NO在Er2O3/Bi2O3催化剂上的程序升温分解

NOx是造成大气污染的化学物质之一,因此,消除NOx是环境保护的一项重要任务,目前比较成熟的消除NOx工艺是用氨为还原剂和V2O5/TiO2为催化剂的选择催化还原(SCR)法[1],但其成本过高.     

甲壳型液晶高分子的化学结构及其与性能间关系的研究

设计并合成了7种新型甲壳型液晶高分子,研究了液晶基元的化学结构和立体效应对单体及其聚合物液晶性的影响.发现在液晶基元的末端引入极性或可极化的原子基团提高了单体的熔点和液晶相的热稳定性;液晶基元的长径比越大,单体的熔点和清亮点越高;聚合使单体的液晶稳定性增加、液晶相温度范围变宽;侧链液晶基元的极性、刚性和空阻越大,聚合物的玻璃化温度越高;酰胺基团无论是在分子的末端还是在连接部位,都使单体的熔点和聚合物的玻璃化温度提高,但在分子末端时液晶相较稳定,作为中心桥键时不利于液晶相的稳定形成.     

Pt负载钙钛石催化剂上氧空位对CO氧化的促进作用

采用柠檬酸法制备了LaMnO₃、LaFeO₃、La_0.5Sr_0.5MnO₃、La_0.5Sr_0.5FeO₃,通过负载纳米Pt合成了Pt负载钙钛石催化剂,XRD与IR数据表明合成的催化剂具有钙钛石相,TEM数据表明合成的纳米Pt粒径为~3 nm,均匀分散在钙钛石上。在CO氧化反应中,发现钙钛石的氧化-还原性能是影响其活性的重要因素,因而,Mn系钙钛石表现出较高的CO氧化活性。负载纳米Pt后,Fe系钙钛石则显示出更优异的CO氧化活性,CO完全转化的温度从350 ℃降至120 ℃。吸附实验表明钙钛石上氧空位对促进O₂的吸附起着非常重要的作用,也是影响CO低温氧化的重要因素之一。     

MgF2对Mn4+掺杂锗酸盐红色荧光粉发光的影响

3.5MgO·0.5MgF₂·GeO₂∶Mn⁴⁺作为优异热稳定性和良好发光性能的红色荧光粉而被市场应用,然而,该粉体中MgF₂的作用影响机理尚不明晰,阻碍其性能进一步优化和发展。采用高温固相法制备了系列Mn⁴⁺激活的锗酸盐荧光粉,通过对比加入MgF₂、H₃BO₃(助熔剂),研究了该粉体的结构、形貌、发光性能等变化规律,阐明了MgF₂的发光影响作用。研究表明,加入MgF₂、H₃BO₃和不加任何助熔剂时的样品,其最佳烧结温度分别为1 150、1 250和1 350 ℃,上述温度下发光强度均为最佳值,其中加入MgF₂、H₃BO₃的样品在最佳温度处生成了纯相。MgF₂的添加,一方面同H₃BO₃一样作为助熔剂对生成纯相、提高样品结晶度起了积极的作用;另一方面,通过研究分析,确认F^-离子成功掺杂进入晶格,促使样品生成的晶体结构为Mg₁₄Ge₅(O,F)₂₄。加入MgF₂、H₃BO₃在最佳烧结温度的样品的荧光寿命分别为0.93和0.75 ms。     

顶空气相色谱法测定瑞替加滨原料药中残留溶剂

建立了测定瑞替加滨原料药中残留溶剂乙醇、正己烷、四氢呋喃、三乙胺的顶空气相色谱方法。采用氢火焰离子化检测器,以N,N-二甲基甲酰胺为样品溶剂,通过对色谱条件优化,建立了以DB-624为分析柱、110℃为平衡温度、15 min为平衡时间的残留溶剂测定方法。经方法学验证,上述4种溶剂的方法检出限依次为0.007 5%、0.000 48%、0.002 4%、0.01%;峰面积的相对标准偏差均小于2.1%;平均回收率为100%～102%;4种溶剂的线性系数均大于0.995。结果表明,该方法的检测灵敏度高、精密度好、准确度高、线性关系良好,能够满足对瑞替加滨质量的控制要求。将该方法应用于3批瑞替加滨原料药的残留溶剂检测,均只检出乙醇和正己烷,且乙醇和正己烷的最高残留量分别为0.149%和0.022%,均未超出限量规定。     

醋酸酐衍生-气相色谱-质谱联用测定葡萄酒中的糖醇

建立了先采用醋酸酐衍生然后用气相色谱-质谱联用仪检测葡萄酒中糖醇的方法。在葡萄酒中加入吡啶涡旋混合均匀,以5000 r/min (4℃)离心10 min。取上清液过有机滤膜,加入吡啶、醋酸酐衍生。加无水硫酸钠吸水后,经DB-5MS毛细管气相色谱柱分离,在选择离子监测(SIM)模式下进行检测。各目标物在0.019~1.25 mg/L (乳糖醇在0.039~2.50 mg/L)范围内线性关系良好,相关系数(r²)均大于0.99。赤藓糖醇、木糖醇、甘露糖醇、山梨糖醇、半乳糖醇和乳糖醇的定量限(信噪比(S/N)=10)分别为0.17、0.29、0.43、0.46、0.47和2.88 mg/L;检出限(S/N=3)分别为0.05、0.08、0.13、0.14、0.14和1.38 mg/L。在40 mg/L和80 mg/L加标水平下,6种糖醇在葡萄酒基质中的回收率为80.15%~108.75%,相对标准偏差(RSD)为2.16%~6.97%。该方法的灵敏度、准确度和精密度均符合相关的技术要求,适合于葡萄酒中糖醇含量的快速检测。     

磷在氧化锆-碳纳米管复合材料上的吸附研究

采用水热合成法成功制备了氧化锆-碳纳米管复合材料,并研究了对磷的吸附行为。表征结果表明,碳纳米管经氧化锆修饰后仍具备介孔结构;氧化锆粒子可均匀分散在碳纳米管表面。吸附实验结果表明,氧化锆粒子的粒径越小,氧化锆对磷的标化平衡吸附量越高,吸附速率越快。磷在氧化锆-碳纳米管复合材料上的吸附等温线符合Freundlich等温吸附模式,属于优先吸附,吸附动力学可用拟二级动力学模型描述。降低离子强度和溶液pH可促进磷的吸附,共存离子对磷吸附具有抑制作用,影响顺序依次为F->NO3-≈SO42-,其中F-影响最大,NO3-和SO42-次之。     

氮氧化硅反相色谱固定相材料的制备及色谱分离性能评价

硅胶是目前高效液相色谱(HPLC)固定相中应用最为广泛的基质材料,其流动相的最佳使用范围为pH 2～8。在高pH(pH＞8)的流动相条件下,流动相中的氢氧根会进攻硅胶基质表面残余的硅醇基,导致硅胶基质固定相骨架溶解。在前期的研究中,我们将高温氨气处理多孔硅胶微球得到的氮氧化硅材料用作HPLC固定相,氮氧化硅在高pH流动相条件下表现出了较硅胶更高的稳定性。本文利用元素分析对氮氧化硅材料的氮化程度及含氮量进行系统的表征,并考察了氮氧化硅材料在不同pH条件下的静态稳定性。利用十八烷基二甲基氯硅烷试剂对氮氧化硅材料表面进行疏水性修饰,并以元素分析和核磁共振波谱对表面键合氮氧化硅材料进行了表征。考察了不同碳链的烷基苯、酸性化合物、碱性化合物在疏水改性的C₁₈氮氧化硅反相色谱固定相上的色谱分离性能。进一步分别以酸、碱和中性化合物为分析对象,比较了C₁₈-SiON1050(10)与C₁₈-SiO₂色谱保留的差异。     

导数同步荧光法同时测定吲哚-3-乙酸和萘氧乙酸

采用荧光光谱法同时测定混合物体系中萘氧乙酸(BNOA)和吲哚-3-乙酸(IAA)两种植物激素。在pH 8.5的条件下,以水为溶剂,选择Δλ=100 nm,在200～500 nm的波长范围对两者的混合物进行了同步荧光光谱扫描,并做一阶导数处理,对其进行定量分析。BNOA和IAA的线性范围是0.01～0.3μg/mL和0.045～0.64μg/mL,检出限分别为0.003μg/mL和0.012μg/mL。方法用于果蔬中BNOA和IAA的同时检测,效果良好。该法可作为植物激素快速检测方法。     

煤油裂解产物/空气与煤油/空气在宽温度范围内点火延迟的对比研究

Kerosene is an ideal endothermic hydrocarbon. Its pyrolysis plays a significant role in the thermal protection for high-speed aircraft. Before it reacts, kerosene experiences thermal decomposition in the heat exchanger and produces cracked products. Thus, to use cracked kerosene instead of pure kerosene, knowledge of their ignition properties is needed. In this study, ignition delay times of cracked kerosene/air and kerosene/air were measured in a heated shock tube at temperatures of 657–1333 K, an equivalence ratio of 1.0, and pressures of 1.01 × 10⁵–10.10 × 10⁵ Pa. Ignition delay time was defined as the time interval between the arrival of the reflected shock and the occurrence of the steepest rise of excited-state CH species (CH*) emission at the sidewall measurement location. Pure helium was used as the driver gas for high-temperature measurements in which test times needed to be shorter than 1.5 ms, and tailored mixtures of He/Ar were used when test times could reach up to 15 ms. Arrhenius-type formulas for the relationship between ignition delay time and ignition conditions (temperature and pressure) were obtained by correlating the measured high-temperature data of both fuels. The results reveal that the ignition delay times of both fuels are close, and an increase in the pressure or temperature causes a decrease in the ignition delay time in the high-temperature region (> 1000 K). Both fuels exhibit similar high-temperature ignition delay properties, because they have close pressure exponents (cracked kerosene: τ_ign∝P^-0.85; kerosene:τ_ign∝P^-0.83) and global activation energies (cracked kerosene: E_a = 143.37 kJ·mol^-1; kerosene: E_a = 144.29 kJ·mol^-1). However, in the low-temperature region (< 1000 K), ignition delay characteristics are quite different. For cracked kerosene/air, while the decrease in the temperature still results in an increase in the ignition delay time, the negative temperature coefficient (NTC) of ignition delay does not occur, and the low-temperature ignition data still can be correlated by an Arrhenius-type formula with a much smaller global activation energy compared to that at high temperatures. However, for kerosene/air, this NTC phenomenon was observed, and the Arrhenius-type formula fails to correlate its low-temperature ignition data. At temperatures ranging from 830 to 1000 K, the cracked kerosene ignites faster than the kerosene; at temperatures below 830 K, kerosene ignition delay times become much shorter than those of cracked kerosene. Surrogates for cracked kerosene and kerosene are proposed based on the H/C ratio and average molecular weight in order to simulate ignition delay times for cracked kerosene/air and kerosene/air. The simulation results are in fairly good agreement with current experimental data for the two fuels at high temperatures (> 1000 K). However, in the low-temperature NTC region, the results are in very good agreement with kerosene ignition delay data but disagree with cracked kerosene ignition delay data. The comparison between experimental data and model predictions indicates that refinement of the reaction mechanisms for cracked kerosene and kerosene is needed. These test results are helpful to understand ignition properties of cracked kerosene in developing regenerative cooling technology for high-speed aircraft.