CN110564992A - sr, Zr, Ti and Ce quaternary composite microalloyed Al-Si-Cu series cast aluminum alloy and preparation method thereof - Google Patents
sr, Zr, Ti and Ce quaternary composite microalloyed Al-Si-Cu series cast aluminum alloy and preparation method thereof Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 76
- 229910052726 zirconium Inorganic materials 0.000 title claims abstract description 32
- 229910052684 Cerium Inorganic materials 0.000 title claims abstract description 28
- 229910018594 Si-Cu Inorganic materials 0.000 title claims abstract description 28
- 229910008465 Si—Cu Inorganic materials 0.000 title claims abstract description 28
- 239000011219 quaternary composite Substances 0.000 title claims abstract description 28
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 28
- 238000002360 preparation method Methods 0.000 title claims abstract description 13
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 49
- 239000000956 alloy Substances 0.000 claims abstract description 49
- 239000010936 titanium Substances 0.000 claims abstract description 38
- 229910052712 strontium Inorganic materials 0.000 claims abstract description 34
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 16
- 239000010703 silicon Substances 0.000 claims abstract description 16
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 14
- 239000010949 copper Substances 0.000 claims abstract description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000005266 casting Methods 0.000 claims abstract description 9
- 238000000137 annealing Methods 0.000 claims abstract description 7
- 230000032683 aging Effects 0.000 claims abstract description 6
- 229910052802 copper Inorganic materials 0.000 claims abstract description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 4
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims abstract description 4
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims abstract description 4
- 238000007670 refining Methods 0.000 claims description 21
- 239000012535 impurity Substances 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 229910018125 Al-Si Inorganic materials 0.000 claims description 6
- 229910018520 Al—Si Inorganic materials 0.000 claims description 6
- 239000003795 chemical substances by application Substances 0.000 claims description 6
- VHHHONWQHHHLTI-UHFFFAOYSA-N hexachloroethane Chemical compound ClC(Cl)(Cl)C(Cl)(Cl)Cl VHHHONWQHHHLTI-UHFFFAOYSA-N 0.000 claims description 6
- 239000002893 slag Substances 0.000 claims description 6
- 229910018182 Al—Cu Inorganic materials 0.000 claims description 5
- 229910018580 Al—Zr Inorganic materials 0.000 claims description 5
- 150000001875 compounds Chemical class 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 238000010791 quenching Methods 0.000 claims description 3
- 230000000171 quenching effect Effects 0.000 claims description 3
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 3
- 230000004927 fusion Effects 0.000 claims 1
- 238000010438 heat treatment Methods 0.000 claims 1
- 239000006104 solid solution Substances 0.000 claims 1
- 239000000243 solution Substances 0.000 claims 1
- 239000000203 mixture Substances 0.000 abstract description 9
- 238000005516 engineering process Methods 0.000 abstract description 6
- 238000005275 alloying Methods 0.000 abstract description 4
- 238000000265 homogenisation Methods 0.000 abstract description 4
- 238000005728 strengthening Methods 0.000 abstract description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 16
- 238000001878 scanning electron micrograph Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 230000004048 modification Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 5
- 230000005496 eutectics Effects 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 230000006911 nucleation Effects 0.000 description 4
- 238000010899 nucleation Methods 0.000 description 4
- 239000002131 composite material Substances 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000011573 trace mineral Substances 0.000 description 2
- 235000013619 trace mineral Nutrition 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009750 centrifugal casting Methods 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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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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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
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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
- C22C21/04—Modified aluminium-silicon alloys
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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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Abstract
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al‑Si‑Cu系铸造铝合金,主要由铝、硅、铜、锶、锆、钛和铈组成,其制备方法,依次包括:(1)熔铸,(2)均质化退火,(3)固溶处理,(4)时效。本发明的铸造铝合金的抗拉强度为360MPa~391.58MPa,断裂伸长率为5.75~%7.5%。本发明使用四元复合微合金化技术,相比Sr、Zr二元微合金化组织更致密,合金的成分更加均匀,减小了初生硅相的尺寸和数量,更有效的提高了铸造铝合金的强度和塑性;本发明制备的铸造铝合金具有较高的抗拉强度和断裂伸长率,满足了汽车工业对合金部件轻量化、高强化和高韧性的要求。
A high-strength and high-plasticity Al-Si-Cu cast aluminum alloy of Sr, Zr, Ti and Ce quaternary composite microalloying, mainly composed of aluminum, silicon, copper, strontium, zirconium, titanium and cerium, and a preparation method thereof , in turn including: (1) casting, (2) homogenization annealing, (3) solution treatment, (4) aging. The tensile strength of the cast aluminum alloy of the present invention is 360 MPa to 391.58 MPa, and the elongation at break is 5.75 to 7.5%. Compared with the Sr and Zr binary micro-alloying technology, the invention uses the quaternary composite micro-alloying technology, the structure is denser, the composition of the alloy is more uniform, the size and quantity of the primary silicon phase are reduced, and the cast aluminum alloy is more effectively improved. The cast aluminum alloy prepared by the invention has high tensile strength and elongation at break, and meets the requirements of the automobile industry for lightweight, high strengthening and high toughness of alloy parts.
Description
技术领域technical field
本发明涉及一种铸造铝合金,尤其是一种Al-Si-Cu系铸造铝合金,具体而言是一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金及其制备方法。The invention relates to a cast aluminum alloy, in particular to an Al-Si-Cu series cast aluminum alloy, in particular to a high-strength and high-plastic Al-Si alloyed with Sr, Zr, Ti and Ce quaternary composite microalloying -Cu-based cast aluminum alloy and its preparation method.
背景技术Background technique
铸造铝合金具有较高的抗拉强度和延伸率、优良的铸造性能以及耐蚀性,广泛应用于工业制造的各个领域,如:汽车、航空航天等领域。随着汽车数量的快速增长、汽车性能的不断提升以及能源资源问题的日益凸显,汽车工业对产品轻量化和高强化的要求越来越严格,提高铸造铝合金的力学性能就成为当今社会迫切需要解决的问题。Cast aluminum alloys have high tensile strength and elongation, excellent casting properties and corrosion resistance, and are widely used in various fields of industrial manufacturing, such as automobiles, aerospace and other fields. With the rapid growth of the number of automobiles, the continuous improvement of automobile performance and the increasingly prominent problems of energy resources, the automobile industry has become more and more strict with the requirements of lightweight and high-strengthening products, and improving the mechanical properties of cast aluminum alloys has become an urgent need in today's society. solved problem.
专利申请号201710193447.9公开了一种高强铸造铝合金的制备方法,获得的合金具有较高的强度和硬度,耐磨性和耐腐蚀性好,但该合金使用离心铸造,生产成本较高;专利申请号201611031488.X公开了2A12铝合金铸造工艺,所得工件抗拉强度较低;专利申请号201010607633.0公开了高强度铸造铝合金,所得合金室温抗拉强度较高,但断裂伸长率较低。迄今为止市场上尚未出现强度和塑性完全满足使用要求的铸造铝合金。向合金中加入适量的微量元素可以提高铝合金的性能,基于微合金化“多元少量”的设计思路,本发明提出了四元复合微合金化技术。Patent Application No. 201710193447.9 discloses a preparation method of high-strength cast aluminum alloy. The obtained alloy has high strength and hardness, and good wear resistance and corrosion resistance, but the alloy uses centrifugal casting, and the production cost is relatively high; patent application No. 201611031488.X discloses the 2A12 aluminum alloy casting process, and the obtained workpiece has a low tensile strength; Patent Application No. 201010607633.0 discloses a high-strength cast aluminum alloy, and the obtained alloy has a high room temperature tensile strength, but a low elongation at break. So far, there has not been a cast aluminum alloy whose strength and plasticity fully meet the requirements of use on the market. Adding an appropriate amount of trace elements to the alloy can improve the performance of the aluminum alloy. Based on the design idea of "multi-element and small amount" of micro-alloying, the present invention proposes a quaternary composite micro-alloying technology.
Sr作为变质剂,在合金液中主要以Al4Sr存在,该化合物不稳定,易分解,不能起到非均匀形核作用,对细化一次硅无效,但游离Sr吸附在生长着的Si表面,阻止共晶硅按片状方式生长。Ce的加入可形成CeO2,而CeO2可作为共晶硅非均匀形核核心。所以,Sr、Ce同时加入达到了复合变质效果,即使共晶硅形核率增高,又改变了共晶硅生长形态使之碎化为细密点状。因此Sr、Ce同时加入更好的细化了组织,使组织更致密,且减小了初生硅相的尺寸和数量,更有效的提升了铝合金的性能。As a modifier, Sr mainly exists as Al 4 Sr in the alloy liquid. This compound is unstable and easy to decompose, and cannot play a role in non-uniform nucleation. It is ineffective for refining primary silicon, but free Sr is adsorbed on the surface of growing Si. , preventing eutectic silicon from growing in a sheet-like manner. The addition of Ce can form CeO 2 , and CeO 2 can act as a heterogeneous nucleation core of eutectic silicon. Therefore, the simultaneous addition of Sr and Ce achieves the effect of compound modification. Even if the nucleation rate of eutectic silicon is increased, the growth form of eutectic silicon is changed to be fragmented into fine dots. Therefore, the addition of Sr and Ce at the same time can better refine the structure, make the structure more dense, and reduce the size and quantity of the primary silicon phase, and more effectively improve the performance of the aluminum alloy.
Zr元素加入到铝合金中,在合金凝固过程中Zr元素与Al形成A13Zr等高熔点物相,对合金的后续凝固起到非均质形核作用,细化铸态基体组织,提高液态合金的流动性和元素分布均匀性。Ti也是铝合金常用的微量元素,加入后Ti可在铝合金中形成Al3Ti相,形成结晶时的非自发核心,显著细化了铸造组织。而Zr和Ti同时加入时形成的Al3ZrxT1-x相,可以更好的细化组织,具有比单一的A13Zr相、Al3Ti相更好的细化效果,因此同时加入Zr和Ti比只加Zr或只加Ti更好的强化效果。Zr element is added to the aluminum alloy, during the solidification process of the alloy, Zr element and Al form high melting point phases such as A1 3 Zr, which play a heterogeneous nucleation effect on the subsequent solidification of the alloy, refine the as-cast matrix structure, and improve the liquid state. Alloy fluidity and element distribution uniformity. Ti is also a commonly used trace element in aluminum alloys. After adding Ti, it can form Al 3 Ti phase in the aluminum alloy, forming a non-spontaneous core during crystallization, which significantly refines the casting structure. The Al 3 Zr x T 1-x phase formed when Zr and Ti are added at the same time can better refine the structure and has a better refining effect than the single A1 3 Zr phase and Al 3 Ti phase. Zr and Ti have better strengthening effect than only Zr or only Ti.
迄今为止,市场上尚未出现使用Sr、Zr、Ti和Ce四元复合微合金化进行强化的铸造铝合金。为了解决现有技术存在的铸造铝合金抗拉强度较低和塑性不高的问题,急需发明一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金及其制备方法。To date, there are no cast aluminum alloys fortified using quaternary composite microalloying of Sr, Zr, Ti and Ce on the market. In order to solve the problems of low tensile strength and low plasticity of cast aluminum alloys in the prior art, it is urgent to invent a high-strength and high-plasticity Al-Si-Cu system with Sr, Zr, Ti and Ce quaternary composite microalloying Cast aluminum alloy and preparation method thereof.
发明内容SUMMARY OF THE INVENTION
本发明的目的是针对现有的铸造铝合金存在的不足,使用Sr、Zr、Ti和Ce四元复合微合金化技术(利用Sr、Ce复合变质效果,利用Zr、Ti复合形成的Al3ZrxT1-x相),提出一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金及其制备方法,解决了铸造铝合金抗拉强度低和塑性差的问题。The purpose of the present invention is to aim at the deficiencies existing in the existing cast aluminum alloys, using Sr, Zr, Ti and Ce quaternary composite microalloying technology (using Sr, Ce composite modification effect, using Zr, Ti composite formed Al 3 Zr x T 1-x phase), proposed a high-strength and high-plastic Al-Si-Cu cast aluminum alloy with Sr, Zr, Ti and Ce quaternary composite microalloying and its preparation method, which solved the problem of tensile strength of cast aluminum alloy. The problem of low strength and poor plasticity.
本发明的技术方案之一是:One of the technical solutions of the present invention is:
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金,其特征在于其主要由铝(Al)、硅(Si)、铜(Cu)、锶(Sr)、锆(Zr)、钛(Ti)和铈(Ce)组成,其中,硅(Si)的质量百分比为7.5~11.16%,铜(Cu)的质量百分比为4.34~5.31%,锶(Sr)的质量百分比为0.55~0.7%,锆(Zr)的质量百分比为0.42~0.59%,钛(Ti)的质量百分比为0.14~0.18%,铈(Ce)的质量百分比为0.15~0.23%,其余为铝和不可避免的杂质元素;各组份之和为100%。A high-strength and high-plastic Al-Si-Cu cast aluminum alloy with Sr, Zr, Ti and Ce quaternary composite microalloying, characterized in that it is mainly composed of aluminum (Al), silicon (Si), copper (Cu) , strontium (Sr), zirconium (Zr), titanium (Ti) and cerium (Ce), wherein the mass percentage of silicon (Si) is 7.5~11.16%, and the mass percentage of copper (Cu) is 4.34~5.31%, The mass percent of strontium (Sr) is 0.55~0.7%, the mass percent of zirconium (Zr) is 0.42~0.59%, the mass percent of titanium (Ti) is 0.14~0.18%, and the mass percent of cerium (Ce) is 0.15~0.23 %, the rest are aluminum and inevitable impurity elements; the sum of each component is 100%.
本发明的技术方案之二是:The second technical scheme of the present invention is:
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金的制备方法,其特征是其依次包括:(1)熔铸,(2)均质化退火,(3)固溶处理,(4)时效;A method for preparing a high-strength and high-plastic Al-Si-Cu cast aluminum alloy by quaternary composite microalloying of Sr, Zr, Ti and Ce, characterized in that the method comprises the following steps: (1) melting and casting, (2) homogeneous Chemical annealing, (3) solution treatment, (4) aging;
所述的熔铸是指:待Al、Al-Si中间合金、Al-Cu中间合金熔化后,升温到850±10℃,再依次加入Al-Sr中间合金、Al-Zr中间合金、Al-Ti-B中间合金、Al-Ce中间合金,待所有中间合金和金属熔化后,保温2-2.5小时,将温度降到750-780℃,加入六氯乙烷精炼剂精炼,精炼后静置10 min,静置后去渣,再次加入六氯乙烷精炼剂精炼,精炼后静置10 min,静置后去渣,浇铸成锭;The melting and casting refers to: after the Al, Al-Si master alloy and Al-Cu master alloy are melted, the temperature is raised to 850±10°C, and then Al-Sr master alloy, Al-Zr master alloy, Al-Ti- B master alloy and Al-Ce master alloy, after all master alloys and metals are melted, keep the temperature for 2-2.5 hours, reduce the temperature to 750-780 ℃, add hexachloroethane refining agent for refining, let stand for 10 min after refining, After standing, remove slag, add hexachloroethane refining agent again for refining, let stand for 10 min after refining, remove slag after standing, and cast into ingots;
所述的均质化退火是指:250±10℃×6h+350±10℃×6h+450±10℃×6h+The homogenization annealing refers to: 250±10℃×6h+350±10℃×6h+450±10℃×6h+
480±10℃×20h;480±10℃×20h;
所述的固溶处理是指480±10℃×1h+490±10℃×1h,然后室温下水淬;The solution treatment refers to 480±10℃×1h+490±10℃×1h, and then water quenching at room temperature;
所述的时效是指:191±10℃×12h;The aging period refers to: 191±10℃×12h;
以过上述四步法即可获得Sr、Zr、Ti和Ce四元复合微合金化的即可获得Sr、Zr、Ti和Ce四元复合微合金化的、抗拉强度360MPa~391.58MPa、断裂伸长率5.75~%7.5%的高强度高塑性Al-Si-Cu系铸造铝合金。The quaternary composite microalloying of Sr, Zr, Ti and Ce can be obtained by the above four-step method, and the quaternary composite microalloying of Sr, Zr, Ti and Ce can be obtained. High strength and high plasticity Al-Si-Cu cast aluminum alloy with elongation of 5.75~%7.5%.
所述的Al-Si中间合金中Si的质量百分比为17%,Al-Cu中间合金中Cu的质量百分比为50.12%,Al-Sr中间合金中Sr的质量百分比为9.89%,Al-Zr中间合金中Zr的质量百分比为4.11%,Al-Ti-B中间合金中Ti的质量百分比为5.11%,Al-Ce中间合金中Ce的质量百分比为10%。The mass percentage of Si in the Al-Si master alloy is 17%, the mass percentage of Cu in the Al-Cu master alloy is 50.12%, the mass percentage of Sr in the Al-Sr master alloy is 9.89%, and the Al-Zr master alloy is 9.89%. The mass percentage of Zr in the Al-Ti-B master alloy is 4.11%, the mass percentage of Ti in the Al-Ti-B master alloy is 5.11%, and the mass percentage of Ce in the Al-Ce master alloy is 10%.
本发明具有以下有益效果:The present invention has the following beneficial effects:
(1)使用四元复合微合金化技术,Sr、Ce同时加入具有复合变质效果,组织更致密,合金成分更均匀,减小了初生硅相的数量和尺寸,更有效的提升了铝合金的性能;Zr和Ti同时加入形成的Al3ZrxT1-x相,可以更好的细化组织,具有比单一的A13Zr相、Al3Ti相更好的细化效果,更有效的提高了铸造铝合金的强度和塑性。(1) Using the quaternary composite microalloying technology, the simultaneous addition of Sr and Ce has a composite modification effect, the structure is denser, the alloy composition is more uniform, the number and size of the primary silicon phase are reduced, and the aluminum alloy is more effectively improved. performance; the Al 3 Zr x T 1-x phase formed by the addition of Zr and Ti at the same time can better refine the structure, and has a better refining effect than the single A1 3 Zr phase and Al 3 Ti phase, and is more effective. The strength and plasticity of the cast aluminum alloy are improved.
(2)本发明制备的铸造铝合金具有较高的抗拉强度和断裂伸长率,满足了汽车工业对合金部件轻量化、高强化和高韧性的要求。(2) The cast aluminum alloy prepared by the present invention has high tensile strength and elongation at break, and meets the requirements of the automobile industry for lightweight, high strengthening and high toughness of alloy parts.
附图说明Description of drawings
图1为本发明实施例1的四元复合微合金化Al-Si-Cu系铸造铝合金拉伸断口SEM图像。FIG. 1 is a SEM image of the tensile fracture of the quaternary composite microalloyed Al-Si-Cu cast aluminum alloy in Example 1 of the present invention.
图2为本发明实施例1的四元复合微合金化Al-Si-Cu系铸造铝合金表面SEM图像。FIG. 2 is an SEM image of the surface of the quaternary composite microalloyed Al-Si-Cu cast aluminum alloy in Example 1 of the present invention.
图3为本发明实施例2的Al-Si-Cu系铸造铝合金拉伸断口SEM图像;Fig. 3 is the SEM image of the tensile fracture of the Al-Si-Cu cast aluminum alloy in Example 2 of the present invention;
图4为本发明实施例1的四元复合微合金化Al-Si-Cu系铸造铝合金表面SEM图像。4 is an SEM image of the surface of the quaternary composite microalloyed Al-Si-Cu cast aluminum alloy in Example 1 of the present invention.
图5为本发明对比例1的四元复合微合金化Al-Si-Cu系铸造铝合金拉伸断口SEM图像。5 is a SEM image of a tensile fracture of the quaternary composite microalloyed Al-Si-Cu based cast aluminum alloy of Comparative Example 1 of the present invention.
图6为本发明实施例1的四元复合微合金化Al-Si-Cu系铸造铝合金表面SEM图像。FIG. 6 is a SEM image of the surface of the quaternary composite microalloyed Al-Si-Cu cast aluminum alloy in Example 1 of the present invention.
图7为本发明对比例2的四元复合微合金化Al-Si-Cu系铸造铝合金拉伸断口SEM图像。7 is a SEM image of the tensile fracture of the quaternary composite microalloyed Al-Si-Cu based cast aluminum alloy of Comparative Example 2 of the present invention.
图8为本发明实施例1的四元复合微合金化Al-Si-Cu系铸造铝合金表面SEM图像。8 is a SEM image of the surface of the quaternary composite microalloyed Al-Si-Cu based cast aluminum alloy of Example 1 of the present invention.
具体实施方式Detailed ways
下面结合具体实施例对本发明作进一步的说明。The present invention will be further described below in conjunction with specific embodiments.
实施例1。Example 1.
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金由以下方法制备而成:A Sr, Zr, Ti and Ce quaternary composite micro-alloyed Al-Si-Cu cast aluminum alloy with high strength and high plasticity is prepared by the following method:
首先,将Al、Al-Si中间合金、Al-Cu中间合金熔化后,升温到850±10℃,依次加入Al-Sr中间合金、Al-Zr中间合金、Al-Ti-B中间合金、Al-Ce中间合金,待所有中间合金和金属熔化后,保温2-2.5小时,将温度降到750-780℃,加入六氯乙烷精炼剂精炼,精炼后静置10min,静置后去渣,再次加入六氯乙烷精炼剂精炼,精炼后静置10min,静置后去渣,浇铸成锭。First, after melting the Al, Al-Si master alloy and Al-Cu master alloy, the temperature was raised to 850±10°C, and Al-Sr master alloy, Al-Zr master alloy, Al-Ti-B master alloy, Al- Ce master alloy, after all the master alloys and metals are melted, keep the temperature for 2-2.5 hours, reduce the temperature to 750-780 ℃, add hexachloroethane refining agent for refining, let stand for 10 minutes after refining, remove slag after standing, and then again Add hexachloroethane refining agent for refining, let stand for 10 minutes after refining, remove slag after standing, and cast into ingots.
其次,对铝合金铸锭进行均质化退火,均质化退火工艺为:Secondly, the aluminum alloy ingot is subjected to homogenization annealing, and the homogenization annealing process is as follows:
250±10℃×6h+350±10℃×6h+450±10℃×6h+480±10℃×20h;250±10℃×6h+350±10℃×6h+450±10℃×6h+480±10℃×20h;
第三,再进行固溶处理,固溶处理工艺为480±10℃×1h+490±10℃×1h,室温下水淬;Third, carry out solution treatment again, the solution treatment process is 480±10℃×1h+490±10℃×1h, and water quenching at room temperature;
最后,进行191±10℃×12h的时效处理,即可获得Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金。Finally, an aging treatment of 191±10℃×12h is carried out to obtain a high-strength and high-plastic Al-Si-Cu cast aluminum alloy with quaternary composite microalloying of Sr, Zr, Ti and Ce.
本实施例的铝合金经EDS实际测量成分为:Si11.16%、Cu4.34%、Sr0.70%、Zr0.42%、Ti0.14%、Ce0.19%, 余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si11.16%, Cu4.34%, Sr0.70%, Zr0.42%, Ti0.14%, Ce0.19%, the balance is aluminum and unavoidable impurity elements.
本实施例的铝合金的抗拉强度为391.58MPa,断裂伸长率为5.75%。结合附图1可以看出本实施例的铝合金撕裂棱非常多,组织很均匀致密,没有明显的疏松(缩松);初生硅相非常少,几乎完全溶解,因而合金具有非常高的强度和塑性。The tensile strength of the aluminum alloy of this example is 391.58 MPa, and the elongation at break is 5.75%. With reference to Figure 1, it can be seen that the aluminum alloy of this embodiment has many tear edges, the structure is very uniform and dense, and there is no obvious porosity (shrinkage); the primary silicon phase is very small, and it is almost completely dissolved, so the alloy has very high strength. and plasticity.
实施例2。Example 2.
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金,其制备方法与实施例1相同。A high-strength and high-plasticity Al-Si-Cu based cast aluminum alloy with Sr, Zr, Ti and Ce quaternary composite microalloying, the preparation method is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si 7.66%、Cu 4.84%、Sr 0.57%、Zr0.59%、Ti 0.16%、Ce 0.15%, 余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si 7.66%, Cu 4.84%, Sr 0.57%, Zr 0.59%, Ti 0.16%, Ce 0.15%, and the balance is aluminum and inevitable impurity elements.
本实施例的铝合金的抗拉强度为368MPa,断裂伸长率为7.5%。结合附图2可以看出本实施例的铝合金撕裂棱很多,组织致密均匀,而疏松(缩松)很少;初生硅相很少,且尺寸很小,因而合金具有很高的强度和很好的塑性。The tensile strength of the aluminum alloy of this example is 368 MPa, and the elongation at break is 7.5%. With reference to Figure 2, it can be seen that the aluminum alloy of this embodiment has many tear edges, the structure is dense and uniform, and the porosity (shrinkage) is very small; the primary silicon phase is very small, and the size is small, so the alloy has high strength and Very good plasticity.
实施例3。Example 3.
一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金,其制备方法与实施例1相同。A high-strength and high-plasticity Al-Si-Cu based cast aluminum alloy with Sr, Zr, Ti and Ce quaternary composite microalloying, the preparation method is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si7.5%、Cu5.31%、Sr0.55%、Zr0.46%、Ti0.18%、Ce0.23%, 余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si7.5%, Cu5.31%, Sr0.55%, Zr0.46%, Ti0.18%, Ce0.23%, the balance is aluminum and unavoidable impurity elements.
本实施例的铝合金的抗拉强度为360MPa,断裂伸长率为7.25%。The tensile strength of the aluminum alloy of this example is 360 MPa, and the elongation at break is 7.25%.
对比例1。Comparative Example 1.
一种添加Sr、Zr的 Al-Si-Cu系铸造铝合金,本对比例铝合金的制备方法与实施例1相同。An Al-Si-Cu based cast aluminum alloy added with Sr and Zr. The preparation method of the aluminum alloy of this comparative example is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si7.39%、Cu4.9%、Sr0.54%、Zr0.36%,余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si7.39%, Cu4.9%, Sr0.54%, Zr0.36%, and the balance is aluminum and inevitable impurity elements.
本对比例的铝合金的抗拉强度为218.97MPa,断裂伸长率为3.25%。结合附图3可以看出本对比例的铝合金撕裂棱较少,疏松(缩松)较多,组织不够致密;初生硅相较多,且尺寸非常大,因而具有较低的强度和较差的塑性。The tensile strength of the aluminum alloy of this comparative example was 218.97 MPa, and the elongation at break was 3.25%. Combining with Fig. 3, it can be seen that the aluminum alloy of this comparative example has less tear edges, more porosity (shrinkage porosity), and the structure is not dense enough; the primary silicon is relatively large, and the size is very large, so it has lower strength and higher density. poor plasticity.
对比例2。Comparative Example 2.
一种添加Sr、Zr的 Al-Si-Cu系铸造铝合金,本对比例铝合金的制备方法与实施例1相同。An Al-Si-Cu based cast aluminum alloy added with Sr and Zr. The preparation method of the aluminum alloy of this comparative example is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si7.21%、Cu4.98%、Sr0.51%、Zr0.33%,余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si7.21%, Cu4.98%, Sr0.51%, Zr0.33%, and the balance is aluminum and inevitable impurity elements.
本对比例的铝合金的抗拉强度为208.84MPa,断裂伸长率为5%。结合附图3可以看出本对比例的铝合金撕裂棱很少,有明显的疏松(缩松),且数量很多,组织不致密;初生硅相很多,且尺寸很大,因而具有很低的强度和塑性。The tensile strength of the aluminum alloy of this comparative example is 208.84 MPa, and the elongation at break is 5%. Combining with Figure 3, it can be seen that the aluminum alloy of this comparative example has few tear edges, obvious porosity (shrinkage porosity), and the number is large, and the structure is not dense; the primary silicon phase is many, and the size is large, so it has a very low strength and plasticity.
对比例3。Comparative Example 3.
一种添加Sr、Zr的 Al-Si-Cu系铸造铝合金,本对比例铝合金的制备方法与实施例1相同。An Al-Si-Cu based cast aluminum alloy added with Sr and Zr. The preparation method of the aluminum alloy of this comparative example is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si6.93%、Cu3.45%、Sr0.42%、Zr0.42%,余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si6.93%, Cu3.45%, Sr0.42%, Zr0.42%, and the balance is aluminum and inevitable impurity elements.
本对比例的铝合金的抗拉强度为300.45MPa,断裂伸长率为3.5%。The tensile strength of the aluminum alloy of this comparative example is 300.45 MPa, and the elongation at break is 3.5%.
对比例4。Comparative Example 4.
一种添加Sr、Zr的 Al-Si-Cu系铸造铝合金,本对比例铝合金的制备方法与实施例1相同。An Al-Si-Cu based cast aluminum alloy added with Sr and Zr. The preparation method of the aluminum alloy of this comparative example is the same as that of Example 1.
本实施例的铝合金经EDS实际测量成分为:Si6.11%、Cu3.31%、Sr0.46%、Zr0.54%,余量为铝和不可避免的杂质元素。The actual composition of the aluminum alloy of this embodiment measured by EDS is: Si6.11%, Cu3.31%, Sr0.46%, Zr0.54%, and the balance is aluminum and inevitable impurity elements.
本对比例的铝合金的抗拉强度为299.69MPa,断裂伸长率为4%。The tensile strength of the aluminum alloy of this comparative example is 299.69 MPa, and the elongation at break is 4%.
本发明使用四元微合金化技术,制备的一种Sr、Zr、Ti和Ce四元复合微合金化的高强度高塑性Al-Si-Cu系铸造铝合金,抗拉强度360MPa~391.58MPa,相比Sr、Zr二元合金化的Al-Si-Cu系铸造铝合金最大提高了182.74MPa;断裂伸长率5.75~%7.5%,相比Sr、Zr二元合金化的Al-Si-Cu系铸造铝合金最大提高了4.25%。The invention uses the quaternary microalloying technology to prepare a high-strength and high-plasticity Al-Si-Cu cast aluminum alloy with Sr, Zr, Ti and Ce quaternary composite microalloying, and the tensile strength is 360MPa-391.58MPa, Compared with Sr, Zr binary alloyed Al-Si-Cu cast aluminum alloy, the maximum increase is 182.74MPa; the elongation at break is 5.75~%7.5%, compared with Sr, Zr binary alloyed Al-Si-Cu alloy The maximum increase of 4.25% for cast aluminum alloys.
以上对本发明的具体实施例进行了描述,需要理解的是本发明并不局限于上述特地实施方式,本领域技术人员可以在权利要求范围做出变形和修改,这并不影响本发明的实质内容。The specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the above-mentioned special embodiments, and those skilled in the art can make modifications and modifications within the scope of the claims, which do not affect the essence of the present invention. .
本发明未涉及部分与现有技术相同或可采用现有技术加以实现。The parts not involved in the present invention are the same as or can be implemented by using the prior art.
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111705245A (en) * | 2020-07-13 | 2020-09-25 | 西安工业大学 | A kind of heat treatment method of die-casting aluminum alloy material |
US20220258240A1 (en) * | 2021-02-12 | 2022-08-18 | Desktop Metal, Inc. | The jetting performance of molten metal alloys by controlling the concentration of key alloying elements |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106591638A (en) * | 2015-10-19 | 2017-04-26 | 通用汽车环球科技运作有限责任公司 | New high pressure die casting aluminum alloy for high temperature and corrosive applications |
CN109097646A (en) * | 2018-08-27 | 2018-12-28 | 江苏大学 | 780-820MPa ultrahigh-strength aluminum alloy and preparation method thereof |
US20190194780A1 (en) * | 2017-12-21 | 2019-06-27 | Novelis Inc. | Aluminum alloy articles having improved bond durability and inert surface aluminum alloy articles and methods of making and using the same |
-
2019
- 2019-09-12 CN CN201910865265.0A patent/CN110564992B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106591638A (en) * | 2015-10-19 | 2017-04-26 | 通用汽车环球科技运作有限责任公司 | New high pressure die casting aluminum alloy for high temperature and corrosive applications |
US20190194780A1 (en) * | 2017-12-21 | 2019-06-27 | Novelis Inc. | Aluminum alloy articles having improved bond durability and inert surface aluminum alloy articles and methods of making and using the same |
CN109097646A (en) * | 2018-08-27 | 2018-12-28 | 江苏大学 | 780-820MPa ultrahigh-strength aluminum alloy and preparation method thereof |
Non-Patent Citations (1)
Title |
---|
张秀梅等: "稀土Ce变质对ZL101合金铸态组织和性能的影响", 《铸造》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111705245A (en) * | 2020-07-13 | 2020-09-25 | 西安工业大学 | A kind of heat treatment method of die-casting aluminum alloy material |
US20220258240A1 (en) * | 2021-02-12 | 2022-08-18 | Desktop Metal, Inc. | The jetting performance of molten metal alloys by controlling the concentration of key alloying elements |
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