CN107699748A - A kind of aluminium alloy - Google Patents

A kind of aluminium alloy Download PDF

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Publication number
CN107699748A
CN107699748A CN201710924191.4A CN201710924191A CN107699748A CN 107699748 A CN107699748 A CN 107699748A CN 201710924191 A CN201710924191 A CN 201710924191A CN 107699748 A CN107699748 A CN 107699748A
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CN
China
Prior art keywords
aluminium alloy
aluminium
percentage
surplus
impurity
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Pending
Application number
CN201710924191.4A
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Chinese (zh)
Inventor
魏道金
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.)
Xuzhou Xuanyuan Aluminum Co Ltd
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Xuzhou Xuanyuan Aluminum Co Ltd
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Filing date
Publication date
Application filed by Xuzhou Xuanyuan Aluminum Co Ltd filed Critical Xuzhou Xuanyuan Aluminum Co Ltd
Priority to CN201710924191.4A priority Critical patent/CN107699748A/en
Publication of CN107699748A publication Critical patent/CN107699748A/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
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)

Abstract

The invention discloses a kind of aluminium alloy, consist of the following components in percentage by weight:Si:8%~16%, Zn:0.5%~1%, Mg:1%~3%, Fe:1%~2%, Mn:2%~3%, Cu:5%~8%, Ti:1%~5%, Cr:0.5%~1.5%, Ce:1 ‰~2 ‰, Pr:1 ‰~2 ‰ Nd:1 ‰~2 ‰;Surplus is the impurity of aluminium and content≤1%.The aluminium alloy of the present invention, crackle reduce, good percentage elongation, greatly increase service life, improve elongation and impact flexibility.

Description

A kind of aluminium alloy
Technical field
The present invention relates to a kind of aluminium alloy.
Background technology
Aluminium alloy is most widely used a kind of non-ferrous metal structural material in industry, in Aeronautics and Astronautics, automobile, machinery Widely applied in manufacture, ship and chemical industry.The rapid development of industrial economy, to the demand day of Welded structural member Benefit increases, and the Research on Weldability enabled aluminum alloy to is also goed deep into therewith.Aluminium alloy density is low, but intensity is higher, near or above excellent Matter steel, plasticity is good, can be processed into various section bars, has excellent electric conductivity, thermal conductivity and corrosion stability, industrially widely uses, Usage amount is only second to steel.
The rapid development of industrial economy, the weldability that enables aluminum alloy to increasing to the demand of Welded structural member Research is also goed deep into therewith.Existing aluminium alloy elongation percentage is poor, and service life is short.
The content of the invention
It is an object of the invention to provide a kind of aluminium alloy.
To achieve the above object, the present invention adopts the following technical scheme that:
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:8%~16%, Zn:0.5%~1%, Mg: 1%~3%, Fe:1%~2%, Mn:2%~3%, Cu:5%~8%, Ti:1%~5%, Cr:0.5%~1.5%, Ce: 1 ‰~2 ‰, Pr:1 ‰~2 ‰ Nd:1 ‰~2 ‰;Surplus is the impurity of aluminium and content≤1%.
Preferably, the aluminium alloy, is consisted of the following components in percentage by weight:Si:9%~12%, Zn:0.8%~ 1%, Mg:1.5%~2.5%, Fe:1.5%~2%, Mn:2.2%~2.6%, Cu:6%~7.5%, Ti:2%~ 3.5%, Cr:0.9%~1.3%, Ce:1.5 ‰~2 ‰, Pr:1 ‰~1.5 ‰ Nd:1.2 ‰~1.6 ‰;Surplus is aluminium and contained The impurity of amount≤1%.
Preferably, the aluminium alloy, is consisted of the following components in percentage by weight:Si:10%~12%, Zn:0.8%~ 1%, Mg:1.5%~2%, Fe:1.6%~1.8%, Mn:2.2%~2.5%, Cu:6.5%~7%, Ti:2%~3%, Cr:0.9%~1.1%, Ce:1.5 ‰~1.8 ‰, Pr:1.2 ‰~1.5 ‰ Nd:1.2 ‰~1.5 ‰;Surplus is aluminium and content ≤ 1% impurity.
Preferably, the aluminium alloy, is consisted of the following components in percentage by weight:Si:11%, Zn:0.9%, Mg: 1.8%, Fe:1.7%, Mn:2.3%, Cu:6.8%, Ti:2.5%, Cr:1.0%, Ce:1.6 ‰, Pr:1.3‰Nd:1.4‰; Surplus is the impurity of aluminium and content≤1%.
In terms of above-mentioned aluminium alloy is applied to forging.
The aluminium alloy of the present invention, crackle reduce, good percentage elongation, greatly increase service life, improve elongation and impact Toughness.
Embodiment
With reference to specific embodiment, the invention will be further described.
Embodiment 1
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:8%, Zn:0.5%, Mg:1%, Fe:1%, Mn:2%, Cu:5%, Ti:1%, Cr:0.5~1.5%, Ce:1 ‰, Pr:1 ‰, Nd:1‰;Surplus is aluminium and content≤1% Impurity.
Embodiment 2
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:9%, Zn:0.8%, Mg:1.5%, Fe: 1.5%, Mn:2.2%, Cu:6%, Ti:2%, Cr:0.9%, Ce:1.5 ‰, Pr:1‰Nd:1.2‰;Surplus is aluminium and content ≤ 1% impurity.
Embodiment 3
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:10%, Zn:0.8%, Mg:1.5%, Fe: 1.6%, Mn:2.2%, Cu:6.5%, Ti:2%, Cr:0.9%, Ce:1.5 ‰, Pr:1.2‰Nd:1.2‰;Surplus be aluminium and The impurity of content≤1%.
Embodiment 4
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:11%, Zn:0.9%, Mg:1.8%, Fe: 1.7%, Mn:2.3%, Cu:6.8%, Ti:2.5%, Cr:1.0%, Ce:1.6 ‰, Pr:1.3‰Nd:1.4‰;Surplus is aluminium And the impurity of content≤1%.
Embodiment 5
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:16%, Zn:1%, Mg:3%, Fe:2%, Mn:3%, Cu:8%, Ti:5%, Cr:1.5%, Ce:2 ‰, Pr:2‰Nd:2‰;Surplus is the impurity of aluminium and content≤1%.
Embodiment 6
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:12%, Zn:1%, Mg:2.5%, Fe:2%, Mn:2.6%, Cu:7.5%, Ti:3.5%, Cr:1.3%, Ce:2 ‰, Pr:1.5‰Nd:1.6‰;Surplus be aluminium and content≤ 1% impurity.
Embodiment 7
A kind of aluminium alloy, is consisted of the following components in percentage by weight:Si:12%, Zn:1%, Mg:2%, Fe:1.8%, Mn:2.5%, Cu:7%, Ti:3%, Cr:1.1%, Ce:1.8 ‰, Pr:1.5‰Nd:1.5‰;Surplus is aluminium and content≤1% Impurity.

Claims (5)

1. a kind of aluminium alloy, it is characterised in that consist of the following components in percentage by weight:Si:8%~16%, Zn:0.5% ~1%, Mg:1%~3%, Fe:1%~2%, Mn:2%~3%, Cu:5%~8%, Ti:1%~5%, Cr:0.5%~ 1.5%, Ce:1 ‰~2 ‰, Pr:1 ‰~2 ‰ Nd:1 ‰~2 ‰;Surplus is the impurity of aluminium and content≤1%.
2. a kind of aluminium alloy according to claim 1, it is characterised in that consist of the following components in percentage by weight:Si: 9%~12%, Zn:0.8%~1%, Mg:1.5%~2.5%, Fe:1.5%~2%, Mn:2.2%~2.6%, Cu:6% ~7.5%, Ti:2%~3.5%, Cr:0.9%~1.3%, Ce:1.5 ‰~2 ‰, Pr:1 ‰~1.5 ‰ Nd:1.2 ‰~ 1.6‰;Surplus is the impurity of aluminium and content≤1%.
3. a kind of aluminium alloy according to claim 1, it is characterised in that consist of the following components in percentage by weight:Si: 10%~12%, Zn:0.8%~1%, Mg:1.5%~2%, Fe:1.6%~1.8%, Mn:2.2%~2.5%, Cu: 6.5%~7%, Ti:2%~3%, Cr:0.9%~1.1%, Ce:1.5 ‰~1.8 ‰, Pr:1.2 ‰~1.5 ‰ Nd: 1.2 ‰~1.5 ‰;Surplus is the impurity of aluminium and content≤1%.
4. a kind of aluminium alloy according to claim 1, it is characterised in that consist of the following components in percentage by weight:Si: 11%, Zn:0.9%, Mg:1.8%, Fe:1.7%, Mn:2.3%, Cu:6.8%, Ti:2.5%, Cr:1.0%, Ce:1.6 ‰, Pr:1.3‰Nd:1.4‰;Surplus is the impurity of aluminium and content≤1%.
5. application of the aluminium alloy described in any one of Claims 1-4 in terms of forging.
CN201710924191.4A 2017-09-30 2017-09-30 A kind of aluminium alloy Pending CN107699748A (en)

Priority Applications (1)

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Application Number Priority Date Filing Date Title
CN201710924191.4A CN107699748A (en) 2017-09-30 2017-09-30 A kind of aluminium alloy

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CN107699748A true CN107699748A (en) 2018-02-16

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111411274A (en) * 2020-05-27 2020-07-14 东莞市青鸟金属材料有限公司 High-strength heat-conducting aluminum alloy material and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101294255A (en) * 2008-06-12 2008-10-29 苏州有色金属研究院有限公司 Aluminum alloy for vehicle body plate and method for manufacturing same
CN103924132A (en) * 2014-03-13 2014-07-16 淮北银丰铝业有限公司 Preparation method of high corrosion resistant and high wear resistant aluminium alloy profile for engine cylinder cover
CN104988370A (en) * 2015-06-29 2015-10-21 余姚市朗霞镇大众铸件精工厂 Aluminium alloy
CN105349848A (en) * 2015-11-19 2016-02-24 江苏常铝铝业股份有限公司 Continuously cast and rolled aluminum alloy material for blind window and manufacturing method of continuously cast and rolled aluminum alloy material
CN106048381A (en) * 2016-07-15 2016-10-26 南通纺都置业有限公司 Aluminum alloy

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101294255A (en) * 2008-06-12 2008-10-29 苏州有色金属研究院有限公司 Aluminum alloy for vehicle body plate and method for manufacturing same
CN103924132A (en) * 2014-03-13 2014-07-16 淮北银丰铝业有限公司 Preparation method of high corrosion resistant and high wear resistant aluminium alloy profile for engine cylinder cover
CN104988370A (en) * 2015-06-29 2015-10-21 余姚市朗霞镇大众铸件精工厂 Aluminium alloy
CN105349848A (en) * 2015-11-19 2016-02-24 江苏常铝铝业股份有限公司 Continuously cast and rolled aluminum alloy material for blind window and manufacturing method of continuously cast and rolled aluminum alloy material
CN106048381A (en) * 2016-07-15 2016-10-26 南通纺都置业有限公司 Aluminum alloy

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* Cited by examiner, † Cited by third party
Title
王祝堂等: "《轨道车辆用铝材手册》", 30 November 2013 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111411274A (en) * 2020-05-27 2020-07-14 东莞市青鸟金属材料有限公司 High-strength heat-conducting aluminum alloy material and preparation method thereof

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Application publication date: 20180216