EP0433856B1 - Matériaux mixtes à base de métaux durs comprenant des borures, nitrures et une matrice en métal ferreux - Google Patents
Matériaux mixtes à base de métaux durs comprenant des borures, nitrures et une matrice en métal ferreux Download PDFInfo
- Publication number
- EP0433856B1 EP0433856B1 EP90123854A EP90123854A EP0433856B1 EP 0433856 B1 EP0433856 B1 EP 0433856B1 EP 90123854 A EP90123854 A EP 90123854A EP 90123854 A EP90123854 A EP 90123854A EP 0433856 B1 EP0433856 B1 EP 0433856B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- titanium
- volume
- iron
- zirconium
- mixed
- 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.)
- Expired - Lifetime
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0292—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with more than 5% preformed carbides, nitrides or borides
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/14—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on borides
Definitions
- Hard metals which are understood to mean sintered materials made of metallic hard materials based on high-melting carbides of the metals from groups 4b to 6b of the periodic table and low-melting binder metals from the iron group, in particular cobalt, have long been known. They are mainly used for machining technology and to combat wear. For the production of these hard metals from the usually powdery hard materials, the metal binders are required, which must wet the hard material during the sintering process with the formation of an alloy (solution). This is the only way to create the tough, hard microstructure of the hard metals suitable for use, among which the WC-Co and TiC-WC-Co systems are best known.
- binders from the iron group are also suitable for other high-melting metallic hard materials, such as borides and nitrides (cf. "Ullmanns Enzyklopadie der techn. Chemie", vol. 12, 4th edition 1976, chapter “hard metals” , Pp. 515-521).
- Alloys based on nitrides and carbonitrides of titanium and zirconium with a very high proportion of the binder, in particular iron, (at least 50% and more) are particularly tough, but no longer very hard (HV 1050-1175) (cf. US-A -4,145,213 by Oskarsson et al.). Such materials are believed to be less brittle than the boride-based systems mentioned above. However, due to their low hardness, they are not suitable for processing hard and high-temperature materials such as SiC-reinforced aluminum alloys.
- Density at least 97% TD based on the theoretically possible density of the entire mixed material, Grain size of the hard material phase maximum 5.5 ⁇ m, Hardness (HV 30) at least 1200, Flexural strength (measured according to the 4-point method at room temperature) at least 1,000 MPa and Breaking resistance K IC at least 8.0 MPa m 1/2 .
- Tungsten carbide mixed materials in which the hard material components consist of titanium boride and titanium nitride, together, preferably 50-97% by volume, have proven particularly useful Make up 50 - 90 vol .-%, and in particular about 80 vol .-%, of the entire mixed material. 2.5-40% by volume of the hard material components preferably consist of titanium nitride. The missing proportion of up to 100% by volume in the entire mixed material is distributed among the oxides that may be present, preferably titanium oxide, with a proportion between 0 to 10% by volume and the metallic binding phase from the low-carbon iron or Iron alloy. Alloy components for low-carbon iron types are preferably chromium or chromium-nickel mixtures.
- the hard metal mixing materials according to the invention can be produced by processes known per se, for example by pressure-free sintering of fine starting powder mixtures or by infiltration of porous moldings from the hard material components with the low-carbon binder.
- borides and nitrides selected as hard material components should be as free as possible from carbon-containing impurities, which have a disadvantageous effect on the formation of the microstructure in the finished sintered body.
- titanium diboride which may contain boron carbide in its manufacture, can react not only with graphite, as already mentioned above, but also with boron carbide in the presence of iron to form the undesired Fe2B phase during the sintering process, as the following equations illustrate: TiB2 + 4Fe + C ---> TiC + 2Fe2B (1) TiB2 + 12Fe + B4C ---> TiC + 6Fe2B (2)
- Oxygen which is predominantly in the form of adhering oxides of titanium and zirconium, which includes, for example, TiO2, Ti2O3 and / or TiO and the corresponding oxides of zirconium, does not interfere, however, and can contain up to about 2% by weight in the Starting powders are tolerated.
- the separate addition of such oxides, in particular titanium oxide does not interfere with the sintering process and that, for example, up to 10% by volume of titanium oxide is present in the finished mixed material, the properties of which remain practically unchanged.
- the oxygen can also be present, in whole or in part, in the form of so-called oxynitrides of titanium and zircon.
- iron types with a C content of less than 0.1, preferably less than 0.05% by weight are advantageously used.
- Carbonyl iron powders with an Fe content of 99.95 to 99.98% by weight have proven particularly useful.
- These low-carbon types of iron can contain, for example, chromium in amounts of approximately 12% by weight or nickel-chromium mixtures of, for example, 8% by weight of nickel and 18% by weight of chromium as alloy components.
- grinding units can be used for this purpose, such as ball mills, planetary ball mills and attritors, in which grinding media and grinding vessels are made of material of their own, which in the present case means, for example, titanium diboride and low-carbon iron types.
- the powder mixtures obtained after the mixed grinding are optionally mixed with temporary binders or pressing aids and made free-flowing by spray drying. They are then pressed by conventional measures, such as cold isostatic pressing or die pressing, to form green bodies of the desired shape with a density of at least 60% TD.
- An annealing treatment at about 400 ° C removes binders or pressing aids without residue.
- the green bodies are then heated in the absence of oxygen to temperatures in the range from 1350 ° C. to 1900 ° C., preferably from 1550 ° C. to 1800 ° C., and 10 to 150 minutes, preferably 15, until a liquid iron-rich phase is formed at this temperature to 45 Minutes, held and then slowly cooled to room temperature.
- This sintering process is advantageously carried out in furnace units which are equipped with metallic heating elements, for example made of tungsten, tantalum or molybdenum, in order to avoid unwanted carburization of the sintered bodies.
- the sintered bodies expediently before cooling to room temperature, by applying pressure by means of a gaseous pressure transmission medium such as argon, at temperatures from 1200 ° C to 1400 ° C under a pressure of 150 to 250 MPa, preferably about 200 MPa, 10 continue to heat up to 15 minutes.
- a gaseous pressure transmission medium such as argon
- the hard material components for example titanium boride, titanium nitride and optionally titanium oxide
- these powder mixtures can be molded into green bodies with a density of 50 to 60% TD.
- These porous green bodies are then surrounded in a refractory crucible, for example made of boron nitride or aluminum oxide, with a powder bed of the desired binding metal, which only partially covers the surface of the porous body.
- the crucibles are then heated in furnace assemblies with metallic heating elements (W, Ta, Mo) in a vacuum free of carbon impurities to temperatures above the melting point of the metallic binding phase, whereby the liquid binding metal penetrates into the porous green body by infiltration until its pores are practically completely closed are.
- metallic heating elements W, Ta, Mo
- non-porous mixing materials which also have a density of almost 100% TD.
- the time required for this is essentially determined by the time required for the binder metal to melt.
- the process is generally completed in a period of 30 seconds to 30 minutes depending on the size of the workpiece.
- the hard metal mixed materials according to the invention thus produced are not only very dense, but also very hard, tough and strong.
- the desired combination of toughness and hardness can be varied over a wide range via the mixing ratio of hard materials, since titanium nitride, for example, is somewhat tougher than titanium diboride with a somewhat lower hardness.
- titanium nitride for example, is somewhat tougher than titanium diboride with a somewhat lower hardness.
- even small amounts of titanium nitride can considerably reduce the crater wear that usually occurs with indexable inserts, although such an influence was not to be expected from a hard material component softer than titanium diboride.
- the mixed materials according to the invention are also suitable as cutting tools for machining very hard materials, for example with SiC-reinforced aluminum alloys and nickel-based superalloys, as well as for impact-free machining such as core drilling or sawing of building materials containing silicon dioxide, for example concrete.
- Example 2 The same amounts of titanium diboride and titanium nitride as in Example 1 were mixed with 600 g of a powder made of stainless steel, which contained 18% by weight of nickel, 8% by weight of chromium and ⁇ 0.05% by weight of carbon and an average starting particle size of 20 ⁇ m had ground and processed under the same conditions as described in Example 1. The sintering was carried out at a temperature of 1650 ° C.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Ceramic Products (AREA)
- Powder Metallurgy (AREA)
- Carbon And Carbon Compounds (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Claims (6)
- Matériaux mixtes à base de métaux durs, à base de borures et de nitrures à haut point de fusion des métaux du groupe 4b du système périodique et de métaux à bas point de fusion constitués de fer et d'alliages à base de fer, caractérisés en ce que les matériaux mixtes sont constitués par(1) 40 à 97 % en volume de borures choisis dans le groupe constitué par le diborure de titane, le diborure de zirconium et les cristaux mixtes de ces diborures,(2) 1 à 48 % en volume de nitrures choisis dans le groupe constitué par le nitrure de titane et le nitrure de zirconium,(3) 0 à 10 % en volume d'oxydes choisis dans le groupe constitué par l'oxyde de titane et l'oxyde de zirconium, les constituants (2) et (3) pouvant aussi être présents entièrement ou partiellement sous forme d'oxynitrures choisis dans le groupe constitué par l'oxynitrure de titane et l'oxynitrure de zirconium, et(4) 2 à 59 % en volume de fer et d'alliages à base de fer pauvres en carboneet ont les propriétés suivantes:
une densité d'au moins 97 % de la densité théorique, par rapport à la densité possible en théorie du matériau mixte total,
une taille maximale des particules de la phase de substance dure de 5,5 µm,
une dureté (dureté Vickers 30) d'au moins 1200,
une résistance à la flexion (mesurée par la méthode en quatre points à la température ambiante) d'au moins 1,000 MPa et
une résistance à la rupture KIC d'au moins 8,0 MPa m1/2. - Matériaux mixtes selon la revendication 1, caractérisés en ce que les constituants de la substance dure (1) et (2) consistent en diborure de titane et en nitrure de titane qui représentent ensemble 50 à 97 % en volume du matériau mixte total, et en ce que le constituant de la substance dure (3) consiste en oxyde de titane en une proportion de 0,1 à 10 % en volume.
- Matériaux mixtes selon la revendication 1 et 2, caractérisés en ce que le constituant de métal liant (4) consiste en un alliage à base de fer pauvre en carbone qui contient comme composants de l'alliage du chome ou des mélanges de chrome-nickel.
- Procédé de préparation des matériaux mixtes selon la revendication 1, caractérisé en ce que l'on soumet des poudres de départ très pures des constituants de la substance dure (1), (2) et éventuellement (3) et le métal liant (4) à un broyage autogène et on comprime à froid les mélanges fins de poudres de départ ainsi obtenus en les façonnant en corps crus, puis on les soumet à un frittage sans pression dans une atmosphère exempte de carbone et à l'abri de l'oxygène, à des températures comprises entre 1350°C et 1900°C.
- Procédé selon la revendication 4, caractérisé en ce que l'on soumet les matériaux mixtes frittés sans pression à un recompactage isostatique à chaud en appliquant une pression à l'aide d'un milieu échangeur de pression gazeux à des températures de 1200°C à 1400°C sous une pression de 150 à 250 MPa.
- Procédé de préparation des matériaux mixtes selon la revendication 1, caractérisé en ce que l'on soumet des poudres de départ très pures des constituants de la substance dure (1), (2) et éventuellement (3) à un broyage autogène et on comprime à froid les mélanges fins de poudres de départ ainsi obtenus en les façonnant en corps crus, et on chauffe ces derniers en y versant une poudre composée du constituant métallique liant (4), dans une atmosphère exempte de carbone, à une température supérieure au point de fusion de la phase liante, jusqu'à ce que le métal liant fondu pénètre par infiltration dans les corps crus poreux et en bouche entièrement les pores.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT90123854T ATE102263T1 (de) | 1989-12-15 | 1990-12-11 | Hartmetall-mischwerkstoffe auf basis von boriden, nitriden und eisenbindemetallen. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3941536A DE3941536A1 (de) | 1989-12-15 | 1989-12-15 | Hartmetall-mischwerkstoffe auf basis von boriden, nitriden und eisenbindemetallen |
DE3941536 | 1989-12-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0433856A1 EP0433856A1 (fr) | 1991-06-26 |
EP0433856B1 true EP0433856B1 (fr) | 1994-03-02 |
Family
ID=6395567
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90123854A Expired - Lifetime EP0433856B1 (fr) | 1989-12-15 | 1990-12-11 | Matériaux mixtes à base de métaux durs comprenant des borures, nitrures et une matrice en métal ferreux |
Country Status (8)
Country | Link |
---|---|
US (1) | US5045512A (fr) |
EP (1) | EP0433856B1 (fr) |
JP (1) | JPH08944B2 (fr) |
AT (1) | ATE102263T1 (fr) |
AU (1) | AU633665B2 (fr) |
CA (1) | CA2031640A1 (fr) |
DE (2) | DE3941536A1 (fr) |
ES (1) | ES2050923T3 (fr) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR920019961A (ko) * | 1991-04-26 | 1992-11-20 | 기시다 도시오 | 고영율재료 및 이것을 이용한 표면피복공구 부재 |
FR2678286B1 (fr) * | 1991-06-28 | 1994-06-17 | Sandvik Hard Materials Sa | Cermets a base de borures des metaux de transition, leur fabrication et leurs applications. |
GB9127416D0 (en) * | 1991-12-27 | 1992-02-19 | Atomic Energy Authority Uk | A nitrogen-strengthened alloy |
US5401292A (en) * | 1992-08-03 | 1995-03-28 | Isp Investments Inc. | Carbonyl iron power premix composition |
DE4237423A1 (de) * | 1992-11-05 | 1994-05-11 | Kempten Elektroschmelz Gmbh | Verbundwerkstoffe auf der Basis von Titandiborid und Verfahren zu ihrer Herstellung |
US5427987A (en) * | 1993-05-10 | 1995-06-27 | Kennametal Inc. | Group IVB boride based cutting tools for machining group IVB based materials |
US5409868A (en) * | 1993-12-23 | 1995-04-25 | Electrofuel Manufacturing Co. | Ceramic articles made of compositions containing borides and nitrides |
DE69434357T2 (de) * | 1993-12-27 | 2006-03-09 | Kabushiki Kaisha Toyota Chuo Kenkyusho | Legierung auf Stahlbasis mit hohem Modul und Verfahren zu deren Herstellung |
JPH07300656A (ja) * | 1994-04-30 | 1995-11-14 | Daido Metal Co Ltd | 高温用焼結軸受合金及びその製造方法 |
US5637816A (en) * | 1995-08-22 | 1997-06-10 | Lockheed Martin Energy Systems, Inc. | Metal matrix composite of an iron aluminide and ceramic particles and method thereof |
JP3381487B2 (ja) * | 1995-11-06 | 2003-02-24 | 株式会社日立製作所 | 原子力プラント制御棒駆動装置用ローラ及びそれを用いた制御棒駆動装置 |
US6103651A (en) * | 1996-02-07 | 2000-08-15 | North American Refractories Company | High density ceramic metal composite exhibiting improved mechanical properties |
US5679611A (en) * | 1996-10-09 | 1997-10-21 | Eastman Kodak Company | Ceramic article containing a core comprising tetragonal zirconia and a shell comprising zirconium nitride |
US5688731A (en) * | 1996-11-13 | 1997-11-18 | Eastman Kodak Company | Ceramic articles containing doped zirconia having high electrical conductivity |
US5696040A (en) * | 1996-12-20 | 1997-12-09 | Eastiman Kodak Company | Ceramic article containing a core comprising zirconia and a shell comprising zirconium boride |
US5702766A (en) * | 1996-12-20 | 1997-12-30 | Eastman Kodak Company | Process of forming a ceramic article containing a core comprising zirconia and a shell comprising zirconium boride |
US7175686B2 (en) * | 2003-05-20 | 2007-02-13 | Exxonmobil Research And Engineering Company | Erosion-corrosion resistant nitride cermets |
US7544228B2 (en) * | 2003-05-20 | 2009-06-09 | Exxonmobil Research And Engineering Company | Large particle size and bimodal advanced erosion resistant oxide cermets |
US7175687B2 (en) * | 2003-05-20 | 2007-02-13 | Exxonmobil Research And Engineering Company | Advanced erosion-corrosion resistant boride cermets |
US7153338B2 (en) * | 2003-05-20 | 2006-12-26 | Exxonmobil Research And Engineering Company | Advanced erosion resistant oxide cermets |
US7731776B2 (en) * | 2005-12-02 | 2010-06-08 | Exxonmobil Research And Engineering Company | Bimodal and multimodal dense boride cermets with superior erosion performance |
US8323790B2 (en) * | 2007-11-20 | 2012-12-04 | Exxonmobil Research And Engineering Company | Bimodal and multimodal dense boride cermets with low melting point binder |
DE102008014355A1 (de) * | 2008-03-14 | 2009-09-17 | Esk Ceramics Gmbh & Co. Kg | Verbundwerkstoff auf Basis von Übergangsmetalldiboriden, Verfahren zu dessen Herstellung und dessen Verwendung |
US11174538B2 (en) * | 2017-02-06 | 2021-11-16 | The Regents Of The University Of California | Tungsten tetraboride composite matrix and uses thereof |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE659917C (de) * | 1931-10-24 | 1938-05-13 | Fried Krupp Akt Ges | Gesinterte Hartmetallegierungen |
JPS568886B2 (fr) * | 1974-09-09 | 1981-02-26 | ||
GB2038879A (en) * | 1979-01-03 | 1980-07-30 | Kennametal Inc | Sintered Cemented Titanium Diboride Niobium Nitride |
JPS55128560A (en) * | 1979-03-27 | 1980-10-04 | Agency Of Ind Science & Technol | Boride based ultrahard heat resistant material |
US4419130A (en) * | 1979-09-12 | 1983-12-06 | United Technologies Corporation | Titanium-diboride dispersion strengthened iron materials |
JPS5837274B2 (ja) * | 1980-08-26 | 1983-08-15 | 工業技術院長 | 高強度複合焼結材料 |
JPS5837274A (ja) * | 1981-08-31 | 1983-03-04 | 日産自動車株式会社 | キイシリンダの保持構造 |
WO1984004713A1 (fr) * | 1983-05-27 | 1984-12-06 | Ford Werke Ag | Procede de fabrication et d'utilisation d'un corps comportant du diborure de titane |
US4636481A (en) * | 1984-07-10 | 1987-01-13 | Asahi Glass Company Ltd. | ZrB2 composite sintered material |
JPS6150909A (ja) * | 1984-08-20 | 1986-03-13 | Ichimaru Fuarukosu Kk | 植物生薬の水溶性抽出エキス含有美白化粧料 |
JPS61130437A (ja) * | 1984-11-28 | 1986-06-18 | Kawasaki Steel Corp | 金属蒸着用容器の製造方法 |
JPS627673A (ja) * | 1985-06-19 | 1987-01-14 | 旭硝子株式会社 | ZrB↓2系焼結体 |
US4889836A (en) * | 1988-02-22 | 1989-12-26 | Gte Laboratories Incorporated | Titanium diboride-based composite articles with improved fracture toughness |
US4929417A (en) * | 1989-04-21 | 1990-05-29 | Agency Of Industrial Science And Technology | Method of manufacture metal diboride ceramics |
-
1989
- 1989-12-15 DE DE3941536A patent/DE3941536A1/de not_active Withdrawn
-
1990
- 1990-11-02 US US07/608,231 patent/US5045512A/en not_active Expired - Fee Related
- 1990-12-06 CA CA002031640A patent/CA2031640A1/fr not_active Abandoned
- 1990-12-11 DE DE90123854T patent/DE59004781D1/de not_active Expired - Fee Related
- 1990-12-11 ES ES90123854T patent/ES2050923T3/es not_active Expired - Lifetime
- 1990-12-11 EP EP90123854A patent/EP0433856B1/fr not_active Expired - Lifetime
- 1990-12-11 AT AT90123854T patent/ATE102263T1/de not_active IP Right Cessation
- 1990-12-14 JP JP2419105A patent/JPH08944B2/ja not_active Expired - Lifetime
- 1990-12-14 AU AU68026/90A patent/AU633665B2/en not_active Ceased
Also Published As
Publication number | Publication date |
---|---|
EP0433856A1 (fr) | 1991-06-26 |
JPH06128680A (ja) | 1994-05-10 |
AU6802690A (en) | 1991-06-20 |
JPH08944B2 (ja) | 1996-01-10 |
DE59004781D1 (de) | 1994-04-07 |
DE3941536A1 (de) | 1991-06-20 |
US5045512A (en) | 1991-09-03 |
ES2050923T3 (es) | 1994-06-01 |
CA2031640A1 (fr) | 1991-06-16 |
AU633665B2 (en) | 1993-02-04 |
ATE102263T1 (de) | 1994-03-15 |
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