CN111926220A - Aluminum alloy material for high-performance thin-wall 3D printing sand casting and preparation method thereof - Google Patents
Aluminum alloy material for high-performance thin-wall 3D printing sand casting and preparation method thereof Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 88
- 238000010146 3D printing Methods 0.000 title claims abstract description 52
- 238000007528 sand casting Methods 0.000 title claims abstract description 45
- 238000002360 preparation method Methods 0.000 title claims abstract description 13
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 111
- 229910052782 aluminium Inorganic materials 0.000 claims description 50
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 50
- 238000003756 stirring Methods 0.000 claims description 49
- 239000004576 sand Substances 0.000 claims description 38
- 230000032683 aging Effects 0.000 claims description 36
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 30
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- 238000007872 degassing Methods 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 4
- 239000006104 solid solution Substances 0.000 claims description 3
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 20
- 229910052710 silicon Inorganic materials 0.000 abstract description 18
- 239000012535 impurity Substances 0.000 abstract description 13
- 229910052749 magnesium Inorganic materials 0.000 abstract description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 229910052726 zirconium Inorganic materials 0.000 abstract description 6
- 238000011161 development Methods 0.000 abstract description 5
- 229910052712 strontium Inorganic materials 0.000 abstract description 5
- 229910052706 scandium Inorganic materials 0.000 abstract description 3
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- 238000005266 casting Methods 0.000 description 33
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- 239000000243 solution Substances 0.000 description 23
- 239000002893 slag Substances 0.000 description 22
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 17
- 239000010703 silicon Substances 0.000 description 17
- 230000005496 eutectics Effects 0.000 description 14
- 239000011777 magnesium Substances 0.000 description 13
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- 230000018109 developmental process Effects 0.000 description 4
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- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 3
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 2
- 229910019018 Mg 2 Si Inorganic materials 0.000 description 2
- 229910000676 Si alloy Inorganic materials 0.000 description 2
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 2
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- 238000012360 testing method Methods 0.000 description 2
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- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
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- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
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- C22C1/00—Making non-ferrous alloys
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- C22C1/026—Alloys based on aluminium
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- 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
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- 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
Description
技术领域technical field
本发明涉及铝合金材料技术领域,特别涉及一种高性能薄壁3D打印砂型铸造用的铝合金材料及其制备方法。The invention relates to the technical field of aluminum alloy materials, in particular to an aluminum alloy material for high-performance thin-walled 3D printing sand casting and a preparation method thereof.
背景技术Background technique
随着现代工业的迅猛发展,铸造市场规模持续扩大,产品复杂度和制造灵活性要求越来越高,传统铸造已经无法满足市场对快速交付和高复杂度产品的需求。3D打印与传统树脂砂铸造相互融合形成的3D打印砂型铸造成为铸造的主要发展方向之一。3D打印砂型铸造可制造高度复杂产品,制造快速,尤其适用于复杂零部件(如汽车缸体、缸盖等)的研发和生产。由于环保和节能的需要,产品轻量化已经成为发展潮流,复杂零部件的设计不断向薄壁化、轻量化方向发展。铝合金比强度高,密度低,成为了主要的轻量化材料。With the rapid development of modern industry, the scale of the foundry market continues to expand, and the requirements for product complexity and manufacturing flexibility are getting higher and higher. Traditional casting has been unable to meet the market's demand for fast delivery and high-complexity products. The 3D printing sand casting formed by the fusion of 3D printing and traditional resin sand casting has become one of the main development directions of casting. 3D printing sand casting can manufacture highly complex products with rapid manufacturing, especially for the development and production of complex parts (such as automobile cylinder blocks, cylinder heads, etc.). Due to the needs of environmental protection and energy saving, product lightweighting has become a trend of development, and the design of complex parts is constantly developing towards thin-walled and lightweight. Aluminum alloy has high specific strength and low density, and has become the main lightweight material.
铸造铝合金具有良好的铸造性能,耐腐蚀,铸造成本低,被广泛应用于航空航天和汽车等领域。其中铸造Al-Si合金具有良好的流动性,被广泛应用于成形复杂铸件。微合金化是提高合金性能的重要手段之一。研究表明,在铸造铝硅合金中加入Mg元素可以使得合金在热处理之后析出Mg2Si相,大幅度提高合金的强度;加入Sr元素可以变质共晶硅,使其尺寸细小均匀;加入Zr、Ti、Sc和稀土元素等可以细化合金晶粒,同时提高合金的强度和韧性。Cast aluminum alloys have good casting properties, corrosion resistance, and low casting costs, and are widely used in aerospace and automotive fields. Among them, the cast Al-Si alloy has good fluidity and is widely used in forming complex castings. Microalloying is one of the important means to improve the properties of alloys. The research shows that the addition of Mg element to the cast Al-Si alloy can make the alloy precipitate Mg 2 Si phase after heat treatment, which greatly improves the strength of the alloy; the addition of Sr element can modify the eutectic silicon to make it small and uniform in size; the addition of Zr, Ti , Sc and rare earth elements can refine the alloy grains and improve the strength and toughness of the alloy at the same time.
中国专利CN111074111A公布的一种高强度铸造铝硅合金及其制造方法,铝硅合金的组成按重量百分比计包括:硅6.50-7.50%,镁0.30-0.45%,铁≤0.15%,钛0.10-0.20%,锆0.05-0.15%,锶0.01%-0.02%,硼≤0.20‰,不可避免的杂质≤0.10%,余量为Al。发明合金在热处理后抗拉强度可达320-340MPa,屈服强度280-300MPa,延伸率8%-11%。但是该发明合金的模具预热温度需要250℃,因为模具这个称呼只适用于金属铸型,也就是说该高强度铸造合金由金属模具铸造而成。中国专利CN107385289A公布的一种Zr和Sr复合微合金化的高强韧耐腐蚀亚共晶Al#Si系铸造铝合金及制备方法,该铸造铝合金主要由铝(Al)、硅(Si)、锆(Zr)和锶(Sr)组成,其中,硅(Si)的质量百分比为7.68-8.18%,锆(Zr)的质量百分比为0.184-0.191%,锶(Sr)的质量百分比为0.0199-0.023%,余量为铝和少量杂质元素,各组份的质量百分比之和为100%。该发明指出合金浇入至预热温度为300±10℃的金属模具中浇注成锭,这说明该发明合金的成形方式为金属型铸造。Chinese patent CN111074111A discloses a high-strength cast aluminum-silicon alloy and its manufacturing method. The composition of the aluminum-silicon alloy includes: silicon 6.50-7.50%, magnesium 0.30-0.45%, iron≤0.15%, titanium 0.10-0.20% by weight %, zirconium 0.05-0.15%, strontium 0.01%-0.02%, boron ≤ 0.20‰, inevitable impurities ≤ 0.10%, and the balance is Al. After heat treatment, the inventive alloy has a tensile strength of 320-340 MPa, a yield strength of 280-300 MPa, and an elongation of 8%-11%. However, the mold preheating temperature of the inventive alloy needs to be 250°C, because the name mold is only applicable to metal casting molds, that is to say, the high-strength casting alloy is cast from metal molds. Chinese patent CN107385289A discloses a Zr and Sr composite microalloyed high-strength, toughness, corrosion-resistant hypoeutectic Al#Si cast aluminum alloy and its preparation method. The cast aluminum alloy is mainly composed of aluminum (Al), silicon (Si), zirconium (Zr) and strontium (Sr), wherein the mass percentage of silicon (Si) is 7.68-8.18%, the mass percentage of zirconium (Zr) is 0.184-0.191%, and the mass percentage of strontium (Sr) is 0.0199-0.023% , the balance is aluminum and a small amount of impurity elements, and the sum of the mass percentages of each component is 100%. The invention points out that the alloy is poured into a metal mold with a preheating temperature of 300±10° C. to be cast into an ingot, which indicates that the forming method of the alloy of the invention is metal mold casting.
大量的研究成果是基于金属型铸造的铝合金得来,而3D打印的树脂砂型和金属型相比,具有显著不同的散热能力、渗透性、发气性及机械强度等。并且,因砂型结构复杂,3D打印成形的砂型生坯具有薄壁、多腔、异型的特点,目前的铸铝合金系列材料流动性差,导致其在浇注过程中局部区域充型困难,形成铸造缺陷;砂型冷却速度慢,砂铸铝合金的组织粗大,树枝晶发达,并且3D打印的砂型树脂含量高,容易形成气孔缺陷,导致其力学性能偏低。作为一种发展中的新型快速铸造技术,目前没有专门为其开发的铝合金材料。针对此种情况,急需通过设计优化铝合金成分、通过设计优化铸造工艺,开发一种适用于3D打印砂型铸造用的铝合金材料。A large number of research results are based on aluminum alloys cast by metal molds. Compared with metal molds, 3D printed resin sand molds have significantly different heat dissipation capabilities, permeability, gas generation and mechanical strength. In addition, due to the complex structure of the sand mold, the green sand mold formed by 3D printing has the characteristics of thin wall, multi-cavity and special shape. The current cast aluminum alloy series materials have poor fluidity, which makes it difficult to fill the local area during the pouring process, resulting in casting defects. ; The cooling speed of the sand mold is slow, the structure of the sand cast aluminum alloy is coarse, the dendrites are developed, and the resin content of the 3D printed sand mold is high, which is easy to form pore defects, resulting in low mechanical properties. As a developing new rapid casting technology, there is no aluminum alloy material specially developed for it at present. In view of this situation, it is urgent to optimize the composition of aluminum alloy by design, and optimize the casting process by design, so as to develop an aluminum alloy material suitable for 3D printing sand casting.
发明内容SUMMARY OF THE INVENTION
为了克服现有技术存在的上述不足,本发明的目的是提供一种高性能薄壁3D打印砂型铸造用的铝合金材料及其制备方法。In order to overcome the above deficiencies in the prior art, the purpose of the present invention is to provide an aluminum alloy material for high-performance thin-walled 3D printing sand casting and a preparation method thereof.
有鉴于此,本发明旨在提供一种高性能薄壁3D打印砂型铸造用的铝合金材料及其制备方法。In view of this, the present invention aims to provide an aluminum alloy material for high-performance thin-walled 3D printing sand casting and a preparation method thereof.
本发明的目的至少通过如下技术方案之一实现。The object of the present invention is achieved by at least one of the following technical solutions.
本发明提供的一种高性能薄壁3D打印砂型铸造用的铝合金材料,按照质量百分比计,包括:The aluminum alloy material for high-performance thin-wall 3D printing sand casting provided by the present invention, in terms of mass percentage, includes:
其他不可避免的杂质元素≤0.10%;Other unavoidable impurity elements≤0.10%;
余量为Al。The remainder is Al.
进一步地,所述高性能薄壁3D打印砂型铸造用的铝合金材料,按照质量百分比计,包括:Further, the aluminum alloy material for the high-performance thin-wall 3D printing sand casting, in terms of mass percentage, includes:
其他不可避免的杂质元素≤0.10%;Other unavoidable impurity elements≤0.10%;
余量为Al。The remainder is Al.
本发明提供的高性能薄壁3D打印砂型铸造用的铝合金材料适用于薄壁(2mm-20mm)的3D打印砂型铸造产品。The aluminum alloy material for high-performance thin-wall 3D printing sand casting provided by the present invention is suitable for thin-wall (2mm-20mm) 3D printing sand casting products.
本发明提供的一种制备所述的高性能薄壁3D打印砂型铸造用的铝合金材料的方法,包括如下步骤:A method for preparing the high-performance thin-walled 3D printing aluminum alloy material for sand casting provided by the present invention includes the following steps:
(1)配料,准备A356铝锭、Al-10Zr中间合金,Al-2Sc中间合金,Al-10Sr中间合金,Al-5Ti-B中间合金;在坩埚中加入A356铝锭,将A356铝锭放入电阻炉中,程序升温,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌均匀,确保成分均匀,得到铝液;(1) Ingredients, prepare A356 aluminum ingot, Al-10Zr master alloy, Al-2Sc master alloy, Al-10Sr master alloy, Al-5Ti-B master alloy; add A356 aluminum ingot to the crucible, and put the A356 aluminum ingot into In the resistance furnace, program the temperature, and after the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy, stir evenly with a stirring rod to ensure uniform composition, and obtain molten aluminum;
(2)保持步骤(1)所述铝液的温度为710-730℃,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置,得到混合液;(2) maintaining the temperature of the molten aluminum described in step (1) at 710-730° C., adding Al-5Ti-B master alloy, stirring until it is completely melted, and then standing to obtain a mixed solution;
(3)将步骤(2)所述混合物的温度保持在710-730℃,加入Al-10Sr中间合金,搅拌待其完全熔化,静置,扒渣,得到混合物;(3) maintaining the temperature of the mixture described in step (2) at 710-730 ° C, adding Al-10Sr master alloy, stirring until it is completely melted, standing, and slag removal to obtain a mixture;
(4)往步骤(3)所述混合物中通入高纯氩气进行除气处理,静置,扒渣,将所述混合物的温度稳定在710-740℃,浇注至3D打印的砂型中,然后在数显电阻炉中升温对铸件进行T6热处理,置于室温中空冷,得到所述高性能薄壁3D打印砂型铸造用的铝合金材料。(4) Pour high-purity argon gas into the mixture described in step (3) to carry out degassing treatment, let stand, remove slag, stabilize the temperature of the mixture at 710-740 ° C, and pour it into a 3D printed sand mold, Then, the casting is heated up in a digital display resistance furnace to perform T6 heat treatment, and then placed at room temperature for air cooling to obtain the aluminum alloy material for high-performance thin-walled 3D printing sand casting.
进一步地,步骤(1)所述程序升温为从室温按照每次升高100℃的顺序升温至730-750℃。Further, the temperature program in step (1) is to increase the temperature from room temperature to 730-750°C in an order of increasing 100°C each time.
进一步地,步骤(1)所述搅拌的时间为3-5min。Further, the stirring time of step (1) is 3-5min.
进一步地,步骤(2)所述静置的时间为5-15min。Further, the standing time described in step (2) is 5-15min.
进一步地,步骤(3)所述静置的时间为5-15min。Further, the standing time described in step (3) is 5-15min.
进一步地,步骤(4)中,往所述混合物中通入氩气进行除气处理的时间为5-15min。Further, in step (4), the time for degassing by passing argon into the mixture is 5-15min.
优选地,步骤(4)中,往所述混合物中通入氩气进行除气处理的时间为5min。Preferably, in step (4), the time for degassing treatment by passing argon into the mixture is 5 min.
进一步地,步骤(4)所述静置的时间为5-15min。Further, the standing time described in step (4) is 5-15min.
进一步地,步骤(4)所述3D打印的砂型的温度为25-100℃。Further, the temperature of the 3D printed sand mold in step (4) is 25-100°C.
进一步地,步骤(4)所述T6热处理包括:先进行固溶,固溶温度为480-550℃,固溶时间为3-8h,淬火介质为水,淬火介质的温度为4-100℃,淬火完毕后进行人工时效,时效温度为170-220℃,时效时间为8-12h。Further, the T6 heat treatment in step (4) includes: firstly performing solid solution, the solution temperature is 480-550°C, the solution time is 3-8h, the quenching medium is water, and the temperature of the quenching medium is 4-100°C, After quenching, artificial aging is carried out, the aging temperature is 170-220 ° C, and the aging time is 8-12 hours.
本发明的合金材料含有Si:6.5-8%,具有良好的铸造流动性,适用于3D打印的薄壁、异型的砂型型腔,解决充型困难问题。The alloy material of the invention contains Si: 6.5-8%, has good casting fluidity, is suitable for 3D printing thin-walled, special-shaped sand mold cavities, and solves the problem of difficult filling.
本发明的合金材料含有Mg:0.25-0.45%,合金经过T6热处理后析出Mg2Si相,大幅度提高强度;合金材料中含有Sr:0.01-0.04%,使得合金组织中的共晶硅细小均匀。The alloy material of the invention contains Mg: 0.25-0.45%, and the alloy undergoes T6 heat treatment to precipitate Mg 2 Si phase, which greatly improves the strength; the alloy material contains Sr: 0.01-0.04%, so that the eutectic silicon in the alloy structure is fine and uniform .
本发明的合金材料通过控制Ti、Zr和Sc的含量,使合金适应3D打印的砂型的导热能力,合金晶粒细小均匀,同时提高合金的强度和韧性。By controlling the content of Ti, Zr and Sc, the alloy material of the present invention makes the alloy adapt to the thermal conductivity of the 3D printed sand mold, the alloy grains are fine and uniform, and the strength and toughness of the alloy are improved at the same time.
本发明的合金材料组织细小均匀,气孔缺陷少,致密度高,解决了3D打印砂型铸造的铝合金容易产生气孔缺陷的问题。The alloy material of the invention has fine and uniform structure, few pore defects and high density, and solves the problem that the 3D printing sand casting aluminum alloy is prone to pore defects.
本发明的合金材料经过T6热处理之后,析出了含Zr和含Sc的纳米析出相,可以大幅度提高屈服强度和抗拉强度。After the alloy material of the present invention undergoes T6 heat treatment, nano-precipitated phases containing Zr and Sc are precipitated, which can greatly improve the yield strength and tensile strength.
与现有技术相比,本发明具有如下优点和有益效果:Compared with the prior art, the present invention has the following advantages and beneficial effects:
本发明提供的高性能薄壁3D打印砂型铸造用铝合金材料的制备方法,制备的3D打印砂型铸造薄壁铝合金,其组织细小均匀,呈细小花瓣状,气孔缺陷少,致密度高,热处理后具有更高的屈服强度、抗拉强度和断后伸长率,更高的硬度,将其用于3D打印砂型铸造,复杂薄壁零件将会具有更高的服役安全性,可以降低维护成本。The invention provides a method for preparing an aluminum alloy material for high-performance thin-walled 3D printing sand casting. The prepared 3D printing sand casting thin-walled aluminum alloy has fine and uniform structure, small petal shape, few pore defects, high density, and heat treatment. It has higher yield strength, tensile strength and elongation after fracture, and higher hardness. Using it for 3D printing sand casting, complex thin-walled parts will have higher service safety and reduce maintenance costs.
附图说明Description of drawings
图1为本发明实施例1的铝合金铸态金相图。Fig. 1 is the as-cast metallographic diagram of the aluminum alloy in Example 1 of the present invention.
图2为本发明实施例1的铝合金铸态SEM图。FIG. 2 is an as-cast SEM image of the aluminum alloy in Example 1 of the present invention.
图3为本发明实施例1的铝合金T6态SEM图。3 is an SEM image of the aluminum alloy in the T6 state of Example 1 of the present invention.
图4为本发明实施例2的铝合金铸态金相图。FIG. 4 is the as-cast metallographic diagram of the aluminum alloy in Example 2 of the present invention.
图5为本发明实施例2的铝合金铸态SEM图。FIG. 5 is an as-cast SEM image of the aluminum alloy in Example 2 of the present invention.
图6为本发明实施例2的铝合金T6态SEM图。FIG. 6 is an SEM image of the aluminum alloy in the T6 state of Example 2 of the present invention.
图7为本发明实施例3的铝合金铸态金相图。7 is a metallographic diagram of the as-cast aluminum alloy of Example 3 of the present invention.
图8为本发明实施例3的铝合金铸态SEM图。FIG. 8 is an as-cast SEM image of the aluminum alloy in Example 3 of the present invention.
图9为本发明实施例3的铝合金T6态SEM图。FIG. 9 is an SEM image of the aluminum alloy in the T6 state of Example 3 of the present invention.
图10为本发明实施例4的铝合金铸态金相图。FIG. 10 is the as-cast metallographic diagram of the aluminum alloy in Example 4 of the present invention.
图11为本发明实施例4的铝合金铸态SEM图。11 is an as-cast SEM image of the aluminum alloy of Example 4 of the present invention.
图12为本发明实施例4的铝合金T6态SEM图。12 is an SEM image of the aluminum alloy in the T6 state of Example 4 of the present invention.
图13为本发明实施例5的铝合金铸态金相图。13 is a metallographic diagram of the as-cast aluminum alloy of Example 5 of the present invention.
图14为本发明实施例5的铝合金铸态SEM图。14 is an as-cast SEM image of the aluminum alloy of Example 5 of the present invention.
图15为本发明实施例5的铝合金T6态SEM图。15 is an SEM image of the aluminum alloy in the T6 state of Example 5 of the present invention.
图16为本发明实施例6的铝合金铸态金相图。16 is a metallographic diagram of the as-cast aluminum alloy of Example 6 of the present invention.
图17为本发明实施例6的铝合金铸态SEM图。17 is an as-cast SEM image of the aluminum alloy of Example 6 of the present invention.
图18为本发明实施例6的铝合金T6态SEM图。18 is an SEM image of the aluminum alloy in the T6 state of Example 6 of the present invention.
具体实施方式Detailed ways
以下结合实例对本发明的具体实施作进一步说明,但本发明的实施和保护不限于此。需指出的是,以下若有未特别详细说明之过程,均是本领域技术人员可参照现有技术实现或理解的。所用试剂或仪器未注明生产厂商者,视为可以通过市售购买得到的常规产品。The specific implementation of the present invention will be further described below with reference to examples, but the implementation and protection of the present invention are not limited thereto. It should be pointed out that, if there are any processes that are not described in detail below, those skilled in the art can realize or understand them with reference to the prior art. If the reagents or instruments used do not indicate the manufacturer, they are regarded as conventional products that can be purchased in the market.
本实施例提供的薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:6.5-8%,Mg:0.25-0.45%;Ti:0.1-0.16%;Sr:0.01-0.04%;Fe:0.1-0.2%;Zr:0.16-0.6%;Sc:0-0.4%;其他不可避免的杂质元素≤0.10%;余量为Al。The aluminum alloy material for thin-wall 3D printing sand casting provided in this embodiment has the following main components and mass percentages: Si: 6.5-8%, Mg: 0.25-0.45%; Ti: 0.1-0.16%; Sr: 0.01- 0.04%; Fe: 0.1-0.2%; Zr: 0.16-0.6%; Sc: 0-0.4%; other unavoidable impurity elements≤0.10%; the balance is Al.
本发明还提供一种上述薄壁3D打印砂型铸造用铝合金材料的制备方法,包括如下步骤:The present invention also provides a method for preparing the above-mentioned thin-walled 3D printing aluminum alloy material for sand casting, comprising the following steps:
步骤1:配料,准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金。Step 1: batching, prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy.
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至730-750℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌3-5min,确保成分均匀;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, the resistance furnace is heated up to 730-750 ℃ in the order of increasing 100 ℃ each time, and after the charge is completely melted, add Al-10Zr master alloy and Al-2Sc For the master alloy, stir with a stirring rod for 3-5min to ensure uniform composition;
步骤3:铝液温度稳定在710-730℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置5-15min;Step 3: When the temperature of the molten aluminum is stable at 710-730°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 5-15min;
步骤4:温度回升至710-730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5-15min,扒渣;Step 4: When the temperature rises to 710-730°C, add Al-10Sr master alloy, stir until it is completely melted, let stand for 5-15min, and remove the slag;
步骤5:通入高纯氩气除气,通气时间5-15min,静置5-15min,扒渣。Step 5: Pour high-purity argon gas for degassing, the ventilation time is 5-15min, stand for 5-15min, and the slag is removed.
步骤6:铝液温度稳定至710-740℃,浇注至3D打印的砂型中,砂型温度为25-100℃。Step 6: The temperature of the aluminum liquid is stabilized to 710-740°C, and poured into the 3D printed sand mold, and the sand mold temperature is 25-100°C.
步骤7:在数显电阻炉中对铸件进行T6热处理,具体工艺为:固溶温度470-550℃,固溶时间3-8h,淬火介质为水,温度4-100℃,淬火完毕后立即进行人工时效,时效温度170-220℃,时效时间8-12h。取出后置于室温空冷;Step 7: Perform T6 heat treatment on the casting in a digital display resistance furnace. The specific process is: solution temperature 470-550°C, solution time 3-8h, quenching medium is water, temperature 4-100°C, immediately after quenching. Artificial aging, aging temperature 170-220 ℃, aging time 8-12h. After taking it out, put it in the air to cool at room temperature;
本发明的铝合金材料利用3D打印砂型铸造出的薄壁铸件具有非常高的屈服强度、抗拉强度以及好的断后伸长率。The aluminum alloy material of the present invention uses a 3D printing sand mold to cast a thin-walled casting with very high yield strength, tensile strength and good elongation after fracture.
本发明实施例的3D打印砂型铸造铝合金经过T6热处理后可以大大提高铸件性能。The 3D printing sand casting aluminum alloy in the embodiment of the present invention can greatly improve the casting performance after T6 heat treatment.
本发明实施例的铝合金材料经过T6热处理后硬度可以达到108HB,抗拉强度大于280MPa。The aluminum alloy material in the embodiment of the present invention can have a hardness of 108HB after T6 heat treatment, and a tensile strength greater than 280MPa.
下面结合实施例对本发明作进一步详细的说明。The present invention will be described in further detail below in conjunction with the embodiments.
实施例1Example 1
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:6.5%;Mg:0.35%;Ti:0.136%;Sr:0.031%;Fe:0.138%;Zr:0.16%;Sc:0.15%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 6.5%; Mg: 0.35%; Ti: 0.136%; Sr: 0.031%; Fe: 0.138%; Zr : 0.16%; Sc: 0.15%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:配料,准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金。Step 1: batching, prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy.
步骤2:在坩埚中加入A356铝锭,并放入电阻炉,电阻炉按照每次升高100℃的顺序升温至750℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌3min,确保成分均匀;Step 2: Add A356 aluminum ingot into the crucible and put it into the resistance furnace. The resistance furnace is heated to 750 °C in the order of increasing 100 °C each time. After the charge is completely melted, add Al-10Zr intermediate alloy and Al-2Sc intermediate Alloy, stir with a stirring rod for 3 minutes to ensure uniform composition;
步骤3:铝液温度稳定在710℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置5min;Step 3: When the temperature of the molten aluminum is stabilized at 710°C, add the Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 5 minutes;
步骤4:温度回升至720℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5min,扒渣;Step 4: When the temperature rises back to 720°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至725℃,浇注至3D打印的砂型中,砂型温度为50℃;The temperature of the molten aluminum returned to 725°C, poured into the 3D printed sand mold, and the sand mold temperature was 50°C;
对铸件进行T6热处理,具体工艺为:固溶温度540℃,固溶时间3h,淬火介质为水,温度60℃,淬火完毕后立即进行人工时效,时效温度170℃,时效时间12h。取出后置于室温空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 540°C, solution time 3h, quenching medium was water, temperature 60°C, artificial aging immediately after quenching, aging temperature 170°C, aging time 12h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为10mm。The wall thickness of the cast castings was 10 mm.
图1为实施例1的铝合金铸态金相图,由图1可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图2为实施例1的铝合金铸态SEM图,由图2可知,该材料的共晶硅尺寸细小均匀。图3为实施例1的铝合金T6态SEM图,由图3可知,该材料的共晶硅细小圆整。Figure 1 is the as-cast metallographic diagram of the aluminum alloy of Example 1. It can be seen from Figure 1 that the composition and formula of the material are suitable for the thermal conductivity of the 3D printing sand mold, and the structure is fine and uniform, and there are no coarse dendrites. FIG. 2 is an as-cast SEM image of the aluminum alloy of Example 1. It can be seen from FIG. 2 that the size of the eutectic silicon of the material is small and uniform. FIG. 3 is an SEM image of the aluminum alloy in the T6 state of Example 1. It can be seen from FIG. 3 that the eutectic silicon of the material is small and round.
实施例2Example 2
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:7.12%,Mg:0.38%;Ti:0.05%;Sr:0.038%;Fe:0.2%;Zr:0.25%;Sc:0.3%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 7.12%, Mg: 0.38%; Ti: 0.05%; Sr: 0.038%; Fe: 0.2%; Zr : 0.25%; Sc: 0.3%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:配料,准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: batching, prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌3min,确保成分均匀;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 3 minutes to ensure that the ingredients are uniform;
步骤3:铝液温度稳定在715℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置10min;Step 3: When the temperature of the molten aluminum is stabilized at 715°C, add the Al-5Ti-B master alloy, stir until it is completely melted, and then let it stand for 10 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置15min,扒渣;Step 4: When the temperature rises back to 730°C, add Al-10Sr master alloy, stir until it is completely melted, stand for 15 minutes, and remove the slag;
通入高纯氩气除气,通气时间10min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 10 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为80℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 80°C;
对铸件进行T6热处理,具体工艺为:固溶温度520℃,固溶时间4.5h,淬火介质为水,温度70℃,淬火完毕后立即进行人工时效,时效温度190℃,时效时间10h。取出后置于室温空冷。Perform T6 heat treatment on the castings. The specific process is: solution temperature 520°C, solution time 4.5h, quenching medium is water, temperature 70°C, artificial aging immediately after quenching, aging temperature 190°C, aging time 10h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为20mm。The wall thickness of the cast castings was 20mm.
图4为实施例2的铝合金铸态金相图,由图4可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图5为实施例2的铝合金铸态SEM图,由图5可知,该材料的共晶硅尺寸细小均匀。图6为实施例2的铝合金T6态SEM图,由图6可知,该材料经T6热处理之后,共晶硅细小圆整。Figure 4 is the as-cast metallographic diagram of the aluminum alloy of Example 2. It can be seen from Figure 4 that the composition and formula of the material are suitable for the thermal conductivity of the 3D printing sand mold, and the structure is fine and uniform, and there are no coarse dendrites. FIG. 5 is an as-cast SEM image of the aluminum alloy of Example 2. It can be seen from FIG. 5 that the size of the eutectic silicon of the material is small and uniform. FIG. 6 is the SEM image of the aluminum alloy in the T6 state of Example 2. It can be seen from FIG. 6 that the eutectic silicon is fine and round after the material is heat treated by T6.
实施例3Example 3
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:8%;Mg:0.45%;Ti:0.145%;Sr:0.026%;Fe:0.2%;Zr:0.30%;Sc:0.2%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 8%; Mg: 0.45%; Ti: 0.145%; Sr: 0.026%; Fe: 0.2%; Zr : 0.30%; Sc: 0.2%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:配料,准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: batching, prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,并放入电阻炉,电阻炉按照每次升高100℃的顺序升温至745℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌4min;Step 2: Add A356 aluminum ingot into the crucible and put it into the resistance furnace. The resistance furnace is heated up to 745 °C in the order of increasing 100 °C each time. After the charge is completely melted, add the Al-10Zr intermediate alloy and the Al-2Sc intermediate Alloy, stir with a stirring rod for 4 min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置15min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add the Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 15 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置15min,扒渣;Step 4: When the temperature rises back to 730°C, add Al-10Sr master alloy, stir until it is completely melted, stand for 15 minutes, and remove the slag;
通入高纯氩气除气,通气时间15min,静置10min,扒渣。Introduce high-purity argon to degas, ventilate for 15 minutes, let stand for 10 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为60℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the temperature of the sand mold was 60°C;
对铸件进行T6热处理,具体工艺为:固溶温度510℃,固溶时间5h,淬火介质为水,温度55℃,淬火完毕后立即进行人工时效,时效温度220℃,时效时间8h。取出置于室温放置空冷。Perform T6 heat treatment on the castings, the specific process is: solution temperature 510 ℃, solution time 5h, quenching medium is water, temperature 55 ℃, artificial aging immediately after quenching, aging temperature 220 ℃, aging time 8h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为4mm。The cast castings had a wall thickness of 4 mm.
图7为实施例3的铝合金铸态金相图,由图7可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图8为实施例3的铝合金铸态SEM图,由图8可知,该材料的共晶硅尺寸细小均匀。图9为实施例3的铝合金T6态SEM图,由图9可知,该材料经T6热处理之后,共晶硅细小圆整。FIG. 7 is the as-cast metallographic diagram of the aluminum alloy of Example 3. It can be seen from FIG. 7 that the composition and formula of the material are suitable for the thermal conductivity of the 3D printing sand mold, and the structure is fine and uniform, and there are no coarse dendrites. FIG. 8 is an as-cast SEM image of the aluminum alloy of Example 3. It can be seen from FIG. 8 that the size of the eutectic silicon of the material is small and uniform. FIG. 9 is an SEM image of the aluminum alloy in the T6 state of Example 3. It can be seen from FIG. 9 that the eutectic silicon is fine and round after the material is heat treated by T6.
实施例4Example 4
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:7.53%,Mg:0.40%;Ti:0.16%;Sr:0.034%;Fe:0.156%;Zr:0.16%;Sc:0.4%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 7.53%, Mg: 0.40%; Ti: 0.16%; Sr: 0.034%; Fe: 0.156%; Zr : 0.16%; Sc: 0.4%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至710℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5min,扒渣;Step 4: When the temperature rises to 710°C, add Al-10Sr master alloy, stir until it is completely melted, let stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置5min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 5 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为40℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 40°C;
对铸件进行T6热处理,具体工艺为:固溶温度540℃,固溶时间4.2h,淬火介质为水,温度70℃,淬火完毕后立即进行人工时效,时效温度180℃,时效时间8.5h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 540°C, solution time 4.2h, quenching medium was water, temperature 70°C, artificial aging immediately after quenching, aging temperature 180°C, aging time 8.5h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为2mm。The cast casting wall thickness was 2mm.
图10为实施例4的铝合金铸态金相图,由图10可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图11为实施例4的铝合金铸态SEM图,由图11可知,该材料的共晶硅尺寸细小均匀。12为实施例4的铝合金T6态SEM图,由图12可知,该材料经T6热处理之后,共晶硅细小圆整。Fig. 10 is the as-cast metallographic diagram of the aluminum alloy of Example 4. It can be seen from Fig. 10 that the composition of the material is suitable for the thermal conductivity of the 3D printing sand mold, and the structure is fine and uniform, and there are no coarse dendrites. FIG. 11 is an as-cast SEM image of the aluminum alloy of Example 4. It can be seen from FIG. 11 that the size of the eutectic silicon of the material is fine and uniform. 12 is the SEM image of the aluminum alloy in the T6 state of Example 4. It can be seen from FIG. 12 that the eutectic silicon is fine and round after the material is heat treated by T6.
实施例5Example 5
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:6.5%;Mg:0.32%;Ti:0.10%;Sr:0.01%;Fe:0.16%;Zr:0.6%;Sc:0%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 6.5%; Mg: 0.32%; Ti: 0.10%; Sr: 0.01%; Fe: 0.16%; Zr : 0.6%; Sc: 0%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5min,扒渣;Step 4: When the temperature rises back to 730°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置15min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 15 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为100℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 100°C;
对铸件进行T6热处理,具体工艺为:固溶温度550℃,固溶时间3h,淬火介质为水,温度70℃,淬火完毕后立即进行人工时效,时效温度220℃,时效时间8h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 550°C, solution time 3h, quenching medium was water, temperature 70°C, artificial aging immediately after quenching, aging temperature 220°C, aging time 8h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为12mm。The cast casting wall thickness was 12mm.
图13为实施例5的铝合金铸态金相图,由图13可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图14为实施例5的铝合金铸态SEM图,由图14可知,该材料的共晶硅尺寸细小均匀。图15为实施例5的铝合金T6态SEM图,由图15可知,该材料经T6热处理之后,共晶硅细小圆整。Figure 13 is the as-cast metallographic diagram of the aluminum alloy of Example 5. It can be seen from Figure 13 that the composition of the material is suitable for the thermal conductivity of the 3D printing sand mold, and its structure is fine and uniform, and there are no coarse dendrites. FIG. 14 is an as-cast SEM image of the aluminum alloy of Example 5. It can be seen from FIG. 14 that the size of the eutectic silicon of the material is fine and uniform. FIG. 15 is the SEM image of the aluminum alloy in the T6 state of Example 5. It can be seen from FIG. 15 that the eutectic silicon is fine and round after the material is heat treated by T6.
实施例6Example 6
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:6.9%,Mg:0.4%;Ti:0.145%;Sr:0.04%;Fe:0.1%;Zr:0.2%;Sc:0.02%;其他不可避免的杂质元素≤0.10%;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 6.9%, Mg: 0.4%; Ti: 0.145%; Sr: 0.04%; Fe: 0.1%; Zr : 0.2%; Sc: 0.02%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5分钟,扒渣;Step 4: When the temperature rises to 730°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为25℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 25°C;
对铸件进行T6热处理,具体工艺为:固溶温度480℃,固溶时间8h,淬火介质为水,温度4℃,淬火完毕后立即进行人工时效,时效温度180℃,时效时间11h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 480°C, solution time 8h, quenching medium was water, temperature 4°C, artificial aging immediately after quenching, aging temperature 180°C, aging time 11h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为6mm。The cast castings had a wall thickness of 6 mm.
图16为实施例6的铝合金铸态金相图,由图16可知,该材料的成分配方适应3D打印砂型的导热能力,其组织细小均匀,不存在粗大的树枝晶。图17为实施例6的铝合金铸态SEM图,由图17可知,该材料的共晶硅尺寸细小均匀。图18为实施例6的铝合金T6态SEM图,由图18可知,该材料经T6热处理之后,共晶硅细小圆整。Fig. 16 is the as-cast metallographic diagram of the aluminum alloy of Example 6. It can be seen from Fig. 16 that the composition of the material is suitable for the thermal conductivity of the 3D printing sand mold, and its structure is fine and uniform, and there are no coarse dendrites. FIG. 17 is an as-cast SEM image of the aluminum alloy of Example 6. It can be seen from FIG. 17 that the size of the eutectic silicon of the material is fine and uniform. FIG. 18 is an SEM image of the aluminum alloy in the T6 state of Example 6. It can be seen from FIG. 18 that the eutectic silicon is fine and round after the material is heat-treated by T6.
实施例7Example 7
一种高性能薄壁3D打印砂型铸造用的铝合金材料,其主要成分和质量百分比如下:Si:8%,Mg:0.25%;Ti:0.15%;Sr:0.026%;Fe:0.14%;Zr:0.20%;Sc:0.02%;其他不可避免的杂质元素≤0.10%;;余量为Al。An aluminum alloy material for high-performance thin-wall 3D printing sand casting, the main components and mass percentages are as follows: Si: 8%, Mg: 0.25%; Ti: 0.15%; Sr: 0.026%; Fe: 0.14%; Zr : 0.20%; Sc: 0.02%; other unavoidable impurity elements≤0.10%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5min,扒渣;Step 4: When the temperature rises back to 730°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间7min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 7 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为50℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 50°C;
对铸件进行T6热处理,具体工艺为:固溶温度540℃,固溶时间4.2h,淬火介质为水,温度70℃,淬火完毕后立即进行人工时效,时效温度180℃,时效时间8.5h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 540°C, solution time 4.2h, quenching medium was water, temperature 70°C, artificial aging immediately after quenching, aging temperature 180°C, aging time 8.5h. Take it out and let it cool at room temperature.
浇注的铸件壁厚为8mm。The cast castings had a wall thickness of 8 mm.
对比例1:成分和质量百分比为:Si:5.91%,Mg:0.23%;Ti:0.146%;Sr:0.011%;Fe:0.136%;Zr:0.1%;Sc:0.05%;余量为Al。Comparative Example 1: The composition and mass percentage are: Si: 5.91%, Mg: 0.23%; Ti: 0.146%; Sr: 0.011%; Fe: 0.136%; Zr: 0.1%; Sc: 0.05%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5分钟,扒渣;Step 4: When the temperature rises to 730°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为25℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 25°C;
对铸件进行T6热处理,具体工艺为:固溶温度480℃,固溶时间8h,淬火介质为水,温度4℃,淬火完毕后立即进行人工时效,时效温度160℃,时效时间11h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 480°C, solution time 8h, quenching medium water, temperature 4°C, artificial aging immediately after quenching, aging temperature 160°C, aging time 11h. Take it out and let it cool at room temperature.
对比例1浇注的铸件壁厚为15mm。The wall thickness of the casting cast in Comparative Example 1 was 15 mm.
对比例2:成分和质量百分比为:Si:8.31%,Mg:0.43%;Ti:0.04%;Sr:0.05%;Fe:0.16%;Zr:0.15%;余量为Al。Comparative Example 2: The composition and mass percentage are: Si: 8.31%, Mg: 0.43%; Ti: 0.04%; Sr: 0.05%; Fe: 0.16%; Zr: 0.15%; the balance is Al.
步骤1:准备A356铝锭、Al-10Zr中间合金、Al-10Sr中间合金、Al-2Sc中间合金和Al-5Ti-B中间合金;Step 1: Prepare A356 aluminum ingot, Al-10Zr master alloy, Al-10Sr master alloy, Al-2Sc master alloy and Al-5Ti-B master alloy;
步骤2:在坩埚中加入A356铝锭,放入电阻炉,电阻炉按照每次升高100℃的顺序升温至740℃,待炉料完全熔化后,加入Al-10Zr中间合金和Al-2Sc中间合金,用搅拌棒搅拌5min;Step 2: Add A356 aluminum ingot into the crucible, put it into the resistance furnace, and the resistance furnace is heated to 740 ℃ in the order of increasing 100 ℃ each time. After the charge is completely melted, add Al-10Zr master alloy and Al-2Sc master alloy , stir with a stirring rod for 5min;
步骤3:铝液温度稳定在720℃时,加入Al-5Ti-B中间合金,搅拌待其完全熔化后,静置8min;Step 3: When the temperature of the molten aluminum is stable at 720°C, add Al-5Ti-B master alloy, stir until it is completely melted, and let it stand for 8 minutes;
步骤4:温度回升至730℃时,加入Al-10Sr中间合金,搅拌待其完全熔化,静置5分钟,扒渣;Step 4: When the temperature rises to 730°C, add Al-10Sr master alloy, stir until it is completely melted, let it stand for 5 minutes, and remove the slag;
通入高纯氩气除气,通气时间5min,静置7min,扒渣。Introduce high-purity argon to degas, ventilate for 5 minutes, let stand for 7 minutes, and remove slag.
铝液温度回升至730℃,浇注至3D打印的砂型中,砂型温度为100℃;The temperature of the molten aluminum returned to 730°C, poured into the 3D printed sand mold, and the sand mold temperature was 100°C;
对铸件进行T6热处理,具体工艺为:固溶温度480℃,固溶时间8h,淬火介质为水,温度4℃,淬火完毕后立即进行人工时效,时效温度250℃,时效时间11h。取出置于室温放置空冷。The castings were subjected to T6 heat treatment. The specific process was: solution temperature 480°C, solution time 8h, quenching medium was water, temperature 4°C, artificial aging immediately after quenching, aging temperature 250°C, aging time 11h. Take it out and let it cool at room temperature.
对比例2浇注的铸件壁厚为15mm。从表1的数据可以看出,本实施例1至7制备得到的3D打印砂型铸造铝合金的屈服强度大于250MPa,抗拉强度大于290MPa,硬度大于100HB,伸长率大于2%。抗拉强度和屈服强度远远大于对比例1和对比例2,伸长率和硬度的数据均大于对比例1和对比例2。并且本发明的铝合金尤其适合薄壁3D打印砂型铸造,可以带来更高的服役安全性和降低维护成本。The wall thickness of the casting cast in Comparative Example 2 was 15 mm. It can be seen from the data in Table 1 that the yield strength of the 3D printed sand casting aluminum alloys prepared in Examples 1 to 7 is greater than 250MPa, the tensile strength is greater than 290MPa, the hardness is greater than 100HB, and the elongation is greater than 2%. The tensile strength and yield strength are much greater than those of Comparative Examples 1 and 2, and the elongation and hardness data are both greater than those of Comparative Examples 1 and 2. And the aluminum alloy of the present invention is especially suitable for thin-wall 3D printing sand casting, which can bring higher service safety and reduce maintenance costs.
对各个实施例和对比例进行室温拉伸力学性能测试(GB/T 228.1-2010)和布氏硬度测试,测试结果如下表1所示。The room temperature tensile mechanical property test (GB/T 228.1-2010) and the Brinell hardness test were performed on each embodiment and the comparative example, and the test results are shown in Table 1 below.
表1Table 1
从表1的数据可以看出,本实施例1至7制备得到的3D打印砂型铸造铝合金的屈服强度大于250MPa,抗拉强度大于290MPa,硬度大于100HB,伸长率大于2%。抗拉强度和屈服强度远远大于对比例1和对比例2,伸长率和硬度的数据均大于对比例1和对比例2。并且本发明的铝合金尤其适合薄壁3D打印砂型铸造,可以带来更高的服役安全性和降低维护成本。It can be seen from the data in Table 1 that the yield strength of the 3D printed sand casting aluminum alloys prepared in Examples 1 to 7 is greater than 250MPa, the tensile strength is greater than 290MPa, the hardness is greater than 100HB, and the elongation is greater than 2%. The tensile strength and yield strength are much greater than those of Comparative Examples 1 and 2, and the elongation and hardness data are both greater than those of Comparative Examples 1 and 2. And the aluminum alloy of the present invention is especially suitable for thin-wall 3D printing sand casting, which can bring higher service safety and reduce maintenance costs.
以上实施例仅为本发明较优的实施方式,仅用于解释本发明,而非限制本发明,本领域技术人员在未脱离本发明精神实质下所作的改变、替换、修饰等均应属于本发明的保护范围。The above examples are only preferred embodiments of the present invention, and are only used to explain the present invention, but not to limit the present invention. Changes, substitutions, modifications, etc. made by those skilled in the art without departing from the spirit of the present invention shall belong to the present invention. the scope of protection of the invention.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114635065A (en) * | 2021-12-26 | 2022-06-17 | 昆明理工大学 | A kind of toughened A356 aluminum alloy and preparation method thereof |
CN115198149A (en) * | 2022-07-21 | 2022-10-18 | 栋梁铝业有限公司 | Heat treatment-free die-casting aluminum alloy and preparation method thereof |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105886854A (en) * | 2016-06-08 | 2016-08-24 | 天津大学 | Preparing method for reducing Fe intermediate phase harm and improving mechanical performance of A356 cast alloy containing scandium and zircon |
CN107282892A (en) * | 2017-07-21 | 2017-10-24 | 北京航星机器制造有限公司 | A kind of 3D printing core formative method of aluminium alloy castings |
CN111074111A (en) * | 2019-12-26 | 2020-04-28 | 中信戴卡股份有限公司 | High-strength cast aluminum-silicon alloy and manufacturing method thereof |
-
2020
- 2020-07-21 CN CN202010706671.5A patent/CN111926220A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105886854A (en) * | 2016-06-08 | 2016-08-24 | 天津大学 | Preparing method for reducing Fe intermediate phase harm and improving mechanical performance of A356 cast alloy containing scandium and zircon |
CN107282892A (en) * | 2017-07-21 | 2017-10-24 | 北京航星机器制造有限公司 | A kind of 3D printing core formative method of aluminium alloy castings |
CN111074111A (en) * | 2019-12-26 | 2020-04-28 | 中信戴卡股份有限公司 | High-strength cast aluminum-silicon alloy and manufacturing method thereof |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114635065A (en) * | 2021-12-26 | 2022-06-17 | 昆明理工大学 | A kind of toughened A356 aluminum alloy and preparation method thereof |
CN115198149A (en) * | 2022-07-21 | 2022-10-18 | 栋梁铝业有限公司 | Heat treatment-free die-casting aluminum alloy and preparation method thereof |
CN115198149B (en) * | 2022-07-21 | 2023-03-10 | 栋梁铝业有限公司 | Heat treatment-free die-casting aluminum alloy and preparation method thereof |
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