不可数多个GO-空间乘积的k-仿紧性

证明了不可数多个GO-空间的乘积是k-仿紧空间(相似文献   

浅谈精益生产在班组中的推广

精益生产的核心是消除一切无效劳动和浪费,通过不断地降低成本、提高质量、增强生产灵活性、实现无废品和零库存等手段确保企业在市场竞争中的优势。精益生产的思想及方法。需要通过通过班组人员的全员参与,共同改善达到减少浪费,降低成本来提高利润成为企业生产的主要目的。     

广州市微波电路新电视塔前端机房设计方案

介绍了广州广播电视微波线路搬迁到新电视塔后前端机房的设计方案,包括编解码设备、矩阵设备和光纤设备的综合组网方法,以及TS流在SDH微波中直接传输的应用、网管配置等技术。     

ATM OVER SDH技术在DVB系统中的应用

主要介绍了ATM技术的相关理论知识,在此基础上详细介绍了唐山有线电视网络前端数字系统的基本构架,并讨论了VPI和VCI在系统中的具体应用。     

梯度型非局部高阶梁理论与非局部弯曲新解法

针对文献中关于纳米结构刚度受非局部效应影响趋势的不一致预测,基于梯度型的非局部微分本构模型,利用迭代法及泰勒展开法求得了非局部高阶应力的无穷级数表达,非局部应力相当于经典弯曲应力与非局部挠度的逐阶梯度之和. 然后推导了梯度型非局部高阶梁弯曲的挠曲轴微分方程,并结合正则摄动思想,求解了非局部挠度的表达式. 最后给出数值算例,具体量化挠度受非局部尺度因子的影响大小. 研究表明:相比于其经典值,纳米结构的非局部弯曲挠度可呈现出或增大或减小或不变的趋势,考虑梯度型非局部高阶应力降低或提高或不影响纳米结构的刚度,具体结果依赖于外载和边界约束的类型. 算例显示外载形式和边界约束条件均各自独立地影响着纳米结构的非局部弯曲挠度,同时首次观察到非局部最大弯曲挠度的位置可能受非局部尺度因子的影响. 研究结论解决了非局部弹性力学应用于纳米结构的若干疑点,并为理论的发展和优化提供支持.      

基于遥感图像的舰船目标检测与参数估计方法

利用遥感图像进行舰船检测与监视的研究和技术开发在海洋遥感领域得到了快速发展,并成为遥感数据重要的海洋应用之一。当海洋遥感图像用于舰船尾迹检测时,就可及时有效地发现和提取舰船目标信息。文中利用光学遥感图像的海面舰船尾迹特征以及相关参数,估测舰船目标的速度与航向。分别通过灰度累积法和Radon变换法两种不同的尾迹长度检测方法,对尾流长度进行了提取,并利用尾流长度特征简单估测了舰船航速与航向。对实验结果和误差进行了分析,并对影响舰船尾流检测的因素进行了讨论。估算结果初步验证了对航速与航向估算方法的有效性     

Experimental study of the mean wake of a tidal stream rotor in a shallow turbulent flow

The mean wake of a three-bladed horizontal axis tidal stream turbine operating at maximum power coefficient has been investigated experimentally in a wide flume with width 11 times the depth, providing minimal restriction to transverse wake development and behaviour of large-scale horizontal turbulence structures. This is an important first stage for understanding wake interaction in turbine arrays and hence large-scale power generation. The rotor diameter has a typical value of 60% of the depth and the thrust coefficient is representative of a full-scale turbine. The shear layers originating from the rotor tip circumference show classic linear expansion downstream, with the rate of a plane shear layer vertically and 1.5 times that horizontally. These shear layers merge by around 2.5 diameters downstream forming a self-similar two-dimensional wake beyond eight diameters downstream with a virtual origin at two diameters downstream of the rotor plane. The spreading rate is somewhat less than that for solid bodies. The detailed velocity measurements made in the near wake show rotation and vorticity similar to that measured previously for wind and marine turbines although with asymmetry associated with bed and surface proximity. The longitudinal circulation in a transverse plane is conserved at about 1% of the swept circulation from the blade tip within two diameters downstream, the extent of detailed measurement. Turbines are usually designed using blade element momentum theory in which velocities at the rotor plane are characterised by axial and tangential induction factors and it is now possible to see how this idealisation relates to actual velocities. The axial induction factor corresponds to velocity deficits at 0.4–0.8 radii from the rotor axis across the near wake while the tangential induction factor at the rotor plane corresponds to velocities at 0.4–0.6 radii between 1–2 diameters downstream, indicating some general correspondence. For the two-dimensional self-similar far wake the two parameters defining the centreline velocity deficit and the transverse velocity profiles are likely to be insensitive to Reynolds number in turbulent conditions.     

交换环上赋值的完全性

对有乘法单位元的交换环上的非精简显赋值定义一种"完全性"。首先就Von Neumann正则环成为完全赋值环给出一个充分必要条件(定理1);并对正则的完全赋值环证明在它的代数扩环上也能给出完全的拓展赋值(定理2)。其次,再对另一种特殊的环给出与定理1和定理2相同的结论(定理3,4)。更多还原     

On Weakly P.P. Rings

We introduce, in this paper, the right weakly p.p. rings as the generalization of right p.p. rings. It is shown that many properties of the right p.p. rings can be extended onto the right weakly p.p. rings. Relative examples are constructed. As applications, we also characterize the regular rings and the semisimple rings in terms of the right weakly p.p. rings.     

基于PTP协议的航空图像高速传输

为了减少传输图像数据量,提高图像传输的速度,实现对航空图像的高速传输,研究一种高速、可行的图像传输方法。基于PTP(Picture Transfer Protocol)协议,采用JPEG图像压缩算法对图像进行压缩,引进文件流的多线程传输模式,自主开发了航空数码相机图像传输系统。介绍了系统设计方案,验证了设计方案的可行性。测试结果显示,图像平均传输速率为53.641 Mb/s,误码率为0.00%,表明该系统能够很好地保证数据的原始性,防止数据丢失,有效地减少数据通道堵塞,实现了图像数据的高速、高质量传输。