CN116099892A - A Method for Strengthening Magnesium-Zinc Alloy by Reciprocating Equal Channel Angular Extrusion - Google Patents
A Method for Strengthening Magnesium-Zinc Alloy by Reciprocating Equal Channel Angular Extrusion Download PDFInfo
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Abstract
Description
技术领域technical field
本发明涉及合金技术领域,特别涉及一种往复等通道角挤压强化镁锌合金的方法。The invention relates to the technical field of alloys, in particular to a method for strengthening magnesium-zinc alloys by reciprocating equal channel angular extrusion.
背景技术Background technique
镁合金作为最轻的金属结构材料,具有质量轻、导热导电性好、阻尼减震、电磁屏蔽等优异性能,在交通、通讯、电器和航空航天等领域有广阔的应用前景。Mg作为人体中的常量元素之一,在体内环境中可以被体液逐渐腐蚀降解,并最终被吸收代谢,因而具有非常优良的生物安全性基础。镁及镁合金具有良好的生物相容性、骨诱导性、抗菌性以及抗肿瘤功能,近十年间已逐渐成为新一代医用可降解植入材料的主流研究方向,展现出广阔的应用前景。然而镁合金在应用过程中仍然存在着强度不高、塑性较差、降解较快的问题。考虑到其生物功能性和生物安全性容易受到合金成分的影响,晶粒细化被认为是目前提高镁合金力学性能最佳的方法之一,其在不改变材料原始成分的基础上可以有效提高塑性变形过程中晶界的协调变形能力,从而提高材料的塑性和韧性。As the lightest metal structural material, magnesium alloy has excellent properties such as light weight, good thermal and electrical conductivity, damping and shock absorption, and electromagnetic shielding. It has broad application prospects in the fields of transportation, communication, electrical appliances, and aerospace. As one of the constant elements in the human body, Mg can be gradually corroded and degraded by body fluids in the internal environment, and finally absorbed and metabolized, so it has a very good basis for biological safety. Magnesium and magnesium alloys have good biocompatibility, osteoinductivity, antibacterial and antitumor functions, and have gradually become the mainstream research direction of a new generation of medical degradable implant materials in the past decade, showing broad application prospects. However, magnesium alloys still have the problems of low strength, poor plasticity and rapid degradation in the application process. Considering that its biological functionality and biological safety are easily affected by the alloy composition, grain refinement is considered to be one of the best methods to improve the mechanical properties of magnesium alloys, which can effectively improve the mechanical properties of magnesium alloys without changing the original composition of the material. The coordinated deformation ability of grain boundaries during plastic deformation, thereby improving the plasticity and toughness of materials.
传统的镁合金晶粒细化方法为严重塑性变形(Severe Plastic Deformation,SPD),其中包括等通道转角挤压(ECAP)、高压扭转应变(HighPressure and Torsion,HPT)和叠层轧合技术(Accumulative Roll Bonding,ARB)等,其中ECAP由于工艺实施简单,可以制备出组织均匀致密的超细晶材料而受到广泛的关注。ECAP的目的是通过塑性变形使得镁合金内部的位错密度增加,诱发再结晶,进而细化晶粒。然而,镁的晶体结构为密排六方结构(hcp),室温下独立滑移系单一,难以积累高位错密度或在三维空间形成大角度晶界诱发纳米晶,且在挤压变形的过程中容易发生开裂。因此,利用传统的严重塑性变形方法很难获得超细晶组织。The traditional methods for grain refinement of magnesium alloys are severe plastic deformation (Severe Plastic Deformation, SPD), including equal channel angular pressing (ECAP), high pressure torsional strain (High Pressure and Torsion, HPT) and laminated rolling technology (Accumulative Roll Bonding, ARB), etc., among which ECAP has received extensive attention because of its simple process implementation and the ability to prepare ultra-fine-grained materials with uniform and dense structures. The purpose of ECAP is to increase the dislocation density inside the magnesium alloy through plastic deformation, induce recrystallization, and then refine the grains. However, the crystal structure of magnesium is a hexagonal close-packed structure (hcp), and the independent slip system is single at room temperature. It is difficult to accumulate high dislocation density or form large-angle grain boundaries in three-dimensional space to induce nanocrystals, and it is easy to Cracking occurs. Therefore, it is difficult to obtain ultra-fine-grained microstructures by traditional severe plastic deformation methods.
发明内容Contents of the invention
有鉴于此,本发明目的在于提供一种往复等通道角挤压强化镁锌合金的方法,本发明强化得到的镁锌合金具有超细晶结构,具有良好的综合力学性能。In view of this, the purpose of the present invention is to provide a method for strengthening magnesium-zinc alloy by reciprocating equal channel angular extrusion. The magnesium-zinc alloy strengthened by the present invention has an ultra-fine grain structure and good comprehensive mechanical properties.
为了实现上述发明目的,本发明提供以下技术方案:In order to achieve the above-mentioned purpose of the invention, the present invention provides the following technical solutions:
本发明提供了一种往复等通道角挤压强化镁锌合金的方法,包括以下步骤:The invention provides a method for strengthening magnesium-zinc alloy by reciprocating equal-channel angular extrusion, comprising the following steps:
将镁锌合金置于等通道角挤压模具中,进行往复等通道角挤压,得到强化镁锌合金;The magnesium-zinc alloy is placed in an equal-channel angular extrusion die, and the reciprocating equal-channel angular extrusion is performed to obtain a strengthened magnesium-zinc alloy;
所述镁锌合金的初始温度为300~450℃;The initial temperature of the magnesium-zinc alloy is 300-450°C;
所述等通道角挤压模具的内转角为90°,外弧度为0~45°;The inner turning angle of the equal channel angular extrusion die is 90°, and the outer radian is 0-45°;
所述往复等通道角挤压的挤压道次为10~20道次。The extrusion pass of the reciprocating equal channel angular extrusion is 10-20 passes.
优选的,所述镁锌合金中的锌含量为0~4wt%。Preferably, the zinc content in the magnesium-zinc alloy is 0-4wt%.
优选的,第1道次等通道角挤压时,所述镁锌合金的温度为300~450℃;后续道次等通道角挤压时,不再对镁锌合金进行加热。Preferably, during the first pass of equal channel angular extrusion, the temperature of the magnesium-zinc alloy is 300-450° C.; during subsequent passes of equal channel angular extrusion, the magnesium-zinc alloy is no longer heated.
优选的,所述往复等通道角挤压的挤压速率为5~20mm/s。Preferably, the extrusion rate of the reciprocating equal channel angular extrusion is 5-20 mm/s.
优选的,所述往复等通道角挤压的每道次变形的应变量为1.15~28.60。Preferably, the amount of strain per pass of the reciprocating equal channel angular extrusion is 1.15 to 28.60.
优选的,所述等通道角挤压模具包括第一端口和第二端口,当进行奇数道次等通道角挤压时,所述镁锌合金自第一端口挤压至第二端口;当进行偶数道次等通道角挤压时,所述镁锌合金自第二端口挤压至第一端口。Preferably, the equal-channel angular extrusion die includes a first port and a second port, and when an odd-numbered equal-channel angular extrusion is performed, the magnesium-zinc alloy is extruded from the first port to the second port; During even-numbered equal-channel angular extrusion, the magnesium-zinc alloy is extruded from the second port to the first port.
本发明提供了一种往复等通道角挤压强化镁锌合金的方法,包括以下步骤:将镁锌合金置于等通道角挤压模具中,进行往复等通道角挤压,得到强化镁锌合金;所述镁锌合金的初始温度为300~450℃;所述等通道角挤压模具的内转角为90°,外弧度为0~45°;所述往复等通道角挤压的挤压道次为10~20道次。本发明采用往复等通道角挤压(EqualChannel Angular Pressing,ECAP)方法,利用往复ECAP过程中的高温应变激活锥面<c+a>位错滑移,获得较强的变形能力,同时诱发动态再结晶,从而避免ECAP过程材料的裂纹产生,可实现多道次加工得到更细小均匀的微观组织以及较高的强度和塑性。相较于镁合金在传统ECAP工艺下容易开裂的现象,本发明方法下镁锌合金即使在经过10~20道次挤压后也不易发生开裂。同时,在高温应变过程中,析出相在晶界处发生均匀动态偏聚,抑制晶界的迁移,使得再结晶晶粒均匀细化。本发明通过控制等通道角挤压模具的角度和挤压道次,能够使镁锌合金具备更细小的晶粒和更稳定的晶界,使得镁锌合金的强度和塑性同步提高,因此具备更好的综合力学性能。The invention provides a method for strengthening magnesium-zinc alloy by reciprocating equal-channel angular extrusion, comprising the following steps: placing the magnesium-zinc alloy in an equal-channel angular extrusion die, and performing reciprocating equal-channel angular extrusion to obtain a strengthened magnesium-zinc alloy The initial temperature of the magnesium-zinc alloy is 300-450°C; the inner rotation angle of the equal-channel angular extrusion die is 90°, and the outer radian is 0-45°; the extrusion path of the reciprocating equal-channel angular extrusion The times are 10-20 times. The invention adopts reciprocating Equal Channel Angular Pressing (EqualChannel Angular Pressing, ECAP) method, utilizes the high temperature strain in the process of reciprocating ECAP to activate the <c+a> dislocation slip of the conical surface, obtains strong deformation ability, and induces dynamic regeneration at the same time. Crystallization, so as to avoid the cracks of the ECAP process material, can achieve multi-pass processing to obtain a finer and more uniform microstructure as well as higher strength and plasticity. Compared with the phenomenon that the magnesium alloy is easy to crack under the traditional ECAP process, the magnesium-zinc alloy under the method of the present invention is not easy to crack even after 10-20 passes of extrusion. At the same time, during the high-temperature strain process, the precipitated phases segregate uniformly and dynamically at the grain boundaries, which inhibits the migration of the grain boundaries and makes the recrystallized grains uniformly refined. The invention can make the magnesium-zinc alloy have finer crystal grains and more stable grain boundaries by controlling the angle and extrusion passes of the equal-channel angular extrusion die, so that the strength and plasticity of the magnesium-zinc alloy can be simultaneously improved, so it has more Good comprehensive mechanical properties.
实施例结果表明,采用本发明方法强化后的镁锌合金晶粒细小均匀,平均晶粒尺寸小于1μm,其抗拉强度强度>250MPa,延伸率>15%。The results of the examples show that the magnesium-zinc alloy strengthened by the method of the present invention has fine and uniform grains, the average grain size is less than 1 μm, the tensile strength is >250 MPa, and the elongation is >15%.
同时,本发明提供的强化方法操作简便,样品在单道次挤压后不需要取出和旋转,中间道次挤压变形过程中不需要进行加热处理,因而加工效率更高,成本更低,更适应于工业化生产。At the same time, the strengthening method provided by the invention is easy to operate, the sample does not need to be taken out and rotated after a single extrusion pass, and no heat treatment is required during the extrusion deformation process of the intermediate pass, so the processing efficiency is higher, the cost is lower, and the Adapt to industrial production.
附图说明Description of drawings
图1为往复等通道角挤压的挤压过程;Fig. 1 is the extrusion process of reciprocating equal channel angular extrusion;
图2为实施例1~3和对比例1~4所得强化镁锌合金的金相结果;Fig. 2 is the metallographic result of embodiment 1~3 and comparative example 1~4 gained strengthened magnesium-zinc alloy;
图3为实施例1~3和对比例1~4所得强化镁锌合金拉伸试验应力-应变曲线。Fig. 3 is the tensile test stress-strain curve of the strengthened magnesium-zinc alloy obtained in Examples 1-3 and Comparative Examples 1-4.
具体实施方式Detailed ways
本发明提供了一种往复等通道角挤压强化镁锌合金的方法,包括以下步骤:The invention provides a method for strengthening magnesium-zinc alloy by reciprocating equal-channel angular extrusion, comprising the following steps:
将镁锌合金置于等通道角挤压模具中,进行往复等通道角挤压,得到强化镁锌合金。The magnesium-zinc alloy is placed in an equal-channel angular extrusion die for reciprocating equal-channel angular extrusion to obtain a strengthened magnesium-zinc alloy.
在本发明中,所述镁锌合金中的锌含量优选为0~4wt%,更优选为0.1~3.5wt%,更优选为0.5~3wt%,进一步优选为1~2.5wt%。本发明对所述镁锌合金材料初始结构不做要求,采用铸态、挤压态均可。In the present invention, the zinc content in the magnesium-zinc alloy is preferably 0-4wt%, more preferably 0.1-3.5wt%, more preferably 0.5-3wt%, even more preferably 1-2.5wt%. The present invention does not require the initial structure of the magnesium-zinc alloy material, and it can be in a cast state or an extruded state.
本发明对所述镁锌合金的尺寸没有特殊的要求,与所述等通道角挤压模具尺寸匹配即可。The present invention has no special requirements on the size of the magnesium-zinc alloy, and only needs to match the size of the equal channel angular extrusion die.
在本发明中,所述等通道角挤压模具由压头以及两个截面完全相同,轴线以一定角度相交且完全连接的通道组成,两通道的内转角为φ,外接弧度为ψ。In the present invention, the equal-channel angular extrusion die is composed of an indenter and two completely connected channels with identical cross-sections and intersecting axes at a certain angle. The inner turning angle of the two channels is φ, and the circumscribed arc is ψ.
在本发明中,所述等通道角挤压模具的内转角φ为90°,外弧度ψ为0~45°,优选为0~30°,进一步优选为0~15°。In the present invention, the inner rotation angle φ of the equal channel angular extrusion die is 90°, and the outer radian ψ is 0-45°, preferably 0-30°, more preferably 0-15°.
在本发明中,所述镁锌合金的初始温度优选为300~450℃,更优选为350~400℃;所述等通道角挤压模具的初始温度优选为300~450℃,更优选为350~400℃。在本发明中,第1道次等通道角挤压时,所述镁锌合金的温度为300~450℃;后续道次等通道角挤压时,不再对镁锌合金和等通道角挤压模具进行加热。In the present invention, the initial temperature of the magnesium-zinc alloy is preferably 300-450°C, more preferably 350-400°C; the initial temperature of the equal channel angular extrusion die is preferably 300-450°C, more preferably 350°C ~400°C. In the present invention, during the first pass of equal channel angular extrusion, the temperature of the magnesium-zinc alloy is 300-450°C; The die is heated.
在本发明中,所述往复等通道角挤压的挤压道次为10~20道次,优选为10~12道次。In the present invention, the extrusion passes of the reciprocating equal channel angular extrusion are 10-20 passes, preferably 10-12 passes.
在本发明中,所述往复等通道角挤压的挤压速率优选为5~20mm/s,更优选为10~15mm/s。In the present invention, the extrusion rate of the reciprocating equal channel angular extrusion is preferably 5-20 mm/s, more preferably 10-15 mm/s.
在本发明中,所述往复等通道角挤压的每道次变形的应变量优选为1.15~28.60。在本发明中,所述每道次变形的应变量优选根据Iwahashi理论公式:ε=(1/√3)[2cot(φ/2+ψ/2)+ψcosec(φ/2+ψ/2)]计算得到,其中,ε表示每道次变形的应变量,φ表示等通道角挤压模具的内转角,ψ表示等通道角挤压模具的外弧度。In the present invention, the amount of strain per pass of the reciprocating equal channel angular pressing is preferably 1.15-28.60 . In the present invention, the strain amount of each pass deformation is preferably according to the Iwahashi theoretical formula: ε=(1/√3)[2cot(φ/2+ψ/2)+ψcosec(φ/2+ψ/2) ] calculated, where ε represents the strain amount of each pass deformation, φ represents the inner rotation angle of the ECA die, and ψ represents the outer radian of the ECA die.
在本发明中,所述等通道角挤压模具包括第一端口和第二端口,当进行奇数道次等通道角挤压时,所述镁锌合金自第一端口挤压至第二端口;当进行偶数道次等通道角挤压时,所述镁锌合金自第二端口挤压至第一端口。在本发明中,镁锌合金在不同道次间沿着模具内部路径做往复挤压,挤压过程中不需要取出样品。在本发明中,所述往复等通道角挤压的挤压过程如图1所示。In the present invention, the equal channel angular extrusion die includes a first port and a second port, and when an odd number of times of equal channel angular extrusion is performed, the magnesium-zinc alloy is extruded from the first port to the second port; When equal-channel angular extrusion is performed with even passes, the magnesium-zinc alloy is extruded from the second port to the first port. In the present invention, the magnesium-zinc alloy is reciprocally extruded along the inner path of the mold between different passes, and samples do not need to be taken out during the extrusion process. In the present invention, the extrusion process of the reciprocating equal channel angular extrusion is shown in FIG. 1 .
本发明通过往复等通道角挤压工艺制备的镁锌合金,在多道次变形后具备了均匀的超细晶组织,因而具有较好的综合力学性能,解决了镁合金在医用领域应用中存在的强度低、塑性差的问题。本发明采用的方法步骤相对简单,在挤压变形过程中不采用加热手段,成本较低。而单道次间将材料沿模具进行往复挤压,样品不需要取出,提高了工艺效率,适用于工业化生产,具有独特的技术创新。本发明进行的多道次挤压变形过程中,合金始终具有较好的塑性和流动性,并未发生开裂,促进其晶粒进一步均匀细化。综上所述,本发明解决了镁合金在等通道角挤压过程中存在的无法兼容晶粒度、强度、塑性和开裂的问题,实现了利用多道次往复挤压制备组织均匀的超细晶镁锌合金,并提高了其强度和塑性,使其具有较高的综合性能。The magnesium-zinc alloy prepared by the reciprocating equal-channel angular extrusion process in the present invention has a uniform ultra-fine grain structure after multi-pass deformation, so it has better comprehensive mechanical properties and solves the problem of magnesium alloys in the medical field. The problem of low strength and poor plasticity. The steps of the method adopted by the invention are relatively simple, no heating means is used in the extrusion deformation process, and the cost is low. In a single pass, the material is reciprocally extruded along the mold, and the sample does not need to be taken out, which improves the process efficiency, is suitable for industrial production, and has unique technological innovations. During the multi-pass extrusion deformation process carried out by the invention, the alloy always has good plasticity and fluidity without cracking, which promotes the further uniform refinement of its crystal grains. In summary, the present invention solves the problems of incompatible grain size, strength, plasticity and cracking of magnesium alloys in the process of equal channel angular extrusion, and realizes the preparation of ultrafine Crystal magnesium zinc alloy, and improve its strength and plasticity, so that it has high comprehensive performance.
实施例结果表明,采用本发明方法强化后的镁锌合金晶粒细小均匀,平均晶粒尺寸小于1μm,其抗拉强度强度>250MPa,延伸率>15%。The results of the examples show that the magnesium-zinc alloy strengthened by the method of the present invention has fine and uniform grains, the average grain size is less than 1 μm, the tensile strength is >250 MPa, and the elongation is >15%.
下面结合实施例对本发明提供的往复等通道角挤压强化镁锌合金的方法进行详细的说明,但是不能把它们理解为对本发明保护范围的限定。The method for strengthening magnesium-zinc alloy by reciprocating equal channel angular extrusion provided by the present invention will be described in detail below in conjunction with the examples, but they should not be construed as limiting the protection scope of the present invention.
实施例1Example 1
镁锌合金材料为铸态Mg-2wt%.Zn。The magnesium-zinc alloy material is cast Mg-2wt%.Zn.
对该合金实施10道次等通道角挤压变形,试样尺寸为15×15×50mm。400℃下进行第1道次的挤压变形,之后试样受往复挤压,挤压速率为12mm/s。The alloy was subjected to 10-pass equal channel angular extrusion deformation, and the sample size was 15×15×50mm. The extrusion deformation of the first pass was carried out at 400°C, and then the sample was subjected to reciprocating extrusion at a extrusion rate of 12mm/s.
实施例2Example 2
镁锌合金材料为铸态Mg-2wt%.Zn。The magnesium-zinc alloy material is cast Mg-2wt%.Zn.
对该合金实施12道次等通道角挤压变形,试样尺寸为15×15×50mm。380℃下进行第1道次的挤压变形,之后试样受往复挤压,挤压速率为10mm/s。The alloy was subjected to 12-pass equal channel angular extrusion deformation, and the sample size was 15×15×50mm. The extrusion deformation of the first pass was carried out at 380°C, and then the sample was subjected to reciprocating extrusion at a extrusion rate of 10 mm/s.
实施例3Example 3
镁锌合金材料为铸态Mg-0wt%.Zn。The magnesium-zinc alloy material is cast Mg-0wt%.Zn.
对该合金实施15道次等通道角挤压变形,试样尺寸为15×15×50mm。400℃下进行第1道次的挤压变形,之后试样受往复挤压,挤压速率为10mm/s。The alloy was subjected to 15 times of equal channel angular extrusion deformation, and the sample size was 15×15×50mm. The extrusion deformation of the first pass was carried out at 400°C, and then the sample was subjected to reciprocating extrusion at a extrusion rate of 10 mm/s.
对比例1Comparative example 1
对铸态Mg-2wt%.Zn合金仅进行1道次挤压变形,模具初始温度为400℃,其余与实施例1相同。The as-cast Mg-2wt%.Zn alloy is subjected to extrusion deformation only one pass, the initial mold temperature is 400° C., and the rest are the same as in Example 1.
对比例2Comparative example 2
对铸态Mg-2wt%.Zn合金进行2道次挤压变形,模具初始温度为400℃,其余与实施例1相同。The as-cast Mg-2wt%.Zn alloy was subjected to 2-pass extrusion deformation, the initial mold temperature was 400° C., and the rest were the same as in Example 1.
对比例3Comparative example 3
对铸态Mg-2wt%.Zn合金进行5道次挤压变形,模具初始温度为400℃,其余与实施例1相同。The as-cast Mg-2wt%.Zn alloy was subjected to extrusion deformation for 5 passes, the initial mold temperature was 400° C., and the rest were the same as in Example 1.
对比例4Comparative example 4
对铸态Mg-2wt%.Zn合金进行10道次挤压变形,模具初始温度为400℃,模具转角弧度ψ=300°,其余与实施例1相同。The as-cast Mg-2wt%.Zn alloy was subjected to extrusion deformation for 10 passes, the initial temperature of the mold was 400°C, and the arc of the mold rotation angle ψ=300°, and the rest were the same as in Example 1.
对比例5Comparative example 5
对铸态Mg-2wt%.Zn合金进行单道次挤压变形,模具温度低于300℃,其余与实施例1相同。3道次后样品发生开裂。The as-cast Mg-2wt%.Zn alloy is subjected to single-pass extrusion deformation, and the mold temperature is lower than 300° C., and the rest is the same as that of Example 1. The sample cracked after 3 passes.
实施例1~3和对比例1~4所得强化镁锌合金的金相结果如图2所示。图2中(a)为仅进行1道次挤压变形的铸态Mg-2wt%.Zn合金(对比例1),可以看出,其金相组织呈现典型的变形组织特征,即晶粒粗大,发生拉长变形,并存在大量孪晶。图2中(b)为进行2道次挤压变形的铸态Mg-2wt%.Zn合金(对比例2),可以看出,相较于对比例1,部分晶粒发生动态再结晶,晶粒形貌为细化的等轴态。图2中(c)为进行5道次挤压变形的铸态Mg-2wt%.Zn合金(对比例3),可以看出,经过5道次变形后,合金的晶粒发生细化,但组织依然不均匀。图2中的(d)为进行10道次挤压变形的铸态Mg-2wt%.Zn合金(实施例1),可以看出,经过10道次变形后,金相结果显示此时得到了超细等轴晶。图2中的(e)为进行12道次挤压变形的铸态Mg-2wt%.Zn合金(实施例2),可以看出,经过12道次变形后,金相结果显示此时得到了超细等轴晶,与10道次相比,部分晶粒发生长大。图2中的(f)为模具转角弧度ψ=300°时10道次挤压变形的铸态Mg-2wt%.Zn合金(对比例4),可以看出,相较于实施例2晶粒尺寸有所增大,晶粒大小不均匀,力学性能降低。图2中的(g)为进行15道次挤压变形后的铸态Mg-0wt%.Zn合金,即纯Mg(实施例3),可以看出,经过15道次变形后,纯Mg的晶粒也发生了均匀细化。The metallographic results of the strengthened magnesium-zinc alloy obtained in Examples 1-3 and Comparative Examples 1-4 are shown in FIG. 2 . (a) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (comparative example 1) that undergoes only one pass of extrusion deformation. It can be seen that its metallographic structure presents typical deformation structure characteristics, that is, coarse grains , elongated deformation occurs, and a large number of twins exist. (b) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (comparative example 2) that undergoes 2-pass extrusion deformation. It can be seen that, compared with comparative example 1, dynamic recrystallization occurs in some grains, and the grain The particle morphology is a fine equiaxed state. (c) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (comparative example 3) that carries out extrusion deformation of 5 passes, it can be seen that after 5 passes of deformation, the crystal grains of the alloy are refined, but The tissue remains uneven. (d) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (embodiment 1) that carried out 10 passes of extrusion deformation, as can be seen, after 10 passes of deformation, the metallographic results show that now obtained Ultrafine equiaxed crystals. (e) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (embodiment 2) that carried out 12 passes of extrusion deformation, as can be seen, after 12 passes of deformation, the metallographic results show that now obtained Ultrafine equiaxed grains, compared with the 10th pass, some grains grow up. (f) in Fig. 2 is the as-cast Mg-2wt%.Zn alloy (comparative example 4) of 10 pass extrusion deformations when mold angle radian ψ=300 °, as can be seen, compared with
性能测试Performance Testing
对实施例和对比例所得强化镁锌合金的屈服强度σ0.2、抗拉强度σb、延伸率进行测试,测试标准参照GB/T228.1-2010,所得结果见表1。实施例和对比例所得强化镁锌合金拉伸试验应力-应变曲线如图3所示。The yield strength σ 0.2 , tensile strength σ b , and elongation of the strengthened magnesium-zinc alloys obtained in the examples and comparative examples were tested. The test standards refer to GB/T228.1-2010. The results are shown in Table 1. The tensile test stress-strain curves of the strengthened magnesium-zinc alloy obtained in the examples and comparative examples are shown in FIG. 3 .
表1实施例和对比例所得强化镁锌合金的力学性能The mechanical properties of strengthened magnesium-zinc alloy obtained in table 1 embodiment and comparative examples
由表1和图3可以看出,本发明强化得到的镁锌合金具有良好的综合力学性能。It can be seen from Table 1 and Figure 3 that the magnesium-zinc alloy strengthened by the present invention has good comprehensive mechanical properties.
以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only a preferred embodiment of the present invention, it should be pointed out that, for those of ordinary skill in the art, without departing from the principle of the present invention, some improvements and modifications can also be made, and these improvements and modifications can also be made. It should be regarded as the protection scope of the present invention.
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1792487A (en) * | 2005-12-22 | 2006-06-28 | 上海交通大学 | Method for extrusion two-step equal channel angle of magnesium alloy |
| KR100768568B1 (en) * | 2006-06-05 | 2007-10-19 | 인하대학교 산학협력단 | Normal temperature ECP method of magnesium material |
| US20090116994A1 (en) * | 2007-11-06 | 2009-05-07 | Gm Global Technology Operations Inc. | High ductility/strength magnesium alloys |
| CN102719717A (en) * | 2012-05-25 | 2012-10-10 | 河海大学 | Degradable, high-toughness and ultrafine-grained magnesium-zinc rare earth alloy used for bone fixation and method for preparing same |
| CN102989764A (en) * | 2012-12-05 | 2013-03-27 | 河海大学 | High-yield processing method of ultra-fine crystal magnesium alloy thin plate |
| CN103215531A (en) * | 2013-04-25 | 2013-07-24 | 东南大学 | Preparation method of nanocrystalline magnesium alloy by continuous and severe plastic deformation |
| CN105886804A (en) * | 2016-05-16 | 2016-08-24 | 扬州大学 | Preparation method of high-performance magnesium-zinc system alloy |
| US20200399742A1 (en) * | 2017-04-12 | 2020-12-24 | University Of Pittsburgh-Of The Commonwealth System Of Higher Education | Properties and parameters of novel biodegradable metallic alloys |
-
2023
- 2023-03-01 CN CN202310188957.2A patent/CN116099892A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1792487A (en) * | 2005-12-22 | 2006-06-28 | 上海交通大学 | Method for extrusion two-step equal channel angle of magnesium alloy |
| KR100768568B1 (en) * | 2006-06-05 | 2007-10-19 | 인하대학교 산학협력단 | Normal temperature ECP method of magnesium material |
| US20090116994A1 (en) * | 2007-11-06 | 2009-05-07 | Gm Global Technology Operations Inc. | High ductility/strength magnesium alloys |
| CN102719717A (en) * | 2012-05-25 | 2012-10-10 | 河海大学 | Degradable, high-toughness and ultrafine-grained magnesium-zinc rare earth alloy used for bone fixation and method for preparing same |
| CN102989764A (en) * | 2012-12-05 | 2013-03-27 | 河海大学 | High-yield processing method of ultra-fine crystal magnesium alloy thin plate |
| CN103215531A (en) * | 2013-04-25 | 2013-07-24 | 东南大学 | Preparation method of nanocrystalline magnesium alloy by continuous and severe plastic deformation |
| CN105886804A (en) * | 2016-05-16 | 2016-08-24 | 扬州大学 | Preparation method of high-performance magnesium-zinc system alloy |
| US20200399742A1 (en) * | 2017-04-12 | 2020-12-24 | University Of Pittsburgh-Of The Commonwealth System Of Higher Education | Properties and parameters of novel biodegradable metallic alloys |
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