EP0277450A1 - Verfahren zur Herstellung von Keramik-Metall-Verbundstoffen unter Verwendung tensioaktiver Metalle an den Keramik-Metall-Kontaktflächen - Google Patents

Verfahren zur Herstellung von Keramik-Metall-Verbundstoffen unter Verwendung tensioaktiver Metalle an den Keramik-Metall-Kontaktflächen Download PDF

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Publication number
EP0277450A1
EP0277450A1 EP19870420356 EP87420356A EP0277450A1 EP 0277450 A1 EP0277450 A1 EP 0277450A1 EP 19870420356 EP19870420356 EP 19870420356 EP 87420356 A EP87420356 A EP 87420356A EP 0277450 A1 EP0277450 A1 EP 0277450A1
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EP
European Patent Office
Prior art keywords
metal
ceramic
phase
powder
manufacturing
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EP19870420356
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English (en)
French (fr)
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EP0277450B1 (de
Inventor
Jöel Demit
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DEMIT, JOEEL
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Demit Joel
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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/005Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides comprising a particular metallic binder
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ

Definitions

  • the present invention relates to ceramic-metal composites and their production methods. It makes it possible to produce, by the methods of powder metallurgy and / or ceramic, a set of homogeneous polyphase materials, which have at least one ceramic phase and one metal phase.
  • Powder metallurgy technologies are now well known. They derive from ceramic art. Details of these can be found, in particular, in French patent 2,057,562.
  • the constituents of the materials to be formed are used in the form of powders, some of which may be pre-alloyed beforehand.
  • the rest of the process is conditioned by the type of shaping used to make the desired article. among the different possible types, it should be mentioned, although this is not limiting: - pouring into a porous mold, - spreading in thin sheet, - extrusion, - thermoplastic injection, - pressing, - electrophoresis, etc ...
  • a temporary binder is generally added to the composition, in the form of an organic polymer. Its role is to gather the grains of powder into small quasi-spherical granules of similar size and provided with plasticity.
  • the pressing dies are fed with this granule. It allows a reproducible filling.
  • a pressure close to 1 T / cm2 by means of two punches, in the case of biaxial pressing. Under the effect of the pressure, the granules deform until they become practically contiguous while expelling residual air from the matrix. Compacts are thus obtained, the density of which can be greater than 70% of the theoretical density.
  • the compacts are then transferred to ovens to be densified by the sintering operation, after purification of the organic binders.
  • This sintering can be carried out with or without pressure at a sufficient temperature, in the vast majority of cases, to achieve volume diffusion of the elements.
  • the compacts evolve towards greater stability, on the one hand, by reducing their surface energy by elimination of the pores and crystal growth and, on the other hand, by forming the stable phases at the considered temperatures.
  • the binding phase has a continuity character: it coats the grains of the dispersed phase or phases, but generally remains a minority in volume; by way of example, it can be said that the binding phase occupies 30% + or - 10% of the volume. It is under these conditions that, in general, the best properties are obtained, without this is an absolute rule.
  • heterogeneities encountered in these systems, at the end of the production processes, such as sintering or infiltration, are of two types: - Porosity, - Poor phase dispersion.
  • the role of the surfactants will be to serve as an intermediary between the dispersed and metal phases, and to lower the energy of GIBBS of the whole. It has been found that certain metals which have a certain affinity for the metal phase and an affinity for the ceramic phase, particularly by forming compounds, of very negative free enthalpy, could play this role. This is particularly the case when the surfactant element has an isotype (or even isomorphic) compound, or a structure close to that of the ceramic phase.
  • These surface-active elements are particularly reactive, and especially with respect to oxygen; this is the reason why, rather than using them directly in metal form, one will preferably use one of their compounds, easily decomposable to heat, such as hydrides.
  • These compounds, generators of surface-active elements are introduced in pulverulent form, before mixing-grinding of the other constituents, with a suitable particle size, so as to obtain an intimate mixture and of uniform particle size of the whole.
  • the systems which are the subject of the invention contain a metallic part, which is a minority in volume, ie from 50% to 5%, and a ceramic part, ie from 50% to 95%; this metallic part, contains, in addition, the surface-active metals, which ensure the connection and the transition between the metallic and ceramic phases, possibly by the formation of compounds, during the sintering process.
  • the ceramic material is chosen from the following compounds: - corundum type compounds: Al203, Cr203, Ti203 Y203, etc ..., - silicon nitride, titanium nitride, boron nitride, - titanium diboride, - silicon carbide, boron carbide, titanium carbide,
  • the metal part is chosen from the metals and alloys below: - nickel, - alloys refractory to Ni, Cr, Co, Fe (type the product known under the brand name Refractaloy) - controlled expansion alloys based on iron and nickel, known under the brand names Invar, ADR, N42, N56, Dilver, or Platinite - aluminum, - alloy used in friction such as lead bronze, tin, aluminum, silicon.
  • ceramics, metals, compounds generating surface-active metals are used in the form of powders. These powders are used by the methods of powder metallurgy (or ceramic), methods well known to those skilled in the art, for the production of objects, obtained in the green state, in an intermediate stage. These objects are then densified in a secondary vacuum oven preferably working under load (although the load is not necessary).
  • the sintering temperature is located near the melting temperature of the metal alloy used (for example more or less 100 ° C). During the heat treatment, the surface-active metal or metals diffuse and ensure the bonding at the interfaces, with possible formation of compounds or alloys.
  • an argon sweep is carried out, with a flow rate of 1 l / min. approximately, for 2 min., in order to expel most of the air. Then we close the jar quickly.
  • the jar is placed on a jar turner, speed of the order of 90 revolutions per minute, and it is rotated for approximately 8 hours. The purpose of this operation is to homogenize and grind the different constituents.
  • the suspension of beads is separated, then it is dried with stirring to avoid demixing of the constituents, optionally under reduced pressure, preferably in a granulator.
  • the powder is then compacted in the press in the form of test tubes, and the residual camphor is sublimed.
  • the test pieces are then treated in a sintering oven under load, working under secondary vacuum.
  • One operates under a vacuum of 10 ⁇ 5 torre and under a load corresponding to a pressure of 10 MPa.
  • the heat treatment comprises a level of decomposition of hydrides between 300 ° C and 500 ° C and a level of sintering 30 min. at 1200 ° C, the temperature rise being carried out in 2 hours.
  • a pellet of density 6.02 is obtained.
  • the duration and the temperature of the sintering stage depend on the pressure exerted: without pressure they can be brought to 2 hours and 1450 ° C, respectively.
  • Ceramic-metal composites are thus obtained, corresponding to the invention.
  • Sintering is carried out under the following conditions: Temperature rise of 1000 ° C, linearly in 75 min. , under vacuum of 10 ⁇ 5 torre without pressure; progressive loading up to a pressure of 10 MPa reached in 15 min. and maintaining the pressure until the end of the heat treatment; rise to 1350 ° C in 1 hour and step of 40 min. at this temperature.
  • a composite pellet of density 5.15 is obtained.
  • Example 2 The procedure is as in Example 1, with a heat treatment of 1 hour at 1360 ° C, according to the following formula: - 438 g of chromium oxide - 236 g of MCrA1Y alloy.
  • the composition of MCrA1Y is in percentage: Ni 10, Co 52, Cr 25, Al 7, Ti 5, YO, 75; Its average particle size is around 25 microns.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Ceramic Products (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Compounds Of Alkaline-Earth Elements, Aluminum Or Rare-Earth Metals (AREA)
EP87420356A 1986-12-29 1987-12-29 Verfahren zur Herstellung von Keramik-Metall-Verbundstoffen unter Verwendung tensioaktiver Metalle an den Keramik-Metall-Kontaktflächen Expired - Lifetime EP0277450B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87420356T ATE90398T1 (de) 1986-12-29 1987-12-29 Verfahren zur herstellung von keramik-metallverbundstoffen unter verwendung tensioaktiver metalle an den keramik-metall-kontaktflaechen.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8618479 1986-12-29
FR8618479A FR2608950B1 (fr) 1986-12-29 1986-12-29 Procede de fabrication de materiaux composites ceramique-metal par utilisation de metaux tensio-actifs aux interfaces ceramique-metal

Publications (2)

Publication Number Publication Date
EP0277450A1 true EP0277450A1 (de) 1988-08-10
EP0277450B1 EP0277450B1 (de) 1993-06-09

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP87420356A Expired - Lifetime EP0277450B1 (de) 1986-12-29 1987-12-29 Verfahren zur Herstellung von Keramik-Metall-Verbundstoffen unter Verwendung tensioaktiver Metalle an den Keramik-Metall-Kontaktflächen

Country Status (5)

Country Link
EP (1) EP0277450B1 (de)
AT (1) ATE90398T1 (de)
DE (1) DE3786163T2 (de)
ES (1) ES2042597T3 (de)
FR (1) FR2608950B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145513A (en) * 1990-04-13 1992-09-08 Centre National De Le Recherche Scientifique Process for the preparing via the in situ reduction of their components and grinding oxide/metal composite materials
WO2015139699A1 (de) * 2014-03-20 2015-09-24 Schaeffler Technologies AG & Co. KG Lagerelement für ein gleit- oder wälzlager

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007005211B4 (de) 2007-01-30 2010-03-11 Iav Gmbh Ingenieurgesellschaft Auto Und Verkehr Verfahren zur Herstellung eines Verbundwerkstoffes

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1473618A (fr) * 1966-03-30 1967-03-17 Sherritt Gordon Mines Ltd Procédé de fabrication d'alliages de nickel et de chrome renforcés par une dispersion d'oxyde réfractaire
FR2057562A5 (de) * 1969-08-27 1971-05-21 Int Nickel Ltd
FR2095826A5 (de) * 1970-06-22 1972-02-11 Sherritt Gordon Mines Ltd
FR2223473A1 (de) * 1973-03-28 1974-10-25 United Aircraft Corp

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1473618A (fr) * 1966-03-30 1967-03-17 Sherritt Gordon Mines Ltd Procédé de fabrication d'alliages de nickel et de chrome renforcés par une dispersion d'oxyde réfractaire
FR2057562A5 (de) * 1969-08-27 1971-05-21 Int Nickel Ltd
FR2095826A5 (de) * 1970-06-22 1972-02-11 Sherritt Gordon Mines Ltd
FR2223473A1 (de) * 1973-03-28 1974-10-25 United Aircraft Corp

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN, vol. 10, no. 17 (C-324)[2074], 23 janvier 1986; & JP-A-60 169 533 (TOSHIBA TUNGALOY K.K.) 03-09-1985 *
PATENT ABSTRACTS OF JAPAN, vol. 5, no. 85 (C-57)[757], 3 juin 1981; & JP-A-56 029 650 (TOSHIBA TUNGALOY K.K.) 25-03-1981 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145513A (en) * 1990-04-13 1992-09-08 Centre National De Le Recherche Scientifique Process for the preparing via the in situ reduction of their components and grinding oxide/metal composite materials
WO2015139699A1 (de) * 2014-03-20 2015-09-24 Schaeffler Technologies AG & Co. KG Lagerelement für ein gleit- oder wälzlager
CN106415036A (zh) * 2014-03-20 2017-02-15 舍弗勒技术股份两合公司 用于滑动轴承或滚动轴承的轴承元件

Also Published As

Publication number Publication date
ATE90398T1 (de) 1993-06-15
DE3786163D1 (de) 1993-07-15
FR2608950A1 (fr) 1988-07-01
EP0277450B1 (de) 1993-06-09
ES2042597T3 (es) 1993-12-16
DE3786163T2 (de) 1994-01-27
FR2608950B1 (fr) 1991-10-18

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