齿轮箱振动测试与分析

在对某型齿轮箱的模态、振动烈度和振动加速度进行测试的基础上,详细分析了测试结果.模态测试得到了齿轮箱的振型和模态参数,振动烈度测试结果表明该齿轮箱处于良好工作状态,振动加速度测试结果显示该齿轮箱的减振措施达到了预期的效果.最后,对测试提出了建议.     

高超声速滑翔再入飞行器的可达区快速预测

防御方对来袭滑翔再入飞行器进行可达区的预测存在先验信息量不足且时效性要求高等难题。为此提出一种基于最优化飞行假设的可达区快速预测方法:仅需已知目标当前位置、速度与最大升阻比(可基于雷达探测数据通过实时弹道估计获得),基于平衡滑翔假设和最大横程的埃格斯解分别获得目标最大纵程和横程终点坐标,在经纬度二维平面内,可达区即可近似为以两个最大横程终点间线段为短轴、最大纵程终点到短轴距离为半长轴的半椭圆区域。仿真结果表明,与传统的数值优化方法和常倾侧角方法相比,提出的方法具有利用先验信息少、精度较高和运算量小的优点,可满足实时性要求。     

Shock wave mitigation using zig-zag structures and cylindrical obstructions

The present study focuses on the mitigation of shock wave using novel geometric passages in the flow field. The strategy is to produce multiple shock reflections and diffractions in the passage with minimum flow obstruction, which in turn is expected to reduce the shock wave strength at the target location. In the present study the interaction of a plane shock front (generated from a shock tube) with various geometric designs such as, 1) zig-zag geometric passage, 2) staggered cylindrical obstructions and 3) zig-zag passage with cylindrical obstructions have been investigated using computational technique. It is seen from the numerical simulation that, among the various designs, the maximum shock attenuation is produced by the zig-zag passage with cylindrical obstructions which is then followed by zig-zag passage and staggered cylindrical obstructions. A comprehensive investigation on the shock wave reflection and diffraction phenomena happening in the proposed complex passages have also been carried out. In the new zig-zag design, the initial shock wave undergoes shock wave reflection and diffraction process which swaps alternatively as the shock front moves from one turn to the other turn. This cyclic shock reflection and diffraction process helps in diffusing the shock wave energy with practically no obstruction to the flow field. It is found that by combining the shock attenuation ability of zig-zag passage (using shock reflection and diffraction) with the shock attenuation ability of cylindrical blocks (by flow obstruction), a drastic attenuation in shock strength can be achieved with moderate level of flow blocking.     

涡轮泵故障检测的频段能量比SOM算法

为了解决缺少故障样本情况下的涡轮泵健康状态判别问题,分析了涡轮泵振动信号的频谱,提取了频段能量比作为其故障检测特征,并讨论了自组织映射的竞争学习原理及聚类结果的U-矩阵表示,提出了一种基于频段能量比的自组织映射故障检测算法,并实现了该算法最佳匹配神经元的选择和权重向量的自适应更新。通过某型液体火箭发动机历史试车数据的验证,结果表明,健康涡轮泵数据利用该算法聚类时仅存在一个类别,相邻神经元距离小于0.1;反之,故障涡轮泵数据利用该算法聚类时明显存在两个或多个类别,且相邻神经元的最大距离大于0.1。因此,基于频段能量比的SOM算法能有效地判别涡轮泵的健康状况。     

基于模态分析的变速箱振动测点优化配置

针对坦克变速箱振动信号在状态监测中测点的选择问题,提出了根据不同测点的频响特性优化振动测点的方法。通过分析变速箱箱体的有限元动力学模型,得到箱体的各阶固有频率和振型,选择模态分析中总位移较大的位置作为最优的测点安装传感器,为试验测点布置以及状态监测和评估提供理论支持。研究结果表明：位于风扇联动装置齿轮箱附近的传感器对变速箱振动信号的强弱变化比较敏感。     

假目标配置数量模型及其效费比分析

在现代战争中,示假伪装的地位越来越重要。引入了真假目标的发现识别概率的指数分布模型,综合考虑作战时间、真假目标价格比等因素,确定战场生存能力和配置假目标成本两个目标函数,并以最小加权偏差法确定两者权重,建立基于多目标决策的假目标配置数量模型。最后结合实际问题,将各参数条件带入模型计算出假目标的最佳配置数量,同时利用假目标的效费比模型进行检验分析,从而为战时假目标配置数量的确定提供参考依据。     

Allocation of two redundancies in two‐component series systems

The allocation of redundancies in a system to optimize the reliability of system performance is an interesting problem in reliability engineering and system security. In this article, we focus on the optimal allocation of two exponentially distributed active (standby) redundancies in a two‐component series system using the tool of stochastic ordering. For the case of active redundancy, stochastic comparisons are carried out in terms of the likelihood ratio and reversed hazard rate orders. For the case of standby redundancy, a likelihood ratio ordering result is developed. The results established here generalize and strengthen corresponding results in the recent literature. In addition, several numerical examples are used to explicate the results. © 2013 Wiley Periodicals, Inc. Naval Research Logistics, 2013     

一种基于节点资源利用率的无标度网络路由策略

本文研究了节点负载处理能力异质条件下的无标度网络交通动力学过程,提出了一种基于节点资源利用率的全局动态路由策略。该策略利用网络中节点资源利用率构建了一种全局代价函数,选择使该代价函数最小的路径来传输负载。实验结果表明该路由策略在略微增加平均路径长度的情况下成倍地提高了网络负载传输能力,与有效路由策略的比较进一步验证了该策略的有效性。     

层次分析法的水下航行器维修性指标分配方法

基于层次分析法的水下航行器维修性指标分配方法把层次分析法应用到水下航行器维修性指标分配方法中,即邀请专家对故障的检测和隔离方式、可达性、可更换性和测试的困难等级进行两两比较,得到评价矩阵,据此,可以得到分配结果.这种方法克服了按故障率和设计特性分配法在设计特性相差不大时存在的缺陷,把定性分析与定量分析相结合.在设计初期即明确设计目标,除了考虑到单元的故障率还兼顾了初期设计过程中的不确定性.将这种方法应用于某水下航行器的维修性分配,结果表明,该方法具有实用价值.     

助推-滑翔飞行器可达区域影响因素研究

利用Radau伪谱法将连续的助推-滑翔飞行器轨迹优化问题转化为非线性规划问题,通过仿真得到了飞行器完整的可达区域,着重分析了升阻比、终端速度以及终端倾角对飞行器可达区域的影响.研究结果表明,可达区域呈现出类椭圆结构,其地理区域覆盖能力由助推火箭关机点速度决定;与终端倾角对飞行器可达区域的影响相比,飞行器升阻比特性和终端速度的影响相对较大.