新型测发控系统方舱结构研究设计

移动测发控系统是实现航天装备快速进入空间需求的首要条件。针对我国现役运载火箭测发控周期较长、地面测试设备复杂、缺乏移动发射能力,在新一代快速发射运载火箭的研发中通过采用“设备集成、线缆集中铺设、人机工程优化、方舱结构为平台”等多项技术,研发出了新型移动快速测发控系统,实现了新一代运载火箭(≤一周左右)快速简易测发的目标。     

悬浮法生产可发性聚苯乙烯(EPS)虚拟仿真实验平台的设计与开发

为实现我校高分子材料与工程专业人才培养目标,即培养高素质工程应用型人才,弥补教学过程中实际操作的缺陷与不足,我们开发了基于实际工业生产的悬浮法生产可发性聚苯乙烯的虚拟仿真实验平台.详述了该平台的设计开发思路与理念,平台主题结构,以及实验主控界面设计思路和主要内容.实践证明,该平台不仅包含工程应用的相关知识,而且极大的提...     

Determination of gallium by graphite furnace atomic absorption spectrometry with combined use of a tungsten-coated L'vov platform tube and a chemical modification technique

Tungsten-coated non-pyrolytic graphite (NPG), pyrolytic graphite (PG) and pyrolytic L'vov platform graphite (PPG) tubes were prepared, and their analytical performances were compared. The coating process simply involved injecting 100 μl of a sodium tungstate solution (0.01 mol l⁻¹) into each graphite tube, followed by heating according to a temperature programme similar to an atomisation cycle for the determination of gallium. This procedure for coating was repeated at least 12, 25, and 7 times towards NPG, PG, and PPG tubes, respectively. Among these tubes, the tungsten-coated PPG tube showed excellent performance for the determination of gallium. By combined use of a chemical modifier such as aluminium(III) or nickel(II) a detection limit (3σ) of 6 pg and sensitivity (1% absorption) of 3–4 pg were achieved. The practical potential of the proposed technique was demonstrated for the determination of gallium in several samples of alloys and fresh water.     

随机风-浪一体化降维建模及风机结构可靠度研究

基于随机脉动风场和随机波浪力场的谱表示降维模拟方法,采用脉动风速Davenport谱与波浪P-M谱对风、浪谱参数进行一体化构造,并应用相同的基本随机变量来保障风、浪模拟的概率信息一致,实现了随机风-浪一体化降维建模。进一步,基于ANSYS有限元软件建立了近海风机塔架数值计算模型,并以顶点位移为指标,进行了三种工况下结构的动力可靠度分析。数值算例验证了随机风-浪一体化降维建模方法的有效性。结构动力分析结果表明,风荷载对风机塔架顶点位移响应的影响占主导地位,同时波浪荷载的作用亦不可忽略。此外,随机风-浪一体化降维方法生成的代表性样本概率信息完备,可与概率密度演化理论结合实现海工结构在风浪共同作用下的精细化动力响应及可靠度分析。     

Microfluidic platform serves as controllable fabrication of binary Mo/Ir nanodots/carbon hetero-material for efficient electrocatalytic nitrogen reduction

Electrocatalytic nitrogen reduction reaction (NRR) is regarded as a potential routine to achieve environment-friendly ammonia production, because of its abundant nitrogen resources, clean energy utilization and flexible operation. However, it is hindered by low activity and selectivity, in which condition well-designed catalysts are urgently in need. In this work, a binary Mo/Ir nanodots/carbon (Mo/Ir/C) hetero-material is efficiently constructed via microfluidic strategy, of which the nanodots are homogeneously distributed on the carbon skeleton and the average size is approximately 1 nm. Excellent performance for NRR is obtained in 1 mol L⁻¹ KOH, of which the optimized ammonia yield and faradic efficiency are 7.27 μg h⁻¹ cm⁻² and 2.31% respectively. Moreover, the optimized ammonia yield of 6.20 μg h⁻¹ cm⁻² and faradic efficiency of 10.59% are also obtained in 0.005 mol L⁻¹ H₂SO₄. This work achieves the continuous-flow synthesis and controllable adjustment of hetero-materials for favorable morphologies, which provides an innovative pathway for catalyst design and further promotes the development of ammonia production field.     

基于网络教学平台的PBL教学模式在物理化学实验教学中的实践

基于网络教学平台系统,结合“蔗糖水解速率常数的测定”“液体饱和蒸气压的测定”“燃烧热的测定”等3个物理化学常规实验,介绍了在物理化学实验教学中实施以问题为导向的教学法（PBL）的具体实施步骤,探讨了该教学模式在化学实验教学实践中的应用。结果表明该教学模式教学效果良好,具有一定的推广价值。     

应用浮动冲击平台考核舰载设备响应分析

为研究安装甲板模拟器的浮动冲击平台系统考核舰载设备的机理,对整个系统建立有限元模型进行数值模拟并建立力学模型进行了理论分析。根据船体甲板结构产生的垂向低通滤波特性,提出甲板模拟器具有减缓高频冲击并满足设备安装频率要求的作用。将被试设备的浮动冲击平台考核系统简化为有阻尼的三自由度系统强迫振动模型,通过拉普拉斯变换方法求解了不同冲击环境下被试设备的响应。数值模拟与理论计算结果比较吻合,被试设备响应迅速达到峰值后逐渐衰减,振动频率由高频向低频过渡,在分析浮动冲击平台舰载设备考核系统长时间响应时需考虑阻尼的影响。     

航空稳像光电平台设计

分析了随机振动对调制传递函数的影响,指出角位移是影响航空成像质量的主要因素.研究了特定条件下可容许的MTF下降,并转变为稳定系统的设计参量,用来指导稳像系统的设计.利用空间机构学及平行四边形平动原理,研制了一种新的无角位移减振稳像平台,满足既无角位移又达到减振要求.根据设计理论给出了设计实例,对频率高于100 HZ的振动,衰减达34dB,并利用动力学软件进行测试仿真,仿真曲线验证无角位移减振的正确性,同时对无角位移机构进行光学测试,结果耦合角度小于8″,可以满足航空成像要求.     

精密工作台的设计与实验研究

微器件装配技术是实现组合结构的微机械电子学系统(MEMS)的关键技术之一,精密工作台系统则是微装配系统的一个重要组成部分。精密工作台系统包括粗动工作台和微动工作台:粗动工作台包括精密机械及其传动系统、光栅定位系统、直流力矩电机驱动系统及计算机控制系统;微动工作台包括微动台、压电陶瓷驱动电源和电感测微移。实验结果表明,粗动台系统的最高速度为5mm/s,最低速度为3.4μm/s,系统的重复定位精度为±1μm;微动台系统的定位精度可达到±1μm。