CN105349853A - High-strength aluminum alloy - Google Patents
High-strength aluminum alloy Download PDFInfo
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- CN105349853A CN105349853A CN201510769766.0A CN201510769766A CN105349853A CN 105349853 A CN105349853 A CN 105349853A CN 201510769766 A CN201510769766 A CN 201510769766A CN 105349853 A CN105349853 A CN 105349853A
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- zinc
- copper
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- aluminum alloy
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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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
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Abstract
The invention relates to a high-strength aluminum alloy. The alloy is composed of, by weight percentage, 0.2%-0.3% of silicon, 0.5%-0.8% of iron, 1.2%-1.5% of copper, 0.3%-0.5% of manganese, 0.5%-0.8% of magnesium, 6.0%-7.0% of zinc, 0.1%-0.3% of tungsten, 0.1%-0.3% of vanadium, 0.5%-1.2% of titanium, the balance aluminum and a small number of avoidless impurities.
Description
Technical field
The invention belongs to aluminum alloy materials, particularly relate to a kind of aldural.
Background technology
Aluminum alloy materials is widely used in the fields such as industry, civilian, building, and current industrial aluminium has many different requirements, as high strength, high tenacity and good corrosion resistance nature etc.The quantity that current aldural uses at industrial circle and increasing extent many, but there is many problems in alloy aluminum of the prior art, cannot meet the aspects such as machine-shaping, surface quality and thermal treatment, this makes to be restricted the use of high-strength aluminum alloy material in industrial circle.
Summary of the invention
The object of this invention is to provide a kind of aluminium alloy technical scheme, good processing characteristics can be had while the high-intensity performance ensureing aluminum alloy materials by the program.
The present invention is achieved by the following technical solutions:
A kind of aldural, include the following material composition counted by weight percentage: 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 zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, the vanadium of 0.1-0.3%, the titanium of 0.5-1.2%, surplus is aluminium and a small amount of unavoidable impurity.
Described aluminum alloy materials, in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc is between 6.0-6.5%; Do not exist when the scope of scope zinc 1.35% time of copper is 6.5%.
The invention has the beneficial effects as follows:
By technical scheme of the present invention, optimize the formula of existing high-strength aluminum alloy material, improve machine-shaping ability, also improve surface quality and the surface treatment properties of converted products, there is high strength simultaneously.
Embodiment
Technical scheme of the present invention is described in detail below in conjunction with specific embodiment.
Aluminum alloy materials is in the inventive solutions produced mainly through hot-work, particularly hot extrusion processing.
The techniques such as process for processing in the present invention with existing aluminum alloy production process and device all identical, change be only change to aluminum alloy materials composition, therefore all illustrate no longer one by one in the present invention and following each embodiment.
Unit selected is in the present invention weight percentage, and when not illustrating, the unit of each composition is weight percentage.
A kind of aldural, include the following material composition counted by weight percentage: 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 zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, the vanadium of 0.1-0.3%, the titanium of 0.5-1.2%, surplus is aluminium and a small amount of unavoidable impurity.
Described aluminum alloy materials, in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc is between 6.0-6.5%; Do not exist when the scope of scope zinc 1.35% time of copper is 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%.
In described composition, the ratio of silicon and iron is 2.5: 1.
Embodiment 1
The silicon of 0.2%, the iron of 0.5%, the copper of 1.2%, the manganese of 0.3%, the magnesium of 0.5%, the zinc of 7.0%, the tungsten of 0.15%, the vanadium of 0.15%, the titanium of 0.5%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 2
The silicon of 0.3%, the iron of 0.8%, the copper of 1.5%, the manganese of 0.5%, the magnesium of 0.8%, the zinc of 6.0%, the tungsten of 0.1%, the vanadium of 0.1%, the titanium of 1.2%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 3
The silicon of 0.25%, the iron of 0.6%, the copper of 1.3%, the manganese of 0.4%, the magnesium of 0.6%, the zinc of 6.8%, the tungsten of 0.3%, the vanadium of 0.3%, the titanium of 0.8%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 4
The silicon of 0.3%, the iron of 0.5%, the copper of 1.4%, the manganese of 0.3%, the magnesium of 0.8%, the zinc of 7.0%, the tungsten of 0.2%, the vanadium of 0.2%, the titanium of 1.0%, surplus is aluminium and a small amount of unavoidable impurity.
Below be only limited embodiment; because cannot enumerate embodiment at this; but these embodiments 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 (3)
1. an aldural, it is characterized in that: include the following material composition counted by weight percentage: 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 zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, the vanadium of 0.1-0.3%, the titanium of 0.5-1.2%, surplus is aluminium and a small amount of unavoidable impurity.
2. aldural according to claim 1, it is characterized in that: in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc is between 6.0-6.5%; Do not exist when the scope of scope zinc 1.35% time of copper is 6.5%.
3. aldural according to claim 1, is characterized in that: in described composition, and the ratio of silicon and iron is 2.5: 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201510769766.0A CN105349853A (en) | 2015-11-12 | 2015-11-12 | High-strength aluminum alloy |
Applications Claiming Priority (1)
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CN201510769766.0A CN105349853A (en) | 2015-11-12 | 2015-11-12 | High-strength aluminum alloy |
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CN105349853A true CN105349853A (en) | 2016-02-24 |
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CN201510769766.0A Pending CN105349853A (en) | 2015-11-12 | 2015-11-12 | High-strength aluminum alloy |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106191578A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of high-strength aluminum alloy |
CN106191579A (en) * | 2016-08-17 | 2016-12-07 | 杨雯雯 | A kind of high-strength aluminum alloy |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030102060A1 (en) * | 1999-02-22 | 2003-06-05 | Ole Daaland | Corrosion-resistant aluminum alloy |
CN102787261A (en) * | 2012-08-30 | 2012-11-21 | 郴州市强旺新金属材料有限公司 | Aluminum-silicon alloy |
CN102876943A (en) * | 2012-09-21 | 2013-01-16 | 史昊东 | Aluminum alloy material |
CN102994831A (en) * | 2012-09-29 | 2013-03-27 | 蔡丛荣 | High-strength aluminium alloy |
-
2015
- 2015-11-12 CN CN201510769766.0A patent/CN105349853A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20030102060A1 (en) * | 1999-02-22 | 2003-06-05 | Ole Daaland | Corrosion-resistant aluminum alloy |
CN102787261A (en) * | 2012-08-30 | 2012-11-21 | 郴州市强旺新金属材料有限公司 | Aluminum-silicon alloy |
CN102876943A (en) * | 2012-09-21 | 2013-01-16 | 史昊东 | Aluminum alloy material |
CN102994831A (en) * | 2012-09-29 | 2013-03-27 | 蔡丛荣 | High-strength aluminium alloy |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106191578A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of high-strength aluminum alloy |
CN106191579A (en) * | 2016-08-17 | 2016-12-07 | 杨雯雯 | A kind of high-strength aluminum alloy |
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Application publication date: 20160224 |
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