Zr基非晶合金在过冷液相区静液挤压的变形行为及结构

研究了Zr41.2Ti13.8Cu12.5Ni10Be22.5非晶合金在过冷液相区内静液挤压的变形行为以及结构变化。结果表明:非晶合金在高应变速率下产生了明显的塑性变形,直径从16 mm变为12 mm,断裂为4段,且样品断口上随机分布着充分发展与未充分发展的脉纹式切变带,由此可看出非晶合金的变形为非牛顿体变形行为;挤压后的样品约有3%的非晶相发生晶化,在非晶基体上析出10~20 nm的纳米晶粒,导致挤压后非晶合金的热稳定性降低;静液挤压高应变速率变形条件使非晶合金产生非均匀流变,是造成非晶合金断裂的主要原因。     

正多边形盒零件冲压成形凸缘变形区的应力分布计算

首先给出正多边形盒零件凸缘变形区的应力分布式 ,接着分析了凸缘变形区的应力变化规律 ,并以0Cr18Ni9板材和方盒零件为算例给出了凸缘变形区的应力分布曲线。正多边形盒零件凸缘变形区圆角部分的拉深变形是发生皱曲和破裂之源并向直边部分转移材料 ,使直边部分松弛乃至皱曲。因此 ,对于皱曲通常选择设置压边装置 (压边圈、拉深筋等 )来解决。对于破裂通常选择增大侧壁间圆角半径或多次拉深来解决。正多边形盒零件冲压成形最好采用分区 (分块 )变压边力拉深或分区 (分块 )恒压边力拉深     

自由曲面数控加工走刀方向的优化研究

走刀方向对数控加工的效率有重要影响，尤其对于多曲面拼接自由曲面不规则轮廓区域的数控加工。针对现有自由曲面数控加工过程走刀方向优化研究存在的问题，提出了基于曲面数控加工区域划分的走刀方向优化策略，建立了简化的刀具轨迹计算模型和加工时间模型，并用实例加以验证，取得了满意的效果。     

溪洛渡电厂18F机组启动试运行试验研究

总结了溪洛渡右岸18F机启动试运行试验。检验了厂家的保证值,划分了18F机在全负荷范围的稳定运行区域,并找出了各运行区域振动的主要频率。试验成果有助于溪洛渡东电机组及电网的安全运行。     

基于分块分形的工业CT图像缺陷自动定位算法

针对传统的缺陷定位必须经过图像分割和缺陷提取等步骤,识别过程比较麻烦而且费时,提出了一种基于分块分形的工业CT图像缺陷自动定位算法.该方法首先对图像进行分块处理,对每个分块区域进行分形维数计算.通过分形维数频域分布直方图进行阈值处理,标记边缘块,最后通过连通区域处理标记块,进而对缺陷进行标记定位.通过对含有不同缺陷数目的固体火箭发动机模型工业CT图像处理,均可以准确地定位缺陷.实验结果表明,该方法能有效、准确地自动定位工业CT图像缺陷,且具有较强的鲁棒性.     

Influence of groove type on welding-induced residual stress,deformation and width of sensitization region in a SUS304 steel butt welded joint

To join a medium or thick plate weldment with a full penetration, a groove is usually prepared in the space between two sections of metal. Because weld metal needs to be deposited within the groove to form the joint, it is expected that different groove type will require different heat input, which may consequently have influence on welding residual stress and deformation. Generally, different groove corresponds to different bead layout, so it can be foreseen that the groove type has a significant effect on temperature history, shape and size of heat affected zone, and region of sensitization in certain alloys such as austenitic stainless steel. The influences of groove type on residual stress, angular distortion and width of sensitization region in a SUS304 butt-welded joint were investigated by means of numerical simulation and experiment. Based on ABAQUS code, a computational approach with considering thermo-mechanical coupling behaviors, moving heat source, strain hardening and annealing effect was developed to simulate temperature profile, stress field and deformation in multi-pass joint. Welding temperature cycles, residual stress distributions and deformations in V, K and X groove joints were calculated through using the proposed computational procedure. Meanwhile, experiments were carried out to obtain residual stress distributions and angular distortions. Through comparing the numerical results and the measured data, the effectiveness and accuracy of the developed computational approach were verified. The simulation results show that groove type has a significant influence on welding residual stress distribution, angular distortion and width of sensitization region.     

一类饱和非有理系统状态反馈设计

本文研究了一类饱和非有理系统状态反馈镇定问题.通过线性分式表示技术,这类非有理系统可以转化为带有两个非线性回路的线性时不变(linear time-invariant,LTI)系统.假设非有理函数项分别满足局部扇形区间不等式以及局部Lipschitz条件,提出了两种基于LMI条件的镇定方法.最后,举例证明了所提出方法的有效性.     

基于自适应阈值和区域生长的SD-OCT糖网图像亮斑分割

硬性渗出是糖尿病性视网膜病变的一个比较显著的症状,频域光学相干断层视网膜图像中的高信号亮斑与渗出有着密切的联系。为了研究渗出与病变的关系,有必要找到一种提取亮斑的方法。但是,目前关于糖网图像亮斑提取的研究还非常少。首先运用层分割算法限制亮斑所在区域,然后采用自适应阈值法确定种子集合,最后使用基于人类视觉特性的区域生长方法提取出亮斑。实验结果表明,本方法可以较准确地分割出糖网图像中的亮斑。     

Analysis of General Ideal Proportional Navigation Guidance Laws

In this work, the capture region of the general ideal proportional navigation guidance law is analyzed with the following constraints: (i) the target's input acceleration is subject to independent or magnitude saturation, and (ii) the missile's input acceleration is subject to magnitude saturation. In addition to the case of unbounded maneuverability of missile with or without knowing the target acceleration, the necessary and sufficient condition for a bounded maneuvering missile that captures a nonmaneuvering target is also derived. Furthermore, the conditions that result in zero impact velocity are discovered and discussed in some of the cases. The capture regions that cannot be obtained analytically are determined numerically by a powerful classifier, the least square support vector machines. To have the capture region ready for least square support vector machines, all the state variables are transformed into modified polar variables and non‐dimensionalized to reduce the number of independent variables. In order to make the implementation possible in real time, an approximation of the Gaussian radial basis function is adopted to obtain the corresponding nonlinear feature mapping function. Through numerous numerical experiments, the proposed technique is found to be adequate for storing the capture region in an onboard fire control computer.     

Energy-efficient control of nanosatellites during distributed region formation flying

In this paper, we present an energy-efficient method for distributed region formation flying of nanosatellites. The proposed framework consists of two concurrent sub-schemes that include estimation and formation. In the estimation sub-scheme, unlike the existing methods on satellite formation flying, that assume the availability of the reference orbital elements to all followers, here, a distributed estimator is developed so that the follower nanosatellites estimate the position of the leader in its orbital slot. In the formation sub-scheme, we consider a region formation strategy which is an efficient method in dealing with the formation of a large number of nanosatellites. We propose an optimal region following formation method based on the receding horizon control (RHC) using the estimated reference orbital elements. Subsequently, an algorithm is presented to solve the proposed energy-efficient formation flying method. Finally, the simulation result is presented that illustrates the purposed method improves the power consumption for each nanosatellite with respect to the existing non-optimal region formation flying controllers.