EP3695920B1 - Lingotière robuste pour la fabrication de composants de verres métalliques en masse - Google Patents

Lingotière robuste pour la fabrication de composants de verres métalliques en masse Download PDF

Info

Publication number
EP3695920B1
EP3695920B1 EP19156906.0A EP19156906A EP3695920B1 EP 3695920 B1 EP3695920 B1 EP 3695920B1 EP 19156906 A EP19156906 A EP 19156906A EP 3695920 B1 EP3695920 B1 EP 3695920B1
Authority
EP
European Patent Office
Prior art keywords
ingot
melt
casting
glass
alloy
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.)
Active
Application number
EP19156906.0A
Other languages
German (de)
English (en)
Other versions
EP3695920A1 (fr
Inventor
Tim GLÄSER
Hamed SHAKUR SHAHABI
Eugen Milke
Hans-Jürgen Wachter
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.)
Heraeus Deutschland GmbH and Co KG
Original Assignee
Heraeus Deutschland GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Heraeus Deutschland GmbH and Co KG filed Critical Heraeus Deutschland GmbH and Co KG
Priority to EP19156906.0A priority Critical patent/EP3695920B1/fr
Priority to PCT/EP2020/052232 priority patent/WO2020164916A1/fr
Priority to CN202080011844.XA priority patent/CN113382815B/zh
Priority to US17/427,597 priority patent/US20220118511A1/en
Priority to TW109103520A priority patent/TWI791947B/zh
Publication of EP3695920A1 publication Critical patent/EP3695920A1/fr
Application granted granted Critical
Publication of EP3695920B1 publication Critical patent/EP3695920B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D25/00Special casting characterised by the nature of the product
    • B22D25/06Special casting characterised by the nature of the product by its physical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C3/00Selection of compositions for coating the surfaces of moulds, cores, or patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D7/00Casting ingots, e.g. from ferrous metals
    • B22D7/005Casting ingots, e.g. from ferrous metals from non-ferrous metals
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/023Alloys based on nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/11Making amorphous alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C16/00Alloys based on zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/02Amorphous alloys with iron as the major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/04Amorphous alloys with nickel or cobalt as the major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/10Amorphous alloys with molybdenum, tungsten, niobium, tantalum, titanium, or zirconium or Hf as the major constituent

Definitions

  • the invention relates to a method for producing mechanically and thermally stable ingots (also called preforms) from alloys that can form a metallic solid glass. Furthermore, the invention relates to an ingot of a solid glass-forming alloy that is produced using the method according to the invention and the use of this ingot in a casting method.
  • BMG bulk metallic glasses
  • a metallic solid glass is to be understood as meaning a material with a critical casting thickness of at least one millimeter.
  • the existing systems include, among other things, precious metal-based alloys such as gold, platinum and palladium-based metallic bulk glasses, early transition metal-based alloys such as titanium or zirconium-based metallic bulk glasses, late transition metal-based systems, e.g. based on Copper, nickel or iron, but also systems based on rare earth metals, e.g. neodymium or terbium.
  • Components made of metallic solid glass can be produced using casting processes, since the necessary cooling rates for amorphous solidification can be achieved with these processes.
  • amorphous components In order to obtain amorphous components from a metallic bulk glass, it is usually necessary to quickly transfer the melt of a bulk glass-forming alloy into a mold. This filling of the mold with the melt preferably takes place by injection (injection molding) or sucking in (suction molding). In this way, the high cooling rates can be achieved and three-dimensional components made of metallic solid glass can be manufactured. Small manufacturing tolerances can be achieved by using casting processes such as injection molding.
  • Ingots of the alloy to be processed are necessary for casting processes, which serve as a supply of material to be processed and can be melted homogeneously. To do this, the ingots must have a sufficient volume so that enough material is available for the entire cast component and the additional spaces in the mold (the sprue ) can also be filled. Therefore, ingots that are as large as possible are desirable.
  • a homogeneous bulk glass-forming alloy is first produced. To do this, the individual components are mixed together and heated above the melting point, resulting in a homogeneous alloy. The individual components can be melted, for example, in an arc or by means of inductive heating. the The homogeneous alloy is then poured into molds and cooled to form an ingot. Generally, these ingots are in the form of cylindrical rods. In order for the ingots to contain enough material to completely fill the mold for a casting process for a three-dimensional component, the ingots must be sufficiently dimensioned. Typical diameters of cylindrical ingots made of bulk glass-forming alloys are in the range of about 20 mm. The length of an ingot is preferably at least 3 cm.
  • An object of the present invention was to provide an ingot made from a solid glass-forming alloy with a high critical casting thickness, which does not shatter during the production process and can be heated up more quickly during further thermal processing, such as injection molding.
  • the object of the invention was to provide a method for producing an ingot from a solid glass-forming alloy with a high critical casting thickness that does not shatter during the production process.
  • Another object of the invention was to provide ingots made of bulk glass-forming alloys that can be heated faster than conventional ingots.
  • the composition of the solid glass-forming alloy is not further restricted.
  • a solid glass-forming alloy is preferably to be understood as meaning an alloy with a critical casting thickness of at least one millimeter. This means that such an alloy can solidify amorphously up to a thickness of one millimeter at a suitable cooling rate.
  • alloys that can form metallic bulk glasses are selected from the group consisting of Ni-Nb-Sn, Co-Fe-Ta-B, Ca-Mg-Ag-Cu, C-oFe-B-Si -Nb, Fe-Ga-(Cr,Mo)(P,C,B), Ti-Ni-Cu-Sn, Fe-Co-Ln-B, Co-(Al,Ga)-(P,B,Si ), Fe-B-Si-Nb and Ni-(Nb,Ta)-Zr-Ti.
  • the metallic bulk glass can be a Zr-Cu-Al-Nb alloy.
  • this Zr-Cu-Al-Nb alloy preferably also has 23.5-24.5% by weight copper, 3.5-4.0% by weight aluminum and 1.5-2.0% by weight On niobium, the proportions by weight adding up to 100% by weight.
  • the latter alloy is commercially available under the name AMZ4® from Heraeus Kunststoff GmbH.
  • the alloy forming solid glass can contain or consist of the elements zirconium, titanium, copper, nickel and aluminum.
  • Particularly stable ingots can be produced from alloys of this composition that form solid glass.
  • a particularly well suited alloy for the production of stable inogts has the composition Zr 52.5 Ti 5 Cu 17.9 Ni 14.6 Al 10 , the indices indicating mol % of the respective elements in the alloy.
  • the alloy that forms solid glass preferably has a critical casting thickness of at least 5 mm, in particular at least 7 mm and entirely particularly preferably of at least 10 mm.
  • the maximum casting thickness is a measure of how easy or difficult it is for a metallic alloy to bring it into the glass state.
  • the alloy to be measured is processed in an electric arc to form a homogeneous melt and then poured into a water-cooled copper mold (also called permanent mold).
  • the mass of the copper mold is preferably at least a factor of 7 greater than the mass of the melt of the alloy to be determined.
  • the temperature of the homogeneous melt before casting is preferably at least 200° C., in particular 300° C. and very particularly preferably at least 400° C. above the melting temperature.
  • the temperature of the copper mold is 20°C.
  • cylindrical molded parts are cast with increasing diameters at a distance of 1 mm (e.g. 2mm, 3mm, 4mm, 5mm, 6mm, etc.).
  • the cylindrical molded parts produced are examined for their crystalline content using differential scanning calorimetry (DSC).
  • DSC differential scanning calorimetry
  • the cylinder diameter that is one millimeter smaller than the cylinder diameter at which the formation of a crystalline phase is first measured by DSC is given as the critical casting thickness.
  • DSC method 2) as described herein was used to determine the presence of a crystalline phase.
  • a homogeneous melt of a bulk glass-forming alloy is provided.
  • the homogeneous melt is preferably prepared by melting the individual elements of the alloy together.
  • the individual elements are preferably melted in an arc or by means of inductive heating.
  • the temperature of the homogeneous melt is preferably at least 200° C., in particular at least 300° C., and very particularly preferably at least 400° C., above the melting temperature of the respective solid glass-forming alloy.
  • the temperature of the melt, measured in degrees Celsius is at least 20%, in particular at least 50%, above the melting temperature of the alloy, since particularly stable ingots can be produced as a result.
  • the homogeneous melt is poured into a casting mold.
  • the shape of the mold is not further restricted.
  • the mold is preferably cylindrical.
  • the volume of the casting mold to be filled preferably has dimensions which are greater in all three spatial directions than the critical casting thickness of the alloy forming solid glass.
  • the material of the mold can preferably be selected from steel, titanium, copper, ceramic or graphite.
  • the mold preferably has a device with which the mold can be actively heated and/or cooled. In one embodiment of the invention, the mold can be actively heated, eg by electrical heating.
  • the ratio between the weight of the mold and the weight of the melt is preferably in the range of 7:1 or more, more preferably in the range of 10:1 or more.
  • the casting mold can be coated in the area that comes into contact with the melt.
  • the material of this coating of the mold is preferably selected from the group consisting of boron nitride, aluminum oxide (eg Al 2 O 3 ) and yttrium oxide (eg Y 2 O 3 ).
  • the coating preferably has or consists of a powder.
  • the thickness of the coating, in particular the powder coating can be in the range of 10-50 ⁇ m in one embodiment.
  • a layer of powder can have an advantageous effect on the mechanical properties of the ingot to be produced.
  • the coating can serve, among other things, to make it easier to remove the ingot from the mold.
  • the casting mold does not cool below the glass formation temperature of the solid glass-forming alloy at the contact surface with the melt for at least 5 seconds, in particular for at least 10 seconds and very particularly preferably for at least 30 seconds.
  • a melt is also referred to after the liquid melt has been transferred to the casting mold, even if the solidification process has already started and the solid glass-forming alloy is partially or completely solid, as long as the glass transition temperature has not yet been fallen below.
  • the casting mold does not cool below the glass formation temperature of the solid glass-forming alloy at any point on the contact surface with the melt for the specified period.
  • the determination of the glass formation temperature of the alloy is described under "Methods".
  • the temperature of the mold at the contact surface with the melt for the aforementioned period is at least 10° C., in particular at least 20° C. and particularly preferably at least 40° C. or at least 80° C. above the glass formation temperature of the solid glass-forming Alloy.
  • a temperature measuring probe can be embedded in the mold in such a way that it reaches the contact surface of the mold with the melt and measures there.
  • the temperature is preferably measured at half the length of the longest dimension of the ingot.
  • the temperature of the mold before filling with the melt is preferably adjusted so that the temperature of the mold after casting at the contact surface with the melt for at least 5 seconds, in particular for at least 10 seconds and most preferably for at least 30 seconds after contact with the mold does not fall below the glass formation temperature of the alloy.
  • the mold is preferably heated prior to contact with the melt.
  • the preferably set temperature of the mold directly before pouring the melt is at least 250°C, in particular at least 400°C and particularly preferably at least 500°C.
  • the casting mold can be heated in an oven, for example.
  • the mold can be actively heated, e.g. by electrical heating.
  • no additional pressure substantially above standard atmospheric pressure is applied to the melt after the melt has been poured.
  • “significantly above standard atmospheric pressure” can be understood to mean an overpressure of 1 bar or more.
  • an ingot can be produced from a bulk glass-forming alloy which does not shatter during the production process. Furthermore, the method can produce an ingot that does not shatter when heated to the melting temperature of the alloy within 50 seconds or less. In particular, an ingot which does not shatter when dropped three times from a height of 30 cm onto a flat, horizontal steel surface can be produced. In particular, the method can be used to produce an ingot that does not have an amorphous layer on the surface. The absence of an amorphous layer can be determined with a light microscope.
  • the invention relates to an ingot of a solid glass-forming alloy, the alloy having a critical casting thickness of at least 5 mm, and the ingot having an extent in all three spatial directions which is greater than the critical casting thickness, characterized in that that the ingot has a crystalline proportion of at least 90% by weight, in particular at least 95% by weight and particularly preferably at least 98% by weight, measured by DSC.
  • the critical casting thickness of the alloy is preferably at least 7 mm and in particular at least 10 mm.
  • the ingot according to the invention can be produced using the method described herein will.
  • the ingot according to the invention has no amorphous layer on the surface.
  • the term "no amorphous layer" can be understood as a layer which is no thicker than 200 ⁇ m, in particular no thicker than 100 ⁇ m and very particularly preferably no thicker than 50 ⁇ m.
  • the absence of an amorphous layer can preferably lead to the reduction of internal stresses in the ingot.
  • the absence of an amorphous layer on the surface of the ingot can be determined by optical microscopy (reflected light microscope).
  • a cross-section of the ingot is created using a diamond saw.
  • the cross-section is also called a metallurgical micrograph or cross-section.
  • the absence of amorphous portions can be determined by the absence of a phase transition visible to the naked eye under the light microscope. Phase transitions can be identified in the light microscope as transitions of different colors or different contrasts.
  • illustration 1 shows a micrograph of a cross section through an ingot that has amorphous areas. These amorphous areas can be seen as a bright area towards the edge (arrow 1). The inner area of the examined ingot shows no bright areas (arrow 2).
  • Figure 2 a micrograph of a cross-section through an ingot that does not have any amorphous areas. This can be recognized by the uniform material appearance without light spots.
  • Figure 3 shows a metallurgical micrograph of the sample Figure 2 at higher magnification. The polycrystalline structures and their grain boundaries can be clearly seen there. Furthermore, it can be seen that the crystalline structure of the ingot according to the invention extends to the edge, which confirms the absence of an amorphous phase (eg in the circled area). If an amorphous phase were to occur, it would preferably form at the edge first, as this is where the cooling rates can potentially be highest.
  • an amorphous phase eg in the circled area
  • the total volume of the amorphous layer on the ingot can be 5% or less, in particular 3% or less.
  • the crystallinity of the ingot can be measured using Differential Scanning Calorimetry (DSC).
  • the ingot is preferably solid and has no cavities, such as air inclusions.
  • the shape of the ingot is not limited.
  • the ingot may have a cylindrical shape.
  • the cylinder diameter preferably has a value of at least 5 mm, in particular at least 15 mm and very particularly preferably at least 25 mm, in each case with the condition that the diameter is greater than the critical casting thickness of the solid glass-forming alloy.
  • the length of the cylinder is preferably at least 3 cm.
  • the invention relates to a method for producing three-dimensional components from metallic solid glasses by means of casting methods, in particular injection molding, using the ingot according to the invention of a solid glass-forming alloy.
  • the ingot according to the invention is melted to form a homogeneous melt (30).
  • the complete melting of the ingot (20) preferably takes no longer than 60 seconds, in particular no longer than 40 seconds and very particularly preferably no longer than 20 seconds, it being possible for the ingot to be heated without cracking.
  • the heating-up time for already known ingots of the same dimensions is typically in the range of 80 seconds.
  • the homogeneous melt (30) is poured, in particular injected, into the mold for a three-dimensional component (40).
  • the casting mold for producing the three-dimensional component by means of the casting process is preferably dimensioned in such a way that it does not exceed the critical casting thickness of the alloy used at any point, since completely amorphous, three-dimensional components can be produced in this way.
  • the ingot can be used to produce three-dimensional components that can be produced with a high throughput in an injection molding machine.
  • the XRD measurements are carried out in accordance with DIN EN 13925-1:2003-07 and DIN EN 13925-2:2003-07.
  • a cross section of the material to be examined is prepared with a diamond saw.
  • the flat surface of the cross section is in the range of approx. 1 cm 2 .
  • the general measurement details used are summarized as follows: Diffraction: Bragg-Brentano; Detector: Scintillation Counter; Radiation: Cu K ⁇ 1.5406 ⁇ ; Source: 40kV, 25mA; Measurement method: reflection.
  • the empty sample holder is measured first to determine the background signal. This background measurement is subtracted from all subsequent measurements of the samples to be examined.
  • Discrete diffraction signals in the diffractogram can be evaluated according to the Debye-Scherrer method using the Bragg equation. When visible from discrete, crystalline peaks above the statistical noise, a crystalline proportion of at least 5% by weight is assumed. If no sharp diffraction signals can be determined in the diffractogram, the crystalline proportion is below 5%.
  • the DSC measurements within the scope of the invention are carried out in accordance with DIN EN ISO 11357-1:2017-02 and DIN EN ISO 11357-3:2018-07.
  • the sample to be measured in the form of a thin disc or foil (approx. 80 - 100 mg) is placed in the measuring device (NETZSCH DSC 404F1, NETZSCH GmbH, Germany).
  • the heating rate is 20.0 K/min.
  • Al 2 O 3 is used as the crucible material.
  • the heat flow is measured against an empty reference crucible, so that only the thermal behavior of the sample is measured.
  • Samples expected to be predominantly crystalline with little amorphous phase are measured according to the measurement method given above.
  • the complete crystallinity of the sample after undergoing the measurement procedure can be additionally confirmed by XRD, by the absence of broad, unspecific signals in the diffraction pattern that would indicate an amorphous phase.
  • the amorphous content of samples with more than 5% by weight can be determined by comparing the crystallization enthalpy of the unknown sample with the value for the completely amorphous sample from DSC method 2) (see below).
  • a sample of each of the cast cylinders is measured using DSC. As long as the diameter of the cylinder is below the critical casting thickness, the sample is completely amorphous before the start of the measurement and crystallizes during the DSC measurement in step a) of the measurement method.
  • the crystallization enthalpy of the alloy is determined from the measurement of the completely amorphous material. The crystallization enthalpy is determined for all samples with increasing cylinder diameter. The crystallization enthalpy determined for samples whose cylinder diameter is below the critical casting thickness is constant within the measurement inaccuracy.
  • the critical casting thickness is determined as the cylinder diameter up to which the crystallization enthalpy is constant with increasing diameter.
  • step a) the crystallization of the amorphous sample takes place.
  • step c) the thermal behavior of the already fully crystallized sample is recorded.
  • the measurement from step c) is subtracted from the measurement from step a).
  • the resulting curve includes an endothermic transition at lower temperature and an exothermic peak at higher temperature.
  • the signal at higher temperature corresponds to the crystallization process.
  • the endothermic signal corresponds to the glass transition.
  • a line tangent to the baseline is determined (by linear fitting) in front of the glass transition region.
  • a second tangent is determined at the inflection point (corresponding to the peak time value of the first derivative) of the glass transition region.
  • the temperature value at the intersection of the two tangents indicates the glass transition temperature (T f according to AST; 1356-03).
  • the individual components were melted under protective gas by means of inductive melting into a homogeneous alloy with the composition Zr 52.5 Ti 5 Cu 17.9 Ni 14.6 Al 10 .
  • This alloy has a glass transition temperature of 403 °C.
  • 80 g of the homogeneous alloy were brought to a temperature above the melting point of the alloy (805° C.) by means of inductive heating in a crucible.
  • Table 1 shows the temperatures of the respective melt for the respective test.
  • the mold was preheated in an oven to a temperature defined in Table 1.
  • the respective homogeneous melt according to Table 1 was then poured into a casting mold.
  • the mold had a cylindrical shape with an inner diameter of 19 mm. The temperature of the melt was continuously measured after filling the cylindrical mold.
  • the measured values for the temperature of the melt after 10 seconds in the mold can be read in Table 1.
  • Table 1 Table 1 ⁇ /b> example 1 2 3 4 5 T melt [°C] 1050 1100 1200 1250 1350 T mold [°C] 50 50 250 400 600 mold copper stolen stolen stolen stolen weight ratio 1:17 1:15 1:9 1:15 1:15 coating d.
  • Examples 1 and 2 in Table 1 are comparative examples, Examples 3-5 are examples according to the invention.
  • the quality of the cast ingots was assessed according to the following criteria: Poor-quality cast parts already shatter while cooling in the mold. Good quality cast ingots will remain intact if heated to melting temperature within 50 seconds or less at a power of 5 kW. Very good quality ingots also withstand a drop test from a height of 30 cm onto a flat steel plate three times in a row without shattering. It is clear from Examples 1-5 that ingots in which the temperature of the melt was above the glass transition temperature after 10 seconds were significantly more robust than ingots in which the temperature of the melt was below.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physical Vapour Deposition (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Continuous Casting (AREA)

Claims (12)

  1. Procédé de fabrication d'un lingot d'un alliage formant un verre en masse, présentant les étapes de :
    a. fourniture d'une masse fondue homogène d'un alliage formant un verre en masse,
    b. coulage de la masse fondue homogène dans un moule de coulage, le moule de coulage ne se refroidissant pas en dessous de la température de vitrification de l'alliage pendant au moins 5 secondes au niveau de la surface de contact avec la masse fondue et
    c. refroidissement de la masse fondue en dessous de la température de transition vitreuse de l'alliage formant un verre en masse avec obtention du lingot, après le coulage de la masse fondue, aucune pression supplémentaire qui serait essentiellement supérieure à la pression atmosphérique standard n'étant appliquée à la masse fondue.
  2. Procédé selon la revendication 1, le moule de coulage ne se refroidissant pas en dessous de la température de vitrification de l'alliage pendant au moins 10 secondes au niveau de la surface de contact avec la masse fondue.
  3. Procédé selon l'une quelconque des revendications 1 ou 2, l'alliage formant un verre en masse présentant une épaisseur de coulée critique de 5 mm ou supérieure,
    l'épaisseur de coulée critique étant déterminée au moyen d'un DSC, comme décrit dans le texte d'inscription, l'alliage à mesurer étant transformé en masse fondue homogène dans l'arc électrique, puis coulé dans un moule de coulage en cuivre cylindrique refroidi à l'eau, la masse du moule de coulage en cuivre étant supérieure d'au moins un facteur 7 à la masse de la masse fondue versée de l'alliage à déterminer, la température de la masse fondue homogène étant avant le coulage d'au moins 200 °C supérieure à la température de fusion et la température du moule de coulage en cuivre étant de 20 °C.
  4. Procédé selon l'une quelconque des revendications 1 à 3, la dimension du lingot dans les trois directions spatiales étant supérieure à l'épaisseur de coulée critique, telle qu'elle est déterminée selon la revendication 3.
  5. Procédé selon l'une quelconque des revendications 1 à 4, le lingot présentant une part cristalline d'au moins 90 %, sur la base du poids, mesurée au moyen d'un DSC.
  6. Procédé selon l'une quelconque des revendications 1 à 5, le lingot présentant une part cristalline d'au moins 95 %, sur la base du poids, mesurée au moyen d'un DSC.
  7. Procédé selon l'une quelconque des revendications 1 à 6, le moule de coulage étant revêtu d'un matériau choisi dans le groupe composé de nitrure de bore, de Y2O3 et d'oxyde d'aluminium.
  8. Procédé selon l'une quelconque des revendications 1 à 7, le rapport entre le poids de la masse fondue et le poids du moule de coulage étant 1:7 ou inférieur.
  9. Procédé selon l'une quelconque des revendications 1 à 8, la température de la masse fondue dans l'étape a) étant d'au moins 20 % supérieure à la température de fusion, mesurée en degrés Celsius.
  10. Lingot d'un alliage formant un verre en masse, présentant une épaisseur de coulée critique d'au moins 5 mm, le lingot présentant dans au moins trois directions spatiales une étendue qui est supérieure à l'épaisseur de coulée critique, caractérisé en ce que le lingot présente une part cristalline d'au moins 90 % en poids, mesurée au moyen d'un DSC, l'épaisseur de coulée critique étant déterminée selon la revendication 3 et le lingot ne présentant aucune couche amorphe sur la surface.
  11. Procédé de fabrication d'un composant tridimensionnel en verre métallique en masse au moyen d'un procédé de coulage, caractérisé en ce qu'un lingot (20) selon la revendication 10 est fondu pour le procédé de coulage.
  12. Procédé selon la revendication 11, la fusion du lingot ne durant pas plus longtemps que 60 secondes, en particulier pas plus longtemps que 40 secondes.
EP19156906.0A 2019-02-13 2019-02-13 Lingotière robuste pour la fabrication de composants de verres métalliques en masse Active EP3695920B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
EP19156906.0A EP3695920B1 (fr) 2019-02-13 2019-02-13 Lingotière robuste pour la fabrication de composants de verres métalliques en masse
PCT/EP2020/052232 WO2020164916A1 (fr) 2019-02-13 2020-01-30 Lingot robuste pour la fabrication de pièces constituées de verres massifs métalliques
CN202080011844.XA CN113382815B (zh) 2019-02-13 2020-01-30 用于生产由块体金属玻璃制成的组件的稳定铸锭
US17/427,597 US20220118511A1 (en) 2019-02-13 2020-01-30 Robust ingot for the production of components made of metallic solid glasses
TW109103520A TWI791947B (zh) 2019-02-13 2020-02-05 用於製造由塊狀金屬玻璃製成的組件的強化錠

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP19156906.0A EP3695920B1 (fr) 2019-02-13 2019-02-13 Lingotière robuste pour la fabrication de composants de verres métalliques en masse

Publications (2)

Publication Number Publication Date
EP3695920A1 EP3695920A1 (fr) 2020-08-19
EP3695920B1 true EP3695920B1 (fr) 2022-04-06

Family

ID=65433574

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19156906.0A Active EP3695920B1 (fr) 2019-02-13 2019-02-13 Lingotière robuste pour la fabrication de composants de verres métalliques en masse

Country Status (5)

Country Link
US (1) US20220118511A1 (fr)
EP (1) EP3695920B1 (fr)
CN (1) CN113382815B (fr)
TW (1) TWI791947B (fr)
WO (1) WO2020164916A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102569110B1 (ko) * 2020-09-28 2023-08-23 서울대학교산학협력단 특성 복귀능을 가지는 기어

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5279349A (en) 1989-12-29 1994-01-18 Honda Giken Kogyo Kabushiki Kaisha Process for casting amorphous alloy member
JP2001300694A (ja) * 2000-04-24 2001-10-30 Hitachi Metals Ltd Fe−Ni系合金薄板製造用インゴットの製造方法
US7520944B2 (en) * 2003-02-11 2009-04-21 Johnson William L Method of making in-situ composites comprising amorphous alloys
CN1438083A (zh) * 2003-03-07 2003-08-27 江苏大学 利用快速冷却技术制备块体金属玻璃的方法
DE10326769B3 (de) * 2003-06-13 2004-11-11 Esk Ceramics Gmbh & Co. Kg Dauerhafte BN-Formtrennschichten für das Druckgießen von Nichteisenmetallen
CN100398687C (zh) * 2005-08-31 2008-07-02 中国科学院物理研究所 一种钐基非晶合金及其制备方法
CN101215679A (zh) * 2008-01-08 2008-07-09 厦门大学 一种无磁性铁基块体非晶合金及其制备方法
EP2113759A1 (fr) * 2008-04-29 2009-11-04 The Swatch Group Research and Development Ltd. Capteur de pression ayant une membrane comprenant un matériau amorphe
US8887532B2 (en) * 2010-08-24 2014-11-18 Corning Incorporated Glass-forming tools and methods
US8701742B2 (en) * 2012-09-27 2014-04-22 Apple Inc. Counter-gravity casting of hollow shapes
US9802247B1 (en) * 2013-02-15 2017-10-31 Materion Corporation Systems and methods for counter gravity casting for bulk amorphous alloys
US9790580B1 (en) * 2013-11-18 2017-10-17 Materion Corporation Methods for making bulk metallic glasses containing metalloids
CN104213054B (zh) * 2014-09-03 2017-02-15 中国科学院金属研究所 液相分离双相块体金属玻璃材料及其制备方法
US20160067766A1 (en) * 2014-09-08 2016-03-10 Apple Inc. 3d printed investment molds for casting of amorphous alloys and method of using same
JP6334626B2 (ja) * 2016-09-01 2018-05-30 アップル インコーポレイテッド アモルファス合金インゴットの金型不要の連続的製造

Also Published As

Publication number Publication date
US20220118511A1 (en) 2022-04-21
TWI791947B (zh) 2023-02-11
WO2020164916A1 (fr) 2020-08-20
CN113382815B (zh) 2023-05-12
CN113382815A (zh) 2021-09-10
EP3695920A1 (fr) 2020-08-19
TW202035718A (zh) 2020-10-01

Similar Documents

Publication Publication Date Title
DE3587572T2 (de) Verfahren zur Erhöhung der Duktilität von verstärkten Gegenständen, gefertigt aus einer rasch erstarrten Legierung.
DE69028009T2 (de) Hochfeste Legierungen auf Magnesium-Basis
DE68916687T2 (de) Hochfeste, hitzebeständige Aluminiumlegierungen.
DE69425251T2 (de) Herstellung von berylliumenthaltenden gläsern
DE68907837T2 (de) Hochfeste Legierungen auf Magnesiumbasis.
DE69222455T2 (de) Amorphe Legierung auf Magnesiumbasis und Verfahren zur Herstellung dieser Legierung
DE69422487T2 (de) Gesinterte karbidlegierungen für schneidwerkzeuge und beschichtete gesinterte karbidlegierung
DE69508319T2 (de) Hochfeste und hochduktile Aluminium-Legierung und Verfahren zu deren Herstellung
DE69501509T2 (de) Verschliessfeste Gusslegierung aus Aluminium und Verfahren zur Herstellung
DE19706768A1 (de) Quinäre Metallglaslegierungen
DE2462117A1 (de) Verbessertes knetaluminiumlegierungsprodukt
DE3043503A1 (de) Kristalline metallegierung
WO2015173211A1 (fr) Procédé de production d'un élément à partir d'un alliage métallique comprenant une phase amorphe
EP1978120A1 (fr) Alliage de fonte, d'aluminium et de silice et son procédé de fabrication
DE69322460T2 (de) Hochfeste, wärmeresistente Legierung auf Aluminiumbasis
EP3444370B1 (fr) Alliage à base de cuivre destiné à la fabrication de verres métalliques solidifiés
WO2008125091A2 (fr) Feuille métallique
WO2016008674A1 (fr) Procédé de production d'un élément à partir d'un alliage métallique présentant une phase amorphe
WO2019179680A1 (fr) Fabrication d'un matériau composite en verre massif métallique par préparation additive à base de poudre
DE69115394T2 (de) Hochfeste Legierungen auf Aluminiumbasis
DE4003568C2 (fr)
DE2556102C3 (de) Verfahren zum Herstellen hxxochverschleißfester Sinterhartmetalle auf Titannitridbasis
DE112023000030T5 (de) Mit Titanpartikeln verstärktes Magnesiummatrix-Verbundmaterial und dessen Herstellungsverfahren
DE69320633T2 (de) Gesinterte karbonitridlegierung auf titanbasis mit extrem feiner korngrösse mit hoher zähigkeit und/oder verschleissfestigkeit
DE69030622T2 (de) Blech aus einer intermetallischen titan-aluminiumverbimdung und verfahren zu ihrer herstellung

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190213

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RAP3 Party data changed (applicant data changed or rights of an application transferred)

Owner name: HERAEUS DEUTSCHLAND GMBH & CO. KG

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20220125

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1480833

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220415

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502019003917

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20220406

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220808

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220706

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220707

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220706

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220806

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502019003917

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20230110

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220406

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20230228

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20230213

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230213

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230213

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230213

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230213

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20230228

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240219

Year of fee payment: 6

Ref country code: CH

Payment date: 20240301

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20240228

Year of fee payment: 6

Ref country code: FR

Payment date: 20240222

Year of fee payment: 6