CN107794419A - A kind of aluminium alloy polynary intermediate alloy and preparation method thereof - Google Patents

A kind of aluminium alloy polynary intermediate alloy and preparation method thereof Download PDF

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Publication number
CN107794419A
CN107794419A CN201710440741.5A CN201710440741A CN107794419A CN 107794419 A CN107794419 A CN 107794419A CN 201710440741 A CN201710440741 A CN 201710440741A CN 107794419 A CN107794419 A CN 107794419A
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alloy
intermediate alloy
preparation
aluminium
polynary
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CN107794419B (en
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陈卫平
兰天翔
柳术平
王晓平
胡双
王力
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HUNAN ORIENTAL SCANDIUM INDUSTRY CO LTD
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HUNAN ORIENTAL SCANDIUM INDUSTRY CO LTD
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/026Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/03Making non-ferrous alloys by melting using master alloys

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture And Refinement Of Metals (AREA)

Abstract

The invention discloses a kind of aluminium alloy polynary intermediate alloy and preparation method thereof, the polynary intermediate alloy quality group turns into Mg 2~6%, Mn 0.2~0.8%, Sc 0.08~0.8%, Zr 0.08~0.4%, surplus Al;Alloy prepares and uses fused salt thermit reduction.The present invention largely reduces the content of scandium zirconium in intermediate alloy, improves scandium zirconium reduction recovery rate, reduces the production cost of Mo-bearing granitoid;It is aided with that magnesium is manganese strengthened simultaneously, the combination property of polynary intermediate alloy of the invention is good, has and strengthens modification effect well.

Description

A kind of aluminium alloy polynary intermediate alloy and preparation method thereof
Technical field
The present invention relates to a kind of aluminium alloy polynary intermediate alloy and preparation method thereof, belong to technical field of aluminum alloy technology.
Background technology
The lightweight of Aero-Space, high ferro and automobile, greatly promotes the development of wrought aluminium alloy, and high-strength light aluminium alloy obtains Obtain extensive use.In the production of wrought aluminium alloy material, addition metal scandium can be obviously improved the performance of aluminium alloy, therefore promote Application of the scandium in aluminium alloy is entered.
Expensive due to scandium, a large amount of additions of scandium can cause the cost increase of aluminium alloy, therefore on the one hand need to seek Seek the alloying element instead of metal scandium.Chinese invention patent discloses aluminium, Seandium, zirconium intermediate alloy and its production of a kind of aluminium alloy Method (application number:2016103412981) it is, to replace part scandium with zirconium, performance is improved by scandium, zirconium.
The feed postition of other alloying elements such as scandium zirconium adds generally in the form of intermediate alloy, as Al-Sc (Sc 2%), Al-Zr (Zr 5%) intermediate alloy, scandium and zirconium are the strong metamorphism elements of aluminium alloy, and wherein scandium is best alterant element, But cost is high.In 5 systems (Al-Mg) and 7 systems (Al-Mg-Zn) aluminium alloy, substitute scandium, the compound addition of scandium zirconium with Partial Elements zirconium Change agent effect is good, cost is excellent.Scandium zirconium can significantly improve yield strength, welding performance, corrosion resisting property and the processability of alloy Energy.On the other hand it is the cost for reducing scandium bearing master alloy.
In Al-Sc (2%) intermediate alloy actual production process, using fused salt aluminum reduction method, for contents of scandium alloy, Scandium is higher, is limited by this method, and the difficulty of production is bigger, in order to reach 2%Sc contents, it is necessary to increase scandium oxide input amount, lead The increase of Al-Sc (2%) production cost is caused, reduces that Sc recovery is low, and component segregation is big that (solid solubility of the scandium in aluminium is low, produces Segregation), and the problem of zirconium uneven components, deviation is big similarly be present in Al-Zr (5%).
The content of the invention
Present invention deficiency for more than, further reduces the content of scandium zirconium, production process is more in the production of intermediate alloy Be easily controlled, component segregation is small, while keep scandium zirconium high reduction yield (>95%) production cost, is reduced, while adds magnesium manganese Reinforced alloys, keep intermediate alloy that there is rotten well strengthen function.
The technical scheme is that, there is provided a kind of polynary intermediate alloy of aluminium alloy, the polynary intermediate alloy quality Form as Mg 2~6%, Mn 0.2~0.8%, Sc 0.08~0.8%, Zr 0.08~0.4%, surplus Al.
Sc content is preferably 0.4~0.8%;More preferably 0.7~0.8%.
The preparation method of above-mentioned polynary intermediate alloy, comprises the following steps:
(1) it is 100 by mass ratio:1~7 pure Al and fused salt is put into smelting furnace, is heated to melting, and 850~980 At DEG C, 0.5-1 hours are incubated;
(2) 720~760 DEG C, metal Mn and Mg are cooled to, is incubated 10-20 minutes, stirring homogenizes alloy;
(3) aluminium liquid surface fused salt is removed, and argon gas is passed through in aluminium liquid, degasification, after standing, is skimmed;
(4) alloy molten solution is obtained into polynary intermediate alloy with water cooled mo(u)ld ingot casting.
Preferably, in step (4), 700~730 DEG C of the temperature of ingot casting is controlled.
Preferably, the smelting furnace is non-vacuum melting stove.
Preferably, the quality group of each composition turns into the fused salt:
Preferably, in step (3), the time of standing is 5~10 minutes.
Preferably, in step (2), metal Mn is first added, adds metal Mg.The magnesium residence time can so be shortened, subtracted The scaling loss of few magnesium.
The present invention sets out from aluminium, Seandium, zirconium intermediate alloy (2wt%Sc, 1-2wt%Zr), further reduces the content of scandium zirconium, makes Sc content is 0.08-0.8%, and Zr content is 0.08-0.4%, at the same be incorporated appropriate magnesium, manganese element form the present invention Intermediate alloy, magnesium manganese is all reinforced alloys element, while manganese also has the effect for reducing harmful element iron in aluminium.It is produced into reduction This while, composition slightly adjust i.e. configurable other 5 be 7 be alloy.
The present invention is using inexpensive Sc2O3、ZrO2For raw material obtain in high yield scandium zirconium (>95%), with reference to water cooled mo(u)ld Quick cooling technique so that the second phase Al of scandium zirconium3(ScZr) particle is tiny, is evenly distributed.
The invention has the advantages that scandium bearing master alloy or aluminium, Seandium, zirconium intermediate alloy are replaced with polynary intermediate alloy, compared with Reduce to big degree the content of intermediate alloy scandium zirconium, improve the reduction yield of scandium zirconium, reduce the production cost of aluminium alloy;Together The manganese strengthened alloying element of Shi Zengjia magnesium, manganese also have the effect for reducing harmful element iron in aluminium.The polynary intermediate alloy of the present invention Combination property is good, has preferably rotten reinforcing effect.
Embodiment
With reference to embodiment, the invention will be further described.
Embodiment 1:In 200kg middle frequency furnaces, 95kg aluminium is put into graphite crucible, and adds and is pre-mixed drying Good 5.17kg fused salts are (wherein:Sc2O3 1.07kg、ZrO2 0.4kg、NH4F 2.0kg、NaF 0.25kg、KCl 1.3kg、 MgCl20.15kg).950 DEG C are heated to, is incubated 40 minutes.Stir, skim, be then cooled to 760 DEG C, add manganese metal 0.4kg, magnesium 5.6kg, stir.After 10 minutes, Ar/N is filled2Degasification, sampling analysis are cooled to 710 DEG C, water cooled mo(u)ld ingot casting, About 100kg ingots, ingot casting constituent analysis are Mg4.9%, Mn 0.4%, Sc 0.71%, Zr 0.3%, surplus Al.
Embodiment 2:In 200kg middle frequency furnaces, 100kg Al is put into graphite crucible, addition is pre-mixed drying Good 6.0kg fused salts are (wherein:Sc2O3 1.2kg、ZrO2 0.5kg、NH4F 2.3kg、NaF 0.3kg、KCl 1.5kg、MgCl2 0.2kg).900 DEG C are heated to, is incubated 1hr.Stir, skim, be then cooled to 740 DEG C, add manganese metal 0.6kg, metal Magnesium 5.5kg, stirs.After 15 minutes, Ar/N is filled2Degasification, sampling analysis are cooled to 720 DEG C, water cooled mo(u)ld ingot casting, about 106kg ingots, ingot casting constituent analysis are Mg5.0%, Mn 0.56%, Sc 0.75%, Zr 0.35%, surplus Al.
Embodiment 3:In 200kg middle frequency furnaces, 100kg Al is put into graphite crucible, addition is pre-mixed drying Good 3.0kg fused salts are (wherein:Sc2O3 0.6kg、ZrO2 0.25kg、NH4F 1.15kg、NaF 0.15kg、KCl 0.75kg、 MgCl20.1kg).900 DEG C are heated to, is incubated 1hr.Stir, skim, be then cooled to 740 DEG C, add manganese metal 0.21kg, magnesium metal 2.5kg, stir.After 15 minutes, Ar/N is filled2Degasification, sampling analysis, 720 DEG C are cooled to, water cooled mo(u)ld Ingot casting, about 102kg ingots, ingot casting constituent analysis are Mg2.2%, Mn 0.2%, Sc 0.37%, Zr 0.17%, surplus Al.
Embodiment 4:In 200kg middle frequency furnaces, 100kg Al is put into graphite crucible, addition is pre-mixed drying Good 1.0kg fused salts are (wherein:Sc2O3 0.2kg、ZrO2 0.08kg、NH4F 0.4kg、NaF 0.05kg、KCl 0.25kg、 MgCl20.02kg).900 DEG C are heated to, is incubated 1hr.Stir, skim, be then cooled to 740 DEG C, add manganese metal 0.4kg, magnesium metal 3.0kg, stir.After 15 minutes, Ar/N is filled2Degasification, sampling analysis, 720 DEG C are cooled to, water-cooled die casting Ingot, about 103kg ingots, ingot casting constituent analysis are Mg2.8%, Mn 0.4%, Sc 0.1%, Zr 0.06%, surplus Al.
Embodiment 5:With the intermediate alloy 100kg of embodiment 2, metallic zinc 8.5kg, metallic copper 1.5kg, fine aluminium is raw material, is matched somebody with somebody It is that alloying component is Zn 7.8%, Mg 2.7%, Cu 1.3%, Mn 0.3%, Zr0.15%, Sc 0.35% to put 7, and remaining is aluminium. Using resistance furnace melting.Temperature control is at 710~750 DEG C.Using carbon trichloride refinery by de-gassing, semicontinuous ingot casting;Ingot casting is through 470 DEG C/2hr homogenization after, air cooling.Peeling, hot rolling after 450 DEG C/4h heating, hot rolling deformation amount 70%, then it is cold rolled to 2mm slabs Material, cold rolling reduction 60%.Melted admittedly in 470 DEG C/2hr, water quenching, 120 DEG C/24h Ageing Treatments, obtain aluminum alloy materials.
The mechanical performance of the aluminum alloy materials of acquisition is tensile strength sigmab=650Mpa, yield strength σ0.2=610Mpa, Elongation percentage δ=11%.
Embodiment 6:With the intermediate alloy 100kg of embodiment 3, magnesium metal 3kg, metallic copper 0.1kg, fine aluminium is raw material, configuration 5 It is that alloying component is Mg 5%, Cu 0.1%, Mn 0.2%, Zr 0.15%, Sc0.35%, remaining is aluminium.Melted using resistance furnace Refining.Temperature control is at 710~750 DEG C.Using carbon trichloride refinery by de-gassing, semicontinuous ingot casting;Ingot casting is uniform through 470 DEG C/10hr After change, air cooling.Peeling, hot rolling after 450 DEG C/2h heating, the deflection of hot rolling 80%, then 2mm heavy-gauge sheetings are cold rolled to, cold rolling 50% becomes Shape amount.Made annealing treatment in 350 DEG C/1hr, obtain aluminum alloy materials.
The mechanical performance of the aluminum alloy materials of acquisition is:Tensile strength sigmab=450MPa, yield strength σ0.2=278MPa, Elongation percentage δ=18%.Compare Mg5%, the 5 of remaining Al be alloy, the mechanical performance under equal conditions is:Tensile strength sigmab= 280MPa, yield strength σ0.2=125MPa, elongation percentage δ=25%.The alloy property prepared with the present invention is significantly lifted.

Claims (7)

  1. A kind of 1. polynary intermediate alloy of aluminium alloy, it is characterised in that the polynary intermediate alloy quality group turn into Mg 2~ 6%, Mn 0.2~0.8%, Sc 0.08~0.8%, Zr 0.08~0.4%, surplus Al.
  2. 2. the preparation method of the polynary intermediate alloy described in a kind of claim 1, it is characterised in that comprise the following steps:
    (1) it is 100 by mass ratio:1~7 pure Al and fused salt is put into smelting furnace, is heated to melting, and at 850~980 DEG C Under, it is incubated 0.5-1 hours;
    (2) 720~760 DEG C are cooled to, adds metal Mn and Mg, is incubated 10-20 minutes, stirring homogenizes alloy;
    (3) aluminium liquid surface fused salt is removed, and argon gas is passed through in aluminium liquid, degasification, after standing, is skimmed;
    (4) alloy molten solution is obtained into polynary intermediate alloy with water cooled mo(u)ld ingot casting.
  3. 3. preparation method according to claim 2, it is characterised in that in step (4), control the temperature 700~730 of ingot casting ℃。
  4. 4. preparation method according to claim 2, it is characterised in that the smelting furnace is non-vacuum melting stove.
  5. 5. preparation method according to claim 2, it is characterised in that the quality group of each composition turns into the fused salt:
  6. 6. preparation method according to claim 2, it is characterised in that in step (3), the time of standing is 5~10 minutes.
  7. 7. preparation method according to claim 2, it is characterised in that in step (2), first add metal Mn, add gold Belong to Mg.
CN201710440741.5A 2017-06-13 2017-06-13 Multi-element intermediate alloy for aluminum alloy and preparation method thereof Active CN107794419B (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108796320A (en) * 2018-09-19 2018-11-13 湖南东方钪业股份有限公司 A kind of Al alloy powder and preparation method thereof for 3D printing
CN109047783A (en) * 2018-08-15 2018-12-21 长沙新材料产业研究院有限公司 A kind of Al alloy powder and preparation method thereof

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104651683A (en) * 2015-03-18 2015-05-27 中南大学 Aluminum alloy subjected to composite microalloying of Sc and Zr and preparation method thereof
CN104694801A (en) * 2015-03-20 2015-06-10 东北轻合金有限责任公司 Al-Mg-Sc-Zr aluminum alloy plate and manufacturing method thereof
CN104818412A (en) * 2015-05-27 2015-08-05 东北轻合金有限责任公司 Low-Sc Al-Mg-Sc-Zr alloy sheet and preparation method thereof
CN105525162A (en) * 2014-09-29 2016-04-27 刘小会 Preparation process for improving Al-5.2 Mg-0.3 Mn alloy by adding Zr and rare earth Sc element
CN105821260A (en) * 2016-05-20 2016-08-03 湖南东方钪业股份有限公司 Aluminum, scandium and zirconium intermediate alloy for aluminum alloy and production method thereof
CN105950923A (en) * 2016-07-15 2016-09-21 东北轻合金有限责任公司 Manufacturing method for flat Sc-containing high-Mg aluminum alloy cast ingot
US20180298473A1 (en) * 2017-04-15 2018-10-18 The Boeing Company Aluminum alloy with additions of magnesium, calcium and at least one of chromium, manganese and zirconium, and method of manufacturing the same
JP2019026897A (en) * 2017-07-31 2019-02-21 株式会社神戸製鋼所 Aluminum alloy sheet for structural member, and manufacturing method of aluminum alloy structural member

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105525162A (en) * 2014-09-29 2016-04-27 刘小会 Preparation process for improving Al-5.2 Mg-0.3 Mn alloy by adding Zr and rare earth Sc element
CN104651683A (en) * 2015-03-18 2015-05-27 中南大学 Aluminum alloy subjected to composite microalloying of Sc and Zr and preparation method thereof
CN104694801A (en) * 2015-03-20 2015-06-10 东北轻合金有限责任公司 Al-Mg-Sc-Zr aluminum alloy plate and manufacturing method thereof
CN104818412A (en) * 2015-05-27 2015-08-05 东北轻合金有限责任公司 Low-Sc Al-Mg-Sc-Zr alloy sheet and preparation method thereof
CN105821260A (en) * 2016-05-20 2016-08-03 湖南东方钪业股份有限公司 Aluminum, scandium and zirconium intermediate alloy for aluminum alloy and production method thereof
CN105950923A (en) * 2016-07-15 2016-09-21 东北轻合金有限责任公司 Manufacturing method for flat Sc-containing high-Mg aluminum alloy cast ingot
US20180298473A1 (en) * 2017-04-15 2018-10-18 The Boeing Company Aluminum alloy with additions of magnesium, calcium and at least one of chromium, manganese and zirconium, and method of manufacturing the same
JP2019026897A (en) * 2017-07-31 2019-02-21 株式会社神戸製鋼所 Aluminum alloy sheet for structural member, and manufacturing method of aluminum alloy structural member

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109047783A (en) * 2018-08-15 2018-12-21 长沙新材料产业研究院有限公司 A kind of Al alloy powder and preparation method thereof
CN109047783B (en) * 2018-08-15 2021-10-01 长沙新材料产业研究院有限公司 Aluminum alloy powder and preparation method thereof
CN108796320A (en) * 2018-09-19 2018-11-13 湖南东方钪业股份有限公司 A kind of Al alloy powder and preparation method thereof for 3D printing

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