细胞培养液中多溴联苯醚以及代谢产物的GC-MS/MS测定方法

利用柱前衍生化耦合气相/质谱/质谱(GC/MS/MS),建立了细胞培养液中13种多溴联苯醚(PBDEs)、8种甲氧基化多溴联苯醚(MeO-PBDEs)和5种羟基化多溴联苯醚(HO-PBDEs)的分析方法.采用氯甲酸甲酯作为HO-PBDEs的衍生化试剂,相比传统重氮甲烷作为衍生化试剂的方法,其衍生化时间明显缩短.同时,衍...     

Ground-state properties of light kaonic nuclei signaling symmetry energy at high densities

A sensitive correlation between the ground-state properties of light kaonic nuclei and the symmetry energy at high densities is constructed under the framework of relativistic mean-field theory. Taking oxygen isotopes as an example, we see that a high-density core is produced in kaonic oxygen nuclei, due to the strongly attractive antikaonnucleon interaction. It is found that the 1 S_(1/2) state energy in the high-density core of kaonic nuclei can directly probe the variation of the symmetry energy at supranormal nuclear density, and a sensitive correlation between the neutron skin thickness and the symmetry energy at supranormal density is established directly. Meanwhile, the sensitivity of the neutron skin thickness to the low-density slope of the symmetry energy is greatly increased in the corresponding kaonic nuclei. These sensitive relationships are established upon the fact that the isovector potential in the central region of kaonic nuclei becomes very sensitive to the variation of the symmetry energy. These findings might provide another perspective to constrain high-density symmetry energy, and await experimental verification in the future.     

斑马鱼卵中多溴联苯醚及其衍生物的同步分析

建立了液液萃取耦合气相色谱/质谱联用(GC/MS/MS)分析斑马鱼卵中10种多溴联苯醚(PBDEs),12种甲氧基化多溴联苯醚(MeO-PBDEs)和9种羟基化多溴联苯醚(HO-PBDEs)不同极性组分的同步分析方法。优化了前处理步骤和色谱质谱条件,采用液液萃取法提取目标化合物,不必分离即可实现目标化合物的衍生化,使样品前处理时间大大缩短,实现了不同极性组分化合物的同步分析。采用干法制备酸性硅胶柱纯化,用15 mL正己烷和15 mL二氯甲烷正己烷(1:1,V/V)混合溶剂洗脱效果良好。31种化合物在4.0～500μg/L浓度范周内线性良好,相关系数均大于0.99,回收率在71.6%～133.0%之间;相对标准偏差低于21.5%;检出限在0.09～17.0 ng/g之间。本方法应用到斑马鱼亲子代间转移研究中,对实际样品的检测良好,并发现BDE-47,6-HO-BDE-47,6-MeO-BDE-47,2’-HO BDE-28和2’-MeC-BDE 28可通过母代斑马鱼暴露后,不同程度地转移到子代中。     

基于耦合算法的三维复杂结构冲击动力学特性

光滑粒子流体动力学-有限元耦合算法（SPH-FEM）较好地结合了SPH和FEM的优势,近年来逐渐被引入冲击动力学相关问题研究中。然而早期的研究对象多为单一材料的简单结构,所取得的研究成果距离实际工程应用仍有一定差距。为此,在总结前人工作的基础上,对SPH-FEM耦合算法进行适当改进,通过引入复合材料损伤模型,对复合材料蒙皮结构飞行器舱段结构进行建模计算,分析其在爆炸冲击激励下的冲击动力学特性。将数值计算结果与试验结果进行对比分析,验证该算法和模型的有效性和准确性,初步实现SPH-FEM的工程实际应用。最后总结了复合材料蒙皮结构飞行器在爆炸冲击激励下的一系列结构动态响应规律,以期为航天飞行器结构设计与防护提供参考。