CN102482738A - Method For Producing An Aluminum-magnesium-based High-strength Alloy - Google Patents
Method For Producing An Aluminum-magnesium-based High-strength Alloy Download PDFInfo
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- CN102482738A CN102482738A CN2010800345878A CN201080034587A CN102482738A CN 102482738 A CN102482738 A CN 102482738A CN 2010800345878 A CN2010800345878 A CN 2010800345878A CN 201080034587 A CN201080034587 A CN 201080034587A CN 102482738 A CN102482738 A CN 102482738A
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- 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
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- 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
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
-
- 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
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C2202/00—Physical properties
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Conductive Materials (AREA)
- Laminated Bodies (AREA)
Abstract
The present invention relates to an Al-Mg-based high-strength alloy comprising 9 to 18 wt % of Mg, Al, and a small amount of Si, Fe, Mn and Ti. The alloy of the present invention has been developed to be used as a material for components of vehicles, bicycles and electronic devices, and as a material for cases for portable communication equipment. The alloy of the present invention can be made into the abovementioned products such that the latter are lightweight have a high strength.
Description
Technical field
The present invention relates to a kind of lightweight high-intensity Al-Mg is alloy.
Recently, be applicable to that the alloy material of auto parts, attachments of a bicycle, electrical/electronic part and robot etc. is asked to possess the light high-intensity characteristic, people have dropped into great effort to the research and development of aforementioned alloy material.
Technical field of the present invention belongs to above-mentioned ultralight amount and HS Al-Mg is an alloy.
Background technology
As typical A l-Mg is alloy, and Hydronalium (Hydronalium) has not only possessed excellent solidity to corrosion, intensity, unit elongation at the Mg that contains on the Al about 5-8wt%, and proportion is little, and machinability is also good.
Above-mentioned Hydronalium (Hydronalium) is a kind ofly to carry out αGu Rongti and β (Al mutually at 450 ℃
3Mg
2Phase) alloy of coexistence operation, segregation more extensively and easily appears in the solidification temperature range of this alloy, and higher in pyritous Mg solid solubility, therefore need be 400 ℃ of thermal treatments of annealing to improve intensity and unit elongation.
In addition; Al-Mg is the easy oxidation of molten soup of alloy; Mg is the strong reducing property metallic element; Can cause the so-called casting mold reaction (Metal-mold reaction) that absorbs hydrogen (H) when contacting and form bubble with airborne hydrogen (H), to need to add a small amount of Be in order preventing and to prevent alloy oxidation on the castings surface.
And, can obtain certain effect when after molding sand is sneaked into the ammonium borofluoride things such as (ammonium fluoroborate) about 2%, processing model.
Yet; Though being alloy, Al-Mg can process the light high-intensity alloy above 8% o'clock at Mg content; But the amount of oxidation of the high more molten soup of Mg content is with to inhale hydrogen (H) amount many more, thereby becomes the reason that causes the alloy surface bubble, so the alloy that Mg content surpasses 8%wt does not possess economy; Difficulty during manufacturing is also high, can't obtain widespread use.
Summary of the invention
Invention needs the technical task of solution
The purpose of this invention is to provide and a kind ofly contain 9 to 18wt% Mg and add the Al-Mg series high strength alloy of a small amount of Si, Fe, Mn and Ti at Al; It is light weight and have good weldableness and the surface is beautiful not only, is suitable as the material of vapour spare, bike, electronic product and portable communications equipped case etc.
Solve the technical scheme of problem
When the molten soup of Al drops into more Mg, can be because Mg oxidation and can't be at the residual Mg of Al matrix organization.
The present invention uses graphite (graphite) crucible to be heated to 600-700 ℃ to Al and processes and drop into solvent (FLUX) after the molten soup of Al and form the oxidation shielding film on the molten soup of Al surface, then toward the following input Mg on the molten soup of Al surface and develop the high Al alloy of Mg content through the fusion that prevents the Mg oxidation.
Beneficial effect
As previously mentioned; Be that alloy contains 9 to 18wt% Mg and develop HS ultralight amount Al-Mg at Al-Mg be alloy material, can be widely used in part, electric appliance and electronic part, robot part and portable communications equipment and so on shells such as the automobile that must possess the ultra lightweighting characteristic and bicycle frame etc.
Embodiment
The Al-Mg that the present invention relates to a kind of Mg of containing 9-18wt%, Si 0.1-0.3wt%, Fe 0.1-0.2wt%, Mn0.3-1.0wt%, Ti 0.15-0.25wt% is an alloy, and it is high for intensity and surface hardness, weight is light about the 2 times super light material of alloy than existing Al-Mg also.
Specifying Al-Mg of the present invention below in conjunction with embodiment is alloy.
(embodiment)
Al 82.9Kg, Si 0.2Kg, Fe 0.2Kg, Mn 0.5Kg, Ti 0.2Kg drop into plumbago crucible and be heated to 600-700 ℃ give fusion after, drop into solvent (FLUX) in the crucible and form the Flux layer that prevents film as oxidation on molten soup surface.
The product that above-mentioned solvent has used the non-ferrous metal fusion to use often.
Afterwards, drop into Mg 16Kg and keep back casting about 0.5-1 hour at 600-700 ℃ to forming in the molten soup that aerobicization prevents layer through long tube, process strength trial then and experimentize with after 2 of the test pieces, table 1 is its result.
Table 1 mechanical properties
Classification | Tensile strength Kgf/mm 2 | Hardness (HB) | The weight ratio of unit volume |
The present invention | 40 | 100 | 0.2 |
Existing Al-Mg (alloy) | 32 | 65 | 1 |
Shown in above-mentioned table 1, the existing Al-Mg of tensile strength and hardness ratio is that alloy has improved about 30-40%, and the weight of unit volume has also alleviated about 1.8 times.
In addition, the restriction of alloy composition ratio of the present invention the reasons are as follows.
①Mg:9-18wt%
Metallic element Mg not only improves the intensity of Al alloy, and dimensional change is less in the process of setting after casting, and weight is lighter, and castibility and machinability, impelling strength and weldableness are all good.
Intensity can reduce when Mg was lower than 9wt%, can be when rolling or extruding when Mg surpasses 18wt% the edge section be destroyed easily and reduce its processibility and productivity.
And; The meeting of stacking fault energy (Stacking fault energy) value reduced and increases the distance between the partial dislocation when Mg content surpassed 18wt%, thereby strengthened stacking fault (Stacking fault) field of alloy substrate tissue and cause taking place on the alloy surface micro bubble.
②Si:0.1-0.3wt%
The Si element is used the back to improve the fatigue strength and the wear resistance of Al alloy by Al matrix (matrix).
Bring into play effect when its content is lower than 0.1wt% hardly, separate out thick Si particle when surpassing 0.3wt% and reduce processibility.
③Fe:0.1-0.3wt%
The Fe element goes out and improves the wear resistance of Al alloy with the intermetallic compound crystalline substance at the Al alloy.
When being lower than 0.1wt%, its content almost do not have wear-resisting effect, thickization of particle when surpassing 0.3wt% and reduce processibility.
④Mn?0.3-1.0wt%
Metallic element Mn makes the Mg based compound to separate out equably, and when the moulding post-heating, improves intensity, is the metallic element that needs when obtaining the fine crystalline grain.
Do not occur above-mentioned effect when its content is lower than 0.3wt%, form thick intermetallic compound when surpassing 1.0wt% and reduce unit elongation, thereby reduce toughness.
Therefore the compositing range of Mn is set at 0.3-1.0wt%.
⑤Ti:0.15-0.25wt%
The Ti element can make the particle miniaturization, is the element that needs when further improving the intensity of Al alloy.
Its content forms thick intermetallic compound when surpassing 0.25wt% and reduces formability (processibility), can not help the raising of alloy strength when being lower than 0.15wt%.
Claims (1)
1. the method for manufacture of a HS aluminium-magnesium alloy, this alloy comprises Mg 9-18wt%, Si0.1-0.3wt%, Fe 0.1-0.3wt%, Mn 0.3-1.0wt%, Ti 0.15-0.25wt%, and surplus is Al, it is characterized in that:
Drop into the plumbago crucible post-heating to the alloy beyond the above-mentioned Mg and process molten soup to 600-700 ℃,
Drop into solvent (FLUX) and melting the surperficial solvent layer (FLUX) that prevents layer as oxidation that forms of soup at above-mentioned molten soup,
Through long tube to be formed with drop in the molten soup that above-mentioned oxidation prevents layer Mg and 600-700 ℃ keep 0.5-1 hour after casting, naturally cooling then.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020090091572A KR100978558B1 (en) | 2009-09-28 | 2009-09-28 | High strength aluminum-magnesium alloy |
KR10-2009-0091572 | 2009-09-28 | ||
PCT/KR2010/006486 WO2011037398A2 (en) | 2009-09-28 | 2010-09-20 | Method for producing an aluminum-magnesium-based high-strength alloy |
Publications (1)
Publication Number | Publication Date |
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CN102482738A true CN102482738A (en) | 2012-05-30 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2010800345878A Pending CN102482738A (en) | 2009-09-28 | 2010-09-20 | Method For Producing An Aluminum-magnesium-based High-strength Alloy |
Country Status (4)
Country | Link |
---|---|
JP (1) | JP2013501854A (en) |
KR (1) | KR100978558B1 (en) |
CN (1) | CN102482738A (en) |
WO (1) | WO2011037398A2 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103898378A (en) * | 2014-04-21 | 2014-07-02 | 黑龙江工程学院 | High magnesium aluminum alloy cold draw bar material and preparation method thereof |
CN104060136A (en) * | 2014-06-19 | 2014-09-24 | 广西中才铝业有限公司 | Aluminum alloy for preparation of triangular frame of bicycle and production method thereof |
CN107757764A (en) * | 2017-10-12 | 2018-03-06 | 宝鸡市金海源钛标准件制品有限公司 | A kind of almag rear bicycle |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR102591353B1 (en) * | 2016-09-29 | 2023-10-20 | 삼성전자주식회사 | Aluminum alloy for die casting and method for manufacturing the same |
KR102303378B1 (en) | 2019-06-14 | 2021-09-16 | 손희식 | Corrosion resistant aluminium alloy containing magnesium for casting |
KR20220087210A (en) | 2020-12-17 | 2022-06-24 | 현대자동차주식회사 | Aluminium sheets material for separator of fuel cell and manufacturing method thereof |
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US5486243A (en) * | 1992-10-13 | 1996-01-23 | Kawasaki Steel Corporation | Method of producing an aluminum alloy sheet excelling in formability |
JPH08199278A (en) * | 1995-01-27 | 1996-08-06 | Nippon Steel Corp | Aluminum alloy sheet excellent in press formability and baking finish hardenability and its production |
CN1740353A (en) * | 2005-09-22 | 2006-03-01 | 上海交通大学 | Prepn process of in-situ grain reinforced anticorrosive cast alumium-base composite material |
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JPS5827336B2 (en) | 1979-11-01 | 1983-06-08 | 株式会社神戸製鋼所 | High toughness, high strength Al alloy casting products |
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JPH03236457A (en) * | 1990-02-09 | 1991-10-22 | Furukawa Electric Co Ltd:The | Surface coating method for wire rod, bar stock, or tube stock made of al or al alloy |
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JP2006009157A (en) * | 2005-08-18 | 2006-01-12 | Fujitsu Ltd | Method for regenerating magnesium alloy material and recycling system |
JP4923498B2 (en) * | 2005-09-28 | 2012-04-25 | 株式会社豊田中央研究所 | High strength and low specific gravity aluminum alloy |
JP4504914B2 (en) * | 2005-12-19 | 2010-07-14 | 株式会社神戸製鋼所 | Aluminum ingot manufacturing method, aluminum ingot, and protective gas for manufacturing aluminum ingot |
KR100741660B1 (en) | 2006-02-28 | 2007-07-23 | 주식회사 대원합금 | Aluminum-magnesium alloy for interior & exterior furnishings of mobile phone and electronic products |
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JP5416795B2 (en) * | 2012-02-15 | 2014-02-12 | 株式会社神戸製鋼所 | Aluminum alloy sheet for forming |
-
2009
- 2009-09-28 KR KR1020090091572A patent/KR100978558B1/en active IP Right Grant
-
2010
- 2010-09-20 WO PCT/KR2010/006486 patent/WO2011037398A2/en active Application Filing
- 2010-09-20 CN CN2010800345878A patent/CN102482738A/en active Pending
- 2010-09-20 JP JP2012524664A patent/JP2013501854A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US5486243A (en) * | 1992-10-13 | 1996-01-23 | Kawasaki Steel Corporation | Method of producing an aluminum alloy sheet excelling in formability |
JPH08199278A (en) * | 1995-01-27 | 1996-08-06 | Nippon Steel Corp | Aluminum alloy sheet excellent in press formability and baking finish hardenability and its production |
CN1740353A (en) * | 2005-09-22 | 2006-03-01 | 上海交通大学 | Prepn process of in-situ grain reinforced anticorrosive cast alumium-base composite material |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103898378A (en) * | 2014-04-21 | 2014-07-02 | 黑龙江工程学院 | High magnesium aluminum alloy cold draw bar material and preparation method thereof |
CN103898378B (en) * | 2014-04-21 | 2015-12-02 | 黑龙江工程学院 | High-magnesium aluminum alloy cold drawn bar and manufacture method thereof |
CN104060136A (en) * | 2014-06-19 | 2014-09-24 | 广西中才铝业有限公司 | Aluminum alloy for preparation of triangular frame of bicycle and production method thereof |
CN107757764A (en) * | 2017-10-12 | 2018-03-06 | 宝鸡市金海源钛标准件制品有限公司 | A kind of almag rear bicycle |
Also Published As
Publication number | Publication date |
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WO2011037398A2 (en) | 2011-03-31 |
JP2013501854A (en) | 2013-01-17 |
KR100978558B1 (en) | 2010-08-27 |
WO2011037398A3 (en) | 2011-08-04 |
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Application publication date: 20120530 |