CN102994830A - High-strength aluminum alloy material - Google Patents
High-strength aluminum alloy material Download PDFInfo
- Publication number
- CN102994830A CN102994830A CN2012103775385A CN201210377538A CN102994830A CN 102994830 A CN102994830 A CN 102994830A CN 2012103775385 A CN2012103775385 A CN 2012103775385A CN 201210377538 A CN201210377538 A CN 201210377538A CN 102994830 A CN102994830 A CN 102994830A
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- China
- Prior art keywords
- zinc
- copper
- aluminum alloy
- alloy material
- scope
- 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.)
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 19
- 239000000956 alloy Substances 0.000 title claims abstract description 18
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 21
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 21
- 239000010949 copper Substances 0.000 claims abstract description 21
- 229910052802 copper Inorganic materials 0.000 claims abstract description 21
- 239000011701 zinc Substances 0.000 claims abstract description 21
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 8
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 8
- 239000011651 chromium Substances 0.000 claims abstract description 8
- 239000012535 impurity Substances 0.000 claims abstract description 8
- 229910052742 iron Inorganic materials 0.000 claims abstract description 8
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 8
- 239000011777 magnesium Substances 0.000 claims abstract description 8
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 8
- 239000010703 silicon Substances 0.000 claims abstract description 8
- 239000010936 titanium Substances 0.000 claims abstract description 8
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 8
- 239000004411 aluminium Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 3
- TVZPLCNGKSPOJA-UHFFFAOYSA-N copper zinc Chemical compound [Cu].[Zn] TVZPLCNGKSPOJA-UHFFFAOYSA-N 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 239000011572 manganese Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
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Abstract
The invention relates to a high-strength aluminum alloy material which comprises the components by weight percentage as follows: 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, 0.03-0.3% of chromium, 6.0-7.0% of zinc, 0.08-0.15% of titanium, and the balance of aluminum and avoidless impurities in a small 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 high-strength aluminum alloy material, 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 0.03-0.3%, 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 high-strength aluminum alloy material, 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 but did not comprise that scope when the scope of copper zinc 1.35% time is 6.5% between 6.0-6.5%.
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 high-strength aluminum alloy material, 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 0.03-0.3%, 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 high-strength aluminum alloy material, 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, 0.3% 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. high-strength aluminum alloy material, 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 0.03-0.3%, 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. high-strength aluminum alloy material 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 but did not comprise that scope when the scope of copper zinc 1.35% time is 6.5% between 6.0-6.5%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103775385A CN102994830A (en) | 2012-09-29 | 2012-09-29 | High-strength aluminum alloy material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103775385A CN102994830A (en) | 2012-09-29 | 2012-09-29 | High-strength aluminum alloy material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102994830A true CN102994830A (en) | 2013-03-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012103775385A Pending CN102994830A (en) | 2012-09-29 | 2012-09-29 | High-strength aluminum alloy material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102994830A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106191577A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of aluminum alloy materials |
| CN106191578A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of high-strength aluminum alloy |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6263641A (en) * | 1985-09-14 | 1987-03-20 | Showa Alum Corp | High-strength aluminum-alloy extruded material excellent in low-cycle fatigue characteristics |
| JPH09268342A (en) * | 1996-04-02 | 1997-10-14 | Aisin Keikinzoku Kk | High strength aluminum alloy |
| CN101086050A (en) * | 2006-06-06 | 2007-12-12 | 上虞市东轻特种铝材厂 | Aluminum alloy pipe |
| 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 |
| CN102876943A (en) * | 2012-09-21 | 2013-01-16 | 史昊东 | Aluminum alloy material |
-
2012
- 2012-09-29 CN CN2012103775385A patent/CN102994830A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6263641A (en) * | 1985-09-14 | 1987-03-20 | Showa Alum Corp | High-strength aluminum-alloy extruded material excellent in low-cycle fatigue characteristics |
| JPH09268342A (en) * | 1996-04-02 | 1997-10-14 | Aisin Keikinzoku Kk | High strength aluminum alloy |
| CN101086050A (en) * | 2006-06-06 | 2007-12-12 | 上虞市东轻特种铝材厂 | Aluminum alloy pipe |
| 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 |
| CN102876943A (en) * | 2012-09-21 | 2013-01-16 | 史昊东 | Aluminum alloy material |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106191577A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of aluminum alloy materials |
| CN106191578A (en) * | 2016-08-17 | 2016-12-07 | 包惠芳 | A kind of high-strength aluminum alloy |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
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Application publication date: 20130327 |