CN107964602B - Effective method for improving plastic forming capability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy - Google Patents
Effective method for improving plastic forming capability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy Download PDFInfo
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- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 43
- 238000000034 method Methods 0.000 title claims abstract description 25
- 239000000956 alloy Substances 0.000 claims abstract description 43
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 41
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 16
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 14
- 238000005096 rolling process Methods 0.000 claims abstract description 12
- 229910001093 Zr alloy Inorganic materials 0.000 claims abstract description 10
- 238000003723 Smelting Methods 0.000 claims description 9
- 239000011777 magnesium Substances 0.000 claims description 9
- 229910052726 zirconium Inorganic materials 0.000 claims description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 8
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 6
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 6
- 229910052779 Neodymium Inorganic materials 0.000 claims description 6
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052749 magnesium Inorganic materials 0.000 claims description 6
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 6
- 229910052727 yttrium Inorganic materials 0.000 claims description 6
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 6
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052786 argon Inorganic materials 0.000 claims description 4
- 239000011888 foil Substances 0.000 claims description 4
- 230000003647 oxidation Effects 0.000 claims description 4
- 238000007254 oxidation reaction Methods 0.000 claims description 4
- 238000005266 casting Methods 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 claims description 2
- 238000001125 extrusion Methods 0.000 claims description 2
- 238000005242 forging Methods 0.000 claims description 2
- 238000005336 cracking Methods 0.000 abstract description 5
- 239000000463 material Substances 0.000 abstract description 4
- 230000015572 biosynthetic process Effects 0.000 abstract description 3
- 238000005098 hot rolling Methods 0.000 abstract 1
- 238000002844 melting Methods 0.000 abstract 1
- 230000008018 melting Effects 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 10
- 229910000733 Li alloy Inorganic materials 0.000 description 9
- 239000001989 lithium alloy Substances 0.000 description 9
- 238000000265 homogenisation Methods 0.000 description 7
- 238000012360 testing method Methods 0.000 description 7
- 239000000203 mixture Substances 0.000 description 6
- 238000012545 processing Methods 0.000 description 6
- 238000009864 tensile test Methods 0.000 description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- 238000012512 characterization method Methods 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 229910003460 diamond Inorganic materials 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 230000005496 eutectics Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000013079 quasicrystal Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
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- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- GCICAPWZNUIIDV-UHFFFAOYSA-N lithium magnesium Chemical group [Li].[Mg] GCICAPWZNUIIDV-UHFFFAOYSA-N 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- VSZWPYCFIRKVQL-UHFFFAOYSA-N selanylidenegallium;selenium Chemical compound [Se].[Se]=[Ga].[Se]=[Ga] VSZWPYCFIRKVQL-UHFFFAOYSA-N 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910001256 stainless steel alloy Inorganic materials 0.000 description 1
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- 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
- C22C1/03—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
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- C22C23/00—Alloys based on magnesium
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Abstract
本发明涉及高强度镁合金的塑性提高领域,具体为一种有效利用元素Li改善高强度Mg‑Gd‑Y‑Nd‑Zr镁合金塑性成型能力的方法,解决了高强度塑性极差的问题。在保持合金中所有元素相对含量不变的前提下,通过添加重量百分含量为5~20%的Li元素,使合金中形成具有较强塑性变形能力的β‑Li相,并控制形成β‑Li相的体积分数(20~90%),制备出具有高强度和较好塑性的含锂Mg‑Gd‑Y‑Nd‑Zr合金,经合金熔炼及后续热轧制加工成板材,其加工工艺操作简单、方便。本发明材料在铸态条件下的抗拉强度为σb=120~250MPa,屈服强度为σ0.2=80~150MPa,延伸率为δ=10~30%,密度为1.50~1.89g/cm3,且板材在室温下经40%轧制量的变形后不会出现边裂现象。The invention relates to the field of plastic enhancement of high-strength magnesium alloys, in particular to a method for effectively utilizing element Li to improve the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloys, which solves the problem of extremely poor high-strength plasticity. Under the premise of keeping the relative contents of all elements in the alloy unchanged, by adding 5-20% Li element by weight, a β-Li phase with strong plastic deformation ability is formed in the alloy, and the formation of β-Li phase is controlled. The volume fraction of Li phase (20-90%), a lithium-containing Mg-Gd-Y-Nd-Zr alloy with high strength and good plasticity is prepared, which is processed into a sheet by alloy melting and subsequent hot rolling. Simple and convenient operation. The tensile strength of the material of the present invention under as-cast conditions is σ b =120-250MPa, the yield strength is σ 0.2 =80-150MPa, the elongation is δ=10-30%, and the density is 1.50-1.89g/cm 3 , And the plate will not appear edge cracking after being deformed by 40% of the rolling amount at room temperature.
Description
技术领域technical field
本发明涉及高强度镁合金的塑性提高领域,具体为一种有效利用元素Li改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的方法。The invention relates to the field of plastic enhancement of high-strength magnesium alloys, in particular to a method for effectively utilizing element Li to improve the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloys.
背景技术Background technique
在所有金属结构材料中,镁合金的密度是最低的,分别为铝合金的2/3,不锈钢的1/4。若镁合金材料能够大部分取代不锈钢和铝合金在飞机和车辆上得到应用的话,不仅可以达到解决自身轻量化和提速的目的,而且还能有效地解决节能和环保相关的一系列问题。同时,镁合金还具有比强度和比刚度高、抗高能粒子穿透能力强、电磁屏蔽性能好、阻尼性能好、切削加工性优良等优点,使得镁合金在航空航天和汽车等高新技术领域有着潜在的应用前景。Among all metal structural materials, magnesium alloy has the lowest density, which is 2/3 of aluminum alloy and 1/4 of stainless steel. If magnesium alloy materials can replace most of stainless steel and aluminum alloys in aircraft and vehicles, it can not only achieve the purpose of reducing its own weight and speed, but also effectively solve a series of problems related to energy saving and environmental protection. At the same time, magnesium alloys also have the advantages of high specific strength and specific stiffness, strong resistance to high-energy particle penetration, good electromagnetic shielding performance, good damping performance, and excellent machinability, which make magnesium alloys in aerospace and automotive high-tech fields. potential application prospects.
然而,与传统金属结构材料相比,镁合金的绝对工程强度较低,很难满足工程构件的承载能力要求,严重制约了该合金的应用与进一步的发展。近年来,研究人员发现稀土元素的添加可以显著强化镁合金,可使Mg-Gd-Y-Nd-Zr合金的最大抗拉强度达到400MPa以上,与中等强度铝合金的基本相当。然而,Mg-Gd-Y-Nd-Zr镁合金的塑性极差,其延伸率很难超过5%,致使合金的塑性成型能力非常有限。However, compared with traditional metal structural materials, the absolute engineering strength of magnesium alloys is relatively low, and it is difficult to meet the requirements of the bearing capacity of engineering components, which seriously restricts the application and further development of the alloys. In recent years, researchers have found that the addition of rare earth elements can significantly strengthen magnesium alloys, and the maximum tensile strength of Mg-Gd-Y-Nd-Zr alloys can reach more than 400MPa, which is basically equivalent to that of medium-strength aluminum alloys. However, the ductility of Mg-Gd-Y-Nd-Zr magnesium alloy is extremely poor, and its elongation is difficult to exceed 5%, resulting in very limited plastic forming ability of the alloy.
早期研究表明,元素Li的加入可以促使镁合金中β-Li相的形成,可显著提高合金的塑性成型能力。可以预测,若向高强度Mg-Gd-Y-Nd-Zr镁合金中添加一定重量百分比的Li元素,形成一定体积分数的β-Li相,可有效地改善合金的塑性成型能力,最终将极大的推动并拓宽高强度镁合金的实际工程应用。Early studies have shown that the addition of elemental Li can promote the formation of β-Li phase in magnesium alloys, which can significantly improve the plastic formability of the alloys. It can be predicted that if a certain weight percentage of Li element is added to the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy to form a certain volume fraction of β-Li phase, the plastic forming ability of the alloy can be effectively improved, and the extreme It will greatly promote and broaden the practical engineering application of high-strength magnesium alloys.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,在保持合金中所有元素相对含量不变的前提下,通过添加一定重量百分比的Li元素,使合金中形成具有较强塑性变形能力的β-Li相,并控制形成β-Li相的体积分数,制备出具有高强度和较好塑性的含锂Mg-Gd-Y-Nd-Zr合金,解决高强镁合金塑性成型能力差等问题。The purpose of the present invention is to provide an effective method for improving the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloys. element, to form a β-Li phase with strong plastic deformation ability in the alloy, and to control the volume fraction of the formed β-Li phase to prepare a lithium-containing Mg-Gd-Y-Nd-Zr with high strength and good plasticity Alloy, to solve the problem of poor plastic forming ability of high-strength magnesium alloy.
本发明的技术方案是:The technical scheme of the present invention is:
一种改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,合金中锂含量为5~20%,所形成β-Li相的体积分数为20~90%。An effective method for improving the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, the lithium content in the alloy is 5-20%, and the volume fraction of the formed β-Li phase is 20-90%.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,按重量百分比计,钆含量为5~10%;钇含量为3~8%;钕含量为0.5~2%;锆含量为0.3~1.0%;锂含量为5~20%;镁余量。In the effective method for improving the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, the gadolinium content is 5-10%; the yttrium content is 3-8%; the neodymium content is 0.5-10% by weight. 2%; Zirconium content is 0.3-1.0%; Lithium content is 5-20%; Magnesium balance.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,合金在铸态条件下的抗拉强度为σb=120~250MPa;屈服强度为σ0.2=80~150MPa;延伸率为δ=10~30%;合金的密度为1.50~1.89g/cm3。In the effective method for improving the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, the tensile strength of the alloy under the as-cast condition is σ b =120~250MPa; the yield strength is σ 0.2 =80~ 150MPa; elongation δ=10~30%; density of alloy is 1.50~1.89g/cm 3 .
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,合金板材在40%轧制量的变形后不会出现边裂现象。According to the effective method for improving the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, the alloy plate does not appear edge cracks after being deformed by 40% of the rolling amount.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,将Mg-Gd-Y-Nd-Zr合金和纯锂锭在真空冶炼炉中熔化、且在有氩气保护的条件下进行,于740~780℃温度下保温3~5小时后,在炉内进行浇铸成型获得铸锭。The described effective method for improving the plastic formability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloys is to melt Mg-Gd-Y-Nd-Zr alloys and pure lithium ingots in a vacuum smelting furnace, and place them in an argon smelting furnace. It is carried out under the condition of gas shielding, and after being kept at a temperature of 740 to 780° C. for 3 to 5 hours, it is cast and formed in a furnace to obtain an ingot.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,将铸锭在300~400℃温度条件下进行6~10小时的均匀化处理,并用铝箔严密包裹,以防止合金的因高温氧化而可能出现的燃烧。The effective method for improving the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy is that the ingot is subjected to a homogenization treatment at a temperature of 300-400 DEG C for 6-10 hours, and is tightly wrapped with aluminum foil, In order to prevent the possible combustion of the alloy due to high temperature oxidation.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,在室温至350℃温度条件下,将均匀化处理后的铸锭进行塑性加工处理。The effective method for improving the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy is to perform plastic processing on the homogenized ingot at a temperature ranging from room temperature to 350°C.
所述的改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法,塑性加工处理为不同变形比的挤压、轧制或锻造。In the effective method for improving the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, the plastic processing is extrusion, rolling or forging with different deformation ratios.
本发明的设计思想是:The design idea of the present invention is:
本发明通过合理向高强度Mg-Gd-Y-Nd-Zr镁合金中添加一定重量百分比的Li元素(优选为8~12%),在保持合金中其它元素相对含量不变的前提下(按重量百分比计,钆(Gd)含量为5~10%;钇(Y)含量为3~8%;钕(Nd)含量为0.5~2%;锆(Zr)含量为0.3~1.0%;含量为5~20%;镁余量),使合金中形成一定体积分数的β-Li相(β-Li相的体积分数优选为60~90%)。经均匀化处理后,使合金中粗大共晶组织得以固溶,这样的作用在于:消除凝固过程中形成大尺寸共晶组织造成的应力集中,极大的发挥出β-Li相具有的塑性变形协调能力,有效避免了塑性加工变形过程中板材的边裂现象,最终显著提高了合金的塑性成型能力。In the present invention, a certain weight percentage of Li element (preferably 8-12%) is added to the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy reasonably, and the relative content of other elements in the alloy is kept unchanged (according to By weight percentage, the content of gadolinium (Gd) is 5-10%; the content of yttrium (Y) is 3-8%; the content of neodymium (Nd) is 0.5-2%; the content of zirconium (Zr) is 0.3-1.0%; The content is 5-20%; magnesium balance), so that a certain volume fraction of β-Li phase is formed in the alloy (the volume fraction of β-Li phase is preferably 60-90%). After the homogenization treatment, the coarse eutectic structure in the alloy can be solid-dissolved. This effect is to eliminate the stress concentration caused by the formation of large-size eutectic structure during the solidification process, and greatly exert the plastic deformation of the β-Li phase. The coordination ability effectively avoids the edge cracking of the plate during the plastic deformation process, and finally significantly improves the plastic forming ability of the alloy.
本发明的优点及有益效果是:The advantages and beneficial effects of the present invention are:
1、本发明采用该方法可以充分利用元素Li对镁合金塑性变形协调能力的提高,显著改善了镁合金塑性加工成型能力,有效推动了镁合金的实际工程应用。1. By adopting this method in the present invention, the enhancement of the plastic deformation coordination ability of the magnesium alloy by the element Li can be fully utilized, the plastic processing and forming ability of the magnesium alloy is significantly improved, and the practical engineering application of the magnesium alloy is effectively promoted.
2、本发明采用该方法获得了具有低密度、高强度、塑性成型能力强的镁合金材料,特别适合于轻质、高强、高韧的用材需求。2. The present invention adopts this method to obtain a magnesium alloy material with low density, high strength and strong plastic forming ability, which is especially suitable for the material requirements of light weight, high strength and high toughness.
3、本发明所用的设备简单,成本较低,加工工艺操作简单、方便。3. The equipment used in the present invention is simple, the cost is low, and the operation of the processing technology is simple and convenient.
附图说明Description of drawings
图1含与不含Li的高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr镁合金(比较例1和实施例1)的XRD相分析结果。图中,横坐标2θ为衍射角(degree),纵坐标Intensity为强度(a.u.)Figure 1 XRD phase analysis results of high strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr magnesium alloys (Comparative Example 1 and Example 1) with and without Li. In the figure, the abscissa 2θ is the diffraction angle (degree), and the ordinate Intensity is the intensity (a.u.)
图2含与不含Li的高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr镁合金(比较例1和实施例1)的微观组织照片。其中,Figure 2 Microstructure photographs of high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr magnesium alloys with and without Li (Comparative Example 1 and Example 1). in,
(a)比较例1合金Mg-7%Gd-5%Y-1%Nd-0.5%Zr;(b)实施例1合金Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li。(a) Comparative Example 1 alloy Mg-7%Gd-5%Y-1%Nd-0.5%Zr; (b) Example 1 alloy Mg-7%Gd-5%Y-1%Nd-0.5%Zr- 10% Li.
图3(a)-图3(b)含与不含Li的高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr镁合金(比较例1和实施例1)的塑性变形能力对比。其中,图3(a)比较例1轧制量为12%的Mg-7%Gd-5%Y-1%Nd-0.5%Zr合金板材侧面,边裂现象严重;图3(b)实施例1轧制量为40%的Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li合金板材侧面,无边裂现象。Fig. 3(a)-Fig. 3(b) Plastic deformation of high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr magnesium alloys with and without Li (Comparative Example 1 and Example 1) Ability comparison. Among them, Fig. 3(a) Comparative Example 1 Mg-7%Gd-5%Y-1%Nd-0.5%Zr alloy plate with a rolling amount of 12% has serious edge cracks on the side surface; Fig.3(b) Example 1 The side surface of the Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li alloy plate with a rolling amount of 40% has no edge cracking phenomenon.
具体实施方式Detailed ways
下面结合具体实施例对本发明做进一步说明,需要说明的是给出的实施例是用于说明本发明,而不是对本发明的限制,本发明的保护范围并不限于以下实施的具体实施例。The present invention will be further described below in conjunction with specific embodiments. It should be noted that the given embodiments are used to illustrate the present invention, rather than limit the present invention, and the protection scope of the present invention is not limited to the specific embodiments implemented below.
比较例1Comparative Example 1
本实施例中,改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法如下:In this embodiment, the effective method to improve the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy is as follows:
Ⅰ)、采用的镁锂合金成分Ⅰ), the composition of magnesium-lithium alloy used
使用高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr合金,其化学成分(重量百分含量)为:钆含量为7%;钇含量为5%;钕含量为1%;锆含量为0.5%;镁余量。Using high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr alloy, its chemical composition (weight percentage) is: gadolinium content is 7%; yttrium content is 5%; neodymium content is 1% ; Zirconium content is 0.5%; Magnesium balance.
Ⅱ)、合金冶炼Ⅱ), alloy smelting
在真空冶炼炉中氩气保护条件下进行合金冶炼,770℃温度下保温4小时后,在炉内进行浇铸成型。Alloy smelting is carried out in a vacuum smelting furnace under the protection of argon gas, and after holding for 4 hours at a temperature of 770 ° C, casting is carried out in the furnace.
Ⅲ)、均匀化处理Ⅲ), homogenization treatment
对高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr合金在400℃保温8小时,并用铝箔严密包裹,以防止合金的因高温氧化而可能出现的燃烧。The high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr alloy was kept at 400°C for 8 hours and tightly wrapped with aluminum foil to prevent the alloy from burning due to high temperature oxidation.
Ⅳ)、塑性加工变形Ⅳ), plastic deformation
在室温条件下,对均匀化后合金进行轧制成型,轧下量为12%。Under the condition of room temperature, the alloy after homogenization is rolled and formed, and the rolling reduction is 12%.
Ⅴ)、微观组织表征Ⅴ), microstructure characterization
组织观察的样品其制备过程如下:采用1000号碳化硅水磨砂纸磨平表面,然后采用油基金刚石研磨膏机械抛光。XRD结果表明,比较例1样品中主要含有α-Mg和Mg5Gd相,相应照片见附图1。光学观察结果表明,比较例1样品中不存在β-Li相,相应照片见附图2(a)。The preparation process of the sample for tissue observation is as follows: the surface is smoothed with No. 1000 silicon carbide water abrasive paper, and then mechanically polished with oil-based diamond abrasive paste. The XRD results show that the sample of Comparative Example 1 mainly contains α-Mg and Mg5Gd phases, and the corresponding photos are shown in Figure 1. The optical observation results show that there is no β-Li phase in the sample of Comparative Example 1, and the corresponding photo is shown in Figure 2(a).
Ⅵ)、力学性能测试Ⅵ), mechanical properties test
合金的室温拉伸性能样品为板状,试样标准长度为25mm,宽度为5mm,厚度为4mm。拉伸试验的应变速率为1×10-3s-1,拉伸试验在MTS(858.01M)拉扭试验机上进行,确定出合金相应的拉伸性能,其屈服和抗拉强度分别为148MPa和220MPa,延伸率为1%,列于表1。The room temperature tensile properties of the alloy samples are plate-shaped, with a standard length of 25 mm, a width of 5 mm, and a thickness of 4 mm. The strain rate of the tensile test was 1×10 -3 s -1 , and the tensile test was carried out on an MTS (858.01M) tensile-torsion testing machine. The corresponding tensile properties of the alloy were determined. The yield and tensile strength were 148MPa and 148MPa, respectively. 220MPa,
Ⅶ)、塑性加工成型能力Ⅶ), plastic forming ability
轧制量为12%时,高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr合金板材侧面出现严重的边裂现象,见图3(a)。When the rolling amount is 12%, serious edge cracks appear on the side of the high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr alloy sheet, as shown in Figure 3(a).
实施例1Example 1
本实施例中,改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法如下:In this embodiment, the effective method to improve the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy is as follows:
Ⅰ)、采用的含锂Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li合金成分Ⅰ), the used lithium-containing Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li alloy composition
使用含锂的高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li合金,其化学成分(重量百分含量)为:钆含量为7%;钇含量为5%;钕含量为1%;锆含量为0.5%;锂含量为10%;镁余量。Using lithium-containing high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li alloy, its chemical composition (weight percentage) is: gadolinium content is 7%; yttrium content is 5% %; Neodymium content is 1%; Zirconium content is 0.5%; Lithium content is 10%; Magnesium balance.
Ⅱ)、合金冶炼Ⅱ), alloy smelting
将Mg-Gd-Y-Nd-Zr合金和纯锂锭在真空冶炼炉中熔化、且在有氩气保护的条件下进行合金冶炼,770℃温度下保温4小时后,在炉内进行浇铸成型。The Mg-Gd-Y-Nd-Zr alloy and pure lithium ingot were melted in a vacuum smelting furnace, and the alloy was smelted under the protection of argon. .
Ⅲ)、均匀化处理Ⅲ), homogenization treatment
对高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li合金在400℃保温8小时,并用铝箔严密包裹,以防止合金的因高温氧化而可能出现的燃烧。The high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li alloy was kept at 400℃ for 8 hours and tightly wrapped with aluminum foil to prevent the alloy from burning due to high temperature oxidation.
Ⅳ)、塑性加工变形Ⅳ), plastic deformation
在室温条件下,对均匀化后合金进行轧制成型,轧下量为40%。Under the condition of room temperature, the alloy after homogenization is rolled and formed, and the rolling reduction is 40%.
Ⅴ)、微观组织表征Ⅴ), microstructure characterization
组织观察的样品其制备过程如下:采用1000号碳化硅水磨砂纸磨平表面,然后采用油基金刚石研磨膏机械抛光。XRD结果表明,实施例1样品中主要含有β-Li、α-Mg和Mg5Gd相,相应照片见附图1。光学观察结果表明,实施例1样品中形成的准晶相体积分数为75%,相应照片见附图2(b)。The preparation process of the sample for tissue observation is as follows: the surface is smoothed with No. 1000 silicon carbide water abrasive paper, and then mechanically polished with oil-based diamond abrasive paste. The XRD results show that the sample of Example 1 mainly contains β-Li, α-Mg and Mg5Gd phases, and the corresponding photos are shown in Figure 1. The optical observation results show that the volume fraction of the quasicrystal phase formed in the sample of Example 1 is 75%, and the corresponding photo is shown in Figure 2(b).
Ⅵ)、力学性能测试Ⅵ), mechanical properties test
拉伸试样加工和拉伸性能测试方法如下:合金的室温拉伸性能样品为板状,试样标准长度为25mm,宽度为5mm,厚度为4mm。拉伸试验的应变速率为1×10-3s-1,拉伸试验在MTS(858.01M)拉扭试验机上进行,确定出合金相应的拉伸性能。测得实施例1合金样品的屈服和抗拉强度分别为105MPa和195MPa,延伸率为24%,列于表1。The tensile specimen processing and tensile properties testing methods are as follows: the room temperature tensile properties of the alloy samples are plate-shaped, and the standard length of the specimen is 25 mm, the width is 5 mm, and the thickness is 4 mm. The strain rate of the tensile test was 1×10 -3 s -1 , and the tensile test was carried out on an MTS (858.01M) tensile-torsion testing machine to determine the corresponding tensile properties of the alloy. The yield and tensile strengths of the alloy samples of Example 1 were measured to be 105 MPa and 195 MPa, respectively, and the elongation was 24%, which are listed in Table 1.
Ⅶ)、塑性加工成型能力Ⅶ), plastic forming ability
轧制量为40%时,高强度Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li合金板材侧面无边裂现象,见图3(b)。When the rolling amount is 40%, the high-strength Mg-7%Gd-5%Y-1%Nd-0.5%Zr-10%Li alloy sheet has no side cracking phenomenon, as shown in Figure 3(b).
实施例2Example 2
本实施例中,改善高强度Mg-Gd-Y-Nd-Zr镁合金塑性成型能力的有效方法如下:In this embodiment, the effective method to improve the plastic forming ability of high-strength Mg-Gd-Y-Nd-Zr magnesium alloy is as follows:
Ⅰ)、采用的含锂Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li合金成分Ⅰ), the used lithium-containing Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li alloy composition
使用含锂的高强度Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li合金,其化学成分(重量百分含量)为:钆含量为9%;钇含量为6%;钕含量为1.5%;锆含量为0.5%;锂含量为10%;镁余量。Using lithium-containing high-strength Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li alloy, its chemical composition (weight percentage) is: gadolinium content is 9%; yttrium content is 6% %; Neodymium content is 1.5%; Zirconium content is 0.5%; Lithium content is 10%; Magnesium balance.
Ⅱ)、合金冶炼Ⅱ), alloy smelting
与实施例1相同。Same as Example 1.
Ⅲ)、均匀化处理Ⅲ), homogenization treatment
与实施例1相同。Same as Example 1.
Ⅳ)、塑性加工变形Ⅳ), plastic deformation
与实施例1相同。Same as Example 1.
Ⅴ)、微观组织表征Ⅴ), microstructure characterization
组织观察方法,与实施例1相同。XRD结果表明,实施例2样品中主要含有β-Li、α-Mg和Mg5Gd相。光学观察结果表明,实施例2样品中形成的准晶相体积分数为75%。The tissue observation method is the same as that of Example 1. XRD results show that the sample in Example 2 mainly contains β-Li, α-Mg and Mg5Gd phases. The optical observation results show that the volume fraction of the quasicrystal phase formed in the sample of Example 2 is 75%.
Ⅵ)、力学性能测试Ⅵ), mechanical properties test
拉伸试样加工和拉伸性能测试方法,与实施例1相同。测得实施例2合金样品的屈服和抗拉强度分别为135MPa和233MPa,延伸率为21%,列于表1。Tensile specimen processing and tensile properties testing methods are the same as in Example 1. The yield and tensile strengths of the alloy samples of Example 2 were measured to be 135 MPa and 233 MPa, respectively, and the elongation was 21%, which are listed in Table 1.
Ⅶ)、塑性加工成型能力Ⅶ), plastic forming ability
轧制量为40%时,高强度Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li合金板材侧面无边裂现象。When the rolling amount is 40%, the high-strength Mg-9%Gd-6%Y-1.5%Nd-0.5%Zr-10%Li alloy sheet has no side cracking phenomenon.
本发明中,含与不含Li元素的高强度Mg-Gd-Y-Nd-Zr合金(比较例1、实施例1和实施例2)的力学性能数据,见表1。In the present invention, the mechanical property data of the high-strength Mg-Gd-Y-Nd-Zr alloys (Comparative Example 1, Example 1 and Example 2) with and without Li element are shown in Table 1.
表1Table 1
实施例结果表明,采用本发明能够有效利用元素Li显著改善了高强度Mg-Gd-Y-Nd-Zr镁合金的塑性成型能力,解决了镁合金塑性差的问题,同时还使合金保留着较高的工程强度,拓宽了该类高强度镁合金的实际工程应用。The results of the examples show that the use of the present invention can effectively utilize the element Li, which can significantly improve the plastic forming ability of the high-strength Mg-Gd-Y-Nd-Zr magnesium alloy, solve the problem of poor plasticity of the magnesium alloy, and at the same time, the alloy retains relatively high plasticity. The high engineering strength broadens the practical engineering application of such high-strength magnesium alloys.
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