退火及超声处理对ZnO薄膜结构和发光特性的影响

 利用对向靶射频磁控溅射系统在Si（100）衬底上制备了ZnO薄膜,并对其进行了退火和超声处理。采用XRD,AFM和光致发光谱对其结构、表面形貌和性能进行了分析。结果表明：沉积态ZnO薄膜（002）择优取向稍差,尺寸较小,表面粗糙度较大。随退火温度的升高,颗粒粒径增大,样品的取向性和结晶度都明显变好,应力状态由压应力转变为张应力,粗糙度降低。超声处理缓解了薄膜中的张应力,晶粒尺寸更趋增大;用波长为280 nm的激发光激发薄膜时,沉积态薄膜无发光峰存在;随着退火温度升高,出现了一个378 nm的紫外峰和一个398 nm的紫峰;紫外峰峰值强度随退火温度升高不断增强,而紫峰的峰位随退火温度升高基本不发生变化,峰值强度增强;700 ℃退火后的薄膜经超声处理后,发光谱中出现了峰值波长为519 nm的绿色发光带。     

C(膜)/Si(SiO2)(纳米微粒)/C(膜) 的光致发光性质研究

用直流辉光溅射法结合真空镀膜法制备出了一种“多层三明治结构”的光致发光材料—C(膜 ) /Si(SiO2 ) (纳米微粒 ) /C(膜 )夹层膜 ,然后分别在 40 0、6 5 0和 75 0℃退火 1h .在波长为 2 5 0nm的紫外光激发下 ,刚制备出来未经退火处理的样品具有一个在 398nm (3.12eV)处的紫光宽带PL1峰 .在 6 5 0℃退火后 ,又出现了一个在 36 0nm (3.44eV)附近的PL2 峰 .PL1和PL2 峰形状和峰位与退火温度和激发波长无关 ,但强度却与退火温度和激发波长密切相关 .结合形态结构分析可知 ,紫光PL1峰可用量子限制 -发光中心 (QC LCs)模型进行解释 :即光激发发生在SiO2 微粒内部 ,而光发射源于SiO2 与Si界面上的缺陷中心 .紫外荧光PL2 峰则源自SiC内部的电子 空穴复合发光     

基于GaAs膜的GaInP/AlGaInP无杂质空位扩散诱导量子阱混杂的研究（英文）

在红光半导体激光器芯片上采用GaAs介质膜进行无杂质空位扩散诱导量子阱混杂研究。激光器芯片的有源区由一个9 nm厚的GaInP量子阱和两个350 nm厚的AlGaInP量子垒构成,利用MOCVD方法在芯片表面生长GaAs介质膜。在950℃的情况下进行不同时长不同GaAs层厚度的高温快速热退火诱发量子阱混杂。通过光致发光光谱分析样品混杂之后的波长蓝移情况和光谱半峰全宽变化规律。当退火时间达到120 s时,样品获得53.4 nm的最大波长蓝移;在1 min退火时间下获得18 nm的最小光谱半峰全宽。     

氧压对飞秒激光沉积ZnO/Si(100)薄膜光学性能的影响

利用飞秒脉冲激光沉积法在n-Si（100）单晶衬底上制备了ZnO薄膜, 分析了衬底温度、激光能量、氧压及退火处理对薄膜结构和光学性能的影响. X射线衍射结果表明, 当激光能量为15?mJ、氧压为10?mPa时, 80?℃生长的薄膜取向性最好. 场扫描电子显微镜结果显示薄膜的晶粒尺寸随激光能量的增加而减小、随衬底温度的升高而增大且退火后明显变大. 紫外-可见透射光谱显示薄膜具有90%以上的可见光透过率.光致发光谱表明当氧压为10 mPa时,除了ZnO的紫外本征峰外, 还有一波长为410 nm的强紫光峰, 当氧压增至20 mPa以上, 所有缺陷峰均消失, 只有376 nm处的紫外本征峰. 与纳秒激光法所制备的薄膜特性进行了比较, 结果表明, 虽然纳秒激光沉积所制备的薄膜具有更高的c轴取向度, 但飞秒激光沉积制备的薄膜具有更好的发光性能. 关键词： 氧化锌 飞秒脉冲激光沉积 透过率 光致发光     

α-Al2O3: Mn单晶的三维热释发光谱研究

测量了α-Al2O3: Mn单晶中子辐照前后的三维热释发光谱.观察到α-Al2O3: Mn:Mn单晶γ射线照射后测量的三维热释发光谱中，峰温在350℃波长为680nm处有一宽发光峰，这可能与Mn2+离子有关；波长为695nm峰温在170℃和350℃的线状光谱，叠加在680nm宽发光峰上，是Cr3+离子的发光谱线,其中可能有Mn4+离子的贡献.与纯α-Al2O3单晶的热释发光谱相比，掺入Mn杂质后，γ射线照射的三维热释发光谱中完全地抑制了波长为416nm的α-Al2O3的F心发光峰.经1017cm-2中子注量辐照和退火后，γ射线照射后测量的三维热释发光谱中，在150℃出现了波长为416和695nm的发光峰，以及在250℃波长为680和695nm的发光峰，其中695nm新发光峰的强度略超过了中子辐照前α-Al2O3:Mn在350℃波长为695nm的发光峰，说明中子辐照产生了大量浅陷阱能级和F心.然而，经1018cm-2中子注量辐照和退火后，γ射线照射后测量的三维热释发光谱中，出现了峰温150℃，190℃和250℃波长为520nm的Mn2+离子发光峰，以及300℃波长为680和695nm的Cr3+（或Mn4+）的发光峰，表明增高中子注量的辐照，产生了温度为190℃，250℃和300℃深陷阱能级和F心，并使Mn2+离子发光峰明显加强. 关键词： α-Al2O3:Mn 三维发光谱 缺陷结构 发光机理     

激光波长对拉曼散射水温遥感系统测温精度及探测深度的影响

机载激光拉曼散射雷达技术可以快速获取次表层海水温度的三维分布,具有重要的实用价值和经济价值.首先,从理论上分析了水的伸缩振动拉曼谱峰值位置和半高全宽与激发波长之间的对应关系,发现随着激发波长的增大,拉曼峰逐渐向长波方向移动,且拉曼光谱半高全宽显著增大.然后,实验测量了不同温度下450 nm激光和532 nm激光激发的水的拉曼光谱,对比验证了上述理论分析结果.并采用单高斯峰拟合法分析了两组拉曼光谱,拟合出高斯峰峰值位置与温度之间的关系,分析了激发波长对温度测量精度的影响.研究发现,采用较长波长的激发光可以提高拉曼光谱的测量精度,从而改善测温精度.最后,建立了拉曼散射雷达方程,分析了拉曼散射系数与激光波长之间的关系,研究了激光波长对雷达系统探测深度的影响.结果表明,激光波长对雷达系统探测深度有很大的影响,采用480 nm以下波长的激光时雷达系统探测深度较大,而采用长波段激光时雷达系统探测深度会大幅降低.实际系统设计中选取激光光源时需要综合考虑上述两方面的影响.     

高分子网络凝胶法制备ZnO超细粉体及其光学性能

采用高分子网络凝胶法制备球形ZnO超细粉体。通过聚乙烯醇(PVA)亚浓溶液交联网络的空间位阻作用,经过烧结,获得了具有球形形貌的粒径为1~3μm的ZnO粉体颗粒。利用X射线衍射(XRD)、扫描电镜(SEM)分析了不同PVA浓度以及退火温度对产物形貌、结构的影响,发现在PVA溶液浓度为5%,并且经500℃热处理所形成的ZnO球形颗粒最为均匀规整。研究了球形ZnO粉体的光致发光性能,室温下经325nm波长激发,观察到两个中心波长分别位于407,468nm的微弱的荧光发射带,在合适温度下,在385nm处还出现了较强的紫外峰。PL光谱表明,退火温度对ZnO的光致发光影响较大,随着退火温度升高,由于表面缺陷和结晶性能发生变化,407nm处发射峰逐渐减弱消失,而紫外发光先增强后减弱,经500℃热处理样品的紫外发光性能达到最佳。     

TiO_2-AgNPs表面增强喇曼基底的制备及其活性

采用532nm、632.8nm和785nm三种不同波长激光束,研制适用于各波长的TiO_2-AgNPs基底,检测罗丹明6g(R6g)和健康人血清两种样品的表面增强喇曼光谱(SERSp),并验证不同波长激光激励对SERSp指纹谱的影响.结果表明:当提拉速度达到200mm/min时,TiO_2薄膜光催化活性不再增加;在440℃~600℃范围内,TiO_2晶型均为锐钛矿结构;膜厚、温度及紫外灯照射时间共同影响银粒子生长,200mm/min提拉速度、520℃煅烧温度及紫外光照射80min条件下获得的TiO_2-AgNPs基底具有较好喇曼增强效果;不同波长激励对SERSp各谱线的增强影响明显,在532nm波长激励的SERSp中,大波数的谱峰增强因子明显高于小波数的谱峰,在785nm波长激励的SERSp中正好相反,而在632.8nm波长激励的SERSp中,大、小波数谱峰增强因子比较均一;不同波长激励样品SERSp指纹谱有明显的差异.     

不同退火条件对纳米多孔氧化铝薄膜光致发光的影响

以草酸为电解液,采用二次阳极氧化法制备出了纳米多孔氧化铝薄膜,经不同退火温度和退火气氛处理氧化铝薄膜后,通过分析其光致发光光谱得出：相同的退火气氛中, 退火温度T≤600 ℃ 时,T=500 ℃具有最大的光致发光强度;退火温度T≥700 ℃时,随着退火温度的升高,样品的发光强度增大。在不同的退火气氛中,多孔氧化铝薄膜随着退火温度的升高,发光峰位改变不同,即在空气中退火处理后,随着退火温度的升高,发光峰位蓝移,而在真空中退火处理后,发光峰位并不随退火温度的升高而变化;通过对1 100 ℃高温退火处理后的氧化铝薄膜的光致发光曲线的高斯拟合,可以看出,经退火处理后的多孔氧化铝,主要存在三个发光中心,发光曲线在350～600 nm范围内对应三个发射峰, 发射波长分别为387,410,439 nm。相同的退火温度下,空气中退火得到的氧化铝薄膜的光致发光强度大于真空中退火处理后的氧化铝薄膜。基于实验结果,结合X射线色散能谱(EDS)、红外反射光谱等表征手段,探讨了多孔氧化铝薄膜的发光机制,并对经过不同退火条件得到的多孔氧化铝薄膜的光致发光特性的改变做出了合理的解释。     

退火对非故意掺杂4H-SiC外延材料386 nm和388 nm发射峰的影响

10 K条件下,采用光致发光(PL)技术研究了不同退火处理后非故意掺杂4H-SiC外延材料的低温PL特性.结果发现,在370—400 nm范围内出现了三个发射峰,能量较高的峰约为3.26 eV,与4H-SiC材料的室温禁带宽度相当.波长约为386 nm和388 nm的两个发射峰分别位于~3.21 eV和~3.19 eV,与材料中的N杂质有关.当退火时间为30 min时,随退火温度的升高,386 nm和388 nm两个发射峰的PL强度先增加后减小,且退火温度为1573 K时,两个发射峰的PL强度均达到最大. 关键词： 光致发光 退火处理 能级 4H-SiC     

NOx formation and flame velocity profiles of iso- and n-isomers of butane and butanol

NO formation and flame propagation are studied in premixed flames of iso- and n-isomers of butane and butanol through experimental measurements and direct simulation of experimental profiles. The stabilized flame is realized through the impingement of a premixed combustible jet from a contraction nozzle against a temperature-controlled plate. The velocity field is obtained by means of Particle Image Velocimetry (PIV) and nitric oxide concentration profiles are measured using Planar Laser Induced Fluorescence (PLIF), calibrated using known NO seeding levels. It is found that NO formation in n- and iso-isomers is comparable under the conditions considered, except for rich butanol mixtures, whereby NO formation is higher for iso-butanol. Generally, less NO is formed in butanol flames than in the butane flames. The experiment is simulated by a 1D chemically reacting stagnation flow model, using literature models of C1–C4 hydrocarbons [Wang et al., 2010] and butanol combustion chemistry [Sarathy et al., 2009, 2012]. NO prediction is tested using two of these mechanisms with a previously-published NO_x submechanism added into the butane and butanol models. While a good level of agreement is observed in the velocity field prediction under lean and stoichiometric conditions, discrepancies exist under rich conditions. Greater discrepancies are observed in NO prediction, except for the C1–C4 mechanism which shows good agreement with the experiment under lean and stoichiometric conditions. The current study provides data for further development of mechanisms with NO_x prediction capabilities for the fuels considered here.     

Quantum and surface properties of free films and nanoshells of molecular and atomic thicknesses

An original technology and the properties of new thin film nanoobjects, free films and shells of molecular and atomic thicknesses, are presented. Special attention is paid to shells of monoatomic or monomoleculer thickness with unique surface properties that have not been found in bulk materials.     

Experimental and Theoretical Study of the Electronic States and Spectra of TeH and TeLi

Gas-phase emission spectra of the hitherto unknown free radical TeLi have been measured in the NIR range with a Fourier-transform spectrometer. The emissions were observed from a fast flow system in which tellurium vapor in argon carrier gas was passed through a microwave discharge and mixed with lithium vapor in an observation tube. Two systems of blue-degraded bands were measured at high spectral resolution in the ranges 8000-9000 and 5700-6700 cm(-1) and vibrational and rotational analyses were performed. In order to aid in the analysis of the experimental data, a series of relativistic configuration interaction calculations has been carried out to obtain potential curves for the low-lying states of TeLi and the isovalent TeH and also electric dipole transition moments connecting them. As in the TeH system, the ground state of TeLi is found to be X(2)Pi(i), but with a remarkably smaller spin-orbit splitting. The TeLi calculations indicate a strongly bound A(2)Sigma(+) state, while in TeH the analogous state is computed to lie significantly higher at approximately 32 000 cm(-1), and it is strongly predissociated. Based on the theoretical analysis, the observed TeLi band systems are assigned to the transitions A(2)Sigma(+)(A1/2)-->X(1)(2)Pi(3/2)(X(1)3/2) and A(2)Sigma(+)(A1/2)-->X(2)(2)Pi(1/2)(X(2)1/2). Analysis of the spectra has yielded the molecular constants (in cm(-1)) X(1)(2)Pi(3/2):omega(e)=457.49(3), omega(e)x(e)=2.482(9), B(0)=0.408908(8); X(2)(2)Pi(1/2): T(e)=2353.44(3), omega(e)=456.28(4), omega(e)x(e)=2.635(8), B(0)=0.414954(8), p(0)=1.00637(4); A(2)Sigma(+): T(e)=8574.64(2), omega(e)=437.81(3), omega(e)x(e)=2.581(8), B(0)=0.423903(8), p(0)=-0.19915(2), where the numbers in parentheses are the standard deviations of the parameters. Comparison of the isovalent TeLi and TeH systems emphasizes that the difference in bonding character (ionic in TeLi vs covalent in TeH) is responsible for qualitative differences in the electronic spectra of these two molecules. Copyright 2001 Academic Press.     

Topological dislocation-type defects and mechanisms of plasticity and failure of nanostructured and amorphous materials

Possible mechanisms of plastic deformation and failure of nanostructured and cluster amorphous materials have been considered. It is shown that the most probable carriers of plastic deformation in these materials are macrodislocations—linear topological defects of the regular nanocrystallite packing in the nanostructure or cluster packing in amorphous materials. Continuum models are proposed to describe the processes of plastic deformation and failure of nanostructured and cluster amorphous materials. Original Russian Text ? L.S. Vasil’ev, S.F. Lomaeva, 2009, published in Izvestiya Rossiiskoi Akademii Nauk. Seriya Fizicheskaya, 2009, Vol. 73, No. 1, pp. 128–131.     

Geometry and Elasticity of Strips and Flowers

We solve several problems that involve imposing metrics on surfaces. The problem of a strip with a linear metric gradient is formulated in terms of a Lagrangian similar to those used for spin systems. We are able to show that the low energy state of long strips is a twisted helical state like a telephone cord. We then extend the techniques used in this solution to two–dimensional sheets with more general metrics. We find evolution equations and show that when they are not singular, a surface is determined by knowledge of its metric, and the shape of the surface along one line. Finally, we provide numerical evidence by minimizing a suitable energy functional that once these evolution equations become singular, either the surface is not differentiable, or else the metric deviates from the target metric.     

MCNP-FISPACT耦合燃耗计算程序开发与测试

反应堆堆芯的燃耗计算关系到堆芯的燃料管理,并直接影响堆芯的经济性评估,因此如何快速且准确地对堆芯进行燃耗计算一直是反应堆物理设计的研究重点之一。随着反应堆的发展,其几何结构和物理特性日渐复杂,现有的一维、二维耦合燃耗程序因其在几何处理上的限制,难以满足先进反应堆精细设计分析的要求。为对复杂反应堆堆芯的燃耗情况进行计算,结合粒子输运程序MCNP 处理复杂几何和燃耗程序FISPACT处理核素全面的特点,开发了接口程序耦合MCNP 和FISPACT来进行燃耗计算,并对耦合程序进行了计算验证。采用了IAEA 基准校核例题和CFETR中国聚变工程实验堆例题进行程序验证,经计算得出的有效倍增因子随燃耗的变化曲线和TBR等数据与标准例题的结果符合良好,其误差在可接受范围内。     

Some problems of analysis and optimization of plates and shells

The classical optimization problems of plates and shells to satisfy a priori given geometry and dynamical characteristics are considered. Orthotropic plates and shells with variable thickness and low transverse stiffness are analyzed. First, some useful theorems and their proofs are given. Then the finite approximation of the problem related to optimization of free vibrations of shells with transverse deformation and rotary inertia is discussed. The varational iteration (MVI) and Bubnov-Galerkin (MB) methods are applied, and their convergence and suitability for application to plates and shells analysis are discussed and numerically evaluated.