WO2009108975A1 - GLEITLAGERLEGIERUNG AUS WEIßMETALL AUF ZINNBASIS - Google Patents

GLEITLAGERLEGIERUNG AUS WEIßMETALL AUF ZINNBASIS Download PDF

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Publication number
WO2009108975A1
WO2009108975A1 PCT/AT2009/000082 AT2009000082W WO2009108975A1 WO 2009108975 A1 WO2009108975 A1 WO 2009108975A1 AT 2009000082 W AT2009000082 W AT 2009000082W WO 2009108975 A1 WO2009108975 A1 WO 2009108975A1
Authority
WO
WIPO (PCT)
Prior art keywords
content
white metal
antimony
bearing alloy
plain bearing
Prior art date
Application number
PCT/AT2009/000082
Other languages
German (de)
English (en)
French (fr)
Inventor
Alexander Eberhard
Falco Langbein
Original Assignee
Miba Gleitlager Gmbh
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Miba Gleitlager Gmbh filed Critical Miba Gleitlager Gmbh
Priority to CN200980107224.XA priority Critical patent/CN101960029B/zh
Priority to JP2010549994A priority patent/JP5563489B2/ja
Priority to DE112009000194T priority patent/DE112009000194A5/de
Publication of WO2009108975A1 publication Critical patent/WO2009108975A1/de

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C13/00Alloys based on tin
    • C22C13/02Alloys based on tin with antimony or bismuth as the next major constituent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/12Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
    • F16C33/121Use of special materials

Definitions

  • the invention relates to a tin-based white metal plain bearing alloy containing antimony as the main alloying element and 1 to 10% by weight of copper.
  • Tin-based plain bearing alloys are known (GB 2 146 354 A) containing 2 to 15% by weight of antimony, 1 to 10% by weight of copper, up to 15% by weight of lead and further alloying elements such as cadmium, nickel, silver, tellurium , Cobalt, magnesium, manganese and arsenic, wherein a content of 0.005 to 0.5 wt.% Titanium refine the microstructure of the bearing material and thus improve the carrying capacity of a sliding bearing.
  • the invention is therefore an object of the invention to increase the strength of a sliding bearing alloy of tin-based white metal of the type described without having to use polluting alloying elements such as cadmium, lead, arsenic and chromium.
  • the cadmium-, lead-, arsenic- and chromium-free white metal apart from unavoidable impurities, contains 4 to 30% by weight of antimony as the main alloying element, at least one element consisting of a cobalt, manganese, scandium and germanium-containing element group a total concentration of between 0.2 and 2.6% by weight, based on the elements used in this group, and at least one element of a magnesium, nickel, zirconium and titanium-containing element group in a total concentration of between 0.05 and 10 based on the elements used in this group 1, 7 wt.%, Wherein the sum content of antimony and copper at a minimum of three times the copper content corresponding antimony content is at most 35 wt.%. In both cases, the minimum content is the efficacy limit, the maximum content prevents extensive, due to their size and number already harmful excretions.
  • the alloying of cobalt, manganese, scandium and / or germanium advantageously achieves a refinement and a rounding off of the precipitated intermetallic phases.
  • Germanium also forms intermetallic compounds with free copper, which positively influences the strength of the alloy, provided that the size of the individual precipitates is kept low. Due to the primary crystallization of these higher melting elements, solidification of the white metal results in the formation of a large number of crystallization nuclei which considerably reduce the precipitation of the intermetallic phases with copper and antimony, thereby increasing their strength The tin matrix can be significantly improved without significantly affecting the deformability of the white metal.
  • the elements of the magnesium, nickel, zirconium and titanium-containing element group bind a part of the antimony in intermetallic phases, in particular at higher antimony contents, which counteracts an otherwise associated with a higher antimony content embrittlement.
  • Magnesium also has a strong deoxidizing effect. Excessive levels of magnesium, however, increase the susceptibility to corrosion, especially the pitting occurs.
  • Nickel is found in the copper-tin crystals and increases their hardness. However, it has no negative influence on the sliding properties of the alloy according to the invention. Nickel also improves corrosion resistance and reduces susceptibility to segregation. Contents above 5 wt.%, However, lead to embrittlement of the alloy due to the coating of large, hard phases.
  • Additions of zirconium in the stated contents have a strengthening effect on the matrix and serve for grain refining. Additions of titanium aid grain refining, thereby improving the bearing capacity of the plain bearing alloy, but its hardness remains almost unchanged.
  • An increased copper content solidifies the alloy because an intermetallic phase forms between antimony and copper. However, the copper content must not exceed the stated limit ratio because of the otherwise excessive formation of nadelfömiger copper-tin phases.
  • the white metal can additionally 0.6 to 1, 8 wt.%, Preferably 0.7 to 0.9 wt. % Zinc can be added. Zinc serves to refine the copper-tin and tin antimony phases by forming additional nuclei. This prevents growth of these phases to a harmful size.
  • Similar effects can be achieved by adding to the white metal at least one element from an elemental group comprising silver, gold, vanadium and iron, the individual parts of these alloying elements not exceeding 4% by weight.
  • the total amount must be limited to the top with 8% by weight.
  • the white metal may have an aluminum content of 0.05 to 2.5 wt.%.
  • the aluminum content must be limited to the top in order not to have to negatively impact the porosity of the white metal.
  • Silicon has a similar influence on the white metal. Excess silicon combines with zirconium and scandium to form intermetallic phases, preventing the formation of wave damaging primary silicon crystals. For this reason, silicon and aluminum are preferably added in hypoeutectic composition to avoid the formation of primary silicon crystals. It should therefore the aluminum and the silicon as a heterogeneous phase mixture are present, wherein the aluminum content corresponds to 7 to 45 times the silicon content.
  • the white metal In order to increase the strength properties of the white metal by intermetallic compounds, it is also possible to alloy lithium in a proportion of 0.05 to 1.6% by weight.
  • the addition of at least one rare earth metal may improve the casting properties of the white metal alloy and reduce the susceptibility to segregation.
  • these rare earths have a grain-refining effect.
  • the total concentration of the rare earths used may not exceed 1, 3 wt.%, If adverse effects are to be suppressed.
  • a plain bearing alloy with 15.4 wt.% Antimony, 4.6 wt.% Copper, 0.3 wt.% Manganese, 0.07 wt.% Cobalt, 0.1 wt.% Magnesium, 0, 05 wt.% Nickel and 0.7 wt.% Zinc, remainder tin.
  • This plain bearing alloy had a casting hardness of 36.1 HBW 2.5 / 15.625 / 15. Although the hardness fell off due to cold rolling, it could be increased again to 37.6 HBW 2.5 / 15.625 / 15 by a heat treatment, ie to a hardness above the casting hardness.
PCT/AT2009/000082 2008-03-03 2009-03-02 GLEITLAGERLEGIERUNG AUS WEIßMETALL AUF ZINNBASIS WO2009108975A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN200980107224.XA CN101960029B (zh) 2008-03-03 2009-03-02 由锡基白色金属构成的滑动轴承合金
JP2010549994A JP5563489B2 (ja) 2008-03-03 2009-03-02 錫基ホワイトメタルから成る滑り軸受合金
DE112009000194T DE112009000194A5 (de) 2008-03-03 2009-03-02 Gleitlagerlegierung aus Weißmetall auf Zinnbasis

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ATA344/2008 2008-03-03
AT3442008A AT505664B1 (de) 2008-03-03 2008-03-03 Gleitlagerlegierung aus weissmetall auf zinnbasis

Publications (1)

Publication Number Publication Date
WO2009108975A1 true WO2009108975A1 (de) 2009-09-11

Family

ID=40427631

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/AT2009/000082 WO2009108975A1 (de) 2008-03-03 2009-03-02 GLEITLAGERLEGIERUNG AUS WEIßMETALL AUF ZINNBASIS

Country Status (6)

Country Link
JP (1) JP5563489B2 (zh)
KR (1) KR101566044B1 (zh)
CN (1) CN101960029B (zh)
AT (1) AT505664B1 (zh)
DE (1) DE112009000194A5 (zh)
WO (1) WO2009108975A1 (zh)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013006388A1 (de) * 2013-04-15 2014-10-16 Zollern Bhw Gleitlager Gmbh & Co. Kg Gleitlagerlegierung auf Zinnbasis
EP2902526A1 (de) 2014-01-31 2015-08-05 Miba Gleitlager GmbH Mehrschichtgleitlager
WO2015113092A1 (de) * 2014-01-31 2015-08-06 Miba Gleitlager Gmbh Gleitlager

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102242293A (zh) * 2011-06-24 2011-11-16 哈尔滨工业大学 一种锡基巴氏合金
CN102248320B (zh) * 2011-07-06 2013-06-05 东南大学 锡基复合巴氏合金及制备焊丝的方法
US20130084209A1 (en) * 2011-09-30 2013-04-04 Siemens Industry, Inc. White Metal Babbitt for Rolling Mill Bushing
AT512442B1 (de) 2012-01-25 2013-10-15 Miba Gleitlager Gmbh Verfahren zur herstellung eines gleitlagers
JP5897934B2 (ja) * 2012-03-02 2016-04-06 大同メタル工業株式会社 摺動材料および軸受装置
CN102994803B (zh) * 2012-12-17 2014-02-12 浙江省诸暨申发轴瓦有限公司 一种高软化点温度的轴承合金材料
JP5636033B2 (ja) * 2012-12-28 2014-12-03 大同メタル工業株式会社 摺動部材及びこれを用いた軸受装置
AT514941B1 (de) * 2013-12-23 2015-05-15 Miba Gleitlager Gmbh Mehrschichtgleitlager
CN104451253A (zh) * 2014-12-02 2015-03-25 常熟市华阳机械制造厂 一种使用寿命长的船用轮架
AT516877B1 (de) * 2015-02-19 2016-12-15 Miba Gleitlager Austria Gmbh Gleitlagerelement
CN105750757A (zh) * 2016-03-22 2016-07-13 苏州虎伏新材料科技有限公司 一种用于堆焊以获得锡基巴氏合金耐磨层的焊接材料
JP6959171B2 (ja) 2018-03-28 2021-11-02 大同メタル工業株式会社 摺動部材及びその製造方法
CN108950266B (zh) * 2018-07-26 2019-07-02 红河学院 一种锡基轴承合金的制备方法
CN109055812A (zh) * 2018-09-07 2018-12-21 浙江申发轴瓦股份有限公司 一种巴氏合金材料
CN110819847B (zh) * 2019-11-22 2021-04-16 四川朗峰电子材料有限公司 一种高锑锡基巴氏合金材料及其制备方法
CN111020286B (zh) * 2019-12-13 2021-07-02 郑州机械研究所有限公司 一种锡基巴氏合金及其方法和用途
CN114058899A (zh) * 2022-01-17 2022-02-18 中机智能装备创新研究院(宁波)有限公司 一种锡基巴氏合金的制备方法

Citations (6)

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GB1523665A (en) * 1976-06-23 1978-09-06 Daido Metal Co Ltd Bearing materials
DE2818099A1 (de) * 1978-04-25 1979-11-08 Hohenzollern Huettenverwalt Weissmetall-legierung und deren verwendung
GB2146354A (en) * 1983-09-12 1985-04-17 Darchem Limited Tin-base bearing alloy with refined structure
GB2285059A (en) * 1993-12-27 1995-06-28 Daido Metal Co A tin-base white metal bearing alloy
DE10145389A1 (de) * 2001-09-14 2003-04-10 Forschungsvereinigung Antriebs Gleitlagerlegierung auf Sn-Basis
US20040076541A1 (en) * 2002-10-22 2004-04-22 Laughlin John P. Friction-resistant alloy for use as a bearing

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JPS53131922A (en) * 1977-04-22 1978-11-17 Daido Metal Co Ltd Tinnbased white metal bearing alloy
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JP2679920B2 (ja) * 1992-09-28 1997-11-19 大同メタル工業株式会社 非焼付性に優れたオーバーレイを有するすべり軸受材料
US5411703A (en) * 1993-06-16 1995-05-02 International Business Machines Corporation Lead-free, tin, antimony, bismtuh, copper solder alloy
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JP4504328B2 (ja) * 2006-03-30 2010-07-14 大同メタル工業株式会社 摺動部材

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Publication number Priority date Publication date Assignee Title
GB1523665A (en) * 1976-06-23 1978-09-06 Daido Metal Co Ltd Bearing materials
DE2818099A1 (de) * 1978-04-25 1979-11-08 Hohenzollern Huettenverwalt Weissmetall-legierung und deren verwendung
GB2146354A (en) * 1983-09-12 1985-04-17 Darchem Limited Tin-base bearing alloy with refined structure
GB2285059A (en) * 1993-12-27 1995-06-28 Daido Metal Co A tin-base white metal bearing alloy
DE10145389A1 (de) * 2001-09-14 2003-04-10 Forschungsvereinigung Antriebs Gleitlagerlegierung auf Sn-Basis
US20040076541A1 (en) * 2002-10-22 2004-04-22 Laughlin John P. Friction-resistant alloy for use as a bearing

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013006388A1 (de) * 2013-04-15 2014-10-16 Zollern Bhw Gleitlager Gmbh & Co. Kg Gleitlagerlegierung auf Zinnbasis
WO2014169890A1 (de) 2013-04-15 2014-10-23 Zollern Bhw Gleitlager Gmbh & Co. Kg Gleitlagerlegierung auf zinnbasis
RU2667188C2 (ru) * 2013-04-15 2018-09-17 Цоллерн Бхв Гляйтлагер Гмбх Унд Ко. Кг Сплав для подшипников скольжения на основе олова
US10190630B2 (en) 2013-04-15 2019-01-29 Zollern Bhw Gleitlager Gmbh & Co. Kg Tin-based sliding bearing alloy
EP2902526A1 (de) 2014-01-31 2015-08-05 Miba Gleitlager GmbH Mehrschichtgleitlager
WO2015113092A1 (de) * 2014-01-31 2015-08-06 Miba Gleitlager Gmbh Gleitlager
US9435376B2 (en) 2014-01-31 2016-09-06 Miba Gleitlager Austria Gmbh Multi-layered plain bearing

Also Published As

Publication number Publication date
JP2011513592A (ja) 2011-04-28
CN101960029B (zh) 2013-06-12
KR101566044B1 (ko) 2015-11-05
JP5563489B2 (ja) 2014-07-30
DE112009000194A5 (de) 2011-04-07
AT505664B1 (de) 2009-03-15
AT505664A4 (de) 2009-03-15
CN101960029A (zh) 2011-01-26
KR20100125232A (ko) 2010-11-30

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