CN104060139A - High-functional magnesium alloy - Google Patents
High-functional magnesium alloy Download PDFInfo
- Publication number
- CN104060139A CN104060139A CN201410306431.0A CN201410306431A CN104060139A CN 104060139 A CN104060139 A CN 104060139A CN 201410306431 A CN201410306431 A CN 201410306431A CN 104060139 A CN104060139 A CN 104060139A
- Authority
- CN
- China
- Prior art keywords
- accounts
- magnesium alloy
- magnesium
- thorium
- cadmium
- 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
Links
Landscapes
- Manufacture And Refinement Of Metals (AREA)
Abstract
The invention discloses a high-functional magnesium alloy which is composed of six metal components, namely magnesium, cerium, thorium, zinc, manganese and cadmium. The high-functional magnesium alloy comprises, by weight, 84.4-89.3 percent of magnesium, 2.5-3.4 percent of cerium, 2.1-3.2 percent of thorium, 3.6-4.5 percent of zinc, 1.7-2.6 percent of magnesium and 0.8-1.9 percent of cadmium. According to the high-functional magnesium alloy, the five metal elements, namely the cerium, the thorium, the zinc, the manganese and the cadmium are added into the magnesium alloy with the manganese as the radical. The high-functional magnesium alloy has the advantages of being high in strength, large in elasticity modulus, good in heat dissipation and shock absorption performance, large in impulse load bearing capacity and good in chemical corrosion resistance performance.
Description
Technical field
The present invention relates to a kind of alloy, be specifically related to a kind of high function magnesium alloy.
Background technology
Magnesium alloy is to take magnesium to add other elementary composition alloys as base.Be mainly used in the industrial sectors such as Aeronautics and Astronautics, transportation, chemical industry, rocket.Magnesium is the lightest metal in practical metal, and the proportion of magnesium is approximately 2/3 of aluminium, is 1/4 of iron.It is the lightest metal in practical metal, high strength, high rigidity.Along with the constant growth of productivity, the user demand of industrial magnesium alloy improves constantly, and existing magnesium alloy cannot meet the user demand in market gradually.
Summary of the invention
The object of the present invention is to provide that a kind of intensity is high, Young's modulus is large, good heat dissipation, shock absorbing is good, the loading capacity that withstands shocks is large, resistance to chemical corrosion is good high function magnesium alloy.
Technical scheme of the present invention is, a kind of high function magnesium alloy, described high function magnesium alloy is combined by magnesium, cerium, thorium, zinc, manganese and six kinds of metal ingredients of cadmium, in described high function magnesium alloy, the shared weight percent of each composition is respectively: described magnesium accounts for 84.4%-89.3%, described cerium accounts for 2.5%-3.4%, and described thorium accounts for 2.1%-3.2%, and described zinc accounts for 3.6%-4.5%, described manganese accounts for 1.7%-2.6%, and described cadmium accounts for 0.8%-1.9%.
In a preferred embodiment of the present invention, in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 88.8%, and described cerium accounts for 2.6%, described thorium accounts for 2.2%, described zinc accounts for 3.7%, and described manganese accounts for 1.8%, and described cadmium accounts for 0.9%.
In a preferred embodiment of the present invention, in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 84.9%, and described cerium accounts for 3.3%, described thorium accounts for 3.1%, described zinc accounts for 4.4%, and described manganese accounts for 2.5%, and described cadmium accounts for 1.8%.
Of the present invention is a kind of high function magnesium alloy, by adding five kinds of metallic elements such as cerium, thorium, zinc, manganese and cadmium in the Magnuminium that magnesium is base and form take, have that intensity is high, Young's modulus large, a good heat dissipation, shock absorbing is good, the loading capacity that withstands shocks is large, resistance to chemical corrosion is good feature.
Embodiment
Below preferred embodiment of the present invention is described in detail, thereby so that advantages and features of the invention can be easier to be it will be appreciated by those skilled in the art that, protection scope of the present invention is made to more explicit defining.
Of the present invention is a kind of high function magnesium alloy, described high function magnesium alloy is combined by magnesium, cerium, thorium, zinc, manganese and six kinds of metal ingredients of cadmium, in described high function magnesium alloy, the shared weight percent of each composition is respectively: described magnesium accounts for 84.4%-89.3%, described cerium accounts for 2.5%-3.4%, described thorium accounts for 2.1%-3.2%, described zinc accounts for 3.6%-4.5%, and described manganese accounts for 1.7%-2.6%, and described cadmium accounts for 0.8%-1.9%.
Further, in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 88.8%, and described cerium accounts for 2.6%, and described thorium accounts for 2.2%, and described zinc accounts for 3.7%, and described manganese accounts for 1.8%, and described cadmium accounts for 0.9%.
Further, in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 84.9%, and described cerium accounts for 3.3%, and described thorium accounts for 3.1%, and described zinc accounts for 4.4%, and described manganese accounts for 2.5%, and described cadmium accounts for 1.8%.
In addition, can, by regulating the Different Weight per-cent of each composition in alloy, the alloy property obtaining just be differed.
Of the present invention is a kind of high function magnesium alloy, by adding five kinds of metallic elements such as cerium, thorium, zinc, manganese and cadmium in the Magnuminium that magnesium is base and form take, have that intensity is high, Young's modulus large, a good heat dissipation, shock absorbing is good, the loading capacity that withstands shocks is large, resistance to chemical corrosion is good feature.
The foregoing is only the specific embodiment of the present invention; but protection scope of the present invention is not limited to this; any those of ordinary skill in the art are in the disclosed technical scope of the present invention; the variation that can expect without creative work or replacement, within all should being encompassed in protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain that claims were limited.
Claims (3)
1. one kind high function magnesium alloy, it is characterized in that: described high function magnesium alloy is combined by magnesium, cerium, thorium, zinc, manganese and six kinds of metal ingredients of cadmium, in described high function magnesium alloy, the shared weight percent of each composition is respectively: described magnesium accounts for 84.4%-89.3%, described cerium accounts for 2.5%-3.4%, described thorium accounts for 2.1%-3.2%, described zinc accounts for 3.6%-4.5%, and described manganese accounts for 1.7%-2.6%, and described cadmium accounts for 0.8%-1.9%.
2. high function magnesium alloy according to claim 1, it is characterized in that: in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 88.8%, described cerium accounts for 2.6%, described thorium accounts for 2.2%, described zinc accounts for 3.7%, described manganese accounts for 1.8%, and described cadmium accounts for 0.9%.
3. high function magnesium alloy according to claim 1, it is characterized in that: in described high function magnesium alloy, the shared weight percent of each composition is specially: described magnesium accounts for 84.9%, described cerium accounts for 3.3%, described thorium accounts for 3.1%, described zinc accounts for 4.4%, described manganese accounts for 2.5%, and described cadmium accounts for 1.8%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410306431.0A CN104060139A (en) | 2014-07-01 | 2014-07-01 | High-functional magnesium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410306431.0A CN104060139A (en) | 2014-07-01 | 2014-07-01 | High-functional magnesium alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104060139A true CN104060139A (en) | 2014-09-24 |
Family
ID=51548068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410306431.0A Pending CN104060139A (en) | 2014-07-01 | 2014-07-01 | High-functional magnesium alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104060139A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104532029A (en) * | 2014-12-15 | 2015-04-22 | 镁联科技（芜湖）有限公司 | High-tenacity magnesium alloy as well as preparation and application of high-tenacity magnesium alloy |
| CN104561712A (en) * | 2014-12-15 | 2015-04-29 | 镁联科技（芜湖）有限公司 | Creep-resistant magnesium alloy as well as preparation method and application thereof |
| CN106498249A (en) * | 2016-11-29 | 2017-03-15 | 常熟市张桥华丰铸造五金厂 | A kind of shock resistance high-performance foundry goods |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1675395A (en) * | 2002-06-21 | 2005-09-28 | 铸造中心有限公司 | Creep resistant magnesium alloy |
| EP1816224A1 (en) * | 2004-09-30 | 2007-08-08 | KAWAMURA, Yoshihito | High-strength and high-toughness metal and process for producing the same |
| CN101985729A (en) * | 2010-11-18 | 2011-03-16 | 重庆大学 | Method for refining crystal grains of magnesium alloy plate |
| CN103316915A (en) * | 2013-06-24 | 2013-09-25 | 东北大学 | Method for preparing wide magnesium alloy sheet |
-
2014
- 2014-07-01 CN CN201410306431.0A patent/CN104060139A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1675395A (en) * | 2002-06-21 | 2005-09-28 | 铸造中心有限公司 | Creep resistant magnesium alloy |
| EP1816224A1 (en) * | 2004-09-30 | 2007-08-08 | KAWAMURA, Yoshihito | High-strength and high-toughness metal and process for producing the same |
| CN101985729A (en) * | 2010-11-18 | 2011-03-16 | 重庆大学 | Method for refining crystal grains of magnesium alloy plate |
| CN103316915A (en) * | 2013-06-24 | 2013-09-25 | 东北大学 | Method for preparing wide magnesium alloy sheet |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104532029A (en) * | 2014-12-15 | 2015-04-22 | 镁联科技（芜湖）有限公司 | High-tenacity magnesium alloy as well as preparation and application of high-tenacity magnesium alloy |
| CN104561712A (en) * | 2014-12-15 | 2015-04-29 | 镁联科技（芜湖）有限公司 | Creep-resistant magnesium alloy as well as preparation method and application thereof |
| CN106498249A (en) * | 2016-11-29 | 2017-03-15 | 常熟市张桥华丰铸造五金厂 | A kind of shock resistance high-performance foundry goods |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP2015528856A5 (en) | ||
| CN104060139A (en) | High-functional magnesium alloy | |
| CN102965555B (en) | Corrosion-resistant magnesium alloy and preparation method thereof | |
| CN103572117A (en) | High-strength aluminum alloy with high corrosion resistance and weldability | |
| CN104046897A (en) | High-strength special steel alloy | |
| CN104046873A (en) | Deforming magnesium alloy for aviation | |
| CN103572120A (en) | Aluminum magnesium silicon alloy | |
| CN103526089A (en) | Hard aluminum alloy metal tube | |
| CN105986143A (en) | High-thermal conductivity titanium alloy | |
| CN104046856B (en) | A kind of aluminum bronze magnesium system duralumin | |
| CN103643090A (en) | Wear resistant silicon, magnesium and aluminum alloy | |
| CN107287467A (en) | A kind of corrosion-resistant low temperature resistant copper-iron alloy reservoir | |
| CN103667821A (en) | Starter aluminum alloy shell | |
| CN103572092B (en) | A kind of formula of composite tin-aluminum alloy metal | |
| CN107245608A (en) | A kind of bicycle use aluminium alloy | |
| CN103320662A (en) | High-performance magnesium alloy sheet material | |
| CN104060130A (en) | Lithium aluminum alloy used for aviation | |
| CN104057212A (en) | High-performance silver-based solder | |
| WO2018112018A3 (en) | Corrosion resistant aluminum alloy | |
| CN102876955A (en) | Aluminum alloy with high thermal conductivity | |
| CN103320661A (en) | Aluminum alloy sheet material | |
| CN107245610A (en) | A kind of high-strength aluminum alloy material | |
| CN104032218A (en) | Metal alloy easy to passivate | |
| CN107160769A (en) | A kind of Environment-friendlycorrosion-resistant corrosion-resistant clad steel | |
| CN104278182A (en) | Magnesium alloy and preparation method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140924 |