CN107034398A - A kind of high-strength aluminum alloy - Google Patents
A kind of high-strength aluminum alloy Download PDFInfo
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- CN107034398A CN107034398A CN201710313493.8A CN201710313493A CN107034398A CN 107034398 A CN107034398 A CN 107034398A CN 201710313493 A CN201710313493 A CN 201710313493A CN 107034398 A CN107034398 A CN 107034398A
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- Prior art keywords
- aluminum alloy
- strength aluminum
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- raw material
- following raw
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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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
-
- 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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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Abstract
The present invention relates to technical field of alloy material, and in particular to a kind of high-strength aluminum alloy.This kind of high-strength aluminum alloy, it is characterised in that be made up of the following raw material:Zn8 ~ 19%, Mg7 ~ 15%, Cu5 ~ 8%, Zr3 ~ 6%, Ti0.9 ~ 2.5%, Mn0.1 ~ 0.9%, Nb1.4 ~ 2.9%, Ni3.1 ~ 6.5%, Rb0.1 ~ 0.6%, Ta0.1 ~ 0.7%, Cr1.3 ~ 1.8% and surplus Al.This kind of high-strength aluminum alloy has excellent mechanical property, especially with higher intensity, toughness, and corrosion-resistant, antioxygenic property is good, and component segregation is slight, and surface quality is good.
Description
Technical field
The present invention relates to technical field of alloy material, and in particular to a kind of high-strength aluminum alloy.
Background technology
Punch forming is a kind of common machining process, refer to depended on pressure machine and mould to sheet material, band, tubing and
Section bar etc. applies external force, is allowed to produce plastic deformation or separates, so that the workpiece of shape and size needed for obtaining(Stamping parts)'s
Processing molding method.The stamping parts application field that punch process is produced is extensive, including consumption electronic product, machinery, five
Gold, means of transport etc..The metal material that punch forming is used is generally steel, copper alloy and aluminium alloy, with to material lightweight
Pay attention to day by day, aluminium alloy obtained increasingly being widely applied.However, existing aluminium alloy is still deficient in terms of intensity
Lack, accordingly, it is desirable to provide a kind of high-strength aluminum alloy is to meet use demand.
The content of the invention
Present invention aims at solving the above problems, there is provided a kind of high-strength aluminum alloy.
To achieve the above object, the invention provides a kind of high-strength aluminum alloy, it is made up of the following raw material:Zn8~19%、
Mg7~15%、Cu5~8%、Zr3~6%、Ti0.9~2.5%、Mn0.1~0.9%、Nb1.4~2.9%、Ni3.1~6.5%、Rb0.1~0.6%、
Ta0.1 ~ 0.7%, Cr1.3 ~ 1.8% and surplus Al.
The high-strength aluminum alloy, is made up of the following raw material:Zn10~15%、Mg10~13%、Cu6~8%、Zr4~6%、Ti1.3
~ 2.2%, Mn0.2 ~ 0.8%, Nb1.6 ~ 2.1%, Ni3.3 ~ 6.1%, Rb0.2 ~ 0.5%, Ta0.3 ~ 0.6%, Cr1.4 ~ 1.7% and surplus
Al。
The high-strength aluminum alloy, is made up of the following raw material:Zn12%、Mg11%、Cu7%、Zr5%、Ti1.8%、Mn0.6%、
Nb1.9%, Ni4.8%, Rb0.3%, Ta0.5%, Cr1.6% and surplus Al.
Beneficial effects of the present invention:This kind of high-strength aluminum alloy has an excellent mechanical property, especially with higher strong
Degree, toughness, corrosion-resistant, antioxygenic property are good, and component segregation is slight, and surface quality is good.
Embodiment
The present invention takes following technical scheme to realize:This kind of high-strength aluminum alloy, is made up of the following raw material:Zn8~19%、
Mg7~15%、Cu5~8%、Zr3~6%、Ti0.9~2.5%、Mn0.1~0.9%、Nb1.4~2.9%、Ni3.1~6.5%、Rb0.1~0.6%、
Ta0.1 ~ 0.7%, Cr1.3 ~ 1.8% and surplus Al.
As the preferred scheme of the present invention, high-strength aluminum alloy is made up of the following raw material:Zn10~15%、Mg10~13%、
Cu6~8%、Zr4~6%、Ti1.3~2.2%、Mn0.2~0.8%、Nb1.6~2.1%、Ni3.3~6.1%、Rb0.2~0.5%、Ta0.3~
0.6%th, Cr1.4 ~ 1.7% and surplus Al.
As the preferred scheme of the present invention, high-strength aluminum alloy is made up of the following raw material:Zn12%、Mg11%、Cu7%、
Zr5%, Ti1.8%, Mn0.6%, Nb1.9%, Ni4.8%, Rb0.3%, Ta0.5%, Cr1.6% and surplus Al.
This kind of high-strength aluminum alloy has excellent mechanical property, corrosion-resistant, anti-especially with higher intensity, toughness
Oxidation susceptibility is good, and component segregation is slight, and surface quality is good.
Preferred embodiment of the invention described in detail above.It should be appreciated that one of ordinary skill in the art without
Need creative work just can make many modifications and variations according to the design of the present invention.Therefore, all technologies in the art
Personnel are available by logical analysis, reasoning, or a limited experiment on the basis of existing technology under this invention's idea
Technical scheme, all should be in the protection domain being defined in the patent claims.
Claims (3)
1. a kind of high-strength aluminum alloy, it is characterised in that be made up of the following raw material:Zn8~19%、Mg7~15%、Cu5~8%、Zr3~
6%、Ti0.9~2.5%、Mn0.1~0.9%、Nb1.4~2.9%、Ni3.1~6.5%、Rb0.1~0.6%、Ta0.1~0.7%、Cr1.3~
1.8% and surplus Al.
2. high-strength aluminum alloy according to claim 1, it is characterised in that be made up of the following raw material:Zn10~15%、Mg10
~13%、Cu6~8%、Zr4~6%、Ti1.3~2.2%、Mn0.2~0.8%、Nb1.6~2.1%、Ni3.3~6.1%、Rb0.2~0.5%、
Ta0.3 ~ 0.6%, Cr1.4 ~ 1.7% and surplus Al.
3. high-strength aluminum alloy according to claim 1, it is characterised in that be made up of the following raw material:Zn12%、Mg11%、
Cu7%, Zr5%, Ti1.8%, Mn0.6%, Nb1.9%, Ni4.8%, Rb0.3%, Ta0.5%, Cr1.6% and surplus Al.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710313493.8A CN107034398A (en) | 2017-05-05 | 2017-05-05 | A kind of high-strength aluminum alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710313493.8A CN107034398A (en) | 2017-05-05 | 2017-05-05 | A kind of high-strength aluminum alloy |
Publications (1)
Publication Number | Publication Date |
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CN107034398A true CN107034398A (en) | 2017-08-11 |
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CN201710313493.8A Withdrawn CN107034398A (en) | 2017-05-05 | 2017-05-05 | A kind of high-strength aluminum alloy |
Country Status (1)
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117089748A (en) * | 2023-09-06 | 2023-11-21 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
-
2017
- 2017-05-05 CN CN201710313493.8A patent/CN107034398A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117089748A (en) * | 2023-09-06 | 2023-11-21 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
CN117089748B (en) * | 2023-09-06 | 2024-04-26 | 威海科米沃新材料有限公司 | Preparation method of high-elongation aluminum alloy material |
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PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WW01 | Invention patent application withdrawn after publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170811 |