CN105441753A - Aluminum alloy rail and manufacturing method thereof - Google Patents

Aluminum alloy rail and manufacturing method thereof Download PDF

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Publication number
CN105441753A
CN105441753A CN201510841276.7A CN201510841276A CN105441753A CN 105441753 A CN105441753 A CN 105441753A CN 201510841276 A CN201510841276 A CN 201510841276A CN 105441753 A CN105441753 A CN 105441753A
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China
Prior art keywords
aluminum alloy
alloy rail
rail
surplus
grouped
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CN201510841276.7A
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Chinese (zh)
Inventor
王林仙
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Danyang Chenxing Environment Protection Equipment Co Ltd
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Danyang Chenxing Environment Protection Equipment Co Ltd
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Priority to CN201510841276.7A priority Critical patent/CN105441753A/en
Publication of CN105441753A publication Critical patent/CN105441753A/en
Pending legal-status Critical Current

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Abstract

The invention provides an aluminum alloy rail. The aluminum alloy rail is composed of, by weight, 1.2 to 1.8 parts of Cu, 1.6 to 2.6 parts of Mg, 0.1 to 0.4 part of Mn, 3 to 5 parts of Zn and the balance Al. The aluminum alloy rail mainly comprises Al-Mg alloy and Al-Mn alloy and is good in corrosion resistance and easy to machine, form and weld, a guide rail profile high in mechanical performance, rust resistance and corrosion resistance can be obtained after extrusion, quenching, drawing and manual aging, and the aluminum alloy rail completely meets the use requirements of the fields of aviation, aerospace, automobiles, mechanical manufacturing, ships, the chemical industry and the like.

Description

A kind of aluminum alloy rail and preparation method thereof
Technical field
The present invention relates to a kind of field of aluminum alloys, particularly a kind of aluminum alloy rail.
Background technology
At present, aluminium alloy has been most widely used structural metallic materials in industry, and it widely applies in Aeronautics and Astronautics, automobile, machinofacture, boats and ships and chemical industry.But the aluminum alloy materials of existing composition proportion, its bad mechanical property, antirust, non-corrosibility is weak, so be badly in need of a kind of aluminum alloy materials of high-quality in orbit.
Summary of the invention
The technical problem to be solved in the present invention is for the deficiencies in the prior art, proposes a kind of mechanical property high, aluminum alloy rail that antirust, non-corrosibility is strong and preparation method thereof.
The technical problem to be solved in the present invention is achieved through the following technical solutions.The present invention is a kind of aluminum alloy rail, is characterized in, is grouped into: Cu1.2-1.8 by the one-tenth of following weight percent; Mg1.6-2.6; Mn0.1-0.4; Zn3-5; Surplus is Al.
In a kind of aluminum alloy rail technical scheme of the present invention, preferred technical scheme feature is further:
1, be grouped into by the one-tenth of following weight percent: Cu1.4-1.6; Mg2-2.4; Mn0.1-0.3; Zn3-4; Surplus is Al;
2, be grouped into by the one-tenth of following weight percent: Cu1.5; Mg2.2; Mn00.2; Zn3.5; Surplus is Al;
The technical problem to be solved in the present invention is achieved through the following technical solutions.The present invention is a kind of preparation method of aluminum alloy rail, is characterized in, aluminium alloy through extruding, quenching, stretch, artificial aging obtains that tensile strength is 500-700MPa, extensibility is 10%-14%, Brinell hardness is the guide rail section of 120-160.
In preparation method's technical scheme of a kind of aluminum alloy rail of the present invention, preferred technical scheme feature is further:
1, the tensile strength of described guide rail section is 600MPa, extensibility is 12%, Brinell hardness is 140;
2, described guide rail section is the I-beam be made up of top board, web plate and back plate, the conical bottom board that described base plate is big up and small down.
Compared with prior art, mainly Al-Mg and Al-Mn alloy in aluminum alloy rail of the present invention, its solidity to corrosion is good, be easy to shape and weld, mechanical property can be obtained high after extruding, quenching, stretching, artificial aging, the guide rail section that antirust, non-corrosibility is strong, meets the service requirements in the fields such as Aeronautics and Astronautics, automobile, machinofacture, boats and ships and chemical industry completely.
Embodiment
Further describe concrete technical scheme of the present invention, so that those skilled in the art understands the present invention further, and do not form the restriction of its power.
Embodiment 1, a kind of aluminum alloy rail, is grouped into by the one-tenth of following weight percent: Cu1.2-1.8; Mg1.6-2.6; Mn0.1-0.4; Zn3-5; Surplus is Al.
Embodiment 2, in the aluminum alloy rail described in embodiment 1: be grouped into by the one-tenth of following weight percent: Cu1.4-1.6; Mg2-2.4; Mn0.1-0.3; Zn3-4; Surplus is Al.
Embodiment 3, in the aluminum alloy rail described in embodiment 1 or 2: be grouped into by the one-tenth of following weight percent: Cu1.5; Mg2.2; Mn00.2; Zn3.5; Surplus is Al.
Embodiment 4, in embodiment 1 or the aluminum alloy rail described in 2 or 3: be grouped into by the one-tenth of following weight percent: Cu1.4; Mg2; Mn0.1; Zn3; Surplus is Al.
Embodiment 5, in the aluminum alloy rail described in any one of embodiment 1-4: be grouped into by the one-tenth of following weight percent: Cu1.6; Mg2.4; Mn0.3; Zn4; Surplus is Al.
Embodiment 6, in a kind of preparation method of aluminum alloy rail: aluminium alloy through extruding, quenching, stretch, artificial aging obtains that tensile strength is 500-700MPa, extensibility is 10%-14%, Brinell hardness is the guide rail section of 120-160.
Embodiment 7, in the preparation method of the aluminum alloy rail described in embodiment 6: the tensile strength of described guide rail section is 600MPa, extensibility is 12%, Brinell hardness is 140.
Embodiment 8, in the preparation method of the aluminum alloy rail described in embodiment 6 or 7: described guide rail section is the I-beam be made up of top board, web plate and back plate, the conical bottom board that described base plate is big up and small down.

Claims (6)

1. an aluminum alloy rail, is characterized in that, is grouped into: Cu1.2-1.8 by the one-tenth of following weight percent; Mg1.6-2.6; Mn0.1-0.4; Zn3-5; Surplus is Al.
2. aluminum alloy rail according to claim 1, is characterized in that, is grouped into: Cu1.4-1.6 by the one-tenth of following weight percent; Mg2-2.4; Mn0.1-0.3; Zn3-4; Surplus is Al.
3. aluminum alloy rail according to claim 1, is characterized in that, is grouped into: Cu1.5 by the one-tenth of following weight percent; Mg2.2; Mn00.2; Zn3.5; Surplus is Al.
4. the preparation method of aluminum alloy rail as described in any one of claim 1-3, is characterized in that: aluminium alloy through extruding, quenching, stretch, artificial aging obtains that tensile strength is 500-700MPa, extensibility is 10%-14%, Brinell hardness is the guide rail section of 120-160.
5. the preparation method of aluminum alloy rail according to claim 4, is characterized in that: the tensile strength of described guide rail section is 600MPa, extensibility is 12%, Brinell hardness is 140.
6. the preparation method of aluminum alloy rail according to claim 4, is characterized in that: described guide rail section is the I-beam be made up of top board, web plate and back plate, the conical bottom board that described base plate is big up and small down.
CN201510841276.7A 2015-11-28 2015-11-28 Aluminum alloy rail and manufacturing method thereof Pending CN105441753A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510841276.7A CN105441753A (en) 2015-11-28 2015-11-28 Aluminum alloy rail and manufacturing method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510841276.7A CN105441753A (en) 2015-11-28 2015-11-28 Aluminum alloy rail and manufacturing method thereof

Publications (1)

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CN105441753A true CN105441753A (en) 2016-03-30

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109837404A (en) * 2017-11-28 2019-06-04 丹阳市延陵镇优越合金厂 A kind of preparation process of aluminium alloy

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Publication number Priority date Publication date Assignee Title
CN1324278A (en) * 1998-09-04 2001-11-28 联结技术两合公司 Light alloy thread-forming screw and its prodn. method
CN1546709A (en) * 2003-12-04 2004-11-17 尧 李 Deformable aluminium alloy containing aluminum, zinc, magnesium, copper and beryllium
CN101445886A (en) * 2008-12-31 2009-06-03 东北轻合金有限责任公司 High-strength high-toughness aluminum alloy pre-tensioned thick plate and preparation method thereof
CN101760679A (en) * 2009-12-28 2010-06-30 东北轻合金有限责任公司 Preparation method of 7B04 aluminium alloy section
CN102066596A (en) * 2008-06-24 2011-05-18 阿勒里斯铝业科布伦茨有限公司 Al-Zn-Mg alloy product with reduced quench sensitivity
CN103189534A (en) * 2010-11-05 2013-07-03 阿莱利斯铝业迪弗尔私人有限公司 Formed automotive part made from an aluminium alloy product and method of its manufacture
CN103320727A (en) * 2013-06-13 2013-09-25 广西南南铝加工有限公司 Aluminum alloy medium plate preparation method
CN103966490A (en) * 2013-01-25 2014-08-06 株式会社神户制钢所 7000 series aluminum alloy member excellent in stress corrosion cracking resistance and method for manufacturing the same
CN103966491A (en) * 2013-01-30 2014-08-06 株式会社神户制钢所 7000 series aluminum alloy member excellent in stress corrosion cracking resistance and method for manufacturing the same
CN104032193A (en) * 2014-05-20 2014-09-10 南京南车浦镇城轨车辆有限责任公司 Al-Zn-Mg alloy and preparation method of sectional material thereof

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1324278A (en) * 1998-09-04 2001-11-28 联结技术两合公司 Light alloy thread-forming screw and its prodn. method
CN1546709A (en) * 2003-12-04 2004-11-17 尧 李 Deformable aluminium alloy containing aluminum, zinc, magnesium, copper and beryllium
CN102066596A (en) * 2008-06-24 2011-05-18 阿勒里斯铝业科布伦茨有限公司 Al-Zn-Mg alloy product with reduced quench sensitivity
CN101445886A (en) * 2008-12-31 2009-06-03 东北轻合金有限责任公司 High-strength high-toughness aluminum alloy pre-tensioned thick plate and preparation method thereof
CN101760679A (en) * 2009-12-28 2010-06-30 东北轻合金有限责任公司 Preparation method of 7B04 aluminium alloy section
CN103189534A (en) * 2010-11-05 2013-07-03 阿莱利斯铝业迪弗尔私人有限公司 Formed automotive part made from an aluminium alloy product and method of its manufacture
CN103966490A (en) * 2013-01-25 2014-08-06 株式会社神户制钢所 7000 series aluminum alloy member excellent in stress corrosion cracking resistance and method for manufacturing the same
CN103966491A (en) * 2013-01-30 2014-08-06 株式会社神户制钢所 7000 series aluminum alloy member excellent in stress corrosion cracking resistance and method for manufacturing the same
CN103320727A (en) * 2013-06-13 2013-09-25 广西南南铝加工有限公司 Aluminum alloy medium plate preparation method
CN104032193A (en) * 2014-05-20 2014-09-10 南京南车浦镇城轨车辆有限责任公司 Al-Zn-Mg alloy and preparation method of sectional material thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109837404A (en) * 2017-11-28 2019-06-04 丹阳市延陵镇优越合金厂 A kind of preparation process of aluminium alloy

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Application publication date: 20160330