EP0227001B1 - Method for manufacturing tools - Google Patents

Method for manufacturing tools Download PDF

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Publication number
EP0227001B1
EP0227001B1 EP86117455A EP86117455A EP0227001B1 EP 0227001 B1 EP0227001 B1 EP 0227001B1 EP 86117455 A EP86117455 A EP 86117455A EP 86117455 A EP86117455 A EP 86117455A EP 0227001 B1 EP0227001 B1 EP 0227001B1
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Prior art keywords
process according
phase
grain size
grain
deformation
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German (de)
French (fr)
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EP0227001A3 (en
EP0227001A2 (en
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Frommeyer Georg Dr
Robert Zapp Werkstofftechnik & Co KG GmbH
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Frommeyer Georg Dr
Robert Zapp Werkstofftechnik & Co KG GmbH
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    • 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
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/005Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
    • 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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/16Both compacting and sintering in successive or repeated steps
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/10Alloys containing non-metals

Definitions

  • the invention relates to a method for producing tools from alloyed steels or stellites by thermoforming.
  • Tool steels and stellites or hard metals are generally characterized by high levels of carbon, chromium, cobalt, molybdenum, vanadium and tungsten. Together with the corresponding carbides, these elements give the material the necessary strength, in particular wear resistance and hardness. However, this is usually at the expense of toughness and is associated with a corresponding increase in the resistance to deformation.
  • a method is known from US Pat. No. 3,951,697 is known in which steels with a very high carbon content are set after a heat treatment at at least 500 ° C by deformation on an equiaxed basic structure with a finely dispersed spherulitic cementite.
  • This process is also suitable for the use of powders as the starting material. This is done in such a way that a starting powder with a carbon content of more than 1%, the carbon of which is predominantly in the form of spherulitic cementite, is mixed with an iron powder with a grain size of less than 10 ⁇ m, then compacted and then sintered at 600 to 700 ° C.
  • the structure of the sintered compact mainly consists of a coaxial grain with an average grain size of less than 10 ⁇ m and an evenly distributed, mainly spherulitic cementite in the temperature range from 723 to 900 ° C. Apart from powder compaction, no deformation takes place in the known method. In addition, the process only affects iron-carbon materials with a carbon content of over 1.0% and otherwise only impurities such as 0.4 to 0.5% manganese and 0.1 to 0.2% silicon.
  • the invention has for its object to provide a method which avoids the aforementioned disadvantages and allows the production of finished parts from alloys, which due to their high deformation resistance normally cannot be deformed or at most can be deformed into a blank which requires machining.
  • a stellitic preform with an equiaxial structure and over 30 vol.% Carbidic and / or boridic precipitation phase is thermoformed at 700 to 1000.degree. C., thereby forming a matrix with a grain size of 1 to 3 ⁇ m and one Elimination phase set with a grain size of 0.2 to 1.0 ⁇ m and finally superplastically shaped.
  • the small grain size set in the process according to the invention ensures a low yield stress due to grain boundary sliding and thus reduces the required forming force and tool wear.
  • the method according to the invention therefore runs in two stages;
  • the first stage of the process is to use the powder-metallurgically produced, due to the high cooling rate of, for example, 104 to 105 SchmelzK / s during melt atomization, already fine crystalline, preferably already equiaxial, multi-phase structure of the alloy powder both with regard to the matrix and also with regard to the carbidic and / or boridic precipitation phase to further refine the consolidated state and thereby a thermally stable microstructure during the subsequent thermomechanical processing as a result of hot forming in the second process stage, with a grain size of 1 to 3 ⁇ m or 0.2 to 1.0, which is preferably fine both for the matrix and for the precipitation phase ⁇ m.
  • the material structure in the first process stage can be conditioned by thermomechanical processing, which is the case with steel alloys in austenitic Condition, for example, begins at about 900 o C and the ⁇ / ⁇ phase conversion in the range from 750 to 820 o C to a final rolling temperature of 650 o C goes through.
  • thermomechanical processing which is the case with steel alloys in austenitic Condition, for example, begins at about 900 o C and the ⁇ / ⁇ phase conversion in the range from 750 to 820 o C to a final rolling temperature of 650 o C goes through.
  • the material to be deformed cools down continuously and, in addition to the phase change, the carbides and / or borides are eliminated.
  • the carbides and / or borides are eliminated in the hot forming of stellites in the temperature range from 1000 to 700 ° C. during the shaping and the associated continuous cooling.
  • thermomechanical conditioning there is a refinement of the matrix grain, which is then equiaxial at the latest, as well as a finer dispersion of the carbide and boride particles as a result of the favorable conditions for nucleation during the phase change. Both have an impact in the direction of higher material strength.
  • the conditioning of the starting material produced by powder metallurgy can also be carried out by isothermal shaping with the aim of recrystallizing the structure and setting a fine-grained structure as a prerequisite for the superplastic state.
  • the isothermal deformation takes place at temperatures below the transformation temperature, for example at 450 ° C., preferably with a low degree of deformation, for example with a cross-sectional decrease of about 10%, and should include a cyclic ⁇ / ⁇ phase transformation which, owing to the different volumes of the ⁇ and ⁇ phase to internal tensions and thus to internal internal tensions induced deformation of the matrix grain.
  • This can be followed by a short primary recrystallization annealing, for example 20 to 60 seconds, to refine the matrix grain size of the hot isostatically pressed blank, which leads to a further grain refinement.
  • the aim of the conditioning of the starting material is to establish a structure which is equiaxial for superplastic shaping in the second process stage and which is characterized by a fine structure grain which favors the forming behavior.
  • the resistance to deformation is reduced and, at the same time, the rate of deformation can be increased.
  • the formed material which is adjusted to a specific multiphase structure, is shaped at a temperature in the order of 50 to 70% of the melting temperature of, for example, 650 to 780 o C, which allows high degrees of deformation at low flow stresses and therefore also manufacture Complicated finished parts made of alloys, the composition of which does not allow shaping by forming without the special pretreatment of the first stage of the method according to the invention.
  • the forming speed is preferably 10 ⁇ 3 to 5.10 ⁇ 1 s ⁇ 1.
  • the forming temperature is below the temperature of the beginning secondary crystallization or grain coarsening, since each grain growth increases the resistance to deformation and therefore requires higher deformation forces.
  • the method according to the invention is particularly suitable for high-carbon cold work steels such as X 178 Cr V 5 2 9 X 155 Cr VW Co 4 5 12 5 X 135 Cr VW Mo 4 4 6 4 X 220 Cr V 17 6 X 245 Cr V 5 10 These have carbon contents from 1.0 to 2.5% and high alloy contents of chromium, vanadium, tungsten, molybdenum and cobalt from 4 to 17%.
  • the following alloys are also suitable: X 375 Cr Mo Fe 25 10 60 X 220 Cr W Co 30 12 56 X 120 Cr Mo Co 27 4 60 X 100 Cr W Co NB 15 15 52 3.
  • the Stellite are iron and cobalt-based stellite with high boron and carbon contents of 1 to 4%, and contents of the alloying elements chromium, molybdenum, tungsten, 15 to 30%, which can be transformed at a relatively low temperature of 650-720 o C.
  • the superplastic shape can be followed by coarse grain annealing in order to increase the creep resistance or heat resistance.
  • the round blank 1 shown in FIG. 1 consists of the high-strength cold work steel X 245 Cr V 5 10, which was produced by powder metallurgy by hot isostatic pressing and was set to a structure with a matrix grain size of 1 to 3 ⁇ m. It serves to manufacture the disk-shaped rotary knife shown in FIG. 2 with a cone angle ⁇ of 150 to 160 ° , a thickness of 1.0 to 1.5 mm and an inner diameter of 50 mm and an outer diameter of 100 mm.
  • the circular blank 1 was produced by punching from a powder metallurgy and then rolled out at a temperature of 1150 to 1250 ° C. to a thickness of 2.5 mm and measuring 100 ⁇ 200 ⁇ 8 mm. In order to create a sufficient material reserve for the formation of the cutting edges 2 of the rotary knife, the thickness of the board exceeded the finished thickness of the rotary knife by 1 mm.
  • the low forming temperature saves energy, ensures minimal scaling and prevents harmful grain growth.
  • superplastic forming results in a higher density because pores and cracks weld, as well as higher strength and toughness. Because there is no machining, there are no fatigue cracks in the machining grooves, which increases the tool life by 25 to 30%.
  • the method according to the invention is suitable for producing cut bells and tools, shape cutting tools, knives, for example disc, filter and tobacco knives with a thickness of less than 3 mm, embossing dies, jam and pressure rings for extruders, sintering compression tools, extrusion tools and dies, molding tools for the wobble extrusion and multi-hole plates each made of cold work steels, for the production of profile milling cutters, form turning steels and profile countersunk heads from high speed steels as well as for the production of glass blow molding tools, profile rods, nozzles, impellers, turbine disks and valve seats made of stellites. It is characterized by low forming temperatures and a low power requirement.
  • the finely dispersed, equiaxial and texture-free microstructure guarantees constant and reproducible mechanical properties, in particular high strength with excellent ductility and good fatigue behavior.
  • the dimensional accuracy and surface quality are so good that reworking is not necessary.
  • the surface roughness is usually less than 1 ⁇ m.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
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  • Treatment Of Steel In Its Molten State (AREA)

Abstract

To manufacture tools from medium- and high-alloy steels or stellites by superplastic precision-forming, a powder-metallurgically produced starting material of equiaxial structure with more than 30 % by volume of a carbidic and/or boridic precipitation phase of a particle size of 1 to 0.2 mu m is adjusted by thermomechanical processing (hot-forming) to a matrix grain size of 1 to 3 mu m and formed in the superplastic state. <IMAGE>

Description

Die Erfindung bezieht sich auf ein Verfahren zum Herstellen von Werkzeugen aus legierten Stählen oder Stelliten durch Warmformen.The invention relates to a method for producing tools from alloyed steels or stellites by thermoforming.

Werkzeugstähle und Stellite bzw. Hartmetalle zeichnen sich im allgemeinen durch hohe Gehalte an Kohlenstoff, Chrom, Kobalt, Molybdän, Vanadium und Wolfram aus. Diese Elemente verleihen dem Werkstoff zusammen mit den entsprechenden Karbiden die notwendige Festigkeit, insbesondere Verschleißfestigkeit und Härte. Das geht jedoch zumeist auf Kosten der Zähigkeit und ist mit einer entsprechenden Erhöhung des Verformungswiderstandes verbunden.Tool steels and stellites or hard metals are generally characterized by high levels of carbon, chromium, cobalt, molybdenum, vanadium and tungsten. Together with the corresponding carbides, these elements give the material the necessary strength, in particular wear resistance and hardness. However, this is usually at the expense of toughness and is associated with a corresponding increase in the resistance to deformation.

Bei hohem Verformungswiderstand scheidet das Kalt-, aber auch das konventionelle Warmumformen zum Erzeugen der Fertigkontur aus und kommt demzufolge nur ein Urformen durch Block- oder Stranggießen und ein anschließendes Walzen oder Schmieden, oder ein Formgießen und Pulverpressen in Frage. Diese Verfahren erfordern jedoch in aller Regel eine spanende Bearbeitung des urgeformten Teils bis zur Fertigkontur und zum Fertigmaß. Das aber stößt gerade bei verschleißfesten Teilen insofern auf Schwierigkeiten, als die spanende Bearbeitung Werkzeuge mit einer Verschleißfestigkeit erfordert, die die verschleißfestigkeit des zu bearbeitenden Teils erheblich übersteigt. Außerdem ist spanende Bearbeitung mit einem erheblichen Materialverlust verbunden. Die Bearbeitungskosten sind daher erheblich, ohne daß sich immer eine gute oberflachenbeschaffenheit ergibt.With high resistance to deformation, cold as well as conventional hot forming to create the finished contour are ruled out and, as a result, only undergo primary shaping Block or continuous casting and a subsequent rolling or forging, or a molding and powder pressing in question. However, as a rule, these processes require machining of the preformed part to the finished contour and finished size. However, this is particularly difficult with wear-resistant parts insofar as machining requires tools with a wear resistance that significantly exceeds the wear resistance of the part to be machined. In addition, machining is associated with a considerable loss of material. The processing costs are therefore considerable without always having a good surface finish.

Hinzu kommen verfahrensspezifische Nachteile wie die hohen Energiekosten des Warmwalzens und -schmiedens oder die Beeinträchtigung der Oberflächenqualität durch intensive Oxydationsvorgänge der Legierungen. Ein weiterer Nachteil ist das gerade im Hinblick auf verwickelte Fertigformen zumeist nicht ausreichende Fließvermögen beim Urformen wie auch beim Formgießen. Das führt zu Rohlingen, die sich erheblich vom Fertigteil unterscheiden und daher eine zu einem erheblichen Materialverlust führende spanende Bearbeitung erfordern. Die damit verbundenen Kosten sind wegen der hohen Gehalte der betreffenden Werkstoffe an teuren Legierungsmitteln ganz erheblich. Hinzu kommt die aus dem hohen Verformungswiderstand resultierende Notwendigkeit hoher Verformungskräfte, die entsprechend teure Umformaggregate und hohe Energiekosten mit sich bringen.There are also process-specific disadvantages such as the high energy costs of hot rolling and forging or the impairment of the surface quality due to intensive oxidation processes of the alloys. Another disadvantage is that, especially with regard to entangled finished molds, the fluidity is usually not sufficient for primary molding as well as for molding. This leads to blanks that differ significantly from the finished part and therefore require machining that leads to a considerable loss of material. The associated costs are very considerable due to the high content of expensive alloying agents in the materials concerned. In addition, there is the need for high deformation forces resulting from the high resistance to deformation, which entails correspondingly expensive forming units and high energy costs.

Aus der US-Patentschrift 3 951 697 ist ein Verfahren bekannt, bei dem Stähle mit sehr hohem Kohlenstoffgehalt im Anschluß an eine Wärmebehandlung bei mindestens 500°C im Wege einer Verformung auf ein gleichachsiges Grundgefüge mit einem feindispers verteilten sphärolithischen Zementit eingestellt werden. Dieses Verfahren eignet sich auch für die Verwendung von Pulvern als Ausgangsmaterial. Dies geschieht in der Weise, daß ein Ausgangspulver mit einem Kohlenstoffgehalt über 1%, dessen Kohlenstoff überwiegend als sphärolithischer Zementit vorliegt, mit einem Eisenpulver einer Korngröße unter 10 µm gemischt, anschließend verdichtet und sodann bei 600 bis 700°C gesintert wird. Das Gefüge des gesinterten Preßlings besteht überwiegend aus einem gleichachsigen Korn mit einer mittleren Korngröße unter 10 µm und einem gleichmäßig verteilten, im Temperaturbereich von 723 bis 900°C vornehmlich sphärolithischen Zementit. Außer dem Pulververdichten findet bei dem bekannten Verfahren keine Verformung statt. Darüber hinaus betrifft das Verfahren ausschließlich Eisen-Kohlenstoff-Werkstoffe mit einem Kohlenstoffgehalt über 1,0% und ansonsten lediglich Verunreinigungen wie 0,4 bis 0,5% Mangan und 0,1 bis 0,2% Silizium.A method is known from US Pat. No. 3,951,697 is known in which steels with a very high carbon content are set after a heat treatment at at least 500 ° C by deformation on an equiaxed basic structure with a finely dispersed spherulitic cementite. This process is also suitable for the use of powders as the starting material. This is done in such a way that a starting powder with a carbon content of more than 1%, the carbon of which is predominantly in the form of spherulitic cementite, is mixed with an iron powder with a grain size of less than 10 μm, then compacted and then sintered at 600 to 700 ° C. The structure of the sintered compact mainly consists of a coaxial grain with an average grain size of less than 10 µm and an evenly distributed, mainly spherulitic cementite in the temperature range from 723 to 900 ° C. Apart from powder compaction, no deformation takes place in the known method. In addition, the process only affects iron-carbon materials with a carbon content of over 1.0% and otherwise only impurities such as 0.4 to 0.5% manganese and 0.1 to 0.2% silicon.

Der Erfindung liegt nun die Aufgabe zugrunde, ein Verfahren zu schaffen, das die vorerwähnten Nachteile vermeidet und das Herstellen von Fertigteilen aus Legierungen erlaubt, die sich wegen ihres hohen Verformugswiderstandes normalerweise nicht umformen oder allenfalls zu einem Rohling verformen lassen, der eine spanende Bearbeitung erfordert.The invention has for its object to provide a method which avoids the aforementioned disadvantages and allows the production of finished parts from alloys, which due to their high deformation resistance normally cannot be deformed or at most can be deformed into a blank which requires machining.

Die Lösung dieser Aufgabe besteht darin, daß bei einem Verfahren der eingangs erwähnten Art erfindungsgemäß ein Vorkörper aus einem hochlegierten Stahl mit äquiaxialem Gefüge und über 30 Vol.-% karbidischer und/oder boridischer Ausscheidungsphase unterhalb A₁ mit einer zyklischen Alpha/Gamma Phasenumwandlung oder im austenitischen Zustand warmverformt und dabei auf eine Matrix mit einer Korngröße von 1 bis 3 µm und einer Ausscheidungsphase mit einer Korngröße von 0,2 bis 1,0 µm eingestellt sowie abschließend superplastisch fertiggeformt wird.The solution to this problem is that in a method of the type mentioned in the invention, a preform made of a high-alloy steel with an equiaxial structure and over 30 vol .-% carbidic and / or boridic elimination phase below A 1 with a cyclic alpha / gamma phase transformation or in the austenitic state thermoformed and adjusted to a matrix with a grain size of 1 to 3 µm and a separation phase with a grain size of 0.2 to 1.0 µm and finally superplastically shaped.

Bei einer alternativen Lösung der vorerwähnten Aufgabe wird hingegen ein stellitischer Vorkörper mit äquiaxialem Gefüge und über 30 Vol.-% karbidischer und/oder boridischer Ausscheidungsphase bei 700 bis 1000°C warmverformt und dabei auf eine Matrix mit einer Korngröße von 1 bis 3 µm und eine Ausscheidungsphase mit einer Korngröße von 0,2 bis 1,0 µm eingestellt sowie abschließend superplastisch fertiggeformt.In an alternative solution to the above-mentioned task, on the other hand, a stellitic preform with an equiaxial structure and over 30 vol.% Carbidic and / or boridic precipitation phase is thermoformed at 700 to 1000.degree. C., thereby forming a matrix with a grain size of 1 to 3 µm and one Elimination phase set with a grain size of 0.2 to 1.0 µm and finally superplastically shaped.

Die bei dem erfindungsgemäßen Verfahren eingestellte geringe Korngröße gewährleistet eine niedrige Fließspannung durch Korngrenzengleiten und verringert damit die erforderliche Umformungskraft sowie den Werkzeugverschleiß.The small grain size set in the process according to the invention ensures a low yield stress due to grain boundary sliding and thus reduces the required forming force and tool wear.

Das erfindungsgemäße Verfahren läuft mithin zweistufig ab; die erste Verfahrensstufe dient dazu, das pulvermetallurgisch hergestellte, infolge der hohen Abkühlungsgeschwindigkeit von beispielsweise 10⁴ bis 10⁵ ⁰K/s beim Schmelzzerstäuben an sich schon feinkristalline, vorzugsweise bereits äquiaxiale Mehrphasengefüge der Legierungspulver sowohl hinsichtlich der Matrix als auch hinsichtlich der karbidischen und/oder boridischen Ausscheidungsphase im konsolidierten Zustand weiter zu verfeinern und dabei ein beim sich anschließenden thermomechanischen Prozessieren infolge Warmumformens in der zweiten Verfahrensstufe thermisch stabiles Mikrogefüge mit einer vorzugsweise sowohl für die Matrix als auch für die Ausscheidungsphase feinen Korngröße von 1 bis 3 µm bzw. 0,2 bis 1,0 µm einzustellen.The method according to the invention therefore runs in two stages; The first stage of the process is to use the powder-metallurgically produced, due to the high cooling rate of, for example, 10⁴ to 10⁵ SchmelzK / s during melt atomization, already fine crystalline, preferably already equiaxial, multi-phase structure of the alloy powder both with regard to the matrix and also with regard to the carbidic and / or boridic precipitation phase to further refine the consolidated state and thereby a thermally stable microstructure during the subsequent thermomechanical processing as a result of hot forming in the second process stage, with a grain size of 1 to 3 μm or 0.2 to 1.0, which is preferably fine both for the matrix and for the precipitation phase µm.

Das Konditionieren des Werkstoffgefüges in der ersten Verfahrensstufe kann durch ein thermomechanisches Prozessieren geschehen, das bei den Stahllegierungen im austenitischen Zustand, beispielsweise bei etwa 900oC beginnt und die γ/α -Phasenumwandlung im Bereich von 750 bis 820oC bis zu einer Endwalztemperatur von 650oC durchläuft. Während des Warmverformens, beispielsweise eines Walzens oder Schmiedens kühlt das Verformungsgut kontinuierlich ab und kommt es neben der Phasenumwandlung zum Ausscheiden der Karbide und/oder Boride.The material structure in the first process stage can be conditioned by thermomechanical processing, which is the case with steel alloys in austenitic Condition, for example, begins at about 900 o C and the γ / α phase conversion in the range from 750 to 820 o C to a final rolling temperature of 650 o C goes through. During the thermoforming, for example rolling or forging, the material to be deformed cools down continuously and, in addition to the phase change, the carbides and / or borides are eliminated.

In ähnlicher Weise scheiden sich bei einem Warmverformen von Stelliten etwa im Temperaturbereich von 1000 bis 700oC während des Verformens und des damit verbundenen kontinuierlichen Abkühlens die Karbide und/oder Boride aus. Darüber hinaus kommt es während des thermomechanischen Konditionierens sowohl zu einer Verfeinerung des spätestens dann äquiaxialen Matrixkorns als auch infolge der günstigen Bedingungen für die Keimbildung während der Phasenumwandlung zu einer feinerdispersen Verteilung der Karbid- und Boridteilchen. Beides wirkt sich in Richtung einer höheren Werkstoffestigkeit aus.In a similar manner, the carbides and / or borides are eliminated in the hot forming of stellites in the temperature range from 1000 to 700 ° C. during the shaping and the associated continuous cooling. In addition, during thermomechanical conditioning, there is a refinement of the matrix grain, which is then equiaxial at the latest, as well as a finer dispersion of the carbide and boride particles as a result of the favorable conditions for nucleation during the phase change. Both have an impact in the direction of higher material strength.

Des weiteren kann das Konditionieren des pulvermetallurgisch hergestellten Ausgangsmaterials auch durch isothermes Verformen mit dem Ziel geschehen, das Gefüge umzukristallisieren und ein feinerkörniges Gefüge als Voraussetzung für den superplastischen Zustand einzustellen. Das isotherme Verformen findet bei Temperaturen unterhalb der Umwandlungstemperatur, beispielsweise bei 450oC vorzugsweise bei einem geringen Verformungsgrad, beispielsweise bei einer Querschnittsabnahme von etwa 10% statt und sollte eine zyklische γ/α Phasenumwandlung einschließen, die infolge des unterschiedlichen Volumens der γ -und der α -Phase zu inneren Spannungen und damit zu einer durch innere Eigenspannungen induzierten Verformung des Matrixkorns führt. Dem kann sich zur Verfeinerung der Matrixkorngröße des heißisostatisch gepreßten Rohlings ein kurzes, beispielsweise 20 bis 60 Sekunden dauerndes Primärrekristallisationsglühen anschließen, das zu einer weiteren Kornverfeinerung führt.Furthermore, the conditioning of the starting material produced by powder metallurgy can also be carried out by isothermal shaping with the aim of recrystallizing the structure and setting a fine-grained structure as a prerequisite for the superplastic state. The isothermal deformation takes place at temperatures below the transformation temperature, for example at 450 ° C., preferably with a low degree of deformation, for example with a cross-sectional decrease of about 10%, and should include a cyclic γ / α phase transformation which, owing to the different volumes of the γ and α phase to internal tensions and thus to internal internal tensions induced deformation of the matrix grain. This can be followed by a short primary recrystallization annealing, for example 20 to 60 seconds, to refine the matrix grain size of the hot isostatically pressed blank, which leads to a further grain refinement.

Insgesamt zielt das Konditionieren des Ausgangsmaterials darauf ab, ein für die superplastische Formgebung in der zweiten Verfahrensstufe äquiaxiales Gefüge einzustellen, das sich durch ein das Umformverhalten begünstigendes feines Gefügekorn auszeichnet. Mit abnehmender Korngröße verringert sich nämlich der Verformungswiderstand und läßt sich gleichzeitig die Verformungsgeschwindigkeit erhöhen.Overall, the aim of the conditioning of the starting material is to establish a structure which is equiaxial for superplastic shaping in the second process stage and which is characterized by a fine structure grain which favors the forming behavior. With decreasing grain size, the resistance to deformation is reduced and, at the same time, the rate of deformation can be increased.

In der zweiten Verfahrensstufe wird der umgeformte und auf ein bestimmtes Mehrphasen-Gefüge eingestellte Werkstoff bei einer Temperatur in der Größenordnung von 50 bis 70% der Schmelztemperatur von beispielsweise 650 bis 780oC geformt, die bei niedrigen Fließspannungen hohe Verformungsgrade erlaubt und daher auch das Herstellen komplizierter Fertigteile aus Legierungen ermöglicht, deren Zusammensetzung ohne die spezielle Vorbehandlung der ersten Stufe des erfindungsgemäßen Verfahrens eine Formgebung durch Umformen nicht erlaubt. Die Umformgeschwindigkeit liegt vorzugsweise bei 10⁻³ bis 5.10⁻¹ s⁻¹. Dabei kann der Dehngeschwindigkeitsexponent m, wie er sich aus der Gleichung

s = K . e ̇ m ,

Figure imgb0001


ergibt, in der s die Fließspannung, K eine Materialkonstante und ė die Verformungs- bzw. Kriechgeschwindigkeit für Stahllegierungen von 0,4 bis 0,5 und für Stellite von 0,35 bis 0,4 ist. Daraus ergibt sich, daß die Formgebung sehr geringer Fließspannungen bzw. Umformungskräfte bedarf; da sie zudem bei verhältnismäßig niedrigen Temperaturen stattfindet, zeichnet sich das erfindungsgemäße Verfahren, insbesondere wenn das Konditionieren in der ersten Verfahrensstufe durch isothermes Verformen unterhalb der Umwandlungstemperatur stattfindet, durch geringe Kosten sowohl unter dem Aspekt des apparativen Aufwandes als auch hinsichtlich des Energieverbrauchs aus.In the second stage of the process, the formed material, which is adjusted to a specific multiphase structure, is shaped at a temperature in the order of 50 to 70% of the melting temperature of, for example, 650 to 780 o C, which allows high degrees of deformation at low flow stresses and therefore also manufacture Complicated finished parts made of alloys, the composition of which does not allow shaping by forming without the special pretreatment of the first stage of the method according to the invention. The forming speed is preferably 10⁻³ to 5.10⁻¹ s⁻¹. The expansion speed exponent m, as it results from the equation

s = K. e ̇ m ,
Figure imgb0001


results in s the yield stress, K a material constant and ė the rate of deformation or creep for Steel alloys from 0.4 to 0.5 and for stellites from 0.35 to 0.4. It follows that the shaping requires very low yield stresses or forming forces; since it also takes place at relatively low temperatures, the process according to the invention, particularly if the conditioning in the first process stage takes place by isothermal shaping below the transition temperature, is characterized by low costs both in terms of the outlay on equipment and in terms of energy consumption.

Die Umformtemperatur liegt dabei unterhalb der Temperatur der beginnenden Sekundärkristallisation bzw. Kornvergröberung, da jedes Kornwachstum den Verformungswiderstand erhöht und damit höhere Verformungskräfte erfordert.The forming temperature is below the temperature of the beginning secondary crystallization or grain coarsening, since each grain growth increases the resistance to deformation and therefore requires higher deformation forces.

Das erfindungsgemäße Verfahren eignet sich besonders für die hoch kohlenstoffhaltigen Kaltarbeitsstähle wie
X 178 Cr V 5 2 9
X 155 Cr V W Co 4 5 12 5
X 135 Cr V W Mo 4 4 6 4
X 220 Cr V 17 6
X 245 Cr V 5 10
Diese besitzen Kohlenstoffgehalte von 1,0 bis 2,5% und hohe Legierungsgehalte an Chrom, Vanadium, Wolfram, Molybdän und Kobalt von 4 bis 17%.
The method according to the invention is particularly suitable for high-carbon cold work steels such as
X 178 Cr V 5 2 9
X 155 Cr VW Co 4 5 12 5
X 135 Cr VW Mo 4 4 6 4
X 220 Cr V 17 6
X 245 Cr V 5 10
These have carbon contents from 1.0 to 2.5% and high alloy contents of chromium, vanadium, tungsten, molybdenum and cobalt from 4 to 17%.

Weiterhin eignen sich die folgenden Legierungen:
X 375 Cr Mo Fe 25 10 60
X 220 Cr W Co 30 12 56
X 120 Cr Mo Co 27 4 60
X 100 Cr W Co N B 15 15 52 3.
The following alloys are also suitable:
X 375 Cr Mo Fe 25 10 60
X 220 Cr W Co 30 12 56
X 120 Cr Mo Co 27 4 60
X 100 Cr W Co NB 15 15 52 3.

Die Stellite sind Eisen- sowie Kobaltbasisstellite mit hohen Bor- und Kohlenstoffgehalten von 1 bis 4% sowie Gehalten der Legierungselemente Chrom, Molybdän, Wolfram von 15 bis 30%, die sich bei einer verhältnismäßig niedrigen Temperatur von 650 bis 720oC umformen lassen.The Stellite are iron and cobalt-based stellite with high boron and carbon contents of 1 to 4%, and contents of the alloying elements chromium, molybdenum, tungsten, 15 to 30%, which can be transformed at a relatively low temperature of 650-720 o C.

Der superplastischen Formgebung kann sich ein Grobkornglühen anschließen, um die Kriechfestigkeit bzw. Warmfestigkeit zu erhöhen.The superplastic shape can be followed by coarse grain annealing in order to increase the creep resistance or heat resistance.

Die Erfindung wird nachfolgend anhand eines in der Zeichnung dargestellten Ausführungsbeispiels des näheren erläutert. In der Zeichnung zeigen:

Fig. 1
die Seitenansicht einer Ronde zum Herstellen eines Rotationsmessers, teilweise im Schnitt und
Fig. 2
das aus der Ronde der Fig. 1 durch superplastische Formgebung hergestellte Rotationsmesser teilweise im Schnitt.
The invention is explained below with reference to an embodiment shown in the drawing. The drawing shows:
Fig. 1
the side view of a circular blank for producing a rotary knife, partly in section and
Fig. 2
the rotary knife manufactured from the blank of FIG. 1 by superplastic shaping, partly in section.

Die in Fig. 1 dargestellte Ronde 1 besteht aus dem hochfesten Kaltarbeitsstahl X 245 Cr V 5 10, der pulvermetallurgisch durch isostatisches Heißpressen hergestellt wurde und auf ein Gefüge mit einer Matrixkorngröße von 1 bis 3 µm eingestellt wurde. Sie dient zum Herstellen des in Fig. 2 dargestellten scheibenförmigen Rotationsmessers mit einem Kegelwinkel α von 150 bis 160o, einer Dicke von 1,0 bis 1,5 mm und einem Innendurchmesser von 50 mm sowie einem Außendurchmesser von 100 mm.The round blank 1 shown in FIG. 1 consists of the high-strength cold work steel X 245 Cr V 5 10, which was produced by powder metallurgy by hot isostatic pressing and was set to a structure with a matrix grain size of 1 to 3 μm. It serves to manufacture the disk-shaped rotary knife shown in FIG. 2 with a cone angle α of 150 to 160 ° , a thickness of 1.0 to 1.5 mm and an inner diameter of 50 mm and an outer diameter of 100 mm.

Die Ronde 1 wurde durch Stanzen aus einer pulvermetallurgisch hergestellten und alsdann bei einer Temperatur von 1150 bis 1250oC auf eine Dicke von 2,5 mm ausgewalzten Platine der Abmessung 100 x 200 x 8 mm hergestellt. Um eine ausreichende Materialreserve für die Ausbildung der Schneiden 2 des Rotationsmessers zu schaffen, überstieg die Dicke der Platine die Fertigdicke des Rotationsmessers um 1 mm.The circular blank 1 was produced by punching from a powder metallurgy and then rolled out at a temperature of 1150 to 1250 ° C. to a thickness of 2.5 mm and measuring 100 × 200 × 8 mm. In order to create a sufficient material reserve for the formation of the cutting edges 2 of the rotary knife, the thickness of the board exceeded the finished thickness of the rotary knife by 1 mm.

Die Ronde 1 besaß einen Durchmesser von 95 mm und eine Dicke von 2,5 mm, er wurde nach dem Stanzen auf eine Temperatur von 760oC erwärmt und mit Hilfe eines üblichen, auf 350oC Vorgewärmten Werkzeugs aus Ober- und Untergesenk mit einer Umformgeschwindigkeit von 5.10⁻³ s⁻¹ in einer Preßzeit von 25 s zu dem in Fig 2 dargestellten Rotationsmesser umgeformt, wie sich aus der Gleichung

Figure imgb0002

ergibt, in der Ao die Kreisringfläche der Ronde 1,ΔA die Kegelmantelfläche A, verringert um die Fläche Ao des Schlitzprofils ε und ε̇ = 5 . 10⁻³ s⁻¹ ist.The blank 1 had a diameter of 95 mm and a thickness of 2.5 mm, it was heated after punching to a temperature of 760 o C and with the help of a conventional tool preheated to 350 o C from the upper and lower die with a Forming speed of 5.10⁻³ s⁻¹ in a pressing time of 25 s to the rotary knife shown in Figure 2, as can be seen from the equation
Figure imgb0002

in which A o is the circular ring area of the round blank 1, ΔA is the conical surface area A, reduced by the area A o of the slot profile ε and ε̇ = 5. Is 10⁻³ s⁻¹.

Die geringe Umformtemperatur spart Energie, gewährleistet eine minimale Verzunderung und verhindert ein schädliches Kornwachstum. Außerdem ergibt sich beim superplastischen Umformen eine höhere Dichte, weil Poren und Risse verschweißen, sowie eine höhere Festigkeit und Zähigkeit. Wegen des Wegfalls einer spanenden Bearbeitung kommt es auch nicht zu Ermüdungsrisse auslösendem Bearbeitungsriefen, wodurch sich die Standzeit eines Werkzeugs um 25 bis 30% erhöht.The low forming temperature saves energy, ensures minimal scaling and prevents harmful grain growth. In addition, superplastic forming results in a higher density because pores and cracks weld, as well as higher strength and toughness. Because there is no machining, there are no fatigue cracks in the machining grooves, which increases the tool life by 25 to 30%.

Experimentell ergab sich in guter Übereinstimmung mit dem rechnerisch ermittelten Wert eine Umformzeit von 25 s. Rechnet man dazu eine Zustellzeit für das Werkzeug von 35 s hinzu, so ergibt sich je Rotationsmesser eine Fertigungszeit von 60 s, die weit unter der Bearbeitungszeit beim spanenden Bearbeiten eines Rohlings liegt.Experimentally, in good agreement with the calculated value, a forming time of 25 s was found. If you add a delivery time for the tool of 35 s, this results in a production time of 60 s for each rotary knife, which is far less than the machining time for machining a blank.

Das erfindungsgemäße Verfahren eignet sich zum Herstellen von Schnittglocken und -werkzeugen, Formschneidwerkzeugen, Messern, beispielsweise Scheiben-, Filter- und Tabakmessern mit einer Dicke unter 3 mm, Prägestempeln, Stau- und Druckringen für Extruder, Sinterformpreßwerkzeugen, Fließpreßwerkzeugen und -stempeln, Formwerkzeugen für das Taumelfließpressen und Viellochplatten jeweils aus Kaltarbeitsstählen, zum Herstellen von Profilfräsern, Formdrehstählen und Profilsenkköpfen aus Schnellarbeitsstählen sowie zum Herstellen von Glasblasformwerkzeugen, Profilstangen, Düsen, Laufrädern, Turbinenscheiben und Ventilsitzen aus Stelliten. Es zeichnet sich durch niedrige Umformtemperaturen und einen geringen Kraftbedarf aus. Das feindisperse, äquiaxiale und texturfreie Mikrogefüge gewährleistet gleichbleibende und reproduzierbare mechanische Eigenschaften, insbesondere eine hohe Festigkeit bei ausgezeichneter Duktilität und gutem Ermüdungsverhalten. Die Maßhaltigkeit und Oberflächenbeschaffenheit sind dabei so gut, daß ein Nachbearbeiten nicht erforderlich ist. So liegt die Oberflächenrauhigkeit normalerweise unter 1 µm.The method according to the invention is suitable for producing cut bells and tools, shape cutting tools, knives, for example disc, filter and tobacco knives with a thickness of less than 3 mm, embossing dies, jam and pressure rings for extruders, sintering compression tools, extrusion tools and dies, molding tools for the wobble extrusion and multi-hole plates each made of cold work steels, for the production of profile milling cutters, form turning steels and profile countersunk heads from high speed steels as well as for the production of glass blow molding tools, profile rods, nozzles, impellers, turbine disks and valve seats made of stellites. It is characterized by low forming temperatures and a low power requirement. The finely dispersed, equiaxial and texture-free microstructure guarantees constant and reproducible mechanical properties, in particular high strength with excellent ductility and good fatigue behavior. The dimensional accuracy and surface quality are so good that reworking is not necessary. The surface roughness is usually less than 1 µm.

Claims (16)

  1. A process for producing steel tools in which a powder metallurgically produced starting body is hot consolidated, characterised in that a starting body of a high alloy steel having an equiaxed structure and more than 30% by volume of precipitated carbidic and/or boridic phase is hot worked beneath A₁ with a cyclic alpha/gamma phase transformation or in the austenitic state to bring it to have a matrix with a grain size of 1 to 3 µm and a precipitated phase with a grain size of 0.2 to 1.0 µm and then finish formed superplastically.
  2. A process for producing tools in which a powder metallurgically produced starting body is hot consolidated, characterised in that a stellitic starting body having an equiaxed structure and more than 30% by volume of precipitated carbidic and/or boridic phase is hot worked at 700 to 1000°C to give a matrix with a grain size of 1 to 3 µm and a precipitated phase with a grain size of 0.2 to 3 µm, and then finish formed superplastically.
  3. A process according to claim 1 or claim 2, characterised in that a starting material with an equiaxed structure is superplastically formed to final size.
  4. A process according to one or more of claims 1 to 3, characterised in that powder metallurgical tool steels and stellites are superplastically formed at temperatures of about 0.5 to 0.7 Tm and then continuously cooled.
  5. A process according to claim 4, characterised by a working temperature of from 900° to 650 °C.
  6. A process according to one of claims 1 to 3, characterised in that a stellitic starting material is hot worked in the course of continuous cooling from 1000° to 760°C.
  7. A process according to one of claims 4 to 6, characterised in that the degree of deformation exceeds 30% and the elongation amounts to some hundreds percent.
  8. A process according to one of claims 1 to 3, characterised in that powder metallurgically produced tool steels are isothermally and superplastically formed below their transformation temperature.
  9. A process according to claim 8, characterised in that the degree of deformation is up to 800%.
  10. A process according to claim 8 or claim 9, characterised by grain boundary slip and dynamic recrystallisation at 600 to 700 C.
  11. A process according to one of claims 1 to 10, characterised by superplastic shaping at a temperature below the temperature of the secondary recrystallisation and grain growth.
  12. A process according to one of claims 8 to 11, characterised by superplastic shaping of alloy steels at 650° to 780°C.
  13. A process according to claim 11 or claim 12, characterized in that the rate of deformation ε̇ = 10⁻³ to 10⁻¹s⁻¹.
  14. A process according to one or more of claims 11 to 13, characterised in that the elongation rate exponent m = 0.4 to 0.5.
  15. A process according to one or more of claims 11 to 13, characterised in that for stellites the elongation rate exponent m = from 0.35 to 0.4.
  16. A process according to one or more of claims 11 to 15, characterised in that the shaped article is subjected to grain coarsening annealing.
EP86117455A 1985-12-18 1986-12-16 Method for manufacturing tools Expired - Lifetime EP0227001B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT86117455T ATE90899T1 (en) 1985-12-18 1986-12-16 PROCESS FOR MAKING TOOLS.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19853544759 DE3544759A1 (en) 1985-12-18 1985-12-18 METHOD FOR PRODUCING TOOLS
DE3544759 1985-12-18

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EP0227001A2 EP0227001A2 (en) 1987-07-01
EP0227001A3 EP0227001A3 (en) 1988-05-04
EP0227001B1 true EP0227001B1 (en) 1993-06-23

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JP (1) JPS62156203A (en)
AT (1) ATE90899T1 (en)
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ES (1) ES2041242T3 (en)

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US4969099A (en) * 1986-03-11 1990-11-06 Toyota Jidosha Kabushiki Kaisha Double-detecting, trouble-judging and failsafe devices in system for integrally controlling automatic transmission and engine
US4945481A (en) * 1986-05-08 1990-07-31 Toyota Jidosha Kabushiki Kaisha System for integrally controlling automatic transmission and engine
US4838124A (en) * 1986-06-30 1989-06-13 Toyota Jidosha Kabushiki Kaisha System for integrally controlling automatic transmission and engine
JPH0712809B2 (en) * 1986-07-07 1995-02-15 トヨタ自動車株式会社 Integrated control device for automatic transmission and engine
WO2005094274A2 (en) * 2004-03-24 2005-10-13 Smith International, Inc. Solid state processing of hand-held knife blades to improve blade performance

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FR2127082A5 (en) * 1971-02-22 1972-10-13 Charbonnages De France
JPS5510642B2 (en) * 1973-10-31 1980-03-18
US4073648A (en) * 1974-06-10 1978-02-14 The International Nickel Company, Inc. Thermoplastic prealloyed powder
US3976482A (en) * 1975-01-31 1976-08-24 The International Nickel Company, Inc. Method of making prealloyed thermoplastic powder and consolidated article
US3951697A (en) * 1975-02-24 1976-04-20 The Board Of Trustees Of Leland Stanford Junior University Superplastic ultra high carbon steel
JPS5485106A (en) * 1977-12-20 1979-07-06 Seiko Epson Corp Magnet made from inter-rare-earth-metallic compound
JPS5887204A (en) * 1981-11-17 1983-05-25 Kobe Steel Ltd Constant temperature forging method for superalloy using quickly soldified powder
JPS5893802A (en) * 1981-11-30 1983-06-03 Sumitomo Electric Ind Ltd Manufacture of wire rod of difficultly workable alloy
US4533390A (en) * 1983-09-30 1985-08-06 Board Of Trustees Of The Leland Stanford Junior University Ultra high carbon steel alloy and processing thereof
DE3346089A1 (en) * 1983-12-21 1985-07-18 Dr. Weusthoff GmbH, 4000 Düsseldorf METHOD FOR MANUFACTURING HIGH-STRENGTH, DUCTILE BODY FROM CARBON-BASED IRON-BASED ALLOYS
US4582536A (en) * 1984-12-07 1986-04-15 Allied Corporation Production of increased ductility in articles consolidated from rapidly solidified alloy
JPS62134130A (en) * 1985-12-05 1987-06-17 Agency Of Ind Science & Technol Super-plastic worm die pack forging method for high strength/hard-to-work material

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US5028386A (en) 1991-07-02
EP0227001A3 (en) 1988-05-04
ES2041242T3 (en) 1993-11-16
EP0227001A2 (en) 1987-07-01
DE3544759A1 (en) 1987-06-19
JPS62156203A (en) 1987-07-11
ATE90899T1 (en) 1993-07-15

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