CN106801167A - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- CN106801167A CN106801167A CN201510830072.3A CN201510830072A CN106801167A CN 106801167 A CN106801167 A CN 106801167A CN 201510830072 A CN201510830072 A CN 201510830072A CN 106801167 A CN106801167 A CN 106801167A
- Authority
- CN
- China
- Prior art keywords
- aluminium alloy
- weight
- tin
- aluminium
- silicon
- 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.)
- Pending
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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
- C22C21/003—Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
-
- 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 provides a kind of aluminium alloy, and step one, its each group percentage by weight is as follows, silicon：0.5-1, tin：3-3.5, copper：0.5-1, zinc：2-3, chromium 1-2, remaining is aluminium and a small amount of unavoidable impurity, and each component is matched；Step 2, the raw material of step one is sufficiently stirred for；Step 3, carries out cast bar in die casting machine.Thermal conductivity of the present invention, intensity are preferable, long service life.
Description
Technical field
The present invention relates to a kind of aluminium alloy.
Background technology
Aluminium alloy is most widely used class non-ferrous metal structural material in industry, aviation,
Widely applied in space flight, automobile, machine-building, ship and chemical industry.Industrial economy
Develop rapidly, the demand to Welded structural member is increasing, the weldability for enabling aluminum alloy to
Research is also goed deep into therewith.Existing aluminium alloy thermal conductivity, intensity are poor.
The content of the invention
(1) technical problem to be solved
The problem to be solved in the present invention is to provide a kind of aluminium alloy, to overcome heat conduction in the prior art
The poor defect of property, intensity.
(2) technical scheme
To solve the technical problem, the present invention provides a kind of aluminium alloy, step one, its each group
Percentage by weight is as follows, silicon：0.5-1, tin：3-3.5, copper：0.5-1, zinc：2-3, chromium 1-2,
Remaining is aluminium and a small amount of unavoidable impurity, and each component is matched；Step 2, will walk
Rapid one raw material is sufficiently stirred for；Step 3, carries out cast bar in die casting machine.
Further, the silicon percentage by weight is 0.8.
Further, the tin percentage by weight is 3.2.
(3) beneficial effect
Aluminium alloy of the invention, thermal conductivity, intensity are preferable, long service life.
Specific embodiment
With reference to embodiment, specific embodiment of the invention is described in further detail.
Following examples are used to illustrate the present invention, but are not limited to the scope of the present invention.
A kind of aluminium alloy of the invention, step one, its each group percentage by weight is as follows, silicon：0.5-1,
Tin：3-3.5, copper：0.5-1, zinc：2-3, chromium 1-2, remaining is aluminium and a small amount of unavoidable
Impurity, each component is matched；Step 2, the raw material of step one is sufficiently stirred for；
Step 3, carries out cast bar in die casting machine.
The present embodiment is preferred：The silicon percentage by weight is 0.8；The tin percentage by weight is
3.2；Weight of copper percentage is 0.6, and zinc percentage by weight is 2.5, and weight of chromium percentage is 1.5.
Aluminium alloy of the invention, thermal conductivity, intensity are preferable, long service life.
In sum, above-mentioned implementation method is not restricted implementation method of the invention, all
Modification or wait that the technical staff in field is carried out on the basis of substance of the invention
Effect deformation, in technology category of the invention.
Claims (3)
1. a kind of aluminium alloy, it is characterised in that step one, its each group percentage by weight is as follows,
Silicon：0.5-1, tin：3-3.5, copper：0.5-1, zinc：2-3, chromium 1-2, remaining is for aluminium and on a small quantity
Unavoidable impurity, each component is matched；Step 2, the raw material of step one is carried out
It is sufficiently stirred for；Step 3, carries out cast bar in die casting machine.
2. aluminium alloy according to claim 1, it is characterised in that：The silicon weight hundred
Divide than being 0.8.
3. aluminium alloy according to claim 1, it is characterised in that：The tin weight hundred
Divide than being 3.2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510830072.3A CN106801167A (en) | 2015-11-25 | 2015-11-25 | Aluminium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510830072.3A CN106801167A (en) | 2015-11-25 | 2015-11-25 | Aluminium alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106801167A true CN106801167A (en) | 2017-06-06 |
Family
ID=58975777
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510830072.3A Pending CN106801167A (en) | 2015-11-25 | 2015-11-25 | Aluminium alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106801167A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109881057A (en) * | 2019-03-08 | 2019-06-14 | 安徽信息工程学院 | A kind of high-strength and high ductility material and preparation method thereof |
-
2015
- 2015-11-25 CN CN201510830072.3A patent/CN106801167A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109881057A (en) * | 2019-03-08 | 2019-06-14 | 安徽信息工程学院 | A kind of high-strength and high ductility material and preparation method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170606 |
|
| WD01 | Invention patent application deemed withdrawn after publication |