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EP0005668A1 - Verfahren zur Herstellung von Formkörpern aus einer Legierung durch Pulvermetallurgie - Google Patents

Verfahren zur Herstellung von Formkörpern aus einer Legierung durch Pulvermetallurgie Download PDF

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Publication number
EP0005668A1
EP0005668A1 EP79400302A EP79400302A EP0005668A1 EP 0005668 A1 EP0005668 A1 EP 0005668A1 EP 79400302 A EP79400302 A EP 79400302A EP 79400302 A EP79400302 A EP 79400302A EP 0005668 A1 EP0005668 A1 EP 0005668A1
Authority
EP
European Patent Office
Prior art keywords
alloy
powder
temperature
mixture
powders
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP79400302A
Other languages
English (en)
French (fr)
Other versions
EP0005668B1 (de
Inventor
Jacques Devillard
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.)
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Commissariat a lEnergie Atomique CEA
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 Commissariat a lEnergie Atomique CEA filed Critical Commissariat a lEnergie Atomique CEA
Publication of EP0005668A1 publication Critical patent/EP0005668A1/de
Application granted granted Critical
Publication of EP0005668B1 publication Critical patent/EP0005668B1/de
Expired legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based 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
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/09Mixtures of metallic powders

Definitions

  • the subject of the present invention is a method for manufacturing alloy parts by powder metallurgy, and more particularly a method for manufacturing superalloy parts based on nickel or on iron, having the form of discs or blades of turbines for rotating machines.
  • the manufacturing methods by casting and by forging have certain drawbacks, in particular for the production of alloy parts very loaded with additives because the operations of casting and transformation by forging become more and more complex due to the difficulties due mainly the appearance of segregations which increase the brittleness of the alloys.
  • the powder metallurgy manufacturing methods make it possible to avoid the aforementioned drawback because by dividing the alloy into micro-ingots which are then combined by sintering, it is possible to produce highly alloyed preforms having a minimum of segregation.
  • the methods using liquid phase sintering require the use of a sintering aid such as phosphorous nickel to lower the temperature and the pressure for shaping the powder, and the addition of a foreign element, even at very low contents, risk of profoundly altering the mechanical properties of the alloy
  • the present invention specifically relates to a method of manufacturing alloy parts by powder metallurgy which overcomes the aforementioned drawbacks because it allows sintering in the liquid phase without requiring the addition of a foreign element and without implementing high pressures.
  • the method according to the invention is characterized in that it consists in preparing from the constituents of said alloy an powder or a mixture of two powders each comprising all the constituents of said alloy, said powder or the mixture of said powders comprising a solid phase fuse at a temperature T 1 lower than the theoretical burning temperature T of said alloy, then sintering under load said powder or the mixture of said powders at a temperature at least equal to T 1 , said temperature being such that only one of the phases of the powder is liquid.
  • said alloy is preferably chosen from the group comprising nickel-based alloys and iron-based alloys.
  • the method as characterized above advantageously takes advantage of the fact that, starting from a powder or a mixture of powders having the property of forming a liquid phase at a temperature below what is agreed to call the theoretical temperature of "burning" of the alloy, that is to say the temperature which corresponds to the melting of a phase of an alloy in which several phases are in equilibrium, phase sintering can be carried out liquid of the powder at a lower temperature, in addition in certain cases avoiding that the whole of the powder forms a liquid phase.
  • said powder is prepared by rapidly cooling liquid droplets of said alloy to obtain by solidification of said droplets powder particles comprising a solid phase whose composition does not correspond to equilibrium, said solid phase being fusible at a temperature T 1 lower than the theoretical burning temperature of the alloy.
  • the liquid droplets can for example be formed from a cylindrical ingot of said alloy by bringing to a melting temperature the end surface of said ingot rotated about its axis so that the molten alloy is ejected from the surface end of the ingot, under the action of centrifugal force, in the form of liquid droplets.
  • the liquid present at the solidification interface rapidly reaches the eutectic composition while the solidified part of the alloy does not have the composition corresponding to the solubility limit.
  • This mode of formation of a more fusible phase in the powder particles can be applied to alloys other than nickel alloys and in particular to all alloys which can be reduced to binary alloys, for example steels in which the interdendritic spaces consist of ferrite.
  • said powder is prepared by homogeneously mixing a powder of an alloy A 1 and a powder of a alloy A 2 , said alloys A 1 and A 2 comprising all the constituents of said alloy but having a different content in at least two of said constituents so that the alloy A 1 forms a liquid phase at a temperature T 1 lower than the temperature T 2 at which the alloy A 2 forms a liquid phase, and said mixture of powders is sintered under load at a temperature between T 1 and T 2 .
  • the concentration of the main constituents of the alloys A 1 and A 2 is identical and only the contents of certain addition elements present at minor concentrations vary, in particular, the contents of certain addition elements such as carbon , boron and zirconium.
  • This second embodiment of the process of the invention proves to be particularly advantageous since the use of two types of powder makes it possible to form a liquid phase only in a single type of powder without requiring the addition of an element. foreign and by modifying only very little the content of one of the powders in one of the constituents of the alloy.
  • the mixture of powders is, for example, constituted by equal volumes of powder of alloy A 1 and of powder of alloy A 2 whose particle sizes are substantially identical for example of the order of 50 to 300p.
  • variable volumes of powder of alloy A 1 and of powder of alloy A 2 provided, however, that in the mixture homogeneous powders, each less fusible particle of alloy A- is in contact with a more fusible particle of alloy A 1 .
  • variable particle sizes can be used for each of the powders of alloy A and alloy A 2 , for example in order to obtain a more compact stacking of powder particles.
  • the duration and the pressure of sintering are chosen according to the nature of the alloy.
  • the sintering pressure is advantageously of the order of 100 bars and the duration of sixty minutes.
  • the powder or the mixture of powders For the operation of sintering the powder or the mixture of powders, it is preferable to bring the powder or the mixture of powders to the sintering temperature as quickly as possible, for example by heating so as to increase the temperature of the powder or mixture of powders from 1,000 to 10,000 ° C per hour. By operating in this way, large diffusion and homogenization during heating of the powder are avoided, which would be detrimental to obtaining good sintering kinetics.
  • the powder or powder mixture when the powder or powder mixture is at the sintering temperature, it is important to keep the powder or the powder mixture at this sintering temperature only for a relatively short time to avoid diffusion and magnification. grains and thus obtain a dense structure, well sintered and generally homogeneous.
  • the powder or mixture of powders is maintained at the sintering temperature for a period of at most one hour.
  • An example relates to the manufacture of a piece of nickel alloy, according to the second embodiment of the method of the invention, that is to say by sintering of a mixture of powders of two alloys having a similar composition, the other relating to a sintering of an iron-based alloy according to the first embodiment.
  • the first powder of alloy A 1 contains 12% chromium, 18% cobalt, 3% molybdenum, 4% titanium, 5% aluminum, 0.011% boron, 0.05% zirconium and 0.2 % carbon, the rest being nickel
  • the second powder of alloy A 2 contains 12% chromium, 18% cobalt, 3% molybdenum, 4% titanium, 5% aluminum, 0.011% boron, 0.05% zirconium and 0.003% carbon, the rest being nickel.
  • the powders of alloy A 1 and of alloy A 2 each have a particle size between 50 and 300 ⁇ .
  • the mold is then placed inside a heating device, by inserting between the walls of the mold and the device a refractory metal powder having a low sinterability, at the temperature chosen for sintering the powder mixture.
  • the mold containing the powder mixture is then brought to a temperature of approximately 1,290 ° C., heating the mold filled with powders very quickly, by example by increasing its temperature by 1000 ° C per hour.
  • the mold is then kept at the chosen temperature of 1290 ° C., under a uniaxial pressure of 50 to 100 bars, for a period of approximately sixty minutes to ensure the sintering of the powder mixture.
  • the compression of the powder during sintering is carried out by means of a piston of refractory material which takes place at the top of the mold and can slide in the cylindrical counterweight in order to load inside the mold the additional quantity of powder initially placed in this feeder, thus helping to eliminate the porosity in the sintered part.
  • the parts After demolding, the parts have a perfect surface condition with grains with an average size of 50 ⁇ .
  • This powder obtained by centrifugation of a bar, reveals by metallography a ferritic structure 6 with excess eutectic liquid coming from the non-equilibrium during solidification.
  • This powder whose grain diameter is between 100 and 600 ⁇ , is sintered at 1,200-1,220 ° C for three minutes under 300 bars.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
EP79400302A 1978-05-16 1979-05-14 Verfahren zur Herstellung von Formkörpern aus einer Legierung durch Pulvermetallurgie Expired EP0005668B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR7814432A FR2425906A1 (fr) 1978-05-16 1978-05-16 Procede de fabrication de pieces en alliage par metallurgie des poudres
FR7814432 1978-05-16

Publications (2)

Publication Number Publication Date
EP0005668A1 true EP0005668A1 (de) 1979-11-28
EP0005668B1 EP0005668B1 (de) 1984-11-28

Family

ID=9208274

Family Applications (1)

Application Number Title Priority Date Filing Date
EP79400302A Expired EP0005668B1 (de) 1978-05-16 1979-05-14 Verfahren zur Herstellung von Formkörpern aus einer Legierung durch Pulvermetallurgie

Country Status (4)

Country Link
EP (1) EP0005668B1 (de)
JP (1) JPS54150309A (de)
DE (1) DE2967309D1 (de)
FR (1) FR2425906A1 (de)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0095607A1 (de) * 1982-05-28 1983-12-07 General Electric Company Verfahren zum Reparieren eines Superlegierungskörpers und Metallegierungspulvermischung zur Anwendung dieses Verfahrens
FR2610856A1 (fr) * 1987-02-18 1988-08-19 Snecma Procede d'assemblage de pieces en superalliages a base de nickel par frittage en phase liquide et compaction isostatique a chaud
WO2003010347A1 (en) * 2001-07-24 2003-02-06 Mitsubishi Heavy Industries, Ltd. Ni-BASE SINTERED ALLOY

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU561663B2 (en) * 1982-05-28 1987-05-14 General Electric Company Homogeneous superalloy powder mixture for the repair of nickel and cobalt superalloy articles
JP5384079B2 (ja) * 2008-10-29 2014-01-08 Ntn株式会社 焼結軸受

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR949279A (fr) * 1940-03-07 1949-08-25 Gen Motors Corp Procédé perfectionné de fabrication d'objets métalliques poreux et produits en résultant
FR968581A (fr) * 1948-06-30 1950-11-30 Boehler & Co Ag Geb Procédé pour la fabrication d'alliages d'acier frittés
FR1263847A (fr) * 1960-04-14 1961-06-19 Birmingham Small Arms Co Ltd Perfectionnements concernant la métallurgie des poudres
GB888274A (en) * 1959-03-19 1962-01-31 Gen Electric Co Ltd Improvements in or relating to the manufacture of sintered alloy bodies
FR2296491A1 (fr) * 1975-01-06 1976-07-30 United Technologies Corp Charge metallique et son application dans une methode d'obturation des fissures des pieces metalliques
GB1535409A (en) * 1976-09-25 1978-12-13 Ford Motor Co Master alloy powders
FR2394614A1 (fr) * 1977-06-16 1979-01-12 Us Energy Alliage a base de cuivre pour le frittage avec phase liquide des poudres ferreuses

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR949279A (fr) * 1940-03-07 1949-08-25 Gen Motors Corp Procédé perfectionné de fabrication d'objets métalliques poreux et produits en résultant
FR968581A (fr) * 1948-06-30 1950-11-30 Boehler & Co Ag Geb Procédé pour la fabrication d'alliages d'acier frittés
GB888274A (en) * 1959-03-19 1962-01-31 Gen Electric Co Ltd Improvements in or relating to the manufacture of sintered alloy bodies
FR1263847A (fr) * 1960-04-14 1961-06-19 Birmingham Small Arms Co Ltd Perfectionnements concernant la métallurgie des poudres
FR2296491A1 (fr) * 1975-01-06 1976-07-30 United Technologies Corp Charge metallique et son application dans une methode d'obturation des fissures des pieces metalliques
GB1535409A (en) * 1976-09-25 1978-12-13 Ford Motor Co Master alloy powders
FR2394614A1 (fr) * 1977-06-16 1979-01-12 Us Energy Alliage a base de cuivre pour le frittage avec phase liquide des poudres ferreuses

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0095607A1 (de) * 1982-05-28 1983-12-07 General Electric Company Verfahren zum Reparieren eines Superlegierungskörpers und Metallegierungspulvermischung zur Anwendung dieses Verfahrens
FR2610856A1 (fr) * 1987-02-18 1988-08-19 Snecma Procede d'assemblage de pieces en superalliages a base de nickel par frittage en phase liquide et compaction isostatique a chaud
WO2003010347A1 (en) * 2001-07-24 2003-02-06 Mitsubishi Heavy Industries, Ltd. Ni-BASE SINTERED ALLOY
US6884275B2 (en) 2001-07-24 2005-04-26 Mitsubishi Heavy Industries, Ltd. Ni-based sintered alloy
US7261758B2 (en) 2001-07-24 2007-08-28 Mitsubishi Heavy Industries, Ltd. Ni-based sintered alloy

Also Published As

Publication number Publication date
DE2967309D1 (en) 1985-01-10
JPS54150309A (en) 1979-11-26
EP0005668B1 (de) 1984-11-28
FR2425906A1 (fr) 1979-12-14
JPS6312133B2 (de) 1988-03-17
FR2425906B1 (de) 1982-10-22

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