CN1740353A - Prepn process of in-situ grain reinforced anticorrosive cast alumium-base composite material - Google Patents
Prepn process of in-situ grain reinforced anticorrosive cast alumium-base composite material Download PDFInfo
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- CN1740353A CN1740353A CN 200510029882 CN200510029882A CN1740353A CN 1740353 A CN1740353 A CN 1740353A CN 200510029882 CN200510029882 CN 200510029882 CN 200510029882 A CN200510029882 A CN 200510029882A CN 1740353 A CN1740353 A CN 1740353A
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Abstract
The in-situ grain reinforced anticorrosive cast aluminum-base composite material consists of Mg 7.5-9.5 wt%, Zn 1.0-1.5 wt%, Be 0.03-0.1 wt%, Ti 0.1-0.2 wt% and TiB2 1-20 wt% except Al. The preparation process includes the following steps: 1. smelting industrial pure aluminum in crucible inside a resistive furnace, heating and covering with covering agent; 2. mixing KFB4 and KTiF6, stoving and adding into the melt via stirring; 3. taking out the side product after reaction, adding Al-Be intermediate alloy and Al-Ti intermediate alloy, and covering; 4. leading protecting gas to over the crucible liquid; 5. lowering the temperature of the molten alloy, adding industrial pure Mg and Al-Zn intermediate alloy, stirring, scumming, pumping vacuum and letting stand; and 6. low pressure casting formation. The composite material of the present invention has excellent anticorrosive strength, high plasticity and high modulus, and the present invention is suitable for industrial production.
Description
Technical field
The present invention relates to the preparation method's in a kind of material technology field, particularly a kind of in-situ grain reinforced anticorrosive cast alumium-base composite material preparation method.
Background technology
Cast aluminium alloy is corrosion-resistant, density is low, certain specific tenacity and specific rigidity are arranged, and some important structure such as radar base, case class, porthole, handle, engine and electrical component etc. on the boats and ships adopt casting alloy to alleviate the deadweight of boats and ships to improve the speed of a ship or plane and stability.The cast aluminium alloy of widespread use mainly contains two classes on the boats and ships at present: a class is to have good casting technique performance, and it is cast aluminium alloy (as ZL101) that corrosion proof preferably Al-Si is arranged again; Another kind of is to have excellent seawater corrosion resistance but the relatively poor relatively Al-Mg of casting technique performance is cast aluminium alloy (ZL301, ZL305).These materials generally speaking have certain corrosion resisting property.Industrial ZL301 alloy contains 9.5～11.0%Mg, and the good mechanical performance is arranged after the quenching, but this alloy causes easily that owing to the unstable of natural aging foundry goods produces stress corrosion crack, or postpones cracking.Add the granules preparation aluminum matrix composite, exist enhanced granule and the matrix wetting property is poor, surface reaction is difficult to control, and defectives such as enhanced granule skewness make the solidity to corrosion variation of matrix material, has influenced the performance of aluminum matrix composite.
Find through literature search prior art, Zhang Lin and grade are in " aluminium processing " 2002,25 (2): " the novel ship cast aluminium alloy corrosive nature research " delivered on the 38-40, the material of this article introduction is a kind of novel Al-Mg-Si alloy (1.32%Mg, 1.8%Si, 0.35%Mn, 0.16%Cr), its preparation method is: carry out melting with plumbago crucible in the resistance crucible furnace, alloy liquid pours in the metal die of preheating.Though this preparation methods is simple, and this material has certain corrosion resisting property and castability preferably, and the specific tenacity and the specific modulus of this material are relatively low, have limited its use.
Summary of the invention
The objective of the invention is at deficiency of the prior art, a kind of preparation method of in-situ grain reinforced anticorrosive cast alumium-base composite material is provided, make its matrix material that makes have good corrosion strength, plasticity, and possesses high modulus, method is simple, and cost is low, be suitable for large-scale production and application.
The present invention is achieved by the following technical solutions, and described in-situ grain reinforced anticorrosive cast alumium-base composite material weight percentages of components is: 7.5～9.5%Mg, 1.0～1.5%Zn, 0.03～0.1%Be, 0.1～0.2%Ti, 1～20%TiB
2, surplus is Al.The preparation of this material may further comprise the steps: (1) adds commercial-purity aluminium and carries out melting in the resistance furnace in the crucible, after the fusing, be warming up to 680～800 ℃, covers with insulating covering agent, and insulating covering agent does not have the Na insulating covering agent for the Al-Mg alloy.
(2) with KFB
4, KTiF
6To be about 1: 1.5 quality than uniform mixing, the oven dry back adds in the melt, carries out mechanical stirring, and stirring velocity is 200～500rpm, and churning time is 10～30min.
(3) after reaction finishes, take out by product, add Al-Be master alloy, Al-Ti master alloy, and cover.
(4) the overhead logical shielding gas of liquid level in crucible.
(5) after cooling is cooled to 680～760 ℃, add technical pure Mg, Al-Zn master alloy, stir 10～30min, take off removing dross, vacuumize and leave standstill, time of repose is 5～15min, 680～760 ℃ of dwell temperature.
(6) adopt low-pressure casting to be shaped.Technological process is: assembling median septum, riser pipe, mould, die temperature: 25～400 ℃, adopt the low-voltage equipment low pressure of controllable process parameter to be shaped, vacuum-formed concrete processing parameter is as follows: the type temperature of filling that this composite material low pressure is shaped is 680～760 ℃, and filling velocity 20～150mm/s fills type top pressure 10～150KPa, after die cavity is full of, solidify pressurize, dwell pressure is 100～500KPa, dwell time 10s～10min.
The present invention adopts casting Al-Mg alloy to make matrix, adds Zn, Cu, and Al, elements such as Mn reduce the velocity of diffusion of atom, have controlled the shape and size of precipitated phase, can improve the natural aging stability of alloy, and the TiB of in-situ authigenic
2Particle stability in matrix is fine, long-time timeliness, and particle and basal body interface can not react yet, thereby make that the aging stability of such matrix material is fine.Again because the thermal expansivity of matrix is more many greatly than the thermal expansivity of wild phase, thereby in preparation and heat treatment process, all can in body material, form high density dislocation, the dislocation of intracrystalline and crystal boundary all can produce slippage and hinder, produce and strengthen usefulness, this just makes such material have higher specific tenacity; Certainly, high-modulus TiB
2Particulate adds, and can significantly improve the modulus of material.
Comprehensive these factors make such matrix material have specific tenacity and specific rigidity preferably, have extraordinary corrosion resisting property simultaneously.This technology can be used to cast corrosion-resistant, and density is low, and the in-situ Al-base composition of certain specific tenacity and specific rigidity is arranged.The TiB that the present invention makes
2The enhanced granule anticorrosive cast alumium-base composite material, its new as-quenched condition tensile strength is 335～362MPa, timeliness after 18 months tensile strength be: 349～373MPa, modulus ranges: 77.2～92.5GPa, preparation technology is simple, and cost is low, be suitable for large-scale production and application, can be widely used on the boats and ships in some important structure parts, as radar base, case class, porthole, handle, engine and electrical component etc., be used for alleviating the deadweight of boats and ships to improve the speed of a ship or plane and stability.
Embodiment
Below by embodiment the present invention is described.
Embodiment 1:
The prepared composition mass percent is formed 9.5%Mg, 1.0%Zn, 0.1%Be, 0.2%Ti, 1%TiB
2, all the other are the anticorrosive cast alumium-base composite material of Al.
Preparation process is as follows:
The technical pure aluminium ingot being put into crucible, be warming up to 680 ℃, add insulating covering agent and cover melt, after the fusing, take insulating covering agent off, will be 1: 1.5 KFB through the mass ratio of oven dry
4, KTiF
6Mix and join in the melt, stir, stirring velocity 200rpm, churning time 30min takes out by product, adds Al-Be master alloy, Al-Ti master alloy, covers, and feeds shielding gas CO
2, cool to 680 ℃, add technical pure Mg; the Al-Zn master alloy; cover; stir 10min, vacuumize and leave standstill, 680 ℃ of dwell temperature; time of repose 15min; vacuum breaker continues logical shielding gas, skims; the assembling median septum; riser pipe; mould; 25 ℃ of metal die temperature adopt the low-voltage equipment low pressure of controllable process parameter to be shaped, and vacuum-formed concrete processing parameter is as follows: the type temperature of filling that this composite material low pressure is shaped is 680 ℃; filling velocity 20mm/s; fill type top pressure 10KPa, after die cavity is full of, solidify pressurize; dwell pressure is 100KPa, dwell time 10s.This material granule interface is clean, even particle distribution, and material T4 attitude room-temperature mechanical property:
σ
b＝335MPa，σ
0.2＝266MPa，δ＝4.8％，E＝77.2GPa，
After the natural aging 18 months:
σ
b＝349MPa，σ
0.2＝274MPa，δ＝4.7％，E＝78.1GPa。
Embodiment 2:
The prepared composition mass percent is formed 7.5%Mg, 1.5%Zn, 0.03%Be, 0.1%Ti, 20%TiB
2, all the other are the anticorrosive cast alumium-base composite material of Al.
Preparation process is as follows:
The technical pure aluminium ingot being put into crucible, be warming up to 800 ℃, add insulating covering agent and cover melt, after the fusing, take insulating covering agent off, will be 1: 1.5 KFB through the mass ratio of oven dry
4, KTiF
6Mix and join in the melt, stir, stirring velocity 500rpm, churning time 20min takes out by product, adds Al-Be master alloy, Al-Ti master alloy, covers, and feeds shielding gas N
2, cool to 730 ℃, add technical pure Mg; the Al-Zn master alloy; cover; stir 20min, vacuumize and leave standstill, 730 ℃ of dwell temperature; time of repose 5min; vacuum breaker continues logical shielding gas, skims; the assembling median septum; riser pipe; mould; 400 ℃ of metal die temperature adopt the low-voltage equipment low pressure of controllable process parameter to be shaped, and vacuum-formed concrete processing parameter is as follows: the type temperature of filling that this composite material low pressure is shaped is 760 ℃; filling velocity 150mm/s; fill type top pressure 100KPa, after die cavity is full of, solidify pressurize; dwell pressure is 500KPa, dwell time 10min.
This material granule interface is clean, even particle distribution, and material T4 attitude room-temperature mechanical property:
σ
b＝362MPa，σ
0.2＝289MPa，δ＝1.9％，E＝92.5GPa，
After the natural aging 18 months:
σ
b＝373MPa，σ
0.2＝297MPa，δ＝1.9％，E＝92.3GPa。
Embodiment 3:
The prepared composition mass percent is formed 8.9%Mg, 1.2%Zn, 0.02%Be, 0.1%Ti, 10%TiB
2, all the other are the anticorrosive cast alumium-base composite material of Al.
Preparation process is as follows:
The technical pure aluminium ingot being put into crucible, be warming up to 780 ℃, add insulating covering agent and cover melt, after the fusing, take insulating covering agent off, will be 1: 1.5 KFB through the mass ratio of oven dry
4, KTiF
6Mix and join in the melt, stir, stirring velocity 300rpm, churning time 20min takes out by product, adds Al-Be master alloy, Al-Ti master alloy, covers, and feeds shielding gas Ar
2, cool to 720 ℃, add technical pure Mg; the Al-Zn master alloy; cover; stir 15min, vacuumize and leave standstill, 720 ℃ of dwell temperature; time of repose 10min; vacuum breaker continues logical shielding gas, skims; the assembling median septum; riser pipe; mould; 200 ℃ of metal die temperature adopt the low-voltage equipment low pressure of controllable process parameter to be shaped, and vacuum-formed concrete processing parameter is as follows: the type temperature of filling that this composite material low pressure is shaped is 730 ℃; filling velocity 80mm/s; fill type top pressure 50KPa, after die cavity is full of, solidify pressurize; dwell pressure is 300KPa, dwell time 5min.
This material granule interface is clean, even particle distribution, and material T4 attitude room-temperature mechanical property:
σ
b＝353MPa，σ
0.2＝277MPa，δ＝2.9％，E＝83.8GPa，
After the natural aging 18 months:
σ
b＝366MPa，σ
0.2＝283MPa，δ＝2.8％，E＝84.1GPa。
Claims (8)
1, a kind of in-situ particle strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that the in-situ grain reinforced anticorrosive cast alumium-base composite material weight percentages of components is: 7.5～9.5%Mg, 1.0～1.5%Zn, 0.03～0.1%Be, 0.1～0.2%Ti, 1～20%TiB
2, surplus is Al, its preparation may further comprise the steps:
(1) commercial-purity aluminium is added carry out melting in the resistance furnace in the crucible, heat up, cover with insulating covering agent, insulating covering agent is that aluminium alloy does not have the sodium insulating covering agent;
(2) with KFB
4, KTiF
6Uniform mixing, the oven dry back adds in the melt, carries out mechanical stirring;
(3) after reaction finishes, take out by product, add Al-Be master alloy, Al-Ti master alloy, cover;
(4) the overhead logical shielding gas of liquid level in crucible;
(5) after the alloy liquid cooling cooling, add technical pure Mg, Al-Zn master alloy, stir, take off removing dross, vacuumize and leave standstill;
(6) adopt low-pressure casting to be shaped.
2, in-situ particle according to claim 1 strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that, in the step (1), is warming up between 680～800 ℃.
3, in-situ particle according to claim 1 strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that, and in the step (2), KFB
4: KTiF
6The mixing quality ratio is 1: 1.5.
4, strengthen the preparation method of corrosion-resistant aluminum matrix composite according to claim 1 or 3 described in-situ particles, it is characterized in that in the step (2), stirring velocity is 200～500rpm, churning time 10～30min.
5, in-situ particle according to claim 1 strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that, and in the step (4), the overhead logical shielding gas of liquid level in crucible, protective gas is CO
2, N
2Or Ar
2
6, in-situ particle according to claim 1 strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that, in the step (5), adds Mg and Al-Zn master alloy after alloy liquid cools to 680～760 ℃.
7, strengthen the preparation method of corrosion-resistant aluminum matrix composite according to claim 1 or 6 described in-situ particles, it is characterized in that, in the step (5), churning time 10～30min, time of repose is 10～30min, 680～760 ℃ of dwell temperature, vacuum tightness-0.1MPa.
8, in-situ particle according to claim 1 strengthens the preparation method of corrosion-resistant aluminum matrix composite, it is characterized in that, in the step (6), low-pressure casting is shaped and is specially: the assembling median septum, riser pipe, mould, die temperature: 25～400 ℃, adopt the low-voltage equipment low pressure of controllable process parameter to be shaped, vacuum-formed concrete processing parameter is as follows: the type temperature of filling that this composite material low pressure is shaped is 680～760 ℃, filling velocity 20～150mm/s, fill type top pressure 10～150KPa, after die cavity is full of, solidify pressurize, dwell pressure is 100～500KPa, dwell time 10s～10min.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101880783A (en) * | 2010-06-03 | 2010-11-10 | 南昌大学 | Preparation method of TiAl3 enhanced aluminum-based composite material |
| CN102482738A (en) * | 2009-09-28 | 2012-05-30 | 萨拉蒙株式会社 | Method For Producing An Aluminum-magnesium-based High-strength Alloy |
| CN102912166A (en) * | 2012-10-31 | 2013-02-06 | 济南山大有色金属铸造有限公司 | Aluminum alloy sodium-free refining agent and method for producing same |
| CN104593628A (en) * | 2015-01-08 | 2015-05-06 | 上海交通大学 | Preparation method of aluminum based composite material with low hot-crack tendency |
| CN105063440A (en) * | 2015-08-11 | 2015-11-18 | 中国兵器工业第五九研究所 | High-strength/toughness and high-stability cast aluminum magnesium alloy material and preparation method thereof |
Family Cites Families (1)
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| CN1257297C (en) * | 2003-12-19 | 2006-05-24 | 上海交通大学 | Hybrid reinforced high-damp aluminium base composite material and preparing process thereof |
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2005
- 2005-09-22 CN CNB2005100298825A patent/CN1318623C/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102482738A (en) * | 2009-09-28 | 2012-05-30 | 萨拉蒙株式会社 | Method For Producing An Aluminum-magnesium-based High-strength Alloy |
| CN101880783A (en) * | 2010-06-03 | 2010-11-10 | 南昌大学 | Preparation method of TiAl3 enhanced aluminum-based composite material |
| CN101880783B (en) * | 2010-06-03 | 2012-02-08 | 南昌大学 | Preparation method of TiAl3 enhanced aluminum-based composite material |
| CN102912166A (en) * | 2012-10-31 | 2013-02-06 | 济南山大有色金属铸造有限公司 | Aluminum alloy sodium-free refining agent and method for producing same |
| CN102912166B (en) * | 2012-10-31 | 2013-09-18 | 济南山大有色金属铸造有限公司 | Aluminum alloy sodium-free refining agent and method for producing same |
| CN104593628A (en) * | 2015-01-08 | 2015-05-06 | 上海交通大学 | Preparation method of aluminum based composite material with low hot-crack tendency |
| CN105063440A (en) * | 2015-08-11 | 2015-11-18 | 中国兵器工业第五九研究所 | High-strength/toughness and high-stability cast aluminum magnesium alloy material and preparation method thereof |
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