油浆高温快速裂解过程的气固相产物研究

采用高频炉快速热解装置研究油浆的高温快速热解特性,考察了热解温度、氮气流量对气固相产物的组成和产率的影响。温度是影响气相产物产率的关键因素,气相产物主要为甲烷、氢气和乙烯,升高温度可提高甲烷和氢气的产率,而乙烯产率受高温下二次反应的影响在800℃到达最大值后逐渐降低,乙烷、丙烯产率较小且受二次反应的影响在700℃到达最大值后逐渐降低,温度高于800℃时会有少量乙炔生成且升温可提高乙炔产率。增加氮气流量可降低甲烷、氢气分压,缩短乙烯、丙烯等在高温区的停留时间,从而增加气相产物的产率。积炭产率随热解温度升高迅速增加,氮气流量的增加能够削弱二次反应从而降低积炭产率。     

蔬菜中百菌清及其代谢产物残留的ELISA检测方法研究

以2,4,5-三氯-6-(2-羟基乙氧基)间苯二腈为反应物制备半抗原,利用琥珀酸酐法制备人工抗原。以百菌清-牛血清蛋白(BSA)为免疫原免疫新西兰大白兔,制备特异性兔抗百菌清(CHT)及其代谢产物羟基百菌清(Hydroxy-chlorothalonil,CHT-OH)的多克隆抗体。采用非竞争酶联免疫法(ELISA)以百菌清-卵清蛋白(OVA)偶联物作为包被抗原,当其质量浓度为0.1 mg/L时,测得抗百菌清血清的效价约为1∶1×104。据此建立了百菌清间接竞争ELISA检出方法,并用于蔬菜中百菌清及其代谢产物的残留分析。实验结果表明,该方法对百菌清的检出限(IC20)为0.012 3μg/L,回收率为87%~92%;对其代谢产物的检出限(IC20)为0.019 5μg/L,回收率为105%~111%;总残留量的检测回收率为85%~107%。对百菌清的结构类似物交叉反应率均小于0.01%。ELISA方法的测定结果与高效液相色谱法的测定结果有良好的一致性。建立的方法适合于蔬菜中百菌清和羟基百菌清总残留量的测定。     

尿样中神经性毒剂代谢产物的HPLC/Q-TOF MS/MS检测方法研究

建立了尿样中甲基膦酸单乙酯(EMPA)、甲基膦酸单异丙酯(IMPA)、甲基膦酸频哪基酯(PMPA)3种神经性毒剂代谢产物的HPLC/Q-TOFMS/MS检测方法。以StrataSi-1型固相萃取小柱对尿样中的3种神经性毒剂代谢产物进行分离,HPLC/Q-TOFESIMS/MS进行测定,内标法定量。该方法对EMPA、IMPA、PMPA的线性范围均为5～320μg/L,相关系数均不低于0.9974;EMPA、IMPA、PMPA的加标回收率分别为57%、98%、81%;检出限(S/N≥3)均为0.1μg/L,定量下限(S/N≥10)均为1μg/L。并将该方法应用于禁化武组织(OPCW)首次生物医学样品分析演练未知尿样的检测,结果满意。     

晋城无烟煤加压快速热解特性及其对气化反应的影响

利用自行设计的加压热重固定床反应器进行了晋城无烟煤加压快速热解特性的研究,并结合热天平半焦等温热失重分析,考察了热解温度、停留时间和热解压力等外部操作条件对煤焦快速热解半焦特性的影响。结果表明,随热解温度的提高、停留时间的延长和热解压力的增大,所得到的半焦产率降低,气化反应性减弱,活化能提高;高温产生较小的比表面积,而停留时间的延长和压力的提高产生较大的比表面积,比表面积与气化反应速率无明显的依存关系。水蒸气气化速率是CO2的四倍左右。     

天然产物Kinsenoside的全合成研究

以5-(R)-[(1R，2S，5R)-孟氧基]-2(5H)-呋喃酮为关键手性合成子，完成了具有抗高血脂活性的天然产物kinsenoside的全合成研究。     

离子液体/H_2O_2体系脱硫实验研究

选取四种不同种类离子液体(ILs),1-丁基-3-甲基咪唑溴化物([Bmim]Br)、1-丁基-3-甲基咪唑四氟硼酸盐([Bmim]BF_4)、1-丁基-3-甲基咪唑硫酸氢盐([Bmim]HSO_4)、1-丁基-3-甲基咪唑磷酸二氢盐([Bmim]H_2PO_4)与30%H_2O_2溶液在温和条件下对两种高硫脱灰煤样(LS、QX)进行脱硫实验研究。用化学法测定脱硫前后煤样形态硫含量,并利用傅里叶变换红外光谱(FT-IR)、X射线光电子能谱(XPS)、扫描电子显微镜(SEM)及热重(TG)对脱硫前后的煤样进行表征。结果表明,离子液体的加入使H_2O_2氧化脱硫能力增强,煤中硫铁矿硫和有机硫化物硫被显著脱除;经ILs/H_2O_2体系作用后的煤样中小粒径的颗粒减少,颗粒间的缝隙增大,煤表面的凹坑明显,热重实验结果表明,ILs/H_2O_2体系作用后的煤样相对于原煤热失重增大,部分挥发性物质释放峰温提前。     

ZnO/g-C3 N4微纳米材料的制备及其性能研究

用Zn(NO_3)_2、ZnCl_2、C_4H_6O_4Zn·2H_2O及三聚氰胺为原料,采用热解法合成ZnO/g-C_3N_4复合光催化剂。为了对合成产物的组成、形貌及光吸收性能进行表征,我们利用了X射线衍射(XRD)、扫描电子显微镜(SEM)及UV-Vis等。研究了不同物质含量热解及ZnO的含量对合成产物的影响,并且以六价铬为污染模拟物,对合成的ZnO/g-C_3N_4进行光催化进行评价。结果表明ZnO/g-C_3N_4复合材料有更优秀的光催化性能,用氯化锌为2. 5 wt%、热解温度为510°C、保温时间120 min时,合成的ZnO/g-C_3N_4光催化性能最佳,用氙灯照射270 min后,对六价铬溶液的降解率达到了93. 19%,比用样条件下单一的g-C_3N_4光催化性能提高了44. 92%。     

AB24在MgAl-LDO上的吸附性能及机理研究

本文探讨了nMg/nAl=3的水滑石焙烧产物(MgAl-LDO)对染料酸性黑24(AB24)的吸附性能及其机理。考察了不同因素对MgAl-LDO吸附AB24性能的影响,并研究了吸附过程的热力学和动力学机理。实验结果表明:MgAl-LDO对AB24具有优异的吸附性能,在298 K,pH=10条件下,1.0 g.L-1MgAl-LDO对1 000 mg.L-1AB24溶液的吸附容量和去除率分别达到998.31 mg.g-1和99.83%。动力学和热力学研究表明:MgAl-LDO对AB24的吸附过程同时符合Langmuir和Freundlich等温吸附方程,并且是个放热、自发的过程。计算所得的吉布斯自由能绝对值在10~15 kJ.mol-1,这主要是由染料分子与水滑石层板的氢键作用产生,结合Materials Studio 5.5软件模拟AB24染料分子在MgAl-LDHs上的排列分布,推测MgAl-LDO对AB24的吸附机理是表面吸附(占优势)与层间插层的协同作用。同时,该吸附过程符合准二级反应动力学模型。     

生物样品中速可眠及代谢产物的分析

应用气相色谱／质谱（ＧＣ／ＭＳ）法对一例速可眠中毒病人生物样品进行分析鉴定。样品经酸化、乙醚提取,然后于ＧＣ／ＭＳ分析,在患者胃内容物和血中检出速可眠,在眼药３３ｈ尿内可检出速可眠原型药物以及四个代谢产物。并用外标法对生物样品中速可眠进行定量测定,对临床救治起到了积极作用。     

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.