US3773504A - Copper base alloy having wear resistance at high temperatures - Google Patents

Copper base alloy having wear resistance at high temperatures Download PDF

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Publication number
US3773504A
US3773504A US00176577A US3773504DA US3773504A US 3773504 A US3773504 A US 3773504A US 00176577 A US00176577 A US 00176577A US 3773504D A US3773504D A US 3773504DA US 3773504 A US3773504 A US 3773504A
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percent
wear resistance
alloy
high temperatures
copper base
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US00176577A
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English (en)
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I Niimi
Y Kaneko
Y Komiyama
Y Uchiyama
Y Takeda
S Maeda
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/04Alloys based on copper with zinc 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
    • 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
    • F16C2204/00Metallic materials; Alloys
    • F16C2204/10Alloys based on copper
    • F16C2204/14Alloys based on copper with zinc 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

  • ABSTRACT The present invention relates to copper base alloys having excellent seizure resistance and wear resistance at high temperatures containing copper as the principal constituent, and zinc (Zn), aluminum (Al), manganese (Mn), silicon (Si), chromium (Cr), and phosphorus (P) as alloy elements;
  • the present invention relates to copper base alloys, and more particularly to copper base alloys that have significant wear resistance at elevated temperatures.
  • Alloys having excellent wear resistance at high temperatures have long been sought as materials for parts subjected to considerable frictional loads at high temperatures.
  • exhaust valve seat materials commonly used today for four cycle automobile engines include cast iron, special cast iron, heat resisting steel and the like.
  • these alloys have the disadvantage that when lead-free gasoline, LPG (liquefied propane gas), etc., are used as fuel, they are subject to an unusual wear, lowering of the output of the internal combustion engine, or deterioration of exhaust gas (increase of CO or hydrocarbon). Trouble-free use of these alloys over long periods of time is therefore impossible.
  • the present invention relates to copper base alloys excellent in seizure resistance and wear resistance at high temperatures. These alloys are composed of elements within specific composition ranges.
  • the alloys according to the present invention are copper base alloys having high wear resistance at high temperatures containing copper as a principal constituent, and from 25 to 40 percent zinc, from .1 to 8 percent aluminum, from 1 to percent manganese, from 0.3 to 2.0 percent silicon, from 0.8 to 3 percent chromium, and from 0.3 to 1 percent phosphorus, and may further contain a small quantity of other elements. (All percentages mentioned in the specification represent weight percent.)
  • the copper base alloys according to the present invention are alloys which contain copper as the principal constituent, and zinc, aluminum, .manganese, silicon, chromium and phosphrous as alloy elements, and further may contain a small quantity of other elements.
  • the alloys according to the present invention are suitable as fabricating materials for exhaust valve seats used in internal combustion engines, particularly the type that uses lead-free gasoline, LPG, or the like which does not contain additives such as lead.
  • the alloy of the present invention is used as a valve seat material, the frictional load is reduced to a negligible quantity. Also, high engine revolutions and high loads and operation during a long engine run can be effected without any difficulty.
  • the alloys according to the present invention are also suitable as fabricating materials for components used in a region where dry wear resistance at high temperatures is required, for example, valve-stem guides, synchronizer rings and bearing constructions.
  • copper is the principal constituent. It has excellent heat conductibility and anticorrosiveness, and combines with oxygen in the air at high temperatures to form copper oxide.
  • a thin film of this copper oxide produces self-lubricating action thereby contributing to the increase of wear resistance of the alloy.
  • Zinc dissolves into copper as a solid solution, reinforcing the crystal matrix, and combines as high temperature with oxygen in the air to produce zinc oxide.
  • This thin film of zinc oxide also produces selflubricating action and remarkably ameliorates the wear resistance of the alloy. Further, zinc lowers the melting point of alloy and ameliorates its castability. Accordingly, when the reinforcement of the crystal matrix and the castability of alloy is taken into consideration, it is desirable that the content of zinc be more than 25 percent.
  • the machinabilty of the alloy is reduced when zinc coexists with other elements which contribute to the reinforcement of the crystal matrix and the wear resistance.
  • the content of zinc has been determined to be less than 40 percent.
  • Aluminum reinforces the crystal matrix and ameliorates the wear resistance, but since this reinforcement is low in degree, with less than 1 percent aluminum the content of zinc has been determined to be more than 1 percent.
  • the machinability deteriorates when it coexits with chromium and the content of aluminum is determined to be less than 8 percent.
  • Chromium reinforces the crystal matrix and increases the hardness equally as aluminum. It also contributes to the amelioration of wear resistance. However, with less than 0.8 percent chromium, the effect of aluminum is small, and the content of chromium has been determined to be more than 0.8 percent. Further, with more than 3 percent chromium, the machinability of the alloy decreases, and the content of chromium has been determined to be less than 3.0 percent. As for manganese, it reinforces the crystal matrix in the same manner as in the case of aluminum, and ameliorates the wear resistance, producing at the same time a remarkably hard intermetallic compound conjointly with silicon. This intermetallic compound I is uniformly dispersed in a finely divided state in the crystal matrix thereby remarkably ameliorating the wear resistance.
  • the content of manganese has been determined to be more than 1 percent.
  • the machinability of the alloy is decreased due to coexistence of manganese with zinc, aluminum, silicon, chromium and the like.
  • the content of manganese is determined to be less than 5 percent.
  • silicon although it produces a remarkably hard intermetallic compound conjointly with manganese and contributes to the increase of wear resistance of the alloy, the quantity produced of hard intermetal- 3 4 lic compound conjointly with manganese is small and g g; the contribution to the wear resistance is small when 01% the content of silicon is less than 0.3 percent.
  • Ti 03 the content of silicon has been determined to be more w 03% arena;
  • the machinability of the alloy is lowered due to the coexistence of zinc, aluminum, manganese, chromium and the like.
  • the content of silicon is determined to be less than 2 percent.
  • Phosphorus is used as a deoxidizer, and with more than 0.3 percent phosphorus it tends to increase the hardness of the alloy and also contribute to the amelioration of wear resistance. However, when the phosphorus content is more than 1 percent, the machinability of alloy decreases. Therefore, the content of phosphorus is determined to be less than 1 percent.
  • composition of the alloy B according to the present invention Composition of the alloy A according to the present invention The determination of the was; quantity mentioned 7 above has been effected by fixing an annular specimen that had been heated to 400450C. in an aluminum alloy, rotating it 10 times per minute, imparting by means of a jig made of heat resisting steel repetitive shocks with collision velocity of 0.2m/sec., surface pressure of 30 Kg/cm, and 2,500 turns/min, and determining the variations of thickness of the specimens for a determined period.
  • the alloys according to the present invention have extremely excellent wear resistance when compared with ordinary cast iron, special cast iron and heat resisting steel.
  • the alloys of the present invention are particularly suitable for fabricating exhaust valve seats which are exposed to extremely high temperatures of the four cycle engines for automobiles which use leadfree gasoline and LPG as fuel.
  • a copper base alloy having wear resistance at high temperature consisting essentially of 25 to 40 percent zinc, l to 8 percent aluminum, 1 to 5 percent manganese, 0.3 to 2.0 percent silicon, 0.8 to 3.0 percent chromium, and 0.3 to 1.0 percent phosphorus, and the balance copper.
  • a copper base alloy as in claim 1 including additional elements of less than 2 percent of any element selected from the group consisting of iron and nickel, less than 1 percent of any element selected from the group consisting of tin, lead, titanium, zirconium, beryllium, boron, cobalt and tungsten and wherein the total sum of said additional elements is less than 5 percent.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Lift Valve (AREA)
US00176577A 1970-12-28 1971-08-31 Copper base alloy having wear resistance at high temperatures Expired - Lifetime US3773504A (en)

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JP12019570 1970-12-28

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US (1) US3773504A (de)
DE (1) DE2145710A1 (de)
GB (1) GB1306484A (de)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3964145A (en) * 1974-03-06 1976-06-22 Ford Motor Company Apex seal material
US4025336A (en) * 1975-05-16 1977-05-24 Hitachi, Ltd. Aluminum bronze having a good wear resistance
US4087971A (en) * 1975-03-24 1978-05-09 Delta Materials Research Limited Devices and methods for converting heat energy to mechanical energy
US4113474A (en) * 1974-09-12 1978-09-12 Toyo Valve Company, Ltd. Copper alloys of excellent corrosion resistance, moldability and workability
US4180398A (en) * 1978-06-22 1979-12-25 Olin Corporation Modification of leaded brasses to improve hot workability
US4337793A (en) * 1974-12-23 1982-07-06 Sumitomo Light Metal Industries, Ltd. Copper-alloy tube water supply
US4378332A (en) * 1981-06-15 1983-03-29 Ford Motor Company Aluminum hardened copper alloy
US4723518A (en) * 1985-12-25 1988-02-09 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder head with valve seat formed integrally by copper alloy cladding layer and underlying alloy layer
US4995924A (en) * 1987-03-24 1991-02-26 Mitsubishi Metal Corporation Synchronizer ring in speed variator made of copper-base alloy
US5000915A (en) * 1986-09-08 1991-03-19 Oiles Corporation Wear-resistant copper alloy
US5069874A (en) * 1986-09-08 1991-12-03 Oiles Corporation Method for reducing high-load, low-speed wear resistance in sliding members
US5544859A (en) * 1994-06-03 1996-08-13 Hazen Research, Inc. Apparatus and method for inhibiting the leaching of lead in water
WO2006058744A1 (de) * 2004-12-02 2006-06-08 Diehl Metall Stiftung & Co. Kg Verwendung einer kupfer-zink-legierung
US20080219881A1 (en) * 2005-04-04 2008-09-11 Diehl Metall Stiftung & Co., Kg Use of a copper zinc alloy
US20080283353A1 (en) * 2006-03-01 2008-11-20 Diehl Metall Stiftung & Co. Kg Brass Alloy and Synchronizing Ring
US20090022620A1 (en) * 2007-06-28 2009-01-22 Kai Weber Copper-zinc alloy, production method and use
US20090311126A1 (en) * 2008-06-11 2009-12-17 Chuankai Xu Lead-free free-cutting phosphorous brass alloy and its manufacturing method
US20100098579A1 (en) * 2008-06-11 2010-04-22 Xiamen Lota International Co., Ltd. Lead-Free, Bismuth-Free Free-Cutting Phosphorous Brass Alloy And Its Manufacturing Method
US20100135848A1 (en) * 2008-12-02 2010-06-03 Chuankai Xu Lead-free free-cutting silicon brass alloy
US20130330227A1 (en) * 2004-12-02 2013-12-12 Diehl Metall Stiftung & Co. Kg Copper-Zinc Alloy for a Valve Guide
DE102013008822A1 (de) * 2013-05-24 2014-11-27 Wieland-Werke Ag Mine für Kugelschreiber und Verwendung
CN104388747A (zh) * 2014-11-13 2015-03-04 无锡信大气象传感网科技有限公司 一种耐磨耐腐传感器用铜合金材料及制造方法
EP4108794A1 (de) * 2021-06-25 2022-12-28 Otto Fuchs - Kommanditgesellschaft - Hochfeste, warmumformbare sondermessinglegierung für ein hoch belastetes bauteil

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2919478A1 (de) * 1979-05-15 1980-11-27 Diehl Gmbh & Co Kupfer-zink-legierung und ihre verwendung
JPS60138032A (ja) * 1983-12-26 1985-07-22 Mitsubishi Metal Corp Cu系形状記憶合金
DE3427740A1 (de) * 1984-07-27 1986-02-06 Diehl GmbH & Co, 8500 Nürnberg Messinglegierung, herstellungsverfahren und verwendung
US5171720A (en) * 1988-09-20 1992-12-15 Asahi Kogaku Kogyo K.K. Porous ceramic sinter and process for producing same
CA2022271C (en) * 1989-07-31 1996-03-12 Soya Takagi Dispersion strengthened copper-base alloy for overlay
DE102005059391A1 (de) 2005-12-13 2007-06-14 Diehl Metall Stiftung & Co.Kg Kupfer-Zink-Legierung sowie daraus hergestellter Synchronring
PL2009122T3 (pl) 2007-06-28 2015-03-31 Wieland Werke Ag Stop miedź-cynk, sposób jego wytwarzania i zastosowanie
DE102008036657B4 (de) * 2008-08-06 2016-09-01 Federal-Mogul Burscheid Gmbh Kolbenring mit adaptiver Beschichtung und Herstellungsverfahren davon
DE102011016318A1 (de) * 2011-04-07 2012-10-11 Wieland-Werke Ag Hartphasenhaltige Kupfer-Zinn-Mehrstoffbronze, Herstellungsverfahren und Verwendung

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB352639A (en) * 1930-02-13 1931-07-16 Hirsch Kupfer & Messingwerke Improvements in and relating to copper-silicon-zinc alloys
GB578874A (en) * 1941-10-17 1946-07-16 Maurice Cook Improvements in or relating to copper base alloys
US3337335A (en) * 1964-06-08 1967-08-22 Mueller Brass Company Leaded silicon manganese bearing brass

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB352639A (en) * 1930-02-13 1931-07-16 Hirsch Kupfer & Messingwerke Improvements in and relating to copper-silicon-zinc alloys
GB578874A (en) * 1941-10-17 1946-07-16 Maurice Cook Improvements in or relating to copper base alloys
US3337335A (en) * 1964-06-08 1967-08-22 Mueller Brass Company Leaded silicon manganese bearing brass

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
The Automobile Engineer, January 1935, pages 23 & 24 *

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3964145A (en) * 1974-03-06 1976-06-22 Ford Motor Company Apex seal material
US4113474A (en) * 1974-09-12 1978-09-12 Toyo Valve Company, Ltd. Copper alloys of excellent corrosion resistance, moldability and workability
US4337793A (en) * 1974-12-23 1982-07-06 Sumitomo Light Metal Industries, Ltd. Copper-alloy tube water supply
US4087971A (en) * 1975-03-24 1978-05-09 Delta Materials Research Limited Devices and methods for converting heat energy to mechanical energy
US4025336A (en) * 1975-05-16 1977-05-24 Hitachi, Ltd. Aluminum bronze having a good wear resistance
US4180398A (en) * 1978-06-22 1979-12-25 Olin Corporation Modification of leaded brasses to improve hot workability
US4378332A (en) * 1981-06-15 1983-03-29 Ford Motor Company Aluminum hardened copper alloy
US4723518A (en) * 1985-12-25 1988-02-09 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder head with valve seat formed integrally by copper alloy cladding layer and underlying alloy layer
AU589727B2 (en) * 1985-12-25 1989-10-19 Toyota Jidosha Kabushiki Kaisha Aluminium alloy cylinder head with valve seat formed integrally by copper alloy cladding layer and underlying alloy layer
US5000915A (en) * 1986-09-08 1991-03-19 Oiles Corporation Wear-resistant copper alloy
US5069874A (en) * 1986-09-08 1991-12-03 Oiles Corporation Method for reducing high-load, low-speed wear resistance in sliding members
US4995924A (en) * 1987-03-24 1991-02-26 Mitsubishi Metal Corporation Synchronizer ring in speed variator made of copper-base alloy
US5544859A (en) * 1994-06-03 1996-08-13 Hazen Research, Inc. Apparatus and method for inhibiting the leaching of lead in water
US5632825A (en) * 1994-06-03 1997-05-27 Technology Management Advisors Llc Apparatus and method for inhibiting the leaching of lead in water
US8435361B2 (en) 2004-12-02 2013-05-07 Diehl Metall Stiftung & Co. Kg Copper-zinc alloy for a valve guide
US20070227631A1 (en) * 2004-12-02 2007-10-04 Diehl Metall Stiftung & Co. Kg Copper-zinc alloy for a valve guide
US20130330227A1 (en) * 2004-12-02 2013-12-12 Diehl Metall Stiftung & Co. Kg Copper-Zinc Alloy for a Valve Guide
WO2006058744A1 (de) * 2004-12-02 2006-06-08 Diehl Metall Stiftung & Co. Kg Verwendung einer kupfer-zink-legierung
KR101138778B1 (ko) * 2004-12-02 2012-04-24 디일 메탈 스티프퉁 운트 코. 카게 구리-아연 합금의 용도
US20080219881A1 (en) * 2005-04-04 2008-09-11 Diehl Metall Stiftung & Co., Kg Use of a copper zinc alloy
CN103290257A (zh) * 2005-04-04 2013-09-11 迪尔金属合作两合公司 铜锌合金的用途
US20080283353A1 (en) * 2006-03-01 2008-11-20 Diehl Metall Stiftung & Co. Kg Brass Alloy and Synchronizing Ring
US20090022620A1 (en) * 2007-06-28 2009-01-22 Kai Weber Copper-zinc alloy, production method and use
US8273192B2 (en) 2008-06-11 2012-09-25 Xiamen Lota International Co., Ltd. Lead-free, bismuth-free free-cutting phosphorous brass alloy
US20100098579A1 (en) * 2008-06-11 2010-04-22 Xiamen Lota International Co., Ltd. Lead-Free, Bismuth-Free Free-Cutting Phosphorous Brass Alloy And Its Manufacturing Method
US20090311126A1 (en) * 2008-06-11 2009-12-17 Chuankai Xu Lead-free free-cutting phosphorous brass alloy and its manufacturing method
US20100135848A1 (en) * 2008-12-02 2010-06-03 Chuankai Xu Lead-free free-cutting silicon brass alloy
DE102013008822A1 (de) * 2013-05-24 2014-11-27 Wieland-Werke Ag Mine für Kugelschreiber und Verwendung
US9637808B2 (en) 2013-05-24 2017-05-02 Wieland-Werke Ag Refill for a ball-point pen and use thereof
CN104388747A (zh) * 2014-11-13 2015-03-04 无锡信大气象传感网科技有限公司 一种耐磨耐腐传感器用铜合金材料及制造方法
CN104388747B (zh) * 2014-11-13 2016-04-27 无锡信大气象传感网科技有限公司 一种耐磨耐腐传感器用铜合金材料及制造方法
EP4108794A1 (de) * 2021-06-25 2022-12-28 Otto Fuchs - Kommanditgesellschaft - Hochfeste, warmumformbare sondermessinglegierung für ein hoch belastetes bauteil
WO2022268676A1 (de) * 2021-06-25 2022-12-29 Otto Fuchs - Kommanditgesellschaft Hochfeste, warmumformbare sondermessinglegierung für ein hoch belastetes bauteil
EP4310354A3 (de) * 2021-06-25 2024-03-20 Otto Fuchs - Kommanditgesellschaft - Hochfeste, warumumformbare sondermessinglegierung für ein hoch belastetes bauteil

Also Published As

Publication number Publication date
GB1306484A (en) 1973-02-14
DE2145710A1 (de) 1972-07-27

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