CN107779698A - Magnesium-aluminium alloy material - Google Patents

Magnesium-aluminium alloy material Download PDF

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Publication number
CN107779698A
CN107779698A CN201711386504.1A CN201711386504A CN107779698A CN 107779698 A CN107779698 A CN 107779698A CN 201711386504 A CN201711386504 A CN 201711386504A CN 107779698 A CN107779698 A CN 107779698A
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CN
China
Prior art keywords
magnesium
alloy material
aluminium alloy
aluminium
count
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
Application number
CN201711386504.1A
Other languages
Chinese (zh)
Inventor
李远发
黄永铨
刘建平
朱永权
曾祥胜
颜军鹏
张亚琴
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiayi Technology (huizhou) Co Ltd
Original Assignee
Jiayi Technology (huizhou) Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiayi Technology (huizhou) Co Ltd filed Critical Jiayi Technology (huizhou) Co Ltd
Priority to CN201711386504.1A priority Critical patent/CN107779698A/en
Publication of CN107779698A publication Critical patent/CN107779698A/en
Pending legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Prevention Of Electric Corrosion (AREA)

Abstract

The present invention relates to a kind of magnesium alloy.The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 55 58%, magnesium 30 38%, silicon 2 3%, manganese 1 1.5%, zirconium 0.5 1.5%;Most preferred group is divided into aluminium 56%, magnesium 38%, silicon 2%, manganese 1.5%, zirconium 0.5%, thorium 0.5%, silver 1.5%.The magnesium-aluminium alloy material is compared to aluminum alloy materials similar in corrosion resistance and tensile property, and quality is lighter, and application is more extensive.

Description

Magnesium-aluminium alloy material
Technical field
The present invention relates to a kind of magnesium-aluminium alloy material.
Background technology
The density of magnesium is smaller, but the corrosion resistance of magnesium is poor, it is impossible to is used separately as section bar, it is necessary to other metal systems Into alloy material, its effect of competence exertion.The alloy material made of magnesium is widely used with light famous.Magnesium alloy is exactly Wherein more common one kind, magnesium alloy have good intensity, rigidity and dimensional stability.Because application scenario is different, to magnesium The requirements such as the hardness of aluminium alloy, quality are then different.The present invention is intended to provide a kind of corrosion resistance and the excellent magnalium of tensile property Alloy material.
The content of the invention
To achieve the above object, the present invention provides a kind of magnesium-aluminium alloy material.
Technical scheme is as follows:Magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 55-58%, magnesium 30-38%, silicon 2-3%, manganese 1-1.5%, zirconium 0.5-1.5%.
Preferably, the magnesium-aluminium alloy material, thorium 0.25-0.5% is also contained count by weight percentage.
Preferably, the magnesium-aluminium alloy material, silver-colored 0.5-1.5% is also contained count by weight percentage.
Preferably, the magnesium-aluminium alloy material, count by weight percentage, including aluminium 56%, magnesium 38%, silicone content 2%, Manganese 1.5%, zirconium 0.5%, thorium 0.5%, silver 1.5%.
Compared with prior art, the beneficial effects of the present invention are:The magnesium-aluminium alloy material has well anticorrosive Property, while also there is extraordinary tensile property and die casting, convenient processing after shaping;Compared to corrosion resistance and stretching The aluminum alloy materials of similar nature, this magnesium-aluminium alloy material quality is lighter, and application is more extensive.
Embodiment
With reference to embodiment, the present invention is described in further detail, embodiment be only used for illustrate rather than Limit protection scope of the present invention.
Embodiment 1:
The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 56%, magnesium 38%, silicon 3%, manganese 1.5%, zirconium 1.5%.
Embodiment 2:
The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 58%, magnesium 38%, silicon 2%, manganese 1%, zirconium 1%.
Embodiment 3:
The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 58%, magnesium 35%, silicon 2.5%, manganese 1.5%, zirconium 1.5%, Thorium 0.5%, silver 1%.
Embodiment 4:
The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 55%, magnesium 38%, silicon 2%, manganese 1.5%, zirconium 1.5%, thorium 0.5%, silver 1.5%.
Embodiment 5:
The magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 57%, magnesium 36%, silicon 3%, manganese 1.5%, zirconium 1.5%, thorium 0.25%, silver 0.75%.
Embodiment 6:
The magnesium-aluminium alloy material, count by weight percentage, including aluminium 56%, magnesium 38%, silicone content 2%, manganese 1.5%, zirconium 0.5%, thorium 0.5%, silver 1.5%.
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, will not be described here.
Although description of this invention combination embodiments above is carried out, those skilled in the art Many replacements, modifications and variations can be carried out according to above-mentioned content, are obvious.Therefore, it is all such to substitute, change Enter and change to be included in the spirit and scope of appended claims.

Claims (4)

1. magnesium-aluminium alloy material, count by weight percentage, including:Aluminium 55-58%, magnesium 30-38%, silicon 2-3%, manganese 1-1.5%, zirconium 0.5-1.5%。
2. magnesium-aluminium alloy material according to claim 1, it is characterised in that also contain thorium count by weight percentage 0.25-0.5%。
3. magnesium-aluminium alloy material according to claim 2, it is characterised in that also contain silver-colored 0.5- count by weight percentage 1.5%。
4. magnesium-aluminium alloy material according to claim 3, it is characterised in that count by weight percentage, including aluminium 56%, Magnesium 38%, silicone content 2%, manganese 1.5%, zirconium 0.5%, thorium 0.5%, silver 1.5%.
CN201711386504.1A 2017-12-20 2017-12-20 Magnesium-aluminium alloy material Pending CN107779698A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711386504.1A CN107779698A (en) 2017-12-20 2017-12-20 Magnesium-aluminium alloy material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711386504.1A CN107779698A (en) 2017-12-20 2017-12-20 Magnesium-aluminium alloy material

Publications (1)

Publication Number Publication Date
CN107779698A true CN107779698A (en) 2018-03-09

Family

ID=61437292

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711386504.1A Pending CN107779698A (en) 2017-12-20 2017-12-20 Magnesium-aluminium alloy material

Country Status (1)

Country Link
CN (1) CN107779698A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108441730A (en) * 2018-06-04 2018-08-24 芜湖征途电子科技有限公司 A kind of magnesium-aluminium alloy material for unmanned plane
CN112795824A (en) * 2020-12-24 2021-05-14 昆山智盛精密铸造有限公司 Magnesium-aluminum alloy material and preparation process thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103589920A (en) * 2013-11-16 2014-02-19 袁辉 Magnesium aluminum alloy
CN105200284A (en) * 2015-09-18 2015-12-30 霍山县龙鑫金属制品有限公司 Magnesium-aluminum alloy
CN106636800A (en) * 2016-12-05 2017-05-10 东莞市欧比迪精密五金有限公司 Magnesium aluminum alloy material and processing technique thereof

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103589920A (en) * 2013-11-16 2014-02-19 袁辉 Magnesium aluminum alloy
CN105200284A (en) * 2015-09-18 2015-12-30 霍山县龙鑫金属制品有限公司 Magnesium-aluminum alloy
CN106636800A (en) * 2016-12-05 2017-05-10 东莞市欧比迪精密五金有限公司 Magnesium aluminum alloy material and processing technique thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108441730A (en) * 2018-06-04 2018-08-24 芜湖征途电子科技有限公司 A kind of magnesium-aluminium alloy material for unmanned plane
CN112795824A (en) * 2020-12-24 2021-05-14 昆山智盛精密铸造有限公司 Magnesium-aluminum alloy material and preparation process thereof

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Application publication date: 20180309