WO1999049089A1 - Magnesium alloying - Google Patents
Magnesium alloying Download PDFInfo
- Publication number
- WO1999049089A1 WO1999049089A1 PCT/AU1999/000189 AU9900189W WO9949089A1 WO 1999049089 A1 WO1999049089 A1 WO 1999049089A1 AU 9900189 W AU9900189 W AU 9900189W WO 9949089 A1 WO9949089 A1 WO 9949089A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- alloy
- master alloy
- alloying
- molten
- master
- 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.)
- Ceased
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
-
- 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
- C22C1/03—Making non-ferrous alloys by melting using master alloys
-
- 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
Definitions
- the present invention relates to a method for producing an alloy containing magnesium (Mg) and aluminium (Al) and to alloys produced by the method. It is to be understood that the alloy may contain constituents other than Mg and Al (for example, zinc
- the present invention also relates to a master alloy suitable for use in the method for producing Mg-Al alloy.
- Mn manganese
- Fe iron
- MnCl 2 manganese chloride
- MnCl 2 reacts with molten Mg to form magnesium chloride (MgCl 2 ) which precipitates and thereby effects loss of Mg and also results in the formation of gaseous hydrochloric acid (HC1) when MnCl 2 or MgCl 2 hydrolyse in the presence of atmospheric moisture.
- HC1 gaseous hydrochloric acid
- US patent no. 5248477 (issued 28 September 1993) teaches a process for producing Mg-Al alloy in which Mn is added to molten Mg or molten Mg alloy as molten elemental Mn or a molten mixture of elemental Mn and Al . The process is thus a liquid-liquid alloying technique.
- US patent no. 5248477 (issued 28 September 1993) teaches a process for producing Mg-Al alloy in which Mn is added to molten Mg or molten Mg alloy as molten elemental Mn or a molten mixture of elemental Mn and Al . The process is thus a liquid-liquid alloying technique.
- Mn can be added as elemental Mn or it can be added in the form of a commercially available mixture of metals in particulate or powder form, usually in the form of a briquette, comprising about 75% Mn and about 25% Al " (see - 2 - column 3 lines 10-14) but teaches that "the addition of the elemental Mn in solid form has little effect on the reduction of Fe content in the melt” (see column 3 lines 18-20) .
- US patent no. 5248477 goes on to teach that the "reason for the addition of the MnCl 2 as opposed to the addition of elemental Mn either in pure or mixed form is that the effectiveness for Fe precipitation is significantly greater and the Mn alloying efficiency itself is significantly greater as well.
- the present invention provides a method for producing an Mg-Al alloy in an alloying vessel containing molten Mg or molten Mg alloy, the method including the steps of establishing the temperature of the molten Mg or Mg alloy in the range of 650-750°C and thereafter adding a solid master alloy containing Al and Mn to the alloying vessel whereby Mn is released for reaction with Fe in the alloying vessel.
- the present invention provides Mg-Al alloy prepared by a method according to the first aspect of the present invention.
- the Al-Mn master alloy is added to molten Mg or molten Mg alloy at temperature in the range 650-750°C.
- the temperature is in the range 650-710°, more preferably 680-700°C.
- Some of the Al alloying component and possibly other alloying components can be added to the alloying vessel separately from the Al-Mn master alloy.
- all alloying components are - 3 - added to the alloying vessel by way of the Al-Mn master alloy.
- the Mg-Al alloy may be produced by adding the master alloy to molten primary Mg and, where that is the case, the primary Mg may have been produced by electrolysis of anhydrous MgCl in an electrolytic cell. Molten Mg typically leaves the electrolytic cell at a temperature of about 655°C.
- the Mg-Al alloy may be produced by adding the master alloy to molten Mg or Mg alloy derived from recycling of scrap material.
- the conventional process where MnCl 2 is used requires heating the Mg or Mg alloy to 730-750°C, adding Al and any other alloying components (for example, Zn) over a period of 5-10 minutes, stirring in MnCl 2 over a period of about 20 minutes, and cooling the contents of the alloying vessel to about 670°C over a period of about 20 minutes prior to transferring the resulting Mg-Al alloy to a settling furnace.
- Al and any other alloying components for example, Zn
- the batch time for producing Mg-Al alloy in accordance with the first aspect of the present invention can be reduced as compared with the conventional MnCl 2 process because the alloying vessel does not need to be heated to 730-750°C, the Al and Mn can be added in a single step, and less time is required for cooling.
- Reduction of batch time in accordance with the present invention is desirable in a Mg smelter because energy consumption is reduced and capital costs associated with requirement for a plurality of alloying vessels can be reduced. It is also to be noted that in contrast to the liquid-liquid alloying technique of US patent no. 5248477, the requirement for a separate vessel for melting the alloying components and the energy consumption associated therewith are avoided.
- the present invention is also believed to be advantageous in relation to the chemical composition of Fe-Mn intermetallic compound that is formed. Without wishing to be bound by theory, it is believed that Fe-Mn intermetallic compounds formed at higher temperatures - 4 - contain a greater proportion of Fe than those formed at lower temperatures and that corrosion problems are lessened in Mg-Al alloys in which the Fe-Mn intermetallic compounds formed during their production contain lesser proportions of Fe .
- the Al-Mn master alloy used in the process according to the first aspect of the present invention must be capable of releasing Mn for reaction with Fe when added to the Mg or Mg alloy at a temperature in the range of 650-750°C. Any Al-Mn master alloy that meets this requirement falls within the scope of the present invention but various properties of the master alloy are preferred.
- the Al-Mn master alloy may include other alloying components, for example, Zn .
- the master alloy contains a minority of Mn, for example, less than 10 percent by weight Mn. This is to be contrasted with the Mn-Al briquette referred to in US patent no. 5248477 which contained about 75 percent Mn .
- the majority of the Mn in the Al-Mn master alloy is present in the form of an Al-Mn intermetallic compound (for example, AlgMn) with a minority of the Mn present as elemental Mn .
- the Al-Mn intermetallic compound is preferably in the form of fine needles or thin platelets.
- the balance of the Al in the master alloy is preferably ⁇ -Al .
- the solid master alloy is added to molten Mg or Mg alloy at temperature in the range of 650- 710°C which is cooler than in prior art techniques.
- preferred AlgMn containing solid master alloys are believed to enable lower Mg temperatures to be used because:
- AlgMn is much more soluble in Mg than elemental Mn
- AlgMn is surrounded by ⁇ -Al when formed with the result that the surface of AlgMn particles are not coated with an oxide - 5 - layer which would inhibit dissolution in Mg, and (3) AlgMn melts at about 705°C compared to elemental Mn which melts at 1246°C.
- the Al-Mn master alloy has a nickel (Ni) content less than 30ppm and a copper (Cu) content less than 50ppm.
- the master alloy is produced by cooling a molten master alloy precursor, for example, by quench casting.
- the Al-Mn master alloy may be of granular form.
- Granules of the Al-Mn master alloy may be produced using a water-cooled wheel in a manner analogous to that used for producing aluminium granules.
- the use of granular Al-Mn master alloy enables the master alloy to be added to the alloying vessel from an overhead hopper under gravity.
- the hopper is mounted on load cells or the like and has a gate enabling a predetermined mass of Al-Mn master alloy to be added to the alloying vessel.
- the hopper is heated to drive any moisture off granular Al-Mn master alloy which obviates any requirement for an alloying pre-heat furnace.
- the master alloy may be in the form of cast ingots in which case the master alloy is preferably added to the alloying vessel from an overhead conveyor.
- the conveyor is preferably arranged to be heated to drive moisture from the master alloy and the ingots are preferably of a consistent mass whereby the mass of master alloy added to the alloying vessel is controllable by addition of a predetermined number of the ingots.
- the present invention provides an Al-Mn master alloy containing less than 10% by weight Mn, wherein a majority of the Mn is in the form of an Al-Mn intermetallic compound and a minority of the Mn is elemental Mn.
- the master alloy is suitable for use as - 6 - the master alloy in the process according to the first aspect of the present invention.
- Example 1 Preparation of Solid Al-Mn Master Alloy Solid master alloy was prepared in two stages. In the first stage master alloy precursor was prepared by addition of a source of Mn to molten Al at 800°C to produce Al-Mn alloy containing 5.5% by weight Mn . Three sources of Mn were used, namely (a) Mn-Al splatter containing 60% by weight Mn, (b) Mn-Al Altabs containing 75% by weight Mn, and (c) Mn coarse injection powder. In all cases the master alloy precursor was prepared within 10 minutes of addition of the source of Mn by moderate stirring.
- Mg-Al alloys were prepared by addition of solid Al-Mn master alloys from Example 1 to molten primary Mg at 680°C and 700°C. Only 5-10 minutes was required to achieve the ASTM minimum Mn level of 0.26% in the AM60 alloy at both 680°C and 700°C. After two hours of settling and a reduction in temperature of the melt to 660 °C, the Fe level was reduced from approximately 300ppm to less than 40ppm and Mn recovery was greater than 80%. - 7 -
- Comparative Example 1 Preparation of Mg-Al Alloy Example 2 was repeated using Mn-Al splatter containing 60% by weight Mn in lieu of solid Al-Mn master alloys from Example 1. Mn from the Mn-Al splatter could not be readily released into the primary Mg at temperatures below 710°C. Even at 730°C with 20 minutes of stirring, a Mn level of only 0.20% was achieved at a Mn recovery of less than 50%. Comparative Example 2 - Preparation of Mq-Al Alloy
- Example 2 was repeated using Mn-Al Altabs containing 75% by weight Mn in lieu of solid Al-Mn master alloys from Example 1. Mn from the Mn-Al Altabs could not be readily released into the primary Mg at temperatures below 710°C. Stirring for 20 minutes at 730°C was required to achieve the ASTM minimum Mn level with a Mn recovery of less than 80%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
Description
Claims
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002324961A CA2324961A1 (en) | 1998-03-20 | 1999-03-22 | Magnesium alloying |
| AU29158/99A AU2915899A (en) | 1998-03-20 | 1999-03-22 | Magnesium alloying |
| EP99910034A EP1073774A4 (en) | 1998-03-20 | 1999-03-22 | PRODUCTION OF A MAGNESIUM ALLOY |
| MXPA00009225A MXPA00009225A (en) | 1998-03-20 | 1999-03-22 | Magnesium alloying. |
| IL13852699A IL138526A0 (en) | 1998-03-20 | 1999-03-22 | Magnesium alloying |
| IS5630A IS5630A (en) | 1998-03-20 | 2000-09-19 | Magnesium alloy. |
| NO20004676A NO20004676L (en) | 1998-03-20 | 2000-09-19 | magnesium Alloy |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AUPP2469A AUPP246998A0 (en) | 1998-03-20 | 1998-03-20 | Magnesium alloying |
| AUPP2469 | 1998-03-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO1999049089A1 true WO1999049089A1 (en) | 1999-09-30 |
Family
ID=3806731
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/AU1999/000189 Ceased WO1999049089A1 (en) | 1998-03-20 | 1999-03-22 | Magnesium alloying |
Country Status (9)
| Country | Link |
|---|---|
| EP (1) | EP1073774A4 (en) |
| AU (1) | AUPP246998A0 (en) |
| CA (1) | CA2324961A1 (en) |
| CZ (1) | CZ20003374A3 (en) |
| IL (1) | IL138526A0 (en) |
| IS (1) | IS5630A (en) |
| MX (1) | MXPA00009225A (en) |
| NO (1) | NO20004676L (en) |
| WO (1) | WO1999049089A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2003056050A1 (en) * | 2001-12-26 | 2003-07-10 | Jsc 'avisma Titanium-Magnesium Works' | Magnesium-based alloy and method for the production thereof |
| WO2003056049A1 (en) * | 2001-12-26 | 2003-07-10 | Jsc 'avisma Titanium-Magnesium Works' | Magnesium-based alloy and method for the production thereof |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116240411B (en) * | 2022-12-22 | 2025-04-11 | 安徽鑫铂铝业股份有限公司 | A method for developing high-precision corrosion-resistant medical aluminum alloy profiles |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR771023A (en) * | 1933-06-20 | 1934-09-28 | Manufacturing process of magnesium alloys and resulting alloys | |
| GB519304A (en) * | 1937-04-16 | 1940-03-21 | Georg Von Giesche S Erben | Improvements in magnesium alloys |
| GB533266A (en) * | 1939-04-27 | 1941-02-10 | Fritz Christen | Improvements in and relating to magnesium alloys |
| GB628289A (en) * | 1946-05-02 | 1949-08-25 | Bendix Aviat Corp | Improvements in or relating to the heat treatment of magnesium alloy castings |
| US5248477A (en) * | 1991-09-12 | 1993-09-28 | The Dow Chemical Company | Methods for producing high purity magnesium alloys |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4179287A (en) * | 1978-12-19 | 1979-12-18 | Union Carbide Corporation | Method for adding manganese to a molten magnesium bath |
| JPH0849025A (en) * | 1994-08-05 | 1996-02-20 | Mitsui Mining & Smelting Co Ltd | Al-Mn master alloy additive for producing aluminum-containing magnesium-based alloy |
-
1998
- 1998-03-20 AU AUPP2469A patent/AUPP246998A0/en not_active Abandoned
-
1999
- 1999-03-22 WO PCT/AU1999/000189 patent/WO1999049089A1/en not_active Ceased
- 1999-03-22 CA CA002324961A patent/CA2324961A1/en not_active Abandoned
- 1999-03-22 IL IL13852699A patent/IL138526A0/en unknown
- 1999-03-22 MX MXPA00009225A patent/MXPA00009225A/en unknown
- 1999-03-22 CZ CZ20003374A patent/CZ20003374A3/en unknown
- 1999-03-22 EP EP99910034A patent/EP1073774A4/en not_active Withdrawn
-
2000
- 2000-09-19 IS IS5630A patent/IS5630A/en unknown
- 2000-09-19 NO NO20004676A patent/NO20004676L/en not_active Application Discontinuation
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR771023A (en) * | 1933-06-20 | 1934-09-28 | Manufacturing process of magnesium alloys and resulting alloys | |
| GB519304A (en) * | 1937-04-16 | 1940-03-21 | Georg Von Giesche S Erben | Improvements in magnesium alloys |
| GB533266A (en) * | 1939-04-27 | 1941-02-10 | Fritz Christen | Improvements in and relating to magnesium alloys |
| GB628289A (en) * | 1946-05-02 | 1949-08-25 | Bendix Aviat Corp | Improvements in or relating to the heat treatment of magnesium alloy castings |
| US5248477A (en) * | 1991-09-12 | 1993-09-28 | The Dow Chemical Company | Methods for producing high purity magnesium alloys |
Non-Patent Citations (2)
| Title |
|---|
| POLMEAR I J, ARNOLD E: "Light Alloys", LIGHT ALLOYS METALLURGY OF THE LIGHT METALS, XX, XX, 1 January 1981 (1981-01-01), XX, pages 127 - 161, XP002966285 * |
| See also references of EP1073774A4 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2003056050A1 (en) * | 2001-12-26 | 2003-07-10 | Jsc 'avisma Titanium-Magnesium Works' | Magnesium-based alloy and method for the production thereof |
| WO2003056049A1 (en) * | 2001-12-26 | 2003-07-10 | Jsc 'avisma Titanium-Magnesium Works' | Magnesium-based alloy and method for the production thereof |
| EP1460142A4 (en) * | 2001-12-26 | 2005-01-26 | Jsc Avisma Titanium Magnesium | Magnesium-based alloy and method for the production thereof |
| EP1460141A4 (en) * | 2001-12-26 | 2006-09-06 | Jsc Avisma Titanium Magnesium | Magnesium-based alloy and method for the production thereof |
| US7135079B2 (en) | 2001-12-26 | 2006-11-14 | Joint Stock Company “AVISMA-titanium-magnesium works” | Magnesium-based alloy and method for the production thereof |
| US7156931B2 (en) * | 2001-12-26 | 2007-01-02 | Public Stock Company Vsmpo-Avisma Corporation | Magnesium-base alloy and method for the production thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| NO20004676D0 (en) | 2000-09-19 |
| AUPP246998A0 (en) | 1998-04-09 |
| IL138526A0 (en) | 2001-10-31 |
| EP1073774A1 (en) | 2001-02-07 |
| EP1073774A4 (en) | 2002-01-23 |
| IS5630A (en) | 2000-09-19 |
| NO20004676L (en) | 2000-11-09 |
| CZ20003374A3 (en) | 2001-11-14 |
| MXPA00009225A (en) | 2002-06-04 |
| CA2324961A1 (en) | 1999-09-30 |
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