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CN104294116A - High-performance aluminum alloy - Google Patents

High-performance aluminum alloy Download PDF

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Publication number
CN104294116A
CN104294116A CN201410591202.8A CN201410591202A CN104294116A CN 104294116 A CN104294116 A CN 104294116A CN 201410591202 A CN201410591202 A CN 201410591202A CN 104294116 A CN104294116 A CN 104294116A
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CN
China
Prior art keywords
zinc
copper
scope
aluminum alloy
composition
Prior art date
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Pending
Application number
CN201410591202.8A
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Chinese (zh)
Inventor
严静儿
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Individual
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Individual
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Publication date
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Priority to CN201410591202.8A priority Critical patent/CN104294116A/en
Publication of CN104294116A publication Critical patent/CN104294116A/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
    • C22C21/10Alloys based on aluminium with zinc 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 relates to a high-performance aluminum alloy. The high-performance aluminum alloy comprises the following materials by weight percentage: 0.2-0.3% of silicon, 0.5-0.8% of iron, 1.2-1.5% of copper, 0.3-0.5% of manganese, 0.01-0.03% of molybdenum, 0.08-0.15% of nickel, 0.01-0.03% of boron, 0.001-0.003% of tellurium, 0.01-0.03% of vanadium, 0.5-0.8% of magnesium, 0.03-0.3% of chrome, 6.0-7.0% of zinc, 0.08-0.15% of titanium, and the balance of aluminum and a bit of unavoidable impurities.

Description

A kind of high-performance aluminium alloy
Technical field
The invention belongs to aluminum alloy materials, particularly relate to a kind of high-performance aluminium alloy.
Background technology
Aluminum alloy materials is widely used in the fields such as industry, civilian, building, and current industrial aluminium has many different requirements, as high strength, high tenacity and good corrosion resistance nature etc.The quantity that current aldural uses at industrial circle and increasing extent many, but there is many problems in alloy aluminum of the prior art, cannot meet the aspects such as machine-shaping, surface quality and thermal treatment, this makes to be restricted the use of high-strength aluminum alloy material in industrial circle.
Summary of the invention
The object of this invention is to provide a kind of aluminium alloy technical scheme, good processing characteristics can be had while the high-intensity performance ensureing aluminum alloy materials by the program.
The present invention is achieved by the following technical solutions:
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.3-0.5%, the molybdenum of 0.01-0.03%, the nickel of 0.08-0.15%, the boron of 0.01-0.03%, the tellurium of 0.001-0.003%, the vanadium of 0.01-0.03%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.3%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
Described aldural, in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc between 6.0-6.5%, but does not comprise when the scope of scope zinc 1.35% time of copper is 6.5%.
The invention has the beneficial effects as follows:
By technical scheme of the present invention, optimize the formula of existing high-strength aluminum alloy material, improve machine-shaping ability, also improve surface quality and the surface treatment properties of converted products, there is high strength simultaneously.
Embodiment
Technical scheme of the present invention is described in detail below in conjunction with specific embodiment.
Aluminum alloy materials is in the inventive solutions produced mainly through hot-work, particularly hot extrusion processing.
The techniques such as process for processing in the present invention with existing aluminum alloy production process and device all identical, change be only change to aluminum alloy materials composition, therefore all illustrate no longer one by one in the present invention and following each embodiment.
Unit selected is in the present invention weight percentage, and when not illustrating, the unit of each composition is weight percentage.
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the molybdenum of the manganese 0.01-0.03% of 0.3-0.5%, the nickel of 0.08-0.15%, the boron of 0.01-0.03%, the tellurium of 0.001-0.003%, the vanadium of 0.01-0.03%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.3%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
Described high performance aluminium materials, in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, and the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc is between 6.0-6.5%; Do not exist when the scope of scope zinc 1.35% time of copper is 6.5%.The mid point of wherein said copper refers to (1.2%+1.5%)/2=1.35%; The mid point of described zinc refers to (6.0%+7.0%)/2=6.5%.
Embodiment 1
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage, the silicon of 0.2%, the iron of 0.5%, the copper of 1.2%, the manganese of 0.3%, the molybdenum of 0.01%, the nickel of 0.08%, the boron of 0.01%, the tellurium of 0.001%, the vanadium of 0.01%, the magnesium of 0.5%, the chromium of 0.03%, the zinc of 7.0%, the titanium of 0.08%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 2
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage, the silicon of 0.3%, the iron of 0.8%, the copper of 1.5%, the manganese of 0.5%, the molybdenum of 0.03%, the nickel of 0.15%, the boron of 0.03%, the tellurium of 0.003%, the vanadium of 0.03%, the magnesium of 0.8%, the chromium of 0.3%, the zinc of 6.0%, the titanium of 0.15%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 3
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage, the silicon of 0.25%, the iron of 0.6%, the copper of 1.3%, the manganese of 0.4%, the molybdenum of 0.015%, the nickel of 0.09%, the boron of 0.015%, the tellurium of 0.002%, the vanadium of 0.022%, the magnesium of 0.6%, the chromium of 0.1%, the zinc of 6.8%, the titanium of 0.1%, surplus is aluminium and a small amount of unavoidable impurity.
Embodiment 4
A kind of high-performance aluminium alloy, includes the following material composition counted by weight percentage, the silicon of 0.3%, the iron of 0.5%, the copper of 1.4%, the manganese of 0.3%, the molybdenum of 0.022%, the nickel of 0.12%, the boron of 0.02%, the tellurium of 0.0015%, the vanadium of 0.015%, the magnesium of 0.8%, the chromium of 0.05%, the zinc of 7.0%, the titanium of 0.12%, surplus is aluminium and a small amount of unavoidable impurity.
Below be only limited embodiment; because cannot enumerate embodiment at this; but these embodiments are not limitations of the present invention, should be appreciated that those skilled in the art is by being protection scope of the present invention to the change of technical solution of the present invention and the limited increase and decrease of component.

Claims (2)

1. a high-performance aluminium alloy, is characterized in that: include the following material composition counted by weight percentage: the silicon of 0.2-0.3%, the iron of 0.5-0.8%, the copper of 1.2-1.5%, the manganese of 0.3-0.5%, the molybdenum of 0.01-0.03%, the nickel of 0.08-0.15%, the boron of 0.01-0.03%, the tellurium of 0.001-0.003%, the vanadium of 0.01-0.03%, the magnesium of 0.5-0.8%, the chromium of 0.03-0.3%, the zinc of 6.0-7.0%, the titanium of 0.08-0.15%, surplus is aluminium and a small amount of unavoidable impurity.
2. high-performance aluminium alloy according to claim 1, it is characterized in that: in its composition, the relation of copper and zinc two kinds of elements is in the content range of two elements, the middle point range of copper is 1.35%, the mid point of zinc is 6.5%, and when the compositing range of copper is between 1.2-1.35%, the scope of zinc is between 6.5-7.0%; When the composition of copper is between 1.35-1.5%, the scope of zinc between 6.0-6.5%, but does not comprise when the scope of scope zinc 1.35% time of copper is 6.5%.
CN201410591202.8A 2014-10-29 2014-10-29 High-performance aluminum alloy Pending CN104294116A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410591202.8A CN104294116A (en) 2014-10-29 2014-10-29 High-performance aluminum alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410591202.8A CN104294116A (en) 2014-10-29 2014-10-29 High-performance aluminum alloy

Publications (1)

Publication Number Publication Date
CN104294116A true CN104294116A (en) 2015-01-21

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CN201410591202.8A Pending CN104294116A (en) 2014-10-29 2014-10-29 High-performance aluminum alloy

Country Status (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105349854A (en) * 2015-11-12 2016-02-24 俞虹 High-strength aluminum alloy
CN105401006A (en) * 2015-11-12 2016-03-16 俞虹 Novel aluminum alloy preparing method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1780925A (en) * 2003-04-10 2006-05-31 克里斯铝轧制品有限公司 High strength al-zn alloy and method for producing such an alloy product
JP2008516079A (en) * 2004-10-05 2008-05-15 アレリス、アルミナム、コブレンツ、ゲゼルシャフト、ミット、ベシュレンクテル、ハフツング High strength, high toughness Al-Zn alloy products and methods for producing such products
CN102876943A (en) * 2012-09-21 2013-01-16 史昊东 Aluminum alloy material
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1780925A (en) * 2003-04-10 2006-05-31 克里斯铝轧制品有限公司 High strength al-zn alloy and method for producing such an alloy product
JP2008516079A (en) * 2004-10-05 2008-05-15 アレリス、アルミナム、コブレンツ、ゲゼルシャフト、ミット、ベシュレンクテル、ハフツング High strength, high toughness Al-Zn alloy products and methods for producing such products
CN102876943A (en) * 2012-09-21 2013-01-16 史昊东 Aluminum alloy material
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105349854A (en) * 2015-11-12 2016-02-24 俞虹 High-strength aluminum alloy
CN105401006A (en) * 2015-11-12 2016-03-16 俞虹 Novel aluminum alloy preparing method

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Application publication date: 20150121