CN101643871A - Super-high-plasticity high-strength cast magnesium alloy and preparation method thereof - Google Patents
Super-high-plasticity high-strength cast magnesium alloy and preparation method thereof Download PDFInfo
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Abstract
The invention relates to a super-high-plasticity high-strength cast magnesium alloy and a preparation method thereof. The cast magnesium alloy comprises the following chemical components by mass percent: 0.5-8.05% of tin, 1.0-6.0% of aluminum and the balance of magnesium. The preparation method comprises the following steps: under the protection of gases, melting preheated the pure magnesium at apreset low temperature, adding the tin and the aluminum in a certain proportion into the melt, evenly stirring after completely melting, heating to a high preset temperature to refine and remove slag,and finally casting to form ingots, The cast magnesium alloy has the advantages of super-high plasticity and high strength; and the preparation method has the advantages of simple technique, high reliability, easy popularization and application, and the like.
Description
Technical field
The present invention relates to metal material field, particularly relate to a kind of super-high-plasticity, cast Mg alloy with high strength and preparation method thereof.
Background technology
Magnesium alloy is as the lightest engineering structure metallic substance, special performance with many excellences, good as specific tenacity height, specific rigidity height, electrical and thermal conductivity, have good damping shock absorption and capability of electromagnetic shielding concurrently, good advantages such as regeneration have a good application prospect in fields such as automobile, communication equipment, aviation.Especially aspect lightweight, has the alternate of being difficult to significant advantage.Yet the crystalline structure of magnesium is a close-packed hexagonal, and slip system is few, and plastic deformation ability is poor, has limited its application to a great extent.Cast magnesium alloys can the moulding complicated shape, enjoys favor aborning, but that the shortcoming of cast magnesium alloys is a plasticity is relatively poor.Patent 200610045693.1 and 200710011886.X have provided the approach that improves the magnesium alloy performance respectively.Yet its technology is relatively complicated.In addition, the kind of magnesium alloy is less at present, is difficult to satisfy the requirement of different operating modes, is badly in need of developing a kind of super-high-plasticity, cast Mg alloy with high strength.
Summary of the invention
It is simple, reliable to the purpose of this invention is to provide a kind of technology, and the super-high-plasticity that is easy to apply, cast Mg alloy with high strength and preparation method thereof.
Technical scheme of the present invention is: under gas shield; preheated pure magnesium is melted under predetermined lesser temps, then a certain proportion of tin and aluminium are joined in the melt, stir until completely melted; be warming up to higher preset temperature refining and scarfing cinder again and handle, last casting ingot-forming.
A kind of super-high-plasticity, cast Mg alloy with high strength, the mass percent of the chemical ingredients of this alloy is: tin 0.5-8.0, aluminium 1.0-6.0, all the other are magnesium.
Described tin content mass percent is 2.0-5.0, and aluminium content mass percent is 2.0-4.0;
According to above-mentioned a kind of super-high-plasticity, the preparation method of cast Mg alloy with high strength, this method may further comprise the steps:
(1) gets the raw materials ready according to the magnesium alloy component proportions;
(2) in the gas shield smelting furnace, the pure magnesium ingot that will prepare in proportion is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) that will prepare in proportion respectively and add in the magnesium melt through the pure tin of 200 ℃ of preheatings and fine aluminium, continue to leave standstill insulation 5-10 minute at 650-680 ℃, stirred then 2-20 minute, make composition even;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder is handled, direct casting ingot-forming.
The present invention compares with present existing technology has following characteristics:
It is simple, reliable, easy to operate to the invention provides a kind of technology, and the composition of the cast magnesium alloys that is easy to apply and preparation method.
1) this cast magnesium alloys has super-high-plasticity, has high strength simultaneously, and under as-cast condition, it is that 20-35%, tensile strength are 220-250MPa, repeatedly the rolling deformation rate is greater than 80-85% that the alloy behind the optimizing components can obtain unit elongation.
2) tin and aluminium are as alloying element, and the composition range of the application's patent does not appear in the newspapers;
3) adopt castmethod production, technology is simple;
4) adopt low smelting heat and element homogenizing, rise to high temperature refining and scarfing cinder, at utmost reduce oxidization burning loss and pollution;
Embodiment
Embodiment one
(1) taking by weighing starting material by mass percentage is: pure tin 0.5%, and fine aluminium 1%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-0.5Sn-1Al alloy.
Embodiment two
(1) taking by weighing starting material by mass percentage is: pure tin 2%, and fine aluminium 2%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-2Sn-2Al alloy.
Embodiment three
(1) taking by weighing starting material by mass percentage is: pure tin 3%, and fine aluminium 3%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-3Sn-3Al alloy.This alloy casting performance is: unit elongation greater than 30-35%, tensile strength greater than for 230-250MPa, deformation rate greater than 85%.
Embodiment four
(1) taking by weighing starting material by mass percentage is: pure tin 5%, and fine aluminium 2%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-5Sn-2Al alloy.
Embodiment five
(1) taking by weighing starting material by mass percentage is: pure tin 5%, and fine aluminium 4%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-5Sn-4Al alloy.
Embodiment six
(1) taking by weighing starting material by mass percentage is: pure tin 2%, and fine aluminium 4%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-2Sn-4Al alloy.
Embodiment seven
(1) taking by weighing starting material by mass percentage is: pure tin 8%, and fine aluminium 1%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-8Sn-1Al alloy.
Embodiment eight
(1) taking by weighing starting material by mass percentage is: pure tin 8%, and fine aluminium 6%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-8Sn-6Al alloy.
Embodiment nine
(1) taking by weighing starting material by mass percentage is: pure tin 3%, and fine aluminium 6%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-3Sn-6Al alloy.This alloy casting performance is: unit elongation greater than 20-25%, tensile strength greater than being 240-250MPa.
Embodiment ten
(1) taking by weighing starting material by mass percentage is: pure tin 4%, and fine aluminium 3%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-4Sn-3Al alloy.
Embodiment 11
(1) taking by weighing starting material by mass percentage is: pure tin 3%, and fine aluminium 5%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-3Sn-5Al alloy.This alloy deformation rate is greater than 80%.
Embodiment 12
(1) taking by weighing starting material by mass percentage is: pure tin 2%, and fine aluminium 5%, all the other are magnesium;
(2) in the gas shield smelting furnace, the pure magnesium ingot with above-mentioned content is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) respectively with in above-mentioned content and the pure tins and fine aluminium adding magnesium melt, continue to leave standstill insulation 5-10 minute, stirred then 2-20 minute, make composition even at 650-680 ℃ through 200 ℃ of preheatings;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder was handled, directly casting ingot-forming made the Mg-2Sn-5Al alloy.
Claims (3)
1, a kind of super-high-plasticity, cast Mg alloy with high strength is characterized in that, the mass percent of the chemical ingredients of this alloy is: tin 0.5-8.0, and aluminium 1.0-6.0, all the other are magnesium.
2, super-high-plasticity according to claim 1, cast Mg alloy with high strength is characterized in that, described tin content mass percent is 2.0-5.0, and aluminium content mass percent is 2.0-4.0.
3, the preparation method of a kind of super-high-plasticity according to claim 1, cast Mg alloy with high strength is characterized in that, this method may further comprise the steps:
(1) gets the raw materials ready according to the magnesium alloy component proportions;
(2) in the gas shield smelting furnace, the pure magnesium ingot that will prepare in proportion is preheated to 350-400 ℃ in crucible earlier, is warming up to 650-680 ℃ then and melts;
(3) that will prepare in proportion respectively and add in the magnesium melt through the pure tin of 200 ℃ of preheatings and fine aluminium, continue to leave standstill insulation 5-10 minute at 650-680 ℃, stirred then 2-20 minute, make composition even;
(4) add No. 2 flux, temperature is warming up to 730-820 ℃, leave standstill insulation 5-10 minute, the blowing argon gas refining, after scarfing cinder is handled, direct casting ingot-forming.
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CN102517480A (en) * | 2012-01-08 | 2012-06-27 | 吉林大学 | High-work-hardening magnesium alloy and preparation method thereof |
CN103781928A (en) * | 2011-10-20 | 2014-05-07 | 浦项工科大学校产学协力团 | Non-heat treated magnesium alloy sheet with excellent formability at room temperature in which segregation is minimized |
CN107287483A (en) * | 2017-05-27 | 2017-10-24 | 重庆科技学院 | High plastic magnesium alloy sheet material and its processing method |
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CN101781729A (en) * | 2010-02-23 | 2010-07-21 | 南京信息工程大学 | Magnesium-based wear-resistant damping alloy material and preparation method thereof |
CN103781928A (en) * | 2011-10-20 | 2014-05-07 | 浦项工科大学校产学协力团 | Non-heat treated magnesium alloy sheet with excellent formability at room temperature in which segregation is minimized |
EP2770072A4 (en) * | 2011-10-20 | 2015-06-17 | Postech Acad Ind Found | Non-heat treated magnesium alloy sheet with excellent formability at room temperature in which segregation is minimized |
CN102517480A (en) * | 2012-01-08 | 2012-06-27 | 吉林大学 | High-work-hardening magnesium alloy and preparation method thereof |
CN107287483A (en) * | 2017-05-27 | 2017-10-24 | 重庆科技学院 | High plastic magnesium alloy sheet material and its processing method |
CN109280827A (en) * | 2017-07-19 | 2019-01-29 | 北京普润医疗器械有限公司 | Anastomosis staple and its preparation method and application |
CN107398548A (en) * | 2017-07-28 | 2017-11-28 | 河南明镁镁业科技有限公司 | A kind of grain refiner and its preparation and application method of significantly Refining Mg Alloy tissue |
CN107460351A (en) * | 2017-07-28 | 2017-12-12 | 河南明镁镁业科技有限公司 | A kind of production method of high cleanliness magnesium alloy |
CN107460351B (en) * | 2017-07-28 | 2019-03-22 | 河南明镁镁业科技有限公司 | A kind of production method of high cleanliness magnesium alloy |
CN108004446A (en) * | 2017-12-11 | 2018-05-08 | 于海松 | The synthesis technique of high-ductility magnesium tin alloy |
CN110777288A (en) * | 2019-12-13 | 2020-02-11 | 陕西易莱德新材料科技有限公司 | High-strength corrosion-resistant magnesium alloy and preparation method thereof |
CN113862535A (en) * | 2021-10-08 | 2021-12-31 | 青岛海骊准晶新材料科技有限公司 | Magnesium alloy for low temperature, preparation method and application thereof, and cold chain tray |
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