CN109706369A - A kind of magnesium alloy - Google Patents

A kind of magnesium alloy Download PDF

Info

Publication number
CN109706369A
CN109706369A CN201711017188.0A CN201711017188A CN109706369A CN 109706369 A CN109706369 A CN 109706369A CN 201711017188 A CN201711017188 A CN 201711017188A CN 109706369 A CN109706369 A CN 109706369A
Authority
CN
China
Prior art keywords
parts
magnesium alloy
alloy
ratio
magnesium
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
CN201711017188.0A
Other languages
Chinese (zh)
Inventor
侯光勇
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.)
Zunyi Auspicious Fukang Doors And Windows Co Ltd
Original Assignee
Zunyi Auspicious Fukang Doors And Windows 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 Zunyi Auspicious Fukang Doors And Windows Co Ltd filed Critical Zunyi Auspicious Fukang Doors And Windows Co Ltd
Priority to CN201711017188.0A priority Critical patent/CN109706369A/en
Publication of CN109706369A publication Critical patent/CN109706369A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses a kind of magnesium alloys, according to poidometer, it is made of Mg:18~36 part, Al:18~36 part, Si:6~12 part, Fe:6~12 part, Cu:2~4 part, Mn:0.1~0.3 part, Cr:0.1~0.3 part, Zn:0.1~0.3 part, Ti:0.1~0.3 part and Zr:0.1~0.3 part.The present invention in aluminium alloy by adding Si, Fe, Cu, Mn, Cr, Zn, Ti and Zr, crystal grain can be refined, improve the tensile property of magnesium alloy, improve magnesium alloy creep ability, also it can improve casting character, and the corrosion resistance and wear-resisting property of alloy can be improved, magnesium alloy produced by the invention has many advantages, such as that tensile strength is high, hardness is high, corrosion resistance is strong and wear-resisting property is good.

Description

A kind of magnesium alloy
Technical field
The present invention relates to a kind of magnesium alloys, belong to technical field of alloy.
Background technique
Magnesium alloy aluminium sheet essential element is aluminium, then mixes a small amount of magnesium or other metal materials to reinforce it firmly Degree.Using Mg as the aluminium alloy of main adding elements, since its corrosion stability is good, also known as rust-preventing aluminum alloy.Cause inherently metal, Its heating conduction and intensity are especially prominent.Magnesium-aluminum alloy plate matter heavily fortified point amount is light, density is low, thermal diffusivity is preferable, crushing resistance is stronger, can fill Point meet electronic product Highgrade integration, lightening, micromation, drop resistant hit the requirement of electromagnetic shielding and heat dissipation.Its hardness is The several times of conventional plastic casing, but weight is only the one third of the latter.But it is closed using the magnalium that conventional method processes Gold, due to being limited by material and processing method, the defects of being easy to appear fracture, wrinkle, fatigue in process, finished product Rate is lower, results in the waste of material.Meanwhile production efficiency is lower, increases labor intensity, increases production cost.
Summary of the invention
The object of the present invention is to provide a kind of magnesium alloys.The magnesium alloy has tensile strength height, hardness high, resistance to The advantages that corrosivity is strong and wear-resisting property is good
Technical solution of the present invention: a kind of magnesium alloy, according to poidometer, by Mg:18~36 part, Al:18~36 part, Si:6~ 12 parts, Fe:6~12 part, Cu:2~4 part, Mn:0.1~0.3 part, Cr:0.1~0.3 part, Zn: 0.1~0.3 part, Ti:0.1~ 0.3 part and Zr:0.1~0.3 part composition.
Magnesium alloy above-mentioned, according to poidometer, by Mg:27 parts, Al:27 parts, Si:9 parts, Fe:9 parts, Cu:3 parts, Mn: 0.2 part, Cr:0.2 parts, Zn:0.2 parts, Ti:0.2 parts and Zr:0.2 parts composition.
Magnesium alloy above-mentioned, the Mg and Al are mixed according to the ratio of 1:1.
Magnesium alloy above-mentioned, described Si, Fe and Cu are mixed according to the ratio of 3:3:1.
Magnesium alloy above-mentioned, described Mn, Cr, Zn, Ti and Zr are mixed according to the ratio of 1:1:1:1:1.
Beneficial effects of the present invention: compared with prior art, magnesium alloy of the invention has the advantage that
The present invention can refine crystal grain, improve magnesium alloy by adding Si, Fe, Cu, Mn, Cr, Zn, Ti and Zr in aluminium alloy Tensile property, improve magnesium alloy creep ability, can also improve casting character, and can be improved alloy corrosion resistance and Wear-resisting property, magnesium alloy produced by the invention have tensile strength is high, hardness is high, corrosion resistance is strong and wear-resisting property is good etc. Advantage.
Specific embodiment
The embodiment of the present invention 1.
A kind of magnesium alloy, according to poidometer, by Mg:18~36 part, Al:18~36 part, Si:6~12 part, Fe:6~12 Part, Cu:2~4 part, Mn:0.1~0.3 part, Cr:0.1~0.3 part, Zn: 0.1~0.3 part, Ti:0.1~0.3 part and Zr:0.1 ~0.3 part of composition.
The magnesium alloy, according to poidometer, by Mg:27 parts, Al:27 parts, Si:9 parts, Fe:9 parts, Cu:3 parts, Mn: 0.2 part, Cr:0.2 parts, Zn:0.2 parts, Ti:0.2 parts and Zr:0.2 parts composition.
The Mg and Al is mixed according to the ratio of 1:1.
Described Si, Fe and Cu are mixed according to the ratio of 3:3:1.
Described Mn, Cr, Zn, Ti and Zr are mixed according to the ratio of 1:1:1:1:1.
The embodiment of the present invention 2.
A kind of magnesium alloy, according to poidometer, by Mg:18 parts, Al:18 parts, Si:6 parts, Fe:6 parts, Cu:2 parts, Mn:0.1 Part, Cr:0.1 parts, Zn: 0.1 part, Ti:0.1 parts and Zr:0.1 parts of compositions.
The Mg and Al is mixed according to the ratio of 1:1.
Described Si, Fe and Cu are mixed according to the ratio of 3:3:1.
Described Mn, Cr, Zn, Ti and Zr are mixed according to the ratio of 1:1:1:1:1.
The embodiment of the present invention 3.
A kind of magnesium alloy, according to poidometer, by Mg:36 parts, Al:36 parts, Si:12 parts, Fe:12 parts, Cu:4 parts, Mn:0.3 parts, Cr:0.3 parts, Zn: 0.3 part, Ti:0.3 parts and Zr:0.3 parts compositions.
The Mg and Al is mixed according to the ratio of 1:1.
Described Si, Fe and Cu are mixed according to the ratio of 3:3:1.
Described Mn, Cr, Zn, Ti and Zr are mixed according to the ratio of 1:1:1:1:1.

Claims (5)

1. a kind of magnesium alloy, it is characterised in that: according to poidometer, by Mg:18~36 part, Al:18~36 part, Si:6~12 Part, Fe:6~12 part, Cu:2~4 part, Mn:0.1~0.3 part, Cr:0.1~0.3 part, Zn: 0.1~0.3 part, Ti:0.1~ 0.3 part and Zr:0.1~0.3 part composition.
2. magnesium alloy according to claim 1, it is characterised in that: according to poidometer, by Mg:27 parts, Al:27 parts, Si: 9 parts, Fe:9 parts, Cu:3 parts, Mn:0.2 parts, Cr:0.2 parts, Zn:0.2 parts, Ti:0.2 parts and Zr:0.2 parts compositions.
3. magnesium alloy according to claim 1 or 2, it is characterised in that: the Mg and Al is mixed according to the ratio of 1:1.
4. magnesium alloy according to claim 1 or 2, it is characterised in that: described Si, Fe and Cu according to 3:3:1 ratio Mixing.
5. magnesium alloy according to claim 1 or 2, it is characterised in that: described Mn, Cr, Zn, Ti and Zr are according to 1:1:1: The ratio of 1:1 mixes.
CN201711017188.0A 2017-10-26 2017-10-26 A kind of magnesium alloy Pending CN109706369A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711017188.0A CN109706369A (en) 2017-10-26 2017-10-26 A kind of magnesium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711017188.0A CN109706369A (en) 2017-10-26 2017-10-26 A kind of magnesium alloy

Publications (1)

Publication Number Publication Date
CN109706369A true CN109706369A (en) 2019-05-03

Family

ID=66253498

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711017188.0A Pending CN109706369A (en) 2017-10-26 2017-10-26 A kind of magnesium alloy

Country Status (1)

Country Link
CN (1) CN109706369A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103643090A (en) * 2013-11-25 2014-03-19 简玉君 Wear resistant silicon, magnesium and aluminum alloy
CN105970072A (en) * 2016-07-15 2016-09-28 南通纺都置业有限公司 Aluminum alloy
CN106048379A (en) * 2016-07-14 2016-10-26 南通中兴多元复合钢管有限公司 Aluminum alloy

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103643090A (en) * 2013-11-25 2014-03-19 简玉君 Wear resistant silicon, magnesium and aluminum alloy
CN106048379A (en) * 2016-07-14 2016-10-26 南通中兴多元复合钢管有限公司 Aluminum alloy
CN105970072A (en) * 2016-07-15 2016-09-28 南通纺都置业有限公司 Aluminum alloy

Similar Documents

Publication Publication Date Title
Nasiri et al. Microstructure and tensile properties of cast Al–15% Mg2Si composite: Effects of phosphorous addition and heat treatment
CN103343268B (en) A kind of pack alloy
CN104313403B (en) A kind of aluminium alloy with high intensity excellent chip performance and preparation method thereof
CN101979692B (en) Preparation process of Al-Zn-Mg-Cu aluminum alloy with ultra-high strength
CN111155007B (en) Preparation method of high-strength 2000 series aluminum alloy based on selective laser melting forming technology
Nasiri et al. Microstructural evolution and tensile properties of the in situ Al–15% Mg2Si composite with extra Si contents
CN106399781A (en) Novel high-strength corrosion-resistant rare earth aluminum alloy material and preparation method
CN105200277A (en) Aluminum alloy and manufacturing method thereof
CN102002617B (en) Cast aluminum alloy for automobile and preparation method thereof
CN106011565B (en) A kind of aluminum alloy materials and its production technology
CN101876018A (en) High-strength casting aluminium-silicon alloy for piston and preparation method thereof
CN105200284A (en) Magnesium-aluminum alloy
CN102644013A (en) High-strength and high-elongation cast magnesium alloy and production method thereof
CN104195365B (en) Low-lead brass alloy and preparing method thereof
CN109706369A (en) A kind of magnesium alloy
CN103409673A (en) High-strength die-cast aluminum-titanium alloy
CN102925776A (en) High-strength and high-toughness magnesium alloy
CN106086545A (en) A kind of aluminium alloy and preparation method thereof
Rao et al. Effect of particle size on mechanical properties of al-rmp metal matrix composites
CN105734337A (en) Wearing-resistant cooper alloy mold material
CN105463264A (en) Aluminum-magnesium alloy and preparation method thereof
CN105420558A (en) Aluminum alloy sheet
CN105331866B (en) Enhanced AZ91 magnesium alloys of a kind of Mg Zn Gd quasi-crystalline substances and preparation method thereof
CN105728567A (en) High-strength stamping die
CN103966494A (en) Highly heat-resistant magnalium containing calcium and rare earth

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190503