CN105543626A - Aluminum alloy material - Google Patents
Aluminum alloy material Download PDFInfo
- Publication number
- CN105543626A CN105543626A CN201510935182.6A CN201510935182A CN105543626A CN 105543626 A CN105543626 A CN 105543626A CN 201510935182 A CN201510935182 A CN 201510935182A CN 105543626 A CN105543626 A CN 105543626A
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- CN
- China
- Prior art keywords
- parts
- aluminum alloy
- alloy material
- aluminium
- alloy materials
- 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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Adornments (AREA)
Abstract
The invention discloses an aluminum alloy material which comprises the following raw materials: 3-5 parts of Mn, 2-4 parts of Ti, 6-8 parts of Mg, 4-6 parts of Cr, 3-6 parts of Bi, 1-3 parts of Nb, 2-3 parts of Sr, 5-6 parts of Ba, 4-7 parts of Ni, 12-16 parts of Fe, 8-13 parts of Cu, and 35-42 parts of Al. The aluminum alloy material is high in hardness value, strength, comprehensive performance, heat resistance and abrasive resistance, and remarkable in antioxidant capacity.
Description
Technical field
The present invention relates to technical field of alloy, particularly relate to a kind of aluminum alloy materials.
Background technology
Aluminium alloy is a most widely used class non-ferrous metal structured material in industry, widely applies in Aeronautics and Astronautics, automobile, machinofacture, boats and ships and chemical industry.The develop rapidly of industrial economy, increasing to the demand of Welded structural part, make the Research on Weldability of aluminium alloy also thereupon deeply, maximum alloys applied by aluminum current alloy, but mechanical properties or the thermotolerances etc. such as the hardness of aluminium alloy is not high, its intensity need to strengthen, to adapt to the requirement of more high-tech sector.
Summary of the invention
For solving above-mentioned Problems existing, the invention provides a kind of hardness value high, intensity good combination property, thermotolerance is strong, and resistance of oxidation is remarkable, the aluminum alloy materials of high-wearing feature.
The technical scheme that the present invention solves the problems of the technologies described above employing is: a kind of aluminum alloy materials, comprises the raw material of following component:
Manganese 3-5 part, titanium 2-4 part, magnesium 6-8 part, chromium 4-6 part, bismuth 3-6 part, niobium 1-3 part, strontium 2-3 part, barium 5-6 part, nickel 4-7 part, iron 12-16 part, copper 8-13 part, aluminium 35-42 part.
Above-mentioned aluminum alloy materials, comprises the raw material of following component:
4 parts, manganese, titanium 3 parts, 7 parts, magnesium, chromium 5 parts, bismuth 5 parts, niobium 2 parts, 2.6 parts, strontium, barium 5.5 parts, 6 parts, nickel, iron 14 parts, copper 11 parts, 39 parts, aluminium.
The beneficial effect that technical solution problem of the present invention is brought is: hardness value of the present invention is high, intensity good combination property, and thermotolerance is strong, and resistance of oxidation is remarkable, high-wearing feature.
Embodiment
Below in conjunction with specific embodiment, the present invention is described in further details.
Embodiment 1
A kind of aluminum alloy materials, comprises the raw material of following component:
3 parts, manganese, titanium 2 parts, 6 parts, magnesium, chromium 4 parts, bismuth 3 parts, niobium 1 part, 2 parts, strontium, barium 5 parts, 4 parts, nickel, iron 12 parts, copper 8 parts, 35 parts, aluminium.
Embodiment 2
A kind of aluminum alloy materials, comprises the raw material of following component:
4 parts, manganese, titanium 3 parts, 7 parts, magnesium, chromium 5 parts, bismuth 5 parts, niobium 2 parts, 2.6 parts, strontium, barium 5.5 parts, 6 parts, nickel, iron 14 parts, copper 11 parts, 39 parts, aluminium.
Embodiment 3
A kind of aluminum alloy materials, comprises the raw material of following component:
5 parts, manganese, titanium 4 parts, 8 parts, magnesium, chromium 6 parts, bismuth 6 parts, niobium 3 parts, 3 parts, strontium, barium 6 parts, 7 parts, nickel, iron 16 parts, copper 13 parts, 42 parts, aluminium.
Although above-mentioned, the specific embodiment of the present invention is described; but not limiting the scope of the invention; one of ordinary skill in the art should be understood that; on the basis of technical scheme of the present invention, those skilled in the art do not need to pay various amendment or distortion that creative work can make still within protection scope of the present invention.
Claims (2)
1. an aluminum alloy materials, is characterized in that: the raw material comprising following component:
Manganese 3-5 part, titanium 2-4 part, magnesium 6-8 part, chromium 4-6 part, bismuth 3-6 part, niobium 1-3 part, strontium 2-3 part, barium 5-6 part, nickel 4-7 part, iron 12-16 part, copper 8-13 part, aluminium 35-42 part.
2. aluminum alloy materials according to claim 1, is characterized in that: the raw material comprising following component:
4 parts, manganese, titanium 3 parts, 7 parts, magnesium, chromium 5 parts, bismuth 5 parts, niobium 2 parts, 2.6 parts, strontium, barium 5.5 parts, 6 parts, nickel, iron 14 parts, copper 11 parts, 39 parts, aluminium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510935182.6A CN105543626A (en) | 2015-12-15 | 2015-12-15 | Aluminum alloy material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510935182.6A CN105543626A (en) | 2015-12-15 | 2015-12-15 | Aluminum alloy material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105543626A true CN105543626A (en) | 2016-05-04 |
Family
ID=55823179
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510935182.6A Pending CN105543626A (en) | 2015-12-15 | 2015-12-15 | Aluminum alloy material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105543626A (en) |
-
2015
- 2015-12-15 CN CN201510935182.6A patent/CN105543626A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160504 |