CN107937768A - A kind of extrusion casint aluminum alloy materials and preparation method thereof - Google Patents
A kind of extrusion casint aluminum alloy materials and preparation method thereof Download PDFInfo
- Publication number
- CN107937768A CN107937768A CN201711366311.XA CN201711366311A CN107937768A CN 107937768 A CN107937768 A CN 107937768A CN 201711366311 A CN201711366311 A CN 201711366311A CN 107937768 A CN107937768 A CN 107937768A
- Authority
- CN
- China
- Prior art keywords
- aluminum alloy
- alloy materials
- extrusion casint
- manganese
- silicon
- 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.)
- Granted
Links
Classifications
-
- 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
- C22C21/04—Modified aluminium-silicon alloys
-
- 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
-
- 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
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Extrusion Of Metal (AREA)
- Prevention Of Electric Corrosion (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Abstract
The present invention provides a kind of extrusion casint aluminum alloy materials and preparation method thereof, and extrusion casint aluminum alloy materials of the invention by weight, include following component：Silicon is 8% 12%；Iron is ＜ 0.9%；Copper is 1 4%；Manganese is 0.2 0.8%；Magnesium is 0.3% 0.8%, and zinc be ＜ 0.35%, and tin is≤0.01%, and cadmium is≤0.01%；Other impurities total amount and no more than 0.3%；Surplus is aluminium.The extrusion casint aluminium alloy of the present invention has preferable tensile strength, yield strength and hardness, and can meet heavy wall pipe shaping thin wall at the same time.
Description
Technical field
The invention belongs to aluminum alloy materials field, and in particular to a kind of extrusion casint aluminum alloy materials and preparation method thereof.
Background technology
Aluminium alloy is that one kind is conducive to the light-weighted more performance materials of equipment.By adjusting the difference of various elements component,
Aluminium alloy can have high heat conduction, high conductivity, high-yield strength, high-tensile, anticorrosive, high tenacity, high rigidity respectively
Etc. different performances.It is widely used in the fields such as communication, automobile, communications and transportation, power and space flight and aviation.With science and technology it is continuous
Development, requirement of the new and high technology for material are also higher and higher.In the past single performance can not meet that the development of technology will
Ask.Not only the chemical composition basic to its has strict requirements to present aluminum alloy materials, it is also necessary to meets various special make
With requiring, multiple performance is taken into account.Among these performances, some were even considered mutually in the past, and there are certain contradiction.
For different materials'use features, by itself specific requirement, various composition in material and its performance are rationally adjusted
Match somebody with somebody, optimize, be allowed to create a kind of corresponding new aluminum alloy materials be current so that one section of developing period from now on it is objective
Need.
ADC12 is the Japanese trade mark, also known as No. 12 aluminium material, Al-Si-Cu systems alloy, is that one kind can die casting also extrudable casting
Aluminium alloy, be adapted to cylinder head the cover, sensor stand, cylinder body class etc..Its die casting performance is good, and has certain power
Performance is learned, so being widely used in various general casting.But since die casting is using the mode of high speed and high pressure, die casting
Gas is inevitably involved in, influences quality.And extrusion casint is a kind of casting mode of low speed heavy pressure, its feature
It is volume gas phenomenon when can substantially reduce casting shaping in die cavity, improves the compactness of casting, improves the quality of casting.It
It is a kind of casting molding mode for meeting high performance requirements.For higher mechanical property requirements, existing ADC12 alloys
It cannot all be met by the way of die casting or extrusion casint.Therefore, it is excellent to be badly in need of a kind of performance ratio ADC12 alloys, and
It can meet the aluminum alloy materials of heavy wall pipe thin-walled squeeze cast form at the same time.
The content of the invention
In view of the deficiencies of the prior art, the present invention, which provides one kind, can meet heavy wall pipe shaping thin wall, and tension at the same time
Intensity, yield strength and the more preferable extrusion casint aluminum alloy materials of hardness and preparation method thereof.
The present invention provides a kind of extrusion casint aluminum alloy materials, in addition to aluminum, by weight, including following component：Silicon is
8%-12%；Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, and zinc is ＜ 0.35%.
Preferably, the extrusion casint aluminum alloy materials further include lead as≤0.1%.
Preferably, the extrusion casint aluminum alloy materials further include tin as≤0.01%.
Preferably, the extrusion casint aluminum alloy materials further include cadmium as≤0.01%.
The present invention also provides a kind of extrusion casint aluminum alloy materials, by weight, include following component：Silicon is 8%-
12%；Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, and zinc is ＜ 0.35%,；Tin is
≤ 0.01%, cadmium is≤0.01%；Other impurities total amount and no more than 0.3%；Surplus is aluminium.
Preferably, the iron is 0.15%-0.9%.
Preferably, the zinc is 0.05%-0.35%.
Preferably, silicon 10%-12%；Iron is 0.1%-0.5%；Copper is 2%-3%；Manganese is 0.4%-0.8%；Magnesium is
0.4%-0.8%, zinc 0.05-0.35%.
Preferably, silicon 10%-11.5%；Iron is 0.1%-0.3%；Copper is 2%-2.9%；Manganese is 0.4%-0.6%；
Magnesium is 0.4%-0.6%, zinc 0.05-0.1%.
The present invention also provides a kind of preparation method of above-mentioned extrusion casint aluminum alloy materials, include the following steps：
(1) aluminium ingot and silicon are put into smelting furnace, heating makes it be molten into molten metal；
(2) treat that molten metal temperature reaches 800 DEG C -880 DEG C, add manganese additive, ferro element additive and copper coin
Plain additive；
(3) molten metal is cooled to 760-780 DEG C；
(4) add refining agent and carry out refining purification, slagging-off；
(5) add magnesium and make its fusing, then add a small amount of antimony element additive and go bad, obtain molten aluminum；
(6) by temperature of aluminum liquid in 740-760 DEG C of scope cast aluminum alloys ingot.
The present invention extrusion casint aluminum alloy materials by after extrusion casint have higher tensile strength, yield strength and
Hardness, and can meet heavy wall pipe shaping thin wall at the same time.
Embodiment
Technical solution of the present invention is described in further detail with reference to specific embodiment, so that the technology of this area
Personnel can be better understood from the present invention and can be practiced, but illustrated embodiment is not as a limitation of the invention.
The embodiment of the present invention provides a kind of extrusion casint aluminum alloy materials, in addition to aluminum, by weight, including such as the following group
Point：Silicon is 8%-12%；Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, zinc ＜
0.35%.
In a preferred embodiment, extrusion casint aluminum alloy materials further include lead as≤0.1%.
In a preferred embodiment, extrusion casint aluminum alloy materials further include tin as≤0.01%.
In a preferred embodiment, extrusion casint aluminum alloy materials further include cadmium as≤0.01%.
The present invention also provides a kind of extrusion casint aluminum alloy materials, by weight, include following component：Silicon is 8%-
12%；Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, and zinc is ＜ 0.35%,；Tin is
≤ 0.01%, cadmium is≤0.01%；Other impurities total amount and no more than 0.3%；Surplus is aluminium.
In a preferred embodiment, iron 0.15%-0.9%.
In a preferred embodiment, zinc 0.05%-0.35%.
In a preferred embodiment, silicon 10%-12%；Iron is 0.1%-0.5%；Copper is 2%-3%；Manganese is 0.4%-
0.8%；Magnesium is 0.4%-0.8%, zinc 0.05-0.35%.
In a preferred embodiment, silicon 10%-11.5%；Iron is 0.1%-0.3%；Copper is 2%-2.9%；Manganese is
0.4%-0.6%；Magnesium is 0.4%-0.6%, zinc 0.05-0.1%.
The present invention also provides a kind of preparation method of above-mentioned extrusion casint aluminum alloy materials, include the following steps：
(1) aluminium ingot and silicon are put into smelting furnace, heating makes it be molten into molten metal；
(2) treat that molten metal temperature reaches 800 DEG C -880 DEG C, add manganese additive, ferro element additive and copper coin
Plain additive；
(3) molten metal is cooled to 760-780 DEG C；
(4) add refining agent and carry out refining purification, slagging-off；
(5) add magnesium and make its fusing, then add a small amount of antimony element additive and go bad, obtain molten aluminum；
(6) by temperature of aluminum liquid in 740-760 DEG C of scope cast aluminum alloys ingot.
The present invention extrusion casint aluminum alloy materials by after extrusion casint have preferable tensile strength, yield strength and
Hardness, and can meet heavy wall pipe shaping thin wall at the same time.
The extrusion casint aluminium alloy of the embodiment of the present invention can greatly improve the properties of casting after T6 is heat-treated.
The extrusion casint aluminum alloy materials of the embodiment of the present invention are suitable for extrusion casint, material good moldability.Extrudable casting
Thick member is made, can also meet the thin-wall part extrusion casint of 0.35-0.5mm thickness.It is adapted to various mechanical structured members, communication apparatus part
Deng.
Embodiment 1
Raw material proportioning, count by weight percentage：Silicon, content 11.06%；Iron, content 0.165%；Copper, content are
2.75%；Manganese, content 0.475%；Magnesium, content 0.494%, zinc, content 0.0695%, lead, content for≤
0.0021%；Tin, content are≤0.00058%；Cadmium, content are≤0.00052%；Surplus is aluminium.
Alloy is prepared according to said ratio, step is as follows：
Aluminium ingot and silicon are put into smelting furnace, and heating makes it be molten into metallic solution, the temperature of metallic solution is reached 830
℃；Manganese additive, ferro element additive and copper additive carry out alloying in metallic solution, are completely melt it
Molten metal is cooled to 770 DEG C afterwards, refining agent is then added and carries out refining purification, slagging-off；Add magnesium and make its fusing, adopt
Degasification is carried out to metallic solution with nitrogen then to metallic solution inspection by sampling component, is subsequently added into additive containing antimony element, then
By temperature of aluminum liquid in 740-760 DEG C of scope cast aluminum alloys ingot.
Embodiment 2
Raw material proportioning, count by weight percentage：Silicon, content 10.87%；Iron, content 0.189%；Copper, content are
2.75%；Manganese, content 0.472%；Magnesium, content 0.472%, zinc, content 0.0689%, lead, content for≤
0.0026%；Tin, content are≤0.00065%；Cadmium, content are≤0.00060%；Surplus is aluminium.
Alloy is prepared according to said ratio, step is as follows：
Aluminium ingot and silicon are put into smelting furnace, and heating makes it be molten into metallic solution, the temperature of metallic solution is reached 830
℃；Manganese additive, ferro element additive and copper additive carry out alloying in metallic solution, are completely melt it
Molten metal is cooled to 770 DEG C afterwards, refining agent is then added and carries out refining purification, slagging-off；Add magnesium and make its fusing, adopt
Degasification is carried out to metallic solution with nitrogen then to metallic solution inspection by sampling component, is subsequently added into additive containing antimony element, then
By temperature of aluminum liquid in 740-760 DEG C of scope cast aluminum alloys ingot.
Comparative example
By Japanese ADC12 as a comparison case, the main chemical compositions standard of ADC12 is：
Copper (Cu) 1.5-3.5, silicon (Si) 9.6-12.0, magnesium (Mg)≤0.3, zinc (Zn)≤1.0, iron (Fe)≤1.3, manganese
(Mn)≤0.5, tin (Sn)≤0.3, lead (Pb)≤0.1, cadmium (Cd)≤0.005, surplus are aluminium (Al).
Effect example
Mechanics Performance Testing
By the ADC12 alloys of embodiment 1, embodiment 2 and comparative example by carrying out tensile strength, surrender after extrusion casint by force
The test of degree, elongation percentage, hardness.Specific data are as shown in table 1.
Table 1
The extrusion casint aluminium alloy tension that the present embodiment 1 and embodiment 2 are prepared it can be seen from the data of table 1 is strong
Spend ＞ 300MPa, yield strength ＞ 200MPa, elongation percentage ＞ 1.8%, hardness ＞ 80HB.Tensile strength, yield strength and extension
The data of rate are all higher than the data of ADC12 alloys, and hardness is suitable with the hardness of ADC12 alloys.And the extrusion casint of the present invention
Aluminium alloy can meet heavy wall pipe shaping thin wall at the same time, and alternative ADC12 alloys use.
The foregoing is merely the preferred embodiment of the present invention, is not intended to limit the scope of the invention, every utilization
The equivalent structure or equivalent flow shift that present specification is made, is directly or indirectly used in other relevant technologies
Field, is included within the scope of the present invention.
Claims (10)
- A kind of 1. extrusion casint aluminum alloy materials, it is characterised in that in addition to aluminum, by weight, including following component：Silicon is 8%-12%；Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, and zinc is ＜ 0.35%.
- 2. extrusion casint aluminum alloy materials as claimed in claim 1, it is characterised in that further include lead as≤0.1%.
- 3. extrusion casint aluminum alloy materials as claimed in claim 1, it is characterised in that further include tin as≤0.01%.
- 4. extrusion casint aluminum alloy materials as claimed in claim 1, it is characterised in that further include cadmium as≤0.01%.
- 5. a kind of extrusion casint aluminum alloy materials, it is characterised in that by weight, include following component：Silicon is 8%-12%； Iron is ＜ 0.9%；Copper is 1-4%；Manganese is 0.2%-0.8%；Magnesium is 0.3%-0.8%, and zinc is ＜ 0.35%,；Tin for≤ 0.01%, cadmium is≤0.01%；Other impurities total amount and no more than 0.3%；Surplus is aluminium.
- 6. extrusion casint aluminum alloy materials as claimed in claim 5, it is characterised in that the iron is 0.15%-0.9%.
- 7. extrusion casint aluminum alloy materials as claimed in claim 5, it is characterised in that the zinc is 0.05%-0.35%.
- 8. extrusion casint aluminum alloy materials as claimed in claim 5, it is characterised in that by weight, silicon 10%- 12%；Iron is 0.1%-0.5%；Copper is 2%-3%；Manganese is 0.4%-0.8%；Magnesium is 0.4%-0.8%, zinc 0.05- 0.35%.
- 9. extrusion casint aluminum alloy materials as claimed in claim 8, it is characterised in that by weight, silicon 10%- 11.5%；Iron is 0.1%-0.3%；Copper is 2%-2.9%；Manganese is 0.4%-0.6%；Magnesium is 0.4%-0.6%, and zinc is 0.05-0.1%.
- 10. the preparation method of extrusion casint aluminum alloy materials as claimed in claim 5, it is characterised in that include the following steps：(1) aluminium ingot and silicon are put into smelting furnace, heating makes it be molten into molten metal；(2) treat that molten metal temperature reaches 800 DEG C -880 DEG C, add manganese additive, ferro element additive and copper and add Add agent；(3) molten metal is cooled to 760-780 DEG C；(4) add refining agent and carry out refining purification, slagging-off；(5) add magnesium and make its fusing, then add a small amount of antimony element additive and go bad, obtain molten aluminum；(6) by temperature of aluminum liquid in 740-760 DEG C of scope cast aluminum alloys ingot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711366311.XA CN107937768B (en) | 2017-12-18 | 2017-12-18 | Extrusion casting aluminum alloy material and preparation method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711366311.XA CN107937768B (en) | 2017-12-18 | 2017-12-18 | Extrusion casting aluminum alloy material and preparation method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107937768A true CN107937768A (en) | 2018-04-20 |
| CN107937768B CN107937768B (en) | 2019-12-17 |
Family
ID=61943739
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711366311.XA Active CN107937768B (en) | 2017-12-18 | 2017-12-18 | Extrusion casting aluminum alloy material and preparation method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107937768B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108396205A (en) * | 2018-04-28 | 2018-08-14 | 广州致远新材料科技有限公司 | A kind of aluminum alloy materials and preparation method thereof |
| CN112391562A (en) * | 2019-11-26 | 2021-02-23 | 比亚迪股份有限公司 | Aluminum alloy and preparation method thereof |
| CN113444925A (en) * | 2020-03-24 | 2021-09-28 | 比亚迪股份有限公司 | Aluminum alloy and preparation method thereof |
| WO2024099374A1 (en) * | 2022-11-11 | 2024-05-16 | 蔚来动力科技(合肥)有限公司 | Die-cast aluminum alloy material, preparation method therefor, and use thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004091822A (en) * | 2002-08-29 | 2004-03-25 | Denso Corp | High-strength aluminum alloy casting and its manufacturing method |
| US20070246132A1 (en) * | 2006-03-27 | 2007-10-25 | Dasgupta Rathindra | Squeeze cast rear suspension components using ADC12-T4 aluminum alloy |
| CN101569926A (en) * | 2009-05-27 | 2009-11-04 | 中国兵器工业第五二研究所 | Method for casting aluminum piston with insert ring and cooling coil pipe |
| CN102943192A (en) * | 2012-10-29 | 2013-02-27 | 中国兵器工业第五二研究所 | Aluminum piston manufacturing method |
| CN105220032A (en) * | 2015-11-11 | 2016-01-06 | 太仓海嘉车辆配件有限公司 | A kind of aluminium alloy for high strength and endurance quality support and preparation method thereof |
| CN106119625A (en) * | 2016-08-30 | 2016-11-16 | 太仓海嘉车辆配件有限公司 | A kind of automobile steering device gear case variator Al-alloy casing and preparation method thereof |
| CN107217182A (en) * | 2017-06-08 | 2017-09-29 | 江苏华晟电气科技有限公司 | The manufacture method of aluminium alloy oil pump case and its aluminium alloy oil pump case of manufacture |
-
2017
- 2017-12-18 CN CN201711366311.XA patent/CN107937768B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004091822A (en) * | 2002-08-29 | 2004-03-25 | Denso Corp | High-strength aluminum alloy casting and its manufacturing method |
| US20070246132A1 (en) * | 2006-03-27 | 2007-10-25 | Dasgupta Rathindra | Squeeze cast rear suspension components using ADC12-T4 aluminum alloy |
| CN101569926A (en) * | 2009-05-27 | 2009-11-04 | 中国兵器工业第五二研究所 | Method for casting aluminum piston with insert ring and cooling coil pipe |
| CN102943192A (en) * | 2012-10-29 | 2013-02-27 | 中国兵器工业第五二研究所 | Aluminum piston manufacturing method |
| CN105220032A (en) * | 2015-11-11 | 2016-01-06 | 太仓海嘉车辆配件有限公司 | A kind of aluminium alloy for high strength and endurance quality support and preparation method thereof |
| CN106119625A (en) * | 2016-08-30 | 2016-11-16 | 太仓海嘉车辆配件有限公司 | A kind of automobile steering device gear case variator Al-alloy casing and preparation method thereof |
| CN107217182A (en) * | 2017-06-08 | 2017-09-29 | 江苏华晟电气科技有限公司 | The manufacture method of aluminium alloy oil pump case and its aluminium alloy oil pump case of manufacture |
Non-Patent Citations (1)
| Title |
|---|
| 中国标准出版社 等: "《中国机械工业标准汇编 铸造卷 下》", 30 April 2002 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108396205A (en) * | 2018-04-28 | 2018-08-14 | 广州致远新材料科技有限公司 | A kind of aluminum alloy materials and preparation method thereof |
| CN112391562A (en) * | 2019-11-26 | 2021-02-23 | 比亚迪股份有限公司 | Aluminum alloy and preparation method thereof |
| EP4067521A4 (en) * | 2019-11-26 | 2023-01-04 | BYD Company Limited | Aluminum alloy and preparation method therefor |
| CN113444925A (en) * | 2020-03-24 | 2021-09-28 | 比亚迪股份有限公司 | Aluminum alloy and preparation method thereof |
| CN113444925B (en) * | 2020-03-24 | 2022-11-11 | 比亚迪股份有限公司 | Aluminum alloy and preparation method thereof |
| WO2024099374A1 (en) * | 2022-11-11 | 2024-05-16 | 蔚来动力科技(合肥)有限公司 | Die-cast aluminum alloy material, preparation method therefor, and use thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107937768B (en) | 2019-12-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110551924B (en) | Aluminum alloy and preparation method and application thereof | |
| CN102753715B (en) | There is magnesium alloy and the manufacture method thereof of outstanding ignition resistance and mechanical performance | |
| CN107829000B (en) | Die-casting aluminum alloy material and preparation method thereof | |
| CN105296818A (en) | Aluminum alloy and preparation method and application thereof | |
| CN109652685B (en) | A kind of high thermal conductivity high corrosion resistant casting aluminium alloy and preparation method thereof | |
| CN107937768A (en) | A kind of extrusion casint aluminum alloy materials and preparation method thereof | |
| CN112176231A (en) | High-strength and high-toughness die-casting aluminum alloy for automobile structural member and preparation method and application thereof | |
| CN105838936B (en) | A kind of high heat conduction cast aluminium alloy gold and preparation method thereof | |
| CN110029250A (en) | High-elongation birmastic and its compression casting preparation method | |
| CN104561688A (en) | Heat-resistant cast aluminum alloy and gravity casting method thereof | |
| CN104004945B (en) | Containing the Al-Zn-Mg-Zr Alloy And Preparation Method of scandium high strength | |
| CN109732239A (en) | High magnesium manganese chromium cobalt aluminium alloy and preparation method thereof for manufacturing welding wire | |
| KR20160011136A (en) | Magnesium alloy having improved corrosion resistance and method for manufacturing magnesium alloy member using the same | |
| CN114457263A (en) | High-strength high-toughness high-heat-conductivity die-casting aluminum alloy and manufacturing method thereof | |
| CN104630577A (en) | Heat-resistant cast aluminum alloy and pressure casting method thereof | |
| CN108950319A (en) | A kind of high thermal conductivity aluminum alloy materials and preparation method thereof | |
| CN111041302A (en) | Novel high-strength die-casting aluminum alloy with remarkable natural aging strengthening characteristic and preparation method thereof | |
| CN107881378A (en) | Aluminum alloy composition, aluminum alloy member, the preparation method of communication product and aluminum alloy member | |
| CN111575554A (en) | Production method of high-strength wear-resistant aluminum alloy | |
| CN105401005A (en) | Al-Si alloy material and production method thereof | |
| CN117965969A (en) | Aluminum alloy and preparation method thereof, casting and preparation method thereof and vehicle | |
| JP4201434B2 (en) | Method for producing high-strength aluminum alloy extruded material with excellent corrosion resistance | |
| CN115433857A (en) | Lightweight aluminum-silicon alloy with good plasticity and preparation process thereof | |
| CN101914704B (en) | Cr-containing creep-resisting extruded zinc alloy and preparation method thereof | |
| CN104264018A (en) | Aluminum alloy and manufacturing method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |