CN105401017A - Magnalium alloy material - Google Patents

Magnalium alloy material Download PDF

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Publication number
CN105401017A
CN105401017A CN201510773601.0A CN201510773601A CN105401017A CN 105401017 A CN105401017 A CN 105401017A CN 201510773601 A CN201510773601 A CN 201510773601A CN 105401017 A CN105401017 A CN 105401017A
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CN
China
Prior art keywords
alloy material
magnesium
aluminium alloy
aluminium
weight percent
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
CN201510773601.0A
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Chinese (zh)
Inventor
张忍
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.)
Taicang Wangmei Mold Co Ltd
Original Assignee
Taicang Wangmei Mold 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 Taicang Wangmei Mold Co Ltd filed Critical Taicang Wangmei Mold Co Ltd
Priority to CN201510773601.0A priority Critical patent/CN105401017A/en
Publication of CN105401017A publication Critical patent/CN105401017A/en
Pending legal-status Critical Current

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Abstract

The invention provides a magnalium alloy material. The magnalium alloy material comprises, by weight, 10%-25% of magnesium, 1.5%-3% of silicon, 0.3%-1% of manganese, 0.01%-0.1% of copper, 0.03%-0.35% of titanium, 0.05%-0.4% of zinc, 0.005%-0.04% of carbon, 0.005%-0.035% of iron, and the balance aluminum and few impurities. The magnalium alloy material has excellent mechanical strength and toughness, and meanwhile the defects such as breakage, wrinkles and fatigue are avoided in the machining process; in addition, the preparation method is easy, the production efficiency is improved, the labor intensity and the production cost are reduced, and the service life of the material is prolonged.

Description

A kind of magnesium-aluminium alloy material
Technical field
The present invention relates to technical field of metal, be specifically related to a kind of magnesium-aluminium alloy material.
Background technology
Aluminium alloy is a most widely used class non-ferrous metal structured material in industry, and the density of fine aluminium is little, and be only 1/3 of iron, fusing point is low.Aluminium is face-centred cubic structure, has very high plasticity, and be easy to processing, can be made into various section bar, sheet material, corrosion resistance is good; But the intensity of fine aluminium is very low, structured material should not be made.The damping performance that magnesium-aluminium alloy material has light weight, hard, corrosion resistance nature is strong, thermal diffusivity is good and good, is widely used in various industry in recent years, as cell phone, removable computer, automobile etc.Particularly in field of mobile phones; the application of magnesium-aluminium alloy material not only can increase metal-like; improve Consumer's Experience effect; simultaneously along with the development trend of mobile phone giant-screen; need the center of a high strength to protect large-sized touch-control display panel, avoid touch-control display panel shaking or easy cracked malfunctioning problem in slightly falling.
Magnalium traditional at present, due to the restriction of material, in the course of processing, easily occur the defects such as fracture, wrinkle, fatigue, yield rate is lower, result in the waste of material.Meanwhile, production efficiency is lower, adds labour intensity, adds production cost.
Therefore, for the problems referred to above, the present invention proposes a kind of new technical scheme.
Summary of the invention
The object of this invention is to provide and a kind of there is excellent wear resistance, the magnesium-aluminium alloy material of ductility.
The present invention is achieved through the following technical solutions:
A kind of magnesium-aluminium alloy material, comprises the raw material composition of following weight percent content:
Magnesium 10% ~ 25%;
Silicon 1.5% ~ 3%;
Manganese 0.3% ~ 1%;
Copper 0.01% ~ 0.1%;
Titanium 0.03% ~ 0.35%;
Zinc 0.05% ~ 0.4%;
Carbon 0.005% ~ 0.04%;
Iron 0.005% ~ 0.035%;
Surplus is aluminium and a small amount of impurity.
A kind of magnesium-aluminium alloy material, comprises the raw material composition of following weight percent content:
Magnesium 12% ~ 25%;
Silicon 1.5% ~ 2.5%;
Manganese 0.4% ~ 1%;
Copper 0.025% ~ 0.1%;
Titanium 0.05% ~ 0.3%;
Zinc 0.05% ~ 0.25%;
Carbon 0.005% ~ 0.04%;
Iron 0.01% ~ 0.035%;
Surplus is aluminium and a small amount of impurity.
Further, the molybdenum that weight percent is 0.05% ~ 0.25% is also comprised.
Further, the scandium that weight percent is 0.03% ~ 0.4% is also comprised.
The invention has the beneficial effects as follows: magnalium proposed by the invention has excellent physical strength, and toughness is high, simultaneously, avoid occurring the defects such as fracture, wrinkle, fatigue in the course of processing, and preparation method is simple, improve production efficiency, reduce labour intensity of knowing clearly, reduce production cost, improve the work-ing life of material.
Embodiment
Below in conjunction with embodiment, the present invention is described further.
Embodiment 1
A kind of magnesium-aluminium alloy material, comprises the raw material composition of following weight percent content:
Magnesium 10%;
Silicon 1.5%;
Manganese 0.3%;
Copper 0.01%;
Titanium 0.03%;
Zinc 0.05%;
Carbon 0.005%;
Iron 0.005%;
Molybdenum 0.05%;
Scandium 0.03%;
Surplus is aluminium and a small amount of impurity.
Embodiment 2
A kind of magnesium-aluminium alloy material, comprises the raw material composition of following weight percent content:
Magnesium 15%;
Silicon 2%;
Manganese 0.5%;
Copper 0.045%;
Titanium 0.12%;
Zinc 0.25%;
Carbon 0.025%;
Iron 0.01%;
Molybdenum 0.1%;
Scandium 0.25%;
Surplus is aluminium and a small amount of impurity.
Embodiment 3
A kind of magnesium-aluminium alloy material, comprises the raw material composition of following weight percent content:
Magnesium 25%;
Silicon 3%;
Manganese 1%;
Copper 0.1%;
Titanium 0.35%;
Zinc 0.4%;
Carbon 0.04%;
Iron 0.035%;
Molybdenum 0.25%;
Scandium 0.4%;
Surplus is aluminium and a small amount of impurity.
Magnalium proposed by the invention has excellent physical strength, and toughness is high, simultaneously, avoid occurring the defects such as fracture, wrinkle, fatigue in the course of processing, and preparation method is simple, improve production efficiency, reduce labour intensity of knowing clearly, reduce production cost, improve the work-ing life of material.
The above is only embodiments of the invention, is not restriction the present invention being made to any other form, and any amendment done according to embodiment proposed by the invention or equivalent variations, still belong to the present invention's scope required for protection.

Claims (4)

1. a magnesium-aluminium alloy material, is characterized in that: the raw material composition comprising following weight percent content:
Magnesium 10% ~ 25%;
Silicon 1.5% ~ 3%;
Manganese 0.3% ~ 1%;
Copper 0.01% ~ 0.1%;
Titanium 0.03% ~ 0.35%;
Zinc 0.05% ~ 0.4%;
Carbon 0.005% ~ 0.04%;
Iron 0.005% ~ 0.035%;
Surplus is aluminium and a small amount of impurity.
2. according to claim 1 magnesium-aluminium alloy material, it is characterized in that: the raw material composition comprising following weight percent content:
Magnesium 12% ~ 25%;
Silicon 1.5% ~ 2.5%;
Manganese 0.4% ~ 1%;
Copper 0.025% ~ 0.1%;
Titanium 0.05% ~ 0.3%;
Zinc 0.05% ~ 0.25%;
Carbon 0.005% ~ 0.04%;
Iron 0.01% ~ 0.035%;
Surplus is aluminium and a small amount of impurity.
3. a kind of magnesium-aluminium alloy material according to claim 1, is characterized in that: also comprise the molybdenum that weight percent is 0.05% ~ 0.25%.
4. a kind of magnesium-aluminium alloy material according to claim 1, is characterized in that: also comprise the scandium that weight percent is 0.03% ~ 0.4%.
CN201510773601.0A 2015-11-13 2015-11-13 Magnalium alloy material Pending CN105401017A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510773601.0A CN105401017A (en) 2015-11-13 2015-11-13 Magnalium alloy material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510773601.0A CN105401017A (en) 2015-11-13 2015-11-13 Magnalium alloy material

Publications (1)

Publication Number Publication Date
CN105401017A true CN105401017A (en) 2016-03-16

Family

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Family Applications (1)

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CN201510773601.0A Pending CN105401017A (en) 2015-11-13 2015-11-13 Magnalium alloy material

Country Status (1)

Country Link
CN (1) CN105401017A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107955894A (en) * 2017-12-13 2018-04-24 苏州浩焱精密模具有限公司 A kind of mould high-strength aluminium-magnesium alloy material
CN108441746A (en) * 2018-06-04 2018-08-24 芜湖征途电子科技有限公司 A kind of unmanned plane magnesium alloy

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279915A (en) * 1962-10-15 1966-10-18 Honda Motor Co Ltd Hydroalium alloy for die-casting use
WO2011090451A1 (en) * 2010-01-21 2011-07-28 Tetiana Legka CASTING ALLOY OF THE AIMgSI TYPE
CN103103387A (en) * 2012-11-09 2013-05-15 安徽欣意电缆有限公司 Al-Fe-C-RE aluminium alloy, preparation method thereof and power cable
CN104451286A (en) * 2014-12-02 2015-03-25 绥阳县耐环铝业有限公司 Magnesium-aluminum alloy and processing technique thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279915A (en) * 1962-10-15 1966-10-18 Honda Motor Co Ltd Hydroalium alloy for die-casting use
WO2011090451A1 (en) * 2010-01-21 2011-07-28 Tetiana Legka CASTING ALLOY OF THE AIMgSI TYPE
CN103103387A (en) * 2012-11-09 2013-05-15 安徽欣意电缆有限公司 Al-Fe-C-RE aluminium alloy, preparation method thereof and power cable
CN104451286A (en) * 2014-12-02 2015-03-25 绥阳县耐环铝业有限公司 Magnesium-aluminum alloy and processing technique thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王祝堂,熊慧: "《轨道车辆用铝材手册》", 30 November 2013, 中南大学出版社 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107955894A (en) * 2017-12-13 2018-04-24 苏州浩焱精密模具有限公司 A kind of mould high-strength aluminium-magnesium alloy material
CN108441746A (en) * 2018-06-04 2018-08-24 芜湖征途电子科技有限公司 A kind of unmanned plane magnesium alloy

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