正癸烷与二甲苯在超临界压力下的热裂解

采用连续流动装置对正癸烷和二甲苯在超临界压力下的热裂解对比研究. 用气相色谱和色质联用仪对其气相产物和液相产物进行分析, 计算气相产物产率和裂解转化率, 并运用计算化学方法获得正癸烷和二甲苯不同化学键的键能, 从实验和理论上分析其裂解反应的难易程度和裂解规律. 实验结果表明, 在4 MPa和650、700、750 ℃条件下, 正癸烷比二甲苯更容易裂解, 正癸烷裂解产物以C₁-C₃小分子的烃类和氢气为主, 而二甲苯裂解产物主要为乙苯、甲苯和其它芳香类化合物; 键能计算结果表明, 正癸烷碳链骨架的C－C键能和C－H键能均较小, 裂解反应的诱发步骤应该是C－C键断裂, 而二甲苯苯环上C－C和C－H键能均较大, 裂解诱发步骤应该是侧链甲基脱氢反应. 因此正癸烷裂解反应以C－C键断裂和脱氢反应为主, 二甲苯裂解主要发生侧链甲基C－C键断裂和脱氢反应, 而芳环则比较稳定, 理论计算键能分析与裂解实验结果一致.     

两个2,6-二氨基-3,5-二硝基吡嗪-1-氧化物含能配合物的合成、晶体结构及催化性能

合成了2,6-二氨基-3,5-二硝基吡嗪-1-氧化物(LLM-105)₂种含能配合物[Cu₄O₂(C₄N₆O₅H₂)₂(CH₃COO)₂(DMF)₂]·DMF(1)((C₄N₆O₅H₂)^2- 为配体LLM-105失去2个H⁺)和[Co(C₄N₆O₅H₃)₃]·7H₂O(2)((C₄N₆O₅H₃)^- 为LLM-105失去1个H⁺),用X射线单晶衍射法测定了其分子结构。配合物1属正交晶系,空间群为Pbca,配合物2属三斜晶系,空间群为R3。用DSC,TG-DTG技术对配体和2个配合物的热分解进行了研究。用Kissinger法和Ozawa-Doyle法对配合物热分解过程中放热峰的表观活化能进行了计算。同时研究了2种配合物对AP热分解催化效果的影响,结果表明,2种配合物使AP的高温分解峰温分别提前117.42和71.85℃,分解放热量增加1916.97和1433.76J·g^-1,对AP热分解具有非常显著的催化效果。     

聚四氟乙烯和石墨对聚醚酰亚胺摩擦学性能的影响

将聚四氟乙烯(PTFE)和石墨两类减摩耐磨填料填充到聚醚酰亚胺(PEI)中,表征其摩擦性能,利用扫描电子显微镜分析了磨损表面的显微结构,并分析了磨损机制.研究结果表明,PTFE和石墨的填充明显改善了PEI的摩擦磨损性,摩擦系数降低到0.3以下(纯PEI的摩擦系数为0.41),磨损率降低了3个数量级.在PTFE体系中,PTFE质量分数为10%时,PEI基共混材料的摩擦系数最低为0.23;而在质量分数为15%的石墨体系中,PEI基共混材料摩擦系数最低为0.27.磨损率随着填料含量的增加而逐渐下降,在填料质量分数为20%之后,摩损率下降平缓.因此PTFE和石墨的填充对PEI的摩擦学性能起到了很好的改善作用,而且PTFE比石墨的改善效果更优益.共混物的机械性能测试结果表明,在填料质量分数为5%~15%时,共混物具有良好的机械性能.     

CYP2C9酶与Warfarin结合模型的立体选择性理论研究

对CYP2C9酶与S-Warfarin复合物的晶体结构进行分子对接、分子动力学模拟、通道分析及结合自由能计算,发现原晶体结构中的结合模式为"亚稳态",提出了CYP2C9与S-Warfarin结合的可催化模式;比较了CYP2C9与S-和R-Warfarin结合的异同,确定了在结合过程中起重要作用的锚定氨基酸残基,尤其是位于活性位点区域的苯丙氨酸簇.在结合过程中这些残基通过芳香环的移动对稳定底物的结合模式起到至关重要的作用,阐明了该酶呈现相关底物选择性的原因.对于CYP2C9与底物对接模式及立体选择性的研究有助于在分子层面上理解特异性底物与酶的结合特点,为潜在的药物设计提供了合理可信的理论依据.     

铱(Ir~Ⅲ)-稀土(Ln~Ⅲ)异核配合物发光性能研究

稀土离子(LnⅢ)丰富的4f电子跃迁能级,使稀土发光材料获得重要而广泛的应用.稀土配合物中天线基团的引入,弥补了稀土离子f-f跃迁禁阻而导致吸收较低的不足.而具有三重态吸收的过渡金属配合物作为天线基团,更使稀土离子的激发窗口红移.相关研究具有重要的理论意义和实际应用价值.本文主要综述近年来有关铱(IrⅢ)-稀土(LnⅢ)异核发光配合物方面的研究进展.     

有机半导体非平衡态HOMO和LUMO能量位移规律与OLED中“热激子”形成的唯象理解

以能斯特方程为基础, 通过分析电流密度与氧化还原物种活度变化, 即载流子浓度变化的关系, 计算出有机半导体材料电极电势的变化, 从而建立起有机半导体前线轨道, 即最高占据分子轨道(HOMO)能级和最低未被占据分子轨道(LUMO)能级相对于热力学平衡态的能量位移随电流密度变化的数学关系. 进而依据能级能量位移引起的能隙变化, 提出了有机电致发光显示器（OLED）中“热激子”的产生机制.     

Co3O4/UiO-66@α-Al2O3陶瓷膜对VOCs废气的分离催化性能

以α-Al₂O₃为支撑层, UiO-66为分离层, Co₃O₄为催化层, 构建了Co₃O₄/UiO-66@α-Al₂O₃陶瓷膜.对其形貌结构进行了表征, 并研究了其对挥发性有机物(VOCs)的分离催化性能. 结果表明, 该陶瓷膜对喷涂行业废气中苯与吡啶两种主要成分体现出良好的分离性, 透过侧的气体中吡啶与苯的摩尔浓度比值可由给料侧的1提高至17; 体系中引入臭氧后, 给料侧苯的浓度明显降低, 其去除率可达到89%. 透过侧的吡啶去除率仅为27%, 得到了较大程度的保留, 剩余的吡啶经收集后可进行单独的深度处理. Co₃O₄/UiO-66@α-Al₂O₃陶瓷膜在对喷涂行业废气中苯成分高效降解的同时, 能够有效解决喷涂行业废气处理过程中氮氧化物的排放问题, 有望成为喷涂行业废气预处理工艺的理想选择.     

表面限域掺杂提升高比能正极材料稳定性

Lithium ion batteries (LIBs) have broad applications in a wide variety of a fields pertaining to energy storage devices. In line with the increasing demand in emerging areas such as long-range electric vehicles and smart grids, there is a continuous effort to achieve high energy by maximizing the reversible capacity of electrode materials, particularly cathode materials. However, in recent years, with the continuous enhancement of battery energy density, safety issues have increasingly attracted the attention of researchers, becoming a non-negligible factor in determining whether the electric vehicle industry has a foothold. The key issue in the development of battery systems with high specific energies is the intrinsic instability of the cathode, with the accompanying question of safety. The failure mechanism and stability of high-specific-capacity cathode materials for the next generation of LIBs, including nickel-rich cathodes, high-voltage spinel cathodes, and lithium-rich layered cathodes, have attracted extensive research attention. Systematic studies related to the intrinsic physical and chemical properties of different cathodes are crucial to elucidate the instability mechanisms of positive active materials. Factors that these studies must address include the stability under extended electrochemical cycles with respect to dissolution of metal ions in LiPF₆-based electrolytes due to HF corrosion of the electrode; cation mixing due to the similarity in radius between Li⁺ and Ni²⁺; oxygen evolution when the cathode is charged to a high voltage; the origin of cracks generated during repeated charge/discharge processes arising from the anisotropy of the cell parameters; and electrolyte decomposition when traces of water are present. Regulating the surface nanostructure and bulk crystal lattice of electrode materials is an effective way to meet the demand for cathode materials with high energy density and outstanding stability. Surface modification treatment of positive active materials can slow side reactions and the loss of active material, thereby extending the life of the cathode material and improving the safety of the battery. This review is targeted at the failure mechanisms related to the electrochemical cycle, and a synthetic strategy to ameliorate the properties of cathode surface locations, with the electrochemical performance optimized by accurate surface control. From the perspective of the main stability and safety issues of high-energy cathode materials during the electrochemical cycle, a detailed discussion is presented on the current understanding of the mechanism of performance failure. It is crucial to seek out favorable strategies in response to the failures. Considering the surface structure of the cathode in relation to the stability issue, a newly developed protocol, known as surface-localized doping, which can exist in different states to modify the surface properties of high-energy cathodes, is discussed as a means of ensuring significantly improved stability and safety. Finally, we envision the future challenges and possible research directions related to the stability control of next-generation high-energy cathode materials.     

激光等离子体中电子热流变化的数值模拟

利用二维相对论电磁粒子模拟程序研究了激光等离子体中电子热流在各向异性等离子体中的发展演化过程,提出了单位时间内等离子体临界表面上输运的能量与电子自由路程之间的函数关系,得到了用经典Spitzer-Harm理论来描述的电子热传导公式,探讨了经典电子热传导模型与被限制的自由热流随时间的变化情形。数值结果表明,强激光照射等离子体薄靶时的初始时刻电子热流迅速增大,但由于周边的自生磁场对电子的运动有限制作用,因此热流随时间缓慢地减少。对这些过程的研究对于电子热流的衰减和热输运等过程有重要意义。     

高超声速脉冲风洞模型自由飞试验技术

风洞模型自由飞试验利用高速相机记录自由飞行模型的运动历程, 再根据模型运动特征参数反演模型的气动特性.由于没有支撑系统的干扰, 该试验能够较真实地模拟飞行状态, 在飞行器静/动稳定特性研究中具有独特的优势.文章在JF-8A高超声速脉冲风洞中开展了10°尖锥模型自由飞试验, 并以圆球模型的自由飞运动测量风洞动压, 对模型运动特征参数的数字图像提取技术及气动参数的辨识方法等关键技术进行了研究.