WO2006094325A1 - Procede de fabrication de materiaux composites metalliques - Google Patents
Procede de fabrication de materiaux composites metalliques Download PDFInfo
- Publication number
- WO2006094325A1 WO2006094325A1 PCT/AT2006/000097 AT2006000097W WO2006094325A1 WO 2006094325 A1 WO2006094325 A1 WO 2006094325A1 AT 2006000097 W AT2006000097 W AT 2006000097W WO 2006094325 A1 WO2006094325 A1 WO 2006094325A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- starting material
- deformation
- metallic
- ductility
- composite
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/001—Extruding metal; Impact extrusion to improve the material properties, e.g. lateral extrusion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/01—Extruding metal; Impact extrusion starting from material of particular form or shape, e.g. mechanically pre-treated
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/02—Preliminary treatment of metal stock without particular shaping, e.g. salvaging segregated zones, forging or pressing in the rough
- B21J1/025—Preliminary treatment of metal stock without particular shaping, e.g. salvaging segregated zones, forging or pressing in the rough affecting grain orientation
Definitions
- the invention relates to a method for producing massive metallic composite materials with a particle size in the nm range (nanocomposites).
- Submicron or nanocrystalline materials in particular of metals, alloys or intermetallic compounds, are ideally suited for a wide range of applications and have a wide variety of mechanical and electromagnetic properties. In part, these properties change abruptly with changes in the fine structure, in particular with the grain size of individual components of metallic composite materials.
- nanocomposites which, for example, can be produced by powder metallurgy. For example, tungsten powder with a 20% or 30% copper content can be produced by mechanical alloying and then cold pressed into shape.
- the grain size of the W-Cu powder in the starting material is 20 nm to 30 nm.
- amorphous metal alloys can be prepared by very rapid solidification.
- nanocomposites can also be produced by different coating methods, but this is also limited to the production of very thin films.
- the starting elements are mixed as powders with particle sizes of 2 ⁇ m to 250 ⁇ m and subjected to high mechanical forces to achieve a secondary powder with a nanocrystalline structure.
- the secondary powder is obtained by mixing and cold working the starting powders or by mixing and high energy milling of the starting powders.
- a disadvantage of such methods is the dust load due to the harmful nanopowder, as well as the considerable effort required to minimize the release of nanoparticles of different, partially toxic metal powders.
- WO 03/026815 A1 discloses an apparatus and a method for producing finely crystalline materials, in which a starting material is mechanically processed by cyclic deformation until a previously defined fine structure of the material sample is achieved. The individual deformation steps are carried out at temperatures between the ambient temperature and the half-melting temperature of the respective material. By multiple plastic deformation, for example, the strength of recrystallized pure metals can be increased many times without having to accept significant losses in the elongation at break in purchasing. As starting materials, however, only single-phase materials, such as pure metals and, for example, intermetallic Ni 3 Al materials, called.
- the object of the invention is to propose a method for producing massive metallic composite materials with a particle size in the nm range, which is suitable for as many combinations of different starting materials and which is further technically easy to apply.
- the inventive method is based on a solid, coarse composite material as starting material, which is at least two-phase and thus consists of at least two non-detachable components.
- the end product of the process is also present in solid form as a so-called nanocomposite, ie at least one or each of the two components is present in the composite material as nanoparticles with a particle size and a particle distance of a few nanometers.
- nanocomposite ie at least one or each of the two components is present in the composite material as nanoparticles with a particle size and a particle distance of a few nanometers.
- known nanocrystalline, single-phase materials have crystallites with a particle size of a few nanometers, they are confined to similar particles so that no nanocomposites are present.
- the comparative strain according to MISES can be used.
- the comparative strain or deformation ⁇ is, for example, in the case of high-pressure torsional deformation
- n is the number of revolutions r is the radius (at which the deformation is measured) and t is the sample thickness. If specified in percent, the ⁇ value must be multiplied by 100. A comparative strain of, for example, 100 thus corresponds to 10,000%.
- HPT High Pressure Torsion
- ECA Equal Channel Angular Extrusion
- CCDC Cyclic Channel Compression
- ARB Accumulative Roll Bonding
- the material sample to be deformed is in a cylindrical recess of a pressure-resistant mold and is pressurized with a pressure piston with a cylindrical cross-section.
- a rotational movement of the mold or the plunger about the common axis there is a high-pressure torsional deformation of the sample, which reaches the desired degree of deformation in certain radial regions.
- an angled channel is provided in a pressure-resistant form, through which the material sample is pressed through with the aid of a punch. After removal of the material sample from the angled channel this is again introduced into the channel and the process continues until the desired fine structure is achieved.
- the starting material is deformed by frequent folding and rolling.
- the component with the higher ductility can form a matrix in which the component with the lower ductility is embedded. If the two metals in a metal-metal composite have different strength properties and different ductility, it is possible to severely break up the brittle and solid phase at a high deformation rate. For example, in the W-Cu tungsten system, the much firmer and much more brittle partner at room temperature is copper, the softer and more ductile partner.
- the yield stress or the ductility of one of the two metallic documents should be at least twice as large as that of the second metallic component.
- biphasic Pb / Fe, Cu / Fe, Ag / Fe or Cu / Cr composite material is used as starting material.
- the at least two individual components can also be alloys that are not soluble in each other.
- the deformation according to point b) can be carried out at temperatures between room temperature (20 0 C) and 200 0 C, but also at low temperatures, for example at liquid nitrogen temperature.
- the invention will be explained in more detail below with reference to drawings. Show it:
- Fig. 1 is a micrograph of the starting material in an enlarged view, as well
- FIGS 2, 3, 4, 5 and 6 micrographs of nanocomposites produced by the method according to the invention in different process stages and particle sizes.
- the starting material used is a coarse-grained W-25% Cu composite, which according to FIG. 1 shows an inhomogeneous distribution of the W particles which have a size of between 2 ⁇ m and 10 ⁇ m.
- the proportion of W grains in the Cu matrix is relatively large, so that in the subsequent high-pressure torsional deformation, the individual W particles do not "float" in the matrix but are pressed or rubbed against each other so that the particles break up and larger ones Deformation values massive particle size reduction is observable.
- HPT high-pressure torsion deformation
- the starting material is used in the form of a disk-shaped sample with a diameter of 5 mm to 10 mm and a thickness of 0.5 mm to 2 mm.
- the plate has a diameter of 8 mm and a thickness t of 0.8 mm, so that according to formula (1) with a radius r of 3 mm and the corresponding selection of revolutions n different deformation values ⁇ can be achieved.
- the deformation takes place in the example shown at room temperature, at a pressure between 5 GPa and 10 GPa, preferably at 8 GPa.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE112006000504T DE112006000504A5 (de) | 2005-03-08 | 2006-03-07 | Verfahren zur Herstellung metallischer Verbundwerkstoffe |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ATA398/2005 | 2005-03-08 | ||
AT3982005A AT501546B1 (de) | 2005-03-08 | 2005-03-08 | Verfahren zur herstellung metallischer verbundwerkstoffe |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2006094325A1 true WO2006094325A1 (fr) | 2006-09-14 |
Family
ID=36481416
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AT2006/000097 WO2006094325A1 (fr) | 2005-03-08 | 2006-03-07 | Procede de fabrication de materiaux composites metalliques |
Country Status (3)
Country | Link |
---|---|
AT (1) | AT501546B1 (fr) |
DE (1) | DE112006000504A5 (fr) |
WO (1) | WO2006094325A1 (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7617750B2 (en) * | 2006-12-06 | 2009-11-17 | Purdue Research Foundation | Process of producing nanocrystalline bodies |
CN103785844A (zh) * | 2014-01-13 | 2014-05-14 | 上海交通大学 | 一种纳米结构块体镁材料及制备方法 |
CN104511595A (zh) * | 2014-12-30 | 2015-04-15 | 中南大学 | 一种高纯钛粉的制备方法 |
CN109554638A (zh) * | 2019-01-10 | 2019-04-02 | 北京理工大学 | 一种高熵合金梯度纳米材料制备方法 |
CN112063940A (zh) * | 2020-09-23 | 2020-12-11 | 燕山大学 | 一种提高稀土镁合金强度的方法 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012109929A1 (de) * | 2012-10-18 | 2014-05-08 | Karlsruher Institut für Technologie | Verfahren zur Herstellung einer magnetischen Legierung und mit diesem Verfahren hergestellte magnetische Legierung |
CN112391563B (zh) * | 2019-08-19 | 2021-11-09 | 南京理工大学 | 一种层状纳米异构铝镁合金块体材料制备方法 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4710239A (en) * | 1984-09-14 | 1987-12-01 | General Motors Corporation | Hot pressed permanent magnet having high and low coercivity regions |
DE3714239C2 (de) * | 1987-04-29 | 1996-05-15 | Krupp Ag Hoesch Krupp | Verfahren zur Herstellung eines Werkstoffs mit einem Gefüge nanokristalliner Struktur |
AT411027B (de) * | 2001-09-25 | 2003-09-25 | Reinhard Dipl Ing Ddr Pippan | Vorrichtung und verfahren zur herstellung feinkristalliner werkstoffe |
-
2005
- 2005-03-08 AT AT3982005A patent/AT501546B1/de not_active IP Right Cessation
-
2006
- 2006-03-07 WO PCT/AT2006/000097 patent/WO2006094325A1/fr not_active Application Discontinuation
- 2006-03-07 DE DE112006000504T patent/DE112006000504A5/de not_active Withdrawn
Non-Patent Citations (2)
Title |
---|
MURAYAMA M ET AL: "Dissolution of the [theta]' precipitates in an Al-1.7 at.% Cu alloy deformed by equal-channel angular pressing", ULTRAFINE GRAINED MATERIALS. PROCEEDINGS OF A SYMPOSIUM TMS - MINER. METALS & MATER. SOC WARRENDALE, PA, USA, 2000, pages 145 - 153, XP002384010, ISBN: 0-87339-472-0 * |
SAHA S ET AL: "Synthesis of Fe-Pd and Fe-Pd/Ta magnetic nanocomposites by severe plastic deformation", PRESENTATION; JOURNAL OF APPLIED PHYSICS AIP USA, vol. 97, no. 10, 8 November 2004 (2004-11-08), pages 10F301 - 1, XP002384011, ISSN: 0021-8979 * |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7617750B2 (en) * | 2006-12-06 | 2009-11-17 | Purdue Research Foundation | Process of producing nanocrystalline bodies |
CN103785844A (zh) * | 2014-01-13 | 2014-05-14 | 上海交通大学 | 一种纳米结构块体镁材料及制备方法 |
CN104511595A (zh) * | 2014-12-30 | 2015-04-15 | 中南大学 | 一种高纯钛粉的制备方法 |
CN109554638A (zh) * | 2019-01-10 | 2019-04-02 | 北京理工大学 | 一种高熵合金梯度纳米材料制备方法 |
CN112063940A (zh) * | 2020-09-23 | 2020-12-11 | 燕山大学 | 一种提高稀土镁合金强度的方法 |
Also Published As
Publication number | Publication date |
---|---|
AT501546A1 (de) | 2006-09-15 |
AT501546B1 (de) | 2007-02-15 |
DE112006000504A5 (de) | 2008-01-17 |
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