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首页> 外文期刊>Journal of Physics, D. Applied Physics: A Europhysics Journal >Modeling on plasma energy balance and transfer in a hollow cathode
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Modeling on plasma energy balance and transfer in a hollow cathode

机译:血浆能量平衡和空心阴极转移的建模

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摘要

The hollow cathode lifetime is largely determined by the dissipation of the active emitter material and the ion-induced sputtering erosion. These two critical factors are involved in the physical mechanisms of the internal energy balance and plasma energy transfer to the cathode walls. Based on particle kinetic dynamics and behaviour statistics, a plasma energy balance and transfer model for the hollow cathode was established. The hollow cathode discharge process and steady-state plasma parameters were investigated by employing the self-consistent full particle-in-cell approach combined with Monte Carlo collisions. Relevant 2D numerical simulations for the partially ionized gas in hollow cathode were performed. The calculated parameters of the plasma energy balance and transfer model mainly include the plasma potential, plasma density, particle velocity, resistivity distribution, ohmic heating and electric-field work. In the full particle-in-cell code, the hollow cathode operated at a planar diode regime with a discharge current of 10.0 A and a gas flow rate of 3.5 sccm. The simulation results show that the electric field power is 85.9 W in the insert region, 37.5 W in the orifice region and 147.4 W in the plume region, respectively. The work performed by the electron pressure gradient in the insert region, orifice region and plume region is in the ratio of about 1.2:1:5.3. The ion kinetic-energy flux is negligible compared with the electron kinetic-energy transfer.
机译:空心阴极寿命主要通过活性发射器材料的耗散和离子诱导的溅射腐蚀来决定。这两个关键因素涉及内部能量平衡和等离子体能量转移到阴极壁的物理机制。基于粒子动力学和行为统计,建立了空心阴极的等离子体能量平衡和转移模型。通过采用自我一致的全粒子内接近与蒙特卡罗碰撞相结合,研究了中空阴极放电过程和稳态等离子体参数。进行中空阴极中部分电离气体的相关2D数值模拟。等离子体能量平衡和转移模型的计算参数主要包括等离子体电位,等离子体密度,颗粒速度,电阻率分布,欧姆加热和电场工作。在完整的粒子内代码中,空心阴极在平面二极管状态下操作,排出电流为10.0a和3.5 sccm的气体流速。仿真结果表明,在孔区域中的插入区域中的电场功率为85.9W,孔区域中的孔区域中的37.5W和147.4W。通过插入区域,孔口区域和羽流区域中的电子压梯度执行的作品为约1.2:1:5.3的比率。与电子动能转移相比,离子动能通量可忽略不计。

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    Beihang Univ Sch Astronaut Key Lab Spacecraft Design Optimizat &

    Dynam Simul Minist Educ Beijing 100083 Peoples R China;

    Beihang Univ Sch Astronaut Key Lab Spacecraft Design Optimizat &

    Dynam Simul Minist Educ Beijing 100083 Peoples R China;

    Beihang Univ Sch Space &

    Environm Key Lab Spacecraft Design Optimizat &

    Dynam Simul Minist Educ Beijing 100083 Peoples R China;

    Beihang Univ Sch Astronaut Key Lab Spacecraft Design Optimizat &

    Dynam Simul Minist Educ Beijing 100083 Peoples R China;

    Beihang Univ Sch Instrumentat &

    Optoelect Engn Beijing 100083 Peoples R China;

    Beihang Univ Sch Astronaut Key Lab Spacecraft Design Optimizat &

    Dynam Simul Minist Educ Beijing 100083 Peoples R China;

    Beihang Univ Sch Space &

    Environm Beijing 100083 Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 应用物理学;
  • 关键词

    hollow cathode; full-PIC; plasma energy balance; energy transfer;

    机译:空心阴极;全拍;等离子能量平衡;能量转移;

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