MDS图在液态模锻工艺过程单片机仿真控制系统中的应用

本文介绍了液态模锻工艺过程单片机仿真控制系统的设计方法，包括液态模锻工艺程确立、逻辑量确立、硬件系统设计、ＭＤＳ图的建立及软件实现，在工艺设备的逻辑性控制中应用ＭＤＳ图控制结构设计的控制器可方便方便地实现ＰＬＣ的控制功能，也可主便地实现其他娄字逻辑系统的控制功能。     

Mathematical description of the NaK model for MASTER-2005

The release of NaK droplets has been modeled for the new version of the European Meteoroid and Space Debris Terrestrial Environment Reference model MASTER-2005. Previously published versions of the model have been revised. The parameters of the model are introduced and discussed. NaK droplets consist of eutectic sodium–potassium alloy and have been released during RORSAT reactor core ejections. They contributed to the space debris environment in the centimeter and millimeter size regime. Sixteen nuclear powered RORSATs launched between 1980 and 1988 activated a reactor core ejection system in Sufficiently High Orbits (SHO), mostly between 900 and 950 km altitude. The core ejection caused an opening of the primary coolant circuit. The liquid coolant has been released into space during these core ejections. The outflow is considered as a discrete event for each of the sixteen core ejections in total. The NaK coolant has been forming droplets up to a diameter of 5.5 cm. NaK releases are restricted to a very narrow region near 65° inclination. This paper gives the parameters of the NaK release model as it is implemented in MASTER-2005. The quantitative values of all model parameters including characteristic diameter and uniformity parameter are presented. The ratio of the characteristic droplet size to the orifice diameter is discussed. It is estimated that altogether 128 kg of NaK-78 (8 kg per RORSAT) was released on orbit. Simulation runs show that there are still 45,000 droplets with a total mass of 97 kg in orbit at the reference epoch 1 May 2005, whereas the smallest droplet has a diameter of 5 mm. Results of orbit propagation simulation runs are presented in terms of spatial density.     

多孔介质空心圆柱绕流的摄动解

本文主要讨论了绕多孔介质空心圆柱的有势流动问题。运用摄动方法,给出了速度势的四阶近似,然后得到了圆柱表面的无量纲的压力系数和阻力系数。结果发现在势流的情况下多孔介质圆柱受到附加阻力作用,并且在圆柱的喷射或吸收流体的特征速度与来流特征速度的比值是一个小量的时候,阻力系数与特征速度比成简单的线性关系。     

一种用于液晶曝光中的激光检测系统

介绍了一种非接触式激光检测系统，可用于检测液晶曝光中液晶模板与基板之间的间隙，给出了该种系统的测量原理、硬件系统、信号处理方法、测量结果、分辨力和误差分析，并指出了这种测量系统的应用。     

Integration and calibration of a multi slit spectropolarimeter

Multi-slit spectropolarimeter is a next-generation spectropolarimeter to obtain vector magnetic field information at high spatial, spectral, and temporal resolution for studying the magnetic structures on the Sun. Once developed, it can be used as ground based instrument at solar observatories, also as a space payload for various solar missions. A high spectral resolution is invariably an important parameter for accurate vector magnetic field measurements and faster cadence is required for the study of dynamical evolution of structures (e.g., solar flares, sunspots etc.) on the Sun and hence better understanding on the physics behind their evolution.     

液膜法处理石化厂碱渣含酚废水的研究

本文研究了液膜法处理石化厂碱渣含酚废水的最佳制乳条件，最佳传质条件，并应用于不同浓度含酚水样处理。当挥发酚浓度低于７０００ＰＰｍ时，顷一级传质可使含酚量低于１００ＰＰｍ，７０００￣２００００ＰＰｍ，级二级传质可使含酚量低于１００ＰＰｍ，处理后废水可直接排放到石化厂和生化厂处理，为进一步进行中试研究提供了理论依据。     

跃变型介质中原油渗流有限元计算

本文建立跃变型介质中原油渗流的数学模型,可用来描述油层(尤其是低渗透层)超高压注水条件下的不稳定渗流过程及其特征。用Galerkin有限元法进行了数值计算,讨论了介质跃变的影响。     

火箭发动机基于神经网络非线性辨识的故障检测

应用神经网络方法，提出了一种液体火箭发动机故障实时检测算法。神经网络采用非线性辨识技术贴近发动机的工作过程，并输出包合发动机故障信息的辨识误差信号。若辨识误差变大超过一定阈值，检测逻辑就预报发动机故障。在发动机启动阶段离线训练神经网络，在发动机稳态过程可以采用离线或在线学习算法。实验研究表明神经网络可以成功地应用于大型泵压式液体火箭发动机的故障检测。     

一种液体火箭发动机试验台螺纹拧紧力矩量化控制方法

针对液体火箭发动机试验台工艺装配可靠性提升的需求,提出一种螺纹拧紧力矩量化控制方法。利用非试验和试验环境的力矩值统计与分析,确定液体火箭发动机试验台螺纹拧紧力矩值区间;通过拧紧力矩强度理论计算,验证力矩值区间的合理性;结合试验台螺纹空间位置的具体特点,确定适用不同空间位置的力矩量化控制方法和流程,并在试验中进行了应用。应用结果表明,本文提出的方法可有效提高发动机试验工艺的可靠性。