EP2047004B1 - Nickel-based alloy - Google Patents

Nickel-based alloy Download PDF

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EP2047004B1
EP2047004B1 EP07785601A EP07785601A EP2047004B1 EP 2047004 B1 EP2047004 B1 EP 2047004B1 EP 07785601 A EP07785601 A EP 07785601A EP 07785601 A EP07785601 A EP 07785601A EP 2047004 B1 EP2047004 B1 EP 2047004B1
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nickel
mass
max
master alloy
alloy according
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EP2047004A1 (en
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Jutta KLÖWER
Frank Scheide
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VDM Metals GmbH
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ThyssenKrupp VDM GmbH
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/058Alloys based on nickel or cobalt based on nickel with chromium without Mo and W

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  • the invention relates to a nickel-based alloy with silicon, aluminum and reactive elements as alloying constituents.
  • Nickel-base alloys are used inter alia to produce electrodes of ignition elements for internal combustion engines. At wear of such electrodes are two damage mechanisms to consider, namely the high temperature corrosion and spark erosion.
  • the wear caused by high-temperature corrosion can be determined by mass loss measurements as well as by metallographic investigations after aging at given test temperatures.
  • Spark erosion is a material burn caused by the spark. At each flashover, a limited volume of material is melted out of the electrodes and partially evaporated.
  • various alloying elements are known in nickel-based alloys.
  • aluminum has a positive effect on the oxide layer formation.
  • reactive elements can improve the adhesion of the forming oxide layer and then increase the lifetime.
  • a nickel alloy has been disclosed consisting of (in mass%) about 0.2 to 3% Si, about 0.5% or less Mn, at least two metals selected from the group consisting of about 0.2 to 3% Cr , about 0.2 to 3% Al and about 0.01 to 1% Y, balance nickel.
  • nickel-based alloy which contains (in mass%) 1.8 to 2.2% silicon, 0.05 to 0.1% yttrium and / or hafnium and / or zirconium, 2 to 2.4% aluminum, Rest has nickel.
  • Such alloys can be processed only in difficult conditions with respect to the high aluminum and silicon contents and are therefore not very suitable for large-scale industrial use.
  • the object of the subject invention is to provide a nickel-based alloy, by which an increase in the life of components made therefrom by increasing the spark erosion and oxidation resistance at the same time good formability and weldability can be brought about.
  • This goal is achieved by a nickel-based alloy containing (in% by mass) al 1.2 - ⁇ 2.0% Si 1.2 - ⁇ 1.8% C 0.001 - 0.1% S 0.001 - 0.1% Cr 0.03 - 0.1% Mn 0.03 - 0.1% Cu Max. 0.1% Fe 0.02 - 0.2% mg 0.005 - 0.06% pb Max. 0.005% Y 0.05-0.15% and Hf 0.05-0.10% or Y 0.05-0.15% and La 0.05-0.10% or Y 0.05-0.15% and Hf 0.05-0.10% and La 0.05-0.10% Ni Remainder and production-related impurities.
  • Nickel-based alloy with (in% by mass)
  • Nickel-based alloy with (in% by mass)
  • Nickel-based alloy with (in% by mass)
  • the nickel-based alloy according to the invention is preferably usable as a material for electrodes of spark plugs for gasoline engines.
  • an improvement in the lifetime of electrode materials can be achieved by increasing the resistance to spark erosion and oxidation while at the same time providing good formability and weldability become.
  • the element Mg is of particular importance for the setting of sulfur, so that it is possible to selectively set low sulfur contents in the nickel-based alloy according to the invention.
  • Preferred aluminum contents are (in% by mass) in the range of 1.2-1.5%.
  • Preferred silicon contents are (in mass%) in the range between 1.2 and 1.8%, in particular between 1.2 and 1.5%, while the preferred Mg content (in% by mass) is between 0.008 and 0, 05% is set.
  • Table 1 shows a comparison of four inventive laboratory batches in comparison with two related to the prior art large-scale batches.
  • the laboratory batch 1132 represents an example in which the reactive elements Y + Hf are given in the nickel-based alloy according to the invention.
  • Lab batch 1140 shows an example in which the reactive elements Y + La are present in the alloy of the invention.
  • the two comparative alloys show flaking at 900 ° C of the pre-built oxide layer. Although this also applies to the alloys according to the invention at 1,000 ° C., it does not apply to the same extent as in the case of the comparative alloys.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Spark Plugs (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
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Abstract

Nickel-based alloy, consisting of (in % by mass) Al 1.2-<2.0% Si 1.2-<1.8% C 0.001-0.1% S 0.001-0.1% Cr 0.03-0.1% Mn 0.03-0.1% Cu max. 0.1% Fe 0.02-0.2% Mg 0.005-0.06% Pb max. 0.005% Y 0.05-0.15% and Hf 0.05-0.10% or Y 0.05-0.15% and La 0.05-0.10% or Y 0.05-0.15% and Hf 0.05-0.10% and La 0.05-0.10% Ni remainder together with manufacturing-related impurities.

Description

Die Erfindung betrifft eine Nickelbasislegierung mit Silizium, Aluminium und reaktiven Elementen als Legierungsbestandteile.The invention relates to a nickel-based alloy with silicon, aluminum and reactive elements as alloying constituents.

Nickelbasislegierungen werden unter anderem dazu eingesetzt, Elektroden von Zündelementen für Verbrennungskraftmaschinen zu erzeugen. An Verschleiß derartiger Elektroden sind zwei Schadensmechanismen zu betrachten, nämlich die Hochtemperaturkorrosion und die Funkenerrosion.Nickel-base alloys are used inter alia to produce electrodes of ignition elements for internal combustion engines. At wear of such electrodes are two damage mechanisms to consider, namely the high temperature corrosion and spark erosion.

Der Verschleiß durch Hochtemperaturkorrosion lässt sich durch Masseverlustmessungen sowie durch metallographische Untersuchungen nach Auslagerung bei vorgegebenen Prüftemperaturen bestimmen.The wear caused by high-temperature corrosion can be determined by mass loss measurements as well as by metallographic investigations after aging at given test temperatures.

Funkenerrosion ist ein Materialabbrand, der durch den Zündfunken verursacht wird. Bei jedem Funkenüberschlag wird ein begrenztes Materialvolumen aus den Elektroden herausgeschmolzen und teilweise verdampft.Spark erosion is a material burn caused by the spark. At each flashover, a limited volume of material is melted out of the electrodes and partially evaporated.

Für beide Schadensmechanismen ist die Art der Oxidschichtausbildung von besonderer Bedeutung.For both damage mechanisms, the type of oxide layer formation is of particular importance.

Um eine optimale Oxidschichtausbildung für den konkreten Anwendungsfall zu erreichen, sind bei Nickelbasislegierungen verschiedene Legierungselemente bekannt. So wirkt sich zum Beispiel Aluminium positiv auf die Oxidschichtausbildung aus. Auch ist bekannt, dass reaktive Elemente die Haftung der sich ausbildenden Oxidschicht verbessern können und dann die Lebensdauer erhöhen.In order to achieve an optimum oxide layer formation for the specific application, various alloying elements are known in nickel-based alloys. For example, aluminum has a positive effect on the oxide layer formation. It is also known that reactive elements can improve the adhesion of the forming oxide layer and then increase the lifetime.

Durch die GB-A 2031950 ist eine Nickellegierung bekannt geworden, bestehend aus (in Masse-%) etwa 0,2 bis 3 % Si, etwa 0,5 % oder weniger Mn, wenigstens zwei Metallen, ausgewählt aus der Gruppe bestehend aus etwa 0,2 bis 3 % Cr, etwa 0,2 bis 3 % Al und etwa 0,01 bis 1 % Y, Rest Nickel.By the GB-A 2031950 For example, a nickel alloy has been disclosed consisting of (in mass%) about 0.2 to 3% Si, about 0.5% or less Mn, at least two metals selected from the group consisting of about 0.2 to 3% Cr , about 0.2 to 3% Al and about 0.01 to 1% Y, balance nickel.

In der DE-A 102 24 891 wird eine Legierung auf Nickelbasis vorgeschlagen, welche (in Masse-%) 1,8 bis 2,2 % Silizium, 0,05 bis 0,1 % Yttrium und/oder Hafnium und/oder Zirkonium, 2 bis 2,4 % Aluminium, Rest Nickel aufweist. Derartige Legierungen lassen sich bezüglich der hohen Aluminium- und Siliziumgehalte nur unter schwierigen Bedingungen bearbeiten und sind somit für den technischen Großeinsatz wenig geeignet.In the DE-A 102 24 891 a nickel-based alloy is proposed which contains (in mass%) 1.8 to 2.2% silicon, 0.05 to 0.1% yttrium and / or hafnium and / or zirconium, 2 to 2.4% aluminum, Rest has nickel. Such alloys can be processed only in difficult conditions with respect to the high aluminum and silicon contents and are therefore not very suitable for large-scale industrial use.

Ziel des Erfindungsgegenstandes ist es, eine Nickelbasislegierung bereitzustellen, durch welche eine Erhöhung der Lebensdauer von daraus hergestellten Bauteilen durch Erhöhung der Funkenerrosions- und Oxidationsbeständigkeit bei gleichzeitig guter Umformbarkeit und Schweißbarkeit herbeiführbar ist.The object of the subject invention is to provide a nickel-based alloy, by which an increase in the life of components made therefrom by increasing the spark erosion and oxidation resistance at the same time good formability and weldability can be brought about.

Dieses Ziel wird erreicht durch eine Nickelbasislegierung, beinhaltend (in Masse-%) Al 1,2 - < 2,0 % Si 1,2 - < 1,8 % C 0,001 - 0,1 % S 0,001 - 0,1 % Cr 0,03 - 0,1 % Mn 0,03 - 0,1 % Cu max. 0,1 % Fe 0,02 - 0,2 % Mg 0,005 - 0,06 % Pb max. 0,005 % Y 0,05 - 0,15 % und Hf 0,05 - 0,10 % oder Y 0,05 - 0,15 % und La 0,05 - 0,10 % oder Y 0,05 - 0,15 % und Hf 0,05 - 0,10 % und La 0,05 - 0,10 % Ni Rest und herstellungsbedingte Verunreinigungen. This goal is achieved by a nickel-based alloy containing (in% by mass) al 1.2 - <2.0% Si 1.2 - <1.8% C 0.001 - 0.1% S 0.001 - 0.1% Cr 0.03 - 0.1% Mn 0.03 - 0.1% Cu Max. 0.1% Fe 0.02 - 0.2% mg 0.005 - 0.06% pb Max. 0.005% Y 0.05-0.15% and Hf 0.05-0.10% or Y 0.05-0.15% and La 0.05-0.10% or Y 0.05-0.15% and Hf 0.05-0.10% and La 0.05-0.10% Ni Remainder and production-related impurities.

Bevorzugte alternative Ausgestaltungen des Erfindungsgegenstandes sind den Unteransprüchen wie folgt zu entnehmen.Preferred alternative embodiments of the subject invention are set forth in the dependent claims as follows.

Nickelbasislegierung mit (in Masse-%)Nickel-based alloy with (in% by mass)

Alal 1,2 - < 2,0 %1.2 - <2.0% SiSi 1,2 - < 1,8 %1.2 - <1.8% CC 0,001 - 0,05 %0.001 - 0.05% SS 0,001 - 0,05 %0.001 - 0.05% CrCr 0,03 - 0,1 %0.03 - 0.1% MnMn 0,03 - 0,1 %0.03 - 0.1% CuCu max. 0,1 %Max. 0.1% FeFe 0,02 - 0,2 %0.02 - 0.2% Mgmg 0,005 bis 0,06 %0.005 to 0.06% Pbpb max. 0,005 %Max. 0.005% YY 0,10 - 0,15 % und Hf 0,05 - 0,10 %0.10 - 0.15% and Hf 0.05 - 0.10% NiNi Rest und herstellungsbedingte Verunreinigungen.Remainder and production-related impurities.

Nickelbasislegierung mit (in Masse-%)Nickel-based alloy with (in% by mass)

Alal 1,2 - < 2,01.2 - <2.0 SiSi 1,2 - < 1,8%1.2 - <1.8% CC 0,001 - 0,05 %0.001 - 0.05% SS 0,001 - 0,05 %0.001 - 0.05% CrCr 0,03 - 0,1 %0.03 - 0.1% MnMn 0,03-0,1 %0.03-0.1% CuCu max. 0,1 %Max. 0.1% FeFe 0,02- 0,2 %0.02-0.2% Mgmg 0,005 - 0,06 %0.005 - 0.06% Pbpb max. 0,005 %Max. 0.005% YY 0,10 - 0,15 % und La 0,05 bis 0,10 %0.10-0.15% and La 0.05-0.10% NiNi Rest und herstellungsbedingte Verunreinigungen.Remainder and production-related impurities.

Nickelbasislegierung mit (in Masse-%)Nickel-based alloy with (in% by mass)

Alal 1,2 - < 2,01.2 - <2.0 SiSi 1,2 - < 1,8 %1.2 - <1.8% CC 0,001 - 0,05 %0.001 - 0.05% SS 0,001 - 0,05 %0.001 - 0.05% CrCr 0,03 - 0,1 %0.03 - 0.1% MnMn 0,03 - 0,1 %0.03 - 0.1% CuCu max. 0,1 %Max. 0.1% FeFe 0,02 - 0,2 %0.02 - 0.2% Mgmg 0,005 - 0,06 %0.005 - 0.06% Pbpb max. 0,005 %Max. 0.005% YY 0,10 - 0,15 % und Hf 0,05 bis 0,10 % und La 0,05 - 0,10 %.0.10-0.15% and Hf 0.05-0.10% and La 0.05-0.10%.

Bezüglich der reaktiven Elemente sind somit drei Varianten denkbar, nämlich
Y + Hf,
Y + La sowie
Y + Hf + La.
With regard to the reactive elements, three variants are thus conceivable, namely
Y + Hf,
Y + La as well
Y + Hf + La.

Die erfindungsgemäße Nickelbasislegierung ist bevorzugt einsetzbar als Werkstoff für Elektroden von Zündkerzen für Benzinmotoren.The nickel-based alloy according to the invention is preferably usable as a material for electrodes of spark plugs for gasoline engines.

Durch gezielte Einstellung einerseits der Elemente Al, Si, Cr, Mn, Mg und andererseits der reaktiven Elemente Y, Hf, La in ihren jeweiligen Kombinationen kann eine Verbesserung der Lebensdauer von Elektrodenwerkstoffen durch Erhöhung der Funkenerrosions- und Oxidationsbeständigkeit bei gleichzeitig guter Umformbarkeit und Schweißbarkeit herbeigeführt werden.By selective adjustment of the elements Al, Si, Cr, Mn, Mg on the one hand and the reactive elements Y, Hf, La in their respective combinations on the other hand, an improvement in the lifetime of electrode materials can be achieved by increasing the resistance to spark erosion and oxidation while at the same time providing good formability and weldability become.

Dem Element Mg kommt bezüglich der Abbindung von Schwefel eine besondere Bedeutung zu, so dass hier gezielt geringe Schwefelgehalte in der erfindungsgemäßen Nickelbasislegierung eingestellt werden können.The element Mg is of particular importance for the setting of sulfur, so that it is possible to selectively set low sulfur contents in the nickel-based alloy according to the invention.

Bevorzugte Aluminiumgehalte werden (in Masse-%) gesehen im Bereich von 1,2 - 1,5 %.Preferred aluminum contents are (in% by mass) in the range of 1.2-1.5%.

Bevorzugte Siliziumgehalte werden (in Masse-%) gesehen im Bereich zwischen 1,2 und 1,8 %, insbesondere zwischen 1,2 und 1,5 %, während der bevorzugte Mg-Gehalt (in Masse-%) zwischen 0,008 und 0,05 % eingestellt wird.Preferred silicon contents are (in mass%) in the range between 1.2 and 1.8%, in particular between 1.2 and 1.5%, while the preferred Mg content (in% by mass) is between 0.008 and 0, 05% is set.

Tabelle 1 zeigt als Gegenüberstellung vier erfindungsgemäße Laborchargen im Vergleich mit zwei dem Stand der Technik zugehörigen großtechnischen Chargen.Table 1 shows a comparison of four inventive laboratory batches in comparison with two related to the prior art large-scale batches.

Die Laborcharge 1132 stellt ein Beispiel dar, bei welchem die reaktiven Elemente Y + Hf in der erfindungsgemäßen Nickelbasislegierung gegeben sind.The laboratory batch 1132 represents an example in which the reactive elements Y + Hf are given in the nickel-based alloy according to the invention.

Die Laborcharge 1140 zeigt ein Beispiel, bei welchem die reaktiven Elemente Y + La in der erfindungsgemäßen Legierung vorhanden sind.Lab batch 1140 shows an example in which the reactive elements Y + La are present in the alloy of the invention.

Die Laborchargen 1141 und 1142 offenbaren Beispiele, bei welchen als reaktive Elemente Y + La + Hf in der erfindungsgemäßen Nickelbasislegierung eingestellt wurden. Element LB 1132 LB 1140 LB 1141 LB 1142 NiCr2MnSi NiAI1Si1Y Ni 96,83 96,91 96,89 96,79 96,24 97,56 Si 1,47 1,36 1,36 1,42 0,49 0,96 Al 1,38 1,43 1,44 1,40 0,02 0,98 Zr Y 0,15 0,12 0,14 0,13 0,17 Hf 0,08 0,078 0,073 La 0,09 0,096 0,096 Ti 0,1 0,01 0,01 C 0,002 0,006 0,004 0,003 0,003 0,03 S 0,002 0,002 0,002 0,002 0,002 0,002 Co 0,04 0,05 Cu 0,01 0,01 Cr 0,04 0,03 0,06 0,04 1,57 0,01 Zr 0,01 Mg 0,02 0,03 0,01 0,03 0,02 0,04 Mn 0,06 0,03 0,03 0,06 1,48 0,02 Fe 0,03 0,03 0,03 0,04 0,08 0,13 Pb 0,001 0,001 Die Figuren 1 und 2 zeigen für die Legierungen gemäß Tabelle 1 Masseverlustuntersuchungen bei Temperaturen von einerseits 900° C und andererseits 1.000° C.Laboratory batches 1141 and 1142 disclose examples in which Y + La + Hf were set as reactive elements in the nickel-based alloy of the present invention. element LB 1132 LB 1140 LB 1141 LB 1142 NiCr2MnSi NiAI1Si1Y N i 96.83 96.91 96.89 96.79 96.24 97.56 Si 1.47 1.36 1.36 1.42 0.49 0.96 al 1.38 1.43 1.44 1.40 0.02 0.98 Zr Y 0.15 0.12 0.14 0.13 0.17 Hf 0.08 0.078 0.073 La 0.09 0.096 0.096 Ti 0.1 0.01 0.01 C 0,002 0,006 0,004 0,003 0,003 0.03 S 0,002 0,002 0,002 0,002 0,002 0,002 Co 0.04 0.05 Cu 0.01 0.01 Cr 0.04 0.03 0.06 0.04 1.57 0.01 Zr 0.01 mg 0.02 0.03 0.01 0.03 0.02 0.04 Mn 0.06 0.03 0.03 0.06 1.48 0.02 Fe 0.03 0.03 0.03 0.04 0.08 0.13 pb 0.001 0.001 The Figures 1 and 2 show for the alloys according to Table 1 mass loss studies at temperatures of one hand 900 ° C and on the other hand 1000 ° C.

Die beiden Vergleichslegierungen zeigen bereits bei 900°C Abplatzungen der vorab aufgebauten Oxidschicht. Bei 1.000°C trifft dies zwar auch auf die erfindungsgemäßen Legierungen zu, nicht jedoch in gleichem Umfang, wie bei den Vergleichslegierungen.The two comparative alloys show flaking at 900 ° C of the pre-built oxide layer. Although this also applies to the alloys according to the invention at 1,000 ° C., it does not apply to the same extent as in the case of the comparative alloys.

Claims (11)

  1. A nickel master alloy composed of (in % by mass) Al 1.2 - < 2.0% Si 1.2 - < 1.8% C 0.001 - 0.1 % S 0.001 - 0.1 % Cr 0.03-0.1% Mn 0.03-0.1% Cu max. 0.1 % Fe 0.02 - 0.2% Mg 0.005 - 0.06% Pb max.0.005% Y 0.05 - 0.15% and Hf 0.05 - 0.10% or Y 0.05 - 0.15% and La 0.05 - 0.10% or Y 0.05 - 0.15% and Hf 0.05 - 0.10% and La 0.05 - 0.10% Ni rest and elaboration dependent impurities.
  2. A nickel master alloy according to claim 1 comprising (in % by mass) Al 1.2 - < 2.0% Si 1.2 - < 1.8% C 0.001 - 0.05% S 0.001 - 0.05% Cr 0.03-0.1% Mn 0.03-0.1% Cu max. 0.1 % Fe 0.02 - 0.2% Mg 0.005 - 0.06% Pb max.0.005% Y 0.10 - 0.15% and Hf 0.05 - 0.10% Ni rest and elaboration dependent impurities.
  3. A nickel master alloy according to claim 1 comprising (in % by mass) Al 1.2 - < 2.0% Si 1.2 - < 1.8% C 0.001 - 0.05% S 0.001 - 0.05% Cr 0.03-0.1% Mn 0.03-0.1% Cu max. 0.1 % Fe 0.02 - 0.2% Mg 0.005 - 0.06% Pb max.0.005% Y 0.10 - 0.15% and La 0.05 - 0.10% Ni rest and elaboration dependent impurities.
  4. A nickel master alloy according to claim 1 comprising (in % by mass) Al 1.2 - < 2.0% Si 1.2 - < 1.8% C 0.001 - 0.05% S 0.001 - 0.05% Cr 0.03-0.1% Mn 0.03-0.1% Cu max. 0.1 % Fe 0.02 - 0.2% Mg 0.005 - 0.06% Pb max.0.005% Y 0.10 - 0.15% and Hf 0.05 - 0.10% and La 0.05 - 0.10%.
  5. A nickel master alloy according to one of the claims 1 through 4 comprising a content of (in % by mass) Al 1.2 - 1.5% Si 1.2 - 1.5%.
  6. A nickel master alloy according to one of the claims 1 through 5 comprising a content of (in % by mass) Mg 0.008 - 0.05%.
  7. A nickel master alloy according to one of the claims 1 through 6 comprising a content of (in % by mass) Y + Hf 0.11 - 0.18%.
  8. A nickel master alloy according to one of the claims 1 through 6 comprising a content of (in % by mass) Y + La 0.11 - 0.18%.
  9. A nickel master alloy according to one of the claims 1 through 6 comprising a
    content of (in % by mass) Y + Hf+La 0.18 - 0.22%.
  10. A nickel master alloy according to one of the claims 1 through 9 comprising a content of (in % by mass) Y + Mg 0.11 - 0.13%.
  11. Use of the nickel master alloy according to one of the claims 1 through 10 as electrode material of ignition elements of combustion engines.
EP07785601A 2006-07-29 2007-07-06 Nickel-based alloy Active EP2047004B1 (en)

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Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9137482B2 (en) * 2010-03-31 2015-09-15 Verizon Patent And Licensing Inc. Methods and systems for resolution-based modification of recording instructions associated with a scheduled recording of a media content instance
DE102010024488B4 (en) * 2010-06-21 2012-04-26 Thyssenkrupp Vdm Gmbh Nickel-based alloy
EP2634871B1 (en) * 2010-10-26 2019-09-04 NGK Spark Plug Co., Ltd. Spark plug
JP5697484B2 (en) * 2011-02-25 2015-04-08 株式会社デンソー Spark plug electrode material
DE102011007532A1 (en) * 2011-04-15 2012-10-18 Robert Bosch Gmbh A spark plug electrode material and spark plug, and a method of manufacturing the spark plug electrode material
EP2698439B1 (en) * 2012-08-17 2014-10-01 Alstom Technology Ltd Oxidation resistant nickel alloy
DE102013004365B4 (en) * 2013-03-14 2015-09-24 VDM Metals GmbH Nickel-based alloy with silicon, aluminum and chrome
DE102013005677B3 (en) 2013-04-03 2014-07-17 Geräte- und Pumpenbau GmbH Dr. Eugen Schmidt Shaft bearing with shaft seal, especially for water pumps in motor vehicles
US20170009704A1 (en) * 2015-07-06 2017-01-12 Rohr, Inc. Thrust reverser staggered translating sleeve

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB943141A (en) * 1961-01-24 1963-11-27 Rolls Royce Method of heat treating nickel alloys
US4013459A (en) * 1975-10-24 1977-03-22 Olin Corporation Oxidation resistant nickel base alloys
GB1542283A (en) * 1975-12-19 1979-03-14 Draftex Dev Ag Channel-shaped sealing strips
JPS6043897B2 (en) * 1978-09-07 1985-10-01 日本特殊陶業株式会社 Nickel alloy for spark plug electrodes
US5204059A (en) * 1988-07-25 1993-04-20 Mitsubishi Metal Corporation Ni base alloy for spark plug electrodes of internal combustion engines
JP2550158B2 (en) * 1988-07-25 1996-11-06 三菱マテリアル株式会社 Spark plug electrode material for internal combustion engines
JPH0445239A (en) * 1990-06-08 1992-02-14 Toshiba Corp Alloy for spark plug
EP1090155A1 (en) * 1998-06-30 2001-04-11 Federal-Mogul Corporation Spark plug electrode alloy
CA2348145C (en) * 2001-05-22 2005-04-12 Surface Engineered Products Corporation Protective system for high temperature metal alloys
DE10224891A1 (en) * 2002-06-04 2003-12-18 Bosch Gmbh Robert Nickel alloy suitable for internal combustion engine spark plug electrodes, contains silicon and aluminum with yttrium, hafnium or zirconium
JP4769070B2 (en) * 2005-01-31 2011-09-07 日本特殊陶業株式会社 Spark plug for internal combustion engine

Also Published As

Publication number Publication date
RU2399690C1 (en) 2010-09-20
EP2047004A1 (en) 2009-04-15
JP5273620B2 (en) 2013-08-28
DE102006035111B4 (en) 2010-01-14
DE102006035111A1 (en) 2008-02-07
JP2009544855A (en) 2009-12-17
PL2047004T3 (en) 2011-10-31
WO2008014741A1 (en) 2008-02-07
ATE510034T1 (en) 2011-06-15
US20100003163A1 (en) 2010-01-07
BRPI0715515A2 (en) 2013-03-05
BRPI0715515B1 (en) 2015-08-04
MX2009000987A (en) 2009-02-06

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