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CN108796324A - A kind of room temperature high-ductility magnesium-tin-yttrium-zircaloy and preparation method thereof - Google Patents

A kind of room temperature high-ductility magnesium-tin-yttrium-zircaloy and preparation method thereof Download PDF

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CN108796324A
CN108796324A CN201810717720.8A CN201810717720A CN108796324A CN 108796324 A CN108796324 A CN 108796324A CN 201810717720 A CN201810717720 A CN 201810717720A CN 108796324 A CN108796324 A CN 108796324A
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magnesium
yttrium
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tin
ingot
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蒋斌
王庆航
宋江凤
柴炎福
赵俊
黄光胜
张丁非
胡耀波
潘复生
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Chongqing University
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/03Making non-ferrous alloys by melting using master alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/06Alloys based on magnesium with a rare earth metal as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

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Abstract

本发明涉及一种室温高塑性镁‑锡‑钇‑锆合金及其制备方法,属于镁合金技术领域,该镁合金按质量百分比计,由如下组分组成:Sn 0.2‑0.4%;Y 0.4‑0.9%;Zr 0.4‑0.6%;不可避免杂质≤0.15%;余量为镁。通过向镁合金中加入Sn、Y和Zr元素并同时控制三种元素的含量,不但可以保证最终制备的镁合金具有高塑性,伸率高达40%,还可以保证该镁合金拥有中等的屈服强度和抗拉强度。在制备该镁合金时,只需加入少量的稀土元素,就能显著改变镁合金的塑性,且其制备方法简单,只需进行一次传统挤压,并不需要复杂的加工工艺,所使用的熔炼炉、挤压机均为常规通用设备,可移植性强,便于在工业中实现。

The invention relates to a magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature and a preparation method thereof, belonging to the technical field of magnesium alloys. The magnesium alloy consists of the following components in terms of mass percentage: Sn 0.2-0.4%; Y 0.4-0.4% 0.9%; Zr 0.4‑0.6%; unavoidable impurities ≤ 0.15%; the balance is magnesium. By adding Sn, Y and Zr elements to the magnesium alloy and controlling the content of the three elements at the same time, not only can the final magnesium alloy be guaranteed to have high plasticity, the elongation rate is as high as 40%, and the magnesium alloy can also be guaranteed to have a medium yield strength. and tensile strength. When preparing the magnesium alloy, only a small amount of rare earth elements can be added to significantly change the plasticity of the magnesium alloy, and the preparation method is simple, only one traditional extrusion is required, and no complicated processing technology is required. Furnace and extruder are general-purpose equipment, which are highly portable and easy to implement in industry.

Description

一种室温高塑性镁-锡-钇-锆合金及其制备方法A kind of magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature and preparation method thereof

技术领域technical field

本发明属于镁合金技术领域,具体涉及一种室温高塑性镁-锡-钇-锆合金及其制备方法。The invention belongs to the technical field of magnesium alloys, in particular to a magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature and a preparation method thereof.

背景技术Background technique

镁及镁合金具有低密度、高比强度、高比刚度、良好的电磁屏蔽性能等优点,在航空航天、汽车轻量化、电子通讯等领域具有极其重要的应用价值和广阔前景。Magnesium and magnesium alloys have the advantages of low density, high specific strength, high specific stiffness, and good electromagnetic shielding performance. They have extremely important application values and broad prospects in the fields of aerospace, automotive lightweight, and electronic communications.

与铸造镁合金相比,变形镁合金具有更大的发展潜力,通过对材料结构的调控可获得更优良的力学性能。镁合金由于具有密排六方晶体结构,室温下的滑移系少,导致加工变形困难,因此,变形镁合金需要通过挤压、轧制等热变形手段加工而成,但是有限的滑移系使得镁合金发生塑性变形后容易形成强的基面织构,这种强的基面织构将会恶化后续镁合金板材的力学性能和室温成形性能。近年来,研究者们提出利用合金化的手段来调控基面织构,进而改善镁合金的力学性能和室温成形性能。在镁合金中添加稀土元素能够有效的弱化基面织构,改善镁合金的塑性和成形性能。但是由于稀土元素昂贵的价格,迫使研究者们开发低成本高性能镁合金。Compared with cast magnesium alloys, wrought magnesium alloys have greater development potential, and better mechanical properties can be obtained by adjusting the material structure. Due to the close-packed hexagonal crystal structure of magnesium alloy, there are few slip systems at room temperature, which makes it difficult to process and deform. Therefore, deformed magnesium alloys need to be processed by hot deformation methods such as extrusion and rolling, but the limited slip system makes Magnesium alloys tend to form a strong basal texture after plastic deformation, and this strong basal texture will deteriorate the mechanical properties and room temperature formability of subsequent magnesium alloy sheets. In recent years, researchers have proposed the use of alloying methods to control the basal texture, thereby improving the mechanical properties and room temperature forming properties of magnesium alloys. The addition of rare earth elements in magnesium alloys can effectively weaken the basal texture and improve the plasticity and formability of magnesium alloys. However, due to the high price of rare earth elements, researchers are forced to develop low-cost high-performance magnesium alloys.

发明内容Contents of the invention

有鉴于此,本发明的目的之一在于提供一种室温高塑性镁-锡-钇-锆合金;目的之二在于提供一种室温高塑性镁-锡-钇-锆合金的制备方法。In view of this, one of the objectives of the present invention is to provide a room temperature high plasticity magnesium-tin-yttrium-zirconium alloy; the second purpose is to provide a room temperature high plasticity magnesium-tin-yttrium-zirconium alloy preparation method.

为达到上述目的,本发明提供如下技术方案:To achieve the above object, the present invention provides the following technical solutions:

1、一种室温高塑性镁-锡-钇-锆合金,按质量百分比计,所述镁合金由如下组分组成:Sn 0.2-0.4%;Y 0.4-0.9%;Zr 0.4-0.6%;不可避免杂质≤0.15%;余量为镁。1. A magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature. In terms of mass percentage, the magnesium alloy is composed of the following components: Sn 0.2-0.4%; Y 0.4-0.9%; Zr 0.4-0.6%; Avoid impurities ≤ 0.15%; the balance is magnesium.

优选的,按质量百分比计,所述镁合金由如下组分组成:Sn 0.21%;Y 0.41%;Zr0.46%;不可避免杂质≤0.15%;余量为镁。Preferably, in terms of mass percentage, the magnesium alloy is composed of the following components: Sn 0.21%; Y 0.41%; Zr 0.46%; unavoidable impurities ≤ 0.15%; the balance is magnesium.

优选的,按质量百分比计,所述镁合金由如下组分组成:Sn 0.38%;Y 0.90%;Zr0.52%;不可避免杂质≤0.15%;余量为镁。Preferably, in terms of mass percentage, the magnesium alloy is composed of the following components: Sn 0.38%; Y 0.90%; Zr 0.52%; unavoidable impurities ≤ 0.15%; the balance is magnesium.

2、所述的一种室温高塑性镁-锡-钇-锆合金的制备方法,所述方法包括如下步骤:2. The preparation method of a room temperature high plasticity magnesium-tin-yttrium-zirconium alloy, the method comprising the following steps:

(1)熔炼:在保护气氛下,将纯镁锭加热到670-700℃,待所述纯镁锭全部熔化后打渣,然后升温至710-730℃,加入纯锡锭、镁钇中间合金和镁锆中间合金,充分搅拌熔炼,于710-730℃下保温20-30min后得到镁合金熔液;(1) Smelting: In a protective atmosphere, heat the pure magnesium ingot to 670-700°C, slag after the pure magnesium ingot is completely melted, then heat up to 710-730°C, add pure tin ingot, magnesium yttrium master alloy and magnesium-zirconium master alloy, fully stirred and smelted, and kept at 710-730°C for 20-30 minutes to obtain a magnesium alloy melt;

(2)铸造:将步骤(1)中得到的镁合金熔液打渣后浇注成型,空冷后得铸锭;(2) Casting: cast the magnesium alloy melt obtained in the step (1) after slag casting, and get an ingot after air cooling;

(3)机加工:将步骤(2)中得到的铸锭锯切、车皮后备用;(3) Machining: the ingot obtained in the step (2) is sawed, and the car is back for subsequent use;

(4)均匀化处理;(4) Homogenization treatment;

(5)挤压。(5) Squeeze.

优选的,步骤(1)中,所述保护气氛为CO2和SF6按体积比99:1形成的混合气体。Preferably, in step (1), the protective atmosphere is a mixed gas formed of CO 2 and SF 6 at a volume ratio of 99:1.

优选的,步骤(1)中,所述镁钇中间合金钇的质量百分比为28-30%。Preferably, in step (1), the mass percent of the magnesium-yttrium master alloy yttrium is 28-30%.

优选的,步骤(1)中,所述镁锆中间合金锆的质量百分比为28-30%。Preferably, in step (1), the mass percentage of the magnesium-zirconium master alloy zirconium is 28-30%.

优选的,步骤(1)中,所述加入纯锡锭、镁钇中间合金和镁锆中间合金的具体方式为:待所述纯锡锭熔化后,静置5min后加入镁钇中间合金,再待所述镁钇中间合金熔化后,再静置5min后加入镁锆中间合金。Preferably, in step (1), the specific method of adding the pure tin ingot, magnesium-yttrium master alloy and magnesium-zirconium master alloy is: after the pure tin ingot is melted, add the magnesium-yttrium master alloy after standing for 5 minutes, and then After the magnesium-yttrium master alloy is melted, the magnesium-zirconium master alloy is added after standing still for 5 minutes.

优选的,步骤(4)中,所述均匀化处理具体为在350-370℃下保温12-24h。Preferably, in step (4), the homogenization treatment is specifically heat preservation at 350-370° C. for 12-24 hours.

优选的,步骤(5)中,所述挤压具体为:将挤压模具及经步骤(4)处理的铸锭在350-370℃下预热1-2h后,在挤压温度为350-370℃,挤压速度为6-10m·min-1,挤压比为33-55:1条件下进行。Preferably, in step (5), the extrusion specifically includes: after preheating the extrusion die and the ingot treated in step (4) at 350-370°C for 1-2h, the extrusion temperature is 350- 370°C, the extrusion speed is 6-10m·min -1 , and the extrusion ratio is 33-55:1.

本发明的有益效果在于:本发明提供了一种室温高塑性镁-锡-钇-锆合金及其制备方法,通过向镁合金中加入Sn、Y和Zr元素并同时控制三种元素的含量,不但可以保证最终制备的镁合金具有高塑性,伸率高达40%,还可以保证该镁合金拥有中等的屈服强度和抗拉强度。原因在于,纯镁中添加的三种元素的含量极少,大部分均固溶于镁基中,致使第二相的形成在很大程度上被减少,所以在拉伸过程中这些稀少的第二相便不足以成为拉伸裂纹源,进而保证最终制备的合金具有高塑性,表现为具有较高的延伸率。加之,由于Y元素主要以固溶在镁基体的形式存在,在挤压过程中促使稀土织构的形成,弱化合金的基面织构,在拉伸变形时促进基面滑移的开启,大大提高了合金的塑性。另外,固溶在镁基体的三种元素在一定程度上能起到固溶强化的效果,其中,Zr元素在熔炼过程中以α-Zr形式存在并作为形核质点,细化铸态合金的晶粒尺寸,进而使得挤压态合金的晶粒尺寸更为细小,促进合金拉伸强度的提高。固溶于镁基体的三种元素以原子的形式在晶界处富集,一方面能有效的阻碍晶界的运动,提高拉伸强度,两一方面又能提高晶界的结合能力,防止拉伸时晶界裂纹的产生,从而在一定程度上提高合金强度的同时有能大幅度增加合金的塑性。在制备该镁合金时所使用的原料成本低,只需加入少量的稀土元素,就能显著改变镁合金的塑性,且其制备方法简单,只需进行一次传统挤压,并不需要复杂的加工工艺,所使用的熔炼炉、挤压机均为常规通用设备,可移植性强,便于在工业中实现。The beneficial effects of the present invention are: the present invention provides a magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature and a preparation method thereof, by adding Sn, Y and Zr elements to the magnesium alloy and simultaneously controlling the content of the three elements, Not only can it ensure that the final prepared magnesium alloy has high plasticity and the elongation rate is as high as 40%, but it can also ensure that the magnesium alloy has medium yield strength and tensile strength. The reason is that the content of the three elements added in pure magnesium is very small, and most of them are solid-dissolved in the magnesium matrix, so that the formation of the second phase is greatly reduced, so these rare first phases are reduced during the stretching process. The two phases are not enough to be the source of tensile cracks, thereby ensuring that the final prepared alloy has high plasticity, which is manifested by high elongation. In addition, because the Y element mainly exists in the form of solid solution in the magnesium matrix, it promotes the formation of rare earth texture during the extrusion process, weakens the basal texture of the alloy, and promotes the opening of the basal slip during tensile deformation, greatly Improve the plasticity of the alloy. In addition, the three elements dissolved in the magnesium matrix can play a solid solution strengthening effect to a certain extent. Among them, the Zr element exists in the form of α-Zr during the smelting process and acts as a nucleation point to refine the as-cast alloy. Grain size, which in turn makes the grain size of the extruded alloy smaller and promotes the improvement of the tensile strength of the alloy. The three elements solid-soluble in the magnesium matrix are enriched at the grain boundary in the form of atoms. On the one hand, it can effectively hinder the movement of the grain boundary and improve the tensile strength. The generation of grain boundary cracks during stretching can improve the strength of the alloy to a certain extent and at the same time greatly increase the plasticity of the alloy. The cost of raw materials used in the preparation of the magnesium alloy is low, only a small amount of rare earth elements can be added to significantly change the plasticity of the magnesium alloy, and the preparation method is simple, only one traditional extrusion is required, and no complicated processing is required The process, the smelting furnace and the extruder used are all conventional general-purpose equipment, which are highly portable and easy to realize in industry.

附图说明Description of drawings

为了使本发明的目的、技术方案和有益效果更加清楚,本发明提供如下附图进行说明:In order to make the purpose, technical scheme and beneficial effect of the present invention clearer, the present invention provides the following drawings for illustration:

图1为实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的XRD图;((a)、(b)、(c)依次为实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的XRD图)Fig. 1 is the XRD figure of the magnesium-tin-yttrium-zirconium alloy sheet material prepared in embodiment 1, embodiment 2 and comparative example; ((a), (b), (c) are embodiment 1, embodiment successively 2 and the XRD pattern of the magnesium-tin-yttrium-zirconium alloy plate prepared in the comparative example)

图2为实施例1中制备的镁-锡-钇-锆合金板材的扫描电镜图;Fig. 2 is the scanning electron micrograph of the magnesium-tin-yttrium-zirconium alloy sheet material prepared in embodiment 1;

图3为实施例2中制备的镁-锡-钇-锆合金板材的扫描电镜图;Fig. 3 is the scanning electron micrograph of the magnesium-tin-yttrium-zirconium alloy sheet material prepared in embodiment 2;

图4为对比实施例中制备的镁-锡-钇-锆合金板材的扫描电镜图;Fig. 4 is the scanning electron micrograph of the magnesium-tin-yttrium-zirconium alloy sheet material prepared in the comparative example;

图5为将对比实施例中镁合金板材拉伸10%应变后的镁-锡-钇-锆合金板材的扫描电镜图;Fig. 5 is the scanning electron micrograph of the magnesium-tin-yttrium-zirconium alloy plate after stretching the magnesium alloy plate in the comparative example to 10% strain;

图6为实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的组织和织构图。((a)、(b)、(c)依次实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的IPF图;(d)、(e)、(f)依次实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的(0002)微观极图)Fig. 6 is the microstructure and texture diagram of the magnesium-tin-yttrium-zirconium alloy plates prepared in Example 1, Example 2 and Comparative Example. ((a), (b), (c) the IPF figure of the magnesium-tin-yttrium-zirconium alloy sheet material prepared in successive embodiment 1, embodiment 2 and comparative example; (d), (e), (f ) the (0002) microscopic pole figure of the magnesium-tin-yttrium-zirconium alloy plate prepared in sequentially embodiment 1, embodiment 2 and comparative example)

具体实施方式Detailed ways

下面将对本发明的优选实施例进行详细的描述。Preferred embodiments of the present invention will be described in detail below.

实施例1Example 1

一种室温高塑性镁-锡-钇-锆合金,按质量百分比计,该镁合金由如下组分组成:Sn 0.21%;Y 0.41%;Zr 0.46%;不可避免杂质≤0.15%;余量为镁。A magnesium-tin-yttrium-zirconium alloy with high plasticity at room temperature, the magnesium alloy is composed of the following components in terms of mass percentage: Sn 0.21%; Y 0.41%; Zr 0.46%; unavoidable impurities ≤ 0.15%; the balance is magnesium.

该室温高塑性镁-锡-钇-锆合金的制备方法如下:The preparation method of this room temperature high plasticity magnesium-tin-yttrium-zirconium alloy is as follows:

(1)熔炼:在CO2和SF6按体积比99:1形成的混合气体下,将纯镁锭加热到670℃,待所述纯镁锭全部熔化后打渣,然后升温至720℃,首先加入纯锡锭,待纯锡锭熔化后,静置5min,再加入镁钇中间合金,待镁钇中间合金熔化后,再静置5min,最后加入镁锆中间合金,充分搅拌熔炼,于720℃下保温20min后得到镁合金熔液,其中镁钇中间合金中钇的质量百分比为28%;镁锆中间合金锆的质量百分比为30%。(1) Smelting: Under the mixed gas of CO2 and SF6 at a volume ratio of 99:1, heat the pure magnesium ingot to 670°C, slag after the pure magnesium ingot is completely melted, and then raise the temperature to 720°C, First add pure tin ingot, after the pure tin ingot is melted, let it stand still for 5 minutes, then add the magnesium-yttrium master alloy, wait for the magnesium-yttrium master alloy to melt, then let it stand still for 5 minutes, finally add the magnesium-zirconium master alloy, fully stir and smelt, at 720 After being kept at ℃ for 20 minutes, a magnesium alloy melt was obtained, wherein the mass percentage of yttrium in the magnesium-yttrium master alloy was 28%; the mass percentage of zirconium in the magnesium-zirconium master alloy was 30%.

(2)铸造:将步骤(1)中得到的镁合金熔液打渣后浇注成型,空冷后得铸锭;(2) Casting: cast the magnesium alloy melt obtained in the step (1) after slag casting, and get an ingot after air cooling;

(3)机加工:将步骤(2)中得到的铸锭锯切、车皮至直径为70mm,高为60mm的锭子备用;(3) Machining: sawing and turning the ingot obtained in the step (2) to a diameter of 70mm and a height of 60mm for subsequent use;

(4)均匀化处理:将经步骤(3)处理后的铸锭在350℃下保温12h。(4) Homogenization treatment: keeping the ingot treated in step (3) at 350° C. for 12 hours.

(5)挤压:将挤压模具及经步骤(4)处理的铸锭在350℃下预热1.5h后,在挤压温度为350℃,挤压速度为6m·min-1,挤压比为33:1条件下进行挤压,制得镁-锡-钇-锆合金板材。(5) Extrusion: After preheating the extrusion die and the ingot treated in step (4) at 350°C for 1.5h, the extrusion temperature is 350°C and the extrusion speed is 6m·min -1 The extrusion is carried out under the condition of a ratio of 33:1 to obtain a magnesium-tin-yttrium-zirconium alloy plate.

实施例2Example 2

一种室温高塑性镁-锡-钇-锆合金,按质量百分比计,该镁合金由如下组分组成:Sn 0.38%;Y 0.90%;Zr 0.52%;不可避免杂质≤0.15%;余量为镁。A room temperature high plasticity magnesium-tin-yttrium-zirconium alloy, the magnesium alloy is composed of the following components by mass percentage: Sn 0.38%; Y 0.90%; Zr 0.52%; unavoidable impurities ≤ 0.15%; magnesium.

该室温高塑性镁-锡-钇-锆合金的制备方法如下:The preparation method of this room temperature high plasticity magnesium-tin-yttrium-zirconium alloy is as follows:

(1)熔炼:在CO2和SF6按体积比99:1形成的混合气体下,将纯镁锭加热到700℃,待所述纯镁锭全部熔化后打渣,然后升温至730℃,首先加入纯锡锭,待纯锡锭熔化后,静置5min,再加入镁钇中间合金,待镁钇中间合金熔化后,再静置5min,最后加入镁锆中间合金,充分搅拌熔炼,于730℃下保温30min后得到镁合金熔液,其中镁钇中间合金中钇的质量百分比为30%;镁锆中间合金锆的质量百分比为28%。(1) Smelting: Under the mixed gas formed by CO2 and SF6 at a volume ratio of 99:1, heat the pure magnesium ingot to 700°C, slag after the pure magnesium ingot is completely melted, and then raise the temperature to 730°C, First add pure tin ingot, after the pure tin ingot is melted, let it stand still for 5 minutes, then add the magnesium-yttrium master alloy, wait for the magnesium-yttrium master alloy to melt, then let it stand still for 5 minutes, finally add the magnesium-zirconium master alloy, fully stir and smelt, at 730 After being kept at ℃ for 30 minutes, a magnesium alloy melt is obtained, wherein the mass percentage of yttrium in the magnesium-yttrium master alloy is 30%; the mass percentage of zirconium in the magnesium-zirconium master alloy is 28%.

(2)铸造:将步骤(1)中得到的镁合金熔液打渣后浇注成型,空冷后得铸锭;(2) Casting: cast the magnesium alloy melt obtained in the step (1) after slag casting, and get an ingot after air cooling;

(3)机加工:将步骤(2)中得到的铸锭锯切、车皮至直径为70mm,高为60mm的锭子备用;(3) Machining: sawing and turning the ingot obtained in the step (2) to a diameter of 70mm and a height of 60mm for subsequent use;

(4)均匀化处理:将经步骤(3)处理后的铸锭在370℃下保温24h。(4) Homogenization treatment: keeping the ingot treated in step (3) at 370° C. for 24 hours.

(5)挤压:将挤压模具及经步骤(4)处理的铸锭在370℃下预热2h后,在挤压温度为370℃,挤压速度为10m·min-1,挤压比为55:1条件下进行挤压,制得镁-锡-钇-锆合金板材。(5) Extrusion: After preheating the extrusion die and the ingot treated in step (4) at 370°C for 2 hours, the extrusion temperature is 370°C, the extrusion speed is 10m·min -1 , and the extrusion ratio Extrusion is carried out under the condition of 55:1 to obtain a magnesium-tin-yttrium-zirconium alloy plate.

对比实施例comparative example

一种中等Sn和Y含量的镁-锡-钇-锆合金,按质量百分比计,该镁合金由如下组分组成:Sn 2.1%;Y 2.0%;Zr 0.56%;不可避免杂质≤0.15%;余量为镁。该合金的制备方法参见实施例1。A magnesium-tin-yttrium-zirconium alloy with medium Sn and Y content, the magnesium alloy is composed of the following components in terms of mass percentage: Sn 2.1%; Y 2.0%; Zr 0.56%; unavoidable impurities ≤ 0.15%; The balance is magnesium. Refer to Example 1 for the preparation method of the alloy.

利用X射线衍射仪(Rigaku D/Max 2500)分别对实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材进行分析,结果如图1所示,其中,图1中(a)、(b)、(c)依次为实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的XRD图,由图1可知,实施例1中制备的镁-锡-钇-锆合金板材中仅发现α-Mg基体,随着Sn、Y含量的增加,实施例2和对比实施例中的镁-锡-钇-锆合金板材中出现Sn3Y5和MgSnY第二相,但是没有发现含Zr元素的衍射峰。由XRD图的峰强和衍射峰的数量来判断,在实施例2中镁-锡-钇-锆合金板材中MgSnY三元相的衍射峰强度弱,数量少,而对比实施例中镁-锡-钇-锆合金板材中该相的峰强度大,数量多。因此,可以得出Sn3Y5在合金凝固过程中优先形成,随着Sn和Y含量的增加,MgSnY三元相逐渐形成。Utilize X-ray diffractometer (Rigaku D/Max 2500) to analyze the magnesium-tin-yttrium-zirconium alloy sheet material prepared in embodiment 1, embodiment 2 and comparative example respectively, the result is as shown in Figure 1, wherein, (a), (b), and (c) in 1 are successively the XRD patterns of the magnesium-tin-yttrium-zirconium alloy plates prepared in Example 1, Example 2 and Comparative Examples, as can be seen from Figure 1, Example 1 Only α-Mg matrix is found in the magnesium-tin-yttrium-zirconium alloy plate prepared in 3 Y 5 and the second phase of MgSnY, but no diffraction peaks containing Zr elements were found. Judging by the peak intensity and the number of diffraction peaks of the XRD figure, the diffraction peak intensity of the MgSnY ternary phase in the magnesium-tin-yttrium-zirconium alloy plate in Example 2 is weak and the number is small, while the magnesium-tin phase in the comparative example - The phase has a large peak intensity and a large number in the yttrium-zirconium alloy plate. Therefore, it can be concluded that Sn 3 Y 5 is preferentially formed during the solidification process of the alloy, and the MgSnY ternary phase gradually forms with the increase of Sn and Y content.

利用TESCAN VEGA 3LMH扫描电子显微镜分别对实施例1、实施例2、对比实施例中制备的镁-锡-钇-锆合金板材及将对比实施例中镁合金板材拉伸10%应变后的镁-锡-钇-锆合金板材进行分析,结果如图2、图3、图4和图5所示,其中,由图2可知,实施例1中制备的镁-锡-钇-锆合金板材中第二相的数量相当的少,这与其XRD图中除α-Mg相之外的无其它第二相的结果相符;由图3和图4可知,实施例2和对比实施例中制备的镁-锡-钇-锆合金板材中第二相的数量逐渐增加,第二相的形貌呈现不规则的细小颗粒状,沿着挤压方向呈流线分布,且对比实施例中制备的镁-锡-钇-锆合金板材中第二相的数量远大于实施例2制备的镁-锡-钇-锆合金板材中第二相的数量,并且出现较多的大块不规则的第二相,这也与两种板材的XRD图展示的结果相符。Using a TESCAN VEGA 3LMH scanning electron microscope, the magnesium-tin-yttrium-zirconium alloy sheet prepared in Example 1, Example 2, and the comparative example and the magnesium-tin-yttrium-zirconium alloy sheet prepared in the comparative example after stretching the magnesium alloy sheet to 10% strain were respectively analyzed. Tin-yttrium-zirconium alloy plate is analyzed, and the results are as shown in Figure 2, Figure 3, Figure 4 and Figure 5, wherein, as can be seen from Figure 2, the magnesium-tin-yttrium-zirconium alloy plate prepared in Example 1 is the first The quantity of two phases is quite few, and this agrees with the result that there is no other second phase except α-Mg phase in its XRD figure; As can be seen from Fig. 3 and Fig. 4, the magnesium-prepared in embodiment 2 and comparative example- The quantity of the second phase in the tin-yttrium-zirconium alloy plate gradually increases, and the morphology of the second phase presents irregular fine particles, which are distributed in a streamline along the direction of extrusion, and the magnesium-tin prepared in the comparative example - The amount of the second phase in the yttrium-zirconium alloy plate is much greater than the amount of the second phase in the magnesium-tin-yttrium-zirconium alloy plate prepared in Example 2, and there are more large and irregular second phases, which It is also consistent with the results shown in the XRD patterns of the two plates.

由于大量细小弥散分布的第二相能够有效的钉扎晶界,进而细化合金的晶粒尺寸,提高合金的强度,但与此同时,大量大块不规则的第二相在拉伸过程中将成为拉伸裂纹源,在很大程度上降低了合金的塑性。由图5可知,在大块第二相处出现明显的裂纹,由此说明,大量大块不规则的第二相在拉伸过程中可以成为拉伸裂纹源,使得合金塑性降低。Because a large number of fine and dispersed second phases can effectively pin the grain boundaries, thereby refining the grain size of the alloy and improving the strength of the alloy, but at the same time, a large number of large and irregular second phases are in the process of stretching. It will become the source of tensile cracks and reduce the plasticity of the alloy to a large extent. It can be seen from Figure 5 that there are obvious cracks in the bulk second phase, which shows that a large number of large irregular second phases can become the source of tensile cracks during the stretching process, which reduces the plasticity of the alloy.

利用JEOL JSM-7800F场发射电子显微镜分别对实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材进行组织和织构分析,结果如图6所示,图6中(a)、(b)、(c)依次实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的IPF图,由图6中(a)、(b)、(c)可知,随着Sn元素含量的增加,晶粒尺寸越来越小,平均晶粒尺寸从~10μm下降到~6μm,三种合金中由于基体中均匀弥散分布的细小第二相颗粒能够有效促进动态再结晶的形成,同时钉扎在晶界,阻碍再结晶晶粒长大,同时,第二相和晶界还可以阻碍位错运动,起到钉扎位错的作用使得晶粒细化,另外,Zr元素在镁熔体中一部分以α-Zr形式存在,成为镁晶体形核的质点,细化铸态镁-锡-钇-锆合金晶粒尺寸,在进一步的挤压过程中晶粒可以得到进一步的细化。图6中(d)、(e)、(f)依次实施例1、实施例2及对比实施例中制备的镁-锡-钇-锆合金板材的(0002)微观极图,由图6中(d)、(e)、(f)可知,三种合金板材均呈现出典型的双峰织构特性,最大极密度出现在沿挤压方向发生~20°偏转的位置,只是极密度随着Sn元素含量的增加而减少。Utilize JEOL JSM-7800F field emission electron microscope to carry out microstructure and texture analysis to the magnesium-tin-yttrium-zirconium alloy plate prepared in embodiment 1, embodiment 2 and comparative example respectively, the result is as shown in Figure 6, Figure 6 Among (a), (b), (c) the IPF figure of the magnesium-tin-yttrium-zirconium alloy sheet material that prepares in embodiment 1, embodiment 2 and comparative example successively, by (a) among Fig. 6, (b ), (c) it can be seen that with the increase of Sn element content, the grain size becomes smaller and smaller, and the average grain size decreases from ~10μm to ~6μm. Particles can effectively promote the formation of dynamic recrystallization, and at the same time, they are pinned to the grain boundary to hinder the growth of recrystallized grains. In addition, part of the Zr element exists in the form of α-Zr in the magnesium melt, which becomes the nucleation point of the magnesium crystal, and refines the grain size of the as-cast magnesium-tin-yttrium-zirconium alloy. The grains can be further refined during the process. Among Fig. 6 (d), (e), (f) the (0002) microcosmic pole figure of the magnesium-tin-yttrium-zirconium alloy plate that prepares in embodiment 1, embodiment 2 and comparative example successively, by in Fig. 6 (d), (e) and (f), it can be seen that the three alloy sheets all exhibit typical bimodal texture characteristics, and the maximum pole density appears at the position where ~20° deflection occurs along the extrusion direction, but the pole density increases with decrease with the increase of Sn content.

采用CMT5105-300kN微机控制电子万能试验机对商业AZ31镁合金板材、不含Zr元素的微合金化镁-锡-钇合金(Mg-0.4Sn-0.7Y)和实施例1、2及对比实施例中制备的镁-锡-钇-锆合金板材进行拉伸试验,结果如表1所示。Adopt CMT5105-300kN microcomputer control electronic universal testing machine to commercial AZ31 magnesium alloy sheet material, the microalloying magnesium-tin-yttrium alloy (Mg-0.4Sn-0.7Y) that does not contain Zr element and embodiment 1, 2 and comparative embodiment The magnesium-tin-yttrium-zirconium alloy plates prepared in the tensile test were carried out, and the results are shown in Table 1.

由表1可知,不含Zr元素的微合金化镁-锡-钇合金(Mg-0.4Sn-0.7Y)和实施例1、2中制备的镁-锡-钇-锆合金板材的延伸率明显高于商业AZ31和对比实施例中制备的镁-锡-钇-锆合金板材的延伸率,特别是实施例2中制备的镁合金板材的延伸率高达40.1%,且屈服强度和抗拉强度分别提高到180.3MPa和300.8MPa,这种优异的力学性能和延伸率有利于进一步的弯曲和杯突成形性能的提升。虽然在对比实施例中含有大量细小第二相,可以明显增强其屈服强度,但是其织构强度发生明显的弱化,在其二者的综合作用下,强度仍然低于实施例1、2中制备的镁-锡-钇-锆合金板材的强度。此外,由于对比实施例中镁-锡-钇-锆合金板材中大块第二相的出现,在拉伸过程中成为拉伸裂纹源,大大降低了其塑性。而对于不含Zr元素的微合金化镁-锡-钇合金,即使有较高的延伸率,但是该合金所表现出来的屈服强度远远低于实施例1、2中制备的镁-锡-钇-锆合金板材,这是由于Zr元素的添加,能有效的细化晶粒,在提高合金的拉伸强度的同时可以贡献一部分塑性,因此,不含Zr元素的微合金化镁-锡-钇合金和高Sn含量的镁-锡-钇-锆合金均不能适用于实际的工业应用,而本发明中的镁-锡-钇-锆合金板材经过一次热挤压过程后能获得高塑性中等强度的镁-锡-钇-锆合金板材,具有很高的工业应用价值。As can be seen from Table 1, the elongation of the microalloyed magnesium-tin-yttrium alloy (Mg-0.4Sn-0.7Y) and the magnesium-tin-yttrium-zirconium alloy plate prepared in Examples 1 and 2 without Zr element is obvious Higher than the elongation of the magnesium-tin-yttrium-zirconium alloy sheet prepared in the commercial AZ31 and comparative examples, especially the elongation of the magnesium alloy sheet prepared in Example 2 is as high as 40.1%, and the yield strength and tensile strength are respectively Increased to 180.3MPa and 300.8MPa, this excellent mechanical properties and elongation are conducive to further improvement of bending and cupping forming performance. Although the comparative example contains a large amount of fine second phases, which can significantly enhance its yield strength, its texture strength is obviously weakened, and under the combined effect of the two, the strength is still lower than that prepared in Examples 1 and 2. Strength of magnesium-tin-yttrium-zirconium alloy sheets. In addition, due to the appearance of the bulky second phase in the magnesium-tin-yttrium-zirconium alloy sheet in the comparative example, it becomes the source of tensile cracks during the stretching process, greatly reducing its plasticity. For the microalloyed magnesium-tin-yttrium alloy without Zr element, even though it has a higher elongation, the yield strength shown by the alloy is far lower than that of the magnesium-tin-yttrium alloy prepared in Examples 1 and 2. Yttrium-zirconium alloy plate, this is due to the addition of Zr element, which can effectively refine the grain, and can contribute part of the plasticity while improving the tensile strength of the alloy. Therefore, the microalloyed magnesium-tin- Both yttrium alloy and magnesium-tin-yttrium-zirconium alloy with high Sn content are not suitable for practical industrial applications, while the magnesium-tin-yttrium-zirconium alloy plate in the present invention can obtain high plasticity medium after a hot extrusion process High-strength magnesium-tin-yttrium-zirconium alloy sheet has high industrial application value.

最后说明的是,以上优选实施例仅用以说明本发明的技术方案而非限制,尽管通过上述优选实施例已经对本发明进行了详细的描述,但本领域技术人员应当理解,可以在形式上和细节上对其作出各种各样的改变,而不偏离本发明权利要求书所限定的范围。Finally, it should be noted that the above preferred embodiments are only used to illustrate the technical solutions of the present invention and not to limit them. Although the present invention has been described in detail through the above preferred embodiments, those skilled in the art should understand that it can be described in terms of form and Various changes may be made in the details without departing from the scope of the invention defined by the claims.

Claims (10)

1. a kind of room temperature high-ductility magnesium-tin-yttrium-zircaloy, which is characterized in that by mass percentage, the magnesium alloy is by such as The following group is grouped as:Sn 0.2-0.4%;Y 0.4-0.9%;Zr 0.4-0.6%;Inevitable impurity≤0.15%;Surplus is Magnesium.
2. a kind of room temperature high-ductility magnesium-tin-yttrium-zircaloy as described in claim 1, which is characterized in that by mass percentage Meter, the magnesium alloy are grouped as by following group:Sn 0.21%;Y 0.41%;Zr 0.46%;Inevitable impurity≤ 0.15%;Surplus is magnesium.
3. a kind of room temperature high-ductility magnesium-tin-yttrium-zircaloy as described in claim 1, which is characterized in that by mass percentage Meter, the magnesium alloy are grouped as by following group:Sn 0.38%;Y 0.90%;Zr 0.52%;Inevitable impurity≤ 0.15%;Surplus is magnesium.
4. a kind of preparation method of room temperature high-ductility magnesium-tin-yttrium-zircaloy of claim 1-3 any one of them, feature exist In described method includes following steps:
(1) melting:Under protective atmosphere, pure magnesium ingot is heated to 670-700 DEG C, the slag hitting after the pure magnesium ingot all fusing, 710-730 DEG C is then heated to, pure tin ingot, magnesium yttrium intermediate alloy and Mg-Zr intermediate alloy is added, melting is sufficiently stirred, in 710- Magnesium alloy melt is obtained after keeping the temperature 20-30min at 730 DEG C;
(2) it casts:By moulding by casting after the magnesium alloy melt slag hitting obtained in step (1), ingot casting is obtained after air-cooled;
(3) it machines:It will be spare after the ingot casting sawing obtained in step (2), railway carriage;
(4) Homogenization Treatments;
(5) it squeezes.
5. method as claimed in claim 4, which is characterized in that in step (1), the protective atmosphere is CO2And SF6By volume Than 99:1 mixed gas formed.
6. method as claimed in claim 4, which is characterized in that in step (1), the quality percentage of the magnesium yttrium intermediate alloy yttrium Than for 28-30%.
7. method as claimed in claim 4, which is characterized in that in step (1), the quality percentage of the Mg-Zr intermediate alloy zirconium Than for 28-30%.
8. method as claimed in claim 4, which is characterized in that in step (1), the addition pure tin ingot, magnesium yttrium intermediate alloy Concrete mode with Mg-Zr intermediate alloy is:After pure tin ingot fusing, magnesium yttrium intermediate alloy is added after standing 5min, then wait for After the magnesium yttrium intermediate alloy fusing, then Mg-Zr intermediate alloy is added after standing 5min.
9. method as claimed in claim 4, which is characterized in that in step (4), the Homogenization Treatments are specially in 350- 12-24h is kept the temperature at 370 DEG C.
10. method as claimed in claim 4, which is characterized in that in step (5), the extruding is specially:By extrusion die and It is 350-370 DEG C squeezing temperature after the ingot casting of step (4) processing preheats 1-2h at 350-370 DEG C, extrusion speed 6- 10m·min-1, extrusion ratio 33-55:It is carried out under the conditions of 1.
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114045421A (en) * 2021-11-22 2022-02-15 东北大学 High-strength plastic and high thermal stability Mg-Sn deformed alloy and preparation method thereof
CN114934217A (en) * 2022-05-25 2022-08-23 鹤壁海镁科技有限公司 Microalloy Mg-Sn-Bi-Gd-Zr high-plasticity magnesium alloy and preparation method thereof

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101550510A (en) * 2009-05-08 2009-10-07 重庆大学 High intensity degradable biological medical magnesium alloy and preparation method thereof
CN101698917A (en) * 2009-11-11 2010-04-28 重庆大学 High strength high plasticity magnesium alloy
CN101812620A (en) * 2010-04-30 2010-08-25 重庆大学 magnesium-zinc-zirconium-yttrium-magnesium alloy
CN102383012A (en) * 2011-11-01 2012-03-21 西安理工大学 Low-rare-earth high-strength heat-resisting magnesium alloy and preparation method thereof
CN102449177A (en) * 2009-05-29 2012-05-09 住友电气工业株式会社 Linear bodies, bolts, nuts and washers each comprising a magnesium alloy
JP2012087379A (en) * 2010-10-20 2012-05-10 Sumitomo Electric Ind Ltd Magnesium alloy
CN104060140A (en) * 2014-07-10 2014-09-24 重庆大学 High temperature oxidation resistant magnesium alloy
CN104087801A (en) * 2014-07-10 2014-10-08 重庆大学 Corrosion-resistant magnesium alloy and method for improving corrosion resistance of corrosion-resistant magnesium alloy
CN106247330A (en) * 2016-08-12 2016-12-21 宁波市鄞州姜山盛旺五金厂 A kind of turbulent burner

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101550510A (en) * 2009-05-08 2009-10-07 重庆大学 High intensity degradable biological medical magnesium alloy and preparation method thereof
CN102449177A (en) * 2009-05-29 2012-05-09 住友电气工业株式会社 Linear bodies, bolts, nuts and washers each comprising a magnesium alloy
CN101698917A (en) * 2009-11-11 2010-04-28 重庆大学 High strength high plasticity magnesium alloy
CN101812620A (en) * 2010-04-30 2010-08-25 重庆大学 magnesium-zinc-zirconium-yttrium-magnesium alloy
JP2012087379A (en) * 2010-10-20 2012-05-10 Sumitomo Electric Ind Ltd Magnesium alloy
CN102383012A (en) * 2011-11-01 2012-03-21 西安理工大学 Low-rare-earth high-strength heat-resisting magnesium alloy and preparation method thereof
CN104060140A (en) * 2014-07-10 2014-09-24 重庆大学 High temperature oxidation resistant magnesium alloy
CN104087801A (en) * 2014-07-10 2014-10-08 重庆大学 Corrosion-resistant magnesium alloy and method for improving corrosion resistance of corrosion-resistant magnesium alloy
CN106247330A (en) * 2016-08-12 2016-12-21 宁波市鄞州姜山盛旺五金厂 A kind of turbulent burner

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114045421A (en) * 2021-11-22 2022-02-15 东北大学 High-strength plastic and high thermal stability Mg-Sn deformed alloy and preparation method thereof
CN114934217A (en) * 2022-05-25 2022-08-23 鹤壁海镁科技有限公司 Microalloy Mg-Sn-Bi-Gd-Zr high-plasticity magnesium alloy and preparation method thereof
CN114934217B (en) * 2022-05-25 2023-09-26 鹤壁海镁科技有限公司 Micro-alloy Mg-Sn-Bi-Gd-Zr high-plasticity magnesium alloy and preparation method thereof

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Application publication date: 20181113