电磁轨道炮高速滑动接触电阻的定量表征

从描述电磁轨道炮炮口电压波形的场路模型出发,构建了电枢/轨道高速滑动接触电阻与轨道电流波形、炮口电压波形、电枢膛内速度曲线和轨道结构参数之间的关系,依据此关系可定量表征电磁轨道炮高速滑动接触电阻。实例计算表明,电枢/轨道高速滑动接触电阻的变化依赖于轨道电流变化,对应电流上升段、平顶段和电流下降段。在平顶段接触电阻最小约0.2mΩ,在电流上升段和电流下降段,接触电阻达3mΩ。     

电磁轨道发射装置隔离式分压器

研制了一套用于测量电磁发射装置轨道电压信号的隔离式分压器,实现了测量回路与被测回路之间的电隔离,简化了电磁发射装置测试系统的复杂性。并对影响隔离式分压器频率响应的元件参数进行了参数扫描,结果表明:研制的分压器在-3 dB区间的频率响应范围为14 Hz~18 MHz,满足电磁发射装置轨道电压信号的测试要求。使用P6015A高压探头进行比对标定,输出信号的前沿约1s,频率响应满足电磁轨道发射装置轨道电压信号的测量要求。同时用隔离式分压器及电阻分压器测量轨道电压信号,两者波形符合较好。     

再入体缩比模型湍流等离子体电磁散射特性测量

介绍了在弹道靶上利用二级轻气炮发射再入体缩比模型开展湍流等离子体电磁散射特性模拟试验方法、湍流等离子体的雷达散射截面积(RCS)测量方法。给出了模型尾迹湍流等离子体的电磁散射特性测量典型试验结果,对获得的试验结果进行了分析,并与一阶畸变波Born方法计算结果进行了比较。结果表明:合理选择缩比模型发射速度和飞行环境压力,在弹道靶上能够模拟产生湍流等离子体;利用激光阴影成像技术获得的锥模型尾迹流场图像证实了尾迹转捩的出现及其湍流形成;在给定的试验条件下,锥模型及其绕流RCS测量值比其尾迹RCS测量值高3个数量级,比背景散射电平高0.5~2.5个数量级,且信号没有周期性,幅度脉动范围为1~15dB,频率脉动范围0.4~40kHz;锥模型湍流尾迹RCS的脉动可能是尾迹电子密度的脉动引起的;单站X波段雷达系统测量的锥模型尾迹亚密湍流等离子体的散射信号测量值与计算结果变化规律一致;弹道靶RCS测量技术可用于再入体缩比模型湍流等离子体电磁散射特性研究,为开展相关研究提供了一种有效的地面模拟实验研究途径。     

分布储能式电磁轨道炮效率分析

分布储能式电磁轨道炮在长导轨发射中具备高发射效率优势,为实现分布储能式电磁轨道炮的恒流特点,建立可供发射器参数、结构设计参考的仿真模型尤为重要。针对口径为60 mm×80 mm的矩形轨道炮,根据电流波形的平稳性要求,沿导轨方向设置电流馈入点,诊断电枢位置并分时序触发各馈入点电源,以测试分布储能式电磁轨道炮的工作性能。在COMSOL三维磁场中建立矩形导轨-电枢模型,基于电流和磁场的多物理场耦合有限元分析得到磁场和电流的分布,并利用电磁场仿真结果实现电流趋肤效应下轨道电阻梯度计算。基于MATLAB SIMULINK平台对电容储能型脉冲功率电源模块建立电气电路;分析分布储能式电磁轨道炮非线性时变的动态特性并建立轨道及电枢阻抗模型,计算正向电磁力、滑动摩擦力构造电枢的运动方程,并使用信号电路建立电枢-导轨模块,通过Simulink测量模块连接两个隔离的网络,仿真计算得到导轨电流及电枢的出膛速度。设计了总储能为4.16 MJ的分布式储能轨道炮,结果显示,电容预充电压为10.8 kV时,导轨长为3 m的分布式电磁轨道炮可将1 kg的弹丸加速至1.4 km/s,与炮尾集中式电磁轨道炮相比,系统发射效率可提升约3%。     

电磁轨道炮滑动电接触的热效应

为了更准确地反映滑动电接触面的温升过程,建立了电磁轨道炮高速滑动条件下非理想电接触的计算模型,采用有限差分法,对接触电阻热效应进行了计算。计算结果表明:非理想电接触的表面温升明显高于理想接触,接触电阻层的厚度越大,电接触面的温升越快;由于速度趋肤效应的影响,接触电阻热的作用范围主要集中在接触面尾部区域;材料的热导率及输入电流的波形均对接触面温度峰值有重要的影响。研究结果为预测接触表面的材料状态,进而预测接触转捩的发生提供了理论依据。     

管身对中口径电磁轨道炮的影响分析

以脉冲电流作为激励的电磁轨道炮无可避免地在不锈钢管身上感应出巨大涡流,涡流不仅自身损耗能量,而且削弱电枢的推进力,降低发射效率。为深入研究管身对电磁轨道炮的影响,结合场路模型计算了电磁轨道炮系统的发射效率和涡流能耗,讨论了不同管身结构和材料下的发射效率,进一步分析了管身对电磁轨道炮力学特性的影响。结果表明:基于10MJ脉冲电源的中口径电磁轨道炮,其不锈钢管身将大幅削弱系统的发射效率,管身涡流能耗比炮口动能的一半还多;采用层压式结构的高导磁材料作为管身,发射效率的提升尤为明显;管身对电枢轴向力的削弱是导致发射效率下降的根本原因,对电枢径向力的削弱则不利于电枢和轨道的良好接触,从而增加接触电阻,降低发射效率;但是对身管各部件径向力的减小有助于降低身管所需预紧力。     

二级轻气炮弹丸速度过程测量实验技术研究

 针对二级轻气炮发射管的特性，设计了测量景深长达13 m的光纤探头，选择条纹常数为100 m/s的高灵敏度激光干涉测速仪，结合任意反射面激光干涉测速技术进行了实验，测量了发射口径Φ32 mm、长度12 m的二级轻气炮弹丸发射过程，测得弹丸运动距离11.3 m时的速度为3 960 m/s，与磁测速的结果一致，通过实验测得的速度历史，进而获得弹丸在发射管内的加速度过程，为炮内弹道研究提供了更直接的实验数据。     

串联型双轨增强电磁轨道炮电路模拟

建立了包括脉冲电源模块和电磁轨道炮的全电路模型,实现了从电源放电至电磁轨道炮发射过程的全电路模拟。根据电源放电与洛伦兹力加速的耦合方程组,在电路模型内将电源的基本单元封装成子电路模块、弹丸受力运动模型转化为电路解耦模块,建立了针对24个基本单元组成的电源网络驱动串联型双轨增强电磁轨道炮的电路模型。将模拟结果与实验结果进行对比,电流模拟结果偏差2.6%,电枢出膛速度模拟结果偏差9.8%,模拟与实验结果基本一致,验证了模型方程和模拟方法的可靠性和合理性。     

高速模型尾迹流场及其电磁散射特性相似性实验研究

高速目标再入大气层或在临近空间飞行时,空气电离形成的等离子体鞘套和尾迹对目标的雷达散射特性会产生影响.为了研究不同模型尾迹流场及其电磁散射特性规律和相似性,以氧化铝球模型为研究对象,在弹道靶设备上开展了双尺度参数相同的条件下高速球模型尾迹流场及其电磁散射相似性实验研究.由二级轻气炮发射模型,模型直径分别为8.0、10.0、12.0、15.0 mm,速度约6 km/s,靶室压力分别为6.3,5.0,4.2,3.3 k Pa,采用阴影照相系统测量模型激波脱体距离、电子密度测量系统测量模型尾迹的电子密度分布、X波段单站雷达系统测量在视角为40?的模型及流场的雷达散射截面(RCS)分布.实验结果表明:在速度不变、双尺度参数相同的条件下,随着模型尺寸的增加,激波脱体距离逐渐增加,激波脱体距离与模型直径之比近似相同;不同模型尾迹电子密度测量曲线的趋势和数量级一致,表明不同模型的尾迹流场适用于双缩尺律;不同尺寸模型尾迹的总体RCS与分布RCS均不相同,表明不同模型尾迹的电磁散射不适用于二元缩尺律;高速球模型全目标电磁散射能量分布在模型及其绕流区域、等离子体尾迹区域;高速球模型全目标电磁散射能量在模型及绕流场区域出现1个强散射中心,在模型湍流尾迹区域出现多个散射中心;高速球模型尾迹的RCS测量信号呈现随机性分布特性,幅度脉动和频率脉动均没有周期性;随着模型尺寸的增加,模型尾迹的总体RCS增加,尾迹脉动频率的变化范围减小.     

电磁轨道炮接触热时空分布特性分析

电磁轨道炮接触热时空分布特性是进行电枢熔化抑制、轨道散热设计和热管理的重要依据。在建立电枢与轨道接触压力、接触电阻计算模型的基础上,建立了接触热时空分布的计算模型,对电磁轨道炮的接触热时空分布进行了仿真计算,并对其特性进行了分析。针对接触热在电枢运动初始阶段相对集中的问题,研究了电枢前级加速对接触热时空分布特性的影响。仿真分析结果表明:接触热主要来源于电流焦耳热,焦耳热功率曲线与驱动电流曲线具有较大相似性;大部分接触热在电枢运动初始阶段传导给轨道,这是引起此阶段轨道烧蚀的主要原因;电枢运动初始阶段单位长度轨道传导的接触热和发射过程中电枢的热积累随着电枢初速度的增大而减小。     

充电参数对聚丙烯蜂窝膜驻极体压电性的影响

通过接触法充电、恒压电晕充电，以及开路热刺激放电技术，对充电参数(例如充电电压，充电时间和充电温度等)对聚丙烯蜂窝膜(PP cellular)驻极体的压电性及其热稳定性的影响的研究，并从孔洞型薄膜压电体的材料结构和理论模型出发，讨论了这些参数对其影响的原因，分析了与压电活性密切相关的空间电荷的动态特性.结果表明，合理地优化充电参数，能使这类呈闭合孔洞的聚合物蜂窝膜驻极体的压电性及其稳定性得以改善，为拓宽这类新型压电功能膜应用领域，推动其产业化进程提供了一定的理论和技术依据. 关键词： 聚丙烯蜂窝膜 压电性 充电参数 电荷输运     

The dynamic characteristics of harvesting energy from mechanical vibration via piezoelectric conversion

As an alternative power solution for low-power devices, harvesting energy from the ambient mechanical vibration has received increasing research interest in recent years. In this paper we study the transient dynamic characteristics of a piezoelectric energy harvesting system including a piezoelectric energy harvester, a bridge rectifier, and a storage capacitor. To accomplish this, this energy harvesting system is modeled, and the charging process of the storage capacitor is investigated by employing the in-phase assumption The results indicate that the charging voltage across the storage capacitor and the gathered power increase gradually as the charging process proceeds, whereas the charging rate slows down over time as the charging voltage approaches to the peak value of the piezoelectric voltage across the piezoelectric materials. In addition, due to the added electrical damping and the change of the system natural frequency when the charging process is initiated, a sudden drop in the vibration amplitude is observed, which in turn affects the charging rate. However, the vibration amplitude begins to increase as the charging process continues, which is caused by the decrease in the electrical damping （i.e., the decrease in the energy removed from the mechanical vibration）. This electromechanical coupling characteristic is also revealed by the variation of the vibration amplitude with the charging voltage.     

Capacitive micromachined ultrasonic transducers (CMUTs) with isolation posts

In this paper, an improved design of a capacitive micromachined ultrasonic transducer (CMUT) is presented. The design improvement aims to address the reliability issues of a CMUT and to extend the device operation beyond the contact (collapse) voltage. The major design novelty is the isolation posts in the vacuum cavities of the CMUT cells instead of full-coverage insulation layers in conventional CMUTs. This eliminates the contact voltage drifting due to charging caused by the insulation layer, and enables repeatable CMUT operation in the post-contact regime. Ultrasonic tests of the CMUTs with isolation posts (PostCMUTs) in air (electrical input impedance and capacitance vs. bias voltage) and immersion (transmission and reception) indicate acoustic performance similar to that obtained from conventional CMUTs while no undesired side effects of this new design is observed.     

Electrostatic charging of a conducting sphere using another conducting sphere at constant voltage

This study uses results of classical electrostatics to predict the resulting voltage of a conducting sphere that is charged by a second sphere maintained at a constant voltage. The voltage of the charged sphere is calculated as a function of the charging voltage and the size ratio of the two spheres. Theoretical predictions are verified experimentally using conducting spheres of various sizes and a Faraday ice pail apparatus. The results may seem somewhat counterintuitive. For example, a charging sphere held at 100 V will charge another sphere of equal size only to 69.3 V by contact.     

电子辐照下聚合物介质内部放电模型研究

空间电子辐照环境中,聚合物介质充放电现象是威胁航天器安全的重要因素. 传统航天器介质充放电模型仅能分析材料充电过程,缺乏对放电前后介质电位残余情况与放电脉冲强弱的评估. 本文通过引入介质放电电导率,在数值积分 充电模型基础上建立同时描述航天器介质内部充电和放电过程的新模型,并将模型计算结果与实验数据进行比较,验证了所构建的模型. 模型分析结果表明,聚合物介质放电残余电位与放电电流脉冲宽度随着样品电阻率的增加而增大,放电电流强度随着临界电场强度和充电时间的增加而增强,其增幅随着辐照电子束流强度的增加而增大. 关键词： 放电模型 内部放电 电子辐照 航天器介质     

Influence of the corona-wire diameter and length on corona discharge characteristics of a cylindrical tri-axial charger

In this paper, the corona discharge characterization in terms of current–voltage relationships of a unipolar cylindrical tri-axial charger on the effects of the corona wire diameter and length have been experimentally studied and discussed. A commercial computational fluid dynamics software package, COMSOL Multiphysics™, was used to predict the electric field distribution in the ion generation and charging zones of the charger and the ion penetration through the perforated screen opening on the inner electrode of the charger. It was found from experimental results that both positive and negative charging currents in the charging zone of the charger increased with increasing corona and ion-driving voltages. At the same corona and ion-driving voltages, both positive and negative coronas were decreased with increasing diameter of the corona-wire. Compared with the corona-wire of 22 mm in length, the magnitude of both positive and negative charging currents were markedly higher for corona-wire of 11 mm in length at the same corona voltage. It was found that the charging currents for negative coronas were about 1.2 times higher than those positive coronas at the same corona and ion-driving voltages. Numerical results of the electric field distribution and the ion and charged particles migrations in the discharge and charging zones of the charger is correlated to have the same direction with the experimental results of the current–voltage relationships. Also, this can be used to guidance in describing the electric field distribution and the behavior of ion and charged particle trajectories that cannot be seen from experiments in order to improve the applicably design and refinement of a unipolar cylindrical tri-axial charger.     

Electrostatic charging of micro- and nano-particles for use with highly energetic applications

Electrostatically charging spherical and cylindrical conducting particles against an electrode with an applied electric field is investigated both theoretically and experimentally as a method of charging micro- and nano-particles for use with a variety of high energy and high velocity applications, which include nano-particle electrostatic space propulsion systems, materials processing, and nano-printing. Increasing the particles' charge-to-mass ratios is critical for maximizing their velocities when accelerated with applied electric fields, which requires minimizing the particles' sizes down to the micro- and nano-meter ranges for some applications. An analysis reveals that the charge-to-mass ratio is maximized with low aspect ratio particles when the maximum electric field strength, which is at the top of the particles, is held constant. Experimental results of charging titanium and aluminum spherical and cylindrical particles are presented, which suggest that under appropriate conditions, the particles are charged as predicted by theory. But that electrical contact resistance between the particles and electrode can influence the charging time. An analysis of the expected particle charging times is presented, which shows a strong dependence on the conductivity and thickness of the oxide layer coating the particles.     

ChargingE-perm for radon measurements

Recharging of commercial E-perm electret detectors used for radon measurement has been investigated. The E-perm was recharged using the poling charging method where a high voltage is applied on a metal nozzle to polarize the electret material. The optimum parameters to recharge the electrets were 5 kV charging voltage and 7 mm height of the nozzle from the electret surface and using an insulator while charging. Under these conditions, charging of E-perm carried out for 15 s attained required voltage and retained the charge for long durations. The response of recharged E-perm for radon activity measurements in a radon calibration chamber and in an open environment was compared with that of CR-39 detectors. Results showed close proximity in radon values.     

传输线充电技术实现高功率亚纳秒电磁脉冲调制

 分析比较了阻抗匹配和失配情况下传输线充电的原理和波过程。分析结果表明：失配情况下的最大优点是能够实现脉冲功率增益。应用阻抗为27 W、长度为540 mm传输线为充电传输线和长度分别为30,45,60 mm、阻抗均为5 W传输线为被充电传输线进行了对比试验。实验结果表明：在距离辐射天线6 m处，输出辐射场强随低阻抗传输线长度增加而略有增加，最大辐射场强为49 kV/m,考虑气体开关的实际能量损耗，这与理论分析的充电电压和功率增益关系相吻合；长度为45 mm的5 W被充电传输线的输出脉冲前沿约210 ps,幅度约为150 kV。