EP1815033B2 - Verwendung einer kupfer-zink-legierung - Google Patents
Verwendung einer kupfer-zink-legierung Download PDFInfo
- Publication number
- EP1815033B2 EP1815033B2 EP05813327.3A EP05813327A EP1815033B2 EP 1815033 B2 EP1815033 B2 EP 1815033B2 EP 05813327 A EP05813327 A EP 05813327A EP 1815033 B2 EP1815033 B2 EP 1815033B2
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- weight
- copper
- zinc
- sintered steel
- 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.)
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- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 title claims description 21
- 229910001297 Zn alloy Inorganic materials 0.000 title claims description 18
- 229910045601 alloy Inorganic materials 0.000 claims description 72
- 239000000956 alloy Substances 0.000 claims description 72
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 239000010949 copper Substances 0.000 claims description 6
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000010703 silicon Substances 0.000 claims description 5
- 239000011701 zinc Substances 0.000 claims description 5
- 229910052725 zinc Inorganic materials 0.000 claims description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 239000011651 chromium Substances 0.000 claims description 2
- 239000010941 cobalt Substances 0.000 claims description 2
- 229910017052 cobalt Inorganic materials 0.000 claims description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims 1
- 229910052787 antimony Inorganic materials 0.000 claims 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims 1
- 229910052796 boron Inorganic materials 0.000 claims 1
- 229910052793 cadmium Inorganic materials 0.000 claims 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims 1
- 229910052698 phosphorus Inorganic materials 0.000 claims 1
- 239000011574 phosphorus Substances 0.000 claims 1
- 229910052720 vanadium Inorganic materials 0.000 claims 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 15
- 239000010959 steel Substances 0.000 description 15
- 239000000463 material Substances 0.000 description 8
- 229910000851 Alloy steel Inorganic materials 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 239000000446 fuel Substances 0.000 description 4
- 239000000314 lubricant Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000000654 additive Substances 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 229910021332 silicide Inorganic materials 0.000 description 3
- 229910017518 Cu Zn Inorganic materials 0.000 description 2
- 229910017752 Cu-Zn Inorganic materials 0.000 description 2
- 229910017943 Cu—Zn Inorganic materials 0.000 description 2
- 238000009749 continuous casting Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 229910000765 intermetallic Inorganic materials 0.000 description 2
- DALUDRGQOYMVLD-UHFFFAOYSA-N iron manganese Chemical compound [Mn].[Fe] DALUDRGQOYMVLD-UHFFFAOYSA-N 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- YPFNIPKMNMDDDB-UHFFFAOYSA-K 2-[2-[bis(carboxylatomethyl)amino]ethyl-(2-hydroxyethyl)amino]acetate;iron(3+) Chemical compound [Fe+3].OCCN(CC([O-])=O)CCN(CC([O-])=O)CC([O-])=O YPFNIPKMNMDDDB-UHFFFAOYSA-K 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- 229910002551 Fe-Mn Inorganic materials 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/04—Alloys based on copper with zinc as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L3/00—Lift-valve, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces; Parts or accessories thereof
- F01L3/02—Selecting particular materials for valve-members or valve-seats; Valve-members or valve-seats composed of two or more materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L3/00—Lift-valve, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces; Parts or accessories thereof
- F01L3/08—Valves guides; Sealing of valve stem, e.g. sealing by lubricant
Definitions
- the invention relates to a use of a copper-zinc alloy according to claim 1.
- Copper-zinc alloys or sintered steel alloys are used for a valve guide in an internal combustion engine.
- such a copper-zinc alloy is known.
- the properties of the Cu-Zn alloys no longer meet the requirements that are placed on such a valve guide that is to be used in the new FSI engines.
- the working temperature of the valve guides can reach and exceed 300 ° C.
- the currently used copper-zinc alloys soften at these temperatures.
- a comparable, disadvantageous effect is also observed with sintered steel alloys.
- Sintered steel alloys also soften at temperatures above 300 ° C, and the hardness also varies greatly. Incidentally, the manufacturing outlay for sintered steel alloys is high as a result of the powder-metallurgical manufacturing process.
- the present invention is therefore based on the problem of providing a copper-zinc alloy for use as a valve guide, the copper-zinc alloy satisfying the requirements for materials for valve guides, particularly at elevated temperatures and being easy to manufacture.
- the ones from the DE 29 19 478 C2 known alloy contains an Al content of 4-6% by weight and an Mn content of 6-8% by weight.
- the DE 759 865 discloses a cold rolled brass alloy for the manufacture of plain bearings.
- the alloy optionally contains Ni, Mn, Fe, Pb, Th and Al.
- DE 764 372 A1 discloses a copper-zinc alloy with a content of at least 0.1% by weight of cobalt.
- the DE 2 145 710 discloses a copper-based alloy with an Al content of 5-12% by weight.
- the specified copper-zinc alloy has a surprisingly high heat resistance which, in combination with its good wear resistance, makes it possible to use it as a valve guide in the first place.
- This surprising combination of material properties offers the possibility of using the known alloy in a new way as a valve guide.
- the use as a valve guide in modern engines requires a combination of high temperature resistance above 300 ° C with good wear resistance, which is necessary as a result of transverse forces acting on the valve tappets.
- the high coefficient of friction is negligible.
- the invention thus defies a prejudice that has hitherto been widespread among experts.
- valve guides can be manufactured in rod form by semi-continuous or fully continuous continuous casting, extrusion and drawing, i.e. by hot and cold forming.
- a copper-zinc alloy not according to the invention for use as a valve guide comprises 70 to 73% copper, 6 to 8% manganese, 4 to 6% aluminum, 1 to 4% silicon, 1 to 3% iron, 0.5 to 1 , 5% lead, 0 to 0.2% nickel, 0 to 0.2% tin, the remainder zinc and unavoidable impurities.
- the structure of the DE 29 19 478 C2 The manufactured alloy consists of an alpha and beta mixed crystal matrix with up to 60 to 85% alpha phase, the body-centered cubic beta phase being the basic matrix in which the face-centered cubic alpha phase is predominantly finely dispersed.
- the structure can also contain hard intermetallic compounds, for example iron-manganese silicides.
- the alpha phase determines the resistance of the alloy.
- Valve guides made from this alloy have a surprisingly high wear resistance, which is even significantly higher than that of sintered steel.
- the dry friction wear of valve guides made of said alloy enables use in engines that require "cleaner" fuels, i.e. those that are lead- or sulfur-free, as the absence of these additives means that there is no additional wear-reducing effect. This is particularly advantageous at temperatures around 300 ° C, the working temperature of the valve guides in FSI engines.
- Another advantage of using this alloy as a valve guide is that a stable hardness level is achieved in the desired working range above 300 ° C, since the alloy only softens above 430 ° C, whereas the copper-zinc used so far has softened -Alloys starts at 150 ° C.
- the associated drop in hardness occurs from 150 ° C as well as the hardness drop in sintered steel alloys from 300 ° C.
- the alloy comprises 69.5 to 71.5% copper, 6.5 to 8% manganese, 4.5 to 6% aluminum, 1 to 2.5% silicon, 1 up to 2.5% iron, 0.5 to 1% lead, 0 to 0.2% nickel, 0 to 0.2% tin, the remainder zinc and unavoidable impurities.
- the structure of the alloy produced in the usual way has an ⁇ - and ⁇ -mixed crystal matrix with up to 80% finely dispersed alpha phase.
- it can contain hard intermetallic compounds, for example Fe-Mn silicides.
- valve guide is particularly advantageous because it has a hot tensile strength that is twice as high as that of conventional copper-zinc alloys that have hitherto been used as valve guides. Further advantageous properties are a high softening temperature, high strength and high wear resistance.
- a copper-zinc alloy is then used for valve guides, the alloy being 60 to 61.5% copper, 3 to 4% manganese, 2 to 3% aluminum, 0.3 to 1% silicon, 0.2 to 1% iron , 0 to 0.5% lead, 0.3 to 1% nickel, 0 to 0.2% tin, the remainder zinc and unavoidable impurities.
- the structure of said and correspondingly produced alloy has a basic mass of ⁇ mixed crystals in which needle-shaped and ribbon-shaped ⁇ precipitates are embedded.
- the structure can also contain randomly dispersed manganese-iron silicides.
- Valve guides made from this alloy have a high level of wear resistance, which is even significantly higher than that of sintered steel.
- the dry friction wear of valve guides made of said alloy enables use in engines that require "cleaner" fuels, i.e. those that are lead- or sulfur-free, as the absence of these additives means that there is no additional wear-reducing effect. This is particularly advantageous at temperatures around 300 ° C, the working temperature of the valve guides in FSI engines.
- a copper-zinc alloy is used for valve guides, which additionally comprises at least one of the following elements with a concentration ⁇ 0.05% chromium, ⁇ 0.05% titanium, ⁇ 0.05% zirconium.
- Sintered steel and copper-zinc alloys with approximately the following composition are currently used as material for valve guides that are not subject to high temperatures: 56 to 60% copper, 0.3 to 1% lead, 0.2 to 1.2% iron, 0 to 0.2 % Tin, 0.74 to 2% aluminum, 1 to 2.5% manganese, 0.4 to 1% silicon and the remainder zinc along with unavoidable impurities.
- Such an alloy is referred to below as a standard alloy.
- Alloy 1 is an example of the alloy of the present invention.
- Alloy 2 is another comparative alloy.
- the softening behavior of the various materials has been investigated up to a temperature of 500 ° C. It has been shown that the standard alloy for valve guides shows a clear and continuous decrease in hardness from 195 HV50 to only 150 HV50 from a temperature of 100 ° C. In the case of sintered steel, there is a drastic decrease in hardness from 195 to a low 130 HV50 in the relevant temperature range from 300 ° C, with the hardness fluctuating upwards and downwards with increasing temperature. In contrast, alloy 2 has a hardness of around 10% higher (224 HV50), which only decreases from 350 ° C to around 170 HV50. The hardness values of sintered steel at room temperature are only reached from 450 ° C.
- alloy 1 shows a clear increase in hardness from 224 to 280 HV50 with increasing temperature up to 350 ° C.
- alloy 1 has a hardness of 140 HV50 higher than sintered steel. Alloy 1 thus has its maximum hardness at the temperatures that correspond to the working temperature of valve guides in FS1 engines.
- the higher hardness of alloy 1 and 2 compared to the conventionally used materials is due on the one hand to the higher initial hardness and on the other hand to hardening effects.
- the electrical conductivity can be used as a measure of the thermal conductivity, with a high value standing for good thermal conductivity.
- the electrical conductivity of the standard alloy is 11 m / ⁇ mm 2 .
- Alloy 2 has a good electrical conductivity of 7.5 m / ⁇ mm 2 , which is only about a quarter lower than that of the standard alloy.
- the electrical conductivity of alloy 1 is 4.6 m / ⁇ mm 2 .
- the heat dissipation of alloys 1 and 2 is significantly improved.
- the wear behavior was investigated with and without a lubricant.
- sintered steel has the highest wear resistance (2500 km / g).
- Alloy 1 also has an excellent wear resistance of 1470 km / g, which is more than a factor of 10 higher than the wear resistance of the standard alloy of 126 km / g.
- the wear resistance of alloy 2 with lubricant (94 km / g) is in this range.
- alloys 1 and 2 have clear advantages over sintered steel and the standard alloy.
- Sintered steel has a wear of 312 km / g, which roughly corresponds to the wear behavior of the standard alloy with 357 km / g.
- the dry wear behavior of alloy 2, at 417 km / g, is significantly better than that of standard alloy and sintered steel. In other words, there is much less wear and tear.
- Alloy 1, at 625 km / g has twice as much wear resistance as sintered steel.
- the low dry friction wear makes alloys 1 and 2 particularly interesting, because the increasing purity of the fuels due to the engine, i.e. the absence of lead or sulfur, the wear-reducing effect of the so-called "blow by", the lubrication by the fuel itself in the additives will not be available in the future.
- the hot tensile strength was determined using tensile tests at 350 ° C.
- the hot tensile strength of the standard alloy is 180 N / mm 2 .
- Alloy 1 has an amount twice as high (384 N / mm 2 ).
- alloy 2 has an approx. 35% higher hot tensile strength, which is 243 N / mm 2 .
- Alloy 1 and alloy 2 can preferably be produced by semicontinuous or fully continuous casting, extrusion, drawing and straightening.
- Alloy 2 and in particular alloy 1 have clear advantages over the previous standard alloy used as a valve guide alloy and compared to sintered steel. These advantages relate to the hot tensile strength, the softening temperature, the strength and the wear resistance. In addition, the conductivity is sufficient, which is why alloys 1 and 2 represent a considerable improvement in terms of use as valve guides, since these alloys meet the requirements for the material at the increased operating temperatures in the new engines.
- Table 1 shows the material properties of a Cu-Zn standard alloy, a sintered steel alloy, alloy 1 and alloy 2 in comparison.
- property Standard alloy Alloy 1 Alloy 2 electr.
- Conductivity (m / ⁇ mm 2 ) 11 4.6 7.5 Hardness (HV50) cold worked (10%) 197 224 224 Dry wear (km / g) 357 625 417 Lubricated wear (km / g) 126 1470 94
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Conductive Materials (AREA)
- Contacts (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004058318A DE102004058318B4 (de) | 2004-12-02 | 2004-12-02 | Verwendung einer Kupfer-Zink-Legierung |
PCT/EP2005/012824 WO2006058744A1 (de) | 2004-12-02 | 2005-12-01 | Verwendung einer kupfer-zink-legierung |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1815033A1 EP1815033A1 (de) | 2007-08-08 |
EP1815033B1 EP1815033B1 (de) | 2015-06-17 |
EP1815033B2 true EP1815033B2 (de) | 2020-11-04 |
Family
ID=35618774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05813327.3A Active EP1815033B2 (de) | 2004-12-02 | 2005-12-01 | Verwendung einer kupfer-zink-legierung |
Country Status (9)
Country | Link |
---|---|
US (1) | US8435361B2 (pt) |
EP (1) | EP1815033B2 (pt) |
JP (1) | JP5225683B2 (pt) |
KR (1) | KR101138778B1 (pt) |
CN (1) | CN100510133C (pt) |
BR (1) | BRPI0518695B1 (pt) |
DE (1) | DE102004058318B4 (pt) |
MX (1) | MX2007006352A (pt) |
WO (1) | WO2006058744A1 (pt) |
Families Citing this family (30)
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EP2806044B1 (de) | 2007-06-28 | 2017-09-13 | Wieland-Werke AG | Kupfer-Zink-Legierung, Verfahren zur Herstellung und Verwendung |
DE102007063643B4 (de) * | 2007-06-28 | 2012-07-26 | Wieland-Werke Ag | Kupfer-Zink-Legierung, Verfahren zur Herstellung und Verwendung |
US20100061884A1 (en) * | 2008-09-10 | 2010-03-11 | Pmx Industries Inc. | White-colored copper alloy with reduced nickel content |
CN101451204B (zh) * | 2008-12-15 | 2010-10-13 | 无锡吉泉五金机械有限公司 | 汽车空调用导向球及其制备方法 |
JP5342882B2 (ja) * | 2009-01-06 | 2013-11-13 | オイレス工業株式会社 | 摺動部材用高力黄銅合金および摺動部材 |
CN101782111B (zh) * | 2010-03-11 | 2011-07-27 | 潍坊金富通机械设备有限公司 | 高硬度耐磨轴瓦 |
CN102859015B (zh) * | 2010-05-21 | 2015-03-04 | 奥依列斯工业株式会社 | 滑动部件用高强度黄铜合金及滑动部件 |
CN101928848B (zh) * | 2010-09-01 | 2012-05-23 | 武汉泛洲中越合金有限公司 | 用含铁的中间合金熔炼铜合金的方法 |
CN101974703A (zh) * | 2010-10-29 | 2011-02-16 | 广州唯科得复合金属科技有限公司 | 一种铜合金及铜合金制品 |
KR101340487B1 (ko) * | 2011-09-30 | 2013-12-12 | 주식회사 풍산 | 쾌삭성 무연 구리합금 및 이의 제조방법 |
CN102337421B (zh) * | 2011-10-26 | 2013-05-29 | 宁波正元铜合金有限公司 | 一种复杂黄铜及其制备方法和用途 |
JP2014095127A (ja) * | 2012-11-09 | 2014-05-22 | Taiho Kogyo Co Ltd | 銅合金 |
DE102013004383B4 (de) * | 2013-03-12 | 2015-06-03 | Diehl Metall Stiftung & Co. Kg | Verwendung einer Kupfer-Zink-Legierung |
US10287653B2 (en) | 2013-03-15 | 2019-05-14 | Garrett Transportation I Inc. | Brass alloys for use in turbocharger bearing applications |
CN103480987B (zh) * | 2013-09-26 | 2015-08-19 | 郑州机械研究所 | 一种高脆性铜锌焊丝/焊片的制备方法 |
EP3102713B1 (de) | 2014-02-04 | 2018-07-18 | Otto Fuchs - Kommanditgesellschaft - | Schmierstoffverträgliche kupferlegierung |
DE102014106933A1 (de) * | 2014-05-16 | 2015-11-19 | Otto Fuchs Kg | Sondermessinglegierung und Legierungsprodukt |
DE102015003687A1 (de) * | 2015-03-24 | 2016-09-29 | Diehl Metall Stiftung & Co. Kg | Kupfer-Zink-Legierung und deren Verwendung |
KR102381852B1 (ko) * | 2015-06-09 | 2022-04-05 | 한국재료연구원 | 내마모형 고력황동 및 이의 제조방법 |
DE102015013201B4 (de) * | 2015-10-09 | 2018-03-29 | Diehl Metall Stiftung & Co. Kg | Verwendung einer nickelfeie weiße CuZn-Legierung |
DE102016001994A1 (de) * | 2016-02-19 | 2017-08-24 | Wieland-Werke Ag | Gleitelement aus einer Kupfer-Zink-Legierung |
DE202016102693U1 (de) | 2016-05-20 | 2017-08-29 | Otto Fuchs - Kommanditgesellschaft - | Sondermessinglegierung sowie Sondermessinglegierungsprodukt |
DE202016102696U1 (de) | 2016-05-20 | 2017-08-29 | Otto Fuchs - Kommanditgesellschaft - | Sondermessinglegierung sowie Sondermessinglegierungsprodukt |
WO2018033360A1 (de) | 2016-08-19 | 2018-02-22 | Otto Fuchs - Kommanditgesellschaft | Sondermessinglegierungsprodukt sowie verwendung desselben |
DE202016104552U1 (de) | 2016-08-19 | 2017-11-21 | Otto Fuchs - Kommanditgesellschaft - | Sondermessinglegierungsprodukt sowie Verwendung desselben |
WO2018076161A1 (zh) * | 2016-10-25 | 2018-05-03 | 广东伟强铜业科技有限公司 | 一种黄铜合金及其制造方法 |
DE102018007045A1 (de) * | 2018-09-06 | 2020-03-12 | Diehl Metall Stiftung & Co. Kg | Verwendung einer Messinglegierung zur Herstellung von Bauteilen für den Heizungsbau |
US10781769B2 (en) * | 2018-12-10 | 2020-09-22 | GM Global Technology Operations LLC | Method of manufacturing an engine block |
CN111455213A (zh) * | 2020-05-27 | 2020-07-28 | 苏州撼力合金股份有限公司 | 一种高强度耐磨特种黄铜合金 |
CN115198139B (zh) * | 2022-08-31 | 2023-06-09 | 宁波金田铜业(集团)股份有限公司 | 一种耐磨黄铜合金棒材及其制备方法 |
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DE1558470A1 (de) * | 1967-02-02 | 1970-03-19 | Dies Dr Ing Kurt | Fliesspressteil |
SE7812591L (sv) * | 1977-12-16 | 1979-06-17 | Diehl Gmbh & Co | Koppar-zink-legering och forfarande for framstellning av densamma |
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DD270931B1 (de) | 1988-02-29 | 1992-06-04 | Hettstedt Walzwerk | Verschleissfeste messinglegierung |
JP2606335B2 (ja) * | 1988-11-11 | 1997-04-30 | 三菱マテリアル株式会社 | 耐摩耗性のすぐれた高強度高靭性Cu基焼結合金 |
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2004
- 2004-12-02 DE DE102004058318A patent/DE102004058318B4/de active Active
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2005
- 2005-12-01 BR BRPI0518695-1A patent/BRPI0518695B1/pt active IP Right Grant
- 2005-12-01 CN CNB2005800414129A patent/CN100510133C/zh active Active
- 2005-12-01 EP EP05813327.3A patent/EP1815033B2/de active Active
- 2005-12-01 MX MX2007006352A patent/MX2007006352A/es active IP Right Grant
- 2005-12-01 KR KR1020077011621A patent/KR101138778B1/ko active IP Right Grant
- 2005-12-01 WO PCT/EP2005/012824 patent/WO2006058744A1/de active Application Filing
- 2005-12-01 JP JP2007543774A patent/JP5225683B2/ja active Active
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- 2007-06-01 US US11/809,575 patent/US8435361B2/en active Active
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Also Published As
Publication number | Publication date |
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CN101068941A (zh) | 2007-11-07 |
KR101138778B1 (ko) | 2012-04-24 |
DE102004058318B4 (de) | 2006-09-28 |
BRPI0518695A2 (pt) | 2008-12-02 |
US20070227631A1 (en) | 2007-10-04 |
BRPI0518695B1 (pt) | 2017-07-18 |
EP1815033B1 (de) | 2015-06-17 |
WO2006058744A1 (de) | 2006-06-08 |
MX2007006352A (es) | 2007-10-17 |
KR20070084467A (ko) | 2007-08-24 |
JP5225683B2 (ja) | 2013-07-03 |
CN100510133C (zh) | 2009-07-08 |
DE102004058318A1 (de) | 2006-06-08 |
JP2008522034A (ja) | 2008-06-26 |
US8435361B2 (en) | 2013-05-07 |
EP1815033A1 (de) | 2007-08-08 |
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