导电玻璃负载CuO/V_2O_5复合纳米纤维光电极的制备及光电催化性能

以聚乙烯吡咯烷酮(PVP)为高分子模板剂,乙酰丙酮钒(C_(15)H_(21)O_6V)和三水合硝酸铜[Cu(NO_3)_2·3H_2O]为原料,导电玻璃(FTO)为载体,结合溶胶-凝胶法和静电纺丝技术制备了前驱体纤维,经高温焙烧后得到分布均匀、具有纤维结构的导电玻璃负载的CuO/V_2O_5复合光电极(CuO/V_2O_5/FTO).采用热重-差热分析仪(TG-DTA)、X射线衍射仪(XRD)、扫描电子显微镜(SEM)、透射电子显微镜(TEM)和X射线光电子能谱仪(XPS)等对材料的结构进行表征,以亚甲基蓝(MB)为目标降解物,探讨了合成产物的光电催化性能.结果表明,CuO与V_2O_5能有效形成异质结构,其光电催化活性均比纯V_2O_5有明显提高,并且改变CuO与V_2O_5的比例对光电催化性能有较大影响,其中n(Cu)∶n(V)=1∶1时降解效率最高,达到96%.     

导电玻璃负载Fe_2O_3/ZnO复合光电极的制备及光电催化性能

以聚乙烯吡咯烷酮(PVP)为纤维骨架,乙醇为溶剂,乙酸锌[Zn(CH_3COO)_2·2H_2O]和三乙酰丙酮铁(C_(15)H_(21)O_6Fe)为原料,利用静电纺丝技术结合溶胶-凝胶法制备前驱体纤维,经焙烧后得到不同摩尔比的FTO导电玻璃负载Fe_2O_3/ZnO复合光电极(Fe_2O_3/ZnO/FTO).利用热重-差热分析仪(TG-DTA)、X射线衍射仪(XRD)、扫描电子显微镜(SEM)和X射线光电子能谱仪(XPS)等对材料进行了表征,以亚甲基蓝(MB)为目标降解物,探讨了复合材料的光电催化活性.结果表明,Fe_2O_3与ZnO的复合能够有效构建p-n异质结,利于光生电子和空穴的分离,其光电催化性能较纯ZnO/FTO和Fe_2O_3/FTO均有明显提高;不同n(Fe)/n(Zn)的复合光电极表现出了不同的光电催化活性,在相同催化时间内,当n(Fe)/n(Zn)=1∶1时,Fe_2O_3/ZnO/FTO对MB催化活性最佳,MB的降解率达到97%.     

同轴静电纺丝法制备ZnO/Ag2O纳米纤维材料及其光电催化性能研究

以醋酸锌和乙酰丙酮银为前驱体, 通过同轴静电纺丝和热处理过程在氟掺杂氧化锡(FTO)导电玻璃上制备了ZnO/Ag₂O同轴纳米纤维. 采用X射线衍射(XRD)、 X射线光电子能谱(XPS)、 扫描电子显微镜(SEM)、 透射电子显微镜(TEM)、 拉曼光谱和紫外-可见漫反射光谱(UV-Vis DRS)等手段对材料进行了表征. 以氙灯模拟可见光光源, 亚甲基蓝为目标降解物, 考察了所制备纳米纤维的光电催化活性. 结果表明, 同轴ZnO/Ag₂O纳米纤维具有壳核类似结构(ZnO为壳, Ag₂O为核), Ag₂O与ZnO形成的异质结和杂质能级降低了ZnO的带隙能, 提高了对可见光的利用率. 在可见光下, 与纯ZnO相比, ZnO/Ag₂O具有很强的光电催化能力, 并且Ag₂O的量对同轴纤维光电催化活性影响很大, 在同样光电催化条件下, ZnO/Ag₂O-7同轴纳米纤维的光电催化效果最好, 亚甲基蓝降解率达93%, 动力学常数最大为1.13×10 ^-2 min ^-1.     

Lubricant film flow and depletion characteristics at head/disk storage interface

The characteristics of lubricant film at head/disk interface(HDI) are essential to the stability of hard disk drives. In this study, the theoretical models of the lubricant flow and depletion are deduced based on Navier–Stokes(NS) and continuity equations. The air bearing pressure on the surface of the lubrication film is solved by the modified Reynolds equation based on Fukui and Kaneko(FK) model. Then the lubricant film deformations for a plane slider and double-track slider are obtained. The equation of lubricant film thickness is deduced with the consideration of van der Waals force, the air bearing pressure, the surface tension, and the external stresses. The lubricant depletion under heat source is simulated and the effects of different working conditions including initial thickness, flying height and the speed of the disk on lubricant depletion are discussed. The main factors that cause the lubricant flow and depletion are analyzed and the ways to reduce the film thickness deformation are proposed. The simulation results indicate that the shearing stress is the most important factor that causes the thickness deformation and other terms listed in the equation have little influence. The thickness deformation is dependent on the working parameter, and the thermal condition evaporation is the most important factor.