CN110284015A - 6 line aluminium alloys of one kind and preparation method thereof - Google Patents
6 line aluminium alloys of one kind and preparation method thereof Download PDFInfo
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- CN110284015A CN110284015A CN201910639926.8A CN201910639926A CN110284015A CN 110284015 A CN110284015 A CN 110284015A CN 201910639926 A CN201910639926 A CN 201910639926A CN 110284015 A CN110284015 A CN 110284015A
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/057—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with copper as the next major constituent
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Abstract
The present invention relates to a kind of 6 line aluminium alloys and preparation method thereof, 6 line aluminium alloy is grouped as by the group of following weight percentage: the iron of 0.1-0.145%, the silicon of 0.71-0.85%, the copper of 0.71-0.82%, the titanium of 0.12-0.25%, the magnesium of 0.65-0.95%, the manganese of 0.15-0.2%, the zirconium of 0.01-0.05%, the strontium of 0.001-0.005%, the zinc not higher than 0.025%, the vanadium not higher than 0.05% and the chromium not higher than 0.05%, surplus are aluminium.For the yield strength of 6 line aluminium alloys of the invention up to 370MPa or more, it 7 is alloy strength that mechanical property, which can match in excellence or beauty,.
Description
Technical field
The present invention relates to aluminium alloy technology, in particular to a kind of 6 line aluminium alloys and preparation method thereof.
Background technique
Aluminium alloy is added alloying elements by fine aluminium and is made, and the Al-Mn that manganese element is developed is added such as in fine aluminium
Alloy adds copper in fine aluminium and develops made of Al-Cu alloy, in fine aluminium while adding copper and magnesium elements develop Al-Cu-
Mg system duralumin, hard alumin ium alloy, adding zinc, magnesium, copper develops Al-Zn-Mg-Cu 7 series extra super duralumin alloy etc. simultaneously in fine aluminium.Aluminium closes
The feature of gold is light, intensity height, good heat dissipation, good hand touch and easy anode oxidation coloration.Under same intensity requirement, aluminium alloy
Components can be made thinner and light than plastics, while being also able to satisfy the Highgrade integration of 3C Product, lightening, micromation, resisting
Fall the requirement for hitting electromagnetic shielding and heat dissipation.The information technoloy equipments such as mobile phone, tablet computer, laptop on the market use now
Aluminium alloy is commonly 6 line aluminium alloys, with the development of science and technology 6 traditional wrought aluminium alloys have been difficult to meet in terms of intensity
The requirement of high-end product is especially bent in resistance to deformation, in terms of the indexs such as anti-drop deformation.
In existing 6 line aluminium alloy, mechanical property, such as yield strength, it is still necessary to further increase.
Summary of the invention
The technical problems to be solved by the present invention are: providing 6 line aluminium alloys of one kind and preparation method thereof, its mechanics can be improved
Performance is good.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention are as follows:
A kind of 6 line aluminium alloys, are grouped as: iron, the 0.71-0.85% of 0.1-0.145% by the group of following weight percentage
Silicon, the copper of 0.71-0.82%, the titanium of 0.12-0.25%, the magnesium of 0.65-0.95%, the manganese of 0.15-0.2%, 0.01-
0.05% zirconium, the strontium of 0.001-0.005%, the zinc not higher than 0.025%, the vanadium not higher than 0.05% and it is not higher than 0.05%
Chromium, surplus is aluminium.
A kind of preparation method of 6 line aluminium alloy is grouped as according to the group of 6 above-mentioned line aluminium alloys and successively carries out ingredient, melts
Change, skim, alloying, casting, homogenizing annealing and sawing operation, obtaining 6 line aluminium alloy.
The beneficial effects of the present invention are:
6 line aluminium alloys of the invention promote Si, Cu ratio in the design of its component, while meeting the requirement of anode bloom,
Suitable for can anode highlight various colors, emphasis solve after anode it is numb, get confused and brightness permeability problem；By increase Cu,
Si increases excessive phase, Mg2Si phase can promote intensity；Meanwhile Mn, Sr, Ti, Zr component content are rationally controlled, to improve anti-crystalline substance
Between corrosive nature so that product grains are uniform in size, it is penetrating to go out light conducive to product surface after anode；6 line aluminium alloys of the invention
It is designed by said components, after tested, yield strength is 370MPa or more, and can match in excellence or beauty 7 is alloy strength, has good power
Learn performance.
Specific embodiment
To explain the technical content, the achieved purpose and the effect of the present invention in detail, it is explained below in conjunction with embodiment.
The most critical design of the present invention is: promoting Si, Cu ratio, and rationally close in the component design of 6 line aluminium alloys
Reason control Mn, Sr, Ti, Zr component content, to improve its yield strength.
6 line aluminium alloys of the invention, are grouped as by the group of following weight percentage: iron, the 0.71- of 0.1-0.145%
0.85% silicon, the copper of 0.71-0.82%, the titanium of 0.12-0.25%, the magnesium of 0.65-0.95%, 0.15-0.2% manganese,
It the zirconium of 0.01-0.05%, the strontium of 0.001-0.005%, the zinc not higher than 0.025%, the vanadium not higher than 0.05% and is not higher than
0.05% chromium, surplus are aluminium.
A kind of preparation method of 6 line aluminium alloy is grouped as according to the group of 6 above-mentioned line aluminium alloys and successively carries out ingredient, melts
Change, skim, alloying, casting, homogenizing annealing and sawing operation, obtaining 6 line aluminium alloy.
As can be seen from the above description, the beneficial effects of the present invention are:
6 line aluminium alloys of the invention promote Si, Cu ratio in the design of its component, while meeting the requirement of anode bloom,
Suitable for can anode highlight various colors, emphasis solve after anode it is numb, get confused and brightness permeability problem；By increase Cu,
Si increases excessive phase, Mg2Si phase can promote intensity；Meanwhile Mn, Sr, Ti, Zr component content are rationally controlled, to improve anti-crystalline substance
Between corrosive nature so that product grains are uniform in size, it is penetrating to go out light conducive to product surface after anode；6 line aluminium alloys of the invention
It is designed by said components, after tested, yield strength is 370MPa or more, and can match in excellence or beauty 7 is alloy strength, has good power
Learn performance.
The embodiment of the present invention one are as follows:
6 line aluminium alloys of the present embodiment, are prepared using following preparation methods:
The group of (1) 6 line aluminium alloy is grouped as: 6 line aluminium alloy is grouped as by the group of following weight percentage: 0.1%
Iron, 0.71% silicon, 0.71% copper, 0.12% titanium, 0.65% magnesium, 0.15% manganese, 0.01% zirconium, 0.001%
Strontium, 0.025% zinc, 0.05% vanadium and 0.05% chromium, surplus is aluminium；Wherein, the total impurities element of 6 line aluminium alloys
Content is lower than 0.1%, and the content of the single impurity element of 6 line aluminium alloy is not higher than 0.05%.
(2) be grouped as according to the group of 6 line aluminium alloys successively carry out ingredient, melt, skim, alloying, casting, homogenization are moved back
Fire and sawing operation obtain 6 line aluminium alloy；The temperature of the casting operation is 685-710 DEG C, is controlled during casting operation
The content of hydrogen manufacturing is 0.12mg/100gAL；The holding temperature of the homogenization practice be 560 ± 10 DEG C, soaking time be 8 ±
0.25h。
The embodiment of the present invention two are as follows:
6 line aluminium alloys of the present embodiment, only " group of 6 line aluminium alloys is grouped as: 6 line aluminium alloy is by following in step (1)
The group of weight percent is grouped as: 0.145% iron, 0.85% silicon, 0.82% copper, 0.25% titanium, 0.95% magnesium,
0.2% manganese, 0.05% zirconium, 0.005% strontium, 0.02% zinc, 0.03% vanadium and 0.03% chromium, surplus is aluminium "
Different from embodiment one, other are the same as example 1.
The embodiment of the present invention three are as follows:
6 line aluminium alloys of the present embodiment, only " group of 6 line aluminium alloys is grouped as: 6 line aluminium alloy is by following in step (1)
The group of weight percent is grouped as: 0.125% iron, 0.8% silicon, 0.78% copper, 0.19% titanium, 0.8% magnesium,
0.18% manganese, 0.03% zirconium, 0.003% strontium, 0.015% zinc, 0.02% vanadium and 0.02% chromium, surplus is
Aluminium " is different from embodiment one, other are the same as example 1.
The embodiment of the present invention four are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the silicon is
0.75%, the content of the copper is 0.78%." different from embodiment one, other are the same as example 1.
The embodiment of the present invention five are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the silicon is
0.85%, the content of the copper is 0.82%." different from embodiment one, other are the same as example 1.
The embodiment of the present invention six are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the silicon is
0.79%, the content of the copper is 0.81%." different from embodiment one, other are the same as example 1.
The embodiment of the present invention seven are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the magnesium is
0.85%." different from example IV, other are identical as example IV.
The embodiment of the present invention eight are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the magnesium is
0.95%." different from example IV, other are identical as example IV.
The embodiment of the present invention nine are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the magnesium is
0.9%." different from example IV, other are identical as example IV.
The embodiment of the present invention ten are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.12%, the content of the manganese is 0.15%, and the content of the zirconium is 0.01%, and the content of the strontium is 0.001%." and it is real
It is different to apply example four, other are identical as example IV.
The embodiment of the present invention 11 are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.15%, the content of the manganese is 0.18%, and the content of the zirconium is 0.02%, and the content of the strontium is 0.003%." and it is real
It is different to apply example four, other are identical as example IV.
The embodiment of the present invention 12 are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.14%, the content of the manganese is 0.16%, and the content of the zirconium is 0.015%, and the content of the strontium is 0.002%." and it is real
It is different to apply example four, other are identical as example IV.
The embodiment of the present invention 13 are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.18%, the content of the manganese is 0.18%, and the content of the zirconium is 0.03%, and the content of the strontium is 0.001% " and implementation
Example four is different, other are identical as example IV.
The embodiment of the present invention 14 are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.25%, the content of the manganese is 0.2%, and the content of the zirconium is 0.05%, and the content of the strontium is 0.003% " and implementation
Example four is different, other are identical as example IV.
The embodiment of the present invention 15 are as follows:
6 line aluminium alloys of the present embodiment, only the group of (1) 6 line aluminium alloy of step be grouped as in " content of the titanium is
0.2%, the content of the manganese is 0.19%, and the content of the zirconium is 0.04%, and the content of the strontium is 0.002% " and implementation
Example four is different, other are identical as example IV.
Measure of merit
The yield strength for 6 line aluminium alloys that embodiment one to embodiment 15 obtains is tested.Specific test side
Method may be selected in the prior art to the common testing methods of the yield strength of aluminium alloy.
The result shows that the yield strength for 6 line aluminium alloys that embodiment one to embodiment 15 obtains is successively are as follows: 372MPa,
375MPa、378MPa、382MPa、386MPa、389MPa、386MPa、384MPa、385MPa、388MPa、383MPa、382MPa、
383MPa、386MPa、384MPa。
In conclusion the yield strength of 6 line aluminium alloy provided by the invention is 370MPa or more, can match in excellence or beauty 7 is that alloy is strong
Degree has good mechanical property.
The above description is only an embodiment of the present invention, is not intended to limit the scope of the invention, all to utilize this hair
Equivalents made by bright specification are applied directly or indirectly in relevant technical field, similarly include of the invention
In scope of patent protection.
Claims (7)
1. a kind of 6 line aluminium alloys, which is characterized in that be grouped as by the group of following weight percentage: the iron of 0.1-0.145%,
The silicon of 0.71-0.85%, the copper of 0.71-0.82%, the titanium of 0.12-0.25%, the magnesium of 0.65-0.95%, 0.15-0.2%
Manganese, the zirconium of 0.01-0.05%, the strontium of 0.001-0.005%, not higher than 0.025% zinc, not higher than 0.05% vanadium and not high
In 0.05% chromium, surplus is aluminium.
2. 6 line aluminium alloy according to claim 1, which is characterized in that the content of the total impurities element of 6 line aluminium alloy
Lower than 0.1%, the content of the single impurity element of 6 line aluminium alloy is not higher than 0.05%.
3. 6 line aluminium alloy according to claim 1, which is characterized in that the content of the silicon is 0.75-0.85%, described
The content of copper is 0.78-0.82%.
4. 6 line aluminium alloy according to claim 3, which is characterized in that the content of the magnesium is 0.85-0.95%.
5. 6 line aluminium alloy according to claim 1, which is characterized in that the content of the titanium is 0.12-0.15%, described
The content of manganese is 0.15-0.18%, and the content of the zirconium is 0.01-0.02%, and the content of the strontium is 0.001-0.003%.
6. 6 line aluminium alloy according to claim 1, which is characterized in that the content of the titanium is 0.18-0.25%, described
The content of manganese is 0.18-0.2%, and the content of the zirconium is 0.03-0.05%, and the content of the strontium is 0.001-0.003%.
7. a kind of preparation method of 6 line aluminium alloys, which is characterized in that according to as claimed in any one of claims 1 to 66 be that aluminium closes
The group of gold, which is grouped as, successively to be carried out ingredient, melts, skims, alloying, casting, homogenizing annealing and sawing operation, obtains described 6
Line aluminium alloy.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910639926.8A CN110284015A (en) | 2019-07-16 | 2019-07-16 | 6 line aluminium alloys of one kind and preparation method thereof |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110951982A (en) * | 2019-11-29 | 2020-04-03 | 辽宁忠旺集团有限公司 | Production process for improving intergranular corrosion resistance of 6-series aluminum alloy |
| CN114293073A (en) * | 2021-12-28 | 2022-04-08 | 广东和胜工业铝材股份有限公司 | Aluminum-based material and preparation method and application thereof |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4614552A (en) * | 1983-10-06 | 1986-09-30 | Alcan International Limited | Aluminum alloy sheet product |
| CN103484736A (en) * | 2013-10-10 | 2014-01-01 | 东北大学 | Ultrahigh strength 6000 series aluminium alloy and preparation method thereof |
-
2019
- 2019-07-16 CN CN201910639926.8A patent/CN110284015A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4614552A (en) * | 1983-10-06 | 1986-09-30 | Alcan International Limited | Aluminum alloy sheet product |
| CN103484736A (en) * | 2013-10-10 | 2014-01-01 | 东北大学 | Ultrahigh strength 6000 series aluminium alloy and preparation method thereof |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110951982A (en) * | 2019-11-29 | 2020-04-03 | 辽宁忠旺集团有限公司 | Production process for improving intergranular corrosion resistance of 6-series aluminum alloy |
| CN114293073A (en) * | 2021-12-28 | 2022-04-08 | 广东和胜工业铝材股份有限公司 | Aluminum-based material and preparation method and application thereof |
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Application publication date: 20190927 |