EP1063310A1 - Utilisation d'une alliage riche en étain de cuivre-étain-fer - Google Patents

Utilisation d'une alliage riche en étain de cuivre-étain-fer Download PDF

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Publication number
EP1063310A1
EP1063310A1 EP00111778A EP00111778A EP1063310A1 EP 1063310 A1 EP1063310 A1 EP 1063310A1 EP 00111778 A EP00111778 A EP 00111778A EP 00111778 A EP00111778 A EP 00111778A EP 1063310 A1 EP1063310 A1 EP 1063310A1
Authority
EP
European Patent Office
Prior art keywords
tin
copper alloy
weight
iron
alloy according
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
EP00111778A
Other languages
German (de)
English (en)
Other versions
EP1063310B1 (fr
Inventor
Andreas Dr. Bögel
Stephan Dr. Hansmann
Uwe Dr. Hofmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wieland Werke AG
Original Assignee
Wieland Werke AG
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Filing date
Publication date
Application filed by Wieland Werke AG filed Critical Wieland Werke AG
Publication of EP1063310A1 publication Critical patent/EP1063310A1/fr
Application granted granted Critical
Publication of EP1063310B1 publication Critical patent/EP1063310B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • C22C9/02Alloys based on copper with tin as the next major constituent

Definitions

  • the invention relates to the use of a Cu-Sn-Fe alloy for mechanical stressed components of machine or vehicle construction.
  • the Cu-Sn-Fe alloy consists of Sn 12 - 20 wt .-%, Fe 0.2 - 5.0 wt .-%, balance Cu and the usual Impurities.
  • the alloy is cooled down sufficiently quickly from the molten state at room temperature in one Get structural state that the preform available for the semi-finished product (Cast strip, cast block, cast bolt) is technically free of coarse, brittle phases and therefore in a special way for the production of semi-finished products Bands, profiles, wires, hollow profiles or pipes - suitable for kneading.
  • This Semi-finished products are ideal for the production of various mechanical Functional parts of precision engineering, vehicle or general mechanical engineering. Because of their chemical composition and manufacturing method draws the above Alloy high mechanical strength or high wear resistance with excellent ductility. She also has one good corrosion resistance and thermal conductivity.
  • CuSn materials are because of their high mechanical strength, their large Resistance to sliding stress or wear and their corrosion resistance for various mechanical components of the general Mechanical engineering used.
  • CuSn wrought alloys with typically 8% by weight Sn are very easy to form and are therefore also suitable for the production of complex ones Functional parts.
  • Sn contents are above 10% by weight.
  • the cast bronze has the required strength, but it is also bad malleable.
  • these phases can also be followed by a thermal aftertreatment cannot be removed without pores or imperfections in the material remain, which in turn affect the deformation.
  • the material is said to have the chemical and mechanical properties of the cast bronze combine with the processing properties of the kneading materials, which is why the adjustment of the cold deformability and at the same time securing a high mechanical strength and hardness is necessary.
  • the material is a tin-rich CuSn alloy with about 12-20% by weight Sn, the rest Cu.
  • the high Sn content ensures the strength of the material.
  • Spray compacting is a suitable method for shaping this alloy or tape casting .
  • the material cools so quickly from the molten state that the segregation that is customary in castings is suppressed.
  • the primary structure of this alloy is therefore free of macroscopic segregation at room temperature .
  • the preforms produced with these processes can be shaped hot or cold.
  • the material so produced is mainly due to its excellent mechanical Properties versatile in the field of mechanical engineering. Yet some shortcomings can be identified.
  • the process of master shaping is difficult for the following reasons: As with conventional, comparatively low tin wrought wrought alloys also in the present case the need to deoxidize the melt. At The conventional alloys are therefore more oxygen-sensitive to the melt Elements such as B. phosphorus added. These additions are usually like this selected that in addition to melt deoxidation also the material properties (e.g. strength) can be influenced favorably. Because of the high affinity for oxygen the added elements tend to burn off when they melt and pour and slagging. As a result, complex process control is required for compliance of defined concentrations necessary, generally affect the oxides The deoxidizer in the melt also sensitive to the melt viscosity and thus the procedural boundary conditions of the primary molding process such as e.g. of spray compacting. Ideally, therefore, a vacuum oven comes for the Melting process used so that oxidation of the additives is largely prevented can be. However, the required process engineering is not always Expedient and economical.
  • Oxides from admixtures with an affinity for oxygen can also be used in hot forming of the tin-rich CuSn alloys. They deteriorate the surface quality of the material to be formed and lead to tool contamination and consequently to a shorter tool life. When cutting or These oxides are also undesirable in the material volume because they are due to promote increased tool wear due to their hardness.
  • the object thus achieved is achieved by the present invention in such a way solved that for mechanical components of machine or vehicle construction Alloy is used which, in addition to copper, has a tin content of 12 to 20% Sn and contains an iron content of 0.2 to 5% Fe.
  • Alloy which, in addition to copper, has a tin content of 12 to 20% Sn and contains an iron content of 0.2 to 5% Fe.
  • the alloy particularly achieves Fe and Sn contents good mechanical properties. On the one hand, they are expressed in a high degree of firmness or hardness, in a high creep or softening resistance and in a high wear resistance. On the other hand, one is sufficient for the materials to determine great toughness due to a related shape change Cold forming of more than 20% possible.
  • Sn also ensures the corrosion resistance of the material.
  • the Sn content should not exceed 20% because then - even with an unconventional casting process - The increased occurrence of brittle phases cannot be prevented.
  • iron can be wholly or partly be replaced by cobalt.
  • the setting of certain cutting properties is due to additives made of lead or graphite up to 3% by volume.
  • these additives ensure improved emergency running properties in components subject to friction or sliding.
  • the Levels have to be limited because lead or graphite additives are disadvantageous affect the forming.
  • aluminum can contain up to 2% by weight. be added. Higher levels are not useful as they are surface processing or impair the joining of the material.
  • phosphorus can be used to deoxidize the melt.
  • a significant one Effect occurs from 0.01% P.
  • the structure of the phosphorus should be matched to the iron concentration, the Fe content / P content> 2.
  • P contents above 0.5% by weight should be avoided because thereby reducing the ductility of the material on the one hand and in Loose layers of heat adhere to the heat, particularly during hot forming to disturb.
  • the invention is illustrated by the following example.
  • the structure in the sprayed state was uniform and metallographically free from Segregations. After the bolt had been machined, it was hot-worked by extrusion into a rod with a diameter of 20 mm. The temperature the material was 650 ° C. The bar stock was straightened.
  • the material was in the soft state after hot forming.
  • the bars were pickled for surface leveling.
  • the further processing was carried out using cold drawing processes to increase the strength properties.
  • the alloy according to the invention clearly achieves by using 0.7% by weight of Fe better mechanical properties than the Fe-free variant and is therefore the known tin arms are also more suitable for mechanically stressed components CuSn wrought alloys.
  • the ductility parameters are for both materials similarly, from which it can be concluded that Fe additions are suitable for the formation of To make pores and embrittling oxide lines more difficult during the primary shaping. This was not to be expected because of this effect of iron in a CuSn alloy was not known.
  • the strength parameters clearly exceed those of a conventionally shaped tin bronze with 8% by weight of Sn , which was similarly shaped and heat treated. This leads to the conclusion that the tin-rich alloys have significantly better mechanical properties at high temperatures (ie softening resistance, relaxation resistance, creep or creep resistance) than the conventional CuSn wrought alloys.
  • the alloy according to the invention is therefore also suitable for use at elevated temperatures.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Sliding-Contact Bearings (AREA)
  • Electroplating And Plating Baths Therefor (AREA)
  • Conductive Materials (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
EP00111778A 1999-06-21 2000-06-03 Utilisation d'une alliage riche en étain de cuivre-étain-fer Expired - Lifetime EP1063310B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19928330 1999-06-21
DE19928330A DE19928330C2 (de) 1999-06-21 1999-06-21 Verwendung einer zinnreichen Kupfer-Zinn-Eisen-Knetlegierung

Publications (2)

Publication Number Publication Date
EP1063310A1 true EP1063310A1 (fr) 2000-12-27
EP1063310B1 EP1063310B1 (fr) 2004-09-15

Family

ID=7911986

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00111778A Expired - Lifetime EP1063310B1 (fr) 1999-06-21 2000-06-03 Utilisation d'une alliage riche en étain de cuivre-étain-fer

Country Status (5)

Country Link
EP (1) EP1063310B1 (fr)
JP (1) JP2001064741A (fr)
AT (1) ATE276378T1 (fr)
DE (2) DE19928330C2 (fr)
ES (1) ES2228344T3 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10107601B4 (de) * 2001-02-17 2006-01-12 Bühler Motor GmbH Schneckenbauteil
DE102006052384A1 (de) * 2006-11-07 2008-05-08 BÖGRA Technologie GmbH Lagerschalenpaar und Verfahren zu seiner Herstellung
CN103964617B (zh) * 2014-05-09 2015-04-08 张志雄 一种外螺纹铜合金海水淡化装置
DE102015012095A1 (de) 2015-09-16 2017-03-16 Audi Ag Verfahren zur Herstellung eines Bauteils, Bauteil und Kraftfahrzeug mit einem derartigen Bauteil

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1002966A (en) * 1963-11-15 1965-09-02 Philip Edward Hustwitt Improvements in or relating to wire cloths
US3615373A (en) * 1968-06-14 1971-10-26 Wangner Hermann Alloy for papermaking wire
US4732625A (en) * 1985-07-29 1988-03-22 Pfizer Inc. Copper-nickel-tin-cobalt spinodal alloy
JPS63235455A (ja) * 1987-03-20 1988-09-30 Mitsubishi Electric Corp 高強度銅合金の製造方法
JPH0417635A (ja) * 1990-05-10 1992-01-22 Hitachi Powdered Metals Co Ltd 耐摩耗性銅系焼結合金
JPH0688156A (ja) * 1992-09-08 1994-03-29 Honda Motor Co Ltd 耐摩耗性Cu系焼結合金

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1928747A (en) * 1928-10-11 1933-10-03 Int Nickel Co Nonferrous alloy
DE659207C (de) * 1935-12-10 1938-04-28 Aeg Verfahren zur Erhoehung der elektrischen Leitfaehigkeit von Zinnbronzen
US2128954A (en) * 1936-10-31 1938-09-06 American Brass Co Hot workable bronze
US2128955A (en) * 1937-11-26 1938-09-06 American Brass Co Hot workable phosphor bronze
US2210670A (en) * 1939-02-18 1940-08-06 Westinghouse Electric & Mfg Co Copper alloy
CA980223A (en) * 1972-10-10 1975-12-23 John T. Plewes Method for treating copper-nickel-tin alloy compositions and products produced therefrom
US4016010A (en) * 1976-02-06 1977-04-05 Olin Corporation Preparation of high strength copper base alloy

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1002966A (en) * 1963-11-15 1965-09-02 Philip Edward Hustwitt Improvements in or relating to wire cloths
US3615373A (en) * 1968-06-14 1971-10-26 Wangner Hermann Alloy for papermaking wire
US4732625A (en) * 1985-07-29 1988-03-22 Pfizer Inc. Copper-nickel-tin-cobalt spinodal alloy
JPS63235455A (ja) * 1987-03-20 1988-09-30 Mitsubishi Electric Corp 高強度銅合金の製造方法
JPH0417635A (ja) * 1990-05-10 1992-01-22 Hitachi Powdered Metals Co Ltd 耐摩耗性銅系焼結合金
JPH0688156A (ja) * 1992-09-08 1994-03-29 Honda Motor Co Ltd 耐摩耗性Cu系焼結合金

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 013, no. 039 (C - 563) 27 January 1989 (1989-01-27) *
PATENT ABSTRACTS OF JAPAN vol. 016, no. 172 (C - 0933) 24 April 1992 (1992-04-24) *
PATENT ABSTRACTS OF JAPAN vol. 018, no. 351 (C - 1220) 4 July 1994 (1994-07-04) *

Also Published As

Publication number Publication date
DE19928330C2 (de) 2003-01-16
JP2001064741A (ja) 2001-03-13
ES2228344T3 (es) 2005-04-16
ATE276378T1 (de) 2004-10-15
DE19928330A1 (de) 2001-01-04
EP1063310B1 (fr) 2004-09-15
DE50007736D1 (de) 2004-10-21

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