in the borehole, the individual string elements are screwed together with high torques. In order to avoid plastic deformation of the threads, the material must have a high yield strength. The surface of the drill string is stressed by abrasion and erosion. Wear is reduced to a minimum by the highest possible material hardness.
  • 3. Toughness: The exact load collectives are generally unknown. However, studies of damage that has occurred have shown that very high vibrating but also sudden loads can occur. The toughness of the materials used therefore plays a decisive role in the safe functioning. The toughness of the copper alloy used should therefore be maximized for a strength level and be as uniform as possible over the cross section.
  • 4. Corrosion resistance: The rock formations are mechanically broken up on the bottom of the borehole and pumped to the surface with a so-called drilling fluid. Increased temperature and the chemical or physico-chemical attack by the rinsing liquid require the materials used to be highly resistant to corrosion. In particular, the material must be resistant to stress corrosion cracking in media containing sulfur.
  • 5. Eating behavior: The screwing of the individual drill string elements under high torque must not lead to cold welding ("seizure"). For this reason, materials of a different type (e.g. steel with non-ferrous metal) should be connected to one another. In the case of threaded connections of drill string components made of austenitic, non-magnetizable steels, intermediate pieces made of a high-strength copper alloy are often screwed in between. For example, copper beryllium (UNS C 17200) has been used as a suitable copper material.
  • Für diese Anforderungen werden nach dem Stand der Technik Komponenten und Werkzeuge aus Kupferwerkstoffen, insbes. aus Cu-Be-Legierungen eingesetzt, die diese Eigenschaften in besonderer Weise auf sich vereinen. Als Beispiel gelten hierfür die Kupfer-Beryllium-Zwischenstücke, die bei austenitischen, nichtmagnetisierbaren Schwerstangen (sog. "drill collars") verwendet werden.According to the state of the art, components and Tools made of copper materials, especially made of Cu-Be alloys, which combine these properties in a special way. As an example the copper-beryllium intermediate pieces, which are used for austenitic, non-magnetizable Drill collars can be used.

    Nachdem nun das Umweltbewußtsein in der Bevölkerung immer stärker wird, rücken Gesichtspunkte der Umweltverträglichkeit und Gesundheitsgefährdung zunehmend auch in das Zentrum des Interesses von Anlagenausrüstern für die Offshore-Technik. Jegliche Kritikpunkte gilt es zu vermeiden. Now that environmental awareness in the population is increasing, consider aspects of environmental compatibility and health risks increasingly also in the center of interest of equipment suppliers for the Offshore technology. Any criticism should be avoided.

    Wegen möglicher gesundheitsgefährdender Wirkungen von Be-Stäuben und -Dämpfen, die bei unsachgemäßer Bearbeitung Be-haltiger Werkstoffe auftreten können, werden daher zunehmend Forderungen nach Be-freien Werkstoffen gestellt.Because of the possible health effects of dust and -Vapors that occur when materials containing materials are improperly processed can, there are therefore increasing demands for free materials posed.

    Der Erfindung liegt daher die Aufgabe zugrunde, einen Kupferwerkstoff zu finden, der das geforderte Eigenschaftsprofil ebenfalls möglichst weitgehend erfüllt, dabei aber Be-frei ist.The object of the invention is therefore to find a copper material, which also fulfills the required property profile as far as possible but is free.

    Die Aufgabe wird erfindungsgemäß durch die Verwendung einer sprühkompaktierten Kupfer-Nickel-Mangan-Legierung gelöst, die aus 10 bis 25 % Nickel, 10 bis 25 % Mangan, Rest Kupfer und üblichen Verunreinigungen, besteht (die Prozentangabe bezieht sich auf das Gewicht).The object is achieved by using a spray-compacted Copper-nickel-manganese alloy dissolved, which consists of 10 to 25% nickel, 10 to There is 25% manganese, the rest copper and usual impurities (the percentage refers to the weight).

    Es hat sich nun überraschend herausgestellt, daß mit Cu-Ni-Mn-Legierungen der vorgeschlagenen Be-freien Zusammensetzung nicht nur alle Anforderungen erfüllt werden können, sondern auch beträchtliche Vorteile in der Verfügbarkeit gegenüber den gebräuchlichen Cu-Be-Legierungen erzielt werden und durch die Herstellung mittels Sprühkompaktierens auch eine selektiv bessere technologische Eignung gefunden wird, insbes. werden die Anforderungen an Bohrstrangkomponenten gemäß API (American Petroleum Institute)-Specification 7 ("Specification for Rotary Drill Stem Elements") 38. Ed., April 1, 1994, erfüllt.It has now surprisingly been found that with Cu-Ni-Mn alloys proposed loading-free composition not only meets all requirements but also have significant advantages in terms of availability the usual Cu-Be alloys can be achieved and by the production by means of spray compacting also a selectively better technological suitability is found, in particular the requirements for drill string components according to API (American Petroleum Institute) Specification 7 ("Specification for Rotary Drill Stem Elements ") 38th Ed., April 1, 1994.

    Es sind zwar Kupfer-Nickel-Mangan-Legierungen als solche bereits bekannt (vgl. beispielsweise US-PS 2.234.552/DEAN) und es ist beispielsweise auch im Bereich der elektrischen und elektronischen Bauteile bekannt, die relativ teuren Cu-Be-Legierungen durch preiswertere Kupfer-Nickel-Mangan-Legierungen zu ersetzen, der beanspruchte Verwendungszweck für eine sprühkompaktierte Legierung dieser Art ist allerdings nicht vorbekannt. Copper-nickel-manganese alloys are already known as such (cf. for example US-PS 2.234.552 / DEAN) and it is for example also in the area of the electrical and electronic components known, the relatively expensive Cu-Be alloys to be replaced by cheaper copper-nickel-manganese alloys, the claimed use for a spray-compacted alloy Art is not known, however.

    Der Urformprozeß für den Kupferwerkstoff erfolgt durch Sprühkompaktieren (vgl. den sog. "OSPREY"-Prozeß beispielsweise nach den GB-PSen 1.379.261/1.599.392 oder EPS 0.225.732). Als Vorform bieten sich Bolzen an, die durch typische Warmformverfahren (Pressen, Walzen, Schmieden) zu Halbzeugfabrikaten (Stangen, Rohren, Profilen, Buchsen) verarbeitet werden.The primary molding process for the copper material is carried out by spray compacting (cf. the so-called "OSPREY" process, for example according to GB-PS 1,379,261 / 1,599,392 or EPS 0.225.732). As a preform, there are bolts that pass through typical thermoforming processes (pressing, rolling, forging) into semi-finished products (Rods, tubes, profiles, bushings) can be processed.

    Bevorzugte Ausführungsformen der Erfindung ergeben sich nach den Ansprüchen 2 bis 6.Preferred embodiments of the invention result from the claims 2 to 6.

    Claims (6)

    Verwendung einer sprühkompaktierten Kupfer-Nickel-Mangan-Legierung, bestehend aus 10 bis 25 % Nickel, 10 bis 25 % Mangan, Rest Kupfer und üblichen Verunreinigungen, als Werkstoff zur Herstellung von Werkzeugen und Komponenten für den Offshore-Bereich und den Bergbau, insbes. für Bohranlagen.Use of a spray-compacted copper-nickel-manganese alloy, consisting of 10 to 25% nickel, 10 to 25% manganese, the rest copper and usual impurities, as a material for the production of tools and components for offshore and mining, especially for Drilling rigs. Verwendung einer sprühkompaktierten Kupfer-Legierung nach Anspruch 1, die 17 bis 23 % Nickel und 17 bis 23 % Mangan enthält, für den Zweck nach Anspruch 1.Use of a spray-compacted copper alloy according to claim 1, containing 17 to 23% nickel and 17 to 23% manganese for the purpose Claim 1. Verwendung einer sprühkompaktierten Kupfer-Legierung nach Anspruch 1 oder 2, die 19,5 bis 20,5 % Nickel und 19,5 bis 20,5 % Mangan enthält, für den Zweck nach Anspruch 1.Use of a spray-compacted copper alloy according to claim 1 or 2, which contains 19.5 to 20.5% nickel and 19.5 to 20.5% manganese for the purpose of claim 1. Verwendung einer sprühkompaktierten Kupfer-Legierung nach einem der Ansprüche 1 bis 3, bei der eine homogene und seigerungsarme Verteilung aller Legierungselemente vorliegt, für den Zweck nach Anspruch 1.Use of a spray-compacted copper alloy according to one of the Claims 1 to 3, in which a homogeneous and low-segregation distribution all alloying elements are present for the purpose of claim 1. Verwendung einer sprühkompaktierten Kupfer-Legierung nach Anspruch 4, die eine mittlere Korngröße DK = 50 bis 70 µm aufweist, für den Zweck nach Anspruch 1. Use of a spray-compacted copper alloy according to claim 4, which has an average grain size D K = 50 to 70 µm, for the purpose according to claim 1. Verwendung einer sprühkompaktierten Kupfer-Legierung nach einem der Ansprüche 1 bis 5 als Werkstoff, der die Anforderungen gemäß API (American Petroleum Institute)-Specification 7 ("Specification for Rotary Drill Stem Elements") 38. Ed., April 1, 1994, erfüllt, für den Zweck nach Anspruch 1.Use of a spray-compacted copper alloy according to one of the Claims 1 to 5 as a material that meets the requirements according to API (American Petroleum Institute) Specification 7 ("Specification for Rotary Drill Stem Elements ") 38th Ed., April 1, 1994, for the purpose of claim 1.
    EP01109660A 2001-04-19 2001-04-19 Use of spray compacted copper-nickel-manganese alloy Expired - Lifetime EP1264906B1 (en)

    Priority Applications (6)

    Application Number Priority Date Filing Date Title
    DE50106520T DE50106520D1 (en) 2001-04-19 2001-04-19 Use of a spray-compacted copper-nickel-manganese alloy
    AT01109660T ATE298007T1 (en) 2001-04-19 2001-04-19 USE OF A SPRAY COMPACTED COPPER-NICKEL-MANGANESE ALLOY
    EP01109660A EP1264906B1 (en) 2001-04-19 2001-04-19 Use of spray compacted copper-nickel-manganese alloy
    NO20021709A NO20021709L (en) 2001-04-19 2002-04-11 Use of a spray-compacted copper-nickel-manganese alloy
    CA002381911A CA2381911C (en) 2001-04-19 2002-04-17 A method of using a spray formed copper-nickel-manganese alloy
    US10/125,291 US6866818B2 (en) 2001-04-19 2002-04-18 Method of using a spray formed copper-nickel-manganese alloy

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    Application Number Priority Date Filing Date Title
    EP01109660A EP1264906B1 (en) 2001-04-19 2001-04-19 Use of spray compacted copper-nickel-manganese alloy

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    EP1264906A1 true EP1264906A1 (en) 2002-12-11
    EP1264906B1 EP1264906B1 (en) 2005-06-15

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    US (1) US6866818B2 (en)
    EP (1) EP1264906B1 (en)
    AT (1) ATE298007T1 (en)
    CA (1) CA2381911C (en)
    DE (1) DE50106520D1 (en)
    NO (1) NO20021709L (en)

    Cited By (1)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    WO2014202221A1 (en) 2013-06-19 2014-12-24 Isabellenhütte Heusler Gmbh & Co. Kg Resistor alloy, component produced therefrom and production method therefor

    Families Citing this family (2)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    CN105648267A (en) * 2016-03-30 2016-06-08 广东合科泰实业有限公司 Low-temperature-coefficient resistor body, preparation method of low-temperature-coefficient resistor body and low-temperature-coefficient resistor with low-temperature-coefficient resistor body
    CN109338202A (en) * 2018-11-23 2019-02-15 中国科学院兰州化学物理研究所 A kind of high entropy copper alloy of high toughness wear resistant

    Citations (1)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US2234552A (en) * 1939-10-23 1941-03-11 Chicago Dev Co Hardened nonferrous alloy

    Family Cites Families (6)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    GB577170A (en) * 1941-04-21 1946-05-08 Maurice Cook Improvements in or relating to hard copper alloys
    BE790453A (en) 1971-10-26 1973-02-15 Brooks Reginald G MANUFACTURE OF METAL ARTICLES
    GB1599392A (en) 1978-05-31 1981-09-30 Osprey Metals Ltd Method and apparatus for producing workable spray deposits
    EP0225732B1 (en) 1985-11-12 1992-01-22 Osprey Metals Limited Production of spray deposits
    GB8527852D0 (en) 1985-11-12 1985-12-18 Osprey Metals Ltd Atomization of metals
    DE4006410C2 (en) * 1990-03-01 1994-01-27 Wieland Werke Ag Semi-finished products made of copper or a copper alloy with added carbon

    Patent Citations (1)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US2234552A (en) * 1939-10-23 1941-03-11 Chicago Dev Co Hardened nonferrous alloy

    Non-Patent Citations (4)

    * Cited by examiner, † Cited by third party
    Title
    CHEMICAL ABSTRACTS, vol. 81, no. 18, 4 November 1974, Columbus, Ohio, US; abstract no. 110011, BELOUSOV, V. YA.: "New materials in gas and petroleum industry machine building" XP002170177 *
    CHEMICAL ABSTRACTS, vol. 87, no. 8, 22 August 1977, Columbus, Ohio, US; abstract no. 57104, ZUBAREV, A. V. ET AL: "Increasing the work efficiency of a cutter reinforced with a composite material" XP002170178 *
    KHIM. NEFT. MASHINOSTR. (1974), (3), 18-20, 1974 *
    MASH. NEFT. OBORUDOVANIE (1977), (2), 12-15, 1977 *

    Cited By (2)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    WO2014202221A1 (en) 2013-06-19 2014-12-24 Isabellenhütte Heusler Gmbh & Co. Kg Resistor alloy, component produced therefrom and production method therefor
    DE102013010301A1 (en) * 2013-06-19 2014-12-24 Isabellenhütte Heusler Gmbh & Co. Kg Resistance alloy, component manufactured therefrom and manufacturing method therefor

    Also Published As

    Publication number Publication date
    CA2381911C (en) 2009-09-08
    US6866818B2 (en) 2005-03-15
    US20020166609A1 (en) 2002-11-14
    NO20021709L (en) 2002-10-21
    NO20021709D0 (en) 2002-04-11
    DE50106520D1 (en) 2005-07-21
    CA2381911A1 (en) 2002-10-19
    ATE298007T1 (en) 2005-07-15
    EP1264906B1 (en) 2005-06-15

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