EP3184211A1 - Material obtained by compacting and densifying metal powder(s) - Google Patents
Material obtained by compacting and densifying metal powder(s) Download PDFInfo
- Publication number
- EP3184211A1 EP3184211A1 EP15201640.8A EP15201640A EP3184211A1 EP 3184211 A1 EP3184211 A1 EP 3184211A1 EP 15201640 A EP15201640 A EP 15201640A EP 3184211 A1 EP3184211 A1 EP 3184211A1
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- EP
- European Patent Office
- Prior art keywords
- powder
- powders
- phase
- process according
- densification
- Prior art date
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- 239000000463 material Substances 0.000 title claims abstract description 38
- 239000000843 powder Substances 0.000 title claims description 77
- 229910052751 metal Inorganic materials 0.000 title claims description 13
- 239000002184 metal Substances 0.000 title claims description 13
- 239000007769 metal material Substances 0.000 claims abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 29
- 238000000034 method Methods 0.000 claims description 26
- 239000000203 mixture Substances 0.000 claims description 23
- 230000008569 process Effects 0.000 claims description 21
- 238000000280 densification Methods 0.000 claims description 20
- 239000010949 copper Substances 0.000 claims description 16
- 229910001369 Brass Inorganic materials 0.000 claims description 15
- 239000010951 brass Substances 0.000 claims description 15
- 238000005056 compaction Methods 0.000 claims description 13
- 229910052802 copper Inorganic materials 0.000 claims description 13
- 229910052759 nickel Inorganic materials 0.000 claims description 12
- 229910000906 Bronze Inorganic materials 0.000 claims description 11
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 10
- 239000010974 bronze Substances 0.000 claims description 10
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 9
- 238000002156 mixing Methods 0.000 claims description 8
- 229910052725 zinc Inorganic materials 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 6
- 238000004663 powder metallurgy Methods 0.000 claims description 6
- 229910045601 alloy Inorganic materials 0.000 claims description 5
- 239000000956 alloy Substances 0.000 claims description 5
- 229910052718 tin Inorganic materials 0.000 claims description 5
- 229910052721 tungsten Inorganic materials 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 229910052737 gold Inorganic materials 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910052758 niobium Inorganic materials 0.000 claims description 3
- 229910052763 palladium Inorganic materials 0.000 claims description 3
- 229910052697 platinum Inorganic materials 0.000 claims description 3
- 229910052720 vanadium Inorganic materials 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 150000002739 metals Chemical class 0.000 claims description 2
- 239000002245 particle Substances 0.000 description 10
- 239000007787 solid Substances 0.000 description 10
- 239000000047 product Substances 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 238000005245 sintering Methods 0.000 description 6
- 239000011135 tin Substances 0.000 description 5
- 238000009826 distribution Methods 0.000 description 4
- 230000003993 interaction Effects 0.000 description 4
- 238000003754 machining Methods 0.000 description 4
- 239000011701 zinc Substances 0.000 description 4
- 239000011230 binding agent Substances 0.000 description 3
- 238000007596 consolidation process Methods 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 239000011812 mixed powder Substances 0.000 description 3
- 238000007493 shaping process Methods 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000006664 bond formation reaction Methods 0.000 description 2
- 239000011195 cermet Substances 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 229910017518 Cu Zn Inorganic materials 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 229910002065 alloy metal Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 238000001033 granulometry Methods 0.000 description 1
- 239000008240 homogeneous mixture Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/16—Both compacting and sintering in successive or repeated steps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/05—Metallic powder characterised by the size or surface area of the particles
- B22F1/052—Metallic powder characterised by the size or surface area of the particles characterised by a mixture of particles of different sizes or by the particle size distribution
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/02—Compacting only
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/08—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of toothed articles, e.g. gear wheels; of cam discs
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0425—Copper-based alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/002—Alloys based on nickel or cobalt with copper as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/06—Alloys containing less than 50% by weight of each constituent containing zinc
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/02—Alloys based on copper with tin as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/04—Alloys based on copper with zinc as the next major constituent
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B1/00—Driving mechanisms
- G04B1/10—Driving mechanisms with mainspring
- G04B1/14—Mainsprings; Bridles therefor
- G04B1/145—Composition and manufacture of the springs
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B13/00—Gearwork
- G04B13/02—Wheels; Pinions; Spindles; Pivots
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B15/00—Escapements
- G04B15/14—Component parts or constructional details, e.g. construction of the lever or the escape wheel
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B17/00—Mechanisms for stabilising frequency
- G04B17/04—Oscillators acting by spring tension
- G04B17/06—Oscillators with hairsprings, e.g. balance
- G04B17/066—Manufacture of the spiral spring
-
- G—PHYSICS
- G04—HOROLOGY
- G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
- G04B31/00—Bearings; Point suspensions or counter-point suspensions; Pivot bearings; Single parts therefor
- G04B31/06—Manufacture or mounting processes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
- B22F2009/0824—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid with a specific atomising fluid
- B22F2009/0828—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid with a specific atomising fluid with water
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2301/00—Metallic composition of the powder or its coating
- B22F2301/10—Copper
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2301/00—Metallic composition of the powder or its coating
- B22F2301/15—Nickel or cobalt
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2301/00—Metallic composition of the powder or its coating
- B22F2301/30—Low melting point metals, i.e. Zn, Pb, Sn, Cd, In, Ga
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2303/00—Functional details of metal or compound in the powder or product
- B22F2303/15—Intermetallic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2304/00—Physical aspects of the powder
- B22F2304/10—Micron size particles, i.e. above 1 micrometer up to 500 micrometer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
Definitions
- the present invention relates to a material and its method of manufacturing powder metallurgy.
- An area of application targeted with this new material is that of mechanics and, more specifically, micromechanics. It is even more specifically adapted for components having complex geometries with severe tolerances, as in watchmaking, for example.
- Powder metallurgy materials are of considerable technological importance and are used in a wide range of fields from nuclear to biomedical.
- the present invention proposes to select the composition of the starting powders according to the desired properties on the final product and to adapt the parameters of the process to limit the interactions between the powders and thus obtain the expected properties on the basis of the initial choice of the powders.
- the figure 1 represents the microstructure of a three-phase material obtained with the method according to the invention.
- the densification was carried out at a temperature close to 500 ° C on a compacted mixture of nickel, brass and bronze.
- the figure 2 represents this same microstructure after image processing to reveal the different phases.
- the Figures 3 and 4 represent the microstructure of the same triphasic material when the densification is operated at a temperature close to 700 ° C.
- the Figures 5 and 6 represent, by way of comparison, the microstructures of materials of the prior art obtained by powder metallurgy.
- To the figure 5 it is a bi-phased sintered solid ( US 5,294,269 ).
- White represents the heavy phase consisting mainly of tungsten.
- the black phase is the metallic binder phase consisting essentially of a nickel, iron, copper, cobalt and molybdenum alloy.
- To the figure 6 it is a sintered cermet ( US 2004/0231459 ).
- Binder is the binder phase made of stainless steel 347SS.
- the ceramic phase is composed of TiC (titanium carbide).
- the last phase consists of precipitates M 7 C 3 where M contains chromium, iron and titanium.
- the present invention relates to a method of manufacturing a material by powder metallurgy and to the material resulting from the process.
- the method is adapted so that the microstructure of the material is perfectly homogeneous through its volume and that it is an image as faithful as possible of the microstructure of the mixed powders and their initial distribution in the mixture.
- the material resulting from the process may be a finished product or a semi-finished product requiring a subsequent machining step.
- the material is a metallic material obtained from a three-step process.
- the first step consists of selecting one or more metal powders and dosing them when several powders are present. It can be powders of a pure metal or an alloy.
- the number of starting powders, their compositions and their respective percentages depend on the physico-mechanical properties desired on the consolidated product.
- the powders are at least two in number to combine the properties of different compositions.
- Each powder is formed of particles having a particle size chosen to guarantee the quality of the material.
- their average diameter d 50 is preferably chosen in a range between 1 and 100 microns.
- the metal powders are chosen from the non-exhaustive list comprising pure metals or alloys based on titanium, copper, zinc, iron, aluminum, nickel, chromium, cobalt, vanadium and zirconium. , niobium, molybdenum, palladium, silver, tantalum, tungsten, platinum and gold.
- the mixture comprises three powders: a nickel powder, a bronze powder and a brass powder.
- the percentages Cu, Sn and Cu, Zn can be respectively modulated.
- the content of Cu and Zn can be respectively 60 and 40% and for bronze, the content of Cu and Sn can be respectively 90 and 10%.
- a second step the different powders are mixed.
- Mixing is carried out in a standard commercial dry blender.
- the setting of the mixer and the duration of mixing are chosen so that at the end of this step, the mixture is perfectly homogeneous.
- the mixing time is greater than 12 hours to ensure this homogeneity and less than 24 hours. It should be noted that in the presence of a single starting powder, the mixing step is optional.
- the homogeneous mixture is shaped, i.e. compacted and densified at a temperature below the melting temperature of the respective powders.
- Hot compaction and densification is performed using impact compaction technology as described in the application. WO 2014/199090 .
- the mixed powders are placed in an impression made in a matrix and compaction of the mixture is carried out by means of a punch.
- the compacted mixture is hot densified by subjecting the punch to impacts.
- the cooling step under pressure can be omitted.
- the process parameters are chosen to obtain a consolidated body with a relative density greater than or equal to 95% and better than or equal to 98%, while limiting the interactions between the different powders.
- the objective is to achieve microstrain between particles to consolidate the material without significantly altering the microstructure of the various powders present.
- the consolidation parameters are chosen to limit the degree of sintering to surface bond formation and not to volume bond formation as observed during actual sintering. Microstructurally, this intergranular bond results in the formation of bridges between particles. Limiting the interactions between particles makes it possible to maintain a distribution of the powders within the consolidated material close to that observed after mixing the powders.
- Compaction and impact densification of the powder mixture thus makes it possible to weld the grains of the powders together while preserving a microstructure with high energy interfaces between the different constitutive phases.
- the material resulting from the process has the characteristics that the constituent elements of the different powders do not mix and that the morphology of the base particles is retained after compaction and densification.
- the morphology of the grains of the obtained material is an image of the morphology of the particles of the initial powder, which is advantageous for guaranteeing mechanical properties on the basis of the initial choice of morphology. powder.
- the powder mixture is at a temperature below the melting temperature of the lower melting point powder during hot densification.
- the mixture is brought to this temperature for a time of between 3 and 30 minutes and, preferably, between 5 and 20 minutes. It can be brought to this temperature before introduction in the press or in the press.
- the time indicated above includes the heating time to reach the given temperature and the maintenance at this temperature.
- the mixture is subjected to a number of impacts of between 1 and 50 with an energy level of between 500 and 2000J, this level being preferably 10 to 30% higher than the energy level required when compaction.
- the product thus obtained has a relative density greater than or equal to 95% and, preferably, 98%, measured conventionally by weighing Archimedes.
- a cut metallurgical reveals a very specific microstructure due to the process of shaping the material.
- the material comprises a number of phases corresponding to the number of initial powders with a distribution of the phases substantially the same as that of the powders within the starting mixture.
- Another very specific characteristic of this microstructure is that the surface energy of the phases thus consolidated is conserved at high levels.
- the native morphology of the powder particles remains almost completely preserved with an interface between irregularly shaped phases, which can also be described as non-spherical.
- the consolidated phases thus retain a high specific surface area.
- Figures 1 and 2 reveal the microstructure obtained from a mixture of three powders: nickel, bronze, brass as shown in Table 1.
- the mixture was compacted and densified at a temperature close to 500 ° C.
- the microstructure has three distinct phases respectively consisting mainly of nickel, bronze and brass.
- the homogeneity of the microstructure obtained is that obtained after the step of mixing the three kinds of powder.
- the product thus obtained has a relative density greater than 95%.
- Figures 3 and 4 this same homogeneity of microstructure with three distinct phases.
- an interdiffusion between the two pairs nickel-bronze and bronze-brass is observed, the phase rich in nickel being surrounded by the phase rich in bronze. This interdiffusion makes it possible to increase the relative density to a value greater than or equal to 98%.
- Tables 1 and 2 Three metal powders listed in Tables 1 and 2 below were selected in step 1) of the process.
- the function of each powder is detailed in Table 1.
- the compositions and percentages of the various powders are detailed in Table 2.
- ⁇ u> Table 1 ⁇ / u> Selected powders Function and / or characteristic Pure nickel (Ni) metal powder Providing consolidated and densified material with good welding behavior, especially laser welding Brass alloy metal powder, with a nominal chemical composition of 60% copper (Cu) and 40% zinc (Zn). Offering good machinability Bronze alloy metal powder, with a nominal chemical composition of 90% copper (Cu) and 10% tin (Sn).
- the powders were mixed in a commercial Turbula T10B mixer.
- the mixing speed is an average speed of the order of 200 rpm for 24 hours.
- the shaping was carried out using a high speed and high energy press of the manufacturer Hydropulsor.
- the formatting was performed in two phases:
- the dosing of the powders in the impression is done volumetrically with a given filling height.
- this filling height is 6 mm to reach a compacted thickness of about 2 mm.
- This parameter - filling height - can vary between 2 mm and 50 mm depending on the desired final thickness on the compacted solid.
- the quantity of powders thus dosed is compacted between the punch above and the punch below, surrounded by a matrix to form a washer of a given diameter.
- This compaction is done in the example with 25 impacts. The goal of this step is to get a solid enough dense for subsequent densification at hot. This compaction also serves to ensure that the solid thus compacted is sufficiently solid for handling operations during hot densification.
- the relative density obtained at this stage is greater than 90%.
- the compacted washer is brought to a temperature close to 700 ° C in an oven preheated to this temperature.
- the compacted puck is placed in the oven for at least 5 minutes and preferably 15 minutes.
- the thus heated washer is transported and placed in the cavity of diameter slightly larger than the diameter of the washer.
- the duration of the transport of the preheated washer of the oven to the press, put in the matrix, is between 2 and 5 seconds.
- the preheated disc is then hot densified between the top punch and the bottom punch with 25 impacts. In the absence of heating means, a decrease in temperature is observed during the densification by impact.
- the final thickness in the example of the densified washer is about 1.8 mm.
- the relative density of the washer is greater than 98%.
- the microstructure is similar to that obtained at figure 3 .
- the solid obtained is a multiphase material comprising phases having different functions.
- the solid thus obtained has a homogeneous microstructure throughout its volume. As a result, there is no internal stress gradient across the solid. This provides geometric stability to the machined part.
- Each phase of the solid obtained and, upstream, each powder is chosen to fulfill a specific function.
- One of the phases may be chosen to improve the weldability, for example, by laser. This function is fulfilled by the phase consisting mainly of nickel in the example.
- Another phase may be chosen to facilitate hot densification without sintering itself.
- one of the phases of solid consists essentially of bronze which has the lowest melting range of the three constituents.
- the third phase which is, as an example, the majority phase, is composed of consolidated brass powder. This phase thus mixed with the other two makes it possible to guarantee better machining aptitude by chip removal.
- the process according to the invention also has advantages. It is thus observed that the morphology of the grains within the material is an image of the morphology of the particles of the starting powder. As the grain size plays an important role in the mechanical properties of the material, it is particularly advantageous to be able to predict the final properties on the basis of the choice of the morphology of the starting powder.
- the morphology of the base powder or powders is maintained while obtaining a product with a high relative density, unlike the known sintering process where the consolidation at relative density values greater than or equal to 95, or even 98% is accompanied by a drastic change in morphology.
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Abstract
La présente invention se rapporte à un matériau métallique compacté et densifié comprenant une ou plusieurs phases formées d'un agglomérat de grains, la cohésion du matériau étant assurée par des ponts formés entre grains, ledit matériau ayant une densité relative supérieure ou égale à 95% et, préférentiellement, à 98%.The present invention relates to a compacted and densified metal material comprising one or more phases formed of an agglomerate of grains, the cohesion of the material being provided by bridges formed between grains, said material having a relative density greater than or equal to 95% and, preferably, 98%.
Description
La présente invention se rapporte à un matériau et à son procédé de fabrication par métallurgie des poudres. Un domaine d'application visé avec ce nouveau matériau est celui de la mécanique et, plus précisément, de la micromécanique. Il est encore plus spécifiquement adapté pour des composants ayant des géométries complexes avec des tolérances sévères, comme dans l'horlogerie par exemple.The present invention relates to a material and its method of manufacturing powder metallurgy. An area of application targeted with this new material is that of mechanics and, more specifically, micromechanics. It is even more specifically adapted for components having complex geometries with severe tolerances, as in watchmaking, for example.
Les matériaux obtenus par métallurgie des poudres ont une importance technologique considérable et sont utilisés dans un large panel de domaines allant du nucléaire au biomédical.Powder metallurgy materials are of considerable technological importance and are used in a wide range of fields from nuclear to biomedical.
A titre d'exemple, on peut citer les documents
La présente invention propose de sélectionner la composition des poudres de départ en fonction des propriétés recherchées sur le produit final et d'adapter les paramètres du procédé pour limiter les interactions entre les poudres et ainsi obtenir les propriétés attendues sur base du choix initial des poudres.The present invention proposes to select the composition of the starting powders according to the desired properties on the final product and to adapt the parameters of the process to limit the interactions between the powders and thus obtain the expected properties on the basis of the initial choice of the powders.
A cette fin, un procédé et un produit selon les revendications annexés sont proposés.For this purpose, a method and a product according to the appended claims are provided.
Les caractéristiques et avantages de la présente invention apparaîtront à la lecture de la description détaillée ci-dessous faisant référence aux figures suivantes.The features and advantages of the present invention will become apparent on reading the detailed description below with reference to the following figures.
La
Les
La présente invention se rapporte à un procédé de fabrication d'un matériau par métallurgie des poudres et au matériau issu du procédé. Le procédé est adapté pour que la microstructure du matériau soit parfaitement homogène au travers de son volume et pour qu'elle soit une image la plus fidèle possible de la microstructure des poudres mélangées et de leur distribution initiale dans le mélange. Le matériau issu du procédé peut être un produit fini ou un demi-produit nécessitant une étape ultérieure d'usinage.The present invention relates to a method of manufacturing a material by powder metallurgy and to the material resulting from the process. The method is adapted so that the microstructure of the material is perfectly homogeneous through its volume and that it is an image as faithful as possible of the microstructure of the mixed powders and their initial distribution in the mixture. The material resulting from the process may be a finished product or a semi-finished product requiring a subsequent machining step.
Le matériau est un matériau métallique obtenu à partir d'un procédé comportant trois étapes.The material is a metallic material obtained from a three-step process.
La première étape consiste à sélectionner une ou plusieurs poudres métalliques et à les doser lorsque plusieurs poudres sont en présence. Il peut s'agir de poudres d'un métal pur ou d'un alliage. Le nombre de poudres de départ, leurs compositions et leurs pourcentages respectifs dépendent des propriétés physico-mécaniques désirées sur le produit consolidé. Préférentiellement, les poudres sont minimum au nombre de deux afin de combiner les propriétés propres à différentes compositions. Chaque poudre est formée de particules ayant une granulométrie choisie pour garantir la qualité du matériau. Bien que dépendant des propriétés visées, leur diamètre moyen d50 est préférentiellement choisi dans une gamme comprise entre 1 et 100 µm.The first step consists of selecting one or more metal powders and dosing them when several powders are present. It can be powders of a pure metal or an alloy. The number of starting powders, their compositions and their respective percentages depend on the physico-mechanical properties desired on the consolidated product. Preferably, the powders are at least two in number to combine the properties of different compositions. Each powder is formed of particles having a particle size chosen to guarantee the quality of the material. Although depending on the targeted properties, their average diameter d 50 is preferably chosen in a range between 1 and 100 microns.
La ou les poudres métalliques sont choisies parmi la liste non exhaustive comprenant les métaux purs ou alliages à base de titane, de cuivre, de zinc, de fer, d'aluminium, de nickel, de chrome, de cobalt, de vanadium, de zirconium, de niobium, de molybdène, de palladium, d'argent, de tantale, de tungstène, de platine et d'or. A titre d'exemple, le mélange comprend trois poudres : une poudre de nickel, une poudre de bronze et une poudre de laiton. La proportion de poudre de bronze est comprise entre 2 et 20% en poids, la proportion de poudre de nickel est comprise entre 3 et 40% en poids, la proportion de poudre de laiton étant la proportion restante (= 100% - la somme des % de poudres de nickel et de bronze). Pour le bronze et le laiton, les pourcentages Cu, Sn et Cu, Zn peuvent être respectivement également modulés. Par exemple, pour le laiton, la teneur en Cu et Zn peut être respectivement de 60 et 40% et pour le bronze, la teneur en Cu et Sn peut être respectivement de 90 et 10%.The metal powders are chosen from the non-exhaustive list comprising pure metals or alloys based on titanium, copper, zinc, iron, aluminum, nickel, chromium, cobalt, vanadium and zirconium. , niobium, molybdenum, palladium, silver, tantalum, tungsten, platinum and gold. By way of example, the mixture comprises three powders: a nickel powder, a bronze powder and a brass powder. The proportion of bronze powder is between 2 and 20% by weight, the proportion of nickel powder is between 3 and 40% by weight, the proportion of brass powder being the remaining proportion (= 100% - the sum of the% of nickel and bronze powders). For bronze and brass, the percentages Cu, Sn and Cu, Zn can be respectively modulated. For example, for brass, the content of Cu and Zn can be respectively 60 and 40% and for bronze, the content of Cu and Sn can be respectively 90 and 10%.
Dans une deuxième étape, les différentes poudres sont mélangées. Le mélange s'effectue dans un mélangeur standard du commerce à sec. Le paramétrage du mélangeur et la durée du mélange sont choisis de manière à ce qu'à la fin de cette étape, le mélange soit parfaitement homogène. Généralement, le temps de mélange est supérieur à 12h pour garantir cette homogénéité et inférieur à 24h. Il est à noter qu'en présence d'une seule poudre de départ, l'étape de mélange est optionnelle.In a second step, the different powders are mixed. Mixing is carried out in a standard commercial dry blender. The setting of the mixer and the duration of mixing are chosen so that at the end of this step, the mixture is perfectly homogeneous. Generally, the mixing time is greater than 12 hours to ensure this homogeneity and less than 24 hours. It should be noted that in the presence of a single starting powder, the mixing step is optional.
Dans une troisième étape, le mélange homogène est mis en forme, c.à.d. compacté et densifié à une température inférieure à la température de fusion des poudres respectives. La compaction et densification à chaud s'effectuent à l'aide d'une technologie de compaction par impact comme décrite dans la demande
Les paramètres du procédé sont choisis pour obtenir un corps consolidé avec une densité relative supérieure ou égale 95% et mieux supérieure ou égale à 98%, tout en limitant les interactions entre les différentes poudres. L'objectif est de réaliser une microsoudure entre particules pour consolider la matière sans altérer notablement la microstructure des différentes poudres en présence. Plus précisément, les paramètres de consolidation sont choisis pour limiter le degré de frittage à une formation de liaison de surface et non à une formation de liaison de volume comme observé lors d'un frittage à proprement dit. Microstructurellement, cette liaison intergranulaire se traduit par la formation de ponts entre particules. Limiter les interactions entre particules permet de maintenir une répartition des poudres au sein du matériau consolidé proche de celle observée après mélange des poudres. La compaction et densification par impacts du mélange de poudres permet ainsi de souder les grains des poudres entre eux tout en préservant une microstructure avec des interfaces à haute énergie entre les différentes phases constitutives. En d'autres mots, le matériau issu du procédé a pour caractéristiques que les éléments constitutifs des différentes poudres ne se mélangent pas et que la morphologie des particules de base est conservée après compaction et densification. De même, en présence d'une seule poudre de départ, la morphologie des grains du matériau obtenu est une image de la morphologie des particules de la poudre initiale, ce qui est avantageux pour garantir des propriétés mécaniques sur base du choix initial de la morphologie de la poudre.The process parameters are chosen to obtain a consolidated body with a relative density greater than or equal to 95% and better than or equal to 98%, while limiting the interactions between the different powders. The objective is to achieve microstrain between particles to consolidate the material without significantly altering the microstructure of the various powders present. More precisely, the consolidation parameters are chosen to limit the degree of sintering to surface bond formation and not to volume bond formation as observed during actual sintering. Microstructurally, this intergranular bond results in the formation of bridges between particles. Limiting the interactions between particles makes it possible to maintain a distribution of the powders within the consolidated material close to that observed after mixing the powders. Compaction and impact densification of the powder mixture thus makes it possible to weld the grains of the powders together while preserving a microstructure with high energy interfaces between the different constitutive phases. In other words, the material resulting from the process has the characteristics that the constituent elements of the different powders do not mix and that the morphology of the base particles is retained after compaction and densification. Likewise, in the presence of a single starting powder, the morphology of the grains of the obtained material is an image of the morphology of the particles of the initial powder, which is advantageous for guaranteeing mechanical properties on the basis of the initial choice of morphology. powder.
Pour obtenir cette microstructure particulière, le mélange de poudres se trouve à une température inférieure à la température de fusion de la poudre de plus bas point de fusion lors de la densification à chaud. Le mélange est porté à cette température pendant un temps compris entre 3 et 30 minutes et, préférentiellement, entre 5 et 20 minutes. Il peut être porté à cette température avant introduction dans la presse ou dans la presse. Le temps indiqué ci-dessus inclut le temps de chauffage pour arriver à la température donnée et le maintien à cette température. Lors de la densification, le mélange est soumis à un nombre d'impacts compris entre 1 et 50 avec un niveau d'énergie compris entre 500 et 2000J, ce niveau étant préférentiellement supérieur de 10 à 30% au niveau d'énergie requis lors de la compaction. Le produit ainsi obtenu a une densité relative supérieure ou égale à 95% et, de préférence, à 98%, mesurée de manière conventionnelle par pesée d'Archimède. Après cette étape de densification, une coupe métallurgique révèle une microstructure bien spécifique due au procédé de mise en forme du matériau. Le matériau comporte un nombre de phases correspondant au nombre de poudres initial avec une répartition des phases sensiblement la même que celle des poudres au sein du mélange de départ. Une autre caractéristique bien spécifique de cette microstructure est que l'énergie de surface des phases ainsi consolidée est conservée à des niveaux élevés. La morphologie native des particules de poudres reste presque totalement conservée avec une interface entre phases de forme irrégulière, qu'on peut également qualifier de non sphérique. Les phases consolidées conservent ainsi une surface spécifique élevée.To obtain this particular microstructure, the powder mixture is at a temperature below the melting temperature of the lower melting point powder during hot densification. The mixture is brought to this temperature for a time of between 3 and 30 minutes and, preferably, between 5 and 20 minutes. It can be brought to this temperature before introduction in the press or in the press. The time indicated above includes the heating time to reach the given temperature and the maintenance at this temperature. During densification, the mixture is subjected to a number of impacts of between 1 and 50 with an energy level of between 500 and 2000J, this level being preferably 10 to 30% higher than the energy level required when compaction. The product thus obtained has a relative density greater than or equal to 95% and, preferably, 98%, measured conventionally by weighing Archimedes. After this densification step, a cut metallurgical reveals a very specific microstructure due to the process of shaping the material. The material comprises a number of phases corresponding to the number of initial powders with a distribution of the phases substantially the same as that of the powders within the starting mixture. Another very specific characteristic of this microstructure is that the surface energy of the phases thus consolidated is conserved at high levels. The native morphology of the powder particles remains almost completely preserved with an interface between irregularly shaped phases, which can also be described as non-spherical. The consolidated phases thus retain a high specific surface area.
A titre d'exemple, les
Par comparaison avec les matériaux obtenus par métallurgie des poudres dans les documents
Un exemple détaillé ci-dessous illustre le procédé selon l'invention.A detailed example below illustrates the process according to the invention.
Dans la première étape, les poudres ont été sélectionnées pour réaliser un matériau présentant un ensemble de propriétés :
- mise en forme facile du demi-produit par un procédé d'usinage par enlèvement de copeaux avec absence de bavure,
- stabilité dimensionnelle, pour éviter une déformation du matériau après l'opération d'usinage ;
- soudable, notamment par laser.
- easy shaping of the semi-finished product by a chip removal machining process with no burrs,
- dimensional stability, to avoid deformation of the material after the machining operation;
- weldable, especially by laser.
Pour répondre à ces critères, trois poudres métalliques reprises dans les tableaux 1 et 2 ci-dessous ont été sélectionnées à l'étape 1) du procédé. La fonction de chaque poudre est détaillée au tableau 1. Les compositions et pourcentages des différentes poudres sont détaillés au tableau 2.
** Poudre SF-BS6040 10µm de Nippon Atomized Metal Powders Corp.
*** Poudre SF-BR9010 10µm de Nippon Atomized Metal Powders Corp.
SF-BS6040 10μm Powder from Nippon Atomized Metal Powders Corp.
*** SF-BR9010 10μm Powder from Nippon Atomized Metal Powders Corp.
Dans la seconde étape, les poudres ont été mélangées dans un mélangeur du commerce de type Turbula T10B. La vitesse de mélange est une vitesse moyenne de l'ordre de 200 tours par minute pendant 24 heures.In the second step, the powders were mixed in a commercial Turbula T10B mixer. The mixing speed is an average speed of the order of 200 rpm for 24 hours.
Dans la troisième étape, la mise en forme a été réalisée à l'aide d'une presse à haute vitesse et à haute énergie du fabriquant Hydropulsor. La mise en forme a été exécutée en deux phases :In the third step, the shaping was carried out using a high speed and high energy press of the manufacturer Hydropulsor. The formatting was performed in two phases:
Le dosage des poudres dans l'empreinte se fait de manière volumétrique avec une hauteur de remplissage donnée. Dans l'exemple, cette hauteur de remplissage est de 6 mm pour arriver à une épaisseur compactée d'environ 2 mm. Ce paramètre - hauteur de remplissage - peut varier entre 2 mm et 50 mm en fonction de l'épaisseur finale désirée sur le solide compacté. La quantité de poudres ainsi dosée est compactée entre le poinçon du dessus et le poinçon du dessous, entourée d'une matrice pour former une rondelle d'un diamètre donné. Cette compaction est faite dans l'exemple avec 25 impacts. L'objectif de cette étape est d'obtenir un solide suffisamment dense pour la densification ultérieure à chaud. Cette compaction sert aussi à ce que le solide ainsi compacté soit suffisamment solide pour les opérations de manipulation lors de la densification à chaud. La densité relative obtenue à cette étape est supérieure à 90 %.The dosing of the powders in the impression is done volumetrically with a given filling height. In the example, this filling height is 6 mm to reach a compacted thickness of about 2 mm. This parameter - filling height - can vary between 2 mm and 50 mm depending on the desired final thickness on the compacted solid. The quantity of powders thus dosed is compacted between the punch above and the punch below, surrounded by a matrix to form a washer of a given diameter. This compaction is done in the example with 25 impacts. The goal of this step is to get a solid enough dense for subsequent densification at hot. This compaction also serves to ensure that the solid thus compacted is sufficiently solid for handling operations during hot densification. The relative density obtained at this stage is greater than 90%.
La rondelle compactée est portée à une température proche de 700°C dans un four préchauffé à cette température. La rondelle compactée est placée dans le four pendant au moins 5 minutes et, de préférence, 15 minutes. La rondelle ainsi chauffée est transportée et mise dans l'empreinte de diamètre légèrement plus grand que le diamètre de la rondelle. La durée du transport de la rondelle préchauffée du four à la presse, mise dans la matrice, est comprise entre 2 et 5 secondes. La rondelle préchauffée est ensuite densifiée à chaud entre le poinçon du dessus et le poinçon du dessous avec 25 impacts. En l'absence de moyens de chauffage, une diminution de la température est observée pendant la densification par impact. L'épaisseur finale dans l'exemple de la rondelle densifiée est d'environ 1.8 mm. La densité relative de la rondelle est supérieure à 98%. La microstructure est semblable à celle obtenue à la
Grâce à la compaction et densification à chaud comme décrit ci-dessus, le solide obtenu est un matériau multi-phasé comprenant des phases ayant des fonctions différentes. De plus, le solide ainsi obtenu présente une microstructure homogène dans tout son volume. De ce fait, il y a absence de gradient de contraintes internes à travers du solide. Ceci offre une stabilité géométrique à la pièce usinée.Thanks to compaction and hot densification as described above, the solid obtained is a multiphase material comprising phases having different functions. In addition, the solid thus obtained has a homogeneous microstructure throughout its volume. As a result, there is no internal stress gradient across the solid. This provides geometric stability to the machined part.
Chaque phase du solide obtenu et, en amont, chaque poudre, est choisie pour remplir une fonction bien précise. Une des phases peut être choisie pour améliorer la soudabilité, par exemple, par laser. Cette fonction est remplie par la phase composée principalement de nickel dans l'exemple. Une autre phase peut être choisie pour faciliter la densification à chaud sans frittage à proprement dit. Dans l'exemple, une des phases du solide est constituée essentiellement de bronze qui a l'intervalle de fusion le plus faible des trois constituants. La troisième phase qui est, toujours à titre d'exemple, la phase majoritaire, est composée de la poudre de laiton consolidée. Cette phase ainsi mélangée aux deux autres permet de garantir une meilleure aptitude à l'usinage par enlèvement de copeaux.Each phase of the solid obtained and, upstream, each powder, is chosen to fulfill a specific function. One of the phases may be chosen to improve the weldability, for example, by laser. This function is fulfilled by the phase consisting mainly of nickel in the example. Another phase may be chosen to facilitate hot densification without sintering itself. In the example, one of the phases of solid consists essentially of bronze which has the lowest melting range of the three constituents. The third phase which is, as an example, the majority phase, is composed of consolidated brass powder. This phase thus mixed with the other two makes it possible to guarantee better machining aptitude by chip removal.
En présence d'une seule poudre de départ, le procédé selon l'invention présente également des avantages. On observe ainsi que la morphologie des grains au sein du matériau est une image de la morphologie des particules de la poudre de départ. La taille de grain jouant un rôle important dans les propriétés mécaniques du matériau, il est particulièrement avantageux de pouvoir prédire les propriétés finales sur base du choix de la morphologie de la poudre de départ.In the presence of a single starting powder, the process according to the invention also has advantages. It is thus observed that the morphology of the grains within the material is an image of the morphology of the particles of the starting powder. As the grain size plays an important role in the mechanical properties of the material, it is particularly advantageous to be able to predict the final properties on the basis of the choice of the morphology of the starting powder.
Grâce au procédé selon l'invention, la morphologie de la ou des poudres de base est conservée tout en obtenant un produit à haute densité relative contrairement au procédé connu de frittage où la consolidation à des valeurs de densité relative supérieures ou égales à 95, voire 98% s'accompagne d'une modification drastique de la morphologie.Thanks to the process according to the invention, the morphology of the base powder or powders is maintained while obtaining a product with a high relative density, unlike the known sintering process where the consolidation at relative density values greater than or equal to 95, or even 98% is accompanied by a drastic change in morphology.
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EP16801424.9A EP3393701B1 (en) | 2015-12-21 | 2016-11-18 | Material obtained by compacting and densifying nickel, bronze and brass powders and method thereof |
US16/064,314 US10987732B2 (en) | 2015-12-21 | 2016-11-18 | Material obtained by compaction and densification of metallic powder(s) |
CN201680079730.2A CN108495730B (en) | 2015-12-21 | 2016-11-18 | Material obtained by compression and densification of metal powders |
JP2018532780A JP6793730B2 (en) | 2015-12-21 | 2016-11-18 | Material obtained by compressing metallic powder to increase the density |
PCT/EP2016/078201 WO2017108293A1 (en) | 2015-12-21 | 2016-11-18 | Material obtained by compacting and densifying metal powder(s) |
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CN104959609A (en) * | 2015-06-05 | 2015-10-07 | 东睦新材料集团股份有限公司 | Preparation method of copper-base powder metallurgy part |
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WO1990011855A1 (en) * | 1989-04-07 | 1990-10-18 | Aktiebolaget Electrolux | Manufacture of dimensionally precise pieces by sintering |
SE0004122D0 (en) * | 2000-11-09 | 2000-11-09 | Hoeganaes Ab | High density compacts and method for the preparation thereof |
JP2008038160A (en) * | 2006-08-01 | 2008-02-21 | Kobe Steel Ltd | Method for producing high density powder molded body |
US9243475B2 (en) * | 2009-12-08 | 2016-01-26 | Baker Hughes Incorporated | Extruded powder metal compact |
JP4906972B1 (en) * | 2011-04-27 | 2012-03-28 | 太陽誘電株式会社 | Magnetic material and coil component using the same |
KR101501067B1 (en) * | 2013-06-07 | 2015-03-17 | 한국생산기술연구원 | Polycrystalline alloy having glass forming ability, method of fabricating the same, alloy target for sputtering and method of fabricating the same |
JP6519100B2 (en) * | 2014-04-23 | 2019-05-29 | セイコーエプソン株式会社 | Sinter-forming method, liquid binder, and sinter-formed product |
US10639719B2 (en) * | 2016-09-28 | 2020-05-05 | General Electric Company | Grain boundary engineering for additive manufacturing |
CN111032896B (en) * | 2017-08-28 | 2021-08-20 | 日本制铁株式会社 | Timepiece component |
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2015
- 2015-12-21 EP EP15201640.8A patent/EP3184211A1/en not_active Withdrawn
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2016
- 2016-11-18 EP EP16801424.9A patent/EP3393701B1/en active Active
- 2016-11-18 JP JP2018532780A patent/JP6793730B2/en active Active
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US20040231459A1 (en) | 2003-05-20 | 2004-11-25 | Chun Changmin | Advanced erosion resistant carbide cermets with superior high temperature corrosion resistance |
WO2010080064A1 (en) * | 2009-01-12 | 2010-07-15 | Metec Powder Metal Ab | Multilevel parts from agglomerated spherical metal powder |
WO2014199090A2 (en) | 2013-06-12 | 2014-12-18 | Centre Technique Des Industries Mecaniques | Method and unit for producing a mechanical part by sintering a powder metal material |
CN104959609A (en) * | 2015-06-05 | 2015-10-07 | 东睦新材料集团股份有限公司 | Preparation method of copper-base powder metallurgy part |
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US20190009331A1 (en) | 2019-01-10 |
CN108495730A (en) | 2018-09-04 |
WO2017108293A1 (en) | 2017-06-29 |
US11759857B2 (en) | 2023-09-19 |
JP6793730B2 (en) | 2020-12-02 |
US20210187608A1 (en) | 2021-06-24 |
CN108495730B (en) | 2021-06-15 |
EP3393701B1 (en) | 2022-05-11 |
JP2019508576A (en) | 2019-03-28 |
US10987732B2 (en) | 2021-04-27 |
EP3393701A1 (en) | 2018-10-31 |
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