EP2430210A2 - Method for carbonitriding - Google Patents

Method for carbonitriding

Info

Publication number
EP2430210A2
EP2430210A2 EP10709725A EP10709725A EP2430210A2 EP 2430210 A2 EP2430210 A2 EP 2430210A2 EP 10709725 A EP10709725 A EP 10709725A EP 10709725 A EP10709725 A EP 10709725A EP 2430210 A2 EP2430210 A2 EP 2430210A2
Authority
EP
European Patent Office
Prior art keywords
phase
carburizing
nitriding
nitrogen
metal part
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
EP10709725A
Other languages
German (de)
French (fr)
Other versions
EP2430210B1 (en
Inventor
Lothar Foerster
Jochen Schwarzer
Laszlo Hagymasi
Thomas Waldenmaier
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP2430210A2 publication Critical patent/EP2430210A2/en
Application granted granted Critical
Publication of EP2430210B1 publication Critical patent/EP2430210B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/34Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases more than one element being applied in more than one step
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/20Carburising
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/24Nitriding
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/28Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases more than one element being applied in one step
    • C23C8/30Carbo-nitriding

Definitions

  • the present invention relates to a process for carbonitriding at least one metal part.
  • the document DE 199 09 694 A1 describes a carbonitriding process, in which the diffusion of nitrogen throughout the process or at
  • Use of nitrogen as donor gas preferably takes place solely in the last process phase.
  • DE 101 18 494 C2 describes a low-pressure carbonitriding process in which steel parts are first carburized and then with a
  • Nitrogen donor gas to be embroidered Nitrogen donor gas to be embroidered.
  • the document DE 103 22 255 A1 describes a method for carburizing steel parts in which nitrogen-emitting gas is added both during the heating phase and during the diffusion phase.
  • the invention is therefore based on the object to provide a method for carbonitriding of metal parts, with which the tempering resistance and / or hardenability of a metal part can be improved and / or a depth of nitrogenation comparable to the carcass depth can be achieved.
  • This object is achieved by the process according to the invention for carbonitriding at least one metal part in which the metal part is heated to a treatment temperature in a heating phase, embroidered with a nitrogen donor gas in at least one nitriding phase and carburized in at least one carburizing phase with a carbon donor gas and characterized in that the first nitriding phase begins after the completion of the heating phase and before the beginning of the first carburizing phase.
  • the fact that the first nitriding phase begins only after the completion of the heating phase has the advantage that temperature gradients within the metal part or within a batch of several metal parts can be reduced and thus an inhomogeneous tempering resistance, hardness, strength and / or wear resistance within the metal part or within a batch of metal parts can be avoided.
  • the fact that the first carburizing phase is started only after the start of the nitriding phase has the advantage that the nitrogen introduced into the surface of the metal part can diffuse into the metal part over the entire further treatment period and increase the tempering resistance, hardness, strength and Wear resistance in the edge zone contributes.
  • the fact that the first carburizing phase starts only after the start of the nitridation phase involves nitrogen diffusion. accelerated carbon diffusion. This is because nitrogen atoms and carbon atoms can occupy the same interstices in the crystal lattice of the metal.
  • a carburizing phase following a nitriding phase freed surface near-interstitial sites can be occupied by carbon atoms, thus making the effusion of nitrogen atoms and the associated nitrogen diffusion towards the surface more difficult.
  • the nitrogen can be introduced by the early supply of nitrogen relatively, for example, up to 1, 5 mm or even up to 6 mm, deep into the surface layer of the metal part.
  • an edge carbon concentration of ⁇ 0.3 mass% to ⁇ 0.7 mass% or even up to 1 mass%, and an edge nitrogen concentration of ⁇ 0.1 mass% to ⁇ 0.35 mass% or even from to to 0.5 mass percent can be achieved.
  • the method according to the invention can be used for carbonitriding the edge layer of a metal part.
  • the inventive method can also be used for carbonitriding of several metal parts.
  • the method according to the invention can be used for carbonitriding one or more metallic workpieces.
  • the metal of the metal part can be both a metal and a metal alloy, for example steel. - A -
  • the first nitriding phase ends, in particular directly before the first carburizing phase or during the first carburizing phase or with the first carburizing phase or after the first carburizing phase.
  • the nitrogen effusion can be reduced or prevented during further carburizing phases, further nitriding phases or diffusion phases.
  • the method according to the invention can have at least one second nitriding phase. This can occur, for example, after the first carburization phase.
  • the second nitriding phase may begin following the first carburizing phase.
  • the method has a temperature equalization phase between the heating phase and the first nitriding phase, in which the treatment temperature for equalizing the temperature in the metal part or
  • a constant atmosphere can be understood as meaning both a vacuum and a, preferably inert, gas atmosphere having a constant pressure and a constant composition.
  • the temperature equalization phase subsequent to the heating phase may
  • the first nitriding phase can in turn follow the
  • Run off temperature equalization phase The temperature uniformity phase may, for example, last at least 5 minutes, in particular 30 minutes.
  • a temperature equalization phase has the advantage that temperature gradients within the metal part or within a batch of several me-
  • the treatment temperature can continue to be kept constant, in particular at the same treatment temperature as in the Temperatur fundamentalfahristspha- se. An increase or decrease in the temperature in a subsequent treatment phase is conceivable, however. 5
  • the method is carried out in a, in particular evacuable, treatment chamber.
  • the method has at least one diffusion phase in which the treatment chamber is evacuated and / or filled with an inert gas, for example argon.
  • the first diffusion phase may, for example, be between the first nitriding phase and the first carburizing phase or between the first
  • the method in addition to the first nitriding phase, has at least one further nitriding phase and / or at least one of the first carburizing phase
  • a further carburizing phase and / or at least one further diffusion phase in addition to the first diffusion phase.
  • the further nitriding phases and / or further carburization phases can take place both in particular directly, one behind the other, for example alternately, as well as partially or completely simultaneously.
  • the carbon and nitrogen diffusion in the structure of the metal part can be advantageously increased.
  • further diffusion phases can take place between the further nitriding phases and / or further carburizing phases.
  • a further carburizing phase may take place during or subsequent to another nitriding phase.
  • the nitrogen donor gas comprises a compound selected from the group consisting of ammonia, nitrogen and mixtures thereof, in particular amines. monia.
  • the nitrogen donor gas may consist of a compound selected from the group consisting of ammonia, nitrogen and mixtures thereof, in particular ammonia.
  • the carbon donor gas comprises a compound selected from the group consisting of acetylene, ethylene, propane, propene, methane and mixtures thereof.
  • the carbon donor gas may be a compound selected from the group consisting of acetylene, ethylene, propane, propene, L-O methane, and mixtures thereof.
  • the process is a low-pressure carbonitriding process.
  • the treatment temperature is in a range of ⁇ 780 0 C to ⁇ 1050 0 C, in particular from ⁇ 780 0 C to ⁇ 950 0 C.
  • a nitrogen donor gas partial pressure of less than 500 mbar for example less than 100 mbar, in particular less than or equal to 50 mbar, for example less than 20 mbar
  • a carbon donor gas partial pressure of less than 300 mbar, in particular less than 20 mbar, for example less than 10 mbar may be present.
  • nitriding the temperature for example, a
  • the nitrogen concentration which is within a range of 850 0 C to 950 0 C adapted / increased; and / or the nitrogen supply, for example by increasing the nitrogen donor gas partial pressure, for example to 50 mbar or 30 mbar, and / or the nitrogen donor gas volume flow rate, for example to 3000 l / h, are increased.
  • the nitrogen concentration for example to 50 mbar or 30 mbar, and / or the nitrogen donor gas volume flow rate, for example to 3000 l / h, are increased.
  • the nitrogen concentration in a subsequent diffusion phase is now reduced due to nitrogen effusion and decreases, for example, to an edge nitrogen concentration of up to 0.5% by mass or, for example, 0.1% by mass to ⁇ 0.35% by mass, an increase in tempering resistance and Hardenability on the surface advantageously still be guaranteed.
  • Another object of the present invention is a metal part, for example a metallic workpiece, in which the nitriding depth is greater than that
  • Carburizing depth is.
  • Such a metal part can be produced by a method according to the invention.
  • the advantage here is that the component can have a deep-reaching support effect under mechanical stress at elevated operating temperatures.
  • Another object of the present invention is a metal part, for example a metallic workpiece, produced by a method according to the invention.
  • the nitriding depth may be greater than the carburizing depth.
  • Fig. 1 shows a graph for schematically illustrating an embodiment of the method according to the invention.
  • the method comprises a heating phase 1, a temperature equalization phase 4, four elevations. tion phases 2a, 2b, 2c, 2d, four carburization phases 3a, 3b, 3c, 3d and two diffusion phases 5a, 5b.
  • FIG. 1 shows that, during the heating phase 1, the temperature is maintained continuously at a constant heating rate, up to a treatment temperature of approx
  • the treatment temperature is kept constant at about 950 0 C.
  • neither a nitrogen donor gas nor a carbon donor gas is supplied.
  • a nitrogen donor gas for example ammonia
  • a nitrogen donor gas partial pressure of about 50 mbar.
  • the treatment temperature is kept constant at about 950 ° C., as in the following nitriding phases 2b, 2c, 2d, carburizing phases 3a, 3b, 3c, 3d and diffusion phases 5a, 5b.
  • the first nitriding phase 2 a is followed by a first carburizing phase 3 a in which the nitrogen donor gas partial pressure is reduced again to 0 mbar and the carbon donor gas partial pressure is increased to about 10 mbar.
  • the first carburization phase 3a is followed by a first diffusion phase 5a, in which the carbon donor gas partial pressure is lowered again to 0 mbar. This can be done, for example, by evacuating the treatment chamber or filling the treatment chamber with an inert gas.
  • the first diffusion phase 5a is followed by a second carburizing phase 3b having a carbon donor gas partial pressure of about 10 mbar and a second nitriding phase 2b having a nitrogen donor gas partial pressure of about
  • FIG. 1 shows that the second carburizing phase 3b and the second nitriding phase 2b start simultaneously. However, the second carburizing phase 3b is longer than the second nitriding phase 2b and thus ends only after the nitriding phase 2b. In the period in which both phases 2b, 3b proceed simultaneously, a carbon donor gas partial pressure of about 10 mbar and a
  • Nitrogen donor gas partial pressure of about 50 mbar ago After completion of the second nitridation phase 2b, however, the nitrogen donor gas partial pressure is lowered to 0 mbar and the carbon donor gas partial pressure of about 10 mbar is maintained until the end of the second carburizing phase 3b.
  • the second carburization phase 3b is followed by a second diffusion phase 5b in which the carburizing donor gas partial pressure is lowered again to 0 mbar.
  • the second diffusion phase 5b in turn is followed by a third carburizing phase 3c with a carbon donor gas partial pressure of about 10 mbar.
  • a carbon donor gas partial pressure of about 10 mbar Upon completion of the third carburizing phase 3c, the carbon donor gas

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)

Abstract

The invention relates to a method for carbonitriding at least one metal part in which the metal part is heated to a treatment temperature in a heating phase (1), is nitrided with a nitrogen donor gas in at least one nitriding phase (2a-2d) and is carburized with a carbon donor gas in at least one carburizing phase (3a-3d). Said method is characterised in that the first nitriding phase (2a) begins once the heating phase (1) has finished and prior to the beginning of the first carburizing phase (3a).

Description

5 Beschreibung 5 description
Titeltitle
Verfahren zur Carbonitrierunq L OProcess for carbonitriding L O
Die vorliegende Erfindung betrifft ein Verfahren zur Carbonitrierung mindestens eines Metallteils.The present invention relates to a process for carbonitriding at least one metal part.
Stand der Technik 15Prior Art 15
Verfahren zur Carbonitrierung von Metallteilen sind aus den Druckschriften DE 199 09 694 A1 , DE 101 18 494 A1 und DE 103 22 255 A1 bekannt.Processes for the carbonitriding of metal parts are known from the publications DE 199 09 694 A1, DE 101 18 494 A1 and DE 103 22 255 A1.
Die Druckschrift DE 199 09 694 A1 beschreibt ein Carbonitrierungsverfahren, in 20 dem die Eindiffusion des Stickstoffs während des gesamten Prozesses oder beiThe document DE 199 09 694 A1 describes a carbonitriding process, in which the diffusion of nitrogen throughout the process or at
Verwendung von Stickstoff als Spendergas vorzugsweise allein in der letzten Prozessphase erfolgt.Use of nitrogen as donor gas preferably takes place solely in the last process phase.
Die Druckschrift DE 101 18 494 C2 beschreibt ein Niederdruck-Carbonitrierungs- 25 verfahren, in dem Stahlteile zunächst aufgekohlt und anschließend mit einemDE 101 18 494 C2 describes a low-pressure carbonitriding process in which steel parts are first carburized and then with a
Stickstoffspendergas aufgestickt werden.Nitrogen donor gas to be embroidered.
Die Druckschrift DE 103 22 255 A1 beschreibt ein Verfahren zur Aufkohlung von Stahlteilen, in dem sowohl während der Aufheizphase als auch während der Dif- 30 fusionsphase stickstoffabgebendes Gas zugegeben wird.The document DE 103 22 255 A1 describes a method for carburizing steel parts in which nitrogen-emitting gas is added both during the heating phase and during the diffusion phase.
Durch ein Aufsticken nach oder während der letzten Aufkohlungsphase wird jedoch nur in einem oberflächennahen Bereich, der eine geringere Tiefe aufweist als der aufgekohlte Bereich, Stickstoff angereichert. Dies führt dazu, dass die An- 35 lassbeständigkeit, Härte, Festigkeit und Verschleißbeständigkeit im aufgekohltenHowever, by embroidering after or during the last carburizing phase, nitrogen is enriched only in a near-surface region having a smaller depth than the carburized region. As a result, the adhesion resistance, hardness, strength and wear resistance in the carburized
Bereich nicht ausreichend erhöht werden kann. Eine Aufstickung während der Aufheizphase führt hingegen zu einer inhomogenen Anlassbeständigkeit, Härte, Festigkeit und/oder Verschleißbeständigkeit innerhalb des Metallteils oder innerhalb einer Charge von Metallteilen. 5Range can not be increased sufficiently. On the other hand, nitriding during the heating phase leads to inhomogeneous tempering resistance, hardness, strength and / or wear resistance within the metal part or within a batch of metal parts. 5
Der Erfindung liegt damit die Aufgabe zu Grunde, ein Verfahren zur Carbonitrie- rung von Metallteilen zur Verfügung zu stellen, mit dem die Anlassbeständigkeit und/oder Härtbarkeit eines Metallteils verbessert und/oder eine mit der Aufkoh- lungstiefe vergleichbare Aufstickungstiefe erzielt werden kann. L OThe invention is therefore based on the object to provide a method for carbonitriding of metal parts, with which the tempering resistance and / or hardenability of a metal part can be improved and / or a depth of nitrogenation comparable to the carcass depth can be achieved. L O
Offenbarung der ErfindungDisclosure of the invention
Diese Aufgabe wird durch das erfindungsgemäße Verfahren zur Carbonitrierung 15 mindestens eines Metallteils gelöst, in dem das Metallteil in einer Aufheizphase auf eine Behandlungstemperatur aufgeheizt, in mindestens einer Aufstickungs- phase mit einem Stickstoffspendergas aufgestickt und in mindestens einer Auf- kohlungsphase mit einem Kohlenstoffspendergas aufgekohlt wird und das dadurch gekennzeichnet ist, dass die erste Aufstickungsphase nach dem Abschluss 20 der Aufheizphase und vor dem Beginn der ersten Aufkohlungsphase beginnt.This object is achieved by the process according to the invention for carbonitriding at least one metal part in which the metal part is heated to a treatment temperature in a heating phase, embroidered with a nitrogen donor gas in at least one nitriding phase and carburized in at least one carburizing phase with a carbon donor gas and characterized in that the first nitriding phase begins after the completion of the heating phase and before the beginning of the first carburizing phase.
Dass die erste Aufstickungsphase erst nach dem Abschluss der Aufheizphase beginnt hat den Vorteil, dass Temperaturgradienten innerhalb des Metallteils oder innerhalb einer Charge von mehreren Metallteilen vermindert werden kön- 25 nen und dadurch eine inhomogene Anlassbeständigkeit, Härte, Festigkeit und/oder Verschleißbeständigkeit innerhalb des Metallteils oder innerhalb einer Charge von Metallteilen vermieden werden kann.The fact that the first nitriding phase begins only after the completion of the heating phase has the advantage that temperature gradients within the metal part or within a batch of several metal parts can be reduced and thus an inhomogeneous tempering resistance, hardness, strength and / or wear resistance within the metal part or within a batch of metal parts can be avoided.
Dass mit der ersten Aufkohlungsphase erst nach dem Beginn der Aufstickungs- 30 phase begonnen wird, hat den Vorteil, dass der in die Oberfläche des Metallteils eingetragene Stickstoff über die ganze weitere Behandlungsdauer in das Metallteil diffundieren kann und zur Erhöhung der Anlassbeständigkeit, Härte, Festigkeit und Verschleißbeständigkeit in der Randzone beiträgt.The fact that the first carburizing phase is started only after the start of the nitriding phase has the advantage that the nitrogen introduced into the surface of the metal part can diffuse into the metal part over the entire further treatment period and increase the tempering resistance, hardness, strength and Wear resistance in the edge zone contributes.
35 Darüber hinaus wird dadurch, dass mit der ersten Aufkohlungsphase erst nach dem Beginn der Aufstickungsphase begonnen wird, die Stickstoffdiffusion bezie- hungsweise Kohlenstoffdiffusion beschleunigt. Dies liegt darin begründet, dass Stickstoffatome und Kohlenstoffatome die gleichen Zwischengitterplätze im Kristallgitter des Metalls belegen können. Mit der Durchführung einer Aufkohlungs- phase im Anschluss an eine Aufstickungsphase können frei werdende oberflä- 5 chennahe Zwischengitterplätze durch Kohlenstoffatome belegt werden und somit die Effusion von Stickstoffatomen und die damit verbundene Stickstoffdiffusion zur Oberfläche hin erschwert werden. Dadurch kann mit der vorgeschlagenen Prozessführung auch eine Reduzierung der im Niederdruckbereich vorkommenden und bekannten Stickstoffeffusion erreicht werden.35 In addition, the fact that the first carburizing phase starts only after the start of the nitridation phase involves nitrogen diffusion. accelerated carbon diffusion. This is because nitrogen atoms and carbon atoms can occupy the same interstices in the crystal lattice of the metal. By carrying out a carburizing phase following a nitriding phase, freed surface near-interstitial sites can be occupied by carbon atoms, thus making the effusion of nitrogen atoms and the associated nitrogen diffusion towards the surface more difficult. As a result, with the proposed process control, it is also possible to achieve a reduction in the known and known low-pressure nitrogen diffusion.
L OL O
Weiterhin kann der Stickstoff durch das frühzeitige Stickstoffangebot verhältnismäßig, beispielsweise bis zu 1 ,5 mm oder sogar bis zu 6 mm, tief in die Randschicht des Metallteils eingebracht werden. Dadurch kann bei Metallteilen, beispielsweise mit einer Betriebstemperatur von bis zu 300 0C oder sogar bis zuFurthermore, the nitrogen can be introduced by the early supply of nitrogen relatively, for example, up to 1, 5 mm or even up to 6 mm, deep into the surface layer of the metal part. As a result, in metal parts, for example, with an operating temperature of up to 300 0 C or even up to
15 350 0C, eine Erhöhung der Anlassbeständigkeit im Randbereich erzielt, eine ausreichende Härte, Festigkeit und/oder Verschleißbeständigkeit erreicht und/oder eine dauerhafte Funktion des Metallteils gewährleistet werden.15 350 0 C, achieved an increase in tempering resistance in the edge region, sufficient hardness, strength and / or wear resistance achieved and / or a permanent function of the metal part can be ensured.
Ferner kann mit dem erfindungsgemäßen Verfahren eine Randkohlenstoffkon- 20 zentration von ≥ 0,3 Massenprozent bis < 0,7 Massenprozent oder sogar von bis zu 1 Massenprozent, und eine Randstickstoffkonzentration von ≥ 0,1 Massenprozent bis < 0,35 Massenprozent oder sogar von bis zu 0,5 Massenprozent erzielt werden. Zur Erhöhung der Anlassbeständigkeit, Härte, Festigkeit und/oder Verschleißbeständigkeit kann im Bereich der Aufkohlungstie- 25 fe, beispielsweise bis zu 1 ,5 mm oder sogar bis zu 6 mm tief, vorteilhafterweise eine Stickstoffkonzentration von mindestens 0,05 Massenprozent, gegebenenfalls von mindestens 0,15 Massenprozent, erreicht werden sein.Furthermore, with the process according to the invention, an edge carbon concentration of ≥ 0.3 mass% to <0.7 mass% or even up to 1 mass%, and an edge nitrogen concentration of ≥ 0.1 mass% to <0.35 mass% or even from to to 0.5 mass percent can be achieved. In order to increase the tempering resistance, hardness, strength and / or wear resistance, in the area of carburizing steels, for example up to 1.5 mm or even up to 6 mm deep, advantageously a nitrogen concentration of at least 0.05% by mass, optionally of at least 0 , 15 percent by mass, to be achieved.
Insbesondere kann das erfindungsgemäße Verfahren zur Carbonitrierung der 30 Randschicht eines Metallteils eingesetzt werden. Das erfindungsgemäße Verfahren kann auch zur Carbonitrierung von mehreren Metallteilen eingesetzt werden. Zum Beispiel kann das erfindungsgemäße Verfahren zur Carbonitrierung von einem oder mehreren metallischen Werkstücken eingesetzt werden.In particular, the method according to the invention can be used for carbonitriding the edge layer of a metal part. The inventive method can also be used for carbonitriding of several metal parts. For example, the method according to the invention can be used for carbonitriding one or more metallic workpieces.
35 Bei dem Metall des Metallteils kann es sich sowohl um ein Metall als auch um eine Metalllegierung, beispielsweise Stahl, handeln. - A -The metal of the metal part can be both a metal and a metal alloy, for example steel. - A -
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens endet die erste Aufstickungsphase, insbesondere direkt vor der ersten Aufkoh- lungsphase oder während der ersten Aufkohlungsphase oder mit der ersten Auf- 5 kohlungsphase oder nach der ersten Aufkohlungsphase. Dadurch, dass die ersteWithin the scope of a further embodiment of the method according to the invention, the first nitriding phase ends, in particular directly before the first carburizing phase or during the first carburizing phase or with the first carburizing phase or after the first carburizing phase. In that the first
Aufkohlungsphase direkt an die erste Aufstickungsphase anschließt oder zumindest teilweise gleichzeitig mit der ersten Aufstickungsphase abläuft kann die Stickstoffeffusion während weiterer Aufkohlungsphasen, weiterer Aufstickungs- phasen oder Diffusionsphasen reduziert oder verhindert werden.After the carburization phase directly adjoins the first nitridation phase or at least partially proceeds simultaneously with the first nitridation phase, the nitrogen effusion can be reduced or prevented during further carburizing phases, further nitriding phases or diffusion phases.
L OL O
Weiterhin kann das erfindungsgemäße Verfahren mindestens eine zweite Aufstickungsphase aufweisen. Diese kann beispielsweise nach der ersten Aufkohlungsphase ablaufen. Insbesondere kann die zweite Aufstickungsphase im An- schluss an die erste Aufkohlungsphase beginnen.Furthermore, the method according to the invention can have at least one second nitriding phase. This can occur, for example, after the first carburization phase. In particular, the second nitriding phase may begin following the first carburizing phase.
1515
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens weist das Verfahren zwischen der Aufheizphase und der ersten Aufstickungsphase eine Temperaturvergleichmäßigungsphase auf, in welcher die Behandlungstemperatur zur Vergleichmäßigung der Temperatur in dem Metallteil oderIn the context of a further embodiment of the method according to the invention, the method has a temperature equalization phase between the heating phase and the first nitriding phase, in which the treatment temperature for equalizing the temperature in the metal part or
20 zwischen mehreren Metallteilen, insbesondere bei einer konstanten Atmosphäre, konstant gehalten wird. Dabei kann unter einer konstanten Atmosphäre sowohl Vakuum als auch eine, vorzugsweise inerte, Gasatmosphäre mit konstantem Druck und konstanter Zusammensetzung verstanden werden. Insbesondere kann die Temperaturvergleichmäßigungsphase anschließend an die Aufheizpha-20 between a plurality of metal parts, in particular at a constant atmosphere, is kept constant. In this case, a constant atmosphere can be understood as meaning both a vacuum and a, preferably inert, gas atmosphere having a constant pressure and a constant composition. In particular, the temperature equalization phase subsequent to the heating phase may
25 se ablaufen. Die erste Aufstickungsphase kann wiederum anschließend an die25 se expire. The first nitriding phase can in turn follow the
Temperaturvergleichmäßigungsphase ablaufen. Die Temperaturvergleichmäßi- gungsphase kann zum Beispiel mindestens 5 min, insbesondere 30 min, dauern. Eine Temperaturvergleichmäßigungsphase hat den Vorteil, dass Temperaturgradienten innerhalb des Metallteils oder innerhalb einer Charge von mehreren Me-Run off temperature equalization phase. The temperature uniformity phase may, for example, last at least 5 minutes, in particular 30 minutes. A temperature equalization phase has the advantage that temperature gradients within the metal part or within a batch of several me-
30 tallteilen weiter vermindert werden können und dadurch eine inhomogene Anlassbeständigkeit, Härte, Festigkeit und/oder Verschleißbeständigkeit innerhalb des Metallteils oder innerhalb einer Charge von Metallteilen weiter vermieden werden kann.30 tallteilen can be further reduced and thus inhomogeneous tempering resistance, hardness, strength and / or wear resistance within the metal part or within a batch of metal parts can be further avoided.
35 In den auf die Temperaturvergleichmäßigungsphase folgenden Phasen, beispielsweise Aufstickungsphasen, Aufkohlungsphasen und/oder Diffusionspha- sen, kann die Behandlungstemperatur weiterhin konstant, insbesondere auf der gleichen Behandlungstemperatur wie in der Temperaturvergleichmäßigungspha- se, gehalten werden. Eine Erhöhung oder Absenkung der Temperatur bei einer anschließenden Behandlungsphase ist jedoch denkbar. 535 In the phases following the temperature equalization phase, for example, nitriding phases, carburization phases and / or diffusion phases. sen, the treatment temperature can continue to be kept constant, in particular at the same treatment temperature as in the Temperaturvergleichfahrigungspha- se. An increase or decrease in the temperature in a subsequent treatment phase is conceivable, however. 5
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens wird das Verfahren in einer, insbesondere evakuierbaren, Behandlungskammer durchgeführt.Within the scope of a further embodiment of the method according to the invention, the method is carried out in a, in particular evacuable, treatment chamber.
L O Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens weist das Verfahren mindestens eine Diffusionsphase auf, in welcher die Behandlungskammer evakuiert und/oder mit einem Inertgas, beispielsweise Argon, gefüllt wird. Die erste Diffusionsphase kann beispielsweise zwischen der ersten Aufstickungsphase und der ersten Aufkohlungsphase oder zwischen der erstenIn the context of a further embodiment of the method according to the invention, the method has at least one diffusion phase in which the treatment chamber is evacuated and / or filled with an inert gas, for example argon. The first diffusion phase may, for example, be between the first nitriding phase and the first carburizing phase or between the first
15 Aufkohlungsphase und der zweiten Aufstickungsphase ablaufen.15 carburizing phase and the second nitriding phase.
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens weist das Verfahren neben der ersten Aufstickungsphase mindestens eine weitere Aufstickungsphase und/oder neben der ersten Aufkohlungsphase mindestensWithin the scope of a further embodiment of the method according to the invention, in addition to the first nitriding phase, the method has at least one further nitriding phase and / or at least one of the first carburizing phase
20 eine weitere Aufkohlungsphase und/oder neben der ersten Diffusionsphase mindestens eine weitere Diffusionsphase auf. Die weiteren Aufstickungsphasen und/oder weiteren Aufkohlungsphasen können sowohl, insbesondere direkt, hintereinander, beispielsweise alternierend, als auch teilweise oder vollständig gleichzeitig ablaufen. Durch gleichzeitige oder hintereinander ablaufende Aufsti-20, a further carburizing phase and / or at least one further diffusion phase in addition to the first diffusion phase. The further nitriding phases and / or further carburization phases can take place both in particular directly, one behind the other, for example alternately, as well as partially or completely simultaneously. By concurrent or consecutive succession of
25 ckungsphasen und Aufkohlungsphasen kann die Kohlenstoff- und Stickstoffdiffusion im Gefüge des Metallteils vorteilhafterweise erhöht werden. Zwischen den weiteren Aufstickungsphasen und/oder weiteren Aufkohlungsphasen können darüber hinaus weitere Diffusionsphasen ablaufen. Beispielsweise kann eine weitere Aufkohlungsphase während oder im Anschluss an eine weitere Aufstickungspha-25 ckungsphasen and Aufkohlungsphasen the carbon and nitrogen diffusion in the structure of the metal part can be advantageously increased. In addition, further diffusion phases can take place between the further nitriding phases and / or further carburizing phases. For example, a further carburizing phase may take place during or subsequent to another nitriding phase.
30 se beginnen oder eine weitere Aufstickungsphase während oder im Anschluss an eine Aufkohlungsphase beginnen. Nach dem Abschluss dieser beiden Phasen kann dann zum Beispiel eine weitere Diffusionsphase beginnen.30 seconds or begin another nitriding phase during or after a carburizing phase. After completing these two phases, for example, another diffusion phase can then begin.
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens 35 umfasst das Stickstoffspendergas eine Verbindung, ausgewählt aus der Gruppe bestehend aus Ammoniak, Stickstoff und Mischungen davon, insbesondere Am- moniak. Insbesondere kann das Stickstoffspendergas aus einer Verbindung, ausgewählt aus der Gruppe bestehend aus Ammoniak, Stickstoff und Mischungen davon, insbesondere Ammoniak, bestehen.In the context of a further embodiment of the method 35 according to the invention, the nitrogen donor gas comprises a compound selected from the group consisting of ammonia, nitrogen and mixtures thereof, in particular amines. monia. In particular, the nitrogen donor gas may consist of a compound selected from the group consisting of ammonia, nitrogen and mixtures thereof, in particular ammonia.
5 Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens umfasst das Kohlenstoffspendergas eine Verbindung, ausgewählt aus der Gruppe bestehend aus Acetylen, Ethylen, Propan, Propen, Methan und Mischungen davon. Insbesondere kann das Kohlenstoffspendergas aus einer Verbindung, ausgewählt aus der Gruppe bestehend aus Acetylen, Ethylen, Propan, Propen, L O Methan und Mischungen davon, bestehen.In a further embodiment of the method according to the invention, the carbon donor gas comprises a compound selected from the group consisting of acetylene, ethylene, propane, propene, methane and mixtures thereof. In particular, the carbon donor gas may be a compound selected from the group consisting of acetylene, ethylene, propane, propene, L-O methane, and mixtures thereof.
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens ist das Verfahren ein Niederdruck-Carbonitrierungsverfahren.Within the scope of a further embodiment of the process according to the invention, the process is a low-pressure carbonitriding process.
15 Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens liegt die Behandlungstemperatur in einem Bereich von ≥ 780 0C bis < 1050 0C, insbesondere von ≥ 780 0C bis < 950 0C.In the context of a further embodiment of the method according to the invention, the treatment temperature is in a range of ≥ 780 0 C to <1050 0 C, in particular from ≥ 780 0 C to <950 0 C.
Im Rahmen einer weiteren Ausführungsform des erfindungsgemäßen Verfahrens 20 liegt während der Aufstickungsphasen ein Stickstoffspendergas-Partialdruck von unter 500 mbar, beispielsweise von unter 100 mbar, insbesondere von unter oder gleich 50 mbar, zum Beispiel von unter 20 mbar, vor. Während der Aufkohlungs- phasen kann zum Beispiel ein Kohlenstoffspendergas-Partialdruck von unter 300 mbar, insbesondere von unter 20 mbar, beispielsweise von unter 10 mbar, 25 vorliegen.Within the scope of a further embodiment of the process 20 according to the invention, a nitrogen donor gas partial pressure of less than 500 mbar, for example less than 100 mbar, in particular less than or equal to 50 mbar, for example less than 20 mbar, is present during the nitridation phases. During the carburizing phases, for example, a carbon donor gas partial pressure of less than 300 mbar, in particular less than 20 mbar, for example less than 10 mbar, may be present.
Um Stickstoffverluste durch Stickstoffeffusion während einer Diffusionssequenz auszugleichen, kann während oder vor einer, insbesondere der Diffusionsphase vorgeschalteten, Aufstickungsphase die Temperatur, beispielsweise auf eineTo compensate for nitrogen losses by nitrogen during a diffusion sequence, during or before, in particular the diffusion phase upstream, nitriding the temperature, for example, a
30 Temperatur, welche innerhalb eines Bereichs von 850 0C bis 950 0C liegt ange- passt/erhöht; und/oder das Stickstoffangebot, beispielsweise durch eine Erhöhung des Stickstoffspendergas-Partialdrucks, beispielsweise auf 50 mbar oder 30 mbar, und/oder des Stickstoffspendergas-Volumendurchsatzes, beispielsweise auf 3000 l/h, erhöht werden. Auf diese Weise kann die Stickstoffkonzentration30 temperature which is within a range of 850 0 C to 950 0 C adapted / increased; and / or the nitrogen supply, for example by increasing the nitrogen donor gas partial pressure, for example to 50 mbar or 30 mbar, and / or the nitrogen donor gas volume flow rate, for example to 3000 l / h, are increased. In this way, the nitrogen concentration
35 im oberflächennahen Bereich, beispielsweise von ≥ 0,1 mm bis ≤ 0,2 mm oder sogar von bis zu 0,3 mm, höher als im Endprodukt eingestellt und eine Stickstof- feffusion kompensiert werden. Wird die Stickstoffkonzentration in einer anschließenden Diffusionsphase nun aufgrund von Stickstoffeffusion verringert und nimmt beispielsweise auf eine Randstickstoffkonzentration von bis zu 0,5 Massen prozent oder beispielsweise auf ≥ 0,1 Massen prozent bis ≤ 0,35 Massenprozent ab, so kann eine Erhöhung der Anlassbeständigkeit und Härtbarkeit an der Oberfläche vorteilhafterweise trotzdem gewährleistet werden.35 in the near-surface region, for example from ≥ 0.1 mm to ≤ 0.2 mm or even up to 0.3 mm, higher than in the final product and a nitrogen be compensated. If the nitrogen concentration in a subsequent diffusion phase is now reduced due to nitrogen effusion and decreases, for example, to an edge nitrogen concentration of up to 0.5% by mass or, for example, 0.1% by mass to ≦ 0.35% by mass, an increase in tempering resistance and Hardenability on the surface advantageously still be guaranteed.
Ein weiterer Gegenstand der vorliegenden Erfindung ist ein Metallteil, beispiels- weise ein metallisches Werkstück, bei dem die Aufstickungstiefe größer als dieAnother object of the present invention is a metal part, for example a metallic workpiece, in which the nitriding depth is greater than that
Aufkohlungstiefe ist. Ein derartiges Metallteil kann durch ein erfindungsgemäßes Verfahren hergestellt werden. Vorteilhaft dabei ist, dass das Bauteil eine tiefreichende Stützwirkung unter mechanischer Belastung bei erhöhten Betriebstemperaturen aufweisen kann.Carburizing depth is. Such a metal part can be produced by a method according to the invention. The advantage here is that the component can have a deep-reaching support effect under mechanical stress at elevated operating temperatures.
Ein weiterer Gegenstand der vorliegenden Erfindung ist ein Metallteil, beispielsweise ein metallisches Werkstück, hergestellt durch ein erfindungsgemäßes Verfahren. Insbesondere kann bei einem derartigen Metallteil die Aufstickungstiefe größer als die Aufkohlungstiefe sein.Another object of the present invention is a metal part, for example a metallic workpiece, produced by a method according to the invention. In particular, in such a metal part, the nitriding depth may be greater than the carburizing depth.
Zeichnungendrawings
Weitere Vorteile und vorteilhafte Ausgestaltungen der erfindungsgemäßen Gegenstände werden durch die Zeichnung veranschaulicht und in der nachfolgenden Beschreibung erläutert. Dabei ist zu beachten, dass die Zeichnung nur beschreibenden Charakter hat und nicht dazu gedacht ist, die Erfindung in irgendeiner Form einzuschränken.Further advantages and advantageous embodiments of the objects according to the invention are illustrated by the drawing and explained in the following description. It should be noted that the drawing has only descriptive character and is not intended to limit the invention in any way.
Fig. 1 zeigt einen Graphen zur schematischen Veranschaulichung einer Ausführungsform des erfindungsgemäßen Verfahrens.Fig. 1 shows a graph for schematically illustrating an embodiment of the method according to the invention.
Im Rahmen der in Figur 1 gezeigten Ausführungsform umfasst das Verfahren ei- ne Aufheizphase 1 , eine Temperaturvergleichmäßigungsphase 4, vier Aufsti- ckungsphasen 2a, 2b, 2c, 2d, vier Aufkohlungsphasen 3a, 3b, 3c, 3d und zwei Diffusionsphasen 5a, 5b.In the context of the embodiment shown in FIG. 1, the method comprises a heating phase 1, a temperature equalization phase 4, four elevations. tion phases 2a, 2b, 2c, 2d, four carburization phases 3a, 3b, 3c, 3d and two diffusion phases 5a, 5b.
Figur 1 zeigt, dass während der Aufheizphase 1 die Temperatur mit einer kon- stanten Aufheizrate kontinuierlich bis auf eine Behandlungstemperatur von etwaFIG. 1 shows that, during the heating phase 1, the temperature is maintained continuously at a constant heating rate, up to a treatment temperature of approx
950 0C erhöht wird.950 0 C is increased.
In der an die Aufheizphase 1 anschließenden Temperaturvergleichmäßigungs- phase 4 wird die Behandlungstemperatur konstant auf etwa 950 0C gehalten. Während der Aufheizphase 1 und der Temperaturvergleichmäßigungsphase 4 wird dabei weder ein Stickstoffspendergas noch ein Kohlenstoffspendergas zugeführt.In the subsequent to the heating phase 1 temperature equalization phase 4, the treatment temperature is kept constant at about 950 0 C. During the heating phase 1 and the temperature equalization phase 4, neither a nitrogen donor gas nor a carbon donor gas is supplied.
In der an die Temperaturvergleichmäßigungsphase 4 anschließenden ersten Aufstickungsphase 2a wird ein Stickstoffspendergas, beispielsweise Ammoniak, mit einem Stickstoffspendergas-Partialdruck von etwa 50 mbar zugeführt. Die Behandlungstemperatur wird dabei ebenso wie in den folgenden Aufstickungs- phasen 2b, 2c, 2d, Aufkohlungsphasen 3a, 3b, 3c, 3d und Diffusionsphasen 5a, 5b konstant auf etwa 950 0C gehalten. An die erste Aufstickungsphase 2a schließt sich eine erste Aufkohlungsphase 3a an, in welcher der Stickstoffspen- dergas-Partialdruck wieder auf 0 mbar gesenkt und der Kohlenstoffspendergas- Partialdruck auf etwa 10 mbar erhöht wird. An die erste Aufkohlungsphase 3a schließt sich eine erste Diffusionsphase 5a an, in welcher der Kohlenstoffspen- dergas-Partialdruck wieder auf 0 mbar gesenkt wird. Dies kann beispielsweise durch Evakuieren der Behandlungskammer oder Füllen der Behandlungskammer mit einem Inertgas erfolgen.In the first nitriding phase 2a adjoining the temperature equalization phase 4, a nitrogen donor gas, for example ammonia, is supplied with a nitrogen donor gas partial pressure of about 50 mbar. The treatment temperature is kept constant at about 950 ° C., as in the following nitriding phases 2b, 2c, 2d, carburizing phases 3a, 3b, 3c, 3d and diffusion phases 5a, 5b. The first nitriding phase 2 a is followed by a first carburizing phase 3 a in which the nitrogen donor gas partial pressure is reduced again to 0 mbar and the carbon donor gas partial pressure is increased to about 10 mbar. The first carburization phase 3a is followed by a first diffusion phase 5a, in which the carbon donor gas partial pressure is lowered again to 0 mbar. This can be done, for example, by evacuating the treatment chamber or filling the treatment chamber with an inert gas.
An die erste Diffusionsphase 5a schließt sich eine zweite Aufkohlungsphase 3b mit einem Kohlenstoffspendergas-Partialdruck von etwa 10 mbar und eine zweite Aufstickungsphase 2b mit einem Stickstoffspendergas-Partialdruck von etwaThe first diffusion phase 5a is followed by a second carburizing phase 3b having a carbon donor gas partial pressure of about 10 mbar and a second nitriding phase 2b having a nitrogen donor gas partial pressure of about
50 mbar an. Figur 1 zeigt, dass die zweite Aufkohlungsphase 3b und die zweite Aufstickungsphase 2b gleichzeitig beginnen. Die zweite Aufkohlungsphase 3b ist jedoch länger als die zweite Aufstickungsphase 2b und endet daher erst nach der Aufstickungsphase 2b. In dem Zeitraum, in dem beide Phasen 2b, 3b gleichzeitig ablaufen, liegt ein Kohlenstoffspendergas-Partialdruck von etwa 10 mbar und ein50 mbar. Figure 1 shows that the second carburizing phase 3b and the second nitriding phase 2b start simultaneously. However, the second carburizing phase 3b is longer than the second nitriding phase 2b and thus ends only after the nitriding phase 2b. In the period in which both phases 2b, 3b proceed simultaneously, a carbon donor gas partial pressure of about 10 mbar and a
Stickstoffspendergas-Partialdruck von etwa 50 mbar vor. Nach Abschluss der zweiten Aufstickungsphase 2b wird der Stickstoffspendergas-Partialdruck jedoch auf 0 mbar gesenkt und der Kohlenstoffspendergas-Partialdruck von etwa 10 mbar bis zum Ende der zweiten Aufkohlungsphase 3b aufrechterhalten. An die zweite Aufkohlungsphase 3b schließt eine zweite Diffusionsphase 5b an, in welcher der Aufkohlungsspendergas-Partialdruck erneut auf 0 mbar gesenkt wird.Nitrogen donor gas partial pressure of about 50 mbar ago. After completion of the second nitridation phase 2b, however, the nitrogen donor gas partial pressure is lowered to 0 mbar and the carbon donor gas partial pressure of about 10 mbar is maintained until the end of the second carburizing phase 3b. The second carburization phase 3b is followed by a second diffusion phase 5b in which the carburizing donor gas partial pressure is lowered again to 0 mbar.
An die zweite Diffusionsphase 5b schließt wiederum eine dritte Aufkohlungsphase 3c mit einem Kohlenstoffspendergas-Partialdruck von etwa 10 mbar an. Nach Abschluss der dritten Aufkohlungsphase 3c wird der Kohlenstoffspendergas-The second diffusion phase 5b in turn is followed by a third carburizing phase 3c with a carbon donor gas partial pressure of about 10 mbar. Upon completion of the third carburizing phase 3c, the carbon donor gas
Partialdruck auf 0 mbar gesenkt und es läuft eine dritte Aufstickungsphase 2c mit einem Stickstoffspendergas-Partialdruck von etwa 50 mbar ab. An diese schließt sich wiederum eine vierte Aufkohlungsphase 3d an, in welcher der Stickstoff- spendergas-Partialdruck auf 0 mbar gesenkt und der Kohlenstoffspendergas- Partialdruck auf etwa 10 mbar erhöht wird. Nach Abschluss der vierten Aufkohlungsphase 3d wird der Kohlenstoffspendergas-Partialdruck wieder auf 0 mbar gesenkt und es läuft eine vierte Aufstickungsphase 2d mit einem Stickstoffspen- dergas-Partialdruck von etwa 50 mbar ab, welche - verglichen mit den vorherigen Aufstickungsphasen 2a-2c - sehr lang ist. Nach dieser letzten Aufstickungsphase 2d wird die Behandlungstemperatur von 950 0C nicht weiter aufrecht gehalten und eine Abschreckung auf Raumtemperatur durchgeführt, um die gewünschte Gefügezusammensetzung einzustellen.Lowered partial pressure to 0 mbar and it runs a third nitriding phase 2c with a nitrogen donor gas partial pressure of about 50 mbar. This is in turn followed by a fourth carburizing phase 3d, in which the nitrogen donor gas partial pressure is lowered to 0 mbar and the carbon donor gas partial pressure is increased to about 10 mbar. After completing the fourth carburizing phase 3d, the carbon donor gas partial pressure is lowered back to 0 mbar and a fourth nitridation phase 2d proceeds with a nitrogen donor gas partial pressure of about 50 mbar, which is very long compared to the previous nitriding phases 2a-2c , After this final nitriding phase 2d, the treatment temperature of 950 ° C. is no longer maintained and quenching is carried out to room temperature to set the desired microstructural composition.
Es versteht sich von selbst, dass auf diese Weise zahlreiche Verfahren zur Car- bonitrierung möglich sind und die Erfindung nicht auf die erläuterte Abfolge undIt goes without saying that numerous methods for carbonitriding are possible in this way and the invention is not based on the sequence described and
Anzahl von vier Aufstickungsphasen 2a, 2b, 2c, 2d, vier Aufkohlungsphasen 3a, 3b, 3c, 3d und zwei Diffusionsphasen 5a, 5b beschränkt ist. Number of four nitriding phases 2a, 2b, 2c, 2d, four carburization phases 3a, 3b, 3c, 3d and two diffusion phases 5a, 5b is limited.

Claims

5 Ansprüche 5 claims
1. Verfahren zur Carbonitrierung mindestens eines metallischen Metallteils, in dem das Metallteil1. A method for carbonitriding at least one metallic metal part, in which the metal part
- in einer Aufheizphase (1 ) auf eine Behandlungstemperatur aufgeheizt L O wird,heated in a heating phase (1) to a treatment temperature L O,
- in mindestens einer Aufstickungsphase (2a-2d) mit einem Stickstoffspendergas aufgestickt wird, und- In at least one nitriding phase (2a-2d) is embroidered with a nitrogen donor gas, and
- in mindestens einer Aufkohlungsphase (3a-3d) mit einem Kohlenstoffspendergas aufgekohlt wird,- is carburized in at least one carburizing phase (3a-3d) with a carbon donor gas,
15 dadurch gekennzeichnet, dass die erste Aufstickungsphase (2a) nach dem Abschluss der Aufheizphase (1 ) und vor dem Beginn der ersten Aufkohlungsphase (3a) beginnt.15 characterized in that the first nitriding phase (2a) begins after completion of the heating phase (1) and before the start of the first carburizing phase (3a).
2. Verfahren nach Anspruch 1 , dadurch gekennzeichnet, dass die erste Aufsti- 20 ckungsphase (2a) vor der ersten Aufkohlungsphase (3a) oder während der ersten Aufkohlungsphase (3a) oder mit der ersten Aufkohlungsphase (3a) oder nach der ersten Aufkohlungsphase (3a) endet.2. The method according to claim 1, characterized in that the first startup phase (2a) before the first carburizing phase (3a) or during the first carburizing phase (3a) or with the first carburizing phase (3a) or after the first carburizing phase (3a ) ends.
3. Verfahren nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass das Ver- 25 fahren zwischen der Aufheizphase (1 ) und der ersten Aufstickungsphase eine Temperaturvergleichmäßigungsphase (4) aufweist, in welcher die Behandlungstemperatur zur Vergleichmäßigung der Temperatur innerhalb des Metallteils oder zwischen mehreren Metallteilen, insbesondere bei einer konstanten Atmosphäre, konstant gehalten wird.3. The method according to claim 1 or 2, characterized in that the drive 25 between the heating phase (1) and the first nitriding a Temperaturvergleichmäßigungsphase (4), in which the treatment temperature to equalize the temperature within the metal part or between a plurality of metal parts , especially at a constant atmosphere, is kept constant.
3030
4. Verfahren nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass das Verfahren in einer, insbesondere evakuierbaren, Behandlungskammer durchgeführt wird. 4. The method according to any one of claims 1 to 3, characterized in that the method is carried out in a, in particular evacuated, treatment chamber.
5. Verfahren nach Anspruch 4, dadurch gekennzeichnet, dass das Verfahren mindestens eine Diffusionsphase (5a, 5b) aufweist, in welcher die Behandlungskammer evakuiert und/oder mit einem Inertgas gefüllt wird.5. The method according to claim 4, characterized in that the method comprises at least one diffusion phase (5a, 5b), in which the treatment chamber is evacuated and / or filled with an inert gas.
5 6. Verfahren nach Anspruch 5, dadurch gekennzeichnet, dass das Verfahren neben der ersten Aufstickungsphase (2a) mindestens eine weitere Aufsti- ckungsphase (2b-2d) und/oder neben der ersten Aufkohlungsphase (3a) mindestens eine weitere Aufkohlungsphase (3b-3d) und/oder neben der ersten Diffusionsphase (5a) mindestens eine weitere Diffusionsphase (5b) auf- L O weist.5 6. The method according to claim 5, characterized in that the method in addition to the first nitriding phase (2a) at least one further Aufsti- ckungsphase (2b-2d) and / or next to the first carburizing phase (3a) at least one further carburizing phase (3b-3d ) and / or at least one further diffusion phase (5b) has LO in addition to the first diffusion phase (5a).
7. Verfahren nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass das Stickstoffspendergas eine Verbindung, ausgewählt aus der Gruppe bestehend aus Ammoniak, Stickstoff und Mischungen davon, umfasst.7. The method of claim 1, wherein the nitrogen donor gas comprises a compound selected from the group consisting of ammonia, nitrogen and mixtures thereof.
1515
8. Verfahren nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass das Kohlenstoffspendergas eine Verbindung, ausgewählt aus der Gruppe bestehend aus Acetylen, Ethylen, Propan, Propen, Methan und Mischungen davon, umfasst.8. The method according to any one of claims 1 to 7, characterized in that the carbon donor gas comprises a compound selected from the group consisting of acetylene, ethylene, propane, propene, methane and mixtures thereof.
2020
9. Verfahren nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass das Verfahren ein Niederdruck-Carbonitrierungsverfahren ist.9. The method according to any one of claims 1 to 8, characterized in that the method is a low-pressure carbonitriding method.
10. Verfahren nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass 25 die Behandlungstemperatur in einem Bereich von ≥ 780 0C bis ≤ 1050 0C liegt.10. The method according to any one of claims 1 to 9, characterized in that the treatment temperature is in a range of ≥ 780 0 C to ≤ 1050 0 C.
1 1. Verfahren nach einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, dass während der Aufstickungsphase (2a-2d) ein Stickstoffspendergas-1 1. A method according to any one of claims 1 to 10, characterized in that during the nitriding phase (2a-2d) a nitrogen donor gas
30 Partialdruck von unter 500 mbar vorliegt.30 partial pressure of less than 500 mbar is present.
12. Metallteil, bei dem die Aufstickungstiefe größer als die Aufkohlungstiefe ist.12. Metal part where the nitriding depth is greater than the carburizing depth.
13. Metallteil, hergestellt durch ein Verfahren nach einem der Ansprüche 1 bis13. Metal part, produced by a method according to one of claims 1 to
35 1 1 . 35 1 1.
EP10709725.5A 2009-05-11 2010-03-18 Method for carbonitriding Active EP2430210B1 (en)

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JP2012526203A (en) 2012-10-25
JP5930960B2 (en) 2016-06-08
WO2010130484A3 (en) 2011-01-13
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WO2010130484A2 (en) 2010-11-18

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