轮南油田注水井污染评价方法探讨

基于塔里木盆地轮南油田注入水对油藏污染的特点,定义注水井的实际注水量(Qt)与理论吸水量(Qf)之比为注水井吸水效率(α),根据α随注水时间(t)的变化所反映的地层污染的变化情况,将地层的污染程度分为无污染(α≥1.0)、轻微污染(0.9≤α<1)、一般污染(0.7≤α<0.9)和严重污染(0≤α<0.7)。α-t曲线可以反映不同注水时期注水井的地层污染状况,间接了解注水水质的变化情况;Qt-Qf图示法能直观反映较长注水时期内注水井的总体污染状况。与通常采用的"表皮系数"法(只能评价注水井在较短时间段内的污染状况,且获取参数成本高)相比,所提出的评价方法具有获取参数容易、分析简单、结果直观的优点,便于监测注水井注入水对地层的污染状况,及时发现注水井的水质问题。图3表3参5     

The construction of assembly and measuring devices for broadband traveling-wave tube electron injectors

The construction of electron injectors for broadband traveling-wave tubes and the effect of a spread in the geometrical dimensions of the parts of the injector on the parameters of the electron beam are considered. Equipment for the assembly and monitoring of the main dimensions of the injector and technological methods of assembly which ensure repeatability of the parameters of the traveling-wave tube and its reliability are proposed. __________ Translated from Izmeritel’naya Tekhnika, No. 12, pp. 45–48, December, 2007.     

一种微秒级脉冲电解加工工程化电源研制

针对针阀体喷孔的去毛刺技术要求,研制了一种以IGBT为开关器件的微秒级脉冲电源。该电源采用直流加斩波输出方案,直流部分采用现有稳压直流电源,设计了该电源斩波部分脉冲发生电路、推动电路、电源主电路和保护电路。使用该电源进行了针阀体电解去毛刺工艺实验,实验数据表明喷孔流量和压力室杂散腐蚀程度达到设计技术要求。     

带不同出油阀结构的双弹簧喷油器燃油系统喷射特性研究

对配有常规等容阀、带削扁的等容阀、阻尼阀、等压出油阀的双弹簧喷油器燃油系统高压喷射特性进行了分析研究。为消除本研究系统中出现的二次喷射,对这四种不同出油阀选择方案进行了比较。同时还分析了出油阀的主要结构参数对喷射特性的影响。     

BEPCII直线加速器定时系统

北京正负电子对撞机升级改造工程BEPCII的重要组成部分--直线加速器于2006年7月通过了所内预验收,其中定时系统是全新建造的基于EVG/EVR的事件定时系统[1],于2006年3月起投入运行,为直线加速器的电子枪、微波激励源、能量倍增器、正电子源、调制器、BPM等设备提供精确的时序触发信号.本文介绍直线加速器定时系统的研制、安装调试、运行和改进等工作情况.     

压电喷油器喷油规律影响因素的研究

基于压电陶瓷的逆压电效应,设计了一种直接作用常闭式压电喷油器结构,并建立了压电喷油器的数学模型,验证了模型的准确性.利用仿真模型分析了喷油器关键结构参数对针阀升程、喷油率等特性的影响.研究结果表明：进、出油孔孔径选择应合适,以便产生理想的先缓后急的喷油规律;控制腔容积应取较小值,以提高喷油器的响应速度;针阀弹簧预紧力的大小应和喷油器的响应时间相匹配.     

高压共轨喷油器蓄压腔进油通道设计

为了满足大功率柴油机的需求,进一步控制系统内的压力波动,减小共轨喷油器内压力波动对系统轨道压力的影响,对一种高压共轨喷油器蓄压腔进油通道进行了优化设计.利用三维流体分析软件FLUENT对喷油器蓄压腔进油通道进行了仿真分析,通过对不同凸边长度的进油通道及不同节流孔的进油通道流场计算,发现蓄压腔进油通道加凸边的设计结构,当凸边结构小于3mm时,可以实现不影响喷油量的同时,降低共轨系统内的压力波动.     

Design study of a 120-keV,3He neutral beam injector

We describe a design for a 120-keV, 2.3-MW,³He neutral beam injector for use on a D-³He fusion reactor. The constraint that limits operating life when injecting He is its high sputtering rate. The sputtering is partly controlled by using an extra grid to prevent ion flow from the neutralizer duct to the electron suppressor grid, but a tradeoff between beam current and operating life is still required. Hollow grid wires functioning as mercury heat pipes cool the grid and enable steady state operation. Voltage holding and radiation effects on the acceleration grid structure are discussed. We also briefly describe the vacuum system and analyze use of a direct energy converter to recapture energy from unneutralized ions exiting the neutralizer. Of crucial importance to the technical feasibility of the³He-burning reactor are the injector efficiency and cost; these are 53% and $5.5 million, respectively, when power supplies are included.The beam is composed of 91 separate, parallel currents that flow in the gaps between the elements or wires of a grid. Each such flow is referred to as a beamlet. The current densities in Figs. 5, 8, and 9 are values within a beamlet, as measured at the beam-forming grid. They are not values averaged over the entire beam cross-section.     

3D computation of hydrogen-fueled combustion around turbine blade-effect of arrangement of injector holes-

Recently,a number of environmental problems caused from fossil fuel combustion have been focused on.Inaddition,with the eventual depletion of fossil energy resources,hydrogen gas is expected to be an alternativeenergy resource in the near future.It is characterized by high energy per unit weight,high reaction rate,widerange of flammability and the low emission property.On the other hand,many researches have been underway inseveral countries to improve a propulsion system for an advanced aircraft.The system is required to have higherpower,lighter weight and lower emissions than existing ones.In such a future propulsion system,hydrogen gaswould be one of the promising fuels for realizing the requirements.Considering these backgrounds,our group hasproposed a new cycle concept for hydrogen-fueled aircraft propulsion system.In the present study,we perform 3dimensional computations of turbulent flow fields with hydrogen-fueled combustion around a turbine blade.Themain objective is to clarify the influence of arrangement of hydrogen injector holes.Changing the chordwise andspanwise spacings of the holes,the 3 dimensional nature of the flow and thermal fields is numerically studied.     

某型柴油机高压共轨喷油器结构改进仿真分析

针对某型柴油机共轨喷油器改进设计的需求,建立了喷油器的数值仿真模型,研究了喷油器针阀质量、控制腔容积及供油道长径比对喷油器特性的影响.研究表明在保证针阀结构强度的情况下,针阀质量应该更小;控制腔容积在满足针阀升程要求等条件下也应更小;在确定长径比的条件下,合理安排喷油器的尺寸结构,适度增加供油管的长度和直径可以降低喷油器内部的压力波动.研究为该型喷油器的改进设计提供了技术支撑.