EP0881958A1 - Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear - Google Patents

Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear

Info

Publication number
EP0881958A1
EP0881958A1 EP97905071A EP97905071A EP0881958A1 EP 0881958 A1 EP0881958 A1 EP 0881958A1 EP 97905071 A EP97905071 A EP 97905071A EP 97905071 A EP97905071 A EP 97905071A EP 0881958 A1 EP0881958 A1 EP 0881958A1
Authority
EP
European Patent Office
Prior art keywords
weight
powder
material according
powder mixture
valve seat
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
EP97905071A
Other languages
German (de)
French (fr)
Other versions
EP0881958B1 (en
Inventor
Ekkehard KÖHLER
Kirit Dalal
Anil V. Nadkarni
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.)
Bleistahl Produktions-GmbH and Co KG
SCM Metal Products Inc
Original Assignee
Bleistahl Produktions-GmbH and Co KG
SCM Metal Products Inc
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 Bleistahl Produktions-GmbH and Co KG, SCM Metal Products Inc filed Critical Bleistahl Produktions-GmbH and Co KG
Publication of EP0881958A1 publication Critical patent/EP0881958A1/en
Application granted granted Critical
Publication of EP0881958B1 publication Critical patent/EP0881958B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C22C32/001Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
    • C22C32/0015Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
    • C22C32/0021Matrix based on noble metals, Cu or alloys thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/09Mixtures of metallic powders
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/07Alloys based on nickel or cobalt based on cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/04Alloys based on tungsten or molybdenum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper

Definitions

  • the invention relates to a material for the powder-metallurgical production of molded parts with high thermal conductivity and high wear and corrosion resistance by pressing, sintering and optionally post-compression of a powder mixture with a copper content of at least about 50% by weight.
  • Sintered materials of this type are required for molded parts which are exposed to hot gases or gas mixtures, for example for the production of valve seat rings and valve guides for internal combustion engines which are exposed to high mechanical loads on the one hand and at the same time to the action of hot combustion gases. They must therefore be made from materials that are not only wear and corrosion resistant, but also have a high thermal conductivity. Thermal conductivity is becoming increasingly important, as the temperature level at the valves increases due to the expansion of the stoichiometric mixture required for emission reasons, and a continuing trend towards more powerful engines can be seen. It is known to reduce the temperature difference between the head of the valve and the cylinder head into which the valve seat ring is incorporated by transporting heat in the valve.
  • the valve stem is provided with a hollow bore and cooled.
  • the diameters of the valve stems have been reduced in recent years to such an extent that in most cases it is no longer possible to provide them with a hollow bore, so that the use of hollow-bore valves, for example filled with sodium, in Future will no longer be possible.
  • the aim is therefore to improve the thermal conductivity of the material from which the valve seat, in particular the valve seat ring, is made, in order in this way to dissipate the heat more quickly, to lower the temperature level, in order to improve the tribological conditions and the system technologically and improve in cost.
  • Powder-metallurgically produced molded parts made of sintered materials based on iron with infiltrated copper are known which have sufficient wear resistance for use as a valve seat ring or valve guide, the thermal conductivity of which is not high enough compared to sintered materials without a copper content.
  • a sintered material is known from DE-PS 21 14 160, which consists of an iron-based material to which carbon and lead and other alloy components have been added.
  • Valve seat rings made from this material do have sufficient heat and wear resistance, but their thermal conductivity is not sufficient to overcome the problem in particular in the outlet area of a modern one
  • PCT-EP 89/01343 discloses a sintered material for the powder metallurgical production of valve seat rings which are said to have increased thermal conductivity with high wear resistance.
  • the sintered material consists of a base metal powder with a copper content of approximately 70 to 100% by weight of copper and an alloy content.
  • the alloy fraction can consist, for example, of 1 to 3% by weight of cobalt or a high-alloy additional metal powder which is mixed into the basic metal powder as a hard phase, the proportion of which then amounts to a maximum of 30% by weight.
  • the invention has for its object to provide a sintered material for powder metallurgical production, in particular of valve seats or valve guides, the wear resistance of which is very high and which at the same time has a significantly high thermal conductivity compared to known sintered materials used for this purpose.
  • the invention consists in that the starting powder mixture consists of a base powder containing the Cu content in an amount of 50 to 90% by weight and a powdery alloy additive containing molybdenum in an amount of 10 to 50% by weight and that the base powder is a dispersion-strengthened copper powder.
  • the dispersion-strengthened copper powder is preferably solidified by Al2O3, contains from 0.1 to 1.1% by weight of Al2O3 and less than 0.5% by weight of impurities and 97/30808 PC17EP97 / 00837
  • the invention is based on the surprising finding that the use of a Cu-Al ⁇ Os powder, preferably dispersion-strengthened by means of Al2O3, as a material for the powder-metallurgical production of moldings leads to products which, on the one hand, have high wear and corrosion resistance and, on the other hand, high thermal conductivity have, so that they are particularly suitable for the production of valve seat rings or valve guides for internal combustion engines.
  • the applicant attributes this to the fact that the distance between the dispersed AbO 3 particles in the copper matrix in the Cu-Al 2 O 3 powder produced by means of internal oxidation is of the order of 3 to 12 nm, whereas it is approximately the same in the case of the powder produced without internal oxidation Is 40 ⁇ m.
  • dispersion-strengthened metals as base powder for the powder-metallurgical production of molded parts, in particular valve seat rings or valve guides.
  • the alloy surcharge consists of a powdery, preferably water-thinned, intermetallic hard phase of 28 to 32, preferably 30,% by weight.
  • Molybdenum 9 to 1 1, preferably 10% by weight of chromium, 2.5 to 3.5, pre- preferably 3% by weight silicon, the rest cobalt, the intermetallic hard phase being present in the powder mixture in an amount of about 10% by weight and the base powder in an amount of about 90% by weight.
  • the intermetallic hard phase consists of 28 to 32, preferably 30% by weight molybdenum, 9 to 11, preferably 10% by weight chromium, 2.5 to 3.5, preferably 3% by weight. % Silicon, balance iron, the intermetallic phase being present in the powder mixture in an amount of about 10% by weight and the base powder in an amount of about 90% by weight.
  • the alloy surcharge can also consist of a hard phase consisting of a high-speed steel powder of approximately 6% by weight of tungsten, approximately 5% by weight of molybdenum, approximately 2% by weight of vanadium, approximately 4% by weight of chromium, the rest being iron Hard phase is present in the powder mixture in an amount of up to about 30% by weight and the base powder in an amount of about 70% by weight or higher.
  • a hard phase consisting of a high-speed steel powder of approximately 6% by weight of tungsten, approximately 5% by weight of molybdenum, approximately 2% by weight of vanadium, approximately 4% by weight of chromium, the rest being iron Hard phase is present in the powder mixture in an amount of up to about 30% by weight and the base powder in an amount of about 70% by weight or higher.
  • the alloy surcharge can also consist of a hard phase from a Mo-PC powder composed of approximately 11% by weight molybdenum, approximately 0.6% by weight phosphorus, approximately 1.2% by weight carbon, the rest being iron, the Hard phase and the base powder are present in the powder mixture in an amount of approximately 50% by weight.
  • the invention further relates to a material which consists of a starting powder mixture of approximately 80% by weight of base powder, approximately 10% by weight of molybdenum powder and approximately 10% by weight of copper powder or approximately 79% by weight of base powder, approximately 10% by weight of molybdenum powder, approximately 10% by weight of copper powder and approximately 1% by weight of powdered molybdenum trioxide.
  • the invention further provides that the base powder additionally molybdenum disulfide (M0S2) and / or manganese sulfide (MnS) and / or tungsten disulfide (WS2) and / or calcium fluoride (CaF2) and / or tellurium (Te) and / or calcium carbonate (CaC03 > in a total amount of at least 1% by weight to a maximum of 3% by weight based on the amount of the base powder.
  • M0S2 molybdenum disulfide
  • MnS manganese sulfide
  • WS2 tungsten disulfide
  • CaF2 calcium fluoride
  • Te tellurium
  • CaC03 calcium carbonate
  • the invention further relates to a process for the powder-metallurgical production of molded parts with high wear and corrosion resistance and high thermal conductivity, in particular for the production of valve seat rings or valve guides for internal combustion engines, in which an initial powder mixture having one of the compositions described above with about 0.3% by weight of a pressure-relieving agent, e.g. B. wax, mixed, molded and pressed into a molded part with a density of about 8.0 g / cm 3 and subjected to a subsequent sintering under protective gas; the sintering is preferably carried out under a protective gas atmosphere of approximately 80% by weight of nitrogen and approximately 20% by weight of hydrogen for a period of approximately 45 minutes at a temperature of approximately 1,040 ° C. If necessary, the sintered molded part can be subjected to post-compression to a density of approximately 8.8 g / cm 3 .
  • a pressure-relieving agent e.g. B. wax
  • An alternative embodiment of the invention provides that the starting memever according to claim 1 contains one or more of the substances or substance mixtures listed below:
  • the proportion should not exceed 5-20% by weight, typically 10% by weight.
  • the materials of group b) do not alloy with the copper matrix and therefore have no noticeable influence on the thermal conductivity. They are however relatively expensive. However, it has been found that a proportion of 5-10% by weight is sufficient.
  • group c) cause the intermetallic components to be excreted and in this way superimpose the hardness effect in addition to the hardening by the Al2O3 particles in the dispersion-strengthened copper. While the aluminum oxide particles effectively harden the copper matrix at high temperatures (> 500 ° C), the precipitation phases result in more effective hardening in the medium temperature range (200 - 500 ° C), which are the typical operating temperatures to which the valve seat rings are concerned are exposed. The higher warm hardness generally leads to higher wear resistance.
  • the wear of the valve seat rings is also caused by the addition of solid lubricants such as graphite, M0S2, MnS, h-BN, CaF ⁇ and the like, as well as metal additives such as Mo, Co, W or the like, which form oxide skins at the operating temperatures, which have a smear effect.
  • solid lubricants such as graphite, M0S2, MnS, h-BN, CaF ⁇ and the like
  • metal additives such as Mo, Co, W or the like
  • the oxidation resistance i. H. Corrosion resistance in operation
  • Zn is the preferred alloy component.
  • an addition of 5-30% by weight is not critical.
  • the starting powder preferably contains one or more of the following powdery substances with an irregular particle shape: 5 - 25 wt .-% Cu high green strength, electrolyte Cu, oxide-reduced Cu, Mo, or the like.
  • the unsintered, green parts made of this material have only a low strength.
  • the green strength can be increased considerably by adding the aforementioned components.
  • the "Cu of high green strength" is powder with long, thin, fiber-like particles that intertwine when pressed together and in this way bring about a high strength of the green body.
  • the addition of pure Cu does not increase the thermal conductivity touched so that 5-25% by weight can be added, the preferred range being 10-15% by weight.
  • the machinability, in particular the machinability, of dispersion-strengthened copper is improved by adding one or more of the substances mentioned below:
  • the radial breaking strength of the valve seat rings which must be given in particular when pressed into the cylinder head, is increased by adding one or more of the following substances:
  • the starting powder mixture can be optimally coordinated with regard to the properties required for the valve seat ring by a corresponding combination of the aforementioned alloy additives.
  • the main advantage with regard to the production of valve seat rings in all of the aforementioned starting powder mixtures according to the invention is that the thermal conductivity is particularly high, ie at least 100 W / m • k.
  • a medium-internal oxidation-strengthened Cu-Al ⁇ Os powder with a content of 0.5% by weight of Al2O3 was mixed with 0.3% by weight of a conventional press-serifying agent and with a press pressure of 800 MN / mm 2 to form valve seat rings the dimensions 36.6 x 30, 1 x 9 mm pressed.
  • the green compacts, which had a pressed density of 8.4 g / cm 3 were then sintered for 45 minutes at a temperature of 1,040 ° C. under a protective gas atmosphere of 80% N2 and 20% hydrogen.
  • the sintered density was 8.4 g / cm 3 .
  • the sintered rings were then subjected to post-compression to a density of 8.8 g / cm 3 at a pressure of 1,600 MN / mm 2 .
  • Table 1 shows the measured densities and hardness values
  • Table 2 the thermal conductivity values, which were determined by the laser flash method.
  • the rings were then sintered for 45 minutes at a temperature of 1,040 ° C. in a protective gas atmosphere composed of 80% N2 and 20% H2; the sintered density was 8.2 g / cm 3 .
  • the densification to a density of 8.7 g / cm 3 was carried out with a pressure of 1,600 MN / mm 2 .
  • Table 3 shows the density and hardness values
  • Table 4 the thermal conductivity values determined by the laser flash method.
  • valve seat rings produced according to Examples 1 and 2 showed an unexpected improvement in thermal conductivity compared to commercially available valve seat rings based on Fe with and without copper infiltration. This is shown in Figure 1.
  • Curve 1 shows the Thermal conductivity values of a valve seat ring according to Example 1
  • curve 2 the values for a ring according to Example 2
  • curve 3 the values of a valve seat ring based on Fe with copper infiltration
  • curve 4 the values of a commercially available valve seat ring from the applicant.
  • the rings produced according to Example 1 have a hardness which permits their use in the inlet area of an internal combustion engine, while the valve seat rings according to Example 2 can be used in the outlet area and have excellent running behavior here. This was determined by tests, the conditions of which are summarized in Table 5.
  • the results of the engine test are summarized in Table 6 and shown graphically in Figure 2.
  • the sinking depth is the sum of the wear of the valve and the valve seat ring.
  • the valve seat ring according to the invention according to Example 2 was compared with the Series material Como1 2 by the applicant, which is used on a large scale.
  • the sinking depth of the valve seat ring according to the invention with a significantly increased thermal conductivity of the material is less than that of a commercially available valve seat ring.

Abstract

The invention concerns a material for the powder-metallurgical production from a powder mixture containing at least approximately 50 wt.% copper in particular of valve seat rings or valve guides with high resistance to wear and corrosion and high heat conductivity. The starting powder mixture consists of between 50 and 90 wt.% of a basic powder, containing the copper portion, and between 10 and 50 wt.% of a powdery molybdenum-containing alloy flux. The basic powder is a copper powder which is dispersion-hardened by Al2O3, has an Al2O3 content of between 0.1 and 1.1 wt.%, and is produced by pulverizing a Cu-Al melt followed by heating in an oxidizing atmosphere. The invention further concerns the use of a dispersion-hardened powder of this type for the powder-metallurgical production in particular of wear and corrosion-resistant valve seat rings or valve guides with high heat conductivity. Finally, the invention concerns a method of producing such valve seat rings or valve guides.

Description

WERKSTOFF ZUR PULVERMETALLURGISCHEN HERSTELLUNG VON FORMTEILEN, INSB. VON VENTILSITZRINGEN ODER VENTILFUHRUNGEN MIT HOHER VERSCHLEISSFESTIGKEITMATERIAL FOR POWDER METALLURGICAL PRODUCTION OF MOLDED PARTS, IN PART. VALVE SEAT RINGS OR VALVE GUIDES WITH HIGH WEAR RESISTANCE
Die Erfindung betrifft einen Werkstoff zur pulvermetallurgischen Herstellung von Formteilen mit hoher Wärmeleitfähigkeit und hoher Verschleiß- und Korrosionsfestigkeit durch Pressen, Sintern und gegebenenfalls Nach¬ verdichten eines Pulvergemisches mit einem Kupferanteil von wenigstens etwa 50 Gew.-%.The invention relates to a material for the powder-metallurgical production of molded parts with high thermal conductivity and high wear and corrosion resistance by pressing, sintering and optionally post-compression of a powder mixture with a copper content of at least about 50% by weight.
Derartige Sinterwerkstoffe werden für Formteile, die heißen Gasen oder Gasgemischen ausgesetzt sind, benötigt, beispielsweise für die Herstellung von Ventilsitzringen und Ventilführungen für Verbrennungsmotoren, die einerseits hohen mechanischen Belastungen und andererseits gleichzeitig der Einwirkung heißer Verbrennungsgase ausgesetzt sind. Sie müssen 0 daher aus Werkstoffen hergestellt werden, die nicht nur verschleiß- und korrosionsfest sind, sondern auch eine hohe Wärmeleitfähigkeit aufweisen. Dabei kommt der Wärmeleitfähigkeit eine steigende Bedeutung zu, da das Temperaturniveau an den Ventilen durch die aus Emissionsgründen erforderliche Ausweitung des stöchiometrischen Gemisches ansteigt und 5 ein anhaltender Trend zu leistungsstärkeren Motoren erkennbar ist. Es ist bekannt, die Temperaturdifferenz zwischen dem Kopf des Ventils und dem Zylinderkopf, in den der Ventilsitzring eingearbeitet ist, durch Wärme¬ transport im Ventil zu erniedrigen. Zu diesem Zweck wird der Ventilschaft mit einer Hohlbohrung versehen und gekühlt. Aus Kosten- und Gewichts- gründen wurden die Durchmesser der Ventilschäfte in den letzten Jahren derart verkleinert, daß es in den meisten Fällen nicht mehr möglich ist, sie mit einer Hohlbohrung zu versehen, so daß der Einsatz von hohlgebohrten und beispielsweise mit Natrium gefüllten Ventilen in Zukunft nicht mehr möglich sein wird. Das Bestreben geht daher dahin, die Wärmeleitfähigkeit des Materials, aus dem der Ventilsitz, insbesondere der Ventilsitzring, hergestellt wird, zu verbessern, um auf diese Weise die Wärme schneller abzuführen, das Temperaturniveau zu senken, um die tribologischen Verhältnisse zu verbessern und das System technologisch und kostenmäßig zu verbessern.Sintered materials of this type are required for molded parts which are exposed to hot gases or gas mixtures, for example for the production of valve seat rings and valve guides for internal combustion engines which are exposed to high mechanical loads on the one hand and at the same time to the action of hot combustion gases. They must therefore be made from materials that are not only wear and corrosion resistant, but also have a high thermal conductivity. Thermal conductivity is becoming increasingly important, as the temperature level at the valves increases due to the expansion of the stoichiometric mixture required for emission reasons, and a continuing trend towards more powerful engines can be seen. It is known to reduce the temperature difference between the head of the valve and the cylinder head into which the valve seat ring is incorporated by transporting heat in the valve. For this purpose, the valve stem is provided with a hollow bore and cooled. For cost and weight reasons, the diameters of the valve stems have been reduced in recent years to such an extent that in most cases it is no longer possible to provide them with a hollow bore, so that the use of hollow-bore valves, for example filled with sodium, in Future will no longer be possible. The aim is therefore to improve the thermal conductivity of the material from which the valve seat, in particular the valve seat ring, is made, in order in this way to dissipate the heat more quickly, to lower the temperature level, in order to improve the tribological conditions and the system technologically and improve in cost.
Es sind pulvermetallurgisch hergestellte Formteile aus Sinterwerkstoffen auf Eisenbasis mit infiltriertem Kupfer bekannt, die einen zur Verwendung als Ventilsitzring oder Ventilführung ausreichenden Verschleißwiderstand auf¬ weisen, dessen Wärmeleitfähigkeit, verglichen mit Sinterwerkstoffen ohne Kupferanteil nicht hoch genug ist. Beispielsweise ist aus der DE-PS 21 14 160 ein Sinterwerkstoff bekannt, der aus einem Eisen¬ basiswerkstoff besteht, dem Kohlenstoff und Blei sowie andere Legierungs¬ bestandteile zugesetzt sind. Aus diesem Werkstoff hergestellte Ventilsitz¬ ringe besitzen zwar eine ausreichende Warm- und Verschleißfestigkeit, ihre Wärmeleitfähigkeit reicht jedoch nicht aus, um das hier insbesondere anstehende Problem im Auslaßbereich eines modernenPowder-metallurgically produced molded parts made of sintered materials based on iron with infiltrated copper are known which have sufficient wear resistance for use as a valve seat ring or valve guide, the thermal conductivity of which is not high enough compared to sintered materials without a copper content. For example, a sintered material is known from DE-PS 21 14 160, which consists of an iron-based material to which carbon and lead and other alloy components have been added. Valve seat rings made from this material do have sufficient heat and wear resistance, but their thermal conductivity is not sufficient to overcome the problem in particular in the outlet area of a modern one
Verbrennungsmotors zu lösen.Solve internal combustion engine.
Aus der PCT-EP 89/01343 ist ein Sinterwerkstoff zur pulvermetallurgischen Herstellung von Ventilsitzringen bekannt, die eine erhöhte Wärmeleitfähigkeit bei hoher Verschleißfestigkeit aufweisen sollen. Der Sinterwerkstoff besteht aus einem Grundmetallpulver mit einem Kupferanteii von etwa 70 bis 100 Gew. -% Kupfer und einem Legierungsanteil. Der Legierungsanteil kann beispielsweise aus 1 bis 3 Gew.-% Kobalt oder einem hochlegierten Zusatzmetallpulver bestehen, das dem Grundmetailpulver als Hartphase beigemischt ist, deren Anteil dann maximal 30 Gew.-% beträgt.PCT-EP 89/01343 discloses a sintered material for the powder metallurgical production of valve seat rings which are said to have increased thermal conductivity with high wear resistance. The sintered material consists of a base metal powder with a copper content of approximately 70 to 100% by weight of copper and an alloy content. The alloy fraction can consist, for example, of 1 to 3% by weight of cobalt or a high-alloy additional metal powder which is mixed into the basic metal powder as a hard phase, the proportion of which then amounts to a maximum of 30% by weight.
Mit einem derartigen Werkstoff durchgeführte Versuche haben ergeben, daß der Werkstoff eine für die Fertigung von Ventilsitzπngen, insbesondere für den Auslaßbereich von Verbrennungsmotoren, nicht ausreichende Ver- schleιßfes:ιgkeιt aufweist. Dies ist darauf zurückzuführen, daß zwar die Härte des Werkstoffes durch die Verfestigung der Matrix durch Einlagerung von Hartstoffen mit einer maximalen Partikelgröße von 150 μm und damit die Verschleißbeständigkeit des Ventilsitzπnges gesteigert werden konnte, daß jedoch auf der anderen Seite durch die relativ großen und scharfkantigen Einlagerungen der Gegenkörper stärker verschlissen wurde. Es war daher der Verschleiß am Ventilsitzring gering, während der für das dauerhafte Funktionieren des Systems wichtige Gesamtverschleiß verschlechtert wurde.Tests carried out with such a material have shown that the material has a wear resistance which is insufficient for the manufacture of valve seats, in particular for the exhaust area of internal combustion engines. This is due to the fact that the hardness of the material could be increased by solidifying the matrix by embedding hard materials with a maximum particle size of 150 μm and thus the wear resistance of the valve seat, but on the other hand by the relatively large and sharp-edged embedments the counter body was worn out more. The wear on the valve seat ring was therefore low, while the overall wear, which is important for the permanent functioning of the system, was worsened.
Der Erfindung liegt die Aufgabe zugrunde, einen Sinterwerkstoff für die pulvermetallurgische Herstellung, insbesondere von Ventilsitzπngen oder Ventilführungen zu schaffen, dessen Verschleißbeständigkeit sehr hoch ist und der gleichzeitig eine signifikant hohe Wärmeleitfähigkeit verglichen mit bekannten, für diesen Zweck benutzten Sinterwerkstoffen aufweist.The invention has for its object to provide a sintered material for powder metallurgical production, in particular of valve seats or valve guides, the wear resistance of which is very high and which at the same time has a significantly high thermal conductivity compared to known sintered materials used for this purpose.
Ausgehend von einem Werkstoff zur pulvermetallurgischen Herstellung von Formteilen mit hoher Verschleiß- und Korrosionsfestigkeit und hoher Wärmeleitfähigkeit, insbesondere zur Herstellung von Ventilsitzπngen oder Ventilführungen für Verbrennungsmotoren, durch Pressen, Sintern und gegebenenfalls Nachverdichten eines Ausgangs-Pulvergemisches mit einem Kupferanteil von wenigstens etwa 50 Gew.-% besteht die Erfindung darin, daß das Ausgangs-Pulvergemisch aus einem den Cu-Anteil enthaltenden Basispulver in einer Menge von 50 bis 90 Gew.-% und einem pulverförmigen, Molybdän enthaltenden Legierungszuschlag in einer Menge von 10 bis 50 Gew.-% besteht und daß das Basispulver ein dispersionsverfestigt.es Kupferpulver ist. Vorzugsweise ist das dispersionsverfestigte Kupferpulver durch AI2O3 verfestigt, enthält von 0, 1 bis 1 , 1 Gew.-% AI2O3 und weniger als 0,5 Gew.-% Verunreinigungen und 97/30808 PC17EP97/00837Starting from a material for the powder metallurgical production of molded parts with high wear and corrosion resistance and high thermal conductivity, in particular for the production of valve seats or valve guides for internal combustion engines, by pressing, sintering and, if necessary, post-compression of a starting powder mixture with a copper content of at least about 50% by weight. %, the invention consists in that the starting powder mixture consists of a base powder containing the Cu content in an amount of 50 to 90% by weight and a powdery alloy additive containing molybdenum in an amount of 10 to 50% by weight and that the base powder is a dispersion-strengthened copper powder. The dispersion-strengthened copper powder is preferably solidified by Al2O3, contains from 0.1 to 1.1% by weight of Al2O3 and less than 0.5% by weight of impurities and 97/30808 PC17EP97 / 00837
ist durch Verdüsen einer Cu-Al-Schmelze und anschließender Erwärmung in oxidierender Atmosphäre zur selektiven Oxidation des Aluminiums hergestellt.is produced by atomizing a Cu-Al melt and then heating in an oxidizing atmosphere for the selective oxidation of the aluminum.
Der Erfindung liegt die überraschende Erkenntnis zugrunde, daß die Verwendung eines in bestimmter Weise vorzugsweise mittels AI2O3 dispersionsverfestigten Cu-AI∑Os-Pulvers als Werkstoff zur pulvermetallurgischen Herstellung von Formteilen zu Erzeugnissen führt, die einerseits eine hohe Verschleiß- und Korrosionsfestigkeit und andererseits eine hohe Wärmeleitfähigkeit aufweisen, so daß sie sich insbesondere zur Herstellung von Ventilsitzringen oder Ventilführungen für Verbrennungsmotoren eignen.The invention is based on the surprising finding that the use of a Cu-Al∑Os powder, preferably dispersion-strengthened by means of Al2O3, as a material for the powder-metallurgical production of moldings leads to products which, on the one hand, have high wear and corrosion resistance and, on the other hand, high thermal conductivity have, so that they are particularly suitable for the production of valve seat rings or valve guides for internal combustion engines.
Für den vorliegenden Verwendungszweck sind nur solche mit AI2O3 disper¬ sionsverfestigten Cu-Pulver geeignet, die nach dem z. B. aus der US-PS 37 79 714 oder der DE-PS 23 55 1 22 bekannten Verfahren durch Innenoxidation und mit anschließender Erwärmung von Cu-Al legiertem Pulver, hergestellt aus Verdüsen einer Cu-Al-Schmelze, in oxidierender Atmosphäre hergestellt sind, während nach einer anderen Methode gemäß der GB-A-2 083 500 hergestellte dispersionsverfestigte Metallpulver, bei denen eine innere Oxidation ausdrücklich ausgeschlossen werden soll, ungeeignet sind. Die Anmelderin führt dies darauf zurück, daß bei dem mittels Innenoxidation hergestellten Cu-Al2θ3-Pulver der Abstand zwischen den dispergierten Abθ3-Teilchen in der Kupfermatrix in der Größenordnung von 3 bis 12 nm liegt, während sie bei dem ohne Innenoxidation hergestell¬ ten Pulver etwa 40 μm beträgt. Auf die erfindungsgemäße Verwendung von dispersionsverfestigten Metallen als Basispulver zur pulvermetallurgischen Herstellung von Formteilen, insbesondere von Ventilsitzringen oder Ventilführungen, findet sich in diesen Druckschriften kein Hinweis.For the present purpose, only those with Al2O3 dispersion-strengthened Cu powder are suitable, which after the z. B. from US-PS 37 79 714 or DE-PS 23 55 1 22 known processes by internal oxidation and subsequent heating of Cu-Al alloy powder, made from atomizers of a Cu-Al melt, in an oxidizing atmosphere, while dispersion-strengthened metal powders produced by another method according to GB-A-2 083 500, in which internal oxidation is expressly to be excluded, are unsuitable. The applicant attributes this to the fact that the distance between the dispersed AbO 3 particles in the copper matrix in the Cu-Al 2 O 3 powder produced by means of internal oxidation is of the order of 3 to 12 nm, whereas it is approximately the same in the case of the powder produced without internal oxidation Is 40 μm. There is no reference in these publications to the use according to the invention of dispersion-strengthened metals as base powder for the powder-metallurgical production of molded parts, in particular valve seat rings or valve guides.
Eine bevorzugte Ausführungsform der Erfindung sieht vor, daß der Legie- rungszuschlag aus einer pulverförmigen, vorzugsweise wasserverdusten intermetallischen Hartphase aus 28 bis 32, vorzugsweise 30 Gew.-%A preferred embodiment of the invention provides that the alloy surcharge consists of a powdery, preferably water-thinned, intermetallic hard phase of 28 to 32, preferably 30,% by weight.
Molybdän, 9 bis 1 1 , vorzugsweise 10 Gew.-% Chrom, 2,5 bis 3,5, vor- zugsweise 3 Gew.-% Silizium, Rest Kobalt besteht, wobei die intermetal¬ lische Hartphase in dem Pulvergemisch in einer Menge von etwa 10 Gew.- % und das Basispulver in einer Menge von etwa 90 Gew.-% vorliegen.Molybdenum, 9 to 1 1, preferably 10% by weight of chromium, 2.5 to 3.5, pre- preferably 3% by weight silicon, the rest cobalt, the intermetallic hard phase being present in the powder mixture in an amount of about 10% by weight and the base powder in an amount of about 90% by weight.
Bei einer anderen Ausführungsform der Erfindung besteht die intermetal- lische Hartphase aus 28 bis 32, vorzugsweise 30 Gew.-% Molybdän, 9 bis 1 1 , vorzugsweise 10 Gew.-% Chrom, 2,5 bis 3,5, vorzugsweise 3 Gew.-% Silizium, Rest Eisen, wobei die intermetallische Phase in dem Pulvergemisch in einer Menge von etwa 10 Gew.-% und das Basispulver in einer Menge von etwa 90 Gew.-% vorliegen.In another embodiment of the invention, the intermetallic hard phase consists of 28 to 32, preferably 30% by weight molybdenum, 9 to 11, preferably 10% by weight chromium, 2.5 to 3.5, preferably 3% by weight. % Silicon, balance iron, the intermetallic phase being present in the powder mixture in an amount of about 10% by weight and the base powder in an amount of about 90% by weight.
Der Legierungszuschlag kann erfindungsgemäß auch aus einer Hartphase aus einem Schnellstahlpulver aus etwa 6 Gew.-% Wolfram, etwa 5 Gew.- % Molybdän, etwa 2 Gew.-% Vanadium, etwa 4 Gew.-% Chrom, Rest Eisen bestehen, wobei die Hartphase in dem Pulvergemisch in einer Menge von bis zu etwa 30 Gew.-% und das Basispulver in einer Menge von etwa 70 Gew.-% oder höher vorliegen.According to the invention, the alloy surcharge can also consist of a hard phase consisting of a high-speed steel powder of approximately 6% by weight of tungsten, approximately 5% by weight of molybdenum, approximately 2% by weight of vanadium, approximately 4% by weight of chromium, the rest being iron Hard phase is present in the powder mixture in an amount of up to about 30% by weight and the base powder in an amount of about 70% by weight or higher.
Der Legierungszuschlag kann auch aus einer Hartphase aus einem Mo-P-C-Puiver aus etwa 1 1 Gew.-% Molybdän, etwa 0,6 Gew.-% Phosphor, etwa 1 ,2 Gew.-% Kohlenstoff, Rest Eisen bestehen, wobei die Hartphase und das Basispulver in dem Pulvergemisch in einer Menge von jeweils etwa 50 Gew.-% vorliegen.The alloy surcharge can also consist of a hard phase from a Mo-PC powder composed of approximately 11% by weight molybdenum, approximately 0.6% by weight phosphorus, approximately 1.2% by weight carbon, the rest being iron, the Hard phase and the base powder are present in the powder mixture in an amount of approximately 50% by weight.
Gegenstand der Erfindung ist ferner ein Werkstoff, der aus einem Aus- gangs-Pulvergemisch aus etwa 80 Gew.-% Basispulver, etwa 10 Gew.-% Molybdänpulver und etwa 10 Gew.-% Kupferpulver oder etwa 79 Gew.-% Basispulver, etwa 10 Gew.-% Molybdänpulver, etwa 10 Gew.-% Kupfer- pulver und etwa 1 Gew.-% pulverförmigem Molybdäntrioxid besteht.The invention further relates to a material which consists of a starting powder mixture of approximately 80% by weight of base powder, approximately 10% by weight of molybdenum powder and approximately 10% by weight of copper powder or approximately 79% by weight of base powder, approximately 10% by weight of molybdenum powder, approximately 10% by weight of copper powder and approximately 1% by weight of powdered molybdenum trioxide.
Die Erfindung sieht ferner vor, daß das Basispulver zusätzlich Molybdän- disulfid (M0S2) und/oder Mangansulfid (MnS) und/oder Wolframdisulfid {WS2) und/oder Calciumfluorid (CaF2) und/oder Tellur (Te) und/oder Caiciumcarbonat (CaC03> in einer Gesamtmenge von wenigstens 1 Gew.-% bis maximal 3 Gew.-% bezogen auf die Menge des Basispulvers enthält. Gegenstand der Erfindung ist ferner ein Verfahren zur pulvermetallurgischen Herstellung von Formteilen mit hoher Verschleiß- und Korrosionsfestigkeit und hoher Wärmeleitfähigkeit, insbesondere zur Herstellung von Ventilsitz¬ ringen oder Ventilführungen für Verbrennungsmotoren, bei dem ein Aus- gangs-Pulvergemisch mit einer der vorstehend beschriebenen Zusammen¬ setzungen mit etwa 0,3 Gew.-% eines preßerleichternden Mittels, z. B. Wachs, gemischt, verformt und zu einem Formteil mit einer bei etwa 8,0 g/cm3 liegenden Dichte verpreßt und einer anschließenden Sinterung unter Schutzgas unterworfen wird; dabei erfolgt die Sinterung vorzugsweise unter einer Schutzgasatmosphäre aus etwa 80 Gew.-% Stickstoff und etwa 20 Gew.-% Wasserstoff während einer Zeit von etwa 45 min bei einer Temperatur von etwa 1 .040 °C. Gegebenenfalls kann das gesinterte Formteil einer Nachverdichtung auf eine Dichte von etwa 8,8 g/cm3 unterworfen werden.The invention further provides that the base powder additionally molybdenum disulfide (M0S2) and / or manganese sulfide (MnS) and / or tungsten disulfide (WS2) and / or calcium fluoride (CaF2) and / or tellurium (Te) and / or calcium carbonate (CaC03 > in a total amount of at least 1% by weight to a maximum of 3% by weight based on the amount of the base powder. The invention further relates to a process for the powder-metallurgical production of molded parts with high wear and corrosion resistance and high thermal conductivity, in particular for the production of valve seat rings or valve guides for internal combustion engines, in which an initial powder mixture having one of the compositions described above with about 0.3% by weight of a pressure-relieving agent, e.g. B. wax, mixed, molded and pressed into a molded part with a density of about 8.0 g / cm 3 and subjected to a subsequent sintering under protective gas; the sintering is preferably carried out under a protective gas atmosphere of approximately 80% by weight of nitrogen and approximately 20% by weight of hydrogen for a period of approximately 45 minutes at a temperature of approximately 1,040 ° C. If necessary, the sintered molded part can be subjected to post-compression to a density of approximately 8.8 g / cm 3 .
Eine alternative Ausführungsform der Erfindung sieht vor, daß das Aus- gangspuiver gemäß Patentanspruch 1 einen oder mehrere der nachfolgend aufgeführten Stoffe bzw. Stoffgemische enthält:An alternative embodiment of the invention provides that the starting puiver according to claim 1 contains one or more of the substances or substance mixtures listed below:
a) 5 - 30 Gew.-% Werkzeugstahl Typ M35 oder Typ T15,a) 5 - 30% by weight tool steel type M35 or type T15,
Ni-Cr-Si-Fe-B-Cu-Mo;Ni-Cr-Si-Fe-B-Cu-Mo;
b) 5 - 10 Gew. -% W, Mo, Nb, WC, TiC, B4C, TiN, c-BN, TiB2;b) 5-10% by weight of W, Mo, Nb, WC, TiC, B 4 C, TiN, c-BN, TiB 2 ;
c) 0,5 - 5 Gew.-% Ti, Cr, Zr, Cr + Zr, Be, Ni + P.c) 0.5-5% by weight of Ti, Cr, Zr, Cr + Zr, Be, Ni + P.
Die Materialien der Gruppe a) legieren mit der Kupfermatrix des dispersions¬ verfestigten Kupfers, indem diese Zusätze in das Kupfer eindiffundieren und dabei die elektrische und thermische Leitfähigkeit signifikant verringern. Um die Wärmeleitfähigkeit oberhalb von 100 W/m k zu halten, soll der Anteil 5 - 20 Gew.-%, typisch 10 Gew.-%, nicht überschreiten.The materials of group a) alloy with the copper matrix of the dispersion-strengthened copper by diffusing these additives into the copper and thereby significantly reducing the electrical and thermal conductivity. In order to keep the thermal conductivity above 100 W / m k, the proportion should not exceed 5-20% by weight, typically 10% by weight.
Die Materialien der Gruppe b) legieren nicht mit der Kupfermatrix und haben deswegen keinen merklichen Einfluß auf die Wärmeleitfähigkeit. Sie sind jedoch relativ kostspielig. Es hat sich allerdings herausgestellt, daß ein Anteil von 5 - 10 Gew.-% ausreichend ist.The materials of group b) do not alloy with the copper matrix and therefore have no noticeable influence on the thermal conductivity. they are however relatively expensive. However, it has been found that a proportion of 5-10% by weight is sufficient.
Die Zusätze der Gruppe c) bewirken eine Ausscheidung der intermetallischen Bestandteile und überlagern auf diese Weise den Härteeffekt zusätzlich zur Härtung durch die Al2θ3-Partikel in dem dispersionsverfestigten Kupfer. Während die Aluminiumoxid-Partikel eine effektive Härtung der Kupfermatrix bei hohen Temperaturen ( > 500 °C) bewirken, bewirken die Ausscheidungsphasen eine effektivere Härtung im mittleren Temperaturbereich (200 - 500 °C), wobei es sich um die typischen Betriebstemperaturen handelt, denen die Ventilsitzringe ausgesetzt sind. Die höhere Warmhärte führt allgemein zu einer höheren Verschleißfestigkeit.The additions of group c) cause the intermetallic components to be excreted and in this way superimpose the hardness effect in addition to the hardening by the Al2O3 particles in the dispersion-strengthened copper. While the aluminum oxide particles effectively harden the copper matrix at high temperatures (> 500 ° C), the precipitation phases result in more effective hardening in the medium temperature range (200 - 500 ° C), which are the typical operating temperatures to which the valve seat rings are concerned are exposed. The higher warm hardness generally leads to higher wear resistance.
Der Verschleiß der Ventilsitzringe wird auch durch den Zusatz von Fest¬ schmierstoffen wie Graphit, M0S2, MnS, h-BN, CaF∑ und dergleichen sowie Metallzusätze wie Mo, Co, W oder dergleichen bewirkt, die bei den Betrieb¬ stemperaturen Oxidhäute bilden, die einen Schmiereffekt haben.The wear of the valve seat rings is also caused by the addition of solid lubricants such as graphite, M0S2, MnS, h-BN, CaF∑ and the like, as well as metal additives such as Mo, Co, W or the like, which form oxide skins at the operating temperatures, which have a smear effect.
Dadurch, daß das Ausgangspulver gemäß einen oder mehreren der nachfol¬ gend aufgeführten Stoffe:The fact that the starting powder according to one or more of the substances listed below:
5 - 20 Gew.-% Zn, 0, 1 - 5 Gew.-% von einem der Elemente AI, Be, Si, Mg, Sn5-20% by weight of Zn, 0.1-5% by weight of one of the elements Al, Be, Si, Mg, Sn
enthält, wird die Oxidationsfestigkeit, d. h. Korrosionsfestigkeit im Betrieb, erheblich erhöht. Im Hinblick auf eine möglichst geringe Reduzierung der Wärmeleitfähigkeit ist Zn der bevorzugte Legierungsbestandteil. Diesbezüg¬ lich ist ein Zusatz von 5 - 30 Gew.-% unkritisch.contains, the oxidation resistance, i. H. Corrosion resistance in operation, significantly increased. With a view to reducing the thermal conductivity as little as possible, Zn is the preferred alloy component. In this regard, an addition of 5-30% by weight is not critical.
Vorzugsweise enthält das Ausgangspulver einen oder mehreren der nach¬ folgend aufgeführten pulverförmigen Stoffe mit unregelmäßiger Partikel¬ form: 5 - 25 Gew.-% Cu hoher Grünfestigkeit, Elektrolyt-Cu, oxidreduziertes Cu, Mo, oder dergleichen.The starting powder preferably contains one or more of the following powdery substances with an irregular particle shape: 5 - 25 wt .-% Cu high green strength, electrolyte Cu, oxide-reduced Cu, Mo, or the like.
Dadurch, daß das verwendete dispersionsverfestigte Kupfer runde, glatte Partikel hat, haben die ungesinterten, grünen Teile aus diesem Material nur eine geringe Festigkeit. Die Grünfestigkeit kann durch Zuführung der vorge¬ nannten Bestandteile erheblich gesteigert werden. Bei dem „Cu hoher Grün¬ festigkeit" handelt es sich um Pulver mit faserartig langen, dünnen Parti¬ keln, die sich beim Zusammenpressen miteinander verflechten und auf diese Weise eine hohe Festigkeit des Grünkörpers bewirken. Die Wärmeleitfähigkeit wird durch die Zuführung von reinem Cu nicht berührt, so daß 5 - 25 Gew.-% zugefügt werden können, wobei der bevorzugte Bereich bei 10 - 1 5 Gew.-% liegt.Because the dispersion-strengthened copper used has round, smooth particles, the unsintered, green parts made of this material have only a low strength. The green strength can be increased considerably by adding the aforementioned components. The "Cu of high green strength" is powder with long, thin, fiber-like particles that intertwine when pressed together and in this way bring about a high strength of the green body. The addition of pure Cu does not increase the thermal conductivity touched so that 5-25% by weight can be added, the preferred range being 10-15% by weight.
Die Bearbeitbarkeit, insbesondere die Zerspanbarkeit von dispersionsver¬ festigten Kupfer wird durch Zusatz eines oder mehrerer der nachfolgend genannten Stoffe verbessert:The machinability, in particular the machinability, of dispersion-strengthened copper is improved by adding one or more of the substances mentioned below:
a). 0,2 - 2 Gew.-% chemische Elemente wie C (Graphit), Te, Se; b). 0,5 - 5 Gew.-% Sulfide wie M0S2, MnS, usw.; c) . 0,5 - 5 Gew.-% Oxide wie M0O3, WÜ3, C03O4 usw.; d). 0,5 - 5 Gew.-% Verbindungen wie hexagonales BN, CaF∑.a). 0.2-2% by weight of chemical elements such as C (graphite), Te, Se; b). 0.5-5 wt% sulfides such as M0S2, MnS, etc .; c). 0.5-5% by weight of oxides such as M0O3, WÜ3, C03O4, etc .; d). 0.5 - 5 wt .-% compounds such as hexagonal BN, CaF∑.
Die radiale Bruchfestigkeit der Ventilsitzringe, die insbesondere beim Ein¬ pressen in den Zylinderkopf gegeben sein muß, wird durch Zusatz eines oder mehrerer der nachfolgenden Stoffe erhöht:The radial breaking strength of the valve seat rings, which must be given in particular when pressed into the cylinder head, is increased by adding one or more of the following substances:
a) 5 - 20 Gew.-% Zn, 0, 1 - 5 Gew.-% von AI oder Sn, usw.; b) 5 - 30 Gew.-% Werkzeugstahl Typ M35 oder Typ T1 5, Ni-Cr-Si-Fe-B-Cu-Moa) 5-20% by weight of Zn, 0.1-1% by weight of Al or Sn, etc .; b) 5 - 30% by weight tool steel type M35 or type T1 5, Ni-Cr-Si-Fe-B-Cu-Mo
Durch eine entsprechende Kombination der vorgenannten Legierungszusätze läßt sich das Ausgangspulvergemisch im Hinblick auf die jeweils beim Ventilsitzring geforderten Eigenschaften optimal abstimmen. Der hauptsachliche Vorteil im Hinblick auf die Fertigung von Ventilsitzringen liegt bei allen vorgenannten, erfindungsgemäßen Ausgangspulvergemischen dann, daß die Wärmeleitfähigkeit besonders hoch ist, d. h. mindestens 100 W/m k.The starting powder mixture can be optimally coordinated with regard to the properties required for the valve seat ring by a corresponding combination of the aforementioned alloy additives. The main advantage with regard to the production of valve seat rings in all of the aforementioned starting powder mixtures according to the invention is that the thermal conductivity is particularly high, ie at least 100 W / m k.
Ausführungsbeispieleembodiments
Beispiel 1example 1
Ein mitteis Innenoxidation dispersionsverfestigtes Cu-AI∑Os-Pulver mit einem Gehalt von 0,5 Gew.-% AI2O3 wurde mit 0,3 Gew.-% eines üblichen preßerieichternden Mittels gemischt und mit einem Preßdruck von 800 MN/mm2 zu Ventilsitzringen mit den Abmessungen 36,6 x 30, 1 x 9 mm gepreßt. Die Grünlinge, die eine Preßdtchte von 8,4 g/cm3 aufwiesen, wurden anschließend 45 min lang bei einer Temperatur von 1 .040 °C unter einer Schutzgasatmosphäre aus 80 % N2 und 20 % Wasserstoff gesintert. Die Sinterdichte betrug 8,4 g/cm3. Die gesinterten Ringe wurden anschließend einer Nachverdichtung auf eine Dichte von 8,8 g/cm3 bei einem Druck von 1 .600 MN/mm2 unterworfen.A medium-internal oxidation-strengthened Cu-Al∑Os powder with a content of 0.5% by weight of Al2O3 was mixed with 0.3% by weight of a conventional press-serifying agent and with a press pressure of 800 MN / mm 2 to form valve seat rings the dimensions 36.6 x 30, 1 x 9 mm pressed. The green compacts, which had a pressed density of 8.4 g / cm 3 , were then sintered for 45 minutes at a temperature of 1,040 ° C. under a protective gas atmosphere of 80% N2 and 20% hydrogen. The sintered density was 8.4 g / cm 3 . The sintered rings were then subjected to post-compression to a density of 8.8 g / cm 3 at a pressure of 1,600 MN / mm 2 .
Tabelle 1 zeigt die gemessenen Dichten und Härtewerte, Tabelle 2 die Wärmeleitfähigkeitswerte, die nach dem Laser-Flash-Verfahren ermittelt wurden.Table 1 shows the measured densities and hardness values, Table 2 the thermal conductivity values, which were determined by the laser flash method.
Tabelle 1 :Table 1 :
Tabelle 2: Table 2:
Beispiel 2Example 2
90 Gew.-% eines mittels Innenoxidation mit einem Gehalt von 0,5 Gew.-% AI2O3 hergestellten dispersionsverfestigten Cu-Al2θ3-Pulvers wurden mit 10 Gew.-% einer wasserverdusten, pulverförmigen, intermetallischen Hart¬ phase und 0,3 Gew.-% eines üblichen preßerleichternden Mittels gemischt. Die intermetallische Hartphase bestand aus 60 Gew.-% Kobalt, 30 Gew.-% Molybdän, 10 Gew.-% Chrom und 3 Gew.-% Silizium. Das Pulvergemisch wurde bei einem Preßdruck von 800 MN/mm2 in Formen zu Ventilsitzringen mit den Abmessungen 36,6 x 30, 1 x 9 mm verpreßt. Die Grünlinge hatten eine Preßdichte von 8,2 g/cm3. Anschließend wurden die Ringe 45 min lang bei einer Temperatur von 1 .040 °C in einer Schutzgasatmosphäre aus 80 % N2 und 20 % H2 gesintert; die Sinterdichte betrug 8,2 g/cm3. Die Nachverdichtung auf eine Dichte von 8,7 g/cm3 erfolgte mit einem Druck von 1 .600 MN/mm2. Tabelle 3 zeigt die Dichte- und Härtewerte, Tabelle 4 die nach dem Laser-Flash-Verfahren ermittelten Wärmeleitfähigkeitswerte.90% by weight of a dispersion-strengthened Cu-Al2θ3 powder produced by means of internal oxidation with a content of 0.5% by weight of Al2O3 was mixed with 10% by weight of a water-soluble, powdery, intermetallic hard phase and 0.3% by weight. % of a conventional press-relieving agent mixed. The intermetallic hard phase consisted of 60% by weight of cobalt, 30% by weight of molybdenum, 10% by weight of chromium and 3% by weight of silicon. The powder mixture was pressed at a pressure of 800 MN / mm 2 into molds to form valve seat rings with the dimensions 36.6 x 30, 1 x 9 mm. The green compacts had a compression density of 8.2 g / cm 3 . The rings were then sintered for 45 minutes at a temperature of 1,040 ° C. in a protective gas atmosphere composed of 80% N2 and 20% H2; the sintered density was 8.2 g / cm 3 . The densification to a density of 8.7 g / cm 3 was carried out with a pressure of 1,600 MN / mm 2 . Table 3 shows the density and hardness values, Table 4 the thermal conductivity values determined by the laser flash method.
Tabelle 3:Table 3:
Tabelle 4:Table 4:
Die gemäß den Beispielen 1 und 2 hergestellten Ventilsitzringe wiesen eine unerwartete Verbesserung hinsichtlich der Wärmeleitfähigkeit gegenüber handelsüblichen Ventilsitzringen auf Fe-Basis mit und ohne Kupferinfiltration auf. Dies ergibt sich aus Bild 1 . Kurve 1 zeigt die Wärmeleitfähigkeitswerte eines Ventilsitzringes gemäß Beispiel 1 , Kurve 2 die Werte für einen Ring gemäß Beispiel 2, Kurve 3 die Werte eines Ventilsitzringes auf Fe-Basis mit Kupferinfiltration und die Kurve 4 die Werte eines im Handel befindlichen Ventilsitzringes der Anmelderin.The valve seat rings produced according to Examples 1 and 2 showed an unexpected improvement in thermal conductivity compared to commercially available valve seat rings based on Fe with and without copper infiltration. This is shown in Figure 1. Curve 1 shows the Thermal conductivity values of a valve seat ring according to Example 1, curve 2 the values for a ring according to Example 2, curve 3 the values of a valve seat ring based on Fe with copper infiltration and curve 4 the values of a commercially available valve seat ring from the applicant.
Die gemäß Beispiel 1 hergestellten Ringe weisen eine Härte auf, die ihren Einsatz im Einlaßbereich eines Verbrennungsmotors zuläßt, während die Ventilsitzringe gemäß Beispiel 2 im Auslaßbereich eingesetzt werden können und hier ein ausgezeichnetes Laufverhalten aufweisen. Dies wurde durch Versuche ermittelt, deren Bedingungen in der Tabelle 5 zusammengestellt sind.The rings produced according to Example 1 have a hardness which permits their use in the inlet area of an internal combustion engine, while the valve seat rings according to Example 2 can be used in the outlet area and have excellent running behavior here. This was determined by tests, the conditions of which are summarized in Table 5.
Tabelle 5:Table 5:
Die Ergebnisse des Motorversuches sind in Tabelle 6 zusammengefaßt und in Bild 2 graphisch dargestellt. Bei der Einsinktiefe handelt es sich um die Summe aus dem Verschleiß des Ventils und des Ventilsitzringes. Der erfin¬ dungsgemäße Ventilsitzring gemäß Beispiel 2 wurde verglichen mit dem Serienwerkstoff Como1 2 der Anmelderin, der in großem Umfang eingesetzt wird.The results of the engine test are summarized in Table 6 and shown graphically in Figure 2. The sinking depth is the sum of the wear of the valve and the valve seat ring. The valve seat ring according to the invention according to Example 2 was compared with the Series material Como1 2 by the applicant, which is used on a large scale.
Tabelle 6:Table 6:
Es zeigt sich, daß die Einsinktiefe des erfindungsgemäßen Ventilsitzringes bei erheblich gesteigerter Wärmeleitfähigkeit des Materials geringer ist, als die eines handelsüblichen Ventilsitzringes. It can be seen that the sinking depth of the valve seat ring according to the invention with a significantly increased thermal conductivity of the material is less than that of a commercially available valve seat ring.

Claims

P a t e n t a n s p r ü c h e Patent claims
1. Werkstoff zur pulvermetallurgischen Herstellung von Formteilen mit hoher Verschleiß- und Korrosionsfestigkeit und hoher s Wärmeleitfähigkeit, insbesondere zur Herstellung von Ventilsitzringen oder Ventilführungen für Verbrennungsmotoren durch Pressen, Sintern und gegebenenfalls Nachverdichten eines Ausgangs-Pulvergemisches mit einem Kupferanteil von wenigstens etwa 50 Gew.-%, d a d u r c h g e k e n n z e i c h n e t , o daß das Ausgangs-Pulvergemisch aus einem den Cu-Anteil enthaltenden Basispulver in einer Menge von 50 bis 90 Gew.-% und einem pulverförmigen, Molybdän enthaltenden Legierungszuschlag in einer Menge von 10 bis 50 Gew.-% besteht und daß das Basispulver ein dispersionsverfestigtes Kupferpulver ist.1. Material for the powder-metallurgical manufacture of molded parts with high wear and corrosion resistance and high thermal conductivity, in particular for the manufacture of valve seat rings or valve guides for internal combustion engines by pressing, sintering and, if necessary, re-compression of a starting powder mixture with a copper content of at least about 50% by weight. , characterized in that the starting powder mixture consists of a base powder containing the Cu content in an amount of 50 to 90% by weight and a powdery alloy additive containing molybdenum in an amount of 10 to 50% by weight and that Base powder is a dispersion-strengthened copper powder.
5 2. Werkstoff nach Anspruch 1, dadurch gekennzeichnet, daß das dispersionsverfestigte Kupferpulver durch AI2O3 verfestigt ist, von 0,1 bis 1,1 Gew.-% AI2O3 und weniger als 0,5 Gew.-% Verunreinigungen enthält und durch Verdüsen einer Cu-Al-Schmelze und anschließender Erwärmung in einer oxidierenden Atmosphäre zur selektiven Oxidation des Aluminiums 0 hergestellt ist.5 2. Material according to claim 1, characterized in that the dispersion-strengthened copper powder is solidified by AI2O3, contains 0.1 to 1.1 wt .-% AI2O3 and less than 0.5 wt .-% impurities and by spraying a Cu -Al melt and subsequent heating in an oxidizing atmosphere for selective oxidation of the aluminum 0 is produced.
3. Werkstoff nach Anspruch 1 und 2, dadurch gekennzeichnet, daß der Legierungszuschlag aus einer pulverförmigen, vorzugsweise wasserver¬ dusten intermetallischen Hartphase besteht. 3. Material according to claim 1 and 2, characterized in that the alloy surcharge consists of a powdery, preferably water-evaporated intermetallic hard phase.
4. Werkstoff nach den Ansprüchen 1 bis 3, dadurch gekennzeich¬ net, daß die intermetallische Hartphase folgende Zusammensetzung hat:4. Material according to claims 1 to 3, characterized gekennzeich¬ net that the intermetallic hard phase has the following composition:
28 bis 32, vorzugsweise 30 Gew.-% Molybdän, 9 bis 1 1 , vorzugsweise 10 Gew.-% Chrom, 2,5 bis 3,5, vorzugsweise 3 Gew.-% Silizium,28 to 32, preferably 30% by weight of molybdenum, 9 to 11, preferably 10% by weight of chromium, 2.5 to 3.5, preferably 3% by weight of silicon,
Rest Kobalt.Rest cobalt.
5. Werkstoff nach Anspruch 4, dadurch gekennzeichnet, daß die intermetallische Hartphase in dem Pulvergemisch in einer Menge von etwa 10 Gew.-% und das Basispulver in einer Menge von etwa 90 Gew.-% vor- liegen.5. Material according to claim 4, characterized in that the intermetallic hard phase in the powder mixture in an amount of about 10 wt .-% and the base powder are present in an amount of about 90 wt .-%.
6. Werkstoff nach den Ansprüchen 1 und 3, dadurch gekennzeich¬ net, daß die intermetallische Hartphase folgende Zusammensetzung hat:6. Material according to claims 1 and 3, characterized gekennzeich¬ net that the intermetallic hard phase has the following composition:
28 bis 32, vorzugsweise 30 Gew.-% Molybdän, 9 bis 1 1 , vorzugsweise 10 Gew.-% Chrom, 2,5 bis 3,5, vorzugsweise 3 Gew.-% Silizium,28 to 32, preferably 30% by weight of molybdenum, 9 to 11, preferably 10% by weight of chromium, 2.5 to 3.5, preferably 3% by weight of silicon,
Rest Eisen.Rest of iron.
7. Werkstoff nach Anspruch 6, dadurch gekennzeichnet, daß die intermetallische Phase in dem Pulvergemisch in einer Menge von etwa 10 Gew.-% und das Basispulver in einer Menge von etwa 90 Gew.-% vor- liegen.7. Material according to claim 6, characterized in that the intermetallic phase in the powder mixture in an amount of about 10 wt .-% and the base powder are present in an amount of about 90 wt .-%.
8. Werkstoff nach den Ansprüchen 1 und 2, dadurch gekenn¬ zeichnet, daß der Legierungszuschlag aus einer Hartphase aus einem Schnellstahlpulver (AISI-Type M2; DIN S-6-5-2) mit folgender Zusammensetzung besteht:8. Material according to claims 1 and 2, characterized gekenn¬ characterized in that the alloy surcharge consists of a hard phase from a high-speed steel powder (AISI type M2; DIN S-6-5-2) with the following composition:
etwa 6 Gew.-% Wolfram, etwa 5 Gew.-% Molybdän, etwa 2 Gew.-% Vanadium, etwa 4 Gew.-% Chrom, Rest Eisen.about 6% by weight of tungsten, about 5% by weight of molybdenum, about 2% by weight of vanadium, about 4% by weight chromium, balance iron.
9. Werkstoff nach Anspruch 8, dadurch gekennzeichnet, daß die Hartphase in dem Pulvergemisch in einer Menge von bis zu 30 Gew.-% und das Basispulver in einer Menge von etwa 70 Gew.-% oder höher vorliegen.9. Material according to claim 8, characterized in that the hard phase in the powder mixture in an amount of up to 30 wt .-% and the base powder in an amount of about 70 wt .-% or higher.
10. Werkstoff nach den Ansprüchen 1 und 2, dadurch gekenn¬ zeichnet, daß der Legierungszuschlag aus einer Hartphase aus einem Mo-P-C-Pulver mit folgender Zusammensetzung besteht:10. Material according to claims 1 and 2, characterized gekenn¬ characterized in that the alloy surcharge consists of a hard phase from a Mo-P-C powder with the following composition:
etwa 1 1 Gew. -% Molybdän, etwa 0,6 Gew.-% Phosphor, etwa 1 ,2 Gew.-% Kohlenstoff, Rest Eisen.about 11% by weight molybdenum, about 0.6% by weight phosphorus, about 1.2% by weight carbon, balance iron.
1 1 . Werkstoff nach Anspruch 10, dadurch gekennzeichnet, daß die Hartphase und das Basispulver in dem Pulvergemisch in einer Menge von jeweils etwa 50 Gew.-% vorliegen.1 1. Material according to claim 10, characterized in that the hard phase and the base powder are each present in the powder mixture in an amount of approximately 50% by weight.
12. Werkstoff nach Anspruch 1 , gekennzeichnet durch folgende Zusammensetzung des Ausgangs-Pulvergemisches:12. Material according to claim 1, characterized by the following composition of the starting powder mixture:
etwa 80 Gew.-% Basispulver, etwa 10 Gew.-% Molybdänpulver, etwa 10 Gew.-% Kupferpulver.about 80% by weight base powder, about 10% by weight molybdenum powder, about 10% by weight copper powder.
13. Werkstoff nach Anspruch 1 , gekennzeichnet durch folgende Zusammensetzung des Ausgangs-Pulvergemisches:13. Material according to claim 1, characterized by the following composition of the starting powder mixture:
etwa 79 Gew.-% Basispulver, etwa 10 Gew.-% Molybdänpulver, etwa 10 Gew.-% Kupferpulver und etwa 1 Gew.-% Molybdäntrioxid. about 79% by weight base powder, about 10% by weight molybdenum powder, about 10% by weight copper powder and about 1% by weight molybdenum trioxide.
14. Werkstoff nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, daß das Basispulver zusätzlich Molybdändisulfid (M0S2) und/oder Mangansulfid (MnS) und/oder Wolframdisulfid (WS2) und/oder Calciumfluorid (CaF2) und/oder Tellur (Te) und/oder Caiciumcarbonat (CaC03) in einer Gesamtmenge von wenigstens 1 Gew.-% bis maximal 3 Gew.-% bezogen auf die Menge des Basispulvers enthält.14. Material according to one of the preceding claims, characterized in that the base powder additionally molybdenum disulfide (M0S2) and / or manganese sulfide (MnS) and / or tungsten disulfide (WS2) and / or calcium fluoride (CaF2) and / or tellurium (Te) and / or calcium carbonate (CaCO3) in a total amount of at least 1% by weight to a maximum of 3% by weight based on the amount of the base powder.
1 5. Verfahren zur pulvermetallurgischen Herstellung von Formteilen mit hoher Verschleiß- und Korrosionsfestigkeit und hoher Wärmeleitfähigkeit, insbesondere zur Hersteilung von Ventilsitzringen oder Ventilführungen für Verbrennungsmotoren, dadurch gekennzeichnet, daß ein Ausgangs-Pulvergemisch gemäß einem der vorhergehenden Ansprüche mit etwa 0,3 Gew.-% eines preßerleichternden Mittels, z. B. Wachs, gemischt, verformt und zu einem Formteil mit einer bei etwa 8,0 g/cm3 liegenden Dichte verpreßt und einer anschließenden Sinterung unter Schutzgas unterworfen wird.1 5. A method for powder metallurgical production of molded parts with high wear and corrosion resistance and high thermal conductivity, in particular for the manufacture of valve seat rings or valve guides for internal combustion engines, characterized in that an initial powder mixture according to one of the preceding claims with about 0.3 wt. % of a pressure-relieving agent, e.g. B. wax, mixed, deformed and pressed into a molded part with a density of approximately 8.0 g / cm 3 and subjected to a subsequent sintering under protective gas.
1 6. Verfahren nach Anspruch 1 5, dadurch gekennzeichnet, daß die Sinterung unter einer Schutzgasatmosphäre aus etwa 80 Gew.-% Stickstoff und etwa 20 Gew.-% Wasserstoff während einer Zeit von etwa 45 min bei einer Temperatur von etwa 1 .040 °C erfolgt.1 6. The method according to claim 1 5, characterized in that the sintering under a protective gas atmosphere of about 80 wt .-% nitrogen and about 20 wt .-% hydrogen for a period of about 45 minutes at a temperature of about 1 .040 ° C is done.
17. Verfahren nach den Ansprüchen 15 und 1 6, dadurch gekenn¬ zeichnet, daß der gesinterte Formkörper einer Nachverdichtung auf eine Dichte von etwa 8,8 g/cm3 unterworfen wird.17. The method according to claims 15 and 1 6, characterized gekenn¬ characterized in that the sintered molded body is subjected to post-compression to a density of about 8.8 g / cm 3 .
18. Verwendung eines mittels AI2O3 dispersionsverfestigten CU-Al2θ3-Pulvers mit einem zwischen 0,3 und 1 , 1 Gew.-% liegenden Gehalt an AI2O3, das durch Verdüsen einer Cu-Al-Schmelze und anschließende Erwärmung in oxidierender Atmosphäre hergestellt ist, zur pulvermetallurgischen Herstellung von verschleiß- und korrosionsfesten Formteiien mit hoher Wärmeleitfähigkeit, insbesondere zur Herstellung von Ventilsitzringen oder Ventilführungen. 18. Use of a Cu-Al2θ3 powder which has been dispersion-strengthened by means of AI2O3 and has a content of AI2O3 of between 0.3 and 1.1% by weight, which is produced by atomizing a Cu-Al melt and then heating in an oxidizing atmosphere Powder metallurgical production of wear and corrosion resistant molded parts with high thermal conductivity, especially for the production of valve seat rings or valve guides.
1 9. Werkstoffe nach Anspruch 1 , dadurch gekennzeichnet, daß das Ausgangspulvergemisch einen oder mehrere der nachfolgend aufgeführten Stoffe bzw. Stoffgemische enthält:1 9. Materials according to claim 1, characterized in that the starting powder mixture contains one or more of the substances or substance mixtures listed below:
a) 5 - 30 Gew.-% Werkzeugstahl Typ M35 oder Typ T15, Ni-Cr-Si-Fe-B-Cu-Mo;a) 5 - 30% by weight tool steel type M35 or type T15, Ni-Cr-Si-Fe-B-Cu-Mo;
b) 5 - 10 Gew.-% W, Mo, Nb, WC, TiC, B4C, TiN, c-BN, TiB∑;b) 5-10% by weight of W, Mo, Nb, WC, TiC, B 4 C, TiN, c-BN, TiB∑;
c) 0,5 - 5 Gew.-% Ti, Cr, Zr, Cr + Zr, Be, Ni + P.c) 0.5-5% by weight of Ti, Cr, Zr, Cr + Zr, Be, Ni + P.
20. Werkstoffe nach Anspruch 1 , dadurch gekennzeichnet, daß das Ausgangspulvergemisch einen oder mehreren der nachfolgend aufgeführten Stoffe enthält:20. Materials according to claim 1, characterized in that the starting powder mixture contains one or more of the substances listed below:
5 - 10 Gew.-% Co, W.5 - 10% by weight Co, W.
21 . Werkstoff nach Anspruch 1 , dadurch gekennzeichnet, daß das Ausgangspulvergemisch einen oder mehreren der nachfolgend aufgeführten Stoffe enthält:21. Material according to claim 1, characterized in that the starting powder mixture contains one or more of the substances listed below:
5 - 20 Gew.-% Zn, 0, 1 - 5 Gew.-% von einen der Elemente AI, Be, Si, Mg, Sn.5-20% by weight of Zn, 0.1-5% by weight of one of the elements Al, Be, Si, Mg, Sn.
22. Werkstoff nach Anspruch 1 , dadurch gekennzeichnet, daß das Ausgangspulvergemisch einen oder mehrere der nachfolgend aufgeführten pulverförmigen Stoffe mit unregelmäßiger Partikelform enthält:22. Material according to claim 1, characterized in that the starting powder mixture contains one or more of the powdery substances listed below with an irregular particle shape:
5 - 25 Gew.-% Cu hoher Grünfestigkeit, Elektrolyt-Cu, oxidreduziertes Cu, Mo.5 - 25 wt .-% Cu high green strength, electrolyte Cu, oxide-reduced Cu, Mo.
23. Werkstoff nach Anspruch 1 , dadurch gekennzeichnet, daß das Ausgangspulvergemisch einen oder mehreren der nachfolgend unter a) . Tenz bis d) . Tenz aufgeführten Stoffe enthält: a) . 0,2 - 2 Gew. -% chemische Elemente wie C (Graphit), Te, Se; b). 0,5 - 5 Gew. -% Sulfide wie M0S2, MnS, usw.; c) . 0,5 - - 5 Gew. - % Oxide wie M0O3, WO3, C03O4 usw.; d). 0,5 - 5 Gew. - % Verbindungen wie hexagonales BN, CaF∑.23. Material according to claim 1, characterized in that the starting powder mixture one or more of the following under a). Tenz to d). Tenz listed substances contains: a). 0.2 - 2% by weight of chemical elements such as C (graphite), Te, Se; b). 0.5-5% by weight sulfides such as M0S2, MnS, etc .; c). 0.5 - 5% by weight oxides such as M0O3, WO3, C03O4, etc .; d). 0.5 - 5 wt .-% compounds such as hexagonal BN, CaF∑.
24. Werkstoff nach Anspruch 1 , dadurch gekennzeichnet, daß das24. Material according to claim 1, characterized in that the
Ausgangspulvergemisch einen oder mehreren der nachfolgend aufgeführten Stoffe enthält:Starting powder mixture contains one or more of the substances listed below:
a) 5 - 20 Gew.-% Zn, 0, 1 - 5 Gew.-% von AI oder Sn, usw.; b) 5 - 30 Gew.-% Werkzeugstahl Typ M35 oder Typ T1 5, Ni-Cr-Si-Fe-B-Cu-Mo.a) 5-20% by weight of Zn, 0.1-1% by weight of Al or Sn, etc .; b) 5 - 30% by weight tool steel type M35 or type T1 5, Ni-Cr-Si-Fe-B-Cu-Mo.
25. Werkstoff nach Anspruch 1 und einem oder mehreren der Ansprüche 18 - 23, dadurch gekennzeichnet, daß das Ausgangs¬ pulvergemisch Kombinationen der Stoffe bzw. der Stoffgemische der Ansprüche 18 - 23 enthält:25. Material according to claim 1 and one or more of claims 18-23, characterized in that the starting powder mixture contains combinations of the substances or the substance mixtures of claims 18-23:
26. Verwendung eines Werkstoffes gemäß Anspruch 1 und einem oder mehreren der Ansprüche 19 - 24 zur Herstellung eines Ventilsitzringes oder Ventilführungen, dessen Wärmeleitfähigkeit mindestens 100 W/m k beträgt. 26. Use of a material according to claim 1 and one or more of claims 19-24 for the production of a valve seat ring or valve guides, the thermal conductivity of which is at least 100 W / m k.
EP97905071A 1996-02-21 1997-02-21 Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear Expired - Lifetime EP0881958B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19606270 1996-02-21
DE19606270A DE19606270A1 (en) 1996-02-21 1996-02-21 Material for powder metallurgical production of molded parts, especially valve seat rings with high thermal conductivity and high wear and corrosion resistance
PCT/EP1997/000837 WO1997030808A1 (en) 1996-02-21 1997-02-21 Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear

Publications (2)

Publication Number Publication Date
EP0881958A1 true EP0881958A1 (en) 1998-12-09
EP0881958B1 EP0881958B1 (en) 2001-05-30

Family

ID=7785898

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97905071A Expired - Lifetime EP0881958B1 (en) 1996-02-21 1997-02-21 Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear

Country Status (5)

Country Link
US (1) US6039785A (en)
EP (1) EP0881958B1 (en)
JP (1) JP4272706B2 (en)
DE (2) DE19606270A1 (en)
WO (1) WO1997030808A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108026800A (en) * 2015-10-02 2018-05-11 株式会社理研 Sinter valve seat

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19925300A1 (en) * 1999-06-02 2000-12-07 Mahle Ventiltrieb Gmbh Cast material with high warm hardness
DE102012013226A1 (en) 2012-07-04 2014-01-09 Bleistahl-Produktions Gmbh & Co Kg High heat conducting valve seat ring
DE102013021059A1 (en) 2013-12-18 2015-06-18 Bleistahl-Produktions Gmbh & Co Kg. Double / triple layer valve guide
CN105940127B (en) * 2014-02-10 2021-03-19 日产自动车株式会社 Sliding mechanism
WO2015198932A1 (en) 2014-06-27 2015-12-30 株式会社リケン Sintered valve seat and method for manufacturing same
CN104561638B (en) * 2015-01-04 2016-06-08 河南科技大学 A kind of Al2O3The preparation method of dispersed and strengthened copper-based composite material
DE102016109539A1 (en) * 2016-05-24 2017-12-14 Bleistahl-Produktions Gmbh & Co Kg. Valve seat ring
WO2018179590A1 (en) 2017-03-28 2018-10-04 株式会社リケン Sintered valve seat
DE102018209682A1 (en) * 2018-06-15 2019-12-19 Mahle International Gmbh Process for the manufacture of a powder metallurgical product
CN109825733B (en) * 2019-03-11 2021-02-19 中南大学 Short-process preparation method of dispersion-strengthened copper alloy
KR20210104418A (en) * 2020-02-17 2021-08-25 현대자동차주식회사 A outer ring for variable oil pump and manufacturing method thereof
US11473456B2 (en) * 2020-09-15 2022-10-18 GM Global Technology Operations LLC Cylinder head valve seat with high thermal conductivity and multiple material cross-section

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3578443A (en) * 1969-01-21 1971-05-11 Massachusetts Inst Technology Method of producing oxide-dispersion-strengthened alloys
JPS55122841A (en) * 1979-03-14 1980-09-20 Taiho Kogyo Co Ltd Sliding material
DE3130920A1 (en) * 1980-09-04 1982-04-01 General Electric Co., Schenectady, N.Y. "ELIGIBLE COPPER ALLOYS"
JPS59145756A (en) * 1983-02-08 1984-08-21 Hitachi Powdered Metals Co Ltd Manufacture of sintered alloy for member of control valve mechanism of internal-combustion engine
US4752334A (en) * 1983-12-13 1988-06-21 Scm Metal Products Inc. Dispersion strengthened metal composites
DE3838461A1 (en) * 1988-11-12 1990-05-23 Krebsoege Gmbh Sintermetall POWDER METALLURGICAL MATERIAL BASED ON COPPER AND ITS USE
SE468466B (en) * 1990-05-14 1993-01-25 Hoeganaes Ab ANNUAL-BASED POWDER AND NUTRITION-RESISTANT HEATHOLD SOLID COMPONENT MANUFACTURED FROM THIS AND THE MANUFACTURING COMPONENT
JPH083133B2 (en) * 1990-07-12 1996-01-17 日立粉末冶金株式会社 Outboard motor valve seat material and manufacturing method thereof
JPH05179232A (en) * 1991-12-26 1993-07-20 Toshiba Tungaloy Co Ltd Sintered metallic friction material for brake
US5296189A (en) * 1992-04-28 1994-03-22 International Business Machines Corporation Method for producing metal powder with a uniform distribution of dispersants, method of uses thereof and structures fabricated therewith
DE4232432A1 (en) * 1992-09-28 1994-03-31 Krebsoege Gmbh Sintermetall Powder metallurgy connecting rod - has at least powder metallurgy big-end bearing forming part of compound connecting rod structure
US5551970A (en) * 1993-08-17 1996-09-03 Otd Products L.L.C. Dispersion strengthened copper
EP0769635A1 (en) * 1995-10-20 1997-04-23 Tokyo Yogyo Kabushiki Kaisha Brake lining material for heavy-load braking device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9730808A1 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108026800A (en) * 2015-10-02 2018-05-11 株式会社理研 Sinter valve seat
EP3358156A4 (en) * 2015-10-02 2019-07-31 Kabushiki Kaisha Riken Sintered valve seat

Also Published As

Publication number Publication date
US6039785A (en) 2000-03-21
JP2001500567A (en) 2001-01-16
JP4272706B2 (en) 2009-06-03
DE19606270A1 (en) 1997-08-28
DE59703672D1 (en) 2001-07-05
EP0881958B1 (en) 2001-05-30
WO1997030808A1 (en) 1997-08-28

Similar Documents

Publication Publication Date Title
DE3327282C2 (en) Sintered alloy for valve seats
DE10046956C2 (en) Thermally applied coating for piston rings made of mechanically alloyed powders
DE102005022104B4 (en) Sintered iron based alloy with dispersed hard particles
DE102006048442B4 (en) A method of manufacturing a wear resistant sintered element, a sintered valve seat, and manufacturing methods therefor
DE102006014291B4 (en) Wear-resistant sintered element and production method thereof
DE102012018964B4 (en) Iron-based sintered body and process for its preparation
DE3224419A1 (en) METHOD FOR PRODUCING A CAM-CAMSHAFT ASSEMBLY
DE3048035A1 (en) WEAR-RESISTANT SINTER ALLOY AND METHOD FOR THE PRODUCTION THEREOF
DE3232001C2 (en) Wear-resistant sintered alloy, process for their production and their use
EP0881958A1 (en) Material for the powder-metallurgical production of shaped parts, in particular valve seat rings or valve guides with high resistance to wear
EP3463722A1 (en) Valve seat ring
DE19506340C2 (en) Sintered alloy and method for producing a sintered body therefrom
DE3744550C2 (en)
DE3224420C2 (en) Process for the aftertreatment of a sintered sliding element
DE19715708B4 (en) Wear resistant sintered alloy at high temperature
EP3409801B1 (en) Solid particles prepared by means of powder metallurgy, hard particle containing composite material, use of a composite material and method for manufacturing a component from a composite material
DE2415035B2 (en) Process for the powder-metallurgical production of a sliding piece of high strength, in particular a crown seal for rotary piston machines
DE60300728T2 (en) Iron-based sintered alloy for use as a valve seat
DE10236015B4 (en) Sintered alloy for a valve seat with excellent wear resistance and a method of manufacturing the same
DE3730082C2 (en)
DE19708197B4 (en) Sintered sliding element and method for its production
EP0719349B1 (en) Process of producing sintered articles
DE10336407B4 (en) Powder metallurgically produced bearing parts for turbochargers and method for producing such bearing parts
DE19513911C2 (en) Bearing parts for use at high temperatures
DE19724899C2 (en) Highly heat-resistant magnesium material, especially for piston construction

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19980826

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

17Q First examination report despatched

Effective date: 20000530

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE

REF Corresponds to:

Ref document number: 59703672

Country of ref document: DE

Date of ref document: 20010705

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20160226

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 59703672

Country of ref document: DE