EP2113576A1 - Verfahren zur herstellung eines baumaterials aus magnesiumhaltiger legierung auf aluminiumbasis - Google Patents
Verfahren zur herstellung eines baumaterials aus magnesiumhaltiger legierung auf aluminiumbasis Download PDFInfo
- Publication number
- EP2113576A1 EP2113576A1 EP07793983A EP07793983A EP2113576A1 EP 2113576 A1 EP2113576 A1 EP 2113576A1 EP 07793983 A EP07793983 A EP 07793983A EP 07793983 A EP07793983 A EP 07793983A EP 2113576 A1 EP2113576 A1 EP 2113576A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- producing
- magnesium
- ingot
- rolling
- melt
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/14—Plants for continuous casting
- B22D11/144—Plants for continuous casting with a rotating mould
-
- 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
-
- 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
- C22C1/02—Making non-ferrous alloys by melting
-
- 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
-
- 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
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- 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
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
Definitions
- the invention relates to foundry and rolling engineering.
- Existing methods for producing structural materials for the automobile industry are generally based on the use of the traditional method for producing ingots from aluminum-based alloys containing magnesium, lithium, zinc, and so on, and for rolling the same.
- the principal requirements made to structural materials for the automobile industry are the need to maintain the ultimate stress thereof within 300 to 400 MPa, relative elongation of 30% to 40%, and density not exceeding 2.65 g/cu.cm., good weldability, and corrosion resistance.
- An aluminum-based alloy AMG5 (GOST Standard 478961) and a method for producing it are known in the prior art.
- the prior art alloy has the following chemical composition (in percent by weight): Magnesium - 4.8 to 5.5 Manganese - 0.3 to 0.6 Titanium - 0.1 to 0.2 Iron - 0.5 to 0.6 Silicon - 0.1 to 0.2 Aluminum - the balance.
- parabolic solidification fronts of a polycrystalline structure are the cause of the absence of a uniform crystallographic orientation, that is, plasticity is different across the ingot at the macro- and micro-level. In general, plasticity decreases by at least a half for this reason. Plasticity of an alloy is characterized by relative elongation of up to 4%-6%, a figure that obviously does not meet the requirements of the automobile industry.
- Processes for producing the AL8 and AL27 alloys related closely to the chemical composition of this invention are suitable for producing corrosion-resistant castings that can be subjected to heat treatment to improve their strength. These processes, however, can be used to cast ingots from the above alloys only. Besides, they cannot, in principle, be used to make plastic ingots from alloys containing about 10% of magnesium, for which reason they are classified as foundry processes.
- This invention is intended to develop a method for producing a structural material from an aluminum-based alloy containing 9% to 10% of magnesium, comprising casting an ingot, subjecting the ingot to heat treatment, and rolling the ingot, in order to improve the strength and plasticity of rolled products and the quality of the process for producing sheet material.
- This objective is achieved by developing a method for producing a structural material from an aluminum-based alloy containing 9% to 11 % of magnesium, said method comprising producing an ingot, subjecting it to heat treatment, and rolling the ingot containing magnesium, manganese, and titanium, wherein the mechanical properties of the alloy are improved by further adding zirconium, cobalt, beryllium, and boron thereto at the following proportions of the ingredients (in percent by weight): Magnesium - 9.0 to 11.0 Zirconium - 0.15 to 0.2 Cobalt - 0.01 to 0.001 Beryllium - 0.001 to 0.02 Aluminum - the balance.
- Solidification is carried out in a revolving mold at a gravitation factor of 220 to 250 during a lifetime of the melt equal to between 12 and 15 sec/kg.
- Heat treatment and rolling are conducted according to the following algorithm:
- the claimed method is based on the use of new physical phenomena attending solidification of melts in strong gravitation fields of centrifuges. Generally, the effect of such fields is as follows:
- the claimed method therefore, helps develop an aluminum-based structural material containing 9% to 11 % of magnesium, and make rolled products therefrom.
- the method of this invention for producing a structural material from an aluminum-based alloy containing 9% to 11 % of magnesium is performed at the ingot producing stage in a revolving mold, the design of which depends on the required ingot shape and weight. In this case, the thermal conditions of solidification depend on the specific design of the mold lining.
- the invention is based on an analytically computed and experimentally confirmed effect of gravity fields on the solidifying melt from the viewpoint of orientation of the crystallographic lattice axes.
- a retarded crystallite is a fully grown nucleus distorted from the spherical shape to nearly an ellipsoid attached to the cellular solidification front.
- Direction of the absolute elastic energy minimum of the lattice is a maximum suitable situation for successive deformation of the solid at minimum external forces applied, for example, by the rolling mill. This is particularly important in this case, with a supersaturated solution of magnesium in aluminum, because this alloy has an improved strength.
- Table 1 Test parameters Rolled product thickness, mm Magnesium concentration, % 2.0 1.0 0.5 0.1 Ultimate strength, MPa 320-380 320-380 325-380 330-390 9 330-400 330-400 330-410 330-420 10 330-390 330-390 320-390 325-380 11 Relative elongation, % 30-40 32-40 32-40 9 32-40 32-40 32-40 33-40 10 31-38 30-37 30-36 30-36 11
- This invention is suitable for application on an industrial scale because it may be performed in a revolving mold known in the art, and the result is achieved by varying alloy production conditions.
- This invention may be used for producing structural materials of practically any thickness from the AMG10 alloy.
- the invention may be used most efficiently for producing rolled materials for motor vehicle bodies and power components of motor vehicles.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metal Rolling (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/RU2007/000026 WO2008091174A1 (fr) | 2007-01-24 | 2007-01-24 | Procédé de fabrication d'un matériau de construction à partir d'un alliage à base d'aluminium contenant du magnésium |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2113576A1 true EP2113576A1 (de) | 2009-11-04 |
EP2113576A4 EP2113576A4 (de) | 2017-11-29 |
EP2113576B1 EP2113576B1 (de) | 2018-11-28 |
Family
ID=39644690
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07793983.3A Active EP2113576B1 (de) | 2007-01-24 | 2007-01-24 | Verfahren zur herstellung eines baumaterials aus magnesiumhaltiger legierung auf aluminiumbasis |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2113576B1 (de) |
CN (1) | CN101583730B (de) |
WO (1) | WO2008091174A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11149332B2 (en) | 2017-04-15 | 2021-10-19 | The Boeing Company | Aluminum alloy with additions of magnesium and at least one of chromium, manganese and zirconium, and method of manufacturing the same |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20200325559A1 (en) * | 2017-12-28 | 2020-10-15 | Fehrmann Alloys GmbH & Co. KG | Use of alloy containing aluminum for additive manufacturing |
CN109112447A (zh) * | 2018-08-17 | 2019-01-01 | 清华大学 | 一种铝-镁系合金环的制备工艺 |
CN109226431B (zh) * | 2018-08-17 | 2019-12-27 | 清华大学 | 一种超高强韧性铝-镁系合金及其管材的旋压方法 |
CN109014086B (zh) * | 2018-08-17 | 2020-05-19 | 清华大学 | 一种高镁铝合金的铸造方法 |
CN109097710B (zh) * | 2018-08-17 | 2020-05-19 | 清华大学 | 一种高镁铝合金管材的挤压方法 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU439535A1 (ru) * | 1972-07-04 | 1974-08-15 | Предприятие П/Я Р-6209 | Сплав на основе алюмини |
JPS5822363A (ja) * | 1981-07-30 | 1983-02-09 | Mitsubishi Keikinzoku Kogyo Kk | 超塑性アルミニウム合金板の製造方法 |
JPH05345963A (ja) * | 1992-06-12 | 1993-12-27 | Furukawa Alum Co Ltd | 高成形性アルミニウム合金板の製造方法 |
WO1994002270A1 (en) * | 1992-07-28 | 1994-02-03 | Anatoly Vladimirovich Popov | Method of making castings by oriented melt crystallization |
CA2109004A1 (en) * | 1992-10-23 | 1994-04-24 | Ryo Shoji | Process for manufacturing a1-mg alloy sheets for press forming |
JPH06136497A (ja) * | 1992-10-23 | 1994-05-17 | Furukawa Alum Co Ltd | 高成形性アルミニウム合金板の製造方法 |
JPH06136496A (ja) * | 1992-10-23 | 1994-05-17 | Furukawa Alum Co Ltd | 高成形性アルミニウム合金板の製造方法 |
RU2111826C1 (ru) * | 1996-07-24 | 1998-05-27 | Виктор Макарьевич Живодеров | Способ литья алюминиевых сплавов, алюминиевый сплав и способ производства из него промежуточных изделий |
EP1842935B1 (de) * | 2005-01-19 | 2014-10-29 | Kabushiki Kaisha Kobe Seiko Sho | Platte aus einer aluminiumlegierung und herstellungsverfahren dafür |
CN1865475A (zh) * | 2006-06-12 | 2006-11-22 | 陈继忠 | 镁铝合金及其制备方法 |
-
2007
- 2007-01-24 CN CN200780050147XA patent/CN101583730B/zh not_active Expired - Fee Related
- 2007-01-24 WO PCT/RU2007/000026 patent/WO2008091174A1/ru active Application Filing
- 2007-01-24 EP EP07793983.3A patent/EP2113576B1/de active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2008091174A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11149332B2 (en) | 2017-04-15 | 2021-10-19 | The Boeing Company | Aluminum alloy with additions of magnesium and at least one of chromium, manganese and zirconium, and method of manufacturing the same |
Also Published As
Publication number | Publication date |
---|---|
EP2113576B1 (de) | 2018-11-28 |
EP2113576A4 (de) | 2017-11-29 |
CN101583730A (zh) | 2009-11-18 |
CN101583730B (zh) | 2011-12-07 |
WO2008091174A1 (fr) | 2008-07-31 |
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