激光二极管与单模光纤自动对准搜索算法

针对激光二极管与单模光纤的自动对准,从搜索路径规划和参数选择出发,给出五自由度自动对准搜索算法解决方案,为了提高搜索效率,提出新的指数函数拟合算法应用到XY平面的搜索过程中,给出了算法的基本原理和实现方法。实验证明,与爬山法相比,这种算法由于减少了采样点数而缩短了搜索时间,从而提高了自动对准的速度。     

SiCw/Al复合材料的强度分析

用简化应力的分析方法推导了SiCw Al复合材料的强度与SiC晶须偏轴角α的关系,并通过试验进行验证.结果表明,计算的SiCw Al复合材料强度与实测值比较接近,其误差归因于压缩变形过程中SiC晶须发生了转动和折断,改变了SiC晶须的偏轴角和平均长径比.     

模糊合成算子在作战方案综合评估的应用研究

在分布式交互仿真中,根据仿真结果对作战方案进行综合评估,运用模糊综合评判的方法进行评判,并着重对合成算子的选择进行分析,确定乘与有界算子M(·, )为比较适合对作战方案评估的算子.     

列车用复合材料阻燃性能研究

不同类别的阻燃剂配合使用能产生协效作用,大大提高阻燃效果。在甲基丙烯酸类不饱和聚酯树脂9001基体中,添加微囊化红磷/氢氧化铝/三氧化二锑/甲基膦酸二甲酯(MRP/Al(OH)3/Sb2O3/DMMP)阻燃剂体系,对其树脂体系固化物及玻璃纤维织物复合材料的力学性能和阻燃性能进行了实验研究,提出了一种有望用于列车复合材料大尺寸构件制造的性能优异、价格低廉的新体系。结果表明,当质量添加比例分别为12%MRP、50%Al(OH)3、2%Sb2O3时,树脂体系室温粘度100mPa.s左右,凝胶时间超过80min,适用于RTM和VIMP等大尺寸构件成型工艺;复合材料拉伸强度215.4MPa,弯曲强度177.15MPa,拉伸模量13.85GPa,弯曲模量13.36GPa,氧指数39.7。     

激光成像雷达空间目标探测与识别技术

研究了激光三维成像雷达在动能拦截器空间目标探测与识别方面的应用。首先介绍了激光3D成像雷达系统基本原理,然后设计了激光3D成像雷达目标识别的工作流程,最后提出了基于旋转图像转换的3D目标识别算法。进一步探索了红外+LADAR主被动复合光学成像导引头在空天防御拦截武器目标探测与识别的应用,分析了复合光学导引头的关键技术,给出了相应的成像结果。     

一种新型甲醛气体清除材料的实验研究

采用溶胶-凝胶法将纳米TiO2负载在活性碳纤维上,制备出一种新型甲醛气体清除材料。在制备中依次掺杂Fe3+和十二烷基苯磺酸钠(SDBS)对纳米TiO2进行改性,研究了纳米TiO2光催化活性的变化,并测试了自制材料的甲醛清除效率。结果表明:Fe3+和SDBS的添加不会改变纳米TiO2的晶型结构,但有利于晶粒的成长和负载膜的光催化活性;添加体积分数分别为0.8%的Fe3+和3%的SDBS时,材料的甲醛清除效率最高。     

大温差条件下碳纤维混凝土无约束变形试验

为了研究碳纤维、聚酯纤维对混凝土在自由条件下的约束作用,通过设计对碳纤维混凝土、聚酯纤维混凝土和素混凝土加热放热试验,比较掺入不同纤维体积分数的纤维混凝土在大温差条件下无约束自由变形的差异,并用温度线膨胀系数表达。对试验数据进行分析,得到体积分数为1%的碳纤维混凝土比素混凝土抗自由变形能力提高了38.8%,在本试验的各种体积分数中效果最好。结果表明碳纤维与混凝土,虽然热力学性能不同,但是二者结合之后碳纤维因其高弹性模量的特性,反而可以更好地抑制混凝土自由变形。试验效果也表明,随着施工工艺的完善,碳纤维体积分数可能会超过1%,碳纤维对混凝土性能的提升仍然有很大的帮助。     

Optimization of buckling load for laminated composite plates using adaptive Kriging-improved PSO: A novel hybrid intelligent method

An effective hybrid optimization method is proposed by integrating an adaptive Kriging (A-Kriging) into an improved partial swarm optimization algorithm (IPSO) to give a so-called A-Kriging-IPSO for maxi-mizing the buckling load of laminated composite plates (LCPs) under uniaxial and biaxial compressions. In this method, a novel iterative adaptive Kriging model, which is structured using two training sample sets as active and adaptive points, is utilized to directly predict the buckling load of the LCPs and to improve the efficiency of the optimization process. The active points are selected from the initial data set while the adaptive points are generated using the radial random-based convex samples. The cell-based smoothed discrete shear gap method (CS-DSG3) is employed to analyze the buckling behavior of the LCPs to provide the response of adaptive and input data sets. The buckling load of the LCPs is maximized by utilizing the IPSO algorithm. To demonstrate the efficiency and accuracy of the proposed methodology, the LCPs with different layers (2, 3, 4, and 10 layers), boundary conditions, aspect ratios and load patterns (biaxial and uniaxial loads) are investigated. The results obtained by proposed method are in good agreement with the literature results, but with less computational burden. By applying adaptive radial Kriging model, the accurate optimal results-based predictions of the buckling load are obtained for the studied LCPs.     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

复合材料层合结构层向理论及应用进展

层向理论是由Reddy提出来的一种用于精确分析复合材料层合结构的三维板壳分析理论。由于不引入任何的变形和应力假设条件,因此相较于传统的等效单层板理论,层向理论在分析大厚度复合材料层合板壳结构的静动态响应及其局部层间效应时具有较大的优势。系统地综述了层向理论近年来的研究进展、数值解法及其应用情况。具体包括:层向理论的基本原理及发展现状、基于层向理论的有限元方法及改进模型、层向理论在复合材料层合结构静动态响应及含损伤问题领域的应用等。并对该理论可进一步拓展的研究方向进行了展望。