CN104046856B - A kind of aluminum bronze magnesium system duralumin - Google Patents
A kind of aluminum bronze magnesium system duralumin Download PDFInfo
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- CN104046856B CN104046856B CN201410306359.1A CN201410306359A CN104046856B CN 104046856 B CN104046856 B CN 104046856B CN 201410306359 A CN201410306359 A CN 201410306359A CN 104046856 B CN104046856 B CN 104046856B
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Abstract
Present invention is disclosed a kind of aluminum bronze magnesium system duralumin, described aluminum bronze magnesium system duralumin is combined by aluminium, copper, magnesium, zinc, titanium and nickel six kinds of metal ingredients, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is respectively: described aluminium accounts for 88.5%-92.9%, described copper accounts for 1.9%-2.8%, described magnesium accounts for 2.3%-3.2%, described zinc accounts for 1.7%-2.6%, and described titanium accounts for 0.8%-1.6%, and described nickel accounts for 0.4%-1.3%.By adding the metallic elements such as copper, magnesium, zinc, titanium and nickel in the aluminium alloy taking aluminium as base, effectively can improve the intensity of aluminium alloy, improve plasticity, facilitate follow-up processing, and there is excellent electroconductibility, thermal conductivity and corrosion stability, expand the use range of industry.
Description
Technical field
The present invention relates to a kind of alloy, be specifically related to a kind of aluminum bronze magnesium system duralumin.
Background technology
Duralumin belongs to thermal treatment can reinforced aluminium alloy, comprises Al-Cu-Mg and Solder for Al-Cu Joint Welding-Mn series alloy.Such alloy is widely used in various component and rivet bar.In shipbuilding, building etc., department also widely applies.The processing performance of Solder for Al-Cu Joint Welding-Mn series alloy is good, is easy to welding, is mainly used in the heat-resisting structured material that welds and forging, relatively narrow in application aspect.The Al-Cu-Mg duralumin scope of application is relatively wide, but the user demand of existing Al-Cu-Mg duralumin cannot meet the user demand in market.
Summary of the invention
The object of the present invention is to provide a kind of improve aluminium alloy intensity, improve plasticity, facilitate follow-up processing, there is excellent electroconductibility, thermal conductivity and corrosion stability, aluminum bronze magnesium system duralumin that use range is wide.
Technical scheme of the present invention is, a kind of aluminum bronze magnesium system duralumin, described aluminum bronze magnesium system duralumin is combined by aluminium, copper, magnesium, zinc, titanium and nickel six kinds of metal ingredients, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is respectively: described aluminium accounts for 88.5%-92.9%, described copper accounts for 1.9%-2.8%, and described magnesium accounts for 2.3%-3.2%, and described zinc accounts for 1.7%-2.6%, described titanium accounts for 0.8%-1.6%, and described nickel accounts for 0.4%-1.3%.
In a preferred embodiment of the present invention, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is specially: described aluminium accounts for 92.3%, and described copper accounts for 2.1%, described magnesium accounts for 2.4%, described zinc accounts for 1.8%, and described titanium accounts for 0.9%, and described nickel accounts for 0.5%.
In a preferred embodiment of the present invention, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is specially: described aluminium accounts for 89.1%, and described copper accounts for 2.7%, described magnesium accounts for 3.1%, described zinc accounts for 2.5%, and described titanium accounts for 1.4%, and described nickel accounts for 1.2%.
Of the present invention is a kind of aluminum bronze magnesium system duralumin, by adding the metallic elements such as copper, magnesium, zinc, titanium and nickel in the aluminium alloy taking aluminium as base, effectively can improve the intensity of aluminium alloy, improve plasticity, facilitate follow-up processing, and there is excellent electroconductibility, thermal conductivity and corrosion stability, expand the use range of industry.
Embodiment
Below preferred embodiment of the present invention is described in detail, can be easier to make advantages and features of the invention be readily appreciated by one skilled in the art, thus more explicit defining is made to protection scope of the present invention.
Of the present invention is a kind of aluminum bronze magnesium system duralumin, described aluminum bronze magnesium system duralumin is combined by aluminium, copper, magnesium, zinc, titanium and nickel six kinds of metal ingredients, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is respectively: described aluminium accounts for 88.5%-92.9%, described copper accounts for 1.9%-2.8%, described magnesium accounts for 2.3%-3.2%, described zinc accounts for 1.7%-2.6%, and described titanium accounts for 0.8%-1.6%, and described nickel accounts for 0.4%-1.3%.
Further, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is specially: described aluminium accounts for 92.3%, and described copper accounts for 2.1%, and described magnesium accounts for 2.4%, and described zinc accounts for 1.8%, and described titanium accounts for 0.9%, and described nickel accounts for 0.5%.
Further, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is specially: described aluminium accounts for 89.1%, and described copper accounts for 2.7%, and described magnesium accounts for 3.1%, and described zinc accounts for 2.5%, and described titanium accounts for 1.4%, and described nickel accounts for 1.2%.
In addition, by regulating the Different Weight per-cent of each composition in alloy, the alloy property height obtained is differed.
Of the present invention is a kind of aluminum bronze magnesium system duralumin, by adding the metallic elements such as copper, magnesium, zinc, titanium and nickel in the aluminium alloy taking aluminium as base, effectively can improve the intensity of aluminium alloy, improve plasticity, facilitate follow-up processing, and there is excellent electroconductibility, thermal conductivity and corrosion stability, expand the use range of industry.
The foregoing is only the specific embodiment of the present invention; but protection scope of the present invention is not limited thereto; any those of ordinary skill in the art are in the technical scope disclosed by the present invention; the change can expected without creative work or replacement, all should be encompassed within protection scope of the present invention.Therefore, the protection domain that protection scope of the present invention should limit with claims is as the criterion.
Claims (1)
1. an aluminum bronze magnesium system duralumin, it is characterized in that: described aluminum bronze magnesium system duralumin is combined by aluminium, copper, magnesium, zinc, titanium and nickel six kinds of metal ingredients, in described aluminum bronze magnesium system duralumin, shared by each composition, weight percent is specially: described aluminium accounts for 92.3%, described copper accounts for 2.1%, described magnesium accounts for 2.4%, described zinc accounts for 1.8%, and described titanium accounts for 0.9%, and described nickel accounts for 0.5%.
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CN201410306359.1A CN104046856B (en) | 2014-07-01 | 2014-07-01 | A kind of aluminum bronze magnesium system duralumin |
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CN201410306359.1A CN104046856B (en) | 2014-07-01 | 2014-07-01 | A kind of aluminum bronze magnesium system duralumin |
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CN104046856A CN104046856A (en) | 2014-09-17 |
CN104046856B true CN104046856B (en) | 2016-04-27 |
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CN110629081B (en) * | 2019-08-27 | 2021-06-22 | 江苏大学 | Novel heat-resistant high-strength high-plasticity corrosion-resistant Al-Cu-Mg-Zn-Ti series aluminum alloy and preparation method thereof |
JPWO2022211062A1 (en) * | 2021-03-31 | 2022-10-06 |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59193239A (en) * | 1983-04-15 | 1984-11-01 | Mitsubishi Alum Co Ltd | Al-alloy for magnetic disk substrate |
JPS63179043A (en) * | 1987-01-21 | 1988-07-23 | Furukawa Alum Co Ltd | Aluminum alloy for forming |
US5108519A (en) * | 1988-01-28 | 1992-04-28 | Aluminum Company Of America | Aluminum-lithium alloys suitable for forgings |
CN1831176A (en) * | 2005-03-07 | 2006-09-13 | 东北轻合金有限责任公司 | Super large-scale aluminium alloy free forging piece and its prodn. method |
CN102286682A (en) * | 2011-08-24 | 2011-12-21 | 吴江市精工铝字制造厂 | High-strength hard aluminum alloy |
CN102639733A (en) * | 2009-07-24 | 2012-08-15 | 美铝公司 | Improved 5xxx aluminum alloys and wrought aluminum alloy products made therefrom |
CN103131918A (en) * | 2011-11-29 | 2013-06-05 | 贵州铝厂 | Aluminum alloy material and preparing method thereof |
CN103667832A (en) * | 2013-11-20 | 2014-03-26 | 茹林宝 | Aluminum alloy pipe |
-
2014
- 2014-07-01 CN CN201410306359.1A patent/CN104046856B/en not_active Expired - Fee Related
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59193239A (en) * | 1983-04-15 | 1984-11-01 | Mitsubishi Alum Co Ltd | Al-alloy for magnetic disk substrate |
JPS63179043A (en) * | 1987-01-21 | 1988-07-23 | Furukawa Alum Co Ltd | Aluminum alloy for forming |
US5108519A (en) * | 1988-01-28 | 1992-04-28 | Aluminum Company Of America | Aluminum-lithium alloys suitable for forgings |
CN1831176A (en) * | 2005-03-07 | 2006-09-13 | 东北轻合金有限责任公司 | Super large-scale aluminium alloy free forging piece and its prodn. method |
CN102639733A (en) * | 2009-07-24 | 2012-08-15 | 美铝公司 | Improved 5xxx aluminum alloys and wrought aluminum alloy products made therefrom |
CN102286682A (en) * | 2011-08-24 | 2011-12-21 | 吴江市精工铝字制造厂 | High-strength hard aluminum alloy |
CN103131918A (en) * | 2011-11-29 | 2013-06-05 | 贵州铝厂 | Aluminum alloy material and preparing method thereof |
CN103667832A (en) * | 2013-11-20 | 2014-03-26 | 茹林宝 | Aluminum alloy pipe |
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