EP1279749A1 - Aluminiumbronze mit hoher Verschleissfestigkeit - Google Patents

Aluminiumbronze mit hoher Verschleissfestigkeit Download PDF

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Publication number
EP1279749A1
EP1279749A1 EP02016598A EP02016598A EP1279749A1 EP 1279749 A1 EP1279749 A1 EP 1279749A1 EP 02016598 A EP02016598 A EP 02016598A EP 02016598 A EP02016598 A EP 02016598A EP 1279749 A1 EP1279749 A1 EP 1279749A1
Authority
EP
European Patent Office
Prior art keywords
weight
aluminum bronze
aluminum
wear resistance
alloy
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.)
Withdrawn
Application number
EP02016598A
Other languages
German (de)
English (en)
French (fr)
Inventor
Jürgen Dr. Rexer
Karin Liebig
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.)
Diehl Metall Stiftung and Co KG
Original Assignee
Diehl Metall Stiftung and Co KG
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 Diehl Metall Stiftung and Co KG filed Critical Diehl Metall Stiftung and Co KG
Publication of EP1279749A1 publication Critical patent/EP1279749A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/01Alloys based on copper with aluminium 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

Definitions

  • the invention relates to an aluminum bronze for the application area of the synchronizer rings.
  • wear resistance is always to be understood as low material removal due to corrosion.
  • Aluminum bronze has compared to other copper alloys e.g. Brass has the advantage that the part weight can be reduced due to the aluminum used. Such alloys are resistant to oxidation due to a protective layer caused by the aluminum. Aluminum bronzes are also highly resilient and wear-resistant sliding materials, their high strength leads to a low wear rate due to the good sliding properties. In addition, aluminum bronzes are easy to weld.
  • the invention proposes an alloy of 7.5-9.5% Al, 7-9.5% Fe, 7-11% Ni, 1.5-4% Si, the rest copper and usual impurities up to a total 1%. All information is given in percent by weight.
  • the alloy a content of 8 - 9% Al, 8 - 9% Fe, 7 - 10% Ni and 3 - 4% Si, the rest copper and usual impurities up to a total of 1% provided.
  • wear resistance values can be achieved, which are significantly higher than those of the brass materials used previously for synchronizer rings.
  • these alloys have a coefficient of friction which is higher than the values customary for these known materials. The invention thus brings a considerable advance over the brass materials previously used in synchronizer rings at approximately comparable costs.
  • a first alloy contains 69.9% Cu, 8.5% Al, 8.2% Fe, 9.4% Ni and 3.5% Si.
  • This alloy has a wear resistance of 1280 km / g and a coefficient of friction of 0.125.
  • the specified wear resistance is defined by the number of kilometers covered until 1 g of material has been removed from the synchronizer ring.
  • the second alloy contains 71.6% Cu, 7.9% Al, 8.5% Fe, 7.4% Ni and 3.5% Si.
  • a wear resistance of 1530 km / g and a coefficient of friction of 0.140 were measured on the synchronizer rings made from this.
  • a third alloy has a content of 71.5% Cu, 8.8% Al, 6.0% Fe, 9.3% Ni, 3.5% Si.
  • a wear resistance of 1320 km / g and a coefficient of friction of 0.115 were determined.
  • silicon is responsible for the formation of the hard wear-resistant intermetallic phases. There should not be any free silicon in the solution, but should be bound by iron and nickel. Iron and nickel also promote the hardening process.
  • the alloys described above were cast at a casting temperature of 1120 to 1180 ° C; This is followed by cooling in air, the cooling rate not being critical. After heating again, hot forming is carried out by extrusion at temperatures of 800 to 900 ° C and cooling again in air. Finally, after re-heating at a temperature of 790 to 890 ° C, the die was drop-forged and the alloy was then cooled in air.
  • the shape of the intermetallic phases is approximately spherical, which is advantageous in terms of the toughness and ductility of the alloy.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Operated Clutches (AREA)
  • Sliding-Contact Bearings (AREA)
EP02016598A 2001-07-27 2002-07-25 Aluminiumbronze mit hoher Verschleissfestigkeit Withdrawn EP1279749A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10136788 2001-07-27
DE2001136788 DE10136788C2 (de) 2001-07-27 2001-07-27 Aluminiumbronze

Publications (1)

Publication Number Publication Date
EP1279749A1 true EP1279749A1 (de) 2003-01-29

Family

ID=7693394

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02016598A Withdrawn EP1279749A1 (de) 2001-07-27 2002-07-25 Aluminiumbronze mit hoher Verschleissfestigkeit

Country Status (4)

Country Link
EP (1) EP1279749A1 (zh)
CN (1) CN1400326A (zh)
BR (1) BR0202859A (zh)
DE (1) DE10136788C2 (zh)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100516833C (zh) * 2003-12-23 2009-07-22 中国印钞造币总公司 铝青铜光谱标准样品及制造方法
WO2020006205A1 (en) * 2018-06-29 2020-01-02 Oerlikon Metco (Us) Inc. Copper-based hardfacing alloy
WO2023167170A1 (ja) 2022-03-01 2023-09-07 オイレス工業株式会社 アルミニウム青銅合金および該合金を用いた摺動部材
US11939646B2 (en) 2018-10-26 2024-03-26 Oerlikon Metco (Us) Inc. Corrosion and wear resistant nickel based alloys
US12076788B2 (en) 2019-05-03 2024-09-03 Oerlikon Metco (Us) Inc. Powder feedstock for wear resistant bulk welding configured to optimize manufacturability

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007211325A (ja) * 2006-02-13 2007-08-23 Sanbo Copper Alloy Co Ltd 半融合金鋳造用原料アルミニウム青銅合金
CN101307419B (zh) * 2008-05-29 2010-06-23 燕山大学 一种铝青铜合金晶粒细化的方法
US20110229367A1 (en) * 2010-03-17 2011-09-22 Shau-Kuan Chiu Copper nickel aluminum alloy
CN108480645B (zh) * 2018-02-07 2021-04-02 东风商用车有限公司 一种汽车同步环材料及其制备方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2458379A1 (de) * 1974-10-21 1976-04-22 Voest Ag Kupferlegierung mit einem gehalt an aluminium, eisen und silizium
DE2621602A1 (de) * 1975-05-16 1976-12-02 Hitachi Ltd Aluminiumbronze mit hoher verschleissfestigkeit
US4818307A (en) * 1986-12-19 1989-04-04 Toyota Jidosha Kabushiki Kaisha Dispersion strengthened copper-base alloy
US5296057A (en) * 1991-09-20 1994-03-22 Hitachi, Ltd. High abrasion resistant aluminum bronze alloy, and sliding members using same
JPH0913133A (ja) * 1995-06-29 1997-01-14 Hitachi Ltd アルミニウム青銅及びそれを用いた摺動部材
US5658401A (en) * 1993-11-18 1997-08-19 Diehl Gmbh & Co. Copper-zinc alloy

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19900385C2 (de) * 1999-01-08 2001-02-01 Man B & W Diesel As Kopenhagen Hubkolbenmaschine
DE19908107C2 (de) * 1999-02-25 2003-04-10 Man B & W Diesel As Kopenhagen Verfahren zur Erzeugung einer verschleißfesten Oberfläche bei aus Stahl bestehenden Bauteilen sowie Maschine mit wenigstens einem derartigen Bauteil

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2458379A1 (de) * 1974-10-21 1976-04-22 Voest Ag Kupferlegierung mit einem gehalt an aluminium, eisen und silizium
DE2621602A1 (de) * 1975-05-16 1976-12-02 Hitachi Ltd Aluminiumbronze mit hoher verschleissfestigkeit
US4818307A (en) * 1986-12-19 1989-04-04 Toyota Jidosha Kabushiki Kaisha Dispersion strengthened copper-base alloy
US5296057A (en) * 1991-09-20 1994-03-22 Hitachi, Ltd. High abrasion resistant aluminum bronze alloy, and sliding members using same
US5658401A (en) * 1993-11-18 1997-08-19 Diehl Gmbh & Co. Copper-zinc alloy
JPH0913133A (ja) * 1995-06-29 1997-01-14 Hitachi Ltd アルミニウム青銅及びそれを用いた摺動部材

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 1997, no. 05 30 May 1997 (1997-05-30) *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100516833C (zh) * 2003-12-23 2009-07-22 中国印钞造币总公司 铝青铜光谱标准样品及制造方法
WO2020006205A1 (en) * 2018-06-29 2020-01-02 Oerlikon Metco (Us) Inc. Copper-based hardfacing alloy
JP2021529668A (ja) * 2018-06-29 2021-11-04 エリコン メテコ(ユーエス)インコーポレイテッド 銅系ハードフェーシング合金
EP3814543B1 (en) * 2018-06-29 2024-05-15 Oerlikon Metco (US) Inc. Copper-based hardfacing alloy
US11939646B2 (en) 2018-10-26 2024-03-26 Oerlikon Metco (Us) Inc. Corrosion and wear resistant nickel based alloys
US12076788B2 (en) 2019-05-03 2024-09-03 Oerlikon Metco (Us) Inc. Powder feedstock for wear resistant bulk welding configured to optimize manufacturability
WO2023167170A1 (ja) 2022-03-01 2023-09-07 オイレス工業株式会社 アルミニウム青銅合金および該合金を用いた摺動部材

Also Published As

Publication number Publication date
CN1400326A (zh) 2003-03-05
BR0202859A (pt) 2003-05-20
DE10136788C2 (de) 2003-06-05
DE10136788A1 (de) 2003-02-13

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