CN110656261A - High-wear-resistance aluminum alloy with new formula - Google Patents
High-wear-resistance aluminum alloy with new formula Download PDFInfo
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- CN110656261A CN110656261A CN201810689867.0A CN201810689867A CN110656261A CN 110656261 A CN110656261 A CN 110656261A CN 201810689867 A CN201810689867 A CN 201810689867A CN 110656261 A CN110656261 A CN 110656261A
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- aluminum alloy
- aluminum
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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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
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- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
A new formula high-wear-resistance aluminum alloy is obtained by adopting aluminum liquid regeneration smelting, and the generated aluminum alloy comprises the following components in percentage by weight: silicon: 18-19%, copper: 5-6%, magnesium: 0.65-0.75%, manganese: less than 0.4%, 0.5-1.0% zinc, 0.3-0.8% iron, 0.2-0.4% nickel, 0.2-0.4% titanium, less than 0.2% of other impurities, and the balance aluminum. The obtained aluminum alloy has high mechanical strength and good wear resistance.
Description
The technical field is as follows:
the invention relates to the field of aluminum alloy, in particular to a high-wear-resistance aluminum alloy with a new formula.
Background art:
the aluminum alloy has low density, high strength similar to or superior to that of high-quality steel, good plasticity, excellent electric conductivity, heat conductivity and corrosion resistance, is widely used in industry, and is second to steel in use amount. Have found numerous applications in the aerospace, automotive, machinery, marine and chemical industries.
Cast aluminum alloys have been used in engines, crankshaft components since 1903, and through the last hundred years of development cast aluminum alloys have evolved into a large series of cast aluminum alloys. Along with social progress, the demand for aviation aluminum and automobile lightweight aluminum is continuously increased, particularly, the requirement on wear resistance in the aspects of pistons and instruments is higher, the aluminum alloy is mainly used as ADC14 at present, and along with the wide use of the turbine increasing technology, the requirement on the wear resistance at high temperature is more urgent.
The aluminum alloy manufactured by the method greatly improves the wear resistance of the product under high pressure and prolongs the service life of the part.
The invention content is as follows:
the invention aims to provide a new formula of high-wear-resistance aluminum alloy, and the obtained aluminum alloy has high mechanical strength and good wear resistance.
The invention also aims to provide the high-wear-resistance aluminum alloy with the new formula, and the formula improves the wear-resistance mechanical property of the aluminum alloy.
The technical scheme adopted by the invention is as follows:
the aluminum alloy is obtained by regenerating and smelting aluminum liquid, and the generated aluminum alloy comprises the following components in percentage by weight: silicon: 18-19%, copper: 5-6%, magnesium: 0.65-0.75%, manganese: less than 0.4%, 0.5-1.0% zinc, 0.3-0.8% iron, 0.2-0.4% nickel, 0.2-0.4% titanium, less than 0.2% of other impurities, and the balance aluminum.
Further, according to the weight ratio: silicon: 19%, copper: 5%, magnesium: 0.65%, manganese: 0.3%, zinc 0.65%, iron 0.3%, nickel 0.2%, titanium 0.2%, total of other impurities 0.2%, and the balance of aluminum.
Further, according to the weight ratio: silicon: 18.5%, copper: 5.5%, magnesium: 0.7%, manganese: 0.35%, zinc 0.75%, iron 0.5%, nickel 0.3%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
Further, according to the weight ratio: silicon: 18%, copper: 6%, magnesium: 0.75%, manganese: 0.35%, zinc 0.8%, iron 0.7%, nickel 0.4%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
The specific implementation mode is as follows:
example 1
A new formula of high-wear-resistance aluminum alloy comprises the following components in parts by weight:
silicon: 19%, copper: 5%, magnesium: 0.65%, manganese: 0.3%, zinc 0.65%, iron 0.3%, nickel 0.2%, titanium 0.2%, total of other impurities 0.2%, and the balance of aluminum.
Example 2
A new formula of high-wear-resistance aluminum alloy comprises the following components in parts by weight:
silicon: 18.5%, copper: 5.5%, magnesium: 0.7%, manganese: 0.35%, zinc 0.75%, iron 0.5%, nickel 0.3%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
Example 3
A new formula of high-wear-resistance aluminum alloy comprises the following components in parts by weight:
silicon: 18%, copper: 6%, magnesium: 0.75%, manganese: 0.35%, zinc 0.8%, iron 0.7%, nickel 0.4%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
The embodiments described above are some, but not all embodiments of the invention. The detailed description of the embodiments of the present invention is not intended to limit the scope of the invention as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Claims (4)
1. A new formula high wear-resistant aluminum alloy is characterized in that: the components of the generated aluminum alloy are as follows by weight ratio: silicon: 18-19%, copper: 5-6%, magnesium: 0.65-0.75%, manganese: less than 0.4%, 0.5-1.0% zinc, 0.3-0.8% iron, 0.2-0.4% nickel, 0.2-0.4% titanium, less than 0.2% of other impurities, and the balance aluminum.
2. Further, according to the weight ratio: silicon: 19%, copper: 5%, magnesium: 0.65%, manganese: 0.3%, zinc 0.65%, iron 0.3%, nickel 0.2%, titanium 0.2%, total of other impurities 0.2%, and the balance of aluminum.
3. Further, according to the weight ratio: silicon: 18.5%, copper: 5.5%, magnesium: 0.7%, manganese: 0.35%, zinc 0.75%, iron 0.5%, nickel 0.3%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
4. Further, according to the weight ratio: silicon: 18%, copper: 6%, magnesium: 0.75%, manganese: 0.35%, zinc 0.8%, iron 0.7%, nickel 0.4%, titanium 0.2-0.4%, other impurities 0.2% in total, and the balance aluminum.
Priority Applications (1)
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CN201810689867.0A CN110656261A (en) | 2018-06-28 | 2018-06-28 | High-wear-resistance aluminum alloy with new formula |
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CN201810689867.0A CN110656261A (en) | 2018-06-28 | 2018-06-28 | High-wear-resistance aluminum alloy with new formula |
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CN201810689867.0A Pending CN110656261A (en) | 2018-06-28 | 2018-06-28 | High-wear-resistance aluminum alloy with new formula |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110241332A (en) * | 2019-06-27 | 2019-09-17 | 广东顺博铝合金有限公司 | A kind of wear-resistant aluminum alloy and its preparation |
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2018
- 2018-06-28 CN CN201810689867.0A patent/CN110656261A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110241332A (en) * | 2019-06-27 | 2019-09-17 | 广东顺博铝合金有限公司 | A kind of wear-resistant aluminum alloy and its preparation |
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Application publication date: 20200107 |