CN102296218A - High-strength heat-resistant magnalium alloy - Google Patents

High-strength heat-resistant magnalium alloy Download PDF

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Publication number
CN102296218A
CN102296218A CN2011102434425A CN201110243442A CN102296218A CN 102296218 A CN102296218 A CN 102296218A CN 2011102434425 A CN2011102434425 A CN 2011102434425A CN 201110243442 A CN201110243442 A CN 201110243442A CN 102296218 A CN102296218 A CN 102296218A
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China
Prior art keywords
alloy
manganese
strength heat
magnalium alloy
good
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CN2011102434425A
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Chinese (zh)
Inventor
谢利荣
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Wujiang Fine Workmanship and Aluminum Word Manufactory
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Wujiang Fine Workmanship and Aluminum Word Manufactory
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Priority to CN2011102434425A priority Critical patent/CN102296218A/en
Publication of CN102296218A publication Critical patent/CN102296218A/en
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Abstract

A high-strength heat-resistant magnalium alloy. The heat-resistant magnalium alloy comprises: by weight, 4.5 to 5.5% of copper, 0.5 to 1.0% of manganese, 0.1 to 0.5% of titanium, 0.15 to 0.25% of cadmium, 0.05 to 0.35% of vanadium, 0.1 to 0.5% of lithium, 0.1 to 0.5% of boron, 0.1 to 0.3% of iron, 0.05 to 0.15% of silicon, 0.01 to 0.05% of magnesium, 0.01 to 0.05% of zinc, 0.1 to 0.5% of manganese, 0.01 to 0.05% of tin, 0.15 to 0.55% of bismuth and the balance aluminum. The invention provides the high-strength heat-resistant magnalium alloy. A casting made of the high-strength heat-resistant magnalium alloy can be strengthened through heat treatment and after being quenched, the casting has the advantages of high strength, good plasticity and thermal properties, high corrosion resistance, good machinability, good casting properties and good weldability, wherein after long-term use, plasticity is better.

Description

The hot magnalium of high strength anti
Technical field
The present invention relates to a kind of high strength heat resistant magnalium.
Background technology
Aluminium is the practical metallic substance that is only second to iron, industrial being of wide application, because aluminium has characteristics such as in light weight, intensity height, as the purposes of structured material also enlarging, in order to improve the intensity of aluminium alloy, toughness, anticorrosion stress-resistant cracking performance and thermotolerance etc., need to add alloying elements, magnesium can improve the molten admittedly thermal treatment of X alloy and the intensity of the back alloy that quenches, and makes aluminium alloy at room temperature have higher intensity and extension performance, but can reduce tensile strength.
Summary of the invention
In order to overcome the deficiencies in the prior art, technical problem to be solved by this invention provides a kind of high strength heat resistant magnalium.
For solving the problems of the technologies described above, the present invention realizes like this
The high strength heat resistant magnalium comprises the alloying element of following mass percent: the aluminium of copper 4.5-5.5%, manganese 0.5-1.0%, titanium 0.1-0.5%, Cd0.15-0.25%, vanadium 0.05-0.35%, lithium 0.1-0.5%, boron 0.1-0.5%, iron 0.1-0.3%, silicon 0.05-0.15%, magnesium 0.01-0.05%, zinc 0.01-0.05%, manganese 0.1-0.5%, tin 0.01-0.05%, bismuth 0.15-0.55% and surplus.
Copper can improve intensity, the hardness of aluminium alloy, but can reduce extensibility; Iron can increase DIMENTIONAL STABILITY and support performance, makes it at high temperature have high strength, hardness, but excessive iron and copper form the Cu2FeA7 component and reduces the required copper amount of annealing effect; Silicon combines with iron, prevents that iron from combining the tensile property that reduces alloy with copper;
Addition element magnesium can improve the intensity of alloy system in zinciferous aluminium alloy, because of magnesium and zinc formation MgZn.But can reduce the overall corrosion resistance of aluminium, can overcome this shortcoming by adding copper or chromium.
Boron, manganese, bismuth, cadmium can increase the recrystallize humidity of aluminium alloy, improve processibility, opourability and the welding property of aluminium alloy; Titanium, boron can crystal grain thinnings, and the processing of control casting original state is with grain fineness number and shape in the ingot casting; Tin can strengthen artificially aged effect after the aluminium alloy solution heat treatment greatly, makes alloy strength increase, and erosion resistance improves, and the nickel of high level causes the alloy thermal crack, exists simultaneously if any small amount of magnesium, and then the artificially aged feature just obviously weakens.Bismuth can improve the machinability of aluminium alloy.
The alloy that the present invention obtains is for being aluminum magnesium alloy, and foundry goods can heat treatment reinforcement, urge fire after, intensity height, and plasticity, hot well life-time service plasticity is good, the solidity to corrosion height, machinability is good, castability is good, weldability is good.
Embodiment
The present invention is described in further detail below in conjunction with embodiment.
Embodiment 1
The high strength heat resistant magnalium comprises the alloying element of following mass percent: the aluminium of copper 4.5%, manganese 0.5%, titanium 0.1%, Cd0.15%, vanadium 0.05%, lithium 0.1%, boron 0.1%, iron 0.1%, silicon 0.05%, magnesium 0.01%, zinc 0.01%, manganese 0.1%, tin 0.01%, bismuth 0.15% and surplus.Castmethod is sand mold casting (S), permanent mold casting or investment cast.Alloy state is T4, and the aluminium alloy tensile strength that the present invention obtains is 289MPa, and elongation is 3.2%, and Bu Shi intensity is 80HBS.
Embodiment 2
The high strength heat resistant magnalium comprises the alloying element of following mass percent: the aluminium of copper 5.5%, manganese 1.0%, titanium 0.5%, Cd0.25%, vanadium 0.35%, lithium 0.5%, boron 0.5%, iron 0.3%, silicon 0.15%, magnesium 0.05%, zinc 0.05%, manganese 0.5%, tin 0.05%, bismuth 0.55% and surplus.Castmethod is sand mold casting (S), permanent mold casting or investment cast.Alloy state is T4, and the aluminium alloy tensile strength that the present invention obtains is 495MPa, and elongation is 2.8%, and Bu Shi intensity is 75HBS.
Embodiment 3
The high strength heat resistant magnalium comprises the alloying element of following mass percent: the aluminium of copper 4.0%, manganese 0.8%, titanium 0.3%, Cd0.2%, vanadium 0.15%, lithium 0.3%, boron 0.3%, iron 0.2%, silicon 0.8%, magnesium 0.04%, zinc 0.03%, manganese 0.4%, tin 0.02%, bismuth 0.19% and surplus.Castmethod is sand mold casting (S), permanent mold casting or investment cast.Alloy state is T4, and the aluminium alloy tensile strength that the present invention obtains is 312MPa, and elongation is 2.1%, and Bu Shi intensity is 95HBS.
Above-mentioned embodiment does not limit technical scheme of the present invention in any form, and the technical scheme that mode obtained that every employing is equal to replacement or equivalent transformation all drops on protection scope of the present invention.

Claims (1)

1. high strength heat resistant magnalium comprises the alloying element of following mass percent: the aluminium of copper 4.5-5.5%, manganese 0.5-1.0%, titanium 0.1-0.5%, Cd0.15-0.25%, vanadium 0.05-0.35%, lithium 0.1-0.5%, boron 0.1-0.5%, iron 0.1-0.3%, silicon 0.05-0.15%, magnesium 0.01-0.05%, zinc 0.01-0.05%, manganese 0.1-0.5%, tin 0.01-0.05%, bismuth 0.15-0.55% and surplus.
CN2011102434425A 2011-08-24 2011-08-24 High-strength heat-resistant magnalium alloy Pending CN102296218A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011102434425A CN102296218A (en) 2011-08-24 2011-08-24 High-strength heat-resistant magnalium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011102434425A CN102296218A (en) 2011-08-24 2011-08-24 High-strength heat-resistant magnalium alloy

Publications (1)

Publication Number Publication Date
CN102296218A true CN102296218A (en) 2011-12-28

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CN (1) CN102296218A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102952979A (en) * 2012-11-20 2013-03-06 无锡常安通用金属制品有限公司 Aluminium alloy material
CN104018033A (en) * 2014-06-13 2014-09-03 苏州列治埃盟新材料技术转移有限公司 Tin/zinc/manganese-added aluminum-lithium alloy material and production method thereof
CN105063435A (en) * 2015-08-25 2015-11-18 广西南宁智翠科技咨询有限公司 Corrosion-resistant aluminum alloy containing molybdenum
CN105063434A (en) * 2015-08-25 2015-11-18 广西南宁智翠科技咨询有限公司 High-strength aluminum alloy
CN105177366A (en) * 2015-08-25 2015-12-23 广西南宁智翠科技咨询有限公司 Wear-resistant and corrosion-resistant aluminium alloy
CN105385910A (en) * 2015-10-23 2016-03-09 安徽华铝铝业有限公司 High-strength heat-resisting aluminum pipe and manufacturing method thereof
CN106048321A (en) * 2016-07-13 2016-10-26 安徽祈艾特电子科技股份有限公司 Nanosized titanium nitride modified and reinforced aluminium-magnesium alloy material for automobile electronic packaging and preparation method of alloy material
CN104018033B (en) * 2014-06-13 2016-11-30 苏州列治埃盟新材料技术转移有限公司 A kind of aluminium lithium alloy material adding stannum zinc-manganese and production method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100999797A (en) * 2005-08-22 2007-07-18 莱茵费尔登炼铝厂有限责任公司 Heat resistant aluminium alloy
CN101100716A (en) * 2006-07-03 2008-01-09 杰出材料科技股份有限公司 Aluminum with nano composite phase and application thereof
EP1997924A1 (en) * 2007-05-24 2008-12-03 ALUMINIUM RHEINFELDEN GmbH High-temperature aluminium alloy
CN101413079A (en) * 2008-09-17 2009-04-22 北京有色金属研究总院 Cobaltiferous aluminum alloy material and preparation thereof
US20090260724A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation Heat treatable L12 aluminum alloys

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100999797A (en) * 2005-08-22 2007-07-18 莱茵费尔登炼铝厂有限责任公司 Heat resistant aluminium alloy
CN101100716A (en) * 2006-07-03 2008-01-09 杰出材料科技股份有限公司 Aluminum with nano composite phase and application thereof
EP1997924A1 (en) * 2007-05-24 2008-12-03 ALUMINIUM RHEINFELDEN GmbH High-temperature aluminium alloy
US20090260724A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation Heat treatable L12 aluminum alloys
CN101413079A (en) * 2008-09-17 2009-04-22 北京有色金属研究总院 Cobaltiferous aluminum alloy material and preparation thereof

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102952979A (en) * 2012-11-20 2013-03-06 无锡常安通用金属制品有限公司 Aluminium alloy material
CN104018033A (en) * 2014-06-13 2014-09-03 苏州列治埃盟新材料技术转移有限公司 Tin/zinc/manganese-added aluminum-lithium alloy material and production method thereof
CN104018033B (en) * 2014-06-13 2016-11-30 苏州列治埃盟新材料技术转移有限公司 A kind of aluminium lithium alloy material adding stannum zinc-manganese and production method thereof
CN105063435A (en) * 2015-08-25 2015-11-18 广西南宁智翠科技咨询有限公司 Corrosion-resistant aluminum alloy containing molybdenum
CN105063434A (en) * 2015-08-25 2015-11-18 广西南宁智翠科技咨询有限公司 High-strength aluminum alloy
CN105177366A (en) * 2015-08-25 2015-12-23 广西南宁智翠科技咨询有限公司 Wear-resistant and corrosion-resistant aluminium alloy
CN105385910A (en) * 2015-10-23 2016-03-09 安徽华铝铝业有限公司 High-strength heat-resisting aluminum pipe and manufacturing method thereof
CN105385910B (en) * 2015-10-23 2018-04-24 安徽华铝铝业有限公司 A kind of high strength heat resistant aluminum pipe and preparation method thereof
CN106048321A (en) * 2016-07-13 2016-10-26 安徽祈艾特电子科技股份有限公司 Nanosized titanium nitride modified and reinforced aluminium-magnesium alloy material for automobile electronic packaging and preparation method of alloy material

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Application publication date: 20111228