CN106191579A - A kind of high-strength aluminum alloy - Google Patents
A kind of high-strength aluminum alloy Download PDFInfo
- Publication number
- CN106191579A CN106191579A CN201610683003.9A CN201610683003A CN106191579A CN 106191579 A CN106191579 A CN 106191579A CN 201610683003 A CN201610683003 A CN 201610683003A CN 106191579 A CN106191579 A CN 106191579A
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- CN
- China
- Prior art keywords
- zinc
- copper
- aluminum alloy
- scope
- strength aluminum
- Prior art date
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Classifications
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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
Abstract
The present invention relates to a kind of high-strength aluminum alloy, include following material count by weight percentage and form: the silicon of 0.2 0.3%, the ferrum of 0.5 0.8%, the copper of 1.2 1.5%, the manganese of 0.03 0.05%, the magnesium of 0.5 0.8%, the vanadium of 0.3 0.5%, the zirconium of 0.05 0.1%, the chromium of 0.05 0.2%, the tungsten of 0.1 0.3%, the scandium of 0.001 0.003%, the boron of 0.001 0.005%, the zinc of 6.0 7.0%, the titanium of 0.03 0.05%, surplus is aluminum and a small amount of unavoidable impurity.
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 field such as industry, civilian, building, and current industrial aluminum has many different wanting
Ask, such as high intensity, high tenacity and good decay resistance etc..The quantity that at present high-strength aluminum alloy uses at industrial circle with
Scope gets more and more, but alloy aluminum of the prior art exists many problems, it is impossible to meet machine-shaping, surface quality and Re Chu
The aspects such as reason, this makes to be restricted high-strength aluminum alloy material use in industrial circle.
Summary of the invention
It is an object of the invention to provide a kind of aluminium alloy technical scheme, aluminum alloy materials can ensured by the program
There is while high-intensity performance good processing characteristics.
The present invention is achieved by the following technical solutions:
A kind of high-strength aluminum alloy, includes following material count by weight percentage and forms: the silicon of 0.2-0.3%,
The ferrum of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.03-0.05%, the magnesium of 0.5-0.8%, the vanadium of 0.3-0.5%, 0.05-
The zirconium of 0.1%, the chromium of 0.05-0.2%, the zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, the scandium of 0.001-0.003%, 0.001-
The boron of 0.005%, the titanium of 0.03-0.05%, surplus is aluminum and a small amount of unavoidable impurity.
Described high-strength aluminum alloy, in its composition, the relation of copper and two kinds of elements of zinc is the content range at two elements
In, the middle point range of copper is 1.35%, and the midpoint of zinc is 6.5%, the zinc when the compositing range of copper is between 1.2-1.35%
Scope 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 deposit
In the scope of zinc when the scope of copper is 1.35% 6.5%.
The invention has the beneficial effects as follows:
By technical scheme, optimize the formula of existing high-strength aluminum alloy material, improve and be processed into
Type ability, also improves surface quality and the surface treatment properties of converted products, has high intensity simultaneously.
Detailed description of the invention
Technical scheme is described in detail below in conjunction with specific embodiment.
Aluminum alloy materials in the inventive solutions is mainly produced by hot-working, and particularly hot extrusion processing is raw
Produce.
The techniques such as production and processing in the present invention compared with aluminum alloy production process and device the most identical, change is only
It is the change to aluminum alloy materials composition, therefore says the most one by one in the present invention and following each embodiment
Bright.
Unit selected in the present invention is weight percentage, respectively forms in the case of not illustrating
Unit be weight percentage.
A kind of high-strength aluminum alloy, includes following material count by weight percentage and forms: the silicon of 0.2-0.3%,
The ferrum of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.03-0.05%, the magnesium of 0.5-0.8%, the vanadium of 0.3-0.5%, 0.05-
The zirconium of 0.1%, the chromium of 0.05-0.2%, the zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, the scandium of 0.001-0.003%, 0.001-
The boron of 0.005%, the titanium of 0.03-0.05%, surplus is aluminum and a small amount of unavoidable impurity.
Described high-strength aluminum alloy, in its composition, the relation of copper and two kinds of elements of zinc is the content range at two elements
In, the middle point range of copper is 1.35%, and the midpoint of zinc is 6.5%, the zinc when the compositing range of copper is between 1.2-1.35%
Scope 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 deposit
In the scope of zinc when the scope of copper is 1.35% 6.5%.The midpoint of wherein said copper refers to (1.2%+1.5%)/2=
1.35%;The midpoint of described zinc refers to (6.0%+7.0%)/2=6.5%.
Embodiment 1
Mass percent is the silicon of 0.2%, the ferrum of 0.5%, the copper of 1.2%, the manganese of 0.03%, the magnesium of 0.5%, 0.3%
Vanadium, the zirconium of 0.05%, the chromium of 0.05%, the zinc of 7.0%, the tungsten of 0.1%, the scandium of 0.001%, the boron of 0.001%, 0.03%
Titanium, surplus is aluminum and a small amount of unavoidable impurity.
Embodiment 2
Mass percent is the silicon of 0.3%, the ferrum of 0.8%, the copper of 1.5%, the manganese of 0.05%, the magnesium of 0.8%, 0.5%
Vanadium, the zirconium of 0.1%, the chromium of 0.2%, the zinc of 6.0%, the tungsten of 0.3%, the scandium of 0.003%, the boron of 0.005%, 0.05%
Titanium, surplus is aluminum and a small amount of unavoidable impurity.
Embodiment 3
Mass percent is the silicon of 0.25%, the ferrum of 0.6%, the copper of 1.3%, the manganese of 0.04%, the magnesium of 0.6%,
The vanadium of 0.35%, the zirconium of 0.07%, the chromium of 0.1%, the zinc of 6.8%, the tungsten of 0.2%, the scandium of 0.002%, the boron of 0.003%,
The titanium of 0.04%, surplus is aluminum and a small amount of unavoidable impurity.
Embodiment 4
Mass percent is the silicon of 0.3%, the ferrum of 0.5%, the copper of 1.4%, the manganese of 0.03%, the magnesium of 0.8%, 0.4%
Vanadium, the zirconium of 0.08%, the chromium of 0.15%, the zinc of 7.0%, the tungsten of 0.15%, the scandium of 0.0022%, the boron of 0.004%,
The titanium of 0.05%, surplus is aluminum and a small amount of unavoidable impurity.
Below being only limited embodiment, because cannot enumerate embodiment at this, but these embodiments are not
It is limitation of the present invention, it will be appreciated that those skilled in the art is by the change of technical solution of the present invention and constituent
The limited increase and decrease of matter is protection scope of the present invention.
Claims (2)
1. a high-strength aluminum alloy, it is characterised in that: include following material composition count by weight percentage: 0.2-
The silicon of 0.3%, the ferrum of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.03-0.05%, the magnesium of 0.5-0.8%, 0.3-0.5%
Vanadium, the zirconium of 0.05-0.1%, the chromium of 0.05-0.2%, the zinc of 6.0-7.0%, the tungsten of 0.1-0.3%, 0.001-0.003%
Scandium, the boron of 0.001-0.005%, the titanium of 0.03-0.05%, surplus is aluminum and a small amount of unavoidable impurity.
High-strength aluminum alloy the most according to claim 1, it is characterised in that: copper and the relation of two kinds of elements of zinc in its composition
Being in the content range of two elements, the middle point range of copper is 1.35%, and the midpoint of zinc is 6.5%, when the compositing range of copper exists
Time 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
Between 6.0-6.5%;There is not when the scope of copper is 1.35% the scope of zinc 6.5%.
Priority Applications (1)
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CN201610683003.9A CN106191579A (en) | 2016-08-17 | 2016-08-17 | A kind of high-strength aluminum alloy |
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CN201610683003.9A CN106191579A (en) | 2016-08-17 | 2016-08-17 | A kind of high-strength aluminum alloy |
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CN106191579A true CN106191579A (en) | 2016-12-07 |
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CN201610683003.9A Pending CN106191579A (en) | 2016-08-17 | 2016-08-17 | A kind of high-strength aluminum alloy |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103924137A (en) * | 2014-04-30 | 2014-07-16 | 南通易实工业制造有限公司 | High-strength aluminium alloy |
CN105274406A (en) * | 2015-11-12 | 2016-01-27 | 黄忠波 | High-strength aluminum alloy |
CN105349853A (en) * | 2015-11-12 | 2016-02-24 | 严静儿 | High-strength aluminum alloy |
CN105349854A (en) * | 2015-11-12 | 2016-02-24 | 俞虹 | High-strength aluminum alloy |
JP2016141843A (en) * | 2015-02-02 | 2016-08-08 | 株式会社神戸製鋼所 | High strength aluminum alloy sheet |
CN106048344A (en) * | 2016-06-30 | 2016-10-26 | 合肥慧林建材有限公司 | High-strength aluminum alloy profile and production process thereof |
-
2016
- 2016-08-17 CN CN201610683003.9A patent/CN106191579A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103924137A (en) * | 2014-04-30 | 2014-07-16 | 南通易实工业制造有限公司 | High-strength aluminium alloy |
JP2016141843A (en) * | 2015-02-02 | 2016-08-08 | 株式会社神戸製鋼所 | High strength aluminum alloy sheet |
CN105274406A (en) * | 2015-11-12 | 2016-01-27 | 黄忠波 | High-strength aluminum alloy |
CN105349853A (en) * | 2015-11-12 | 2016-02-24 | 严静儿 | High-strength aluminum alloy |
CN105349854A (en) * | 2015-11-12 | 2016-02-24 | 俞虹 | High-strength aluminum alloy |
CN106048344A (en) * | 2016-06-30 | 2016-10-26 | 合肥慧林建材有限公司 | High-strength aluminum alloy profile and production process thereof |
Non-Patent Citations (1)
Title |
---|
唐代明: "《金属材料学》", 30 June 2014, 西南交通大学出版社 * |
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Application publication date: 20161207 |