长征数据三维可视化分析平台设计与实现

为用好长征教育资源,引导群众在实践中培育爱国情怀,以长征革命历史为背景,结合大数据三维可视化技术,推出“长征数据三维可视化分析平台”,以大数据三维可视化、云计算赋能长征精神学习,多维度立体展现长征这段历史,激发爱国热情,传承爱国基因。该项目采用Spring Boot框架,整合MyBatis及Thymeleaf模板引擎构建系统架构,使用Maven项目管理工具,通过爬虫技术完成数据采集,依据牛顿冷却定律,提出了“访问量+时间衰减”文章热度值算法,前端展示使用HTML+CSS+JS及ECharts、Highcharts图表以及JS代码库JQuery,实现了三维长征路线、实景展示(VR)、祭扫景点等功能。     

飞秒激光刻写FBG实现5kW近单模光纤振荡器

<正>高功率光纤振荡器具有结构简单、抗回光能力强、成本相对较低等特点,被广泛应用于工业加工领域。光纤布拉格光栅(FBG)是全光纤结构振荡器中不可或缺的器件,扮演着腔镜的角色。目前,工业用的FBG主要通过紫外曝光法制备,光纤需要预先载氢,刻写完成后需要进行退火处理,这些都增加了FBG的制备时间,且对FBG的性能会造成一定的影响。     

改进海鸥算法的多阈值图像分割算法北大核心CSCD

为进一步提高图像分割精度,改善传统多阈值图像分割方法计算量大、分割慢的问题,提出了改进海鸥算法(improved seagull optimization algorithm,ISOA)的多阈值图像分割方案。针对原始海鸥算法(seagull optimization algorithm,SOA)存在早熟、寻优精度不足的问题,首先,采用cubic混沌映射优化初始解,提高搜索效率;其次,引入鹰栖息优化算法(eagle perching optmizer,EPO)的缩放因子和疯狂算子进行扰动,并与麻雀搜索算法(sparow search algorithm,SSA)警戒者的位置更新相结合,优化寻优精度和收敛速度,避免陷入局部最优。利用6种基准测试函数对ISOA进行寻优性能测试。最后,将ISOA与图像分割的最优阈值选取相结合,进行基于Otsu的多阈值图像分割,并与现有分割算法进行对比。仿真结果表明,ISOA在基于Otsu的图像分割中,100%取得了最优值,且80.9%的结果优于其余算法,使图像的分割精度和质量均得到了优化。     

杠杆式力标准机自动控制系统研制

介绍了一种基于可编程控制器(PLC)的杠杆式力标准机自动控制系统,分析了杠杆式力标准机的机械结构和工作原理,并阐述了本控制系统的硬件结构以及控制软件设计。改造后的自动控制系统使原有杠杆式力标准机恢复正常运行,并且提高了整机控制以及检测水平。     

电力设施保护存在问题分析

对电力设施保护存在的问题进行了调查,从内、外部因素对电力设施保护工作存在的问题进行分析.根据分析结果,进行针对性研究并提出完善法律法规、加强运维管理、投入物防技防、加大宣传、联合协同的五个解决对策,最大限度地避免电力设施被破坏,为电网安全运行提供可靠的设备保障.     

基于星弹载嵌入式系统的CAN总线驱动技术研究

针对CAN总线在控制外围设备方面的优势,对基于SJA1000的CAN总线驱动软件的设计与实现展开研究;通过分析星弹载嵌入式系统层次结构和设备驱动的调用关系,提出了通过操作系统的扩展模块调用CAN总线驱动程序的设计理念;结合相关具体应用设计测试用例,并通过ZLGCANTest软件对所研发的CAN总线驱动软件进行了测试;证实所开发的CAN总线驱动软件在可靠性和实时性方面都能满足应用要求。     

复杂渠坡稳定性分析方法比较

目前边坡稳定性分析方法主要有刚体极限平衡法、有限元极限平衡法以及有限元强度折减法3种.为了分析这3种方法以及不同屈服准则在边坡稳定计算中的差异性,以南水北调工程中某典型复杂渠坡为例进行比较计算.结果分析表明,3种计算方法所得渠坡稳定安全系数相近,其中强度折减法中不同的屈服准则对计算结果影响较大.鉴于M-C准则在应力空间中屈服面棱角会对数值计算稳定性产生影响,建议优先采用与M-C准则相匹配的D-P3或D-P4作为强度折减法的屈服准则,由此计算得到的边坡稳定安全系数合理,且参数折减时能保持计算过程具有良好的稳定性.     

Study of the key factors affecting the triple grid lifetime of the LIPS-300 ion thruster

In order to ascertain the key factors affecting the lifetime of the triple grids in the LIPS-300 ion thruster,the thermal deformation,upstream ion density and component lifetime of the grids are simulated with finite element analysis,fluid simulation and charged-particle tracing simulation methods on the basis of a 1500 h short lifetime test.The key factor affecting the lifetime of the triple grids in the LIPS-300 ion thruster is obtained and analyzed through the test results.The results show that ion sputtering erosion of the grids in 5 kW operation mode is greater than in the case of 3 kW.In 5 kW mode,the decelerator grid shows the most serious corrosion,the accelerator grid shows moderate corrosion,and the screen grid shows the least amount of corrosion.With the serious corrosion of the grids in 5 kW operation mode,the intercept current of the acceleration and deceleration grids increases substantially.Meanwhile,the cold gap between the accelerator grid and the screen grid decreases from 1 mm to 0.7 mm,while the cold gap between the accelerator grid and the decelerator grid increases from 1 mm to 1.25 mm after 1500 h of thruster operation.At equilibrium temperature with 5 k W power,the finite element method(FEM)simulation results show that the hot gap between the screen grid and the accelerator grid reduces to 0.2 mm.Accordingly,the hot gap between the accelerator grid and the decelerator grid increases to 1.5 mm.According to the fluid method,the plasma density simulated in most regions of the discharge chamber is 1?×?10~(18)-8?×?10~(18)m~(-3).The upstream plasma density of the screen grid is in the range 6?×?10~(17)-6?×?10~(18)m~(-3)and displays a parabolic characteristic.The charged particle tracing simulation method results show that the ion beam current without the thermal deformation of triple grids has optimal perveance status.The ion sputtering rates of the accelerator grid hole and the decelerator hole are 5.5?×?10~(-14)kg s~(-1)and 4.28?×?10~(-14)kg s~(-1),respectively,while after the thermal deformation of the triple grids,the ion beam current has over-perveance status.The ion sputtering rates of the accelerator grid hole and the decelerator hole are 1.41?×?10~(-13)kg s~(-1)and 4.1?×?10~(-13)kg s~(-1),respectively.The anode current is a key factor for the triple grid lifetime in situations where the structural strength of the grids does not change with temperature variation.The average sputtering rates of the accelerator grid and the decelerator grid,which were measured during the 1500 h lifetime test in5 k W operating conditions,are 2.2?×?10~(-13)kg s~(-1)and 7.3?×?10~(-13)kg s~(-1),respectively.These results are in accordance with the simulation,and the error comes mainly from the calculation distribution of the upstream plasma density of the grids.     

Study on the influence of three-grid assembly thermal deformation on breakdown times and an ion extraction process

In order to study the influence of three-grid assembly thermal deformation caused by heat accumulation on breakdown times and an ion extraction process,a hot gap test and a breakdown time test are carried out to obtain thermal deformation of the grids when the thruster is in 5 k W operation mode.Meanwhile,the fluid simulation method and particle-in-cell-Monte Carlo collision(PICMCC) method are adopted to simulate the ion extraction process according to the previous test results.The numerical calculation results are verified by the ion thruster performance test.The results show that after about 1.2 h operation,the hot gap between the screen grid and the accelerator grid reduce to 0.25–0.3 mm,while the hot gap between the accelerator grid and the decelerator grid increase from 1 mm to about 1.4 mm when the grids reach thermal equilibrium,and the hot gap is almost unchanged.In addition,the breakdown times experiment shows that 0.26 mm is the minimal safe hot gap for the grid assembly as the breakdown times improves significantly when the gap is smaller than this value.Fluid simulation results show that the plasma density of the screen grid is in the range 6?×10~(17)–6?×?10~(18) m~(13) and displays a parabolic characteristic,while the electron temperature gradually increases along the axial direction.The PIC-MCC results show that the current falling of an ion beam through a single aperture is significant.Meanwhile,the intercepted current of the accelerator grid and the decelerator grid both increase with the change in the hot gap.The ion beam current has optimal perveance status without thermal deformation,and the intercepted current of the accelerator grid and the decelerator grid are 3.65 m A and 6.26 m A,respectively.Furthermore,under the effect of thermal deformation,the ion beam current has over-perveance status,and the intercepted current of the accelerator grid and the decelerator grid are 10.46 m A and 18.24 m A,respectively.Performance test results indicate that the breakdown times increase obviously.The intercepted current of the accelerator grid and the decelerator grid increases to 13 m A and 16.5 m A,respectively,due to the change in the hot gap after 1.5 h operation.The numerical calculation results are well consistent with performance test results,and the error comes mainly from the test uncertainty of the hot gap.     

巷道爆破掏槽空腔尺寸对爆破效果影响的模拟研究

为了研究巷道爆破掘进过程中掏槽空腔直径对崩落孔爆破效果的影响,运用ANSYS/LS-DYNA对掏槽空腔附近崩落孔的爆破效果进行模拟计算。建立崩落孔孔距A为450 mm、崩落孔抵抗线L和掏槽空腔直径B均为400 mm的初始模型,并以该模型为基础,保持L和A不变,逐步增大B建立额外4个模型。计算并绘制崩落区岩石的塑性应变图,分析得出:随着掏槽空腔直径的增大,岩石塑性应变区域开始增大,爆破效果逐渐改善,当B/L=2时炮孔之间的塑性应变区域连通,掏槽空腔直径对爆破的改善效果达到最优水平;提取掏槽空腔外一系列监测点的拉、压应力值进行分析后得到相同的结论。研究结果可为巷道爆破孔网参数设计提供理论依据和技术参考。