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EP2253398A1 - Wear-resistant material - Google Patents

Wear-resistant material Download PDF

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Publication number
EP2253398A1
EP2253398A1 EP09450242A EP09450242A EP2253398A1 EP 2253398 A1 EP2253398 A1 EP 2253398A1 EP 09450242 A EP09450242 A EP 09450242A EP 09450242 A EP09450242 A EP 09450242A EP 2253398 A1 EP2253398 A1 EP 2253398A1
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EP
European Patent Office
Prior art keywords
carbon
nitrogen
niobium
wear
tantalum
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
EP09450242A
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German (de)
French (fr)
Other versions
EP2253398B1 (en
Inventor
Werner Theisen
Stephan Huth
Herbert Schweiger
Jochen Perko
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.)
Voestalpine Boehler Edelstahl GmbH and Co KG
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Boehler Edelstahl GmbH and Co KG
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Priority to EP11004405A priority Critical patent/EP2374560A1/en
Publication of EP2253398A1 publication Critical patent/EP2253398A1/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/22Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/06Making metallic powder or suspensions thereof using physical processes starting from liquid material
    • B22F9/08Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
    • B22F9/082Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/26Methods of annealing
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • C22C33/0207Using a mixture of prealloyed powders or a master alloy
    • C22C33/0228Using a mixture of prealloyed powders or a master alloy comprising other non-metallic compounds or more than 5% of graphite
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • C22C33/0257Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • C22C33/0292Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with more than 5% preformed carbides, nitrides or borides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/24Ferrous alloys, e.g. steel alloys containing chromium with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/26Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/28Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/004Dispersions; Precipitations
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/25Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles

Definitions

  • the invention relates to a wear-resistant material containing carbon (C), nitrogen (N), oxygen (O), niobium and / or tantalum (Nb / Ta) as well as metallic elements and impurities remainder with a structure consisting of a metal matrix and in these Hartphasen stored.
  • metallic materials consist of a tough or tough matrix and distributed in this hard phases, which are usually formed as interstitial compounds.
  • a wear-reducing effect of hard phase deposits is well known, with a higher hard phase content in the matrix as much as possible reducing abrasive removal from the workpiece surface when the support force for the hard particles and the matrix hardness are high.
  • wear-resistant iron-based materials eg. Cold work steels, from a hard, preferably thermally tempered metal matrix with distributed in this, precipitated from the residual melt of the alloy during solidification, carbides.
  • Carbide formation in a ledeburitic solidification of an alloyed melt in a cast billet may also result in coarse hard phases with inhomogeneous distribution in the material due to a low solidification rate in the center thereof and segregation.
  • alloys Due to the demand for highly wear-resistant materials, which should possibly have a superior corrosion resistance, alloys have been proposed which have a high content of carbide formers, in particular monocarbide formers, with a corresponding carbon content and a chromium concentration in the matrix of more than 12.0 wt .-%.
  • Nitrogen for hard phase formation is considered an advantageous measure for the production of wear-resistant materials in the WO 2007/024 192 A1 proposed.
  • the invention sets itself the goal of specifying a material which has a high resistance to abrasion under abrasion stress.
  • this material in an alloy variant should also be resistant to chemical corrosion.
  • Another object of the invention is to provide a method for producing a material with greatly reduced wear and optionally desired corrosion properties or high corrosion resistance.
  • the object of the invention mentioned at the outset is essentially achieved by a material containing in% by weight: Carbon (C) more than 0.3 to 3.5 Nitrogen (N) 12:05 to 4.0 Oxygen (O) more than 0002 to 12:25 Niobium / tantalum (Nb / Ta) 3.0 to 18.0 as well as metallic elements and impurities as the remainder with a structure consisting of a metal matrix and embedded in these hard phases, with the proviso that the hard phases are formed as carbides and / or nitrides and / or carbonitrides and / or Kohlenstoffkarbonitride and have a diameter of at most 50 microns and at least 0.2 microns ,
  • the advantages of the wear-resistant material of the invention consist essentially in the fact that due to the niobium / tantalum concentration of 3.0 to 18.0 wt .-% and the carbon content of 0.3 to 3.0 wt .-% and the nitrogen content of 0.05 to 4.0 wt .-% high-hardness niobium and / or tantalum monocarbides, mononitrides or monocarbonitrides are present in a homogeneous distribution with a small diameter and thus a high abrasion resistance is achieved.
  • the oxygen content of 0.0020 to 0.25 in the material acts on the one hand as a formation nucleus for the hard phase with respect to hard particles with specific, small size in a homogeneous distribution in the matrix and on the other hand as a separate hard material former.
  • the hard material particles have a diameter of at most 50 ⁇ m, because with larger phases the danger of breaking them out of the matrix is suddenly increased. Smaller diameters than 0.2 ⁇ m of the hard phases provide only a slight, abrasion-reducing effect.
  • the matrix of the wear-resistant alloy has a martensitic microstructure, then the material itself has an increased abrasion-reducing hardness, minimizing as far as possible the risk of breaking hard phases out of the structure during wear.
  • the concentrations of the alloying metals are coordinated in this material with respect to the carbon activity and the carbide formation kinetics of the respective elements, the contents of the monocarbide formers being decisive for the intended carbon concentration.
  • Nitrogen is limited with a content of 0.6 wt .-% to the top, because in the given case, the hard phases should be designed mainly as carbides. Below 0.15 wt.% Nitrogen, the solidification effect of the matrix is too low, so that the content limits in wt.% Are 0.15 to 0.6 nitrogen.
  • Silicon acts as a deoxidation metal and influences the microstructural transformation of the alloy during the heat treatment.
  • a minimum content of 0.2% by weight of Si is important in terms of effective oxide formation, whereas higher contents than 1.5% by weight adversely affect toughness.
  • a manganese content of 0.3% by weight or more is intended for setting sulfur in the metal, with more than 2.0% by weight of Mn promoting disadvantageous austenite stability.
  • Chromium and molybdenum provide corrosion resistance of the alloy at minimum concentrations of 10.0 and 0.5 wt%, but may also be effective as carbide formers. Higher contents than 20% by weight Cr and 3.0% by weight Mo disadvantageously lead to a stabilization of ferrite in a heat treatment.
  • Vanadium and titanium should not exceed contents of 1.0 wt .-%, because carbides of these elements to a large extent dissolve Cr or incorporate into the crystal lattice, which can cause depletion of Cr in the edge region of the matrix.
  • the elements niobium and tantalum are elements that form in the alloy from a content of 3.0 wt .-% hard, the wear resistance of the material promoting monocarbides. It is important that these elements Nb / Ta show only a slight tendency to incorporate further elements, in particular chromium, in the carbide or carbonitride formation in the crystal lattice, so that in the vicinity of these hard phases no depletion of the matrix of alloy components, especially of chromium and Molybdenum, arises and thus no adverse effect on the corrosion resistance of the material is formed.
  • the high nitrogen content of 1.0 to 4.0 wt .-% at carbon concentrations of 0.3 to 1.0 wt .-% leads to substantially nitrides formed hard phases, whereby the chromium and molybdenum induced passive layer formation and corrosion resistance are promoted.
  • the highly wear-resistant tool material which is based on a type of high-speed steel alloy, can be easily tempered to high hardness values and has outstanding toughness despite its high hardness. Particularly pronounced is the wear resistance of the cutting tools formed from this alloy, which tools thus have a particularly long service life in coarse and interrupted section.
  • the inventive method of the type mentioned above is determined such that in a first step, a metallic liquid alloy containing niobium / tantalum (Nb / Ta) with a concentration of 3.0 to 18.0 wt .-%, and a content of carbon and / or nitrogen, in which no primary excretions formed on carbides and / or nitrides above the Verdüsungstemperatur or liquidus temperature, is atomized to powder material, after which the powder subjected to a process for increasing the carbon content and / or the nitrogen content and / or the oxygen content and subsequently subjected to a hot compacting, in particular a hot isostatic pressing Alternatively, the pellet or HIP body is subjected to a hot deformation and / or a heat treatment alternatively.
  • the method according to the invention has the advantage that materials with a high carbide-nitride or carbonitride hard material content can be produced, the hard-material particles having small diameters and homogeneous distribution in the matrix.
  • the matrix elements can by a thermal tempering or by hardening and tempering of the material impart this high strength and prevent stripping or breaking the larger, optimized hard particles as far as possible. As a result, a particularly pronounced wear resistance of the material is achieved.
  • other hard material particles with a size of 2 to 50 microns to an extent of up to 25 vol .-% can be added to the powder material, which are effective in reducing wear for the given material.
  • Tab. 1 on page 11 shows the composition of two commercially available, wear-resistant alloys with the designations X190 CrVMo 20 4 1, X90 CrVMo 18 1 1, corrosion-resistant, inventive alloys with the designations A, B, C, and of cutting materials according to the invention with the designations D, E, F.
  • the commercial alloys were after the PM process with a deformation of the HIP block (H schreib- I sostatisch-ge p resst) of greater than 6-fold been prepared.
  • Powders for the samples designated A, B, C were made from alloys having the following main components in wt%: description Si Mn Cr Not a word V W Nb Co Fe A 12:43 12:42 11.92 2.21 12:08 12:07 9:02 12:08 rest B 12:51 12:44 16:41 2.19 12:09 12:07 9:56 12:05 rest C 12:43 12:42 11.92 2.21 12:05 12:06 9:02 12:08 rest produced by atomizing by means of nitrogen gas.
  • Atomization with nitrogen was further carried out using melts designated D, E, F with the main constituents in% by weight: description Si Mn Cr Not a word V W Nb Co Fe D 12:30 12:40 4.15 2.94 1:52 2.13 3:34 12:12 rest e 12:28 12:35 3.95 2.84 1:47 2.23 3:45 8.21 rest F 12:37 12:33 3:58 4.10 1.84 5:07 10.73 7:07 rest
  • the alloyed metal powder was then placed under nitrogen atmosphere in steel containers and knock compacted, followed by welding of the containers and hot isostatic pressing at a temperature of 1165 ° C.
  • Table 1 shows the chemical composition of known materials (X190 CrVMo 20 4 1 and X90 CrMoV 18 1 1) and those of steel samples according to the invention
  • the corrosion behavior of the alloys was determined from current density potential curves on the samples according to ASTM G65 in 1N H 2 SO 4 , 20 ° C, with a quenching of the same from 1100 ° C and 1070 ° C and a tempering at 200 ° C. ,
  • Fig. 1 shows, in the relevant potential range of about -300mV to + 300mV, the comparative alloy X190 CrVMo 20 4 1 essentially the highest passive current density in comparison with the inventively assembled samples A, B, C, which reveals their improved corrosion behavior.
  • Fig. 2 shows the hardness of the differently composite alloys after hardening as a function of the tempering temperature after two tempering.
  • the respective hardening temperature can be taken from the designation field for the alloys.
  • the materials A and C of the alloy according to the invention on a comparatively low tempering hardness, because their respective carbon content of improved corrosion resistance due to (see Fig.1 ) was chosen low.
  • the material hardness of the alloys D, E and F are significantly higher in the range of tempering temperatures between 500 ° C and 600 ° C, which discloses a clear superiority of the same for use of, for example, cutting and forming elements.
  • Fig. 3 shows the wear behavior of the samples made from the alloys, determined according to the VDI Progress Reports "Nitrogen-alloyed Tool Steels", Series 5, No. 188 (1990), p. 129 described pin-disk test with Flint 80s Grain. The hardnesses of the samples are above the respective bars in Fig. 3 specified. Both the corrosion resistant alloy B and the alloys E and F according to the invention show superior resistance to wear, indicating a correspondingly favorable choice of carbon and niobium contents.

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  • Chemical Kinetics & Catalysis (AREA)
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Abstract

A wear-resistant material comprises (in weight%) carbon (0.3-3.5), nitrogen (0.05-4), oxygen (0.002-0.25), niobium/tantalum (3-18), and remainder of metallic elements and impurities. A microstructure of the material comprises a metal matrix and hard phases embedded in the matrix. The hard phases comprise carbide, nitride, carbonitride and/or oxide carbonitride, where hard phases have diameter of 0.2-50 mu m. An independent claim is also included for a method for producing a wear-resistant material.

Description

Die Erfindung bezieht sich auf einen verschleißbeständigen Werkstoff, enthaltend Kohlenstoff (C), Stickstoff (N), Sauerstoff (O), Niob und/oder Tantal (Nb/Ta) sowie metallische Elemente und Verunreinigungen als Rest mit einem Gefüge, bestehend aus einer Metallmatrix und in diese eingelagert Hartphasen.The invention relates to a wear-resistant material containing carbon (C), nitrogen (N), oxygen (O), niobium and / or tantalum (Nb / Ta) as well as metallic elements and impurities remainder with a structure consisting of a metal matrix and in these Hartphasen stored.

Gemäß dem technischen Ansatz bestehen verschleißresistente, metallische Werkstoffe aus einer zähfesten oder zähharten Matrix und in dieser verteilt Hartphasen, welche zumeist als interstitielle Verbindungen ausgeformt sind.According to the technical approach wear-resistant, metallic materials consist of a tough or tough matrix and distributed in this hard phases, which are usually formed as interstitial compounds.

Eine verschleißmindernde Wirkung von Hartphaseneinlagerungen ist allgemein bekannt, wobei ein höherer Hartphasenanteil in der Matrix einen abrasiven Abtrag von der Werkstückoberfläche höchstmöglich vermindert, wenn die Stützkraft für die Hartstoffpartikel und die Matrixhärte hoch sind.A wear-reducing effect of hard phase deposits is well known, with a higher hard phase content in the matrix as much as possible reducing abrasive removal from the workpiece surface when the support force for the hard particles and the matrix hardness are high.

Nach dem Stand der Technik bestehen verschleißresistente Eisenbasiswerkstoffe, zB. Kaltarbeitsstähle, aus einer harten, vorzugsweise thermisch vergüteten Metallmatrix mit in dieser verteilten, aus der Restschmelze der Legierung bei der Erstarrung ausgeschiedenen, Karbiden.According to the prior art are wear-resistant iron-based materials, eg. Cold work steels, from a hard, preferably thermally tempered metal matrix with distributed in this, precipitated from the residual melt of the alloy during solidification, carbides.

Eine Karbidbildung bei einer ledeburitischen Erstarrung einer legierten Schmelze in einem Gussblock kann auch aufgrund einer niedrigen Erstarrungsgeschwindigkeit im Zentrum desselben und durch Seigerung zu groben Hartphasen mit inhomogener Verteilung im Werkstoff führen.Carbide formation in a ledeburitic solidification of an alloyed melt in a cast billet may also result in coarse hard phases with inhomogeneous distribution in the material due to a low solidification rate in the center thereof and segregation.

Um eine höhere Konzentration von Hartphasen im Werkstoff, insbesondere bei gleichmäßiger Verteilung in diesem, zu erreichen, ist es bekannt, pulvermetallurgische Herstellverfahren anzuwenden. Im Wesentlichen wird bei diesen PM-Verfahren eine legierte, flüssige Schmelze nach einem Ausfließen aus einer Düse durch Hochdruck-Gasstrahlen in kleine Tröpfchen zerteilt, welche naturgemäß mit hoher Geschwindigkeit abkühlen und dadurch feine Hartphasenpartikel bei der Erstarrung ausscheiden. Durch ein heißisostatisches Pressen (HIP) oder mittels Verformung des Pulvers in einem Behältnis erfolgt eine Herstellung eines weitgehend dichten Werkstoffes mit hohem Anteil an gleichmäßig verteilten Hartphasen mit geringer Korngröße.In order to achieve a higher concentration of hard phases in the material, in particular with a uniform distribution in this, it is known to apply powder metallurgical production methods. Essentially, in these PM processes, an alloyed liquid melt after flowing out of a nozzle is separated by high-pressure gas jets into small droplets which naturally cool at high speed and thereby precipitate fine hard phase particles upon solidification. By a hot isostatic Pressing (HIP) or by deformation of the powder in a container, a production of a largely dense material with a high proportion of uniformly distributed hard phases with a small grain size takes place.

Eine Steigerung der Verschleißresistenz mittels Erhöhung des Volumenanteils von Hartphasen in der Matrix eines Werkstoffes und in der Folge einer Erhöhung der Konzentration der die Hartphasen bildenden Elemente hat jedoch verfahrenstechnische und reaktionskinetische Grenzen. Primäre Ausscheidungen im Flüssigmetall können während des Verdüsungsablaufes zu einer Verringerung der Ausströmung derselben aus der Düse oder zu einem totalen Zuwachsen der Durchtrittsöffnung führen und derart die Herstellbarkeit nachteilig beeinflussen. Größere Legierungsüberhitzungen im Vorratsgefäß einer Anlage zur Metallpulverherstellung können auch metallurgische und/oder reaktionskinetische Nachteile haben.An increase in the wear resistance by increasing the volume fraction of hard phases in the matrix of a material and in consequence of an increase in the concentration of the hard phase-forming elements, however, has procedural and reaction kinetic limits. Primary precipitations in the liquid metal can lead to a reduction in the outflow of the same from the nozzle or to a total growth of the passage opening during the atomization process and thus adversely affect the manufacturability. Larger alloy overheating in the storage vessel of a plant for the production of metal powder may also have metallurgical and / or reaction kinetic disadvantages.

Aufgrund des Bedarfs an höchst verschleißresistenten Werkstoffen, welche gegebenenfalls eine überlegene Korrosionsbeständigkeit aufweisen sollen, wurden vielfach Legierungen vorgeschlagen, welche einen hohen Gehalt an Karbidbildnern, insbesondere Monokarbidbildnern, mit entsprechendem Kohlenstoffgehalt und einer Chromkonzentration in der Matrix von über 12.0 Gew.-% haben.Due to the demand for highly wear-resistant materials, which should possibly have a superior corrosion resistance, alloys have been proposed which have a high content of carbide formers, in particular monocarbide formers, with a corresponding carbon content and a chromium concentration in the matrix of more than 12.0 wt .-%.

In der DE 42 02 339 B4 wird beispielsweise ein korrosionsbeständiger, hochverschleißfester, härtbarer Stahl mit Niobgehalten von 5.0 bis 8.0% Nb vorgeschlagen, welcher ohne Anwendung eines pulvermetallurgischen Verfahrens herstellbar ist.In the DE 42 02 339 B4 For example, a corrosion-resistant, highly wear-resistant, hardenable steel with niobium contents of 5.0 to 8.0% Nb is proposed, which can be produced without the use of a powder metallurgical process.

Um auch bei langsamer Abkühlung eines Bauteiles eine verschleißfeste Matrix mit harter, martensitischer Struktur und einem hohen Karbidanteil zu erreichen, ist gemäß DE 10 2005 020 081 A1 ein hoher Gehalt der Elemente Chrom, Molybdän, Vanadin, und vor allem auch Nickel vorgesehen, weil diese Elemente im ZTU-Schaubild die Perlitnase nach rechts verschieben.In order to achieve a wear-resistant matrix with a hard, martensitic structure and a high carbide content, even with slow cooling of a component, is according to DE 10 2005 020 081 A1 a high content of the elements chromium, molybdenum, vanadium, and especially nickel provided because these elements in the ZTU graph move the perlite nose to the right.

Legierungen, bei welchen kein teures Chrom durch Karbidbildung verloren gehen soll, offenbart die DE 42 31 695 A1 und schlägt vor, einen PM-Werkzeugstahl mit 1 bis 3.5 Gew.-% Stickstoff zu legieren.Alloys in which no expensive chromium is to be lost by carbide formation discloses the DE 42 31 695 A1 and suggests using a PM tool steel with 1 to alloy up to 3.5 wt .-% nitrogen.

Stickstoff zur Hartphasenbildung wird als vorteilhafte Maßnahme für die Herstellung von verschleißbeständigen Werkstoffen in der WO 2007/024 192 A1 vorgeschlagen.Nitrogen for hard phase formation is considered an advantageous measure for the production of wear-resistant materials in the WO 2007/024 192 A1 proposed.

Ausgehend vom technischen Bedarf und dem technologischen Stand der Technik setzt sich die Erfindung zum Ziel, einen Werkstoff anzugeben, welcher einen hohen Widerstand gegen Abtrag bei Abrasionsbeanspruchung aufweist. Mit Vorteil soll dieser Werkstoff in einer Legierungsvariante auch gegen chemische Korrosion beständig zusammengesetzt sein.Based on the technical requirements and the technological state of the art, the invention sets itself the goal of specifying a material which has a high resistance to abrasion under abrasion stress. Advantageously, this material in an alloy variant should also be resistant to chemical corrosion.

Eine weitere Aufgabe der Erfindung ist die Schaffung eines Verfahrens zur Herstellung eines Werkstoffes mit stark verringertem Verschleiß und gegebenenfalls gewünschten Korrosionseigenschaften bzw. hoher Korrosionsbeständigkeit.Another object of the invention is to provide a method for producing a material with greatly reduced wear and optionally desired corrosion properties or high corrosion resistance.

Das Ziel der eingangs genannten Erfindung wird im Wesentlichen durch einen Werkstoff, enthaltend in Gew.-%: Kohlenstoff (C) mehr als 0.3 bis 3.5 Stickstoff (N) 0.05 bis 4.0 Sauerstoff (O) mehr als 0.002 bis 0.25 Niob/Tantal (Nb/Ta) 3.0 bis 18.0 sowie metallische Elemente und Verunreinigungen als Rest
mit einem Gefüge, bestehend aus einer Metallmatrix und in diese eingelagert Hartphasen, mit der Maßgabe erreicht, dass die Hartphasen als Karbide und/oder Nitride und/oder Karbonitride und/oder Oxidkarbonitride gebildet sind und einen Durchmesser von höchstens 50 µm und mindestens 0.2 µm aufweisen.
The object of the invention mentioned at the outset is essentially achieved by a material containing in% by weight: Carbon (C) more than 0.3 to 3.5 Nitrogen (N) 12:05 to 4.0 Oxygen (O) more than 0002 to 12:25 Niobium / tantalum (Nb / Ta) 3.0 to 18.0 as well as metallic elements and impurities as the remainder
with a structure consisting of a metal matrix and embedded in these hard phases, with the proviso that the hard phases are formed as carbides and / or nitrides and / or carbonitrides and / or Kohlenstoffkarbonitride and have a diameter of at most 50 microns and at least 0.2 microns ,

Die Vorteile des erfindungsgemäßen, verschleißfesten Werkstoffes bestehen im Wesentlichen darin, dass infolge der Niob/Tantal-Konzentration von 3.0 bis 18.0 Gew.-% und des Kohlenstoffgehaltes von 0.3 bis 3.0 Gew.-% sowie des Stickstoffgehaltes von 0.05 bis 4.0 Gew.-% hochharte Niob und/oder Tantal-Monokarbide, Mononitride oder Monokarbonitride in homogener Verteilung mit geringem Durchmesser vorliegen und derart ein hoher Abrasionswiderstand erreicht wird.The advantages of the wear-resistant material of the invention consist essentially in the fact that due to the niobium / tantalum concentration of 3.0 to 18.0 wt .-% and the carbon content of 0.3 to 3.0 wt .-% and the nitrogen content of 0.05 to 4.0 wt .-% high-hardness niobium and / or tantalum monocarbides, mononitrides or monocarbonitrides are present in a homogeneous distribution with a small diameter and thus a high abrasion resistance is achieved.

Durch geringere Anteile an Kohlenstoff als 0.3 Gew.-% und Stickstoff als 0.05 Gew.-% kann das Bildungspotential von Verbindungen mit Gehalten von 3.0 bis 18.0 Gew.-% Nb/Ta nicht ausreichend ausgenützt werden, hingegen wirken höhere Gehalte als 3.0 bis 4.0 Gew.-% an Kohlenstoff und Stickstoff gefügeverschlechternd.With lower contents of carbon than 0.3% by weight and nitrogen than 0.05% by weight, the formation potential of compounds with contents of 3.0 to 18.0% by weight Nb / Ta can not be sufficiently exploited, whereas higher contents than 3.0 to 4.0 are effective Wt .-% of carbon and nitrogen microstructural.

Der Sauerstoffgehalt von 0.0020 bis 0.25 im Werkstoff wirkt einerseits als Bildungskeim für die Hartphase im Hinblick auf Hartstoffteilchen mit bestimmter, geringer Größe in homogener Verteilung in der Matrix und andererseits als eigener Hartstoffbildner.The oxygen content of 0.0020 to 0.25 in the material acts on the one hand as a formation nucleus for the hard phase with respect to hard particles with specific, small size in a homogeneous distribution in the matrix and on the other hand as a separate hard material former.

Höhere Sauerstoffgehalte als 0.25 Gew.-% verspröden die Hartphasen, wohingegen geringere Gehalte als 0.0020 Gew.-% keine ausgeprägte Keimwirkung haben.Higher oxygen contents than 0.25 wt .-% embrittle the hard phases, whereas lower contents than 0.0020 wt .-% have no pronounced germination.

Es ist erfindungsgemäß wichtig, dass die Hartstoffteilchen einen Durchmesser von höchstens 50µm aufweisen, weil bei größeren Phasen die Gefahr des Ausbrechens derselben aus der Matrix sprunghaft erhöht ist. Geringere Durchmesser als 0.2µm der Hartphasen erbringen nur eine geringe, abrasionsvermindernde Wirkung.It is important according to the invention that the hard material particles have a diameter of at most 50 μm, because with larger phases the danger of breaking them out of the matrix is suddenly increased. Smaller diameters than 0.2 μm of the hard phases provide only a slight, abrasion-reducing effect.

Wenn, wie gemäß der Erfindung, die Matrix der verschleißbeständigen Legierung eine martensitische Gefügestruktur aufweist, so hat der Werkstoff selbst eine erhöhte abrasionsmindernde Härte, wobei höchstmöglich eine Gefahr des Ausbrechens von Hartphasen aus dem Gefüge bei Verschleißbeanspruchung minimiert ist.If, as in the invention, the matrix of the wear-resistant alloy has a martensitic microstructure, then the material itself has an increased abrasion-reducing hardness, minimizing as far as possible the risk of breaking hard phases out of the structure during wear.

Bei einer Weiterbildung der Erfindung hat sich für einen Werkstoff mit hohem Widerstand gegen Abtrag bei Abrasionsbeanspruchung und mit hoher Korrosionsbeständigkeit eine Zusammensetzung von in Gew.-% Kohlenstoff (C) 0.5 bis 2.5 Stickstoff (N) 0.15 bis 0.6 Silicium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 2.0 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (Nb/Ta) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadium (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest und herstellungsbedingte Verunreinigungen,
mit der Maßgabe, dass der Zusammenhang von Kohlenstoffgehalt und die jeweilige Konzentration von Niob/Tantal sowie Vanadin und Titan einen Wert, gebildet aus % C = 0.3 + % Nb + 2 x % V + % Ti U

Figure imgb0001

erfüllt, und die Zahl U größer als 6, jedoch kleiner als 10 ist, als besonders vorteilhaft herausgestellt.In a development of the invention, for a material with high resistance to abrasion under abrasion stress and with high corrosion resistance, a composition of in% by weight has Carbon (C) 0.5 to 2.5 Nitrogen (N) 12:15 to 0.6 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 2.0 Chrome (Cr) 10.0 to 20.0 Niobium / tantalum (Nb / Ta) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadium (V) 0.1 to 1.0 Titanium (Ti) 0001 to 1.0 Iron (Fe) rest and production-related impurities,
with the proviso that the relationship between carbon content and the respective concentration of niobium / tantalum as well as vanadium and titanium has a value formed from % C = 0.3 + % Nb + 2 x % V + % Ti U
Figure imgb0001

fulfilled, and the number U is greater than 6, but less than 10, as particularly advantageous.

Die Konzentrationen der Legierungsmetalle sind in diesem Werkstoff bezüglich der Kohlenstoffaktivität und der Karbidbildungskinetik der jeweiligen Elemente aufeinander abgestimmt, wobei die Gehalte der Monokarbidbildner maßgebend für die vorgesehene Kohlenstoffkonzentration sind. Stickstoff ist mit einem Gehalt von 0.6 Gew.-% nach obenhin begrenzt, weil im gegebenen Fall die Hartphasen hauptsächlich als Karbide ausgebildet sein sollen. Unter 0.15 Gew.-% Stickstoff ist die Verfestigungswirkung der Matrix zu gering, sodass die Gehaltsgrenzen in Gew.-% 0.15 bis 0.6 Stickstoff sind.The concentrations of the alloying metals are coordinated in this material with respect to the carbon activity and the carbide formation kinetics of the respective elements, the contents of the monocarbide formers being decisive for the intended carbon concentration. Nitrogen is limited with a content of 0.6 wt .-% to the top, because in the given case, the hard phases should be designed mainly as carbides. Below 0.15 wt.% Nitrogen, the solidification effect of the matrix is too low, so that the content limits in wt.% Are 0.15 to 0.6 nitrogen.

Silicium wirkt als Desoxidationsmetall und beeinflusst die Gefügeumwandlung der Legierung bei der Wärmebehandlung. Ein Mindestgehalt von 0.2 Gew.-% Si ist im Hinblick auf eine wirksame Oxidbildung wichtig, wo hingegen höhere Gehalte als 1.5 Gew.-% die Zähigkeit nachteilig beeinflussen.Silicon acts as a deoxidation metal and influences the microstructural transformation of the alloy during the heat treatment. A minimum content of 0.2% by weight of Si is important in terms of effective oxide formation, whereas higher contents than 1.5% by weight adversely affect toughness.

Ein Mangangehalt von 0.3 Gew.-% und mehr ist für eine Abbindung von Schwefel im Metall vorgesehen, wobei über 2.0 Gew.-% Mn eine nachteilig wirkende Austenitstabilität fördert.A manganese content of 0.3% by weight or more is intended for setting sulfur in the metal, with more than 2.0% by weight of Mn promoting disadvantageous austenite stability.

Chrom und Molybdän begründen eine Korrosionsbeständigkeit der Legierung bei Mindestkonzentrationen von 10.0 und 0.5 Gew.-%, können jedoch auch als Karbidbildner wirksam sein. Höhere Gehalte als 20 Gew.-% Cr und 3.0 Gew.-% Mo führen in nachteiliger Weise bei einer Wärmebehandlung zu einer Stabilisierung von Ferrit.Chromium and molybdenum provide corrosion resistance of the alloy at minimum concentrations of 10.0 and 0.5 wt%, but may also be effective as carbide formers. Higher contents than 20% by weight Cr and 3.0% by weight Mo disadvantageously lead to a stabilization of ferrite in a heat treatment.

Vanadin und Titan sollen Gehalte von jeweils 1.0 Gew.-% nicht übersteigen, weil Karbide dieser Elemente im hohen Maße Cr lösen bzw. in das Kristallgitter einbauen, wodurch im Randbereich der Matrix eine Verarmung an Cr entstehen kann.Vanadium and titanium should not exceed contents of 1.0 wt .-%, because carbides of these elements to a large extent dissolve Cr or incorporate into the crystal lattice, which can cause depletion of Cr in the edge region of the matrix.

Durch diese örtliche Chromverarmung erfolgt eine Störung der Ausbildung einer stabilen Passivschicht an der Oberfläche, wodurch die Korrosionsbeständigkeit der Legierung verschlechtert ist. In Gew.-% 0.1 Vanadin und 0.001 Titan wirken für eine Bildung von Monokarbidkeimen günstig.This local chromium depletion interferes with the formation of a stable passive layer on the surface, thereby deteriorating the corrosion resistance of the alloy. In% by weight 0.1 vanadium and 0.001 titanium are favorable for the formation of monocarbide nuclei.

Die Elemente Niob und Tantal sind Elemente, die in der Legierung ab einem Gehalt von 3.0 Gew.-% harte, die Verschleißfestigkeit des Werkstoffes fördernde Monokarbide ausformen. Dabei ist es wichtig, dass diese Elemente Nb/Ta nur eine geringe Neigung zeigen, weitere Elemente, insbesondere Chrom, bei der Karbid- oder Karbonitridbildung in das Kristallgitter einzubauen, sodass im Umfeld dieser Hartphasen keine Verarmung der Matrix an Legierungskomponenten, insbesondere an Chrom und Molybdän, entsteht und somit kein nachteiliger Einfluss auf die Korrosionsbeständigkeit des Werkstoffes entsteht.The elements niobium and tantalum are elements that form in the alloy from a content of 3.0 wt .-% hard, the wear resistance of the material promoting monocarbides. It is important that these elements Nb / Ta show only a slight tendency to incorporate further elements, in particular chromium, in the carbide or carbonitride formation in the crystal lattice, so that in the vicinity of these hard phases no depletion of the matrix of alloy components, especially of chromium and Molybdenum, arises and thus no adverse effect on the corrosion resistance of the material is formed.

Gemäß einer weiteren Ausgestaltung der Erfindung werden ein geringer Verschleiß und eine hohe Korrosionsbeständigkeit des Werkstoffes erreicht, wenn dieser Kohlenstoff (C) mehr als 0.3 bis 1.0 Stickstoff (N) 1.0 bis 4.0 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 1.5 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (Nb/Ta) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadin (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest und herstellungsbedingte Verunreinigungen,
mit der Maßgabe aufweist, dass der Zusammenhang von Stickstoffgehalt und die jeweilige Konzentration von Niob sowie Vanadin einen Wert, gebildet aus % N = 0.3 + % Nb + 2 x % V + % Ti U 1

Figure imgb0002

erfüllt ist, und die Zahl U1 größer als 4 und kleiner als 8 ist.According to a further embodiment of the invention, a low wear and high corrosion resistance of the material is achieved, if this Carbon (C) more than 0.3 to 1.0 Nitrogen (N) 1.0 to 4.0 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 1.5 Chrome (Cr) 10.0 to 20.0 Niobium / tantalum (Nb / Ta) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadin (V) 0.1 to 1.0 Titanium (Ti) 0001 to 1.0 Iron (Fe) rest and production-related impurities,
with the proviso that the relationship between nitrogen content and the respective concentration of niobium and vanadium has a value formed from % N = 0.3 + % Nb + 2 x % V + % Ti U 1
Figure imgb0002

is satisfied, and the number U1 is greater than 4 and less than 8.

Der hohe Stickstoffgehalt von 1.0 bis 4.0 Gew.-% bei Kohlenstoffkonzentrationen von 0.3 bis 1.0 Gew.-% führt zu im Wesentlichen aus Nitriden gebildeten Hartphasen, wobei die durch Chrom und Molybdän bewirkte Passivschichtbildung und die Korrosionsbeständigkeit gefördert werden.The high nitrogen content of 1.0 to 4.0 wt .-% at carbon concentrations of 0.3 to 1.0 wt .-% leads to substantially nitrides formed hard phases, whereby the chromium and molybdenum induced passive layer formation and corrosion resistance are promoted.

Unter Berücksichtigung des Chromgehaltes im Hinblick auf eine Korrosionsbeständigkeit und bei Ausrichtung des Verschleißwiderstandes auf im Wesentlichen Karbide kann gemäß einer weiteren Ausgestaltung der Erfindung ein Werkstoff günstig und wirtschaftlich bereitstellbar sein, der in Gew.-% Kohlenstoff (C) 0.5 bis 3.0 Stickstoff (N) 0.15 bis 0.6 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 2.0 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (NblTa) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadin (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest mit herstellungsbedingten Verunreinigungen
mit der Maßgabe beinhaltet, dass der Zusammenhang von Kohlenstoffgehalt und die jeweilige Konzentration von Niob, Vanadin, Titan und Chrom einen Wert, gebildet aus % C = 0.3 + % Nb + 2 x % V + % Ti U 2 + Cr U 3

Figure imgb0003

erfüllt, und die Zahl U2 größer als 6 und kleiner als 10
und die Zahl U3 größer als 9 und kleiner als 17 sind.Taking into account the chromium content in terms of corrosion resistance and in the orientation of the wear resistance to substantially carbides, according to a further embodiment of the invention, a material can be provided cheaply and economically, which in wt .-% Carbon (C) 0.5 to 3.0 Nitrogen (N) 12:15 to 0.6 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 2.0 Chrome (Cr) 10.0 to 20.0 Niobium / Tantalum (NblTa) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadin (V) 0.1 to 1.0 titanium (Ti) 0001 to 1.0 Iron (Fe) rest with production-related impurities
with the proviso implies that the relationship between carbon content and the respective concentration of niobium, vanadium, titanium and chromium has a value formed from % C = 0.3 + % Nb + 2 x % V + % Ti U 2 + Cr U 3
Figure imgb0003

fulfilled, and the number U2 greater than 6 and less than 10
and the number U3 is greater than 9 and less than 17.

Werden von einem erfindungsgemäßen Werkstoff neben hoher Verschleißfestigkeit auch eine hohe Warmhärte und dgl. Zähigkeit gefordert, wie dies für spanabhebende Werkzeuge von besonderer, größter Bedeutung ist, so kann die Legierung bei abgesenkten Chromgehalten folgende Zusammensetzung und Relationen der Elemente in Gew-% aufweisen Kohlenstoff (C) 1.0 bis 3.5 Stickstoff (N) 0.05 bis 0.4 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 1.0 Chrom (Cr) 2.5 bis 6.0 Niob/Tantal (Nb/Ta) 3.0 bis 18.0 Molybdän (Mo) 2.0 bis 10.0 Wolfram (W) 0.1 bis 12.0 Vanadin (V) 0.1 bis 3.0 Cobalt (Co) 0.1 bis 12.0 Eisen (Fe) Rest mit herstellungsbedingten Verunreinigungen
mit der Maßgabe, dass der Zusammenhang von Kohlenstoffgehalt und die jeweilige Konzentration von Niob/Tantal sowie Vanadin und Titan einen Wert, gebildet aus % C = 0.6 + % Nb + 2 x % V + % Ti U 4 + 2 x % Mo + % W U 5

Figure imgb0004

erfüllt ist, wobei die Zahlenwerte U4 = 6 bis 10 / U5 = 80 bis 100 sind.Be of a material according to the invention in addition to high wear resistance Also, a high hot hardness and the like. Toughness required, as is of special importance for cutting tools, the alloy may have the following composition and ratios of the elements in wt% with lowered chromium contents Carbon (C) 1.0 to 3.5 Nitrogen (N) 12:05 to 0.4 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 1.0 Chrome (Cr) 2.5 to 6.0 Niobium / tantalum (Nb / Ta) 3.0 to 18.0 Molybdenum (Mo) 2.0 to 10.0 Tungsten (W) 0.1 to 12.0 Vanadin (V) 0.1 to 3.0 Cobalt (Co) 0.1 to 12.0 Iron (Fe) rest with production-related impurities
with the proviso that the relationship between carbon content and the respective concentration of niobium / tantalum as well as vanadium and titanium has a value formed from % C = 0.6 + % Nb + 2 x % V + % Ti U 4 + 2 x % Not a word + % W U 5
Figure imgb0004

is satisfied, wherein the numerical values U4 = 6 to 10 / U5 = 80 to 100 are.

Der auf einer Art Schnellstahllegierung basierende, hochverschleißfeste Werkzeugwerkstoff kann auf einfache Weise auf hohe Härtewerte vergütet werden und weist trotz hoher Härte überragende Zähigkeit auf. Besonders ausgeprägt ist die Verschleißfestigkeit der aus dieser Legierung gebildeten Schneidwerkzeuge, welche Werkzeuge dadurch eine besonders hohe Standzeit im groben und unterbrochenen Schnitt haben.The highly wear-resistant tool material, which is based on a type of high-speed steel alloy, can be easily tempered to high hardness values and has outstanding toughness despite its high hardness. Particularly pronounced is the wear resistance of the cutting tools formed from this alloy, which tools thus have a particularly long service life in coarse and interrupted section.

Das erfindungsgemäße Verfahren der eingangs genannten Art ist derart bestimmt, dass in einem ersten Schritt eine metallische, flüssige Legierung, enthaltend Niob/Tantal (Nb/Ta) mit einer Konzentration von 3.0 bis 18.0 Gew.-%, sowie einem Gehalt an Kohlenstoff und/oder Stickstoff, bei welcher keine Primärausscheidungen an Karbiden und/oder Nitriden oberhalb der Verdüsungstemperatur oder Liquidustemperatur gebildet werden, zu Pulvermaterial verdüst wird, wonach das Pulver einem Verfahren zur Erhöhung des Kohlenstoffgehaltes und/oder des Stickstoffgehaltes und/oder des Sauerstoffgehaltes unterworfen und im Folgenden einem Heißkompaktieren, insbesondere einem Heißisostatischen Pressen unterworfen wird, wobei der Pressling bzw. HIP-Körper alternativ einer Warmverformung und/oder einer Wärmebehandlung unterworfen wird.The inventive method of the type mentioned above is determined such that in a first step, a metallic liquid alloy containing niobium / tantalum (Nb / Ta) with a concentration of 3.0 to 18.0 wt .-%, and a content of carbon and / or nitrogen, in which no primary excretions formed on carbides and / or nitrides above the Verdüsungstemperatur or liquidus temperature, is atomized to powder material, after which the powder subjected to a process for increasing the carbon content and / or the nitrogen content and / or the oxygen content and subsequently subjected to a hot compacting, in particular a hot isostatic pressing Alternatively, the pellet or HIP body is subjected to a hot deformation and / or a heat treatment alternatively.

Weil bei hohen Nb/Ta-Gehalten primäre Karbid- und Nitridausscheidungen gebildet werden können, ist es erfindungsgemäß wesentlich, in einer sonst vollständig zusammengesetzten, flüssigen Vorlegierung die Gehalte an Kohlenstoff und Stickstoff unter der Grenze für eine Ausscheidungsbildung zu halten und dieses Flüssigmetall, insbesondere mittels Stickstoffs, zu Pulvermaterial zu verdüsen. Ein derart erhaltenes, festes Metallpulver wird in der Folge bei erhöhter Temperatur durch geeignete Mittel gezielt aufgekohlt und/oder dessen Stickstoffgehalt und/oder Sauerstoffgehalt bis auf vorgesehene Gehalte erhöht. Ein derart in der Zusammensetzung nach der Erfindung eingestelltes Pulver wird in Behältnissen gemäß dem Stand der Technik eingeschlossen, kann durch Heißisostatisches Pressen (HIPen) oder Verformen bei hoher Temperatur kompaktiert und auf gewünschte Abmessungen gebracht werden.Because primary carbide and nitride precipitates can be formed at high Nb / Ta contents, it is important in accordance with the present invention to maintain carbon and nitrogen levels below the limit for precipitate formation in an otherwise fully composite liquid master alloy, and this liquid metal, particularly by Nitrogen, to atomize powder material. A solid metal powder obtained in this way is subsequently carburetted in a targeted manner at elevated temperature by suitable means and / or its nitrogen content and / or oxygen content is increased to intended levels. Such a powder adjusted in the composition according to the invention is enclosed in containers according to the prior art, can be compacted by hot isostatic pressing (HIPing) or deformation at high temperature and brought to desired dimensions.

Das erfindungsgemäße Verfahren hat den Vorteil, dass Werkstoffe mit hohem Karbid-Nitrid- oder Karbonitrid-Hartstoffanteil hergestellt werden können, wobei die Hartstoffpartikel geringe Durchmesser und homogene Verteilung in der Matrix haben. Die Matrixelemente können durch eine thermische Vergütung bzw. durch ein Härten und Anlassen des Werkstoffes diesem eine hohe Festigkeit vermitteln und ein Ausschalen oder Ausbrechen der größeren, optimierten Hartstoffteilchen weitestgehend verhindern. Dadurch wird eine besonders ausgeprägte Verschleißbeständigkeit des Werkstoffes erreicht.The method according to the invention has the advantage that materials with a high carbide-nitride or carbonitride hard material content can be produced, the hard-material particles having small diameters and homogeneous distribution in the matrix. The matrix elements can by a thermal tempering or by hardening and tempering of the material impart this high strength and prevent stripping or breaking the larger, optimized hard particles as far as possible. As a result, a particularly pronounced wear resistance of the material is achieved.

Eine Aufkohlung und/oder einer Erhöhung des Stickstoffgehaltes bei Einstellung des Sauerstoffgehaltes des vorlegierten Metallpulvers kann gemäß der Erfindung durch beigemischten, elementaren Kohlenstoff und/oder durch eine Kohlenstoff und/oder Stickstoff und/oder Sauerstoff abgebende Atmosphäre, insbesondere bei erhöhter Temperatur vor oder bei einer Heißkompaktierung erfolgen.A carburizing and / or an increase in the nitrogen content when adjusting the oxygen content of the pre-alloyed metal powder according to the invention by admixed, elemental carbon and / or by a carbon and / or nitrogen and / or oxygen-emitting atmosphere, in particular at elevated Temperature before or during a hot compaction.

In einer Ausgestaltung der Erfindung können dem Pulverwerkstoff auch weitere Hartstoffpartikel mit einer Größe von 2 bis 50µm in einem Ausmaß bis 25 Vol.-% beigemischt werden, welche in der Folge für den gegebenen Werkstoff verschleißsenkend wirksam sind.In one embodiment of the invention, other hard material particles with a size of 2 to 50 microns to an extent of up to 25 vol .-% can be added to the powder material, which are effective in reducing wear for the given material.

Anhand von lediglich Ausführungswege darstellenden Beispielen sollen im Vergleich mit bekannten Werkstoffen die Eigenschaften der erfindungsgemäßen Legierung
näher dargestellt werden.
By way of examples which merely represent exemplary ways, the properties of the alloy according to the invention are to be compared with known materials
be shown in more detail.

Tab. 1 auf Seite 11 zeigt die Zusammensetzung von zwei handelsüblichen, verschleißfesten Legierungen mit den Bezeichnungen X190 CrVMo 20 4 1, X90 CrVMo 18 1 1, von korrosionsfesten, erfindungsgemäßen Legierungen mit den Bezeichnungen A, B, C, und von Schneidwerkstoffen nach der Erfindung mit den Bezeichnungen D, E, F.Tab. 1 on page 11 shows the composition of two commercially available, wear-resistant alloys with the designations X190 CrVMo 20 4 1, X90 CrVMo 18 1 1, corrosion-resistant, inventive alloys with the designations A, B, C, and of cutting materials according to the invention with the designations D, E, F.

Die handelsüblichen Legierungen waren nach dem PM-Verfahren mit einer Verformung des HIP-Blockes (Heiß-Isostatisch-gepresst) von größer 6-fach
hergestellt worden.
The commercial alloys were after the PM process with a deformation of the HIP block (H eiß- I sostatisch-ge p resst) of greater than 6-fold
been prepared.

Pulver für die Proben mit der Bezeichnung A, B, C wurden aus Legierungen mit folgenden Hauptbestandteilen in Gew.-%: Bezeichnung Si Mn Cr Mo V W Nb Co Fe A 0.43 0.42 11.92 2.21 0.08 0.07 9.02 0.08 Rest B 0.51 0.44 16.41 2.19 0.09 0.07 9.56 0.05 Rest C 0.43 0.42 11.92 2.21 0.05 0.06 9.02 0.08 Rest durch Verdüsen mittels Stickstoffgas hergestellt.Powders for the samples designated A, B, C were made from alloys having the following main components in wt%: description Si Mn Cr Not a word V W Nb Co Fe A 12:43 12:42 11.92 2.21 12:08 12:07 9:02 12:08 rest B 12:51 12:44 16:41 2.19 12:09 12:07 9:56 12:05 rest C 12:43 12:42 11.92 2.21 12:05 12:06 9:02 12:08 rest produced by atomizing by means of nitrogen gas.

Ein Verdüsen mit Stickstoff erfolgte weiters unter Verwendung von Schmelzen mit der Bezeichnung D, E, F mit den Hauptbestandteilen in Gew.-%: Bezeichnung Si Mn Cr Mo V W Nb Co Fe D 0.30 0.40 4.15 2.94 1.52 2.13 3.34 0.12 Rest E 0.28 0.35 3.95 2.84 1.47 2.23 3.45 8.21 Rest F 0.37 0.33 3.58 4.10 1.84 5.07 10.73 7.07 Rest Atomization with nitrogen was further carried out using melts designated D, E, F with the main constituents in% by weight: description Si Mn Cr Not a word V W Nb Co Fe D 12:30 12:40 4.15 2.94 1:52 2.13 3:34 12:12 rest e 12:28 12:35 3.95 2.84 1:47 2.23 3:45 8.21 rest F 12:37 12:33 3:58 4.10 1.84 5:07 10.73 7:07 rest

Als Aufkohlungsmittel wurden versuchsweise für die Werkstoffe mit den Bezeichnungen A bis C verwendet: CH4 + O
Graphit (beigemischt) und Stickstoff + O
CH4 + Stickstoff + O, wobei den Metallpulvern ca. 10% NbC mit einer Korngröße von 28µm beigemischt war.
As carburizing agents were used experimentally for the materials with the designations A to C: CH 4 + O
Graphite (admixed) and nitrogen + O
CH 4 + nitrogen + O, wherein the metal powders about 10% NbC was mixed with a particle size of 28 .mu.m.

Die Metallpulver der weiteren Legierungen D bis F wurden in den Versuchen mit folgenden Aufkohlungs- und Aufstickungsmitteln behandelt:

  • CO + CH4 + O
  • CO + N + O
  • Graphit + CO + N + O
The metal powders of the further alloys D to F were treated in the experiments with the following carburizing and nitriding agents:
  • CO + CH 4 + O
  • CO + N + O
  • Graphite + CO + N + O

Ein Auflegieren der Legierungspulver mit Kohlenstoff, Stickstoff und Sauerstoff
erfolgte bei erhöhter Temperatur.
Alloying the alloy powders with carbon, nitrogen and oxygen
took place at elevated temperature.

Das auflegierte Metallpulver wurde in der Folge unter Stickstoffatmosphäre in Stahlbehälter eingebracht und klopfverdichtet, wonach ein Verschweißen der Behälter und ein Heiß-Isostatisches-Pressen bei einer Temperatur von 1165°C erfolgte.The alloyed metal powder was then placed under nitrogen atmosphere in steel containers and knock compacted, followed by welding of the containers and hot isostatic pressing at a temperature of 1165 ° C.

Nach einem Warmverformen des HIP-Blockes wurden dem Erzeugnis Proben entnommen, analysiert (Tab. 1) und untersucht, wobei wichtige Ergebnisse in Fig. 1 bis Fig. 3 wiedergegeben sind. Tab. 1 Bezeichnung C N Si Mn Cr Mo V W Nb Co X190 CrVMo 20 4 1 1.90 0.20 0.70 0.30 20.00 1.00 4.00 0.60 - - X90 CrVMo 18 1 1 0.90 0.01 0.40 0.40 18.00 1.10 1.00 0.06 - - A 1.45 0.18 0.42 0.41 11.76 2.18 0.08 0.07 8.90 0.08 B 2.30 0.19 0.50 0.43 16.05 2.14 0.09 0.07 9.35 0.05 C 1.45 0.18 0.42 0.41 11.76 2.18 0.05 0.06 8.90 0.08 D 1.30 0.08 0.30 0.40 4.10 2.90 1.50 2.10 3.30 0.12 E 1.40 0.07 0.28 0.35 3.90 2.80 1.45 2.20 3.40 8.10 F 2.45 0.08 0.36 0.32 3.50 4.00 1.80 4.95 10.48 6.90 After hot deformation of the HIP block, the product was sampled, analyzed (Table 1) and examined, with important results in Fig. 1 to Fig. 3 are reproduced. Tab. 1 description C N Si Mn Cr Not a word V W Nb Co X190 CrVMo 20 4 1 1.90 12:20 0.70 12:30 8:00 pm 1:00 4:00 0.60 - - X90 CrVMo 18 1 1 0.90 12:01 12:40 12:40 18:00 1.10 1:00 12:06 - - A 1:45 12:18 12:42 12:41 11.76 2.18 12:08 12:07 8.90 12:08 B 30.2 12:19 12:50 12:43 16.5 2.14 12:09 12:07 9:35 12:05 C 1:45 12:18 12:42 12:41 11.76 2.18 12:05 12:06 8.90 12:08 D 1.30 12:08 12:30 12:40 4.10 2.90 1:50 2.10 3.30 12:12 e 1:40 12:07 12:28 12:35 3.90 2.80 1:45 2.20 3:40 8.10 F 2:45 12:08 12:36 12:32 3:50 4:00 1.80 4.95 10:48 6.90

Tab. 1 zeigt die chemische Zusammensetzung von bekannten Werkstoffen (X190 CrVMo 20 4 1 sowie X90 CrMoV 18 1 1) und jene von Stahlproben gemäß der ErfindungTable 1 shows the chemical composition of known materials (X190 CrVMo 20 4 1 and X90 CrMoV 18 1 1) and those of steel samples according to the invention

Korrosionsverhalten:Corrosion behavior:

Das Korrosionsverhalten der Legierungen wurde anhand von Stromdichte-PotentialKurven an den Proben nach ASTM G65 in 1 n H2SO4, 20°C ermittelt, wobei eine Abschreckung derselben von 1100°C bzw. 1070°C und ein Anlassen bei 200°C erfolgten.The corrosion behavior of the alloys was determined from current density potential curves on the samples according to ASTM G65 in 1N H 2 SO 4 , 20 ° C, with a quenching of the same from 1100 ° C and 1070 ° C and a tempering at 200 ° C. ,

Wie aus Fig. 1 hervorgeht, weist im relevanten Potentialbereich von etwa -300mV bis +300mV die Vergleichslegierung X190 CrVMo 20 4 1 im Wesentlichen die höchste Passivstromdichte im Vergleich mit den erfindungsgemäß zusammengesetzten Proben A, B, C auf, was deren verbessertes Korrosionsverhalten offenbart.How out Fig. 1 shows, in the relevant potential range of about -300mV to + 300mV, the comparative alloy X190 CrVMo 20 4 1 essentially the highest passive current density in comparison with the inventively assembled samples A, B, C, which reveals their improved corrosion behavior.

Fig. 2 zeigt die Härte der unterschiedlich zusammengesetzten Legierungen nach einem Härten in Abhängigkeit von der Anlasstemperatur nach zweimaligem Anlassen. Fig. 2 shows the hardness of the differently composite alloys after hardening as a function of the tempering temperature after two tempering.

Die jeweilige Härtetemperatur ist dem Bezeichnungsfeld für die Legierungen entnehmbar.The respective hardening temperature can be taken from the designation field for the alloys.

Im Vergleich mit X190 CrVMo 20 4 1 weisen die Werkstoffe A und C der erfindungsgemäßen Legierung eine vergleichbar niedrige Anlasshärte auf, weil deren jeweiliger Kohlenstoffgehalt einer verbesserten Korrosionsbeständigkeit wegen (siehe Fig.1) niedrig gewählt wurde.In comparison with X190 CrVMo 20 4 1, the materials A and C of the alloy according to the invention on a comparatively low tempering hardness, because their respective carbon content of improved corrosion resistance due to (see Fig.1 ) was chosen low.

Die Werkstoffhärte der Legierungen D, E und F liegen im Bereich von Anlasstemperaturen zwischen 500°C und 600°C entscheidend höher, was eine deutliche Überlegenheit derselben für einen Einsatz von beispielsweise Schneid- und Formelementen offenlegt.The material hardness of the alloys D, E and F are significantly higher in the range of tempering temperatures between 500 ° C and 600 ° C, which discloses a clear superiority of the same for use of, for example, cutting and forming elements.

Fig. 3 zeigt das Verschleißverhalten der aus den Legierungen gefertigten Proben, ermittelt nach dem in VDI Fortschrittberichte "Stickstofflegierte Werkzeugstähle", Reihe 5, Nr. 188 (1990), S. 129 beschriebenen Stift-Scheibe-Test mit Flint 80er Körnung. Die Härten der Proben sind über den jeweiligen Balken in Fig. 3 angegeben. Sowohl die korrosionsbeständige Legierung B als auch die Legierungen E und F gemäß der Erfindung zeigen überragenden Widerstand gegen Verschleiß, was auf eine entsprechend günstige Wahl von Kohlenstoff- und Niobgehalten hinweist. Fig. 3 shows the wear behavior of the samples made from the alloys, determined according to the VDI Progress Reports "Nitrogen-alloyed Tool Steels", Series 5, No. 188 (1990), p. 129 described pin-disk test with Flint 80s Grain. The hardnesses of the samples are above the respective bars in Fig. 3 specified. Both the corrosion resistant alloy B and the alloys E and F according to the invention show superior resistance to wear, indicating a correspondingly favorable choice of carbon and niobium contents.

Claims (8)

Verschleißbeständiger Werkstoff, enthaltend in Gew.-%: Kohlenstoff (C) mehr als 0.3 bis 3.5 Stickstoff (N) 0.05 bis 4.0 Sauerstoff (O) mehr als 0.002 bis 0.25 Niob/Tantal (Nb/Ta) 3.0 bis 18.0
sowie metallische Elemente und Verunreinigungen als Rest
mit einem Gefüge, bestehend aus einer Metallmatrix und in diese eingelagert Hartphasen, mit der Maßgabe, dass die Hartphasen als Karbide und/oder Nitride und/oder Karbonitride und/oder Oxidkarbonitride gebildet sind und einen Durchmesser von höchstens 50 µm und mindestens 0.2 µm aufweisen.
Wear-resistant material, containing in% by weight: Carbon (C) more than 0.3 to 3.5 Nitrogen (N) 12:05 to 4.0 Oxygen (O) more than 0002 to 12:25 Niobium / tantalum (Nb / Ta) 3.0 to 18.0
as well as metallic elements and impurities as the remainder
with a structure consisting of a metal matrix and embedded in these hard phases, with the proviso that the hard phases are formed as carbides and / or nitrides and / or carbonitrides and / or Kohlenstoffkarbonitride and have a diameter of at most 50 microns and at least 0.2 microns.
Verschleißbeständiger Werkstoff nach Anspruch 1, bei welchem die Matrix eine martensitische Gefügestruktur aufweist.The wear resistant material of claim 1, wherein the matrix has a martensitic structure. Verschleißbeständiger Werkstoff nach Anspruch 1 oder 2 mit hoher Korrosionsbeständigkeit, enthaltend in Gew.-%. Kohlenstoff (C) 0.5 bis 2.5 Stickstoff (N) 0.15 bis 0.6 Silicium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 2.0 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (Nb/Ta) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadium (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest
und herstellungsbedingte Verunreinigungen,
mit der Maßgabe, dass der Zusammenhang von Kohlenstoffgehalt und der Konzentration von Niob/Tantal sowie Vanadin und Titan einen Wert, gebildet aus % C = 0.3 + % Nb + 2 x % V + % Ti U
Figure imgb0005

erfüllt, wobei die Zahl U größer als 6, jedoch kleiner als 10 ist.
A wear-resistant material according to claim 1 or 2 having high corrosion resistance, containing in% by weight. Carbon (C) 0.5 to 2.5 Nitrogen (N) 12:15 to 0.6 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 2.0 Chrome (Cr) 10.0 to 20.0 Niobium / tantalum (Nb / Ta) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadium (V) 0.1 to 1.0 Titanium (Ti) 0001 to 1.0 Iron (Fe) rest
and production-related impurities,
with the proviso that the relationship between carbon content and the concentration of niobium / tantalum as well as vanadium and titanium has a value formed from % C = 0.3 + % Nb + 2 x % V + % Ti U
Figure imgb0005

fulfilled, wherein the number U is greater than 6, but less than 10.
Verschleißbeständiger Werkstoff nach Anspruch 1 oder 2 mit hoher Korrosionsbeständigkeit, enthaltend in Gew.-%: Kohlenstoff (C) mehr als 0.3 bis 1.0 Stickstoff (N) 1.0 bis 4.0 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 1.5 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (Nb/Ta) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadin (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest
und herstellungsbedingte Verunreinigungen,
mit der Maßgabe, dass der Zusammenhang von Stickstoffgehalt und der Konzentration von Niob sowie Vanadin einen Wert, gebildet aus % N = 0.3 + % Nb + 2 x % V + % Ti U 1
Figure imgb0006

erfüllt, wobei die Zahl U1 größer als 4, jedoch kleiner als 8 ist.
Wear-resistant material according to claim 1 or 2 with high corrosion resistance, containing in wt .-%: Carbon (C) more than 0.3 to 1.0 Nitrogen (N) 1.0 to 4.0 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 1.5 Chrome (Cr) 10.0 to 20.0 Niobium / tantalum (Nb / Ta) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadin (V) 0.1 to 1.0 Titanium (Ti) 0001 to 1.0 Iron (Fe) rest
and production-related impurities,
with the proviso that the relationship between nitrogen content and the concentration of niobium as well as vanadium has a value formed from % N = 0.3 + % Nb + 2 x % V + % Ti U 1
Figure imgb0006

fulfilled, wherein the number U1 is greater than 4, but less than 8.
Verschleißfester Werkstoff nach Anspruch 1 oder 2 mit hoher Korrosionsbeständigkeit, enthaltend in Gew.-%: Kohlenstoff (C) 0.5 bis 3.0 Stickstoff (N) 0.15 bis 0.6 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 2.0 Chrom (Cr) 10.0 bis 20.0 Niob/Tantal (Nb/Ta) 3.0 bis 15.0 Molybdän (Mo) 0.5 bis 3.0 Vanadin (V) 0.1 bis 1.0 Titan (Ti) 0.001 bis 1.0 Eisen (Fe) Rest
mit herstellungsbedingten Verunreinigungen
mit der Maßgabe, dass der Zusammenhang von Kohlenstoffgehalt und der Konzentration von Niob, Vanadin, Titan und Chrom einen Wert, gebildet aus % C = 0.3 + % Nb + 2 x % V + % Ti U 2 + Cr U 3
Figure imgb0007

erfüllt, wobei die Zahlenwerte U2 größer als 6, jedoch kleiner als 10 und U3 größer als 9, jedoch kleiner als 17 sind.
Wear-resistant material according to claim 1 or 2 with high corrosion resistance, containing in% by weight: Carbon (C) 0.5 to 3.0 Nitrogen (N) 12:15 to 0.6 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 2.0 Chrome (Cr) 10.0 to 20.0 Niobium / tantalum (Nb / Ta) 3.0 to 15.0 Molybdenum (Mo) 0.5 to 3.0 Vanadin (V) 0.1 to 1.0 Titanium (Ti) 0001 to 1.0 Iron (Fe) rest
with production-related impurities
with the proviso that the relationship between carbon content and the concentration of niobium, vanadium, titanium and chromium is a value formed from % C = 0.3 + % Nb + 2 x % V + % Ti U 2 + Cr U 3
Figure imgb0007

fulfilled, wherein the numerical values U2 are greater than 6, but less than 10 and U3 greater than 9, but less than 17.
Verschleißbeständiger Werkstoff nach Anspruch 1 oder 2 mit hoher Warmhärte und Zähigkeit, insbesondere für spanabhebende Werkzeuge, enthaltend in Gew.-%: Kohlenstoff (C) 1.0 bis 3.5 Stickstoff (N) 0.05 bis 0.4 Silizium (Si) 0.2 bis 1.5 Mangan (Mn) 0.3 bis 1.0 Chrom (Cr) 2.5 bis 6.0 Niob/Tantal (Nb/Ta) 3.0 bis 18.0 Molybdän (Mo) 2.0 bis 10.0 Wolfram (W) 0.1 bis 12.0 Vanadin (V) 0.1 bis 3.0 Cobalt (Co) 0.1 bis 12.0 Eisen (Fe) Rest
mit herstellungsbedingten Verunreinigungen
mit der Maßgabe, dass der Zusammenhang von Kohlenstoffgehalt und der Konzentration von Niob/Tantal sowie Vanadin und Titan einen Wert, gebildet aus % C = 0.6 + % Nb + 2 x % V + % Ti U 4 + 2 x % Mo + % W U 5
Figure imgb0008

erfüllt, wobei die Zahlenwerte U4 = 6 bis 10 und U5 = 80 bis 100 sind.
Wear-resistant material according to claim 1 or 2 with high hot hardness and toughness, in particular for cutting tools, containing in wt .-%: Carbon (C) 1.0 to 3.5 Nitrogen (N) 12:05 to 0.4 Silicon (Si) 0.2 to 1.5 Manganese (Mn) 0.3 to 1.0 Chrome (Cr) 2.5 to 6.0 Niobium / tantalum (Nb / Ta) 3.0 to 18.0 Molybdenum (Mo) 2.0 to 10.0 Tungsten (W) 0.1 to 12.0 Vanadin (V) 0.1 to 3.0 Cobalt (Co) 0.1 to 12.0 Iron (Fe) rest
with production-related impurities
with the proviso that the relationship between carbon content and the concentration of niobium / tantalum as well as vanadium and titanium has a value formed from % C = 0.6 + % Nb + 2 x % V + % Ti U 4 + 2 x % Not a word + % W U 5
Figure imgb0008

fulfilled, wherein the numerical values U4 = 6 to 10 and U5 = 80 to 100 are.
Verfahren zur Herstellung eines verschleißbeständigen Werkstoffes, insbesondere nach Anspruch 1 oder 2, wobei in einem ersten Schritt eine metallische, flüssige Legierung, enthaltend Niob/Tantal (Nb/Ta) mit einer Konzentration von 3.0 bis 18.0 Gew.-%, sowie einem Gehalt an Kohlenstoff und/oder Stickstoff, bei welcher keine Primärausscheidungen an Karbiden und/oder Nitriden oberhalb der Verdüsungstemperatur oder Liquidustemperatur gebildet werden, zu Pulvermaterial verdüst wird, wonach das Pulver einem Verfahren zur Erhöhung des Kohlenstoffgehaltes und/oder des Stickstoffgehaltes und/oder des Sauerstoffgehaltes unterworfen und im Folgenden einem Heißkompaktieren, insbesondere einem Heißisostatischen Pressen unterworfen wird, wobei der Pressling bzw. HIP-Körper alternativ einer Warmverformung und/oder einer Wärmebehandlung unterworfen wird.A method for producing a wear-resistant material, in particular according to claim 1 or 2, wherein in a first step, a metallic liquid alloy containing niobium / tantalum (Nb / Ta) with a concentration of 3.0 to 18.0 wt .-%, and a content of Carbon and / or Nitrogen, in which no primary precipitates of carbides and / or nitrides are formed above the atomization temperature or liquidus temperature, is atomized to powder material, after which the powder subjected to a process for increasing the carbon content and / or the nitrogen content and / or the oxygen content and then a hot compacting , in particular a hot isostatic pressing, wherein the pressed body or HIP body is alternatively subjected to a hot working and / or a heat treatment. Verfahren nach Anspruch 7 zur Herstellung von insbesondere verschleißbeständigen Werkstoffen gemäß den Ansprüchen 3 bis 6, wobei das Pulver mit elementarem Kohlenstoff gemischt und/oder in einer Kohlenstoff und Stickstoff abgebenden Atmosphäre gegebenenfalls bei erhöhter Temperatur behandelt und nachfolgend kompaktiert wird.A method according to claim 7 for the preparation of particular wear-resistant materials according to claims 3 to 6, wherein the powder is mixed with elemental carbon and / or treated in a carbon and nitrogen-releasing atmosphere optionally at elevated temperature and subsequently compacted.
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