CN108034865A - A kind of aluminum alloy materials - Google Patents
A kind of aluminum alloy materials Download PDFInfo
- Publication number
- CN108034865A CN108034865A CN201711386503.7A CN201711386503A CN108034865A CN 108034865 A CN108034865 A CN 108034865A CN 201711386503 A CN201711386503 A CN 201711386503A CN 108034865 A CN108034865 A CN 108034865A
- Authority
- CN
- China
- Prior art keywords
- aluminum alloy
- alloy materials
- count
- present
- weight percentage
- 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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Classifications
-
- 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
-
- 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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
Abstract
The present invention relates to a kind of aluminum alloy materials.The aluminum alloy materials include：Aluminium 96 98%, silicon 0.25 1.5%, manganese 0.5 1.5%, thorium 0.25 1%, above component is count by weight percentage；A certain amount of zinc and silver can be also added in alloy material, by adjusting the proportioning of each component, improves the tensile property of alloy material.Compared with prior art, aluminum alloy materials of the present invention are on the basis of with good solderability and corrosion resistance, while tensile property is also preferable, convenient processing after shaping.
Description
Technical field
The present invention relates to a kind of aluminum alloy materials.
Background technology
Aluminium alloy density is low but intensity is higher, and near or above high-quality steel, plasticity is good, can be processed into various section bars,
With excellent electric conductivity, thermal conductivity and corrosion stability, therefore aluminium alloy is in Aeronautics and Astronautics, automobile, machine-building, ship and change
Learning in industry has extensive application, is most widely used non-ferrous metal structural material in industry.It is at full speed with industrial economy
Development, it is also increasing to the demand of Welded structural member, while corrosion resistance to aluminium alloy, die casting performance etc. will
Ask also higher and higher.A kind of the present invention is intended to provide aluminum alloy materials of high comprehensive performance.
The content of the invention
To achieve the above object, the present invention provides a kind of aluminum alloy materials.
Technical scheme is as follows：The aluminum alloy materials, count by weight percentage, including：Aluminium 96-98%,
Silicone content is 0.25-1.5%, manganese 0.5-1.5%, thorium 0.25-1%.
Preferably, zinc 0.25-0.5% is also contained count by weight percentage.
Preferably, silver 0.5-1.5% is also contained count by weight percentage.
It is furthermore preferred that aluminum alloy materials, count by weight percentage, including aluminium 96%, silicone content 1.1%, manganese 1.2%, thorium
0.6%, zinc 0.5%, silver 0.8%.
Compared with prior art, the beneficial effects of the present invention are：The aluminum alloy materials have good solderability and
Corrosion resistance, while die casting performance and tensile property are also preferable, convenient processing after shaping.
Embodiment
With reference to embodiment, the present invention is described in further detail, and embodiment is only used for explaining the present invention
Illustrate rather than limit protection scope of the present invention.
Embodiment 1：
The aluminum alloy materials, count by weight percentage, including：Aluminium 97%, silicone content 1.2%, manganese 1.5%, thorium 0.3%.
The alloy material that the present embodiment obtains has good corrosion resistance and solderability.
Embodiment 2：
The aluminum alloy materials, count by weight percentage, including：Aluminium 96%, silicone content 1.2%, manganese 1.5%, thorium 0.3%, silver
1%。
The alloy material that the present embodiment obtains has good corrosion resistance and solderability, and tensile property is more preferable.
Embodiment 3：
The aluminum alloy materials, count by weight percentage, including：Aluminium 98%, silicone content 0.25%, manganese 0.5%, thorium 0.25%,
Zinc 0.5%, silver 0.5%.
The alloy material that the present embodiment obtains has good corrosion resistance and solderability, and tensile property is more preferable；Compare
It is slightly worse in Examples 1 and 2 solderability.
Embodiment 4：
The aluminum alloy materials, count by weight percentage, including：Aluminium 97.5%, silicone content 1.5%, manganese 1%, thorium 0.25%, zinc
0.25%。
The alloy material that the present embodiment obtains has good corrosion resistance and solderability, and tensile property is more preferable；Compare
In embodiment 1,2 and 3, corrosion resistance is best.
Embodiment 5：
The aluminum alloy materials, count by weight percentage, including aluminium 96%, silicone content 1.1%, manganese 1.2%, thorium 0.6%, zinc
0.5%, silver 0.8%.
The alloy material that the present embodiment obtains has good corrosion resistance and solderability, and tensile property is more preferable；Compare
In embodiment 1,2 and 3, tensile property is best.
Embodiment 6：
The aluminum alloy materials, count by weight percentage, including：Aluminium 96%, silicone content 0.5%, manganese 1.25%, thorium 0.25%,
Zinc 0.5%, silver 1.5%.
The alloy material that the present embodiment obtains has good corrosion resistance and solderability, and tensile property is more preferable；Compare
In embodiment 1,2 and 3, solderability is best.
The manufacture method of the magnesium-aluminium alloy material is not introduced in the present invention specifically, because its manufacture method can be using existing normal
The manufacture method of rule, this will not be repeated here.
Although description of this invention combination embodiments above carries out, those skilled in the art
Member can carry out many replacements, modifications and variations according to above-mentioned content, be obvious.Therefore, it is all it is such substitute,
Improve and change is included in the spirit and scope of appended claims.
Claims (4)
1. a kind of aluminum alloy materials, count by weight percentage, including：Aluminium 96-98%, silicone content 0.25-1.5%, manganese 0.5-
1.5%, thorium 0.25-1%.
2. aluminum alloy materials according to claim 1, it is characterised in that also contain zinc 0.25- count by weight percentage
0.5%。
3. aluminum alloy materials according to claim 2, it is characterised in that also contain silver 0.5- count by weight percentage
1.5%。
4. aluminum alloy materials, it is characterised in that count by weight percentage, including aluminium 96%, silicone content 1.1%, manganese 1.2%, thorium
0.6%, zinc 0.5%, silver 0.8%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711386503.7A CN108034865A (en) | 2017-12-20 | 2017-12-20 | A kind of aluminum alloy materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711386503.7A CN108034865A (en) | 2017-12-20 | 2017-12-20 | A kind of aluminum alloy materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108034865A true CN108034865A (en) | 2018-05-15 |
Family
ID=62100219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711386503.7A Pending CN108034865A (en) | 2017-12-20 | 2017-12-20 | A kind of aluminum alloy materials |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108034865A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5456012A (en) * | 1977-10-13 | 1979-05-04 | Sumitomo Light Metal Ind | Aluminium alloy for low pressure heating resistance |
| CN105200284A (en) * | 2015-09-18 | 2015-12-30 | 霍山县龙鑫金属制品有限公司 | Magnesium-aluminum alloy |
-
2017
- 2017-12-20 CN CN201711386503.7A patent/CN108034865A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5456012A (en) * | 1977-10-13 | 1979-05-04 | Sumitomo Light Metal Ind | Aluminium alloy for low pressure heating resistance |
| CN105200284A (en) * | 2015-09-18 | 2015-12-30 | 霍山县龙鑫金属制品有限公司 | Magnesium-aluminum alloy |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180515 |