CN103556006A - Aluminum alloy and manufacturing method thereof - Google Patents
Aluminum alloy and manufacturing method thereof Download PDFInfo
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- CN103556006A CN103556006A CN201310541043.6A CN201310541043A CN103556006A CN 103556006 A CN103556006 A CN 103556006A CN 201310541043 A CN201310541043 A CN 201310541043A CN 103556006 A CN103556006 A CN 103556006A
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Abstract
The invention provides an aluminum alloy and a manufacturing method thereof. The aluminum alloy comprises the following components in percentage by weight: 0.7-1.3% of Si, 0.1% of Cu, 0.4-1.0% of Mn, 0.6-1.2% of Mg, 0.1% of Ti and the balance of Al. According to the invention, the mechanical property and processability of the aluminum alloy are improved, the structure is uniform, and the composition is stable; and the aluminum alloy has favorable yield strength, tensile strength and elongation percentage, and has a corrosion-resistant structure.
Description
Technical field
The present invention relates to alloy art, relate in particular to a kind of aluminium alloy and manufacture method thereof.
Background technology
Aluminium alloy, because of the feature of its high strength and high rigidity, is widely used in all trades and professions, comprises mechanical component, aircraft, automobile, precision instrument, radio component parts, building shell, machine casing, consumer electronics, household electrical appliance etc.
At present, conventional car body panel mainly contains A1-Cu-Mg base (2000 are) with aluminium alloy, A1-Mg base (5000 are), A1-Mg-Si base (6000 are) alloy.Wherein 2000 are and 6000 are to be that thermal treatment can reinforced alloys, and 5000 is to be that thermal treatment can not reinforced alloys.2000 is that A1-Cu-Mg alloy has good forging, high strength and good welding property, but its erosion resistance is poor.5000 is A1-Mg base alloy, and its intensity, processability and corrosion resistance are all better, but its forging property is poor, and local delayed yield, and for thermal treatment can not reinforced alloys.6000 is A1-Mg-Si alloy, has suitable intensity and forming property, and is can thermal treatment alloy, therefore, for the aluminium alloy of car body panel, mainly concentrates on 6000 line aluminium alloys.
The following element that aluminium alloy comprises: Mg, Si, Cu, Mn, Ti etc., each element is not isolated working, its impact is wanted to do, wherein any composition number be alloy some performance bring variation.In existing aluminium alloy, at aspects such as mechanical property, processability, homogeneity of structure, segregations, all there is the space of further lifting.
Summary of the invention
The technical problem to be solved in the present invention is also to provide a kind of manufacture method of aluminium alloy, to obtain the aluminium alloy of better mechanical property and processability, homogeneous microstructure, stable components.
The technical solution adopted for the present invention to solve the technical problems is: a kind of aluminium alloy, and described aluminium alloy comprises according to weight percent meter: Si0.7-1.3%; Cu0.1%; Mn0.4-1.0%; Mg0.6-1.2%; Ti0.1%; Surplus is Al.
As a further improvement on the present invention, the weight percent content that the weight percent content that the weight percent content of described Si is 1.0%, Mn is 0.7%, Mg is 0.9%.
As a further improvement on the present invention, also comprise Fe in described aluminium alloy, the weight percent content of described Fe is 0.5%.
As a further improvement on the present invention,, in described aluminium alloy, also comprise Cr, the weight percent content of described Cr is 0.25%.
As a further improvement on the present invention, also comprise Zn in described aluminium alloy, the weight percent content of described Zn is 0.2%.
As a further improvement on the present invention, also comprise Ti in described aluminium alloy, the weight percent content of described Ti is 0.1%.
As a further improvement on the present invention, also comprise refining agent in described aluminium alloy, the weight percent content of described refining agent is 1～1.5%.
As a further improvement on the present invention, described refining agent comprises saltpetre and Graphite Powder 99, and saltpetre, Graphite Powder 99 weight percent are 20～30:1.
Correspondingly, a kind of manufacture method of aluminium alloy, comprises the steps:
S1, according to above-mentioned mass percent, a certain amount of mangal and a certain amount of aluminium titanium silicon are put into stove and heat up, furnace temperature increases to 880 ℃～980 ℃, adds remaining aluminium titanium silicon, aluminum-copper alloy after alloy melting again, is molten into aluminum alloy melt;
S2, reduce the temperature to 730 ℃ of aluminum alloy melt～770 ℃, in aluminum alloy melt, add MAG block, stir, refining agent is wrapped with aluminium foil, then with bell jar, be pressed in aluminium liquid, refining 8～12 minutes, skims;
S3, make solution temperature remain on 770 ℃～790 ℃, standing 25～35 minutes, after skimming, cast obtained aluminium alloy.
As a further improvement on the present invention, described step S2 also comprises: in production process, at chute place, add the required magnesium adding, and be aided with protective atmosphere, described protective atmosphere comprises CO
2, SF
6, described CO
2and SF
6volume ratio be 20～33:67～80.
The invention has the beneficial effects as follows, mechanical property and the processability of aluminium alloy of the present invention are promoted, and homogeneous microstructure, stable components.Its manufacturing approach craft is simple, cost is low.
Embodiment
Below in conjunction with example, the invention will be further described, the span of the quality percentage composition in following examples, and what represent raw material can get quality by interior of this content range, and each embodiment can form the multiple magnitude relation of using.
Embodiment mono-:
, according to weight percent meter, this alloy comprises: Si0.7-1.3%; Cu0.1%; Mn0.4-1.0%; Mg0.6-1.2%; Ti0.1%; Surplus is Al.Preferably, in the present embodiment, the weight percent content that the weight percent content that the weight percent content of Si is 1.0%, Mn is 0.7%, Mg is 0.9%.
The manufacture method of above-mentioned aluminium alloy, comprises the steps:
S1, by above-mentioned mass percent, a certain amount of mangal and a certain amount of aluminium titanium silicon are put into stove and heat up, furnace temperature increases to 880 ℃～980 ℃, adds remaining aluminium titanium silicon, aluminum-copper alloy after alloy melting again, is molten into aluminum alloy melt;
S2, reduce the temperature to 730 ℃ of aluminum alloy melt～770 ℃, in aluminum alloy melt, add MAG block, stir, refining agent is wrapped with aluminium foil, then with bell jar, be pressed in aluminium liquid, refining 8～12 minutes, skims;
S3, make solution temperature remain on 770 ℃～790 ℃, standing 25～35 minutes, after skimming, cast obtained aluminium alloy.
Preferably, in the present embodiment, step S2 also comprises: in production process, at chute place, add the required magnesium adding, and be aided with protective atmosphere, described protective atmosphere comprises CO
2, SF
6, described CO
2and SF
6volume ratio be 20～33:67～80.
Embodiment bis-:
, according to weight percent meter, this alloy comprises: Si0.7-1.3%; Cu0.1%; Mn0.4-1.0%; Mg0.6-1.2%; Ti0.1%.
Further, this aluminium alloy also comprises one or more the combination in Fe0.5%, Cr0.25%, Zn0.2%, Ti0.1%, and surplus is Al.
Preferably, in the present embodiment, the weight percent content that the weight percent content that the weight percent content of Si is 1.0%, Mn is 0.7%, Mg is 0.9%.
Further, this aluminium alloy also comprises refining agent 1～1.5%.
The manufacture method of above-mentioned aluminium alloy, comprises the steps:
S1, by above-mentioned mass percent, a certain amount of mangal and a certain amount of aluminium titanium silicon are put into stove and heat up, furnace temperature increases to 880 ℃～980 ℃, adds remaining metal alloy after alloy melting again, is molten into aluminum alloy melt;
S2, reduce the temperature to 730 ℃ of aluminum alloy melt～770 ℃, in aluminum alloy melt, add MAG block, stir, refining agent is wrapped with aluminium foil, then with bell jar, be pressed in aluminium liquid, refining 8～12 minutes, skims;
S3, make solution temperature remain on 770 ℃～790 ℃, standing 25～35 minutes, after skimming, cast obtained aluminium alloy.
Preferably, in the present embodiment, step S2 also comprises: in production process, at chute place, add the required magnesium adding, and be aided with protective atmosphere, described protective atmosphere comprises CO
2, SF
6, described CO
2and SF
6volume ratio be 20～33:67～80.
Experimental data:
Following table is all kinds of index parameters of the aluminium alloy of heterogeneity, the product that wherein comparative alloy is prior art.
By above-mentioned embodiment, can be found out, mechanical property and the processability of aluminium alloy of the present invention are promoted, and homogeneous microstructure, stable components, have good yield strength, tensile strength and unit elongation, have corrosion stability structure.
The above-mentioned foundation desirable embodiment of the present invention of take is enlightenment, and by above-mentioned description, relevant staff can, within not departing from the scope of this invention technological thought, carry out various change and modification completely.The technical scope of this invention is not limited to the content on specification sheets, must determine its technical scope according to claim scope.
Claims (10)
1. an aluminium alloy, is characterized in that, described aluminium alloy comprises according to weight percent meter:
Surplus is Al.
2. aluminium alloy according to claim 1, is characterized in that, the weight percent content that the weight percent content that the weight percent content of described Si is 1.0%, Mn is 0.7%, Mg is 0.9%.
3. aluminium alloy according to claim 1, is characterized in that, also comprises that Fe, the weight percent content of described Fe are 0.5% in described aluminium alloy.
4. aluminium alloy according to claim 1, is characterized in that, also comprises that Cr, the weight percent content of described Cr are 0.25% in described aluminium alloy.
5. aluminium alloy according to claim 1, is characterized in that, also comprises that Zn, the weight percent content of described Zn are 0.2% in described aluminium alloy.
6. aluminium alloy according to claim 1, is characterized in that, also comprises that Ti, the weight percent content of described Ti are 0.1% in described aluminium alloy.
7. aluminium alloy according to claim 1, is characterized in that, also comprises that refining agent, the weight percent content of described refining agent are 1～1.5% in described aluminium alloy.
8. aluminium alloy according to claim 7, is characterized in that, described refining agent comprises saltpetre and Graphite Powder 99, and saltpetre, Graphite Powder 99 weight percent are 20～30:1.
9. a manufacture method for aluminium alloy as claimed in claim 1, is characterized in that, described in comprise the steps:
S1, according to mass percent claimed in claim 1, a certain amount of mangal and a certain amount of aluminium titanium silicon are put into stove to heat up, furnace temperature increases to 880 ℃～980 ℃, adds remaining aluminium titanium silicon, aluminum-copper alloy after alloy melting again, is molten into aluminum alloy melt;
S2, reduce the temperature to 730 ℃ of aluminum alloy melt～770 ℃, in aluminum alloy melt, add MAG block, stir, refining agent is wrapped with aluminium foil, then with bell jar, be pressed in aluminium liquid, refining 8～12 minutes, skims;
S3, make solution temperature remain on 770 ℃～790 ℃, standing 25～35 minutes, after skimming, cast obtained aluminium alloy.
10. the manufacture method of aluminium alloy according to claim 9, is characterized in that, described step S2 also comprises: in production process, at chute place, add the required magnesium adding, and be aided with protective atmosphere, described protective atmosphere comprises CO
2, SF
6, described CO
2and SF
6volume ratio be 20～33:67～80.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104233018A (en) * | 2014-08-26 | 2014-12-24 | 盐城市鑫洋电热材料有限公司 | Reinforced aluminum alloy and preparation method thereof |
| CN105200277A (en) * | 2015-09-18 | 2015-12-30 | 霍山县龙鑫金属制品有限公司 | Aluminum alloy and manufacturing method thereof |
| CN105215314A (en) * | 2015-09-18 | 2016-01-06 | 霍山县龙鑫金属制品有限公司 | A kind of auto parts machinery pressure casting method |
| CN107365918A (en) * | 2017-07-18 | 2017-11-21 | 合肥万之景门窗有限公司 | A kind of casting technique of aluminium alloy ingots |
| CN108300907A (en) * | 2018-02-10 | 2018-07-20 | 沈阳航空航天大学 | A kind of Al-Mn-Si-Mg alloy materials and preparation method thereof |
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| US6153025A (en) * | 1997-07-17 | 2000-11-28 | Norsk Hydro A.S. | High corrosion resistant aluminum alloy containing titanium |
| CN1570174A (en) * | 2004-04-28 | 2005-01-26 | 郑州大学 | Al-Mg-Si-Cu-Ti-Sr alloy and method for making same |
| JP2010189750A (en) * | 2009-02-20 | 2010-09-02 | Kobe Steel Ltd | High-strength aluminum alloy wire and rod material excellent in softening resistance and method of manufacturing the same |
| CN103014443A (en) * | 2013-01-11 | 2013-04-03 | 中国科学院长春应用化学研究所 | Rare earth aluminum alloy and preparation method thereof |
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2013
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6153025A (en) * | 1997-07-17 | 2000-11-28 | Norsk Hydro A.S. | High corrosion resistant aluminum alloy containing titanium |
| CN1570174A (en) * | 2004-04-28 | 2005-01-26 | 郑州大学 | Al-Mg-Si-Cu-Ti-Sr alloy and method for making same |
| JP2010189750A (en) * | 2009-02-20 | 2010-09-02 | Kobe Steel Ltd | High-strength aluminum alloy wire and rod material excellent in softening resistance and method of manufacturing the same |
| CN103014443A (en) * | 2013-01-11 | 2013-04-03 | 中国科学院长春应用化学研究所 | Rare earth aluminum alloy and preparation method thereof |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104233018A (en) * | 2014-08-26 | 2014-12-24 | 盐城市鑫洋电热材料有限公司 | Reinforced aluminum alloy and preparation method thereof |
| CN105200277A (en) * | 2015-09-18 | 2015-12-30 | 霍山县龙鑫金属制品有限公司 | Aluminum alloy and manufacturing method thereof |
| CN105215314A (en) * | 2015-09-18 | 2016-01-06 | 霍山县龙鑫金属制品有限公司 | A kind of auto parts machinery pressure casting method |
| CN107365918A (en) * | 2017-07-18 | 2017-11-21 | 合肥万之景门窗有限公司 | A kind of casting technique of aluminium alloy ingots |
| CN108300907A (en) * | 2018-02-10 | 2018-07-20 | 沈阳航空航天大学 | A kind of Al-Mn-Si-Mg alloy materials and preparation method thereof |
| CN108300907B (en) * | 2018-02-10 | 2020-07-21 | 沈阳航空航天大学 | Al-Mn-Si-Mg alloy material and preparation method thereof |
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Application publication date: 20140205 |