流动注射分析法测定成烟产物中的Zn^2＋

采用流动注射分析技术建立了Zn^2＋的FIA分析方法．谊分析方法可行、简便。其数据可靠,具有较好的选择性和重现性．样品测定频率大于30个／h;在1．0～5．0mg／L范围内呈良好的线性关系,γ=0．9999;回收率大于98%．实现了烟幕剂成烟产物中Zn^2＋的快速定量测定．     

次氯酸钙乳液消毒剂模拟剂的研究

研究了一种次氯酸钙乳液消毒剂的模拟剂,以及一些影响稳定性因素．该模拟剂是以氢氧化钙为分散相,水为分散介质,表面活性剂和无机盐为稳定剂组成．实验结果表明,该模拟剂具有与次氨酸钙消毒乳液相同的物理性能,并且无污染,可用于教育、作训之中．     

基于特征融合的刀具磨损监测方法

提出了一种基于特征融合的刀具磨损监测方法,将该方法应用于铣刀磨损监测取得了较好的效果,文中论述了特征融合方法的基本思想,多传感器信号的特征关联、抽取及正规化处理,作为融合中心的神经网络的构造及训练等内容。实验分析表明,该方法实现刀具磨损监测是行之有效的。     

一个基于引用的高效连接算法

针对对象关系数据模型和查询语言的新特点 ,提出了一个基于引用的高效连接算法Sort Loop。引用既是对象关系数据模型中一种重要的建模设施 ,同时它也有利于连接算法的设计和高效实现 ,如Hash Loops就是基于指针、面向集合属性的连接算法。Sort Loop克服了Hash Loops算法在数据访问方式和内存使用上存在的不足 ,性能分析表明 ,其性能优于Hash Loops。     

基于委托模式的多分辨率联合仿真

多分辨率联合仿真是实现多层次、多视角仿真的有效方法之一。现有多分辨率联合仿真模式存在一致性偏差和仿真剧情割裂问题,从而影响仿真的有效性。为此,提出基于委托模式的多分辨率联合仿真思路,该模式下能够较好地避免仿真剧情割裂问题,同时降低一致性问题的解决难度。通过实例验证,该方法较好地适用于大规模作战和局部作战行动的多分辨率联合仿真。     

基于混合高斯概率密度的加权打分方法

针对当前评比打分方法不能有效反映选手真实情况的问题,提出了一种基于混合高斯概率密度的加权打分方法。该方法的重点在于引入混合高斯分布来确定专家评分的权重。首先利用EM算法确定混合高斯分布模型参数,然后通过区间划分得到每个区间上的概率,再将专家打分映射到混合高斯概率密度函数区间上得到对应的权重,最后经加权求和得到选手的最终成绩。通过实例证明了该方法的合理性和公正性。     

基于改进Morison公式的海上漂浮软管波浪载荷计算

针对海上漂浮软管波浪载荷计算,分析了软管在海上的形态和受力特点,建立了海上漂浮软管力学分析模型,指出直接运用现有Morison方程计算漂浮软管波浪载荷存在的不足,并根据基本原理提出了改进Morison方程。对海上软质管线处于一定海况,分别运用改进Morison方程与现有Morison方程计算海上波浪载荷,并运用ANSYS软件建立软管模型,结果表明现有Morison方程不适用于计算海上漂浮软管波浪载荷,载荷计算结果偏高约15%,从而验证了改进Morison方程的精确性,有利于准确分析波浪载荷对海上漂浮软管的作用情况。     

Two novel critical shock models based on Markov renewal processes

In this paper, we investigate systems subject to random shocks that are classified into critical and noncritical categories, and develop two novel critical shock models. Classical extreme shock models and run shock models are special cases of our developed models. The system fails when the total number of critical shocks reaches a predetermined threshold, or when the system stays in an environment that induces critical shocks for a preset threshold time, corresponding to failure mechanisms of the developed two critical shock models respectively. Markov renewal processes are employed to capture the magnitude and interarrival time dependency of environment-induced shocks. Explicit formulas for systems under the two critical shock models are derived, including the reliability function, the mean time to failure and so on. Furthermore, the two critical shock models are extended to the random threshold case and the integrated case where formulas of the reliability indexes of the systems are provided. Finally, a case study of a lithium-ion battery system is conducted to illustrate the proposed models and the obtained results.     

Controllable combustion behaviors of the laser-controlled solid propellant

Microsatellites have been widely applied in the fields of communication,remote sensing,navigation and science exploration due to its characteristics of low cost,flexible launch mode and short development period.However,conventional solid-propellant have difficulties in starting and interrupting combustion because combustion is autonomously sustained after ignition.Herein,we proposed a new type of solid-propellant named laser-controlled solid propellant,which is sensitive to laser irradiation and can be started or interrupted by switching on/off the continuous wave laser.To demonstrate the feasibility and investigate the controllable combustion behaviors under different laser on/off conditions,the combus-tion parameters including burning rate,ignition delay time and platform pressure were tested using pressure sensor,high-speed camera and thermographic camera.The results showed that the increase of laser-on or laser-off duration both will lead to the decrease of propellant combustion performance during re-ignition and re-combustion process.This is mainly attributed to the laser attenuation caused by the accumulation of combustion residue and the change of chamber ambient temperature.Simultaneously,the multiple ignition tests revealed that the increased chamber ambient temperature after combustion can make up for the energy loss of laser attenuation and expansion of chamber cavity.However,the laser-controlled combustion performance of solid propellant displayed a decrease trend with the addi-tion of ignition times.Nevertheless,the results still exhibited good laser-controlled agility of laser-controlled solid propellant and manifested its inspiring potential in many aspects of space missions.     

The effect of al particle size on thermal decomposition,mechanical strength and sensitivity of Al/ZrH2/PTFE composite

To study the thermal decomposition of Al/ZrH2/PTFE with different Al particle size as well as mechanical strength and impact sensitivity under medium and low strain rates, molding-vacuum sintering was adopted to prepare four groups of power materials and cylindrical specimens with different Al particle size. The active decomposition temperature of ZrH2 was obtained by TG-DSC, and the quasi-static me-chanics/reaction characteristics as well as the impact sensitivity of the specimen were studied respec-tively by quasi-static compression and drop-hammer test. The results show that the yield strength of the material decreased with the increase of the Al particle size, while the compressive strength, failure strain and toughness increased first and then decreased, which reached the maximum values of 116.61 MPa, 191％, and 119.9 MJ/m respectively when the Al particle size is 12—14μm because of particle size grading. The specimens with the highest strength and toughness formed circumferential open cracks and reacted partly when pressed. Those with developmental cracks formed inside did not react. It is considered that fracture of specimens first triggered initial reaction between Al and PTFE to release an amount of heat. Then ZrH2 was activated and decomposed, and participated in subsequent reaction to generate ZrC. The impact sensitivity of the specimens decreased with the increase of Al particle size.