A Wafer-Level Sn-Rich Au-Sn Bonding Technique and Its Application in Surface Plasmon Resonance Sensors

Sn-rich Au Sn solder bonding is systematically investigated. High shear strength （64 MPa） and good hermeticity （a leak rate lower than 1 × 10-7 torr.1/s） are obtained for Au-Sn solder with 54wt% Sn bonded at 310℃. The AuSn2 phase with the highest Vickers-hardness among the four stable intermetMlic compounds of the Au Sn system makes a major contribution to the high bonding strength. This bonding technique has been successfully used to package the Surface Plasmon Resonance （SPR） sensors. The Sn-rieh Au-Sn solder bonding provides a reliable, low-cost, low-temperature and wafer-level hermetic packaging solution for the micro-electromechanical system devices and has potential applications in high-end biomedical sensors.     

低场核磁共振法对油基钻井液乳状液乳滴稳定性的研究

采用低场核磁共振技术,针对油基钻井液油包水型乳状液乳滴的稳定性进行研究。引入弛豫试剂Mn Cl2·4H2O对W/Q型乳状液的T2分布曲线进行定性分析,位于10~1 000 ms之间的弛豫峰对应于中度可自由移动水和白油弛豫峰的叠合峰,定义为乳状液弛豫峰;1 000~10 000 ms之间的峰为高度可自由移动水的弛豫峰。基于此,以弛豫峰峰形为定性指标,弛豫峰面积比率和弛豫峰间距为定量指标,针对弛豫试剂、油水比和老化温度等因素对乳状液横向弛豫时间T2分布曲线的影响进行了分析,进而深入研究了其对油基钻井液乳状液乳滴稳定性的影响。还将低场核磁共振分析技术运用于油基钻井液乳状液体系相对含油率的测量。结果表明,低场核磁共振是一种高效、快捷、准确反映油基钻井液乳状液稳定性的分析测试技术,同时,还可用于油基钻井液乳状液或原油相对含油率的测量。     

气相色谱-质谱联用技术分析大气细颗粒物对小鼠肺组织代谢轮廓的影响

建立了基于气相色谱-质谱联用技术(GC-MS)分析大气细颗粒物(PM2.5)滴注对小鼠肺组织代谢轮廓的影响的研究方法.通过分析肺组织细胞内代谢物的变化,研究不同浓度PM2.5对小鼠肺组织代谢的毒性机制.鼻腔分别滴注0、7.5、20.0和37.5 g/L的PM2.5悬液,提取肺组织胞内物质,预处理后进行GC-MS分析,结合主成分分析法(PCA)、偏最小二乘判别分析法(PLS-DA)进行数据解析,通过PLS-DA得分图可将不同PM2.5染毒浓度下的肺组织胞内物质明显区分.运用PLS-DA载荷图及模型的变量重要性因子(VIP)值,发现了7种代谢物可作为区别不同浓度PM2.5下代谢组的潜在生物标志物,分别为丙氨酸、缬氨酸、亮氨酸、鸟氨酸、延胡索酸、柠檬酸、嘌呤(p<0.01).代谢途径分析结果表明,PM2.5滴注使小鼠肺组织受到氧化损伤,氧化应激反应增强,抑制了三羧酸循环(TCA循环)及嘌呤代谢.本研究为深入解析PM2.5致毒机理提供了新的方法及理论依据.     

Prediction of hypersonic boundary layer transition on sharp wedge flow considering variable specific heat

When the air temperature reaches 600 K or higher, vibration is excited. The specific heat is not a constant but a function of temperature. Under this condition, the transition position of hypersonic sharp wedge boundary layer is predicted by using the improved eN method considering variable specific heat. The transition positions with different Mach numbers of oncoming flow, half wedge angles, and wall conditions are computed condition, the nearer to the Mach number The results show that for the same oncoming flow condition and wall transition positions of hypersonic sharp wedge boundary layer move much leading edge than those of the flat plate. The greater the oncoming flow the closer the transition position to the leading edge.