CN102876943A - Aluminum alloy material - Google Patents
Aluminum alloy material Download PDFInfo
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- CN102876943A CN102876943A CN2012103583690A CN201210358369A CN102876943A CN 102876943 A CN102876943 A CN 102876943A CN 2012103583690 A CN2012103583690 A CN 2012103583690A CN 201210358369 A CN201210358369 A CN 201210358369A CN 102876943 A CN102876943 A CN 102876943A
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Abstract
The invention relates to an aluminum alloy material which comprises the following substances by weight: 0.2 to 0.3 percent of silicon, 0.5 to 0.8 percent of ferrum, 1.2 to 1.5 percent of copper, 0.3 to 0.5 percent of manganese, 0.5 to 0.8 percent of magnesium, 0.03 to 0.5 percent of chromium, 6.0 to 7.0 percent of zinc, 0.08 to 0.15 percent of titanium, and aluminum and a small amount of inevitable impurities in balancing amount.
Description
Technical field
The invention belongs to aluminum alloy materials, particularly relate to a kind of high-strength aluminum alloy material.
Background technology
Aluminum alloy materials is widely used in the fields such as industry, civilian, building, and present industrial aluminium has many different requirements, such as high strength, high tenacity and good corrosion resistance nature etc.Aldural is more and more in quantity and scope that industrial circle uses at present, but there are many problems in alloy aluminum of the prior art, can't satisfy the aspects such as machine-shaping, surface quality and thermal treatment, this is so that the use in industrial circle is restricted to high-strength aluminum alloy material.
Summary of the invention
The purpose of this invention is to provide a kind of aluminium alloy technical scheme, can in the high-intensity performance that guarantees aluminum alloy materials, have good processing characteristics by this scheme.
The present invention is achieved by the following technical solutions:
A kind of aluminum alloy materials, including the following material of counting by weight percentage forms: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.3-0.5%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.5%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
Described aluminum alloy materials, the relation of copper and two kinds of elements of zinc was in the content range of two elements during it formed, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and the scope of zinc is between 6.5-7.0% when the compositing range of copper is between 1.2-1.35%; When the composition of copper was between 1.35-1.5%, the scope of zinc was between 6.0-6.5%; Do not exist scope when the scope of copper zinc 1.35% time 6.5%.
The invention has the beneficial effects as follows:
By technical scheme of the present invention, optimized the prescription of existing high-strength aluminum alloy material, improved the machine-shaping ability, also improved surface quality and the surface treatment properties of converted products, have simultaneously high strength.
Embodiment
Describe technical scheme of the present invention in detail below in conjunction with specific embodiment.
Aluminum alloy materials in technical scheme of the present invention is mainly by hot-work production, particularly hot extrusion processing.
The techniques such as process for processing in the present invention are all identical with existing aluminum alloy production process and device, change only be change to the aluminum alloy materials composition, therefore in the present invention and following each embodiment, all illustrate no longer one by one.
Selected unit is weight percentage in the present invention, and each unit that forms is weight percentage in situation about not specifying.
A kind of aluminum alloy materials, including the following material of counting by weight percentage forms: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.3-0.5%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.5%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
Described aluminum alloy materials, the relation of copper and two kinds of elements of zinc was in the content range of two elements during it formed, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and the scope of zinc is between 6.5-7.0% when the compositing range of copper is between 1.2-1.35%; When the composition of copper was between 1.35-1.5%, the scope of zinc was between 6.0-6.5%; Do not exist scope when the scope of copper zinc 1.35% time 6.5%.The mid point of wherein said copper refers to (1.2%+1.5%)/2=1.35%; The mid point of described zinc refers to (6.0%+7.0%)/2=6.5%.
Embodiment 1
0.2% silicon, 0.5% iron, 1.2% copper, 0.3% manganese, 0.5% magnesium, 0.03% chromium, 7.0% zinc, 0.08% titanium, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 2
0.3% silicon, 0.8% iron, 1.5% copper, 0.5% manganese, 0.8% magnesium, 0.5% chromium, 6.0% zinc, 0.15% titanium, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 3
0.25% silicon, 0.6% iron, 1.3% copper, 0.4% manganese, 0.6% magnesium, 0.1% chromium, 6.8% zinc, 0.1% titanium, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 4
0.3% silicon, 0.5% iron, 1.4% copper, 0.3% manganese, 0.8% magnesium, 0.05% chromium, 7.0% zinc, 0.12% titanium, surplus is aluminium and a small amount of unavoidable impurity.
Below only be limited embodiment; because can't enumerate one by one embodiment at this; but these embodiment are not limitations of the present invention, should be appreciated that those skilled in the art is by being protection scope of the present invention to the change of technical solution of the present invention and the limited increase and decrease of component.
Claims (2)
1. aluminum alloy materials, it is characterized in that: include the following material of counting by weight percentage and form: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.3-0.5%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.5%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
2. aluminum alloy materials according to claim 1, it is characterized in that: the relation of copper and two kinds of elements of zinc was in the content range of two elements during it formed, the middle point range of copper is 1.35%, the mid point of zinc is 6.5%, and the scope of zinc is between 6.5-7.0% when the compositing range of copper is between 1.2-1.35%; When the composition of copper was between 1.35-1.5%, the scope of zinc was between 6.0-6.5%; Do not exist scope when the scope of copper zinc 1.35% time 6.5%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103583690A CN102876943A (en) | 2012-09-21 | 2012-09-21 | Aluminum alloy material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103583690A CN102876943A (en) | 2012-09-21 | 2012-09-21 | Aluminum alloy material |
Publications (1)
| Publication Number | Publication Date |
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| CN102876943A true CN102876943A (en) | 2013-01-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012103583690A Pending CN102876943A (en) | 2012-09-21 | 2012-09-21 | Aluminum alloy material |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102994830A (en) * | 2012-09-29 | 2013-03-27 | 吴雅萍 | High-strength aluminum alloy material |
| CN104294117A (en) * | 2014-10-29 | 2015-01-21 | 严静儿 | High-ductility aluminum alloy |
| CN104294116A (en) * | 2014-10-29 | 2015-01-21 | 严静儿 | High-performance aluminum alloy |
| CN105274407A (en) * | 2015-11-12 | 2016-01-27 | 严静儿 | Aluminum alloy material |
| CN105274406A (en) * | 2015-11-12 | 2016-01-27 | 黄忠波 | High-strength aluminum alloy |
| CN105349854A (en) * | 2015-11-12 | 2016-02-24 | 俞虹 | High-strength aluminum alloy |
| CN105349853A (en) * | 2015-11-12 | 2016-02-24 | 严静儿 | High-strength aluminum alloy |
| CN107312956A (en) * | 2017-07-18 | 2017-11-03 | 合肥万之景门窗有限公司 | A kind of preparation technology of aluminum alloy materials |
| US11203801B2 (en) | 2019-03-13 | 2021-12-21 | Novelis Inc. | Age-hardenable and highly formable aluminum alloys and methods of making the same |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102071341A (en) * | 2010-12-03 | 2011-05-25 | 中国兵器工业第五二研究所 | Cast aluminum-silicon alloy for engine cylinder head and heat treatment process |
| CN102286683A (en) * | 2011-08-12 | 2011-12-21 | 宁波德精机械有限公司 | Aluminum alloy material and preparation method thereof |
| CN102676892A (en) * | 2012-04-25 | 2012-09-19 | 宁波信泰机械有限公司 | 6410 aluminium alloy and preparation method and application of 6410 aluminium alloy |
-
2012
- 2012-09-21 CN CN2012103583690A patent/CN102876943A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102071341A (en) * | 2010-12-03 | 2011-05-25 | 中国兵器工业第五二研究所 | Cast aluminum-silicon alloy for engine cylinder head and heat treatment process |
| CN102286683A (en) * | 2011-08-12 | 2011-12-21 | 宁波德精机械有限公司 | Aluminum alloy material and preparation method thereof |
| CN102676892A (en) * | 2012-04-25 | 2012-09-19 | 宁波信泰机械有限公司 | 6410 aluminium alloy and preparation method and application of 6410 aluminium alloy |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102994830A (en) * | 2012-09-29 | 2013-03-27 | 吴雅萍 | High-strength aluminum alloy material |
| CN104294117A (en) * | 2014-10-29 | 2015-01-21 | 严静儿 | High-ductility aluminum alloy |
| CN104294116A (en) * | 2014-10-29 | 2015-01-21 | 严静儿 | High-performance aluminum alloy |
| CN105274407A (en) * | 2015-11-12 | 2016-01-27 | 严静儿 | Aluminum alloy material |
| CN105274406A (en) * | 2015-11-12 | 2016-01-27 | 黄忠波 | High-strength aluminum alloy |
| CN105349854A (en) * | 2015-11-12 | 2016-02-24 | 俞虹 | High-strength aluminum alloy |
| CN105349853A (en) * | 2015-11-12 | 2016-02-24 | 严静儿 | High-strength aluminum alloy |
| CN107312956A (en) * | 2017-07-18 | 2017-11-03 | 合肥万之景门窗有限公司 | A kind of preparation technology of aluminum alloy materials |
| CN107312956B (en) * | 2017-07-18 | 2019-02-15 | 合肥万之景门窗有限公司 | A kind of preparation process of aluminum alloy materials |
| US11203801B2 (en) | 2019-03-13 | 2021-12-21 | Novelis Inc. | Age-hardenable and highly formable aluminum alloys and methods of making the same |
| US11932924B2 (en) | 2019-03-13 | 2024-03-19 | Novelis, Inc. | Age-hardenable and highly formable aluminum alloys and methods of making the same |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
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Application publication date: 20130116 |