Ti对单相FCC的CoCrNi体系中/高熵合金组织与性能的影响

在CoCrNi三元、CoCrFeNi四元和Al_0.3CoCrFeNi五元合金中分别添加0.1～0.5(摩尔比)Ti，通过真空电弧炉制备出高硬度和高压缩强度的中/高熵CoCrNiTi_x、CoCrFeNiTi_x和Al_0.3CoCrFeNiTi_x合金棒材。Ti添加量为0.1的合金棒材(以下简称Ti_0.1合金，其余合金作相同处理)均保持单相FCC结构；Ti_0.3合金均出现少量的新相(η或R);CoCrNiTi_0.5合金由FCC+BCC+η+σ相组成，Al_0.3CoCrFeNiTi_0.5合金由FCC+BCC+R+B₂相组成，且二者微观组织均呈“花朵”状；而CoCrFeNiTi_0.5合金则由FCC+Laves+R+σ相组成，为树枝晶状结构。随着Ti含量的增加，三种体系合金的硬度均逐渐提高，且提高幅度按CoCrNiTi_x     

热锻态CoCrNi中熵合金组织及力学性能的研究

通过力学性能测试以及OM、XRD、SEM和EBSD分析,研究了热锻对CoCrNi三主元中熵合金组织和力学性能的影响.结果 表明:热锻后合金的晶粒得到明显的细化,晶体结构为面心立方结构(FCC).晶粒内部的大量退火孪晶与扩展层错的共同作用使得合金具有良好的室温力学性能.屈服强度达到380 MPa,抗拉强度达到850 MP...     

冷轧+退火对CoCrNi中熵合金显微组织和力学性能的影响

研究了CoCrNi中熵合金分别经低温(-196℃)和室温(25℃)冷轧及分别700℃和800℃退火后的显微组织和力学性能。结果表明,合金经低温冷轧+700℃退火后具有优良的强度-韧性匹配,抗拉强度为1023 MPa,总延伸率为34%,相比于室温冷轧+700℃退火、低温冷轧+800℃退火和室温冷轧+800℃退火,其抗拉强度分别提高了16%、13%、37%,主要是由于试样内发生回复与再结晶产生退火孪晶,细化晶粒,减小位错密度,阻碍位错的移动,提高合金强度。     

热处理对Al0.5CoCrFeNiB-0.2高熵合金组织结构及力学性能的影响

采用真空电弧炉制备Al0.5CoCrFeNiB0.2高熵合金,采用X射线衍射仪、金相显微镜、扫描电镜等方法研究铸态合金的组织结构及其热处理的影响,采用显微硬度计和拉伸试验测定合金热处理前后的力学性能。结果表明:Al0.5CoCrFeNiB0.2铸态合金仅由简单的体心立方结构和两个面心立方结构三相组成。合金铸态组织由树枝状初生α1相、粒状α2相和共晶组织(α1相和层片状β相)组成。退火和淬火热处理并未改变Al0.5CoCrFeNiB0.2合金的相结构。但随着热处理温度的提高,初生α1相由共晶组织β相回溶而长大的趋势更加明显。退火和淬火热处理均可强化合金。其中,经800℃×10 h退火后,合金室温抗拉强度由铸态的850.14 MPa提高到1 232 MPa;经1 000℃×10 h淬火后,合金塑性及强度均优于铸态合金,尤其是塑性显著提高。     

粉末冶金制备AlNiCrFexMo0.2CoCu高熵合金及组织和压缩性能的研究

采用粉末冶金法制备了AlNiCrFexMo0.2CoCu(x=0.5、1.0、1.5、2.0)高熵合金,研究了Fe元素对该合金组织和性能的影响.对上述4种合金进行XRD分析,发现当x=0.5、1.0和1.5时,有BCC、FCC和σ相三相组成;当x=2.0时,合金只有BCC和FCC两相;该合金硬度随Fe含量的增加而降低.压缩试验表明,合金断裂强度均超过1100MPa,且具有较好的塑性.     

退火温度对FeMoCrVTiSix高熵合金组织及力学性能的影响

在400、600、800、1100 ℃下对FeMoCrVTiSi_x(x=0、0.3)进行退火处理,利用X射线衍射仪、扫描电镜、差热扫描分析仪、显微硬度计、万能试验机等探究了不同退火温度对合金的组织和力学性能的影响。结果表明,Si元素的添加提高了FeMoCrVTi高熵合金的热稳定性。经过退火处理,FeMoCrVTiSi_x高熵合金的微观组织仍为以BCC固溶相为主的枝晶结构,但在枝晶边缘出现黑色的细小富Ti相,其含量随着退火温度的增加而增多,在1100 ℃下富Ti相回溶。富Ti相的析出提高了合金的硬度,其中,800 ℃退火后试样的硬度达到最大值,FeMoCrVTi试样的硬度达到932 HV0.2,FeMoCrVTiSi_0.3的硬度达到998 HV0.2。     

TiZrHfNbSc难熔高熵合金组织和力学性能研究

利用真空电弧熔炼设备制备了新型TiZrHfNbSc难熔高熵合金,利用XRD、SEM、DSC等方法分析了合金的显微组织,利用显微硬度计、微控电子万能试验机测定了合金的硬度及力学性能。研究结果表明：TiZrHfNbSc难熔高熵合金为单一无序的BCC固溶体结构,晶格常数a=3.443?,合金密度约为7.16g/cm_³;合金的维氏显微硬度约380,屈服强度σ_0.2=650MPa,压缩变形率达到60%以上,合金的强化机制为固溶强化。     

Si对FeMoCrVTiSix高熵合金组织和力学性能的影响

采用真空电弧熔炼工艺制备了FeMoCrVTiSix(x=0、0.3、0.5、1)高熵合金,利用X射线衍射仪、扫描电镜、显微硬度计、万能试验机等设备研究了合金的组织和力学性能。结果表明,x=0时,合金由单一BCC固溶结构组成,随着Si含量增加,合金中逐渐析出(MoCrV)3Si相和(FeCrVSi)2(MoTi)的Laves相,x=1时,Laves相成为主相。随着Si含量增加,合金脆性随之增加,硬度(HV)也呈上升趋势,在x=1时达到最大值1113。     

CoCrxNi中熵合金组织及力学性能研究

以等原子比CoCrNi中熵合金为基础,采用真空电弧熔炼炉制备了CoCr_xNi(x=1.0, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, at%)中熵合金,研究了Cr含量对合金微观组织及力学性能的影响。结果表明:CoCr_xNi(x=1.0, 1.5, 1.6)中熵合金为单一的面心立方相(fcc);随着Cr元素含量增加,CoCr_xNi(x=1.7, 1.8, 1.9, 2.0)中熵合金的fcc相基体中析出了体心立方相的富Cr条状组织;合金的强度、硬度随着Cr元素含量的增加而不断提高,但塑性恶化;与等原子比CoCrNi中熵合金相比,CoCr_1.7Ni中熵合金在保持较高塑性的同时,强度、硬度显著提高。     

轧制变形对高熵合金微观组织和力学性能的影响

对(FeNi)₆₇Cr₁₅Mn₁₀Al₅Ti₃高熵合金进行退火、冷轧和热轧+冷轧等工艺处理,采用X射线衍射仪、扫描电镜和万能试验机分别对合金进行物相组成、组织形貌以及力学性能测试和表征。结果表明,铸态和退火态的非等主元(FeNi)₆₇Cr₁₅Mn₁₀Al₅Ti₃高熵合金更易形成单相固溶体;在中等变形的热轧+冷轧工艺下,合金形成FCC+BCC的双相固溶体,其屈服强度可提高到460.0 MPa;在中等变形的冷轧工艺下,合金会形成细小的金属间化合物,从而具有细小金属间化合物强化机制,使屈服强度显著提升并达到722.0 MPa,同时,合金仍具有约25.7%的均匀伸长率,综合力学性能最佳。     

Microstructure and mechanical properties of equimolar FeCoCrNi high entropy alloy prepared via powder extrusion

An equiatomic FeCoCrNi high alloy (HEA) with both high tensile strength and ductility was produced by a powder metallurgy (P/M) method. The P/M process includes a gas atomization and a hot extrusion of pre-alloyed HEA powder. Microstructures and mechanical properties were characterized using optical microscopy (OP), scanning electron microscopy (SEM), electron backscattered diffraction (EBSD), and tensile tests. The results show that the P/M FeCoCrNi HEA has a single face centered cubic (fcc) structure and an equiaxed microstructure. No obvious porosity and brittle intermetallic phase was found. The as-extruded alloy exhibits a very high tensile strength of 712.5 MPa, and still maintains an elongation as high as 56%. The improvement of the tensile properties is caused by the solid solution strengthening, grain boundary strengthening and homogenous microstructure. Therefore, the powder hot extrusion can be considered as a promising way for preparing large-sized HEAs with high mechanical properties.     

多孔CoCrNi中熵合金的制备和吸能特性分析

本文采用粉末烧结-溶解法成功制备了孔隙率为63%~78%,孔径1.3~2.2mm的多孔CoCrNi中熵合金,借助SEM和XRD对试样的孔形貌和物相组成进行分析,并对试样进行轴向准静态压缩实验研究。结果表明：多孔CoCrNi中熵合金的弹性模量和屈服平台应力均随孔隙率、孔径的增大而减小;相对孔隙率而言,孔径对力学性能的影响程度较低;不同孔隙率的多孔CoCrNi中熵合金其致密应变下单位体积的能量吸收值为34.8~14.3MJ/m₃^,约为泡沫铝的3.8倍,且5种孔隙率的理想吸能效率(I)都接近0.8,说明该多孔CoCrNi中熵合金有潜力成为一种理想的吸能材料。     

粉末冶金碳化物强化铌合金组织演变及其力学行为

采用机械球磨与热压烧结相结合的粉末冶金法对不同球磨时间Nb-35Ti-6Al-5Cr-8V-5C合金的粉末变形行为,微观组织结构和力学行为进行研究。结果表明:随着球磨时间的增加,Nb-35Ti-6Al-5Cr-8V-5C复合粉末中的块状金属颗粒首先变形为片状后在碰撞挤压作用下破碎成絮状,TiC粉末均匀的分布于片状金属粉末表面;Nb-35Ti-6Al-5Cr-8V-5C合金由Nbss和(Nb,Ti)C两相构成,各合金碳化物体积分数均为11%左右,Ti元素主要分布于Nbss晶界和碳化物内,Al、Cr、V元素主要分布于Nbss晶粒内,Nbss和(Nb,Ti)C相尺寸均随球磨时间增加而尺寸减小;Nbss晶粒细化及强化相碳化物弥散化导致合金的室温压缩力学性能和塑性变形能力显著提高,压缩变形后合金Nbss与碳化物具有良好的界面结合能力,但是碳化物内部存在明显的近似平行分布的裂纹;数据对比表明,粉末冶金法制备Nb-35Ti-6Al-5Cr-8V-5C合金的力学性能优于电弧熔炼法。     

Preparation of superfine-grained high entropy alloy by spark plasma sintering gas atomized powder

In this work, nanocrystalline CrMnFeCoNi HEAs were prepared by powder metallurgy. It was found mechanical milling can further refine the microstructures and morphologies of the gas-atomized powder, and increase the sintering ability. The HEAs sintered from the mechanically milled powder have much finer microstructures than that from the gas-atomized powder. The original morphology and defects in both the gas-atomized and the mechanically milled powders can be inherited to the bulk forms after the SPS. The SPSed HEAs have a tensile strength as high as 1000 MPa at room temperature and reasonable ductility. The strengthening mechanism can be attributed to the nanocrystalline microstructures, in which grain boundaries block the movement of dislocations. Powder metallurgy can be taken as a promising way for preparing HEAs with high mechanical properties.     

Microstructure and mechanical properties of magnesium composites prepared by spark plasma sintering technology

Spark plasma sintering (SPS) technology was used to determine the appropriate conditions for SPS sintering of commercially pure magnesium as well as the magnesium alloy AZ31. It was found that the sintering temperatures of 585 °C and 552 °C were the most suitable sintering temperatures for the magnesium and the AZ31 alloy, respectively. Magnesium matrix and AZ31 alloy matrix composites reinforced with SiC particles were then successfully fabricated by the SPS method at sintering temperatures of 585 °C and 552 °C, respectively. A uniform distribution of SiC particles was observed along the boundary between matrix particles. The mechanical properties, i.e. hardness and tensile strength increased with increasing SiC content up to 10 wt%. However, when the SiC content was larger than 10 wt%, the tensile strength decreased due to the agglomeration of SiC particles. The agglomeration of SiC particles was found to lead to the degradation of the interfacial bonding strength between matrix and reinforcement.     

氮元素对CrFeMnVTi6高熵合金显微组织和力学性能的影响

为了评估氮元素的间隙固溶强化机制对高熵合金性能的影响,采用机械冶金化和放电等离子体烧结工艺制备N掺杂CrFeMnVTi6高熵合金,并利用XRD、SEM、TEM和FIB检测手段对合金的相组成及显微组织进行表征.实验结果显示,CrMnFeVTi6合金组织由TiNx、BCC、Laves相和B2有序相组成.因此,合金在低温区域...     

激光烧结制备CrFeNiAlSiTix高熵合金组织与性能

为了验证利用铬铁矿粉直接制备高熵合金的可行性,选取和天然铬铁矿粉成分接近的Cr、Fe、Ni、Al、Si作为基础元素,向其掺杂非等摩尔比的Ti元素混合后压制成坯,采用激光自蔓延烧结制备CrFeNiAlSiTix（x=0-1.2）高熵合金。通过共聚焦显微镜、XRD、SEM和EDS、维氏显微硬度计、电化学工作站等进行表征,分析物相结构、显微组织、密度和孔隙率、硬度、耐磨、耐蚀及高温氧化性能。结果表明：随着Ti含量的增加,合金中BCC相增多,且通过本征参数计算进行验证与实验结果吻合。树枝晶组织减少,花瓣状组织增加,枝晶中主要存在与Ti结合力强的元素。当x=1.0时,合金显微硬度最大为935.62 HV,密度最大为5.01 g/cm3,孔隙率最小为24.01 %,单位面积磨损量最小为34 mg·cm-2,氧化速率最大为5.92×10-6 mg2·cm-4·s-1,腐蚀电流为0.98 μA/cm2,年腐蚀深度为1.01×10-2 mm/a。     

Effect of thermomechanical processing on microstructure and mechanical properties of CoCrFeNiMn high entropy alloy

The CoCrFeNiMn high entropy alloy was produced by homogenization, cold rolling and recrystallization. The effects of thermomechanical processing on microstructures and tensile properties at different temperatures were investigated using X-ray diffractometry (XRD), optical microscopy (OM), scanning electron microscopy (SEM) and multi-functional testing machine. The results show that dendritic structures in cast alloy evolve into equiaxed grains after being recrystallized, with single face-centered cubic (FCC) phase detected. The most refined alloys, stemming from the highest rolling ratio (40%), exhibit the highest strength due to the grain boundary strengthening, while the variation of elongation with temperature shows a concave feature. For the coarse-grained alloys, both the ductility and work hardening ability decrease monotonically with increasing temperature. Serrated flow observed at intermediate temperatures is attributed to the effective pinning of dislocations, which manifests the occurrence of dynamic strain hardening and results in the deterioration in ductility. Besides, dimples on the fracture surfaces indicate the typical ductile rupture mode.     

冷轧退火对FeMnCoCrAl高熵合金组织和力学性能的影响

使用真空电弧炉熔炼出(Fe₅₀Mn₃₀Co₁₀Cr₁₀)₉₄Al₆合金,利用冷轧及在不同温度对合金进行退火,以期望得到由多尺度再结晶晶粒构成的层状结构;并对不同退火温度的样品进行拉伸性能测试。利用扫描电镜和EBSD对合金组织形貌进行表征,采用X射线衍射方法研究其相组成。结果表明:合金在铸态和冷轧后相组成未发生变化,700 ℃退火得到较好的多尺度再结晶晶粒的层状结构,其屈服强度为487 MPa,抗拉强度为708 MPa,断后伸长率为39%,表现出良好的综合力学性能。