铸态Mg-4Al-2Si合金的显微组织与力学性能

采用重力铸造法制备Mg-4Al-2Si(AS42)镁合金,研究了铸态合金的显微组织和室温力学性能。结果表明:铸态AS42合金主要由α-Mg基体、β-Mg17Al12相及Mg2Si相组成;β-Mg17Al12相呈网状和棒状分布于晶界上,粗大的汉字状Mg2Si相沿晶界或穿晶分布,多边形块状Mg2Si相随机分布于基体组织中。铸态合金的硬度为64.5 HV,室温抗拉强度为113.5 MPa,屈服强度为86 MPa,伸长率为4.1%;拉伸断裂形式为准解理脆性断裂。     

Mg-Y-Nd-Zr-Zn 铸造镁合金组织与性能研究

目的研究Mg-Y-Nd-Zr-Zn镁合金的显微组织演变和力学性能。方法采用金相显微镜(OM)、扫描电镜(SEM)、能谱(EDS)以及电子万能实验机等,研究了Mg-Y-Nd-Zr-Zn镁合金铸态及T6态的组织和性能。结果 Mg-Y-Nd-Zr-Zn铸态合金组织由含Y的镁基固溶体、网状富稀土的共晶相和颗粒状的Zr单质组成;经525℃×10 h+200℃×16 h处理后,晶界网状第二相消失,细小的Mg-RE金属间化合物从基体中析出,弥散分布于晶界及晶内。结论 T6处理后,Mg-Y-Nd-Zr-Zn合金力学性能显著提高,抗拉强度、屈服强度和断裂伸长率分别为306 MPa,230 MPa和3.5%。     

大尺寸Al-Cu-Mg-Mn合金铸锭均匀化工艺研究

本工作通过金相、DSC、SEM等手段研究了均匀化工艺对大尺寸Al-Cu-Mg合金扁锭的组织演变和力学性能的影响。研究结果表明,铸态合金中枝晶偏析从芯部区域到边部区域越来越严重,晶界分布大量的块状A_2Cu相和Al_2CuMg相。采用接近低熔点共晶融化温度进行均匀化退火后,选择合适的均匀化时间使得合金中的枝晶偏析基本消除,晶内成分分布较为均匀。经500℃/36 h均匀化后,残留第二相含量为0.88%,经过轧制变形后的薄板T42态的抗拉强度达到480 MPa,屈服强度达到327 MPa,延伸率为19%.     

Mg-5Gd-4Y-0. 3Zr 合金组织和力学性能研究

目的研究均匀化、挤压及时效热处理对Mg-5Gd-4Y-0.3Zr合金组织和力学性能的影响。方法制备了Mg-5Gd-4Y-0.3Zr合金铸棒,并进行了均匀化处理和热挤压处理。对不同状态的试样进行了拉伸试验,观察了金相显微组织,采用X射线衍射方法进行了结构分析。结果铸态合金组织主要由α-Mg基体和第二相Mg5(Gd,Y)组成;经过均匀化处理后,合金的第二相发生了完全回溶,合金的力学性能得到了提升;合金经挤压后,组织得到了明显细化,在200℃保温60 h得到了强度的最大值,抗拉强度、屈服强度和伸长率分别为423.0 MPa,335.0 MPa与9.0%。结论Mg-5Gd-4Y-0.3Zr合金既保证了低成本,又具有优良的力学性能,适合推广应用。     

Mg-Gd-Y-Zr 活塞微观组织及力学性能研究

目的研究Mg-Gd-Y-Zr镁合金活塞本体的微观组织和力学性能。方法采用金属型重力铸造工艺制备镁合金活塞,利用光学显微镜和扫描电镜分析了铸态、固溶态(T4)和固溶时效态(T6)活塞本体的显微组织,利用岛津材料试验机和硬度计测试活塞本体的力学性能。结果铸态Mg-Gd-Y-Zr镁合金活塞本体组织中大量的第二相分布于晶界处,T4处理后大部分固溶到基体中,T6处理后晶粒内部出现麻点状和细条状的析出相。活塞裙部和顶部经T6处理后的抗拉强度随着拉伸温度的升高而逐渐降低,在300℃拉伸时活塞裙部抗拉强度达到226.38 MPa;活塞裙部和顶部的伸长率随着拉伸温度的升高而增加,在350℃拉伸时活塞裙部伸长率达到23.65%。结论镁合金活塞裙部的室温和高温抗拉强度好于活塞顶部,裙部尺寸较均匀。     

铸态Mg-4Al-4Si-0.75Sb合金的显微组织与力学性能

采用重力铸造法制备Mg-4Al-4Si-0.75Sb(AS44-0.75Sb)(质量分数/%,下同)镁合金,研究铸态合金的显微组织和室温力学性能。结果表明:铸态AS44-0.75Sb合金主要由α-Mg基体、β-Mg17Al12相、Mg2Si相和Mg3Sb2相组成;加入0.75Sb后形成高熔点的Mg3Sb2相,显著改善了Mg2Si相的形貌,使粗大的骨骼状Mg2Si转变为相对细小的汉字状Mg2Si。铸态合金的硬度HV为65.9,屈服强度为136.4MPa,抗拉强度为172.3MPa,伸长率为3.3%;拉伸断裂形式为准解理脆性断裂。     

铸态镁合金组织和力学性能研究

对Mg-5．0Y-3．0Nd-0．5Zr镁合金进行熔铸和不同温度的均匀化退火。测试该合金的室温拉伸力学性能。并采用金相显微镜,扫描电镜等方法观察铸态和均匀化退火态组织。结果表明,添加稀土元素能使镁合金的铸态组织得到细化,Nd和Y分别以Mg4、Nd3和Mg24Y化合物形式存在,均匀化退火后,试验合金抗拉强度和伸长率得到提高．其中450℃的均匀化退火效果最好,合金的抗拉强度比铸态时的提高了18．6％,塑性提高了3．5％。     

热变形Ti-45Al-7Nb-0.3W合金的显微组织与力学性能

采用金相显微镜(OM)、扫描电镜(SEM)、透射电镜(TEM)和拉伸试验研究热变形(锻造、轧制)Ti-45Al-7Nb-0.3W(原子分数/%,下同)合金的显微组织与力学性能。结果表明:铸态Ti-45Al-7Nb-0.3W合金为近层片组织,主要由α2/γ层片晶团及分布在层片晶团周围的少量γ相和β相组成,层片晶团平均尺寸为100μm;经热包套锻造后,层片晶团发生破碎、扭折,并且室温抗拉强度较铸态提高了77MPa,800℃抗拉强度提高了36MPa;该锻态合金经热包套轧制后,合金组织转变为细小的双态组织,平均晶粒尺寸为25μm,合金力学性能进一步提高,其中室温抗拉强度提高到603MPa,伸长率为1.0%,800℃抗拉强度提高到716MPa,伸长率为3.6%。     

稀土Y和Sm对AZ91D镁合金组织与性能的影响

采用控制变量法研究单一稀土Y和复合稀土Y,Sm元素对AZ91D镁合金微观组织与力学性能的影响,分析稀土元素对AZ91D合金的细化机理。结果表明：复合添加稀土Y和Sm对AZ91D合金的作用效果明显好于单一添加稀土Y对AZ91D合金的作用效果,添加Y和Sm后,生成了块状相Al₂Y相和针状相Al₂Sm相,可以作为α-Mg的有效异质形核点。当加入量为0.8%（质量分数,下同）Y+1.0% Sm时,α-Mg晶粒尺寸最为细小,分布最为均匀,其合金的硬度、抗拉强度及伸长率分别为67.42HV,153.37 MPa和3.62%,改善了铸态AZ91D合金的室温力学性能,但是超过这个最佳添加量后,合金的室温力学性能开始下降。     

AZ81镁合金挤压组织和性能研究

对AZ81镁舍金铸锭进行(390±10)℃×15h的固溶处理后,在400℃进行挤压,挤压比为32∶1,研究其组织和力学性能.结果表明,挤压AZ81镁合金具有较细的晶粒组织,第二相Mg17Al12被破碎,其分布变得弥散,个别呈流线分布;挤压AZ81镁合金比铸造AZ81镁合金的力学性能有较大提高,其屈服强度为221.6MPa,抗拉强度为311.5MPa,伸长率为14.2%.其挤压态断口表现出明显的塑性断裂特征.     

High-strength Mg95Y3Zn1Ni1 alloy with LPSO structure processed by hot rolling

Microstructures and mechanical properties of Mg₉₅Y₃Zn₁Ni₁ alloy containing long period stacking ordered (LPSO) phase processed by hot rolling were systematically investigated in the present work. The results showed that the as-cast alloy was mainly composed of α-Mg and network 18?R LPSO phase. The thermal stability of 18?R LPSO phase in the as-cast alloys decreased with the decrease of Ni content. After solution treatment at 773?K for 40?h, network 18?R phase at grain boundary dissolved, while fine lamellar phase identified as 14H LPSO precipitated in the interior of grains. When the solid-solution alloy was hot rolled at 723?K with six passes and thickness reduction of 62%, some LPSO phases broke down and kinking of varying degrees occurred in LPSO phase. Meanwhile, the as-rolled α-Mg and LPSO phase redistributed aligned along the rolling orientation. The alloy exhibited excellent mechanical properties: yield strength of 282?MPa, ultimate tensile strength of 383?MPa, and elongation to failure of 16% at ambient temperature along the rolling orientation. The remarkable improvement of strength was ascribed to the refined microstructure induced by the deformation kinking and the crush of LPSO phase.     

热处理对真空压铸NZ30K镁合金微观组织及力学性能的影响

使用光学显微镜(OM)、扫描电镜(SEM)、能谱分析(EDS)、硬度测试和拉伸性能测试等方法,研究了热处理对真空压铸NZ30K镁合金微观组织及力学性能的影响。结果表明：铸态合金的宏观组织分为表层区和心部区,表层区组织由细小α-Mg等轴晶和分布在晶界的Mg₁₂Nd组成,心部区组织则由细小α-Mg等轴晶、粗大预结晶组织(ESCs)和分布在晶界的离异共晶Mg₁₂Nd组成。在固溶处理过程中心部区晶粒的长大比表层区更为显著,晶界迁移速率与晶粒尺寸不均匀呈正相关性,满足晶粒长大模型v=M₀ exp (-Q/RT) A (1/D₁-1/D₂)。合金的优化热处理工艺为540℃×6 h+200℃×8 h。与铸态合金(UTS=186.0±1.5 MPa,YS=131±2.5 MPa,EL=6.6±0.4%)相比,峰值时效态合金的抗拉强度和屈服强度分别提高到了223.6±4.1 MPa和172.8±2.9 MPa,但延伸率降低到了4.2±0.3%。其强度的提高主要得益于时效析出的片状纳米β"相能够有效地阻碍位错在基面上的滑移。铸态和热处理态合金的表层区断裂模式均为韧性断裂,而心部区的断裂模式在铸态下为准解理断裂、在固溶态下为解理断裂、在峰值时效态下为准解理断裂。     

热挤压AZ91D镁合金边角料组织和性能的研究

采用热挤压工艺直接热挤出AZ91D镁合金边角料,研究挤压温度对挤压成形镁合金组织和性能的影响,并讨论其断裂行为.结果表明:在450℃热挤压时,晶粒尺寸均匀,组织中已不存在原始边角料之间未打碎的结合面,边角料之间结合较好;在350～450℃之间热挤出时,AZ91D镁合金随挤压温度的升高,抗拉强度和延伸率均增加,当挤压温度...     

Microstructure evolution and mechanical properties at high temperature of selective laser melted AlSi10Mg

In this study,the microstructure and tensile properties of selective laser melted AlSilOMg at elevated temperature were investigated with focus on the interfacial region.In-situ SEM and in-situ EBSD analysis were proposed to characterize the microstructural evolution with temperature.The as-fabricated AlSilOMg sample presents high tensile strength with the ultimate tensile strength(UTS)of~450 MPa and yield strength(YS)of~300 MPa,which results from the mixed strengthening mechanism among grain boundary,solid solution,dislocation and Orowan looping mechanism.When holding at the temperature below 200℃for 30 min,the micro structure presents little change,and only a slight decrement of yield strength appears due to the relief of the residual stress.However,when the holding temperature further increases to 300℃and 400℃,the coarsening and precipitation of Si particles inα-Al matrix occur obviously,which leads to an obvious decrease of solid solution strength.At the same time,matrix softening and the weakness of dislocation strengthening also play important roles.When the holding temperature reaches to 400℃,the yield strength decreases significantly to about 25 MPa which is very similar to the as-cast Al alloy.This might be concluded that the YS is dominated by the matrix materials.Because the softening mechanism counteracts work hardening,the extremely high elongation occurs.     

Sn对时效态ZM61镁合金高温力学性能的影响

利用金相显微镜(OM)、X射线衍射(XRD)、扫描电镜(SEM)和高温拉伸对时效态ZM61-xSn(x=0,6,8,10,质量分数/%,下同)合金的高温拉伸性能及断裂机制进行了研究。结果表明:ZM61-xSn(x=6,8,10)合金的物相由α-Mg,α-Mn,MgZn2,Mg2Sn相组成。添加Sn元素可有效细化ZM61合金组织,提高合金高温强度,但降低合金塑性。ZM61-xSn(x=6,8,10)合金在300℃下拉伸的抗拉强度分别为149,140,145MPa,较相同温度下拉伸的ZM61合金的抗拉强度分别提高了26%,17%,23%。ZM61-xSn(x=0,6,8,10)合金在300℃下拉伸的伸长率分别为39.95%,5.65%,7.01%和6.33%。拉伸温度对ZM61-xSn(x=6,8,10)合金的断裂机制产生显著影响。当拉伸温度低于220℃,合金为穿晶断裂;高于220℃时,合金变为沿晶断裂。     

Zn对铸态Mg-Y-Nd-Zr合金组织和力学性能的影响

采用光学显微镜(OM)、扫描电子显微镜(SEM)、X射线衍射分析及力学性能测试等研究Zn元素对Mg-Y-Nd-Zr铸态合金显微组织及力学性能的影响。结果表明:随着Zn含量的增加,Mg-Y-Nd-Zr-xZn(x=0.0%,0.5%,1.0%,1.5%,质量分数)合金的晶粒逐渐细化,平均晶粒尺寸由(57±0.8)μm细化至(30±0.3)μm,晶界处共晶相的体积分数也逐渐增加。Mg-Y-Nd-Zr铸态合金中主要存在Mg12Nd相和Mg24Y5相,加入0.5%Zn后,合金中出现Mg12YZn相。随Zn含量的增加,Mg12YZn相的体积分数不断增大,合金的力学性能逐渐提高。当Zn含量为1.0%时,合金具有最优的力学性能,其抗拉强度、屈服强度和伸长率分别为(208±5.9),(159±3.9)MPa和(7.5±0.2)%,较未加Zn的合金分别提高了18,42MPa和1.2%。     

Evolution behavior of δ phase in Cu12Sn2Ni alloy and the corresponding effects on alloy property

With the increase of tin content in tin bronze, the rise of δ phase made the strength, hardness of tin bronze increase and the ductility decrease sharply, that difficult to process. In this paper, the Cu12Sn2Ni alloy was prepared by centrifugal casting, the microstructure and phase formation before and after heat treatment were observed by x-ray diffraction, scanning electron microscope, and transmission electron microscope. The results showed that the as-cast sample microstructure was composed of equiaxed grains rather than coarse dendrites. centrifugal casting inhibits tin diffusion to form metastable phase β′-Cu_13.7Sn. The as-cast sample had good deformability and its tensile strength and elongation were 381.9 MPa and 12.4 %, respectively, which are higher than the mechanical properties of gravity casting. The tensile strength and elongation of the sample after furnace cooling at 620 °C/8 min are 439.5 MPa and 24.4 %, respectively, the increase was 16.6 % and 85.07 %, compared with the as-cast samples, due to the solid solution strengthening, the second phase strengthening and the homogenization of the microstructure.     

A high strength and ductility Mg–Zn–Al–Cu–Mn magnesium alloy

A high strength Mg–8.0Zn–1.0Al–0.5Cu–0.5Mn (wt.%) magnesium alloy with outstanding ductility was developed using a common casting technique and heat treatment. The microstructure of the as-cast alloy is composed of α-Mg, MgZn, MgZnCu and Al–Mn phases. After the solution treatment and subsequent two-step aging treatment, the yield strength (YS), ultimate tensile strength (UTS) and elongation of the alloy at peak hardness reach 228 MPa, 328 MPa and 16.0% at room temperature, respectively. The comprehensive mechanical properties of the alloy are superior to almost all other high performance casting Mg alloys.