常州用电负荷量气象指数初探

分析了常州市1998－1999年全市用电量变化特征，建立与其关系密切的最高气温、最低气温、相对湿度、天气状况等气象要素之间的关系，得出其回归计算方程，并分析引起用电量变化的非气象要素，将得到的预报结果进行订正。通过检验、分析，最后确定了用电负荷量指数的划分标准。     

Increased summer electric power demand in Beijing driven by preceding spring tropical North Atlantic warming

本文利用北京市电力负荷资料,北京市站点观测温度资料,CN05.1温度资料,ERA5大气再分析资料及ERSST v3b海表温度资料,发现3-4月副热带北大西洋海温异常和北京市夏季电力呈很好的正相关关系,并揭示了副热带北大西洋海温异常影响北京市夏季电力的可能物理机制.春季副热带北大西洋海温异常偏暖,热带中太平洋出现东风异常...     

Recent Seismic Electric Signals (SES) activities in Greece

Quite recently two intense Seismic Electric Signals activities were recorded at Pirgos station in western Greece. They have been followed by two strong earth-quakes with magnitudes 6.1 and 6.9 that occurred in western Greece and southern Greece; the latter is the strongest earthquake that occurred in Greece during the last two decades. The compatibility of these results with some relationship between selectivity and earthquake focal mechanism suggested by Uyeda et al. (1999) is discussed.     

海底电性源频率域CSEM勘探建模及水深影响分析

为了探索我国海域油气和水合物等高阻目标体CSEM勘探的可行性和方法技术,本文研究了在海水中水平电性源激励下有限水深海洋地电模型的频率域电磁响应,为进一步的1D和3D仿真计算奠定了理论基础.在推导电磁响应公式时,首先给出了各层介质的Lorentz势,然后根据Coulomb势与Lorentz势的关系,得到了各层介质的Coulomb势.各层介质中的电磁场均可以由Lorentz势或者Coulomb势计算得到,但在有限元计算时Coulomb势具有优势.长导线源的电磁场和势函数可以由电偶源的电磁场和势函数沿导线长度积分得到.文中具体给出了海水中水平电偶源和长导线源在海水层的电磁场公式,并根据该公式计算了不同水深环境下海底表面的电磁场分布,分析了海水深度对海底油气储层电磁异常的影响.结果表明,随着水深减小,异常幅度和形态特征发生明显变化.当水深很浅时(如50 m),只有同线方向的Ex和Ez两个电场分量存在明显异常.最后,以两个已知海底油田为例,计算了不同水深环境下可观测到的电场异常,展示了电性源频率域CSEM在海底勘探中(包括浅海环境)的良好应用前景.对于该方法实用化过程中还需进一步解决的问题,文中结尾部分也进行了初步探讨.     

Study of the Ability of the Magnetotelluric Method to Monitor Earthquakes

Most earthquakes on the Chinese mainland have occurred within the depth range of 10-25 km,which is usually called the seismogenic layer.According to the rule of penetration depth,the precursor of the electric anomaly,which is transferred from the seismogenic layer to the Earth's surface,should be very weak,but the ability to monitor earthquakes can be greatly improved if the field precursor effect is taken into consideration because of expansion of the electric anomaly area.The results of one-and two-dimensional modeling computations are consistent with the observed fact that the apparent resistivity decreases before earthquakes.This provides good evidence for our inference.The corresponding physical mechanism is that the conductivity of the anomaly area may be increased by the rock dilatation and fluid permeation due to the stress effect during the developing process of earthquakes.     

电阻率成像在堤坝勘察中的应用

利用日本OYO公司MCOHM - 2 1型浅层地电仪 ,采用 pole pole方式高密度电阻率探测系统 ,对山东跋山、大冶、会宝岭等几个存在病险需要加固的大中型水库大坝进行了电阻率CT探测。坝体内的断层、破碎、薄弱结构以及人工埋设的暗排水洞在CT断面上反映的非常清晰     

简易花盘夹具与电炉拐臂的修复

夹具是机加工中一种重要的辅助工具。为解决生产触媒用的真空电炉拐臂的修复而设计了花盘夹具，解决了修复电炉拐臂的问题，还可用来加工其它形状复杂的类似零件。花盘夹具设计合理，结构简单，成本低，是一种很有使用价值的机加工工具。     

含环状天线槽正交方位随钻电磁波测井仪器三维有限体积法数值模拟

针对由多环状天线槽构成的方位随钻电磁波测井仪器真实结构,基于柱坐标系下耦合势Helmholtz方程和三维有限体积法研究建立一套相应的三维电磁响应数值模拟算法.首先,采用柱坐标系下三维不规则Yee氏交错网格对计算区域进行剖分,保证了钻铤表面附近的剖分网格与非光滑刻槽钻铤表面同形;并利用电场延拓边界条件逼近钻铤表面的理想电...     

Plasma diagnostics and simulation for the SMART-1 mission

SMART-1 is a technology demonstrator for using primary electric propulsion on interplanetary spacecraft. Hence, studying of the interaction of the plasma emitted by the thruster with the environment and the spacecraft is one of the top priorities during the mission. Two experiments (Electronic propulsion diagnostic package and Spacecraft potential, electron and dust experiment) are available to measure the electron densities and temperatures as well as wave electric fields during the operation of the electric propulsion thruster. Additionally, a retarding potential analyser, a quartz microbalance and a solar-cell sample will analyse data from slow charge-exchange ions which are a potential contamination source. ESTEC is developing a 3D particle-in-cell model in order to study the spacecraft/environment interactions on SMART-1 and interpret the measurements. In the present paper, we will review the contamination effects associated with electric propulsion and how the plasma sensors cover them. We further present preliminary results from the numerical simulation and show how the flight data will be used to validate the modelling code. A successful validation of the simulation will support future interplanetary and commercial missions featuring electric propulsion to reduce the risk of contamination and interference with on board instruments.