CN102876955A - Aluminum alloy with high thermal conductivity - Google Patents

Aluminum alloy with high thermal conductivity Download PDF

Info

Publication number
CN102876955A
CN102876955A CN 201210321952 CN201210321952A CN102876955A CN 102876955 A CN102876955 A CN 102876955A CN 201210321952 CN201210321952 CN 201210321952 CN 201210321952 A CN201210321952 A CN 201210321952A CN 102876955 A CN102876955 A CN 102876955A
Authority
CN
China
Prior art keywords
accounts
thermal conductivity
aluminium alloy
percent
good
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
CN 201210321952
Other languages
Chinese (zh)
Inventor
朱培元
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.)
KUNSHAN YUANFENG ALUMINUM Co Ltd
Original Assignee
KUNSHAN YUANFENG ALUMINUM 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 KUNSHAN YUANFENG ALUMINUM Co Ltd filed Critical KUNSHAN YUANFENG ALUMINUM Co Ltd
Priority to CN 201210321952 priority Critical patent/CN102876955A/en
Publication of CN102876955A publication Critical patent/CN102876955A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses an aluminum alloy with high thermal conductivity. The aluminum alloy comprises the elements in percentage by weight as follows: 3.8-4.9 percent of copper, 2-3.2 percent of silicon, 1.2-1.8 percent of magnesium, 5.7-6.7 percent of zinc, 0.3-0.9 percent of manganese, 40.3-42.3 percent of nickel, 0.5-1 percent of ferrum, 1-2 percent of titanium, 0.1-0.3 percent of chromium, 30-31 percent of lithium and 10-11 percent of other impurities. The aluminum alloy provided by the invention has the effects of high conductivity, high thermal conductivity and high corrosion resistance.

Description

The aluminium alloy that a kind of thermal conductivity is good
Technical field
The present invention relates to a kind of aluminium alloy, be specifically related to the good aluminium alloy of a kind of thermal conductivity.
Background technology
Aluminium alloy is a most widely used class non-ferrous metal structured material in the industry, in Aeronautics and Astronautics, automobile, machinofacture, boats and ships and chemical industry, widely apply, along with the in recent years develop rapidly of science and technology and industrial economy, demand to the Welded structural part is increasing, makes the Research on Weldability of aluminium alloy also thereupon deeply.The widespread use of aluminium alloy has promoted the development of aluminum alloy solder technology, and the Application Areas of aluminium alloy has been expanded again in the simultaneously development of welding technique, so the welding technique of aluminium alloy is just becoming one of focus of research.
The density of fine aluminium is little, and (aluminium is face-centred cubic structure for ρ=2.7g/cm3), approximately be 1/3 of iron, fusing point low (660 ℃), so have very high plasticity (δ: 32 ~ 40%, ψ: 70 ~ 90%), be easy to processing, can be made into various section bars, sheet material.Corrosion resistance is good; But the intensity of fine aluminium is very low, and as-annealed condition σ b value is about 8kgf/mm2, so should not make structured material.By long-term production practice and scientific experiment, people come reinforced aluminum to add the methods such as alloying element and utilization thermal treatment gradually, and this has just obtained a series of aluminium alloy.The alloy that adds certain element formation can also have higher intensity in the advantages such as maintenance fine aluminium light weight, σ b value can reach 24~60kgf/mm2 respectively.Like this so that its " specific tenacity " (ratio σ b/ ρ of intensity and proportion) surpasses a lot of steel alloys, become desirable structured material, be widely used in the aspects such as machinofacture, Transport Machinery, power machine and aircraft industry, the fuselage of aircraft, covering, pneumatic plant etc. are often with the aluminium alloy manufacturing, to alleviate deadweight.Adopt aluminium alloy to replace the welding of steel plate materials, structural weight can alleviate more than 50%.Aluminium alloy density is low, but strength ratio is higher, approaches or surpasses the high-quality steel, and plasticity is good, can be processed into various section bars, has good electroconductibility, thermal conductivity and corrosion stability, industrial being widely used, and usage quantity is only second to steel.
Summary of the invention
The object of the present invention is to provide and make that the good aluminium alloy of thermal conductivity that makes has good conductivity, thermal conductivity is good and the good aluminium alloy of a kind of thermal conductivity of the good effect of solidity to corrosion.
Technical scheme of the present invention is: the aluminium alloy that a kind of thermal conductivity is good, comprise the elements such as copper, silicon, magnesium, zinc, manganese, nickel, iron, titanium, chromium, lithium and other impurity, and each element wt proportioning is that copper accounts for 3.8%-4.9%, silicon accounts for 2%-3.2%, magnesium accounts for 1.2%-1.8%, and zinc accounts for 5.7%-6.7%, and manganese accounts for 0.3%-0.9%, nickel accounts for 40.3%-42.3%, iron accounts for 0.5%-1%, and titanium accounts for 1%-2%, and chromium accounts for 0.1%-0.3%, lithium accounts for 30%-31%, and other impurity account for 10%-11%.
In a preferred embodiment of the present invention, described other impurity comprise aluminium and phosphorus.
In a preferred embodiment of the present invention, each composition weight proportion of aluminium alloy that described thermal conductivity is good is that copper accounts for 4%, and silicon accounts for 3%, and magnesium accounts for 1.5%, and zinc accounts for 6%, and manganese accounts for 0.5%, and nickel accounts for 40.8%, and iron accounts for 1%, and titanium accounts for 2%, and chromium accounts for 0.2%, and lithium accounts for 31%, and other impurity account for 10%.
The good aluminium alloy of a kind of thermal conductivity of the present invention has good conductivity, thermal conductivity is good and solidity to corrosion is good effect.
Embodiment
Below in conjunction with preferred embodiment of the present invention is described in detail, thereby so that advantages and features of the invention can be easier to be it will be appreciated by those skilled in the art that protection scope of the present invention is made more explicit defining.
In one embodiment, the aluminium alloy that a kind of thermal conductivity is good comprises the elements such as copper, silicon, magnesium, zinc, manganese, nickel, iron, titanium, chromium, lithium and other impurity, each element wt proportioning is that copper accounts for 3.8%-4.9%, and silicon accounts for 2%-3.2%, and magnesium accounts for 1.2%-1.8%, zinc accounts for 5.7%-6.7%, and manganese accounts for 0.3%-0.9%, and nickel accounts for 40.3%-42.3%, iron accounts for 0.5%-1%, titanium accounts for 1%-2%, and chromium accounts for 0.1%-0.3%, and lithium accounts for 30%-31%, other impurity account for 10%-11%, and described other impurity comprise aluminium and phosphorus.
Further specify, each composition weight proportion of aluminium alloy that described thermal conductivity is good is that copper accounts for 4%, and silicon accounts for 3%, and magnesium accounts for 1.5%, and zinc accounts for 6%, and manganese accounts for 0.5%, and nickel accounts for 40.8%, and iron accounts for 1%, and titanium accounts for 2%, and chromium accounts for 0.2%, and lithium accounts for 31%, and other impurity account for 10%.
Can debug according to different ratios according to different demands, thereby reach different results of use, wrought aluminium alloy can bear press working.Can be processed into the aluminium alloy material of various forms, specification.Mainly for the manufacture of air material, door and window for building etc.Behaviors of Deformed Aluminum Alloys is divided into again not heat-treatable strengthened type aluminium alloy and heat-treatable strengthened type aluminium alloy.Not heat-treatable strengthened type can not improve mechanical property by thermal treatment, can only realize strengthening by cold deformation, and it mainly comprises rafifinal, industrial rafifinal, commercial-purity aluminium and corrosion-resisting aluminium etc.Heat-treatable strengthened type aluminium alloy can improve mechanical property by thermal treatment means such as quenching and timeliness, and it can be divided into duralumin, wrought aluminium, ultralumin and particular aluminum alloy etc.Cast aluminium alloy according to chemical composition can be divided into aluminum silicon alloy, aluminum-copper alloy, and aluminum magnesium alloy, aluminium-zinc alloy and Al rare earth alloy, wherein aluminum silicon alloy has again the hyper eutectic silicon aluminium alloy, the Eutectic Silicon in Al-Si Cast Alloys aluminium alloy, single Eutectic Silicon in Al-Si Cast Alloys aluminium alloy, cast aluminium alloy uses under as cast condition.The invention provides the good aluminium alloy of a kind of thermal conductivity, have good conductivity, thermal conductivity is good and solidity to corrosion is good effect.
The specific embodiment of the present invention; but protection scope of the present invention is not limited to this; any those of ordinary skill in the art are in the disclosed technical scope of the present invention, and variation or the replacement that can expect without creative work all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain that claims were limited.

Claims (3)

1. aluminium alloy that thermal conductivity is good, it is characterized in that: comprise the elements such as copper, silicon, magnesium, zinc, manganese, nickel, iron, titanium, chromium, lithium and other impurity, each element wt proportioning is that copper accounts for 3.8%-4.9%, silicon accounts for 2%-3.2%, magnesium accounts for 1.2%-1.8%, and zinc accounts for 5.7%-6.7%, and manganese accounts for 0.3%-0.9%, nickel accounts for 40.3%-42.3%, iron accounts for 0.5%-1%, and titanium accounts for 1%-2%, and chromium accounts for 0.1%-0.3%, lithium accounts for 30%-31%, and other impurity account for 10%-11%.
2. the good aluminium alloy of thermal conductivity according to claim 1, it is characterized in that: described other impurity comprise aluminium and phosphorus.
3. the good aluminium alloy of thermal conductivity according to claim 1, it is characterized in that: each composition weight proportion of aluminium alloy that described thermal conductivity is good is that copper accounts for 4%, and silicon accounts for 3%, and magnesium accounts for 1.5%, zinc accounts for 6%, manganese accounts for 0.5%, and nickel accounts for 40.8%, and iron accounts for 1%, titanium accounts for 2%, chromium accounts for 0.2%, and lithium accounts for 31%, and other impurity account for 10%.
CN 201210321952 2012-09-04 2012-09-04 Aluminum alloy with high thermal conductivity Pending CN102876955A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201210321952 CN102876955A (en) 2012-09-04 2012-09-04 Aluminum alloy with high thermal conductivity

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201210321952 CN102876955A (en) 2012-09-04 2012-09-04 Aluminum alloy with high thermal conductivity

Publications (1)

Publication Number Publication Date
CN102876955A true CN102876955A (en) 2013-01-16

Family

ID=47478464

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201210321952 Pending CN102876955A (en) 2012-09-04 2012-09-04 Aluminum alloy with high thermal conductivity

Country Status (1)

Country Link
CN (1) CN102876955A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107186957A (en) * 2017-05-15 2017-09-22 江苏鑫蕴模塑科技有限公司 A kind of stirring barrel of injection machine
CN112567059A (en) * 2018-08-02 2021-03-26 特斯拉公司 Aluminum alloy for die casting

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107186957A (en) * 2017-05-15 2017-09-22 江苏鑫蕴模塑科技有限公司 A kind of stirring barrel of injection machine
CN112567059A (en) * 2018-08-02 2021-03-26 特斯拉公司 Aluminum alloy for die casting

Similar Documents

Publication Publication Date Title
CN103255324A (en) Aluminum alloy material suitable for manufacturing car body panel and preparation method
CN104789833A (en) High-strength magnesium-containing aluminum alloy material and treatment process thereof
CN103233149A (en) High-strength aluminum alloy pipe
CN103572117A (en) High-strength aluminum alloy with high corrosion resistance and weldability
CN104789820A (en) Abrasion-proof aluminum alloy material containing earth elements and treatment process of abrasion-proof aluminum alloy material
CN102876942A (en) Aluminum alloy plate for vehicle
Hong et al. Effects of different tempers on precipitation hardening of 6000 series aluminium alloys
CN102876955A (en) Aluminum alloy with high thermal conductivity
CN104357712B (en) Aluminum alloy materials and preparation method
CN103290281A (en) Manufacturing method of high-strength aluminum alloy pipe
CN102876945A (en) Aluminum alloy with high plasticity
CN105671382A (en) High-hardness aluminum alloy material
CN104357713B (en) A kind of aluminum alloy materials and quenching process
CN104388782A (en) Aluminum alloy material and manufacturing method thereof
CN105543572A (en) Wear-resisting aluminum alloy material
CN106086548A (en) Comprise magnesium and copper can heat-treatable aluminum alloy and preparation method thereof
CN102876952A (en) Aluminum alloy material with good inoxidizability
CN102876958B (en) High-strength and high-ductility Mg-Zn-Ca/Fe particle composite material
CN106048381A (en) Aluminum alloy
CN102876956A (en) Aluminum alloy plate with high strength
CN102878418A (en) Aluminum alloy panel with excellent weldability
CN105401017A (en) Magnalium alloy material
CN104178662A (en) Aluminum alloy sheet material
CN107699748A (en) A kind of aluminium alloy
CN105039790A (en) Aluminum alloy

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130116