Effect of La Doping on Microstructure and Critical Current Density of MgB2

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中南大学学报(增刊)写作格式范例

中南大学学报(增刊)写作格式范例

具体论文写作格式见本刊网站或相关数据库。

论文主要格式(框架)举例如下。

×××对×××合金铸态组织的影响张三1,李四2,王五1,2(1.××大学材料科学与工程学院,湖南长沙,410083;2.××大学××学院,湖南长沙,410083)摘要:××××××。

(按方法、结果、结论的要求写,要详细、具体)关键词:×××;×××;×××(3个或3个以上)中图分类号:TG146.2+1 文献标志码:A 文章编号:1672-7207(2010)Effect of×××on as-cast microstructure of×××alloyZHANG San ,LI Si,WANG Wu(1.School of Materials Science and Engineering, Central South University, Changsha 410083, China;2. School of ××,××University, Changsha 410083, China)Abstract:×××(与中文摘要相对应;用被动语态,研究过程用过去时,研究结果和结论用现在时).Key words:×××(与中文关健词相对应)××××××(正文)一.在论文首页地脚处标注:收稿日期:基 金项目:国家“973”重点基础研究发展规划项目(×××××××(即项目号))通信作者:张三(1968-),男,湖南××人,教授,博士,从事×××研究;电话:×××;E-mail: ×××二.文中图、表举例(注:图题、表题的中英文应对照):表1制备TiO x薄膜的工艺参数Table 1Preparing process parameters of TiO x film样品编号氩气流量/(mL∙min−1)氧气流量/(mL∙min−1)溅射功率/W总气压/Pa沉积速率/(nm∙min−1)1 100 0 300 0.70 25.602 973 300 0.69 23.303 95 5 300 0.68 38.544 93 7 300 0.68 3.285 90 10 300 0.66 5.006 80 20 300 0.62 4.507 70 30 300 0.59 3.80图1 沉积速率随氧气流量的变化Fig.1 Variation of deposition rate on oxygen flow-0.20.00.20.40.60.81.01.21.41.61.82.02.22.4-202468101214a 54321P /k N 位移/m m -0.20.00.20.40.60.81.01.21.41.61.82.02.2100200300400500b 52143P /N 位移/m m(a)-垂直抗压;(b)—Ⅰ抗弯 1—未经热处理; 2—HTT,1 600℃; 3—HTT,2 000℃;4—HTT,2 200℃;5—HTT,2 400℃图2 Ⅰ试样不同热处理温度下的应力-位移曲线Fig.1 Stress-displacement curves of three kinds of C/C under different HTTs……三.参考文献举例:[1] Fang J H, Lu X M, Zhang X F. CdSe/TiO 2 nanocrystalline solar cells[J]. Superamolecularm Science, 1998, 5(5/6):709−711.[2] 王鹤, 杨宏, 于化丛, 等. 单晶硅太阳电池纳米减反射膜的研究[J]. 固体电子学研究与进展, 2003, 23(3): 316−319.WANG He, YANG Hong, YU Hua-cong, et al. The experimental study on nanometer antireflection coating used in single crystalline silicon solar cells[J]. Research & Progress of Solid State Electronics, 2003, 23(3): 316−319.[3] 尹荔松, 谭敏, 陈永平, 等. La 掺杂对纳米TiO 2薄膜晶体结构和光催化性能的影响[J]. 中南大学学报: 自然科学版,2008, 39(4): 665−670.YIN Li-song, TAN Min, CHEN Yong-ping, et al. Effect of La doping on crystal structure and photocatalytic properties of TiO 2 thin film[J]. Journal of Central South University: Science and Technology, 2008, 39(4): 665−670.[4] ZHAO Lei, LIAN Jian-she. Effect of substrate temperature on structural properties and photocatalytic activity of TiO 2 thinfilms[J]. Transactions of Nonferrous Metals Society of China, 2007, 17(4): 772−776..……。

Effect of heat treatment on microstructure and properties of

Effect of heat treatment on microstructure and properties of
Abstract: The effect of heat treatment on the microstructure and properties of a hot-extruded nickel-aluminum bronze was investigated. Experimental materials were heat treated through different processes, including quenching, normalizing, aging and annealing, and their microstructure, corrosion resistance and mechanical properties were characterized. It is found that quenching causes all p phase transformed into p’ phase, however, normalizing causes p phase transformed into p’, a and K phases. When the quenched sample is aged, fine K phase is precipitated from the as-quenched microstructure of p’ phase. Annealing causes the transformation of p’ into a and K phases. The results of mechanical property tests show that quenching, normalizing and aging improve the tensile strength and hardness of the experimental material, with a corresponding fall in elongation. Annealing raises the elongation but reduces the tensile strength and hardness. Furthermore, corrosion resistance of nickel-aluminum bronze ranks from worse to better in the following order: aged, quenched, normalized, hot-extruded and annealed. However, with the exposure time of corrosion test increasing, the difference of average corrosion rate between those nickel-aluminum bronzes turns small.

Effect of Nb addition on the microstructure and properties of AlCoCrFeNi high-entropyalloy

Effect of Nb addition on the microstructure and properties of AlCoCrFeNi high-entropyalloy

article info
Article history: Received 18 January 2011 Received in revised form 20 September 2011 Accepted 28 October 2011 Available online 11 November 2011
Keywords: High entropy alloy Eutectic Laves phase Solid solution
abstract
The microstructures and properties of the AlCoCrFeNbxNi high-entropy alloys (HEAs) were investigated. Two phases were found in the prepared AlCoCrFeNbxNi HEAs: one is body-centered-cubic (BCC) solid solution phase; the other is the Laves phase of (CoCr)Nb type. The microstructures of the alloy series vary from hypoeutectic to hypereutectic, and the compressive yield strength and Vickers hardness have an approximately linear increase with increasing Nb content. The residual magnetization (Mr) reaches a maximum for AlCoCrFeNb0.1Ni alloy, which is 6.106 emu/g. The factor of ˝, which is defined as entropy of mixing times 1000 over enthalpy of mixing, well predicts the phase formation for the multicomponents alloys.

TiAlCN涂层界面扩散机理与结合强度

TiAlCN涂层界面扩散机理与结合强度

TiAlCN涂层界面扩散机理与结合强度孔德军;付贵忠;郭皓元【摘要】利用阴极弧离子镀在Cr12MoV钢表面制备了TiAlCN涂层,通过扫描电镜(SEM)、能量分散光谱法(EDS)、X射线衍射术(XRD)等手段分析了TiAlCN涂层的表面-界面形貌、化学元素分布和物相特性,并对其界面结合机理进行了探讨.结果表明,Al原子第一电离能低于Ti原子,容易从靶材上气化电离出来沉积在基体上,使得涂层中Al元素含量较高;涂层中TiN、AlN和AlTiN为硬质相,其中涂层中高含量的Al原子有利于提高抗磨损性能,无定形C原子有利于降低摩擦系数;Ti、Al、C、N等原子在涂层中产生富集现象,在结合界面处发生扩散,是形成冶金结合的主要机制.另外,用划痕法测得涂层界面结合强度为76.9N,具有较高的抗剥落能力.文中的结果为TiAlCN涂层在冷作模具表面改性处理中的应用提供了实验基础.【期刊名称】《光学精密工程》【年(卷),期】2014(022)005【总页数】7页(P1260-1266)【关键词】TiAlCN涂层;阴极弧离子镀;线扫描;面扫描;结合强度【作者】孔德军;付贵忠;郭皓元【作者单位】常州大学机械工程学院,江苏常州213016;常州大学机械工程学院,江苏常州213016;常州大学机械工程学院,江苏常州213016【正文语种】中文【中图分类】TB431 引言过渡金属氮化物涂层通常采用电弧离子镀和物理气相沉积(Physical Vapor Deposition,PVD)方法制备,这类涂层包括TiN、Cr N、Cr CN、Al-TiN等。

TiN涂层的最高工作温度为500℃,硬度达到2 200 Hv[1],与钢的摩擦系数为0.6,由于其抗氧化温度不高,只能在普通的工作温度下使用,因此,TiN涂层正逐渐被性能更好的Al-TiN涂层所取代。

Al TiN涂层的抗氧化温度高达800℃,硬度达到3 300 Hv,可满足较高工作温度的要求,但由于Al元素的加入提高了Al-TiN涂层的摩擦系数[2],与钢的摩擦系数上升至0.7,会加剧涂层的磨损。

Effect of laser welding process parameters on microstructure and mechanical properties on butt joint

Effect of laser welding process parameters on microstructure and mechanical properties on butt joint

Effect of Laser Welding Process Parameters on Microstructure and Mechanical Properties on Butt Joint of New Hot-Rolled Nano-scale Precipitation-Strengthened SteelMin Zhang •Xiaonan Wang •Guangjiang Zhu •Changjun Chen •Jixin Hou •Shunhu Zhang •Hemin JingReceived:3April 2014/Revised:11May 2014ÓThe Chinese Society for Metals and Springer-Verlag Berlin Heidelberg 2014Abstract A 4kW fiber laser was chosen to weld the new hot-rolled nano-scale precipitation-strengthened steel with a thickness of 4.5mm.The effect of laser power,defocusing distance,and welding speed on the welded joint appearance was examined,and the microstructure and mechanical properties on the typical butt joints were investigated.Results showed that increasing laser welding power may cause faster downward flow of molten metal to produce greater root humping.With the welding speed increasing,the average welding seam (WS)width decreased,and the average WS and heat-affected zone (HAZ)hardness increased.The microstructures of WS,fusion line,and coarse grain heat-affected zone were lath martensite,but the growth direction of the original austenite grain boundaries was significantly different.The microstructures of fine grain heat-affected zone were ferrite and martensite,and the microstructure of mixed grain heat-affected zone contained ferrite,massive M/A island,and a small amount of martensite.The micro-hardness values of WS,HAZ,and base metal (BM)were 358,302,and 265HV,respectively.The butt joint fracture at the BM far from the WS and the welded joint tensile strength are observed to follow proportional relationship with hardness.KEY WORDS:Laser welding;Microstructure;Mechanical properties;Microalloyed steel1IntroductionHot-rolled advanced high-strength steels have received high attention due to the continuing need for vehicle weightreduction and improved safety due to their high strength and ductility [1,2].Hot-rolled high-strength steel is com-monly referred to hot-rolled dual phase,hot-rolled bainitic steel,hot-rolled transformation-induced plasticity,complex phase steel,nano-scale precipitation-strengthened steel [3–5],and martensitic steels which are characterized as steels with a yield strength [300MPa and a tensile strength [600MPa [6].In general,the design idea of the chemical composition of nano-scale precipitation-strengthened steel is mostly adopted,and single or combined microalloy elements such as Mo,Cr,Ni,Nb,V,Ti,etc.are added,which play the role of the grain refinement and precipita-tion strengthening;the microstructure of nano-scale pre-cipitation-strengthened steel is mainly 2–5l m ferrite grain and \20nm microalloy carbonitride in ferrite matrix.700MPa grade hot-rolled ultra-high strength steel is one of the typical nano-scale precipitation-strengthened steel,namely nano-scale precipitation-strengthened steel (NPS steel)[7,8].The strengthening mechanism of the NPS steelAvailable online at /journal/40195M.Zhang ÁC.ChenLaser Processing Research Center,School of Mechanical and Electrical Engineering,Soochow University,Suzhou 215021,ChinaX.Wang (&)ÁJ.Hou ÁS.ZhangShagang School of Iron and Steel,Soochow University,Suzhou 215021,China e-mail:wxn@G.Zhu ÁH.JingSchool of Materials Science &Engineering,Anhui University of Technology,Ma’ansha 243002,ChinaActa Metall.Sin.(Engl.Lett.)DOI 10.1007/s40195-014-0081-zinclude grain refinement strengthening,precipitation strengthening,solid solution strengthening,dislocation strengthening and transformation strengthening,andfine microstructure and a large number of\10nm dispersed (Nb,Ti)C precipitates were obtained,so the NPS steel had excellent mechanical properties and formability.The NPS steels have been successfully used for heavy-duty truck frame and carriage[9].However,the NPS steel belongs to ultra-fine grain steel,the microstructure and mechanical properties of welded joint showed large gradient changes with conventional CO2gas-shielded welding,and fatigue fracture was easily generated in the actual application pro-cess[7].Laser beam has the advantage of high brightness,high directivity,high color,high spatial coherence,etc.,and power density can be up to106W/mm2[10].Compared with the conventional welding technology,laser welding technology has the following advantages:deeper penetra-tion,narrower HAZ,better quality of welded joints,and higher production efficiency[11–14].In the present study, 4.5-mm-thick NPS steels were welded by4kWfiber laser welding,and the laser welding parameters,microstructure,and mechanical properties of the welded joint were studied.Finally,the optimal laser welding process was obtained,and the microstructure and mechanical properties of the optimal welded joints were gradient changed.2Experimental Procedure2.1MaterialIn the present welding experiment,an NPS steel with a thickness of4.5mm was chosen as the welding material. The experimental steel was hot rolled to4.5mm thickness after7passes rolling on the/450two-roll hot-rolling reversing mill.The chemical composition(wt%)and mechanical properties of the experimental steel are shown in Tables1and2.2.2Laser Welding ProcessThe experiments were carried out by a continuous-wavefiber laser(IPG YLS-4000)with a maximum power of4kW,and the laser welding head was mounted on a robotic arm (KUKA KR30HA).The spot diameter of the laser beam was 0.78mm with a focal length of300mm.The ultra-high argon(Ar)was selected as the shielding gas with theflow rate of0.9m3/h.In order to obtain the better laser welding quality quickly and use less material,parameters such as laser power (P),the welding speed(v),and defocusing distance(D f)were chosen to change.The welding parameters used during the experiments are given in Table3.2.3Morphologic ObservationAfter thefiber laser welding,typical cross sections of the samples were cut by electro-discharge machining.Then,the samples were polished and etched with4%nital before being examined by the optical microscope(Carl Zeiss Axio Vert. A1)and the scanning electron microscope(FEI Quanta600).2.4Measurement of Mechanical PropertiesThe micro-hardness of thefiber laser welding joint was performed by micro-hardness tester(HV-1000IS)using a diamond indenter at room temperature of25°C.The micro-hardness gauge was HV,the multiplying power of the objective lens was409,the force was1.961N,and the holding time of the force was10s.The transverse tests were conducted using a universal tensile testing machine(RGM-4100)operated with a crosshead speed of3mm/min.3Results and Discussion3.1Effect of Processing Parameters on Butt JointAppearancesMany important factors can be used to reflect thefiber laser welding quality[15,16].A good welding quality can beTable1Chemical compositions of experimental steel(wt%)C Si Mn P S Al Ti Nb Fe0.1050.20 1.950.0150.0150.050.120.06Bal.Table2Mechanical properties of the experimental steelYield strength(MPa)Tensile strength(MPa)Elongation(%) 66073020Table3Parameters used in the laser welding experiments No.1–7 ser powerP(kW)Welding speed m(m/min)Defocusing distanceD f(mm)1 2.5 1.2-22 3.0 1.2-23 3.5 1.2-24 3.0 1.5-25 3.0 1.8-26 3.0 1.2-37 3.0 1.20M.Zhang et al.:Acta Metall.Sin.(Engl.Lett.)reflected directly from external features,such as the width of the welded butt joint,the penetration depth,the smoothness of the surface appearances,and so on [17].Figure 1shows the surface appearances and cross section images of butt joints at different laser welding powers (P )at a welding speed (v )of 1.2m/min and defocusing distance (D f )of -2mm.When the P is 2.5kW,the neg-ative sides of the fiber laser welding seam (WS)are not in the full penetration statuses,the white arrows zone is incomplete penetration zone (Fig.1a,b,c),and porosity is generated in the WS (Fig.1c).Porosity deteriorates the mechanical properties of welded joints and should be inhibited.These inferior appearances indicate that the laser power may be low and,therefore,should be improved.When the P is 3.0or 3.5kW,the negative sides of the fiber laser WS are in the full penetration statuses (Fig.1d,e,g,h)and there is no porosity in WS (Fig.1f,i).However,comparing Fig.1f with Fig.1i,it can be found that a higher root humping at P of 3.5kW.Laser welding heat input (E )was calculated based on the following equation [18]:E ¼Pv Âd;ð1Þwhere d is the focused laser beam diameter on the sample surface.With increasing of the laser welding,power results in increasing of laser welding line energy and causes adecrease in weld solidification growth rate and cooling rate [18],and the microstructure is obviously coarsened,and the mechanical properties are deteriorated [19].In addition,improving laser welding power may cause faster downward flow of molten metal to produce greater root humping [20].Therefore,to achieve full penetration without defects welded joint of the 4.5-mm-thick NPS steel,the laser power of 3.0kW is preferred.Figure 2shows the surface appearances and cross section images of butt joints at different welding speeds at a laser welding power of 3.0kW and defocusing distance (D f )of -2mm.Full penetration welded joints are achieved at welding speed of 1.2m/min (Fig.2a,b,c),and partial penetration welded joints are obtained at welding speeds of 1.5and 1.8m/min (Fig.2d,e,f,g,h).Moreover,at welding speed of 1.2m/min,the WS widths on the positive and negative surfaces are narrow and uniform.Hence,decrease in the welding speed results in an increase in the penetration depth.According to Eq.(1),decreasing of the welding speed can effectively increase laser welding line energy and improve the penetration [20–22].Therefore,the welding speed of 1.2m/min is determined.Defocusing distance is generally defined as the distance between the focal plane and the specimen surface.According to Eq.(1),the value of defocusing distance determines the spot size and the power density ontheFig.1Typical surface positive and negative appearances (PA and NA)and cross section images of butt joints welded at v =1.2m/min,D f =-2mm,and P ranging from 2.5to 3.5kW:a PA at P of 2.5kW;b NA at P of 2.5kW;c cross section at P of 2.5kW;d PA at P of 3.0kW;e NA at P of 3.0kW;f cross section at P of 3.0kW;g PA at P of 3.0kW;h the NA at P of 3.5kW;i cross section at P of 3.5kWM.Zhang et al .:Acta Metall.Sin.(Engl.Lett.)specimen surface,and also plays an important role in the WS quality [17].Figure 3shows the surface appearances and cross section images of butt joints at different defo-cusing distances (D f )at a laser welding power (P )3.0kW and welding speed (v )of 1.2m/min.Partial penetration welded joints are achieved at defocusing distance of -3mm (Fig.3a,b,c),and full penetration welded joints are achieved without defects at defocusing distance ofFig.2Typical surface appearances and cross section images of butt joints welded at P =3.0kW,D f =-2mm,and v ranging from 1.2to 1.8m/min:a PA at v of 1.2m/min;b NA at v of 1.2m/min;c cross section at v of 1.2m/min;d PA at v of 1.5m/min;e NA at v of 1.5m/min;f cross section at v of 1.5m/min;g PA at v of 1.8m/min;h NA at v of 1.8m/min;i cross section at v of 1.8m/minFig.3Typical surface appearances and cross section images of butt joints welded at P =3.0kW,v =1.2m/min,and D f ranging from 0mm to -3mm:a PA at D f of -3mm;b NA at D f of -3mm;c cross section at D f of -3mm;d PA at D f of -2mm;e NA at D f of -2mm;f cross section at D f of -2mm;g PA at D f of 0mm;h NA at D f of 0mm;i cross section at D f of 0mmM.Zhang et al .:Acta Metall.Sin.(Engl.Lett.)and -2mm (Fig.3d,e,f,g,h,i).Defocusing distance is a key parameter in high power fiber laser welding of stainless steel.Since the welding quality of welded joint is the best when the defocusing distance is a negative value [21],the defocusing distance of -2mm is the best value for 4.5-mm-thick NPS steel.From the above experimental results,it can be found that the most appropriate fiber laser welding parameter combination can be described as follows:the laser power is 3.0kW,the welding speed is 1.2m/min,and the defo-cusing distance is -2mm.3.2Microstructure Evolution and MechanicalProperties of Butt Joint 3.2.1Microstructure EvolutionFigure 4shows the microstructure of laser welding butt joint of NPS steel.The butt joint consists of WS,FL-HAZ,and base metal (BM);the HAZ contained three different regions,namely CG-HAZ,FG-HAZ,and mixed grain heat-affected zone (MG-HAZ),as shown in Fig.4a.The width of laser welding HAZ is only 0.6–1mm,far lessthanFig.4Microstructure of different zones in laser welding butt joint:a OM image of butt joint;b SEM image of WS;c SEM image of CG-HAZ;d SEM image of FG-HAZ;e SEM image of MG-HAZ;f SEM image of BMM.Zhang et al .:Acta Metall.Sin.(Engl.Lett.)conventional CO 2gas-shielded welding HAZ width of 4–5mm [7].The microstructure of BM is mainly ferrite (F)with average grain size of 3–4l m,and a small amount of pearlite (P)and a large number of grain boundary carbides (Fig.4f).The microstructure of MG-HAZ consists of fer-rite,massive M/A island,and a small amount of lath martensite (LM);the average grain sizes of ferrite and M/A island are 3–4and 0.8–1.2l m,respectively (Fig.4e).The microstructure of FG-HAZ is composed of tiny ferrite (F)and a certain amount of LM,and the average grain size of ferrite is 1.5–2.5l m (Fig.4d).Although the micro-structural constituent of WS,FL,and CG-HAZ is LM (Fig.4b,c),the growth direction of original austenite grain boundaries (OAGB)is significantly different.The direction of OAGB in WS and FL has obvious directional charac-teristics,whereas the direction of OAGB in CG-HAZ tends to be straight.The continuous cooling transformation diagram of BMs shows that the butt joint microstructure,depending on the cooling rate,could contain a combination of grain bound-ary ferrite,pearlite,acicular ferrite,bainite,and martensite [4,8].During fiber laser welding,the metal of WS is liq-uefied,then c -Fe is formed with solidification process,and then LM is obtained due to extremely fast cooling rate.Since the fact that the distance from the center of the WS is different,the thermal cycle experiences (the peak temper-ature and cooling rate)of BM are also different.Figure 5shows schematic illustration of CG-HAZ and FG-HAZ microstructure evolution induced by laser welding.For FL and CG-HAZ,the BM near the WS had a high peak tem-perature (greater than the austenitic coarsening tempera-ture),so the original microstructure is completely austenized (Fig.5a).In the subsequent cooling process,since the cooling rates are extremely high (2,000–3,000°C/s)[15,23],carbon and alloy elements inthe austenite do not have enough time to diffuse,and the austenitic structure is fully transformed to martensite at low temperature (Fig.5a).The peak temperature at FG-HAZ reaches the grain refining temperature,resulting in com-plete austenitizing but not coarsening,producing tiny fer-rite and a certain amount of LM after cooling (Fig.5b).Only the high carbon of the original organization partly is austenized in MG-HAZ,so the ferrite,LM,and M/A island are obtained together.In addition,the direction of OAGB in WS near FL has obvious directional characteristics.In the weld pool crys-tallization,comparing with spontaneous nucleation,non-spontaneous nucleation is dominant [24].The energy bar-rier D G for the crystal to nucleate on the substrate is [25]D G ¼4pc 3LC T 2m3D H m D T ðÞ2À3cos h þcos 3h ÀÁ;ð2Þwhere c LC is the surface energy of the liquid–crystalinterface,T m the equilibrium melting temperature,D H m the latent heat of melting,D T the undercooling below T m ,and h is the contact angle.If the liquid can wet the substrate completely,the contact angle h is zero and so is D G .Dur-ing the laser welding NPS steel,the existing BM grains at the FL act as the substrate for nucleation.Since chemical compositions of the liquid metal in the weld pool and substrate are the same,the liquid metal can wet the sub-strate grains (h =0),and the crystals nucleate from the liquid metal upon the substrate grains without difficulties.Epitaxial growth of WS near fusion line and SEM image of laser welding butt joint are shown in Fig.6.In Fig.6a,the arrow in each grain indicates its h 100i direction,and each grain grows without changing its h 100i direction is called epitaxial growth.In Fig.6b,WS and CG-HAZ are weld pool and substrate before crystallizing,respectively.Therefore,the microstructure of WS near fusion line has typical characteristics of epitaxialgrowth.Fig.5Schematic illustration showing CG-HAZ and FG-HAZ microstructure evolution induced by laser welding:a CG-HAZ;b FG-HAZM.Zhang et al .:Acta Metall.Sin.(Engl.Lett.)3.2.2Mechanical PropertiesFigure 7shows the micro-hardness law of NPS steel wel-ded joint at different defocusing distances (D f )at a laser welding power (P ) 3.0kW and welding speed (v )of 1.2m/min.It is seen that the hardness profile exhibited a symmetric characteristic with a higher hardness on the WS and a lower hardness on the BM.For example,at defo-cusing distance of -2mm,the averages of micro-hardness of WS,HAZ,and BM are 358,302,and 265HV,respec-tively.Whereas,in traditional CO 2gas-shielded welding joint,the averages of micro-hardness of WS,HAZ,and BMare 272,259,and 265HV,respectively [7].The micro-hardness of WS and HAZ is higher than that of the BM,because the alloy elements have no time to form the second phase to precipitate due to the extremely high cooling rate,and these elements dissolve to a great degree,which makes solid solution strengthening to occur after the laser welding process.Figure 8displays the effect of welding speed on WS and HAZ average hardness values.Increasing the welding speed from 1.2to 1.8m/min at constant laser power level and defocusing distance causes an increase in the average WS hardness from 358to 385HV and an increase in the average HAZ hardness from 295to 325HV.With increasing the welding speed,the cooling rate was increased [17],more alloy elements were dissolved,andFig.6Epitaxial growth of WS near fusion line [25]a and SEM image of laser welding butt jointbM.Zhang et al .:Acta Metall.Sin.(Engl.Lett.)solid solution strengthening was improved,so the hardness increased.The tensile strength of the welded joint was about 730MPa based on tensile testing,and the tensile stress–strain curve of the butt joint is given in Fig.9.The fracture position is in BM(Fig.10a).Figure10b shows the SEM image of tensile sample fractured surface,there arefine and deep dimples,which indicate that the tensile fracture is a typical ductile fracture.In general,tensile properties of the welded joint depend on their chemical composition and microstructure[26].The strength and hardness of mar-tensite are the highest in all room-temperature micro-structures of the steel.The microstructures of WS and HAZ are all or part of martensite,whereas the microstructure of BM is mainly ferrite,so the tensile testing failure position is in BM.However,in traditional CO2gas-shielded weld-ing joint,the tensile testing failure position is in HAZ[7].Therefore,laser welding can effectively improve the strength of BM and HAZ.In addition,it can found that the welded joint tensile strength is observed to follow pro-portional relationship with hardness[27].4ConclusionsIn this investigation,4.5-mm-thick NPS steel was welded using4kWfiber laser,and the effect of laser welding parameters on welded joint appearance was studied,and the microstructure evolution of welded joint was demon-strated.The main conclusions are as follows:(1)Increase in the welding speed results in a decrease inthe average WS width and causes an increase in the average WS and HAZ hardness.Improving laser welding power may cause faster downwardflow of molten metal to produce greater root humping.For4.5-mm-thick NPS steel,the optimal laser weldingprocess parameters are laser power is3.0kW,weld-ing speed is1.2m/min,and defocusing distance is -2mm.(2)The microstructure of WS,FL,and CG-HAZ wasLM,but the growth direction of the OAGB was significantly different.The microstructure of WS near FL has typical characteristics of epitaxial growth. (3)The microstructure of FG-HAZ was ferrite andmartensite,and the average grain size of ferrite was1.5–2.5l m.The microstructure of MG-HAZ wasferrite,massive M/A island,and a small amount of martensite;the average grain sizes of ferrite and M/A island are3–4l m and0.8–1.2l m,respectively. (4)The micro-hardness values of WS,HAZ,and BMwere358HV,302HV,and265HV,respectively,and the butt joint fracture at the BM was far from theWS.Fig.10Fractured samples after tensile testing a and SEM image of a typical fracture surface bM.Zhang et al.:Acta Metall.Sin.(Engl.Lett.)The welded joint tensile strength is observed to follow proportional relationship with hardness. Acknowledgments This work wasfinancially supported by the National Natural Science Foundation of China(Nos.51305285and 51104110)and the Basic Research Program of Jiangsu Province(Nos. BK20130315and BK20130304).References[1]R.D.K.Misra,H.Nathani,J.E.Hartmann,F.Siciliano,Mater.Sci.Eng.A394,339(2005)[2]M.Olasolo,P.Uranga,J.M.Rodriguez-Ibabe,B.Lopez,Mater.Sci.Eng.A528,2559(2011)[3]S.Kazuhiro,F.Yoshimasa,K.Shinjiro,JFE Tech.Rep.10,19(2007)[4]X.N.Wang,L.X.Du,H.Xie,H.S.Di,D.H.Gu,Steel Res.Int.82,1417(2011)[5]C.Y.Chen,H.W.Yen,F.H.Kao,W.C.Li,C.Y.Huang,J.R.Yang,S.H.Wang,Mater.Sci.Eng.A499,162(2009)[6]Y.L.Kang,Theory and Technology of Processing and Formingfor Advanced Automobile Steel Sheets(Metallurgical Industry Press,Beijing,2009),pp.5–25(in Chinese)[7]X.N.Wang,H.S.Di,C.Zhang,L.X.Du,X.X.Dong,J.Iron.Steel Res.Int.19,64(2012)[8]X.N.Wang,H.S.Di,L.X.Du,Acta.Mater.Sin.48,621(2012)(in Chinese)[9]Y.J.Song,X.N.Wang,Z.G.Xu,J.F.Luo,L.X.Du,J.Mech.Eng.47,69(2011)(in Chinese)[10]H.Serizawa,D.Mori,Y.Shirai,H.Ogiwara,H.Mori,FusionEng.Des.88,2466(2013)[11]L.Quintino,A.Costa,R.Miranda,D.Yapp,V.Kumar,C.J.Kong,Mater.Des.28,1231(2007)[12]S.H.Baghjari,S.A.A.Mousavi Akbari,Mater.Des.43,1(2013)[13]Y.Kawahito,M.Mizutani,M.Katayama,Sci.Technol.Weld.Join.14,288(2009)[14]S.J.Wang,G.L.Qin,Y.H.Su,Acta Metall.Sin.(Engl.Lett.)26,177(2013)[15]M.Sokolov,A.Salminen,M.Kuznetsov,I.Tsibulskiy,Mater.Des.32,5127(2011)[16]W.J.Suder,S.Williams,ser Technol.56,223(2014)[17]L.Zhang,J.Z.Lu,K.Y.Luo,A.X.Feng,F.Z.Dai,J.S.Zhong,M.Luo,Y.K.Zhang,Mater.Sci.Eng.A561,136(2013) [18]H.N.Moosavy,M.R.Aboutalebi,S.H.Seyedein,M.Goodarzi,M.Khodabakhshi,C.Mapelli,S.Barella,ser Technol.57,12(2014)[19]R.Miranda,A.Costa,L.Quintino,D.Yapp,Mater.Des.30,2701(2009)[20]M.J.Zhang,G.Y.Chen,Y.Zhou,S.H.Liao,Mater.Des.53,568(2014)[21]X.Zhang,E.Ashida,S.Katayama,M.Mizutani,Q.J.Jpn.Weld.Soc.27,64(2009)[22]I.J.Pekkarinen,V.Kujanpaa,Phys.Procedia5,517(2010)[23]A.G.Grigoryants,I.N.Shiganov,A.Misyurov,in TechnologicalProcesses of Laser Treatment,ed.by A.G.Grigoryants(Bauman Moscow State Technical University,Moscow,2006), pp.120–127(in Russian)[24]Z.Y.Du,Welding Science Foundation-Materials Welding Sci-ence Foundation(China Machine Press,Beijing,2012), pp.220–225(in Chinese)[25]S.Kou,Welding Metallurgy(Wiley,Manhattan,2002),pp.65–69[26]A.M.Paniagua-Mercado,V.M.Lopez-Hirata,M.L.S.Munoz,J.Mater.Process.Technol.169,346(2005)[27]A.Santillan Esquivel,S.S.Nayak,M.S.Xia,Y.Zhou,Can.Metall.Q.51,328(2012)M.Zhang et al.:Acta Metall.Sin.(Engl.Lett.)。

微波辅助燃烧法制备镁铝尖晶石纳米粉体的研究_英文_

微波辅助燃烧法制备镁铝尖晶石纳米粉体的研究_英文_

第26卷 第5期 无 机 材 料 学 报V ol. 26No. 52011年5月Journal of Inorganic Materials May, 2011Received date: 2010-11-24; Modified date: 2011-01-26; Published online: 2011-03-10Biography: Leila Torkian(1971−), female, PhD, associated professor. E-mail: ltorkian@azad.ac.irArticle ID: 1000-324X(2011)05-0550-05 DOI: 10.3724/SP.J.1077.2011.10815Synthesis of Nano Crystalline MgAl 2O 4 Spinel Powder by Microwave Assisted CombustionLeila Torkian 1, Mostafa M Amini 2, Zohreh Bahrami 3(1. Department of Applied Chemistry, Islamic Azad University, South Tehran Branch, Tehran, Iran; 2. Department of Chem-istry, Shahid Beheshti University, G .C., Tehran, Iran; 3. School of Chemistry, Collage of Science, University of Tehran, Te-hran, Iran)Abstract: Stoichiometric MgAl 2O 4 spinel nanoparticles were synthesized by microwave assisted combustion reactionfrom aluminium nitrate nanohydrate (Al(NO 3)3·9H 2O) and Sol-Gel prepared magnesium hydroxide (Mg(OH)2) in the presence of urea ((NH 2)2CO) as a fuel, in about 20 min of irradiation. X-ray diffraction (XRD) studies reveal that mi-crowave assisted combustion synthesis route yields single-phase spinel nanoparticles with larger crystalline size (around 75 nm) than other conventional heating methods. Scanning electronic microscope (SEM) images show nanoparticles with spherical shape and homogenous morphology. The surface area measurements (S BET ) show crystals with 2.11 m 2/g and 0.0033 mL/g pore volume.Key words: MgAl 2O 4 nanoparticles; spinel; microwave assisted reactionThe magnesium aluminate with spinel structure offers an attractive combination of properties such as high me-chanical strength at high temperature, high melting point (2135℃), high chemical inertness and thermal stability [1-3]. Due to these properties, it is greatly desired as a refractory material [4], humidity sensor [5], catalyst or catalyst support and recently as an excellent transparent ceramic material for high temperature arc-enclosing envelopes and al-kali-metal vapor discharge devices [6]. Nowadays this spinel has owned many applications in metallurgical, chemical, electro technical, catalysis, electronic and glass industries [7-8].Over the last few decades various novel techniques have been applied for the synthesis of MgAl 2O 4 spinel including Sol-Gel [9], spray drying [10], freeze-drying [11], mechanical activation [12], organic gel-assisted citrate process [13]. Al-though wet-chemical techniques have successfully been used for the preparation of pure spinel nanoparticles at rela-tively low temperatures, but have not received much com-mercial attention because of the expensive row materials and multiple processing steps [14-17]. The conventional preparation method of MgAl 2O 4 spinel is to calcine the mixture of metal oxides at elevated temperatures (1625℃ for 2 h), which has disadvantages of large aggregates and inhomogeneous compositions [18-19]. Recent works show combustion synthesis for preparation of binary oxides has many advantages including homogeneity, high purity, for-mation of crystalline oxide powders in shorter time periodsand lower amount of external energy [20-23].In our previous work, the coprecipitation and combus-tion methods were applied to prepare MgAl 2O 4 spinel par-ticles with conventional heating [24]. In this paper, applica-tion of microwave-assisted combustion synthesis tech-nique for preparation of MgAl 2O 4 spinel has been reported and physical properties of the synthesized powders are compared with that of prepared by conventional heating method.1 Experimental procedure1.1 Powder synthesisAnalytical grade aluminum nitrate nonahydrate (Al(NO 3)3·9H 2O), magnesium chloride hexahydrate (MgCl 2.6H 2O) and urea (CH 4N 2O) were purchased from Merck (99%) and were used without further purification. A solid mixture containing aluminum nitrate and Sol-Gel synthesized magnesium hydroxide [25] with n (Al 3+)/ n (Mg 2+)= 1:2 and urea with n (urea)/n (metal) = 5:3 was taken in a pyrex glass dish and after complete mixing was irradiated with microwaves in a domestic microwave oven (National, 1000W, input range 210−230V-ac SOHZ, mi-crowave frequency 2.45GHz).1.2 CharacterizationPhase analysis of the samples was carried out by X-ray diffraction (XRD; Bruker's D8 advance system, Bruker's AXS, GmbH, Germany) using CuK α radiation. The crys-第5期 LeilaTorkian, et al: Instant Synthesis of Nano Crystalline MgAl2O4 Spinel Powder 551tallite size of MgAl2O4 spinel was estimated with the aid of Debye-Scherrer equation (L hkl=Kλ/βhkl cosθ, where K is a constant taken as 1 and βhkl is the integral breadth that depends on the width of the particular (hkl) plane, λ = 0.15406 nm, the wavelength of the CuKα source, and θ is the Bragg's angle) using the XRD data of the spinel (311) reflection[26]. A Micromerities analyzer (Gemini 2375 V4/02 Instrument 1D:1) was used for Brunauer-Emmett- Teller (BET) surface area measurements. The BET surface area was measured by nitrogen physisorption at liquid nitrogen temperature −196℃. Prior to measurements, the samples were evacuated (up to 0.133 Pa) at 180℃ for 2 h.A PHILIPS XL-30 scanning electron microscope (SEM) was used to observe the particle morphology of the syn-thesized and ground spinel powders.2 Results and discussionNanoparticles of magnesium aluminate formed by en-dothermic redox reaction during a microwave assisted combustion method. The combustion reaction can be ex-pressed as follow:2Al(NO3)3·9H2O + Mg(OH)2 + 5CH4N2O → MgAl2O4 + 13N2 + 5CO2 + 29 H2OAluminum nitrate is an oxidizer and urea is a fuel[20-21, 27]. Oxidation valences of the Al, Mg, C, N, O, and H are +3, +2, +4, 0, −2 and +1, respectively[28-30]. Therefore, the total oxidizing and the reducing valences of aluminum nitrate, magnesium hydroxide, and urea become −15, 0 and +6, respectively. In order to obtain maximum energy for the spinel formation reaction, and also balance the total oxidizing and reducing valances in the mixture, the stoichiometric mole ratio (2:1) of the Al(NO3)3·9H2O (total valence ‒15) and Mg(OH)2 (total valence 0) and 5 mole urea are required (2(‒15) + 1(0) + n(+6) = 0 or n = 5).The net enthalpy (∆H, 25℃) of the reaction was calcu-lated from the standard enthalpy of formation (∆H f , 25℃) of products and reactants using the following thermody-namic data: Al(NO3)3·9H2O: −897.38 kcal/mol; Mg(OH)2: −924.5kcal/mol; CH4N2O: 79.7kcal/mol; MgAl2O4: −547.38 kcal/mol; N2: 0 kcal/mol; CO2: −94.05kcal/mol; H2O: −57.79 kcal/mol[31-32]. According to these thermody-namic data the combustion reaction is endothermic (∆H°= 425.77 kcal/mol, 25℃).Within 5 min of irradiation, reaction mixture was con-verted into a clear solution and started to boil. After about 20 min of irradiation, the concentrated mixture solution burst into flames and resulted into a foamy white powder. X-ray diffraction pattern of synthesized powder is shown in Fig. 1. This pattern shows that prepared powders are well crystallized with single-phase spinel structure[33]. Table 1 shows the particle size, BET surface area and pore volume of microwave assisted synthesized MgAl2O4 spinel nanoparticles. The size of particles calculated from XRD peaks by using Scherrer’s formula and the (311) plane was considered for the crystallite size calculation (around 75 nm)[26]. For the purpose of comparison, physi-cal properties of magnesium aluminate spinel nanoparti-cles which were produced by recent various methods, i.e. conventional solid state[34], co-precipitation[24], conventional combustion[24], and microwave-assisted solid-state[14] routes, are listeded in Table 1. Although applying microwave ir-radiation results in formation of spinel powders with larger crystallite size, smaller BET surface area and pore volume than other traditional methods, it reduces the duration of whole preparation process. In the conventional solid-state methods metal oxide powders must be milled, granulated, dry-pressed in the form of pellets and sintered at 1625℃ for at least 2h[34-35]. Furthermore, most times mineral-izer[36], additives like ZnO[37] or sintering aids as AlCl3[7, 38] are required. Applying coprecipitation and also conven-tional combustion methods are also require sintering Fig. 1 X-ray diffraction pattern of MgAl2O4 spinel nanoparticlesTable 1 Physical properties of MgAl2O4 spinel nanoparticles produced by the various methodsMethods BET surface area /(m2·g−1)Crystallite size a /nm Pore volume /(mL·g−1) ReferencesMicrowave combustion 2.1 75 0.0033 This workConventional solid state 8.1 44 − [34] Coprecipitation 8.1 15 0.0313[24] Conventional combustion 28.2 27 0.0436 [24]Microwave solid state 36.0 66 −[14]a MgAl2O4 crystallite size is calculated from (311) plane[26]552 无机材料学报第26卷at high temperatures, i.e. 1000℃ for 2 h[24, 39]. In micro-wave assisted solid-state method carbon black has been added to metal oxides as a microwave susceptor up to 50wt% (after activation at 550℃ for 6 h) and also SiC are used as a bottom plate. These precursors must be irradi-ated by microwave for 60 min in order to magnesium alu-minate spinel to form[14]. According to Ganesh et al., a solid mixture of metal nitrates and urea as a fuel will pro-duce the nanoparticles of spinel in 45 min microwave ir-radiation[40]. It seems that replacing magnesium nitrate by active magnesium hydroxide decreased the irradiation time for more than 55% in this work.It is well known that heating mechanism in microwave processing is fundamentally different from conventional processing. Microwave radiation is absorbed and con-verted rapidly to thermal energy from inside the material and therefore a dramatic decrease of processing time and energy consummation will result[41]. Therefore, by apply-ing microwave irradiation and replacing active magnesium hydroxide as a precursor instead of magnesium oxide or nitrate in this combustion method, the time duration for preparation of spinel nanopowders is decreased and elec-trical heating and sintering process is omitted. This method can be regarded as an effective and economic method for preparation of spinel due to its convenient process, simple experimental setup, significant time and energy saving and high purity products. Therefore, this method should be considered as an alternative route for the fabrication of MgAl2O4 nanopowder.Generally, increasing temperature treatment due to the sintering process increases the crystallite sizes of pow-ders[42-45]. Therefore, it can be concluded that microwave assisted combustion synthesized spinel powders are ex-posed to higher temperatures than conventional heating prepared powders. According to the SEM image (Fig. 2) microwave-assisted combustion synthesized sample has spherical shape with homogenous morphology.Fig. 2 SEM image of MgAl2O43 ConclusionMgAl2O4 spinel nanoparticles can be prepared by mi- crowave-assisted combustion method and applying syn-thesized magnesium hydroxide as a reagent in 20 min. Spinel nanoparticles synthesized through this method are exposed to higher temperatures than conventional heating methods and have larger crystallite size (around 75 nm). This method is technically simple, cost effective and time- and energy-saving compared with conventional heating methods.AcknowledgementThe authors thank the Offices of the Vice-President for Research Affairs of South Tehran Branch of Islamic Azad University and also Shahid Beheshti University for sup-porting this work.References:[1] Pati R K, Pramanik P. Low-temperature chemical synthesis ofnanocrystalline MgAl2O4 spinel powder. Journal of the American Ceramic Society, 2000, 83(7): 1822−1824.[2] Salmans J, Galicia J A, Wang J A, et al. Synthesis and characteri-zation of nanocrystallite MgAl2O4 spinels as catalysts support.Journal of Materials Science Letters, 2000, 19(12): 1033−1037. [3] Li G J, Sun Z R, Chen C H, et al. Synthesis of nanocrystallineMgAl2O4 spinel powders by a novel chemical method. Materials Letters, 2007, 61(17): 3585−3588.[4] Mohapatra D, Sarkar D. Preparation of MgO-MgAl2O4 compositefor refractory application. Journal of Materials Processing Tech-nology, 2007, 189(1/2/3): 279−283.[5] Gusmano G, Montesperelli G, Traversa E, et al. Microstructure andelectrical properties of MgAl2O4 thin films for humidity sensing.Journal of the American Ceramic Society, 1993, 76(3): 743−750. [6] Li J G, Ikegami T, Lee J H, et al. Fabrication of translucent magne-sium aluminium spinel ceramics. Journal of the American Ceramic Society, 2000, 83(11): 2866−2868.[7] Ganesh I, Bhattacharjee S, Saha B P, et al. A new sintering aid formagnesium aluminate spinel. Ceramics International, 2001, 27(7):773−779.[8] Adak A K, Sahanthe S K, Pramanik P. Synthesis and characteriza-tion of MgAl2O4 spinel by PV A evaporation technique. Journal of Material Science Letters, 1997, 16(3): 234−235.[9] Naskar M K, Chattarjee M. Magnesium aluminate (MgAl2O4)spinel powders from water-based sols. Journal of the American第5期 LeilaTorkian, et al: Instant Synthesis of Nano Crystalline MgAl2O4 Spinel Powder 553Ceramic Society, 2005, 88(1): 38−44.[10] Bickmore C R, Waldner K F, Treadwell D R. Ultrafine spinelpowders by flame spray pyrolysis of a magnesium aluminum dou-ble alkoxide. Journal of the American Ceramic Society, 1996, 79(5): 1419−1423.[11] Wang C T, Lin L S, Yang S J.Preparation of MgAl2O4 spinel pow-ders via freeze-drying of alkoxide precursors. Journal of the American Ceramic Society, 1992, 75(8): 2240−2243.[12] Tavangarian F, Emadi R.Synthesis and characterization of purenanocrystalline magnesium aluminate spinel powder. Journal of Alloys and Compounds, 2010, 489(2): 600−604.[13] Montolouillour V, Massior D, Douy A. Characterization ofMgAl2O4 precursor powders prepared by aqueous route. Journal of the American Ceramic Society, 1999, 82(12): 3299−3304. [14] Ganesh I, Srinivas B, Johnson R, et al. Microwave assisted solidstate reaction synthesis of MgAl2O4 spinel powders. Journal of the European Ceramic Society, 2004, 24(2): 201−207.[15] Bhaduri S, Bhaduri S B. Microstructural and mechanical propertiesof nanocrystalline spinel and related composites.Ceramics Inter-national, 2002, 28(2): 153−158.[16] Varnier O, Hovnanian N, Larbot A, et al. Sol-Gel synthesis ofmagnesium aluminate spinel from a heterometallic alkoxide.Ma-terials Research Bulletin, 1994, 29: 479−488.[17] Minani T. Instant synthesis of nanoscale spinel aluminates.Journalof Alloys and Compounds, 2001, 315(1/2): 123−128.[18] Domanski D, Urretavizcaya G, Castro F J, et al. Mechanochemicalsynthesis of magnesium aluminate spinel powder at room tem-perature.Journal of the American Ceramic Society, 2004, 87(11): 2020−2024.[19] Angappan S, Berchmans L J, Augustin C O. Sintering behavior ofMgAl2O4-a prospective anode material. Materials Letters, 2004,58(17/18): 2283−2289.[20] Ganesh I, Srinivas B, Johnson R, et al. Effect of fuel type on mor-phology and reactivity of combustion synthesized MgAl2O4 pow-ders. British Ceramic Transactions, 2002, 101(6): 247−256. [21] Ganesh I, Srinivas B, Johnson R, et al. Effect of preparationmethod on sinterability and properties of nano crystalline MgAl2O4and ZrO2_MgAl2O4 materials. British Ceramic Transactions, 2003, 102(3): 119−128.[22] Reveron H, Gutierrez-Campos D, Rodriguez R M, et al. Chemicalsynthesis and thermal evolution of MgAl2O4 spinel precursor pre-pared from industrial gibbsite and magnesia powder. Materials Letters, 2002, 56(1/2): 97−101.[23] Edwin H Walker, Jr. Owens J W, Etienne M, et al. The novel lowtemperature synthesis of nanocrystalline MgAl2O4 spinel using “gel” precursors. Materials Research Bulletin, 2002, 37(6): 1041−1051. [24] Torkian L, Amini M M, Bahrami Z. Synthesis and characterizationof a nanorefractory dimetaloxide spinel. e-Journal of Surface Sci-ence and Nanotechnology, 2010, 8: 1−3.[25] Xu B, Wei J, Wang H, et al. Nano-MgO: novel preparation and ap-plication as support of Ni catalyst for CO2 reforming of methane.Catalysis Today, 2001, 68(1/2/3): 217−225.[26] Klug H P, Alexander L E. X-ray Diffraction Procedures for Poly-crystalline and Amorphous Materials, 2nd ed., John Wiley and Sons, New York, 1974.[27] Bai J H, Liu J C, Li C F, et al. Mixture of fuels approach for solu-tion combustion synthesis of nanoscale MgAl2O4 powders. Ad-vanced Powder Technology, 2011, 22(1): 72−76.[28] Kambalea R C, Shaikha P A, Haralea N S, et al. Structural andmagnetic properties of Co1-x Mn x Fe2O4 (0≤x≤0.4) spinel ferrites synthesized by combustion route. Journal of Alloys and Com-pounds, 2010, 490(1/2): 568−571.[29] Segadaes A M, Morelli M R, Kiminami R H G A. Combustionsynthesis of aluminum titanate. Journal of European Ceramic So-ciety, 1998, 18(7): 771−781.[30] Jain S R, Adiga K C, Pai V R. A new approach to thermochemicalcalculations of condensed fuel-oxidizer mixtures. Combustion and Flame, 1981, 40: 71−79.[31] Dean J A (Ed.), Lange’s Handbook of Chemistry, 12th ed.,McGraw-Hill, New York, 1979.[32] Lie D R (Ed.), CRC Handbook of Chemistry and Physics. 84th ed.,CRC press, London, 2003−2004.[33] Joint Committee of Powder Diffraction, card Number 1−1157.[34] Ganesh I, Bhattacharjee S, Saha B P, et al. An efficient MgAl2O4spinel additive for improved slag erosion and penetration resis-tance of high-Al2O3 and MgO-C refractories. Ceramics Interna-tional, 2002, 28(3): 245−253.[35] Ganesh I, Reddy G J, Sundararajan G, et al. Influence of process-ing route on microstructure and mechanical properties of MgAl2O4spinel. Ceramics International, 2010, 36(2): 473−482.[36] Chen S K, Cheng M Y, Lin S J. Reducing the sintering temperaturefor MgO-Al2O3 mixtures by addition of cryolite (Na3AlF6). Journal of the American Ceramic Society, 2002, 85(3): 540−544.[37] Ghosh A, Dos S K, Biswas J R, et al. The effect of ZnO additionon the densification and properties of magnesium aluminate spinel.Ceramics International, 2000, 26(6): 605−608.[38] Pacurariu C, Lazau I, Ecsedi Z, et al. New synthesis methods ofMgAl2O4 spinel. Journal of the European Ceramic Society, 2007, 27(2/3): 707−710.[39] Guo J, Lou H, Zhao H, et al. Novel synthesis of high surface areaMgAl2O4 spinel as catalyst support. Materials Letters, 2004, 58(12/13): 1920−1923.[40] Ganesh I, Johnson R, Rao G V N, et al. Microwave-assisted com-554 无机材料学报第26卷bustion synthesis of nano crystalline MgAl2O4 spinel powder. Ce-ramics International, 2005, 31(1): 67−74.[41] Sertkol M, Koseoglu Y, Baykal A, et al. Synthesis and magneticcharacterization of Zn0.7Ni0.3Fe2O4 nanoparticles via microwave- assisted combustion route. Journal of Magnetism and Magnetic Materials, 2010, 322(7): 866−871.[42] Singh R C, Singh M P, Singh O, et al. Influence of synthesis andcalcination temperatures on particle size and ethanol sensing be-havior of chemically synthesized SnO2 nanostructures. Sensors and Actuators B: Chemical, 2009, 143(1): 226−232. [43] Udomporn S, Ananta S. Effect of calcination condition on phaseformation and particle size of lead titanate powders synthesized by the solid-state reaction. Materials Letters, 2004, 58(7/8): 1154−1159.[44] Xu C, Tamaki J, Mura N, et al. Grain size effects on gas sensitivityof porous SnO2-based elements. Sensors and Actuators B, 1991, 3(2): 147−155.[45] Saberi A, Golestani-Fard F, Willert-Porada M, et al. A novel ap-proach to synthesis of nanosize MgAl2O4 spinel powder through Sol-Gel citrate technique and subsequent heat treatment. Ceramics International, 2009, 35(3): 933−937.。

Effect of Sn addition on the microstructure and mechanical properties of Mg–6Zn–1Mn (wt.%) alloy

Effect of Sn addition on the microstructure and mechanical properties of Mg–6Zn–1Mn (wt.%) alloy

Effect of Sn addition on the microstructure and mechanical properties of Mg–6Zn–1Mn (wt.%)alloyFugang Qi a ,⇑,Dingfei Zhang b ,c ,Xiaohua Zhang a ,Xingxing Xu b ,caChina Academy of Engineering Physics,Mianyang 621900,PR ChinabCollege of Materials Science and Engineering,Chongqing University,Chongqing 400045,PR China cNational Engineering Research Center for Magnesium Alloys,Chongqing University,Chongqing 400044,PR Chinaa r t i c l e i n f o Article history:Received 23June 2013Received in revised form 21September 2013Accepted 24September 2013Available online 11October 2013Keywords:Mg–Zn Mg–Sn PrecipitateMechanical propertiesa b s t r a c tThe microstructure and mechanical properties of Mg–6Zn–1Mn alloys with varying Sn contents (0,1,2,4,6,8and 10wt.%)have been examined using optical microscopy (OM),X-ray diffractometer (XRD),scan-ning electron microscopy(SEM),transmission electron microscopy (TEM),hardness test and uniaxial ten-sile test at room temperature,respectively.The samples were prepared by hot-extrusion after casting.The results showed that the as-cast Sn-containing alloys consisted of a -Mg,Mg 7Zn 3,Mn and Mg 2Sn phases.T6treatments could obviously improve the strengths of the as-extruded samples,and the double aged samples exhibited enhanced age-hardening response at an earlier stage compared to the single aged ones.Among them,the 4wt.%Sn containing sample with double peak aging after solution treatment had the highest strengths and moderate elongation.Microstructure characterization indicated that the high-strengths of the peak aged alloys were mainly determined by a synergistic effect on precipitation strengthening of b 01(MgZn 2)and Mg 2Sn precipitates,and the precipitates after double aging were finer than those after single aging.Ó2013Elsevier B.V.All rights reserved.1.IntroductionMagnesium alloys have wide applications in the aerospace,transportation and mobile electronics industries due to their advantages such as low density,high specific strength and stiff-ness,good damping capacity,excellent machinability and good castability [1–4].However,the application of magnesium alloys is still very limited due to the inadequate strength,poor formabil-ity,and high cost of either expensive alloying elements used or special processing technology involved [5–7].Therefore,it is press-ing to develop some low cost and high strength wrought magne-sium alloys for wider applications.Mg–Zn system alloys,which are the most widely used wrought magnesium alloys,have more pronounced response to age harden-ing compared to other magnesium alloys [8–11].The studies on age-hardening and microstructure in this Mg–Zn alloy have been carried out since 1960s [8,9,11–15],and the precipitation sequence from a supersaturated solid solution (SSSS)during aging were re-ported to be [8,9,15,16]:SSSS ?GP zones ?b 01rods,blocks \{0001}Mg ;(MgZn 2)?b 02discs ||{0001}Mg ;laths \{0001}Mg ;(MgZn 2)?b (MgZn or Mg 2Zn 3).Recently,Mg–6Zn–1Mn (wt.%)(ZM61)alloy (hereafter,all compositions are in weight percentsunless stated otherwise),a new promising high-strength magne-sium alloy,has attracted attention due to good castability,excel-lent formability and significant precipitation hardening response [17–20].In our previous study,we reported that T6treatments,especially double aging,could significantly improve the mechani-cal properties of the as-extruded ZM61alloy [17,18].The high-strengths of peak aged ZM61alloy are associated with the precipitation of the rod-shaped transition b 01phase,and double aging promotes the precipitation of b 01phase.Further,the micro-structure and mechanical properties of Mg–x Zn–1Mn alloy were reported [19,20].Accordingly,the Mg–6Zn–1Mn alloy had the best comprehensive mechanical properties.In addition,Mg–Sn alloys are also known as a precipitation-hardening system,which has a relatively high solubility (14.48wt.%)at about 561°C and low solubility at ambient temper-ature [21,22].However,since the Mg 2Sn precipitates forms with a lath-shaped morphology on the (0001)Mg basal planes of the ma-trix,the precipitation hardening response for the Mg–Sn binary al-loy is low [23].Moreover,the peak hardness of Mg–Sn binary alloy occurs after long-term aging,which is not practical for industrial application [23].Sasaki et al.[24–26]reported that a minor addition of Zn can enhance the age-hardening response of the binary alloy by the homogeneous dispersion of the precipitates.It is of great inter-est to explore the possible cumulative effects on precipitation strengthening of MgZn 2and Mg 2Sn precipitates,so as to develop0925-8388/$-see front matter Ó2013Elsevier B.V.All rights reserved./10.1016/j.jallcom.2013.09.156Corresponding author.Tel.:+868163626782.E-mail address:fugangqi@ (F.Qi).1.XRD patterns of the as-cast Mg–6Zn–1Mn–x Sn(x=0,1,2,4,6,8andalloys(the red arrows in thefigure indicate that the intensifying tendency of Mgphase diffraction peak).(For interpretation of the references to colour in thisfigurelegend,the reader is referred to the web version of this article.)micrographs of the as-cast Mg–6Zn–1Mn–x Sn alloys.(a)x=0,(b)x=1,(c)x=2,(d)x=4,(e)x=6,(f)x=as-cast(a)Mg–6Zn–1Mn and(b)Mg–6Zn–1Mn–4Sn alloys,and(c and d)corresponding EDS results of the as-homogenized Mg–6Zn–1Mn–x Sn alloys.(a)x=0,(b)x=1,(c)x=2,(d)x=4,(e)ZG-0.01vacuum induction melting furnace under an Ar atmosphere.The actual chemical compositions of the experimental alloy ingots were analyzed by XRF-800CCDE X-rayfluorescence spectrometer,and the results are shown in Table1. The ingots were then homogenized at330°C for24h followed by the air cooling.Before the ingots were extruded,both the alloy ingots and extrusion die were heated to350°C for60min.The ingots were extruded at350°C with an extrusion ratio of25and a ram speed of2mm/s.Extrusion was conducted under a controlled constant force by a XJ-500Horizontal Extrusion Machine.After extrusion,the extru-sion bars were cooled in open air.Then the extruded bars were solution-treated at 440°C for2h in air atmosphere followed by water quenching(T4).After solution treatment,the following artificial aging treatments(T6)would be divided into sin-gle aging and double aging,respectively.The single aging was carried out at180°C, and the double aging was carried out by pre-aging at90°C for24h,followed by the secondary aging at180°C.Hardness measurements were performed by a micro-Vickers apparatus under a load of50g.The mechanical properties of the as-extruded,single peak aged(180°C/12h) and double peak aged(90°C/24h+180°C/8h)samples were evaluated by tensile tests at room temperature.Tensile tests were carried out using a SANS CMT-5105 electronic universal testing machine.Samples for tensile tests had a cross-sectional diameter of5mm and a gauge length of60mm.the tensile axis paralleled to extru-sion direction and the tests were performed at a cross-heat speed of3mm/min at room temperature.Mechanical properties were determined from a complete 3.Results and discussion3.1.As-cast and as-homogenized microstructuresThe XRD analysis results of the as-cast Mg–6Zn–1Mn alloys with different Sn contents are shown in Fig.1.It can be seen that the Mg–6Zn–1Mn alloy consists of a-Mg,Mg7Zn3and Mn phases, while the alloys with Sn additions consists of four phases,i.e.,a-Mg,Mg7Zn3,Mn and Mg2Sn.It is also evident that the intensity of the Mg2Sn peaks increase with the increasing Sn content.Fig.2shows the optical microstructures of the as-cast alloys with different Sn contents.As shown in Fig.2,the coarse dendritic structure of the as-cast Mg–6Zn–1Mn alloy is generally refined after the Sn addition.The microstructure of the Sn-free alloy mainly consists of a-Mg and eutectic Mg7Zn3phases at the grain boundaries.The addition of Sn leads to the formation of the eutec-tic Mg2Sn phases at the grain boundaries.Furthermore,withHAADF–STEM micrographs of the as-homogenized(a)Mg–6Zn–1Mn and(b and c)Mg–6Zn–1Mn–4Sn alloys,and(d)F.Qi et al./Journal of Alloys and Compounds585(2014)656–666659bright phases includes Mg,Sn and Mn.The bright phase is likely the Mg2Sn phase because the Mg/Sn(in at.%)ratio is approximately 2:1.Fig.4shows the optical microstructure of the as-homogenized alloys with different Sn contents.Discontinuous secondary phases disperse in the alloys,and the secondary phases are identified by means of SEM and EDS.Fig.5a shows the BSE image of the Sn-free 3.2.As-extruded and solution-treated microstructuresMicrostructural changes after the hot extrusion are shown in Figs.6and7.Owing to the deformation and the occurrence of dynamic recrystallization(DRX)during the hot extrusion process, the undissolved blocky eutectic compounds after homogenization treatment are further broken into small particles,which distrib-as-extruded Mg–6Zn–1Mn–x Sn alloys(the extruded direction is horizontal).(a)x=0,(b)x=1,(c)x= 660 F.Qi et al./Journal of Alloys and Compounds585(2014)656–666solution-treated sample consists of a -Mg matrix and Mn phases.For the alloys with Sn content of less than 4%and more than 0%,almost all the secondary phase particles dissolve into the matrix as same as the Sn-free alloy.However,with further increasing Sn content,a lot of undissolved compounds are remained in the matrix.The XRD pattern of the solution-treated Mg–6Zn–1Mn–4Sn alloy is shown in Fig.9d.It is obvious that the solution-treated sample consists of a -Mg matrix,Mn and Mg 2Sn phases.Fig.10a and b shows the BSE and bright-field TEM micrographs in detail of the solution-treated Mg–6Zn–1Mn–4Sn alloy.From the Fig.10,only one spherical phase can be observed.The sizes of these spherical particles range from 10to 70nm,which are randomly distributed within the a -Mg matrix.In addition,No other phases are seen within the a -Mg matrix after solution treatment.Based on XRD result and EDS analysis,we can conclude that the spherical phase is pure Mn particle.3.3.Age-hardening behaviors and peak-aged microstructures Fig.11shows the age-hardening curves of the solution-treated Mg–6Zn–1Mn–x Sn alloys subjected to single aging at 180°C and double aging at 180°C (pre-aging at 90°C for 24h).During the sin-gle aging at 180°C,the hardness of the Mg–6Zn–1Mn alloy in-creases with aging time and reaches a peak hardness after about 12h.The age-hardening curve of the Mg–6Zn–1Mn–4Sn alloy is very similar to that of the Mg–6Zn–1Mn alloy during the single aging,and the time to reach peak hardness is relatively unaffected by the Sn addition.However,the peak hardness increases from 74Hv to 82Hv by increasing the Sn content from 0%to 4%.A slight increase in the hardness for the Mg–6Zn–1Mn alloy is observed by double aging.The peak hardness increases to 85Hv in 8h after starting the secondary aging.The time to reach the peak hardness,8h,is slightly shorter than that for the single aging,12h.Like sin-gle aging,the age-hardening curves of the quaternary alloys are very similar to those of the ternary alloy during the double aging,and the time to reach peak hardness is relatively unaffected bythe Sn addition.Moreover,the peak hardness values increase grad-ually with increasing Sn content.The base hardness for the alloys containing no more than 4%Sn is about 60Hv,while the base hard-ness of the alloys containing more than 4%Sn increases gradually with increasing Sn addition.As mentioned above,almost all the secondary phases for the alloys containing no more than 4%Sn dis-solve into the matrix after solution treatment,while a lot of undis-solved compounds for the alloys containing more than 4%Sn are still remained in the matrix.This suggests that these undissolved compounds after solution treatment mainly contribute to the in-crease of the base hardness.Fig.9b and c and e and f shows the XRD patterns of the Mg–6Zn–1Mn and Mg–6Zn–1Mn–4Sn alloys in single peak aged and double peak aged conditions.As mentioned previously,for the two alloys almost all the Mg–Zn and/or Mg 2Sn phases dissolve into the Mg matrix after solution treatment,which suggests that the uniform solid-solution structure is produced.After T6treatments,MgZn 2precipitates are formed in the Mg–6Zn–1Mn alloy,while the 4%Sn addition bring about the formation of Mg 2Sn precipitates as well as MgZn 2phases as illustrated by XRD patterns.Generally,the MgZn 2precipitation relates to the peak hardness in the Sn-free alloy;while the Sn-containing alloys show a greater magnitude aging response due to a larger amount of precipitations resulting from the Sn addition.Fig.12shows a bright-field TEM and a high resolution TEM (HR–TEM)images of the Mg–6Zn–1Mn–4Sn alloy aged at 90°C for 24h,taken from the [0001]Mg zone axis.This corresponds to the pre-aged condition of the double aging.From the Fig.12a,it can be observed that a number of fine particles ( 9nm)having dark contrast are evenly dispersed in the matrix.The HR–TEM im-age shows a spherical precipitate having 9nm in size in Fig.12b.Clear lattice contrast cannot be seen inside the particle.According to the previous reports [8,27],we can conclude that these fine par-ticles are G.P.zones.Fig.13shows the TEM images of the Mg–6Zn–1Mn–4Sn alloy in single peak aged (180°C/12h)and double peak aged (180°C/8h)(SE)micrographs of the as-extruded (a)Mg–6Zn–1Mn and (b)Mg–6Zn–1Mn–4Sn alloys (the extruded direction of the points indicated in (a and b).conditions.All images are obtained from Fig.13a and b shows the bright-field TEM jected to peak aging by single aging and In both conditions,the microstructure after ner than those after single peak aging.1Mn–4Sn samples have three kinds of Fig.13.One is rod along the [0001]direction second is lying on the (0001)basal plane.studies [8,15,28,29],we can conclude are rod-like b 01and disc-like b 02phases,between the b 01and matrix is coherent,between the b 02and matrix.Therefore as a more enormous impediment to than the b 02precipitate [27].The third is common morphology.In this work,some tates are flaky-like.Fig.13b shows a HR–TEM Mg 2Sn precipitate observed in the single Fourier transform (FFT)pattern obtained taken from the ½11 20 zone axis.Through can be preliminary found that the micrographs of the solution-treated Mg–6Zn–1Mn–x Sn alloys.(a)x =0,(b)x =1,(c)x =2,(d)x =4,(e)x =6,(f)9.XRD patterns of the (a–c)Mg–6Zn–1Mn and (d–f)Mg–6Zn–1Mn–4Sn alloys different states.(a and d)solution-treated,(b and e)Single peak aged at 180°C 12h,and (c and f)double peak aged at 180°C for 8h.[001]Mg2Sn//½11 20Mgand no clear orientation relationshipobserved.It can be concluded there is a certain angle between this Mg2Sn and base level[0001]Mg,otherwise this Mg2Sn phase is ob-served as a rod through the½11 20Mgview direction.Based on the previous studies[21,26],this Mg2Sn precipitate may be parallel to the prismatic plane of the magnesium matrix. many other irregular-shaped Mg2Sn precipitates, is needed to discuss the orientation relationship tates since the reason for this still remains As previously stated,a number of G.P.pre-aging condition.G.P.zones are believed neous nucleation sites for the transitionhigh temperature aging,leading to thetribution offiner precipitates.In addition,like phase for Mg2Sn phase during theand the times to reach the peak hardnessof double peak aging are much shorter than aging,so Mg2Sn precipitates of the doublefiner than those of the single peak agedpeak hardness of the double peak agedthose of single peak aged ones.Furthermore, precipitate b01and b01precipitates occursble peak aged samples than the singleage-hardening is accelerated.In addition,it can be seen that many dispersed in the matrix,which are founditates but not found in disc-like b02precipitates,solution-treated Mg–6Zn–1Mn–4Sn alloy.(a)BSE micrograph and(b)bright-field TEM micrograph,takendiffraction pattern).Fig.11.Age-hardening curves of the Mg–6Zn–1Mn–x Sn(x=0,2,4,6,8and10)alloys subjected to single aging at180°C and double aging at180°C(pre-aging at90°C for24h and secondary aging at180°C).Fig.12.(a)Bright-field and(b)high resolution TEM micrographs of the Mg–6Zn–1Mn–4Sn alloy aged at90°C for24h,taken from3.4.Mechanical propertiesFig.14shows the mechanical properties of the test alloys in the as-extruded,single peak aged (180°C/12h)and double peak aged (90°C/24h +180°C/8h)conditions.It can be seen that Sn addition has a beneficial effect on the mechanical properties of the Mg–6Zn–1Mn alloy.For the as-extruded alloys,the ultimate tensile strength (UTS)and yield strength (YS)increase gradually with increasing Sn content.The alloy containing 4%Sn has the best strengths,i.e.,an UTS of 331MPa and a YS of 272Mpa,which are superior to the commercial high-strength ZK61with an UTS of 305MPa and a YS of 240MPa [30].However,the excessive Sn addi-tion (>4%)results in the decrease of the elongation.As shown in Fig.14,T6treatments result in large increases in the strengths of all the investigated alloys compared to the as-extruded ones.On one hand,with increasing Sn content,the elongation decreases gradually while the UTS and YS significantly increase,and the maximum of the UTS and YS is obtained for the alloy containing 4%Sn.Further increasing Sn content results in a slight reduction of the UTS and YS in the peak-aged conditions.On the other hand,the strengths of the double peak aged samples are higher than that of the single peak aged ones,while the elonga-tions are slightly lower.The mechanical properties of the double peak aged Mg–6Zn–1Mn–4Sn alloy are an UTS of 390MPa,a YS of 378MPa and an elongation of 4.16%,while those of the single peak aged sample are an UTS of 379MPa,a YS of 358MPa and an elongation of 4.24%.These strengths are comparable to those of some T5-treated or T6treated RE-containing magnesium alloys,including Mg–Gd–Y–Zn–Zr [31],Mg–Gd–Y–Nd–Zr [32]and Mg–Y–Sm–Zr [33].The high-strengths of the Mg–Zn–Mn–Sn wrought alloys are mainly determined by grain refinement strengthening and precip-itation strengthening.It is well-known that strengthening via grain size control is particularly effective in magnesium alloys because of the higher Hall–Petch coefficient [34].The strengths of the as-extruded alloys are strongly influenced by the relatively fine grains with an average size of approximately 2.8l m.As shown in Fig.14,the strengths of the as-extruded samples are improved signifi-cantly by the T6aging treatments.After T4treatment,almost all the Mg–Zn and Mg–Sn compounds in the as-extruded alloys with no more than 4%Sn can dissolve into the matrix,which suggests that a uniform and supersaturated solid-solution structure is produced,as shown in Figs.8and 10.Aging the solution-treated samples is necessary so that the fine b 01,b 02and Mg 2Sn precipitates form within the matrix.The precipitate particles act as obstacles to dislocation movement and thereby strengthening the aged alloy.However,when the content of Sn exceeds 4%,some compounds cannot dissolve into the matrix after solution treatment.At subse-quent aging,these undissolved compounds in the matrix will lead to the decrease of the mechanical properties,while they can con-tribute to the increase of the base hardness,resulting in the in-creased hardness values with increasing Sn content.Moreover,the peak hardness of the double peak aged samples is higher than those of the single peak aged ones and the double aging achieves finer microstructure than the single aging,so the strengths of the double aged samples are higher than that of the single agedones.peak aged Mg–6Zn–1Mn–4Sn alloy.(a)Bright-field TEM image of the single peak aged at 180°C for 12h,pattern),(b)HR–TEM image of a Mg 2Sn phase observed in the single peak aged (inset:FFT pattern obtained aged at 180°C for 8h,taken along the ½11 20 zone axis (inset:½11 20 Mgdiffraction pattern)and (d)HAADF–STEM4.ConclusionThe microstructure evolution and mechanical properties of the Mg–6Zn–1Mn–x Sn (x =0,1,2,4,6,8and 10wt.%)alloys subjected to extrusion,single aging and double aging have been investigated by hardness measurements,tensile tests and microstructureanalysis using SEM,XRD and TEM.The following conclusions are obtained:1.The as-cast Mg–6Zn–1Mn alloy mainly consists of a -Mg,Mg 7Zn 3and Mn phases.Sn addition results in the formation of Mg 2Sn phase and the refinement of the eutectic.2.The addition of Sn can clearly improve the mechanical proper-ties of the as-extruded Mg–6Zn–1Mn alloy due to grain refine-ment strengthening.In more detail,with increasing Sn content,the strengths increase gradually while the elongation decreases gradually.3.T6treatments,especially double aging,can markedly improve the strengths of the as-extruded investigated alloys.Among them,the Mg–6Zn–1Mn–4Sn alloy with double peak aging after solution treatment exhibits the highest tensile strength of 390MPa,the highest yield strength of 378MPa and the moder-ate elongation of4.16%.4.The microstructure characterization suggests that the high-strengths of the peak aged alloys are mainly determined by a synergistic effect on precipitation strengthening of the b 01and Mg 2Sn precipitates,and the precipitates of the double aged samples are finer than those of the single aged ones.AcknowledgementsThis work was sponsored by National Great Theoretic Research Project (2007CB613700),National Science &Technology Support Project (2011BAE22B01-3),International Cooperation Project (2010DFR50010,2008DFR50040),Chongqing Science &Technol-ogy Project (2010CSTC-HDLS)and Chongqing Science &Technol-ogy Commission (CSTC2013JJB50006).References[1]A.A.Luo,Int.Mater.Rev.49(2004)13–30.[2]D.Eliezer,E.Aghion,F.H.Froes,Adv.Perform.Mater.5(1998)201–212.[3]J.Wang,S.Gao,P.Song,X.Huang,Z.Shi,F.Pan,J Alloys Comp.509(2011)8567–8572.[4]W.Unsworth,Light Metal Age 45(1987)10–13.[5]Y.Kawamura,K.Hayashi,A.Inoue,T.Masumoto,Mater.Trans.42(2001)1172–1176.[6]D.F.Zhang,H.J.Hu,F.S.Pan,M.B.Yang,J.P.Zhang,Trans.Nonferr.Met.Soc.20(2010)478–483.[7]X.Cao,M.Jahazi,J.P.Immarigeon,W.Wallace,J.Mater.Process.Technol.171(2006)188–204.[8]J.B.Clark,Acta Metall.13(1965)1281–1289.[9]L.Y.Wei,G.L.Dunlop,H.Westengen,Metall.Mater.Trans.A 26A (1995)1705–1716.[10]D.Y.Maeng,T.S.Kim,J.H.Lee,S.J.Hong,S.K.Seo,B.S.Chun,Scripta Mater.43(2000)385–389.[11]J.Chun,J.Byrne,J.Mater.Sci.4(1969)861–872.[12]G.Mima,Y.Tanaka,Mem Fac.Eng.23(1962)93.[13]G.Mima,Y.Tanaka,Aging 1(1971)10.[14]G.Mima,Y.Tanaka,Trans.JIM 12(1971)323–328.[15]X.Gao,J.F.Nie,Scripta Mater.56(2007)645–648.[16]J.Buha,T.Ohkubo,Metall.Mater.Trans.A 39(2008)2259–2273.[17]Q.W.Dai,D.F.Zhang,W.Yuan,G.L.Shi,H.L.Duan,Cailiao Gongcheng (2008)38–42.[18]D.F.Zhang,G.L.Shi,Q.W.Dai,W.Yuan,H.L.Duan,Trans.Nonferr.Met.Soc.18(2008)s59–s63.[19]D.F.Zhang,G.L.Shi,X.B.Zhao,F.G.Qi,Trans.Nonferr.Met.Soc.21(2011)15–25.[20]D.Zhang,X.Zhao,G.Shi,F.Qi,Rare Met.Mater.Eng.40(2011)418–423.[21]C.L.Mendis,C.J.Bettles,M.A.Gibson,C.R.Hutchinson,Mater.Sci.Eng.A 435–436(2006)163–171.[22]T.Massalski,H.Okamoto,Binary Alloy Phase Diagrams,ASM International,Material Park,OH,1990.[23]J.Van Der Planken,J.Mater.Sci.4(1969)927–929.[24]T.T.Sasaki,J.D.Ju,K.Hono,K.S.Shin,Scripta Mater.61(2009)80–83.[25]T.T.Sasaki,K.Oh-ishi,T.Ohkubo,K.Hono,Scripta Mater.55(2006)251–254.[26]T.T.Sasaki,K.Oh-ishi,T.Ohkubo,K.Hono,Mater.Sci.Eng.A 530(2011)1–8.[27]K.Oh-ishi,K.Hono,K.S.Shin,Mater.Sci.Eng.A 496(2008)425–433.[28]L.Y.Wei,G.L.Dunlop,H.Westengen,Metall.Mater.Trans.A –Phys.Metall.Mater.Sci.26(1995)1947–1955.Fig.14.Mechanical properties of the as-extruded,single peak aged (180°C/12and double peak aged (90°C/24h +180°C/8h)Mg–6Zn–1Mn–x Sn (x =0,1,2,4,6,and 10)alloys.(a)Tensile strength,(b)yield strength,and (c)elongation.Compounds 585(2014)656–666665[29]A.Singh,A.P.Tsai,Scripta Mater.57(2007)941–944.[30]Z.Yang,J.Li,J.Zhang,G.Lorimer,J.Robson,Acta Metall.Sin.(Engl.Lett.)21(2008)313–328.[31]X.B.Liu,R.S.Chen,E.H.Han,J.Alloys Comp.465(2008)232–238.[32]K.Zhang,X.-g.Li,Y.-j.Li,M.-l.Ma,Trans.Nonferr.Met.Soc.18(Suppl.1)(2008)s12–s16.[33]D.Q.Li,Q.D.Wang,W.J.Ding,Mater.Sci.Eng.A–Struct.Mater.Prop.Microstruct.Process.448(2007)165–170.[34]J.Bohlen,P.Dobron,J.Swiostek,D.Letzig,F.Chmelik,P.Lukac,K.U.Kainer,Mater.Sci.Eng.A462(2007)302–306.666 F.Qi et al./Journal of Alloys and Compounds585(2014)656–666。

氮含量对纯钛表面类金刚石薄膜内应力与附着力的影响

氮含量对纯钛表面类金刚石薄膜内应力与附着力的影响

氮含量对纯钛表面类金刚石薄膜内应力与附着力的影响张艺君;张翼;尹路【摘要】目的:采用脉冲电弧离子镀膜法于不同氮含量条件下在纯钛表面制备类金刚石膜(DLC)以观察对薄膜内应力和附着力的影响.方法:在四种氮含量条件下纯钛表面制备类金刚石薄膜,利用扫描电镜观察分析不同氮含量下薄膜的表面形貌及能谱分析薄膜成分,显微压痕仪对比分析不同氮含量对薄膜厚度和硬度的影响.结果:薄膜中氮含量与氮气甲烷流量比成正比,当氮含量达到9.6%时,薄膜性能最稳定.氮掺入DLC薄膜后,改变了薄膜的微观结构,产生几十纳米量级的颗粒.SEM、XPS分析表明纳米颗粒是富氮的非晶氮化碳CNx结构.DLC/CNx致密的纳米复合结构,减小薄膜的内应力,提高薄膜对衬底的附着力.结论:氮含量的增加会形成DLC/CNx致密的纳米复合结构,减小薄膜的内应力,提高薄膜对衬底的附着力.【期刊名称】《口腔颌面修复学杂志》【年(卷),期】2014(015)002【总页数】5页(P96-100)【关键词】纯钛;类金刚石;表面改性;压痕实验【作者】张艺君;张翼;尹路【作者单位】厦门市仙岳医院口腔科福建 361012;解放军第一七四医院口腔科福建 361003;厦门市口腔医院修复科福建 361003【正文语种】中文【中图分类】R783.1纯钛作为理想的义齿支架材料已广泛应用于口腔修复领域。

但由于铸造工艺局限,会出现耐磨性差,金属离子析出,卡环折断等缺陷,这些都需要对纯钛进行表面改性来解决。

类金刚石薄膜(DLC)作为上世纪60年代发展起来的新兴工业材料已得到广泛应用,而在口腔修复中应用较少,主要是其自身存在诸多问题,如内应力较高,附着力偏低,易剥脱等[1,2]。

人们在研究类金刚石(DLC)薄膜掺氮的过程中发现,随着氮含量的增加,薄膜中的内应力下降,从而提高了DLC薄膜与基底材料之间的附着力。

Mikami等[3]认为这是DLC薄膜中氢原子含量降低所致。

Franceschini[4]指出,在DLC薄膜中掺入氮降低薄膜的内应力是sp3氮键替代了DLC薄膜中的sp2键碳所致。

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Effect of La Doping on Microstructure and Critical Current Density ofMgB2Chandra Shekhar a, Rajiv Giri a, R S Tiwari a, D S Rana b, S K Malik b and O N Srivastava a*a Department of Physics, Banaras Hindu University, Varanasi 221005, Indiab Tata Institute of Fundamental Research, Mumbai-400005, IndiaAbstractIn the present study, La-doped MgB2superconductors with different doping level (Mg1-x La x B2; x=0.00, 0.01, 0.03 & 0.05) have been synthesized by solid-state reaction routeat ambient pressure. Effect of La doping have been investigated in relation to microstructural characteristics and superconducting properties, particularly intragrain critical current density(J c). The microstructural characteristics of the as synthesized Mg(La)B2 compounds were studied employing transmission electron microscopic (TEM) technique. The TEM investigations reveal inclusion of LaB6 nanoparticles within the MgB2 grains which provide effective flux pinning centres. The evaluation of intragrain J c through magnetic measurementson the fine powdered version of the as synthesized samples reveal that J c of the samples change significantly with the doping level. The optimum result on J c is obtained forMg0.97La0.03B2 at 5K, the J c reaches ~1.4x107A/cm2 in self field, ~2.1 x 106A/cm2 at 1T, ~2.5x 105A/cm2 at 2.5T and ~1.8 x 104 A/cm2 at 4.5T. The highest value of intragrain J c inMg0.97La0.03B2 superconductor has been attributed to the inclusion of LaB6 nanoparticleswhich are capable of providing effective flux pinning centres.PACS : 74.70Ad; 74.25Sv; 74.62Dh; 74.25HaKey words : superconductor, nanoparticle, intragrain J c*Corresponding authorE-mail: hepons@, girirajiv_bhu@IntroductionThe discovery of superconductivity at 40K in MgB2 by Nagamatsu et al. [1] has generated a great deal of excitement in both fundamental and practical investigations of this material. One advantage of MgB2 is in regard to its applications at comparatively higher temperatures (20-30K) region, where the conventional superconductors can not operate. Also, the progress in cryogen free cooling technique at temperature region of 20-30K will promote the development and application of MgB2. Another important aspect in MgB2 bulk material is that supercurrent flow is largely unhindered by grain boundaries (GBs) [2,3], thus providing a high feasibility of scaling up the material to form bulk shapes like wire and tapes. For widespread applications of MgB2 high value of critical current density in higher magnetic field is required and hence need of adequate flux pinning centres is evident. The effective flux pinning is known to occur when core of fluxoids find higher density normal materials to sit on. Strong pinning centres prevent flux melting and the consequent creep. If local structural perturbations are strong and these are isolated, they can act as effective flux pinning centres provided that their sizes are compatible with the coherence length (~6nm). Unfortunately, the bulk materials prepared at ambient pressure always show lower J c value due to poor grain connectivity, low density and poor flux pinning [4,5]. It is found that most efficient techniques used to fabricate high quality MgB2 samples are hot-isostatic pressing and uniaxial hot pressing at high pressures [6,7]. Also, proton and neutron irradiation are applied to enhance J c properties in MgB2 superconductors [8,9]. However, these techniques are not suitable for the preparation of MgB2 wire and tapes because of their complicated nature and the practical difficulty in the use of very large vessels and dyes in case of high temperature and high pressure. On the other hand, it is reported that chemical doping is effective to increase J c in high-T c cuprates superconductors [10]. Similar techniques have been also utilized for the MgB2 materials. Recently Dou et al. [11] and Matsumoto et al. [12] have synthesized MgB2 superconductor in bulk form at ambient pressure through doping of SiC and SiO2 & SiC respectively. They have reported enhancement of flux pinning properties due to nano inclusion of SiC (10-100 nm) into MgB2 grains. Many groups have been trying to improve the J c by chemical doping. At 20K, pure MgB2 generally has a intragrain J c of about 104 A/cm2 under 1T and irreversible field (H irr) is about 4T [7, 13,14]. It may be pointed out that the estimation of J c ~104 A/cm2 (at 1T and 20K) is for undoped samples devoid of any flux pinning centers. However, when doping is done to produce flux pinning centers, this estimate generally become ~105 A/cm2 (at 1T and 20K) [15-18]. The Ti doping (few to ~10atomic%) in MgB2 has been known to enhance intragrain J c (evaluated through magnetization measurement and using Bean’s formula) values upto 105 A/cm2 under 1T and H irr near 5T at 20K with small T c reduction [15, 16]. Shu-Fang Wang et al. [17] have reported that J c increases up to 5 x 105 A/cm2 at 5K and in self field for Cd doped MgB2. Rui et al. have reported enhancement of J c by adding nano-alumina (10-50nm) into MgB2[18]. It should be pointed out that the above authors have used Bean’s formula to estimate intragrain J c. Recently doping of Al, Fe, Au, Pb into MgB2 have been reported for improvement of flux pinning centres and consequently enhancement in intragrain J c values [19-22]. To date, two important factors of low density and poor flux pinning are main obstacles to obtain high J c value in MgB2 superconductor. Therefore, it is necessary to carry out further research by addition and doping of suitable elements into MgB2 to understand the mechanism of the flux pinning in MgB2 and eventually realize the widespread applications of MgB2. It is known that microstructural features affect crucially the critical current density of superconducting materials. Therefore, in order to explore the microstructural characteristics and its possible correlation with superconducting properties, particularly J c, in the present paper, we have studied structural, microstructural characteristics of the as synthesized Mg1-x La x B2 (0.00≤x≤0.1) samples employing transmission electron microscopic (TEM) technique. TEM investigation reveals nanoparticle LaB6 inclusions within the MgB2 grains.The intragrain critical current density (J c) evaluated through magnetic measurement for sample with various compositions have been found to vary significantly e.g. J c of Mg0.97La0.3B2 sample is ~2.1 x 106 A/cm2 and for Mg0.99La0.01B2 sample, it is ~6.5x105A/cm2 at 5K and 1T. A correlation between intragrain J c and details of the microstructure has been shown to exist. The Mg0.97La0.3B2 sample which possesses the highest intragrain J c ~1.4x107A/cm2 in self field at 5K exhibits LaB6 nanoparticle in the MgB2 grains.Experimental detailsThe synthesis of La doped MgB2 with nominal composition of Mg1-x La x B2 (0.00≤ x ≤0.1) has been carried out by solid state reaction method at ambient pressure by employing a special encapsulation technique developed in our laboratory. The powders [Mg (99.9%), La (99%) and B (99%)] were fully mixed and were cold pressed (3.0 tons/inch2) into small rectangular pellets (10 x 5 x 1) mm3. Then the pellets of Mg(La)B2 were encapsulated in a Mg metal cover to circumvent the formation of MgO during sinteringprocess. The pellet configuration was put on a Ta boat and sintered in flowing Ar atmosphere in a tube furnace at 600o C for 1h, at 800o C for 1h and at 900o C for 2h. The pellet was cooled to room temperature at the rate of 100o C/h. The pellet was taken out and encapsulating Mg cover was removed. The details of the synthesis were similar as described in our earlier publication [23]. All the samples in the present investigation were subjected to gross structural characterization by X-ray diffraction technique (XRD, Philips PW-1710 CuK α), electrical transport characterization by four-probe technique (Keithley resistivity Hall set-up), the microstructural characterization by transmission electron microscope (Philips EM-CM-12) and elemental composition was determined by energy dispersive X-ray analysis (EDAX, Oxford-ENCA). The magnetization measurements have been carried out at Tata Institute of Fundamental Research (Mumbai, India) over a temperature range of 5-40K employing a physical property measurement system (PPMS, Quantum Design). Intragrain J c (magnetic J c ) was calculated from the height ‘∆M’ of the magnetization loop (M-H) using Bean’s critical state model [24]. It should be pointed out that Bean’s formula leads to the optimum estimate of intragrain J c for superconductors having weakly coupled grains. It is not quite appropriate for bulk MgB 2 superconductors because of strong grain coupling in this material. The magnetization measurements have been carried out on fine ground powders of the as synthesized samples. In the fine powder form, strong coupling is non-existent, the intragrain critical current density can be estimated employing Bean’s formula and using average size of the powder particles. Usually, the particles after grinding of samples may not correspond to singular grains but are as estimated through SEM small agglomerates of nearly spherical shape ( ~5 µm ) covering only few grains. The intragrain J c , therefore, can be estimated by the following formula :J c = ><∆d M 30Where ‘∆M’ is change in magnetization with increasing and decreasing field (in emu/cm 3) and ‘d’ is average particle size (in cm).Results and discussionThe dc magnetic susceptibility (χ) of Mg 1-x La x B 2 (with x=0.01, 0.03, 0.05) superconducting samples are shown in Fig. 1 for 50 Oe field as a function of temperature. The χ-T curve shows diamagnetic onset transition temperature for Mg 0.99La 0.01B 2,Mg0.97La0.03B2 and Mg0.95La0.05B2 samples to be 40K, 39K and 37K respectively. The central aim of the present investigation is to explore the flux pinning centres originating as a result of doping. We first describe various microstructural features induced by different doping levels of La at Mg site of MgB2 compound. Thereafter, evaluation of critical current density through magnetic hysteresis loop and correlation between microstructural features and intragrain J c will be described and discussed. In order to investigate microstructural features of La doped MgB2, we carried out extensive studies of nature of grain boundaries (GBs) and inclusion of secondary particles by employing the technique of TEM, which is considered to be the viable technique for such studies.Fig. 2(a) shows a representative transmission electron micrograph for Mg0.99La0.01B2 compound. The dominant feature resulting from this doping is the occurrence of LaB6 nanoparticles which are found to be invariably present. The selected area diffraction pattern corresponding to TEM micrograph is shown in Fig. 2(b). The slight splitting of diffraction spots reveals the presence of low angle grain boundaries in Mg0.99La0.01B2 compound.Fig. 2(c) represents the TEM micrograph of Mg0.97La0.03B2 compound. The dominant and specific microstructural feature for this compound is the presence of high density of LaB6 nanoparticles within MgB2 grains. The size of these nanoparticles lies in the range of 5-15nm. Among these nano inclusions, those which are compatible with coherence length of MgB2 (~6nm) may work as effective flux pinning centres. The SAD pattern corresponding to TEM micrograph [shown in Fig. 2(d)] reveals the spotty ring pattern. These diffraction rings, which correspond to LaB6 and MgB2, depict the inclusion of LaB6 nanoparticle in MgB2 grains.The TEM micrograph for Mg0.95La0.05B2 revealing the presence of LaB6 nanoparticles (20-35 nm) is discernible from the micrograph Fig. 2(e). It is interesting to note that the size of LaB6 nanoparticle in this compound is bigger than those of the Mg0.97La0.03B2 compound [as shown in Fig. 2(c)] and has low density of nanoparticles. The SAD pattern corresponding to TEM micrograph [shown in fig. 2(e)] reveals hexagonal arrangement of diffraction spots of MgB2 along with square diffraction spots of cubic LaB6. The diffraction spots of the SAD pattern of Mg0.95La0.05B2 [Fig. 2(f)] have been indexed. These results clearly show that with different doping concentration of La at Mg site of MgB2 their microstructural features manifested by the occurrence of LaB6 nanoparticles vary significantly.The magnetization measurements as a function of magnetic fields have been carried out at temperature 5K, 10K, 20K and 30K, for each samples in the powder form. It mayfurther be pointed out that several workers have employed Bean’s formula for the undoped and doped MgB2 samples [7, 21, 25, 26].Keeping the above in view, in the following we will proceed to describe the estimation of J c (intragrain) for the present Mg1-x La x B2 samples as obtained on powder form. The intragrain J c as function of magnetic field at temperatures of 5K, 10K, 20K and 30K for MgB2, Mg0.99La0.01B2, Mg0.97La0.03B2 and Mg0.95La0.05B2 are shown in Fig. 3(a), 3(b), 3(c) and 3(d) respectively. It is clear from J c vs H curves, the intragrain J c of Mg0.97La0.03B2 compound attains the highest value among all the compounds for all temperature and the whole field region upto 5T. This compound contains high density of LaB6 nanoparticles (~5- 15 nm) inclusion into MgB2 matrix. As for example at 5K, the J c of Mg0.97La0.03B2 compound is ~1.4 x 107A/cm2 in self field and ~2.1 x 106A/cm2 at 1T, ~2.5x 105A/cm2 at 2.5T and ~1.8 x 104A/cm2 at 4.5T. For Mg0.99La0.01B2 compound, which is nearly without inclusion of LaB6 nanoparticles, J c values at 5K are ~6.0 x 106A/cm2 in self field, ~6.5 x 105A/cm2 at 1T, ~8.6 x 104A/cm2 at 2.5T and ~5.6 x 103A/cm2 at 4.5T. The intragrain J c values for Mg0.95La0.05B2 compound, having low density of larger LaB6 nanoparticles in comparison to Mg0.97La0.03B2 compound, are also lower than Mg0.97La0.03B2. The J c value for Mg0.95La0.05B2 compound achieves the value of ~1.2x106A/cm2, ~2.6 x 105A/cm2, ~4.4 x 104A/cm2 and ~1.0 x 104A/cm2 at 5K in self field, 1T, 2.5T and 4.5T respectively. Similar variations of J c with magnetic field were also observed at temperatures 10K, 20K and 30K. Table-1 brings out the comparision of intragrain J c values for the undoped and optimally doped MgB2 samples in the self field and various magnetic fields. As can be seen from this table, Jcs for La doped MgB2 sample (Mg0.97La0.03B2) is higher than undoped version for all fields.These results are first of their type for MgB2 superconductors. All the J c data reported here by us are much higher than the best results reported so far for MgB2 bulk materials including those prepared under high pressure (the typical value of J c is ~2 x 104 A/cm2 at 20K and 1T) [7], Ti doped MgB2 (the typical value of J c is ~2 x 106 A/cm2 at 5K and in self field) [15], Cd doped MgB2 (the typical value of J c at 5K and in self field is ~5 x 105 A/cm2) [17] and Au coated MgB2 thin film (the typical value of J c is ~1.22 x 107 A/cm2 at 5K and in self field [21].It may be noticed from the J c vs H behavior of La doped MgB2 samples that J c decreases slowly with increasing magnetic field. This manifests the presence of effective flux pinning centres in La doped compounds. As revealed by microstructural analyses the nanoparticles of LaB6 (which are comparable in size to the coherence length) may beresponsible for high intragrain J c values in the whole range of temperature and magnetic field investigated in the present work.ConclusionIn conclusion, we have successfully synthesized La doped MgB2 compounds by solid-state reaction at ambient pressure employing a special encapsulation technique. In the present investigation exploration of microstructural features induced by doping of La at Mg site of MgB2 compound and its correlation with intragrain critical density (J c) have been carried out. The highest J c value at 5K (~1.4 x 107 A/cm2 in self field, ~2.1 x 106 A/cm2, ~2.5 x 105 A/cm2 and ~1.8 x 104 A/cm2 at field of 1 T, 2.5T and 4.5T respectively), has been obtained for Mg0.97La0.03B2 compound. This enhancement of J c for specific La doping (Mg0.97La0.03B2) has been found to result due to high density of LaB6 nanoparticle inclusions in MgB2 grains which provide effective flux pinning centres.AcknowledgementThe authors are grateful to Prof. A.R. Verma, Prof. C.N.R. Rao, Prof. A.V. Narlikar and Prof. T.V.Ramakrishnan for fruitful discussions. We put our sincere thanks to Dr. N.P. Lalla for his kind help in EDAX measurements. Financial supports from UGC and CSIR are gratefully acknowledged.References[1]Nagamatsu J, Norimasa N, Muranaka T, Zenitani Y and Akimitsu J 2001Nature 410 63[2]Larbalestier D C et al. 2001 Nature 410 186[3]Bugoslavsky Y, Perkins G K, Qi X, Cohen L F and Caplin A D 2001 Nature410 563[4]Finnemore D K, Ostenson J E, Bud'ko S L, Lapertot G and Canfield P C 2001Phys. Rev. Lett. 86 2420[5]Kambara M, Babu N H, Sadki E S, Cooper J R, Minami H, Cardwell D A,Campbell A M and Inoue I H 2001 Supercond. Sci. Technol. 14 L5[6]Serquis A, Liao X Z, Zhu Y T, Coulter J Y, Huang J Y, Willis J O, Peterson DE, Mueller F M, Moreno N O, Thompson J D, Nesterenko V F and IndrakantiS S 2002 J. Appl. Lett. 92 351[7]Takano Y, Takeya H, Fujii H, Kumakura H, Hatano T Togano K, Kito H andIhara H 2001 Appl. Phys. Lett. 78 2914[8]Bugoslavsky Y, Cohen L F, Perkins G K, Polichetti M, Tate T J, William Rand Caplin D 2001 Nature 411 561[9]Eisterer M, Zehetmayer M, Tönies S, Weber H W, Kambara M, Babu N H,Cardwell D A and Greenwood L R 2002 Supercond. Sci. Technol. 15 L9[10]Giri Rajiv, Singh H K, Tiwari R S, and Srivastava O N 2001 Bull. Mater.Sci.24 523[11]Dou S X, Soltanian S, Horvat J, Wang X L, Zhou S H, Ionescu M, Liu H K,Munroe P, and Tomsic M 2002 Appl. Phys. Lett. 81 3419[12]Matsumoto A, Kumakura H, Kitaguchi H and Hatakeyama H 2003 Supercond.Sci. Technol. 16 926[13]Canfield P C, Bud’ko S L and Finnemore D K 2003 Physica C 385 1[14]Jin S, Mavoori H, Bower C and Dover R B van 2001 Nature 411 563[15]Zhao Y, Cheng C H, Feng Y, Machi T, Huang D X, Zhou L, Koshizuka N andMurakami M 2003 Physica C 386 581[16]Anderson Jr N E, Straszheim W E, Bud’ko S L, Canfield P C, Finnemore D Kand Suplinskas R J 2003 Physica C 390 11[17]Shu-fang Wang et al. 2004 J. Superconductivity :Incorporating novelMagnetism 17 (3) 397[18]Rui X F, Chen J, Chen X, Guo W and Zhang H 2004 Physica C, 412 312[19]Berenov A, Serquis A, Liao X Z, Zhu Y T, Peterson D E, Bugoslavsky Y,Yates K A, Blamire M G, Cohen L F, Mac J L and Driscoll M 2004 Supercond. Sci. Technol. 17 1093[20]Gao Y D, Ding J, Chen Q, Rao G V S and Chowdari B V R 2004 ActaMaterialia 52 1543[21]Choi E M, Lee H S, Kim H, Lee S I, Kim H J and Kang W N 2004 Appl.Phys. Lett. 84 82[22]Gu D W, Cai Y M, Yau J K F, Cui Y G, Wu T, Yuan G Q, Shen L J and Jin X2003 Physica C 386 643[23]Shekhar C, Giri R, Tiwari R S and Srivastava O N 2004 Cryst. Res. Technol.39 718[24]Bean C P 1964 Rev. Mod. Phys. 36 31[25]Joshi Amish G, Pillai C G S, Raj P, Malik S K 2001Solid StateCommunication 118 445[26]Serquis A, Liao X Z, Civale L, Zhu Y T, Coulter J Y, Peterson D E andMueller F M 2003 IEEE trans. Appl. Supercond. 13 3068Figure CaptionsFig. 1: Temperature dependence of dc magnetic susceptibility for Mg1-x La x B2 (with x=0.01, 0.03, 0.05)Fig. 2(a): A representative TEM micrograph of Mg0.99La0.01B2 compound. Presence of low density of LaB6 nanoparticles (some of which are marked by →) may benoticed.Fig. 2(b): Selected area diffraction pattern from the region shown in Fig. 2(a). The splitting of spots is due to the presence of low angle grain boundaries.Fig. 2(c): TEM micrograph corresponding to Mg0.97La0.03B2 compound, showing the high density of LaB6 nanoparticles (~5 to ~15 nm) within the MgB2 grains.Fig. 2(d): Selected area diffraction pattern corresponding to micrograph Fig. 2(c) depicts spotty ring pattern which correspond to MgB2 and LaB6.Fig. 2(e): TEM micrograph corresponding to Mg0.95La0.05B2 compound revealing LaB6 nanoparticles which are bigger in size (~20 to ~35 nm) than those found forMg0.97La0.03B2.Fig. 2(f): Selected area diffraction pattern corresponding to micrograph Fig. 2(e) reveals hexagonal arrangement of diffraction spots of MgB2 along with squarediffraction spots of LaB6 which has cubic lattice (marked by →).Fig. 3: Intragrain critical current density (estimated on fine powder version of the samples) as a function of applied magnetic field at a temperature of 5K, 10K,20K and 30K for (a) MgB2 (b) Mg0.99La0.01B2, (c) Mg0.97La0.03B2,(d) Mg0.95La0.05B2, superconductors. Highest critical current density for theMg0.97La0.03B2 compound may be noticed.Table-1Comparision of intragrain J c (A/cm2) at 5K for undoped MgB2 and optimally dopedMg0.97La0.03B2Compositions IntragrainJ c (A/cm2) at 5Kfield 1T 2.5T 4.5T SelfUndoped MgB2 3.0 x 105 9.4 x 104 1.8 x 1048.7 x 1021.4 x 1072.1 x 106 2.5 x 105 1.8 x 104Mg0.97La0.03B2(optimally doped)-5.0x10-4-4.0x10-4-3.0x10-4-2.0x10-4-1.0x10-40.01.0x10-4Fig. 1S u s c e p t i b i l i t y (e m u /g /O e )T(K)101010101010Fig. 3H (tesla)10101010101010101010101010I n t r a g r a i n c r i t i c a l c u r r e n t d e n s i t y (A /c m 2)1010101010。

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