DE102019129128A1 - Engine valve - Google Patents
Engine valve Download PDFInfo
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- DE102019129128A1 DE102019129128A1 DE102019129128.3A DE102019129128A DE102019129128A1 DE 102019129128 A1 DE102019129128 A1 DE 102019129128A1 DE 102019129128 A DE102019129128 A DE 102019129128A DE 102019129128 A1 DE102019129128 A1 DE 102019129128A1
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- Prior art keywords
- layer
- adhesion promoter
- nickel
- inlet
- regulator valve
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/129—Flame spraying
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/14—Metallic material, boron or silicon
- C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
- C23C14/165—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/137—Spraying in vacuum or in an inert atmosphere
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
- C25D5/14—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium two or more layers being of nickel or chromium, e.g. duplex or triplex layers
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L3/00—Lift-valve, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces; Parts or accessories thereof
- F01L3/02—Selecting particular materials for valve-members or valve-seats; Valve-members or valve-seats composed of two or more materials
- F01L3/04—Coated valve members or valve-seats
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L2301/00—Using particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L2303/00—Manufacturing of components used in valve arrangements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L2820/00—Details on specific features characterising valve gear arrangements
- F01L2820/01—Absolute values
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Electrochemistry (AREA)
- Physical Vapour Deposition (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Abstract
Es wird offenbart ein Ein- bzw. Auslasstellerventil (2), das umfasst einen Ventilschaft (4), mindestens eine im Bereich des Ventilschafts (4) aufgebrachte Haftvermittlerschicht (8) und eine auf der mindestens einen Haftvermittlerschicht (8) aufgebrachte Hartchromschicht (10) auf Basis von Chrom (III).An inlet and outlet regulator valve (2) is disclosed which comprises a valve stem (4), at least one adhesive layer (8) applied in the area of the valve stem (4) and a hard chrome layer (10) applied to the at least one adhesive layer (8). based on chromium (III).
Description
Die vorliegende Erfindung betrifft ein Motorventil. Motorventile können Ein- oder Auslassventile sein, die den Verbrennungsraum abdichten, den Gaswechsel im Motor steuern und somit thermisch und mechanisch hoch beanspruchte Bauteile sein, die zusätzlich auch korrosiven Einflüssen ausgesetzt sind. Die mechanische Beanspruchung entsteht infolge der Durchbiegung des Ventiltellers unter Zünddruck und durch das Aufsetzen beim Schließen (Stoßbeanspruchung).The present invention relates to an engine valve. Engine valves can be inlet or outlet valves that seal the combustion chamber, control the gas exchange in the engine and thus be thermally and mechanically highly stressed components that are also exposed to corrosive influences. The mechanical stress arises as a result of the deflection of the valve disk under ignition pressure and through contact when closing (impact stress).
Ein derartiges Motorventil ist beispielsweise bekannt aus der europäischen Patentschrift
Derartige Motorventile, insbesondere hochbelastete Motorventile, sind im Schaftbereich hartverchromt oder nitriert. Das derzeit am häufigsten verwendete galvanische Hartverchromungsverfahren basiert auf Chrom (VI). Dieses Metall darf jedoch nur noch mit Genehmigung der Europäischen Chemikalienagentur (ECHA) verwendet werden, da das im Prozess verwendete Chrom (VI) ein Gefahrenstoff ist.Such engine valves, in particular highly stressed engine valves, are hard chrome-plated or nitrided in the shaft area. The most frequently used galvanic hard chrome plating process is based on chromium (VI). However, this metal may only be used with the approval of the European Chemicals Agency (ECHA), as the chromium (VI) used in the process is a hazardous substance.
Vor diesem Hintergrund ist es daher die Aufgabe der Erfindung, ein verbessertes Motorventil ohne Gefahrenstoffverwendung bei der Herstellung bereitzustellen.Against this background, it is therefore the object of the invention to provide an improved engine valve without the use of hazardous substances during manufacture.
Diese Aufgabe wird erfindungsgemäß gelöst durch ein Motorventil gemäß Anspruch 1.This object is achieved according to the invention by an engine valve according to claim 1.
Das erfindungsgemäße Ein- bzw. Auslasstellerventil umfasst einen Ventilschaft, mindestens eine im Bereich des Ventilschafts aufgebrachte Haftvermittlerschicht und eine auf der mindestens einen Haftvermittlerschicht aufgebrachte Hartchromschicht auf Basis von Chrom (III), wobei Chrom (III) kein Gefahrenstoff ist.The inlet and outlet valve according to the invention comprises a valve stem, at least one adhesion promoter layer applied in the area of the valve stem and a hard chrome layer based on chromium (III) applied to the at least one adhesion promoter layer, chromium (III) not being a hazardous substance.
Bevorzugt weist die mindestens eine Haftvermittlerschicht Nickel, Silizium, Wolfram und/oder Kobalt auf und ist bevorzugt durch Sputtern aufgebracht. Dadurch wird der Ventilschaft thermisch gering belastet und eine hohe Haftfestigkeit erzielt.The at least one adhesion promoter layer preferably has nickel, silicon, tungsten and / or cobalt and is preferably applied by sputtering. As a result, the valve stem is subjected to low thermal loads and a high level of adhesive strength is achieved.
Bevorzugt weist die mindestens eine Haftvermittlerschicht Silizium und/oder Wolfram auf, bevorzugt als Tetrafluorsilan- oder Wolframhexafluoridhaltiges Gas, und ist bevorzugt durch plasmaunterstützte chemische Gasphasenabscheidung mit einer Schichtdicke von 0,5-3µm, bevorzugt 1-2µm, besonders bevorzugt 1,25-1,75µm aufgebracht. Dadurch wird ein hoher Korrosionsschutz aufgrund der dichten Struktur erzielt.The at least one adhesion promoter layer preferably has silicon and / or tungsten, preferably as a gas containing tetrafluorosilane or tungsten hexafluoride, and is preferably by means of plasma-assisted chemical vapor deposition with a layer thickness of 0.5-3 μm, preferably 1-2 μm, particularly preferably 1.25-1 , 75 µm applied. As a result, a high level of protection against corrosion is achieved due to the dense structure.
Bevorzugt weist die mindestens eine Haftvermittlerschicht MCrAlY auf, wobei der Werkstoff M entweder Kobalt oder Nickel oder einer Kombination beider Werkstoffe entspricht und Aufbringen bevorzugt durch Hochgeschwindigkeitsflammspritzen oder Vakuumplasmaspritzen mit einer Schichtdicke von 20-100µm, bevorzugt 30-70µm, besonders bevorzugt 40-60µm. Eine Beständigkeit gegen Heißkorrosion, Oxidation und Sulfidierung des Ventilschaftes wird dadurch gewährleistet.The at least one adhesion promoter layer preferably has MCrAlY, the material M corresponding to either cobalt or nickel or a combination of both materials and application preferably by high-speed flame spraying or vacuum plasma spraying with a layer thickness of 20-100 μm, preferably 30-70 μm, particularly preferably 40-60 μm. This ensures that the valve stem is resistant to hot corrosion, oxidation and sulphidation.
Bevorzugt weist die mindestens eine Haftvermittlerschicht Halbmetalle auf oder, wenn mindestens zwei Haftvermittlerschichten vorhanden sind, eine metallische Schicht als eine davon, die bevorzugt durch physikalische Gasphasenabscheidung durch Magnetronsputtern oder Hochenergieimpuls-Magnetronsputtern mit einer Schichtdicke von 0,5-15 µm, bevorzugt 1-10µm, besonders bevorzugt 1,5-7,5µm aufgebracht sind. Durch das höhere Ionisierungsvermögen der Elektronen wird die Sputterrate erhöht, d.h. deutlich höhere Beschichtungsraten bei gleichem Prozessdruck. Da das Schichtwachstum und somit die Schichteigenschaften neben der Temperatur vor allem vom Prozessdruck abhängig ist, hat man bei gleichen Wachstumsraten einen geringeren Prozessdruck und dadurch eine dichtere Schicht.The at least one adhesion promoter layer preferably has semimetals or, if at least two adhesion promoter layers are present, a metallic layer as one of them, which is preferably produced by physical vapor deposition by magnetron sputtering or high-energy pulse magnetron sputtering with a layer thickness of 0.5-15 μm, preferably 1-10 μm , particularly preferably 1.5-7.5 µm are applied. The higher ionization capacity of the electrons increases the sputtering rate, i.e. significantly higher coating rates with the same process pressure. Since the layer growth and thus the layer properties depend primarily on the process pressure in addition to the temperature, one has a lower process pressure and thus a denser layer with the same growth rates.
Bevorzugt weist die mindestens eine Haftvermittlerschicht Kupfer oder galvanisch abgeschiedenen oder elementaren Nickel auf, wobei bevorzugt das Kupfer oder Nickel nach einem Nickel-Strike Verfahren galvanisch abgeschieden ist. Diese Haftvermittlerschicht ist eine ideale Ausgangsbasis für weitere Schichten durch die sehr gute Haftfestigkeit, insbesondere für hochlegierte Stähle und Edelstähle.The at least one adhesion promoter layer preferably has copper or electrodeposited or elemental nickel, the copper or nickel preferably being electrodeposited using a nickel strike process. This adhesion promoter layer is an ideal starting point for further layers due to the very good adhesive strength, especially for high-alloy steels and stainless steels.
Bevorzugt weist die mindestens eine Haftvermittlerschicht galvanisch abgeschiedene Halbedelmetalle auf, bevorzugt Kupfer statt Nickel und bevorzugt mit einer Schichtdicke von 0,25-4µm, bevorzugt 0,5-2µm, besonders bevorzugt 0,75-1,5µm, wodurch ein erhöhter Korrosionsschutz erhalten wird.The at least one adhesion promoter layer preferably has electrodeposited semi-precious metals, preferably copper instead of nickel and preferably with a layer thickness of 0.25-4 μm, preferably 0.5-2 μm, particularly preferably 0.75-1.5 μm, whereby increased corrosion protection is obtained .
Bevorzugt ist die mindestens eine Haftvermittlerschicht durch Aluminieren für hohe Temperaturbeständigkeit und Korrosionsschutz aufgebracht.The at least one adhesion promoter layer is preferably applied by aluminizing for high temperature resistance and corrosion protection.
Bevorzugt ist eine Modifikationsschicht entweder zwischen der mindestens einen Haftvermittlerschicht und der Hartchromschicht oder zwischen dem Grundmaterial des Ventilschafts und der mindestens einen Haftvermittlerschicht vorgesehen, die durch bevorzugt Nickel-Strike Behandlung mit einer Schichtdicke von 0,3-1,5µm, bevorzugt 0,5-1µm, besonders bevorzugt 0,5-0,8µm aufgebracht ist. Dadurch wird eine ideale Ausgangsbasis für weitere Schichten durch die sehr gute Haftfestigkeit, insbesondere für hochlegierte Stähle und Edelstähle, erzeugt.A modification layer is preferably provided either between the at least one adhesion promoter layer and the hard chrome layer or between the base material of the valve stem and the at least one adhesion promoter layer, which is preferably coated with a nickel strike with a layer thickness of 0.3-1.5 μm, preferably 0.5 μm. 1 μm, particularly preferably 0.5-0.8 μm, is applied. This creates an ideal starting point for further layers due to the very good adhesive strength, especially for high-alloy steels and stainless steels.
Bevorzugt ist die Hartchromschicht mit einer Schichtdicke von 0,5-75µm, bevorzugt 1-50µm, besonders bevorzugt 5-40µm galvanisch abgeschieden, wodurch die tribologischen Eigenschaften verbessert werden und der Ventilschaft chemisch inert und umweltkonform ist.The hard chrome layer is preferably electrodeposited with a layer thickness of 0.5-75 μm, preferably 1-50 μm, particularly preferably 5-40 μm, whereby the tribological properties are improved and the valve stem is chemically inert and environmentally compatible.
Bevorzugt sind mindestens 2 Haftvermittlerschichten vorgesehen, die unterschiedlich aufgebaut sind, um die Haftfestigkeit weiter zu verbessern.At least 2 adhesion promoter layers are preferably provided, which are structured differently in order to further improve the adhesive strength.
Bevorzugt sind die mindestens eine Haftvermittlerschicht, Modifikationsschicht und/oder Hartchromschicht mit Kupfer und/oder galvanisch abgeschiedenem oder elementaren Nickel beschichtet, wobei bevorzugt das Kupfer oder der Nickel nach einem Nickel-Strike Verfahren mit einer Schichtdicke von 0,25-4µm, bevorzugt 0,5-2µm, besonders bevorzugt 0,75-1,5µm galvanisch abgeschieden ist. Die Ausgangsbasis für weitere Schichten ist somit ideal durch die sehr gute Haftfestigkeit, insbesondere für hochlegierte Stähle und Edelstähle. The at least one adhesion promoter layer, modification layer and / or hard chrome layer are preferably coated with copper and / or electrodeposited or elemental nickel, with the copper or nickel preferably being coated using a nickel strike process with a layer thickness of 0.25-4 μm, preferably 0, 5-2 μm, particularly preferably 0.75-1.5 μm, is electrodeposited. The starting point for further layers is therefore ideal due to the very good adhesive strength, especially for high-alloy steels and stainless steels.
Weitere Vorteile und Anwendungsmöglichkeiten der vorliegenden Erfindung ergeben sich aus der nachfolgenden Beschreibung der Erfindung in Verbindung mit der Zeichnung.Further advantages and possible applications of the present invention emerge from the following description of the invention in conjunction with the drawing.
Eine erste Ausführungsform der Haftvermittlerschicht
Eine zweite Ausführungsform der Haftvermittlerschicht
Eine dritte Ausführungsform der Haftvermittlerschicht
Eine vierte Ausführungsform der Haftvermittlerschicht
Eine fünfte Ausführungsform der Haftvermittlerschicht
Eine sechste Ausführungsform der Haftvermittlerschicht
Eine sechste Ausführungsform der Haftvermittlerschicht
In einer weiteren Ausführungsform sind mindestens 2 unterschiedlich aufgebaute Haftvermittlerschichten
Die Hartchromschicht
ZITATE ENTHALTEN IN DER BESCHREIBUNGQUOTES INCLUDED IN THE DESCRIPTION
Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list of the documents listed by the applicant was generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.
Zitierte PatentliteraturPatent literature cited
- EP 2215334 B1 [0002]EP 2215334 B1 [0002]
- EP 0576190 A1 [0002]EP 0576190 A1 [0002]
Claims (12)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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DE102019129128.3A DE102019129128A1 (en) | 2019-10-29 | 2019-10-29 | Engine valve |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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DE102019129128.3A DE102019129128A1 (en) | 2019-10-29 | 2019-10-29 | Engine valve |
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DE102019129128A1 true DE102019129128A1 (en) | 2021-04-29 |
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DE102019129128.3A Pending DE102019129128A1 (en) | 2019-10-29 | 2019-10-29 | Engine valve |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0576190A1 (en) * | 1992-06-17 | 1993-12-29 | Eaton Corporation | Chrome plated engine valve |
JP2003278597A (en) * | 2002-03-20 | 2003-10-02 | Mitsubishi Heavy Ind Ltd | Engine member, exhaust vale, piston crown and internal combustion engine |
EP1624092A1 (en) * | 2004-08-06 | 2006-02-08 | Yamaha Hatsudoki Kabushiki Kaisha | Chromium plated exhaust pipe |
EP2215334B1 (en) * | 2007-11-02 | 2011-05-04 | Märkisches Werk GmbH | Intake or discharge valve for a combustion engine, and method for the production thereof |
US20180216524A1 (en) * | 2015-11-20 | 2018-08-02 | Federal-Mogul Llc | Combustion engine components with dynamic thermal insulation coating and method of making and using such a coating |
-
2019
- 2019-10-29 DE DE102019129128.3A patent/DE102019129128A1/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0576190A1 (en) * | 1992-06-17 | 1993-12-29 | Eaton Corporation | Chrome plated engine valve |
JP2003278597A (en) * | 2002-03-20 | 2003-10-02 | Mitsubishi Heavy Ind Ltd | Engine member, exhaust vale, piston crown and internal combustion engine |
EP1624092A1 (en) * | 2004-08-06 | 2006-02-08 | Yamaha Hatsudoki Kabushiki Kaisha | Chromium plated exhaust pipe |
EP2215334B1 (en) * | 2007-11-02 | 2011-05-04 | Märkisches Werk GmbH | Intake or discharge valve for a combustion engine, and method for the production thereof |
US20180216524A1 (en) * | 2015-11-20 | 2018-08-02 | Federal-Mogul Llc | Combustion engine components with dynamic thermal insulation coating and method of making and using such a coating |
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