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排序方式: 共有866条查询结果,搜索用时 15 毫秒
1.
三峡工程三期截流提前到 2 0 0 2年 11月上旬进行 ,截流难度显著增大。为了使截流工程顺利进行 ,以先进的计算机可视化技术为基础 ,采用IMAGIS软件生成三维地形图 ,用Creator建模形成导流明渠、纵向围堰及三期围堰等三维实体模型 ,最后通过运用虚拟现实技术 ,开发出三峡工程三期截流施工实时动态演示、查询系统。该系统能根据需要实现漫游 ,可以随意定位到感兴趣的区域作细部观察 ,且具有良好的交互性。通过施工仿真研究 ,将三期截流施工过程生动地显示在屏幕上 ,用以指导施工组织管理 ,为三期截流的决策和控制提供了有效的工具 相似文献
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自韧Si3N4陶瓷的显微结构及其性能研究 总被引:4,自引:0,他引:4
利用热压的方法制得室温断裂韧性和抗弯强度分别为11.2MPa·m ̄(1/2)、823MPa,高温(1350℃)断裂韧性和抗弯强度分别为23.9MPa·m ̄(1/2)、630MPa的自韧Si_3N_4陶瓷。研究了显微结构和力学性能之间的关系。结果表明:玻璃相的含量、β-Si_3N_4的长径比等对性能有重要影响。分析了自韧Si_3N_4陶瓷的增韧机理,通过SEM明显观察到Si_3N_4中存在裂纹偏转、分支和β-Si_3N_4拔出现象。 相似文献
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Molecular dynamics simulation using a universal force field has been employed to determine the diffusion coefficients of O2 and Na2SO4 vapor into B2O3 and SiC from 700 K to 1273 K, respectively. Einstein diffusion was observed in a 250~300 ps simulation. 相似文献
6.
Yubin Gong Yuanlong Mo Yongdong Zhou Xiaolan Zhou 《Journal of Infrared, Millimeter and Terahertz Waves》1996,17(4):769-777
A new type of mm-wave slow wave system, double staggered ladder circuit is analyzed in this paper, by means of “average cavity field method” and three-dimensional finite element method. The influence of the electron beam channel on the dispersion characteristics is discussed. An experimental research is made, the experimental results agree well with the theoretical one. 相似文献
7.
无人机(unmanned aerial vehicle,UAV)电力巡检时的图像数据量急剧增加,为使深度卷积神经网络(deep convolutional neural network,DCN-N)在低功耗的前提下仍能准确识别出电力缺陷,将重点改进传统DCNN算法,以减少机载前端平台中DCNN模型的计算成本,有效提高电力缺陷识别的运行速度,进而延长巡检无人机的续航里程.首先将卷积网络中的浮点运算进行定点化近似,然后通过快速机器学习算法对DCNN模型的输入图像进行自适应选择,最后通过实验对所提方法进行了验证.实验结果证明,DCNN模型经8比特定点优化和自适应选择选择策略后的准确率达88.2%,推理时间缩短了65.9%,能耗减少了71.9%,查准率提高了9.8%.所设计的定点化DCNN模型自适应选择策略不仅能节约电力巡检系统的功耗,而且能提高电力缺陷识别的精度. 相似文献
8.
Three-Dimensional Carbon/Silicon Carbide Composites Prepared by Chemical Vapor Infiltration 总被引:10,自引:0,他引:10
Continuous-carbon-fiber-reinforced silicon carbide composites (C/SiC) were prepared by chemical vapor infiltration in which the preforms were fabricated with the three-dimensional braid method. The mechanical properties and microstructures were investigated. For the composites with no interfacial layer, flexural strength and fracture toughness increased with density of the composites, and the maximum values were 520 MPa and 16.5 MPa·m1/2 , respectively. The fracture behavior was dependent on the interfacial bonding between fiber/matrix and fiber bundle/bundle which was determined by the density of the composites. Heat treatment had a significant influence on the mechanical properties and fracture behavior. The composites with pyrolysis interfacial layers exhibited characteristic fracture and relatively low strength (300 MPa). 相似文献
9.
Yani Zhang Yongdong Xu Jianjun Lou Litong Zhang Laifei Cheng Jianjun Lou Zhijun Chen 《International Journal of Applied Ceramic Technology》2005,2(2):114-121
Carbon fiber-reinforced silicon carbide matrix composites have the potential to overcome the shortcoming of the currently used carbon/carbon friction materials in aircraft brakes. In this article, the carbon/silicon carbide (C/SiC) composites were prepared by chemical vapor infiltration method, and the brake disks with different densities and component content were finally obtained. The friction coefficient and friction stability can be significantly improved by increasing both material density and carbon content. When the density of C/SiC composite is 2.3 g/cm3 , the coefficient of friction measured is 0.23, the coefficient of friction stability remains about 0.43, the liner wear rate is less than 9.3 μm/cycle, and the weight wear rate is less than 9.1 μm/cycle. The rapid increase of friction coefficient approaching the end of braking is mainly related to the increasing of surface temperature in a short time and the enhanced adhesion and abrasion of contact conjunctions and asperities. The C/SiC composites exhibited a good stability of braking against fading versus the braking number and surface temperature. The surfaces of C/SiC brake disks were covered with wear debris including the fragment of carbon fibers after the braking tests. The wear on the surfaces is significantly determined by cyclic mechanical and thermal stresses, which result in the micro-cracks in the SiC matrix, the thin flakes of the surface materials as well as the grooves. 相似文献
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