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两间隙毛细管等离子体发生器出口参数研究 被引量:2

Studies on the Exit Parameters of an Ablative Capillary Discharge Plasma Generator
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摘要 消融放电毛细管等离子体发生器产生的等离子体射流具有高密和相对低温的特性,在许多科学研究和工业应用领域都具有潜在的应用前景。为此,利用数值模拟的方法考察了在1 kJ放电能量水平下两间隙毛细管的长度和半径、主放电电容器组的电容和起始充电电压等放电参数对毛细管出口参数的影响。研究表明,各放电参数的改变都能引起出口处的质量密度、压强的大幅度改变,而出口温度和出口速度相对保持稳定。其中,主放电电容器组充电电压、电容值增大、毛细管半径变小时,所有的出口参数都相应增大;而毛细管长度增大时,密度和压强随之增大,温度和速度反而减小。 Ablative capillary discharge plasma jets are characterized by high density and relatively low temperature. The devices of this kind of plasma jets are of importance to a variety of applications. Two-gap capillary plasma generator (TGCPG) is a realistic alternative to the conventional capillary in electrothermal launchers and a versatile capillary plasma generator for other applications. It is designed to accomplish two goals: repetitive operation and a compact power supply system in which capillary itself serves as a closing switch, thus the conventional closing switches in the power supply system can be eliminated. The TGCPG is composed of two gaps and three electrodes, differing from the conventional capillary in which it contains a trigger circuit and a trigger electrode (TE). When the triggering high-voltage pulse is applied, the first gap between the cathode and the TE is broken down, and a small energy stored in trigger circuit is dissipated into this gap, then a plasma jet is formed, which can flow into the second gap between the anode and the TE to ignite the main discharges between the anode and the cathode. The exit parameters of TGCPG including mass density, pressure, temperature and velocity are of vital for application purposes, from which the properties of the plasma jets can be calculated. In this paper, theoretical calculations of the main discharges of TGCPG are performed with a one-dimensional (1-D), time-dependent plasma model. Some numerical results about the influence of capillary size, capacitance of the main discharge capacitor bank and its initial charged voltage to the exit parameters of TGCPG are obtained. It is found that the mass density and pressure can be drastically changed while the temperature and velocity of the plasma jets are relatively stable. Both an increase of capacitance or voltage and a decrease of capillary radius will lead to an increase of all exit parameters; on the other hand, an increase of capillary length will leads to an increase of the mass density and pressure, but a decrease of temperature and velocity.
出处 《高电压技术》 EI CAS CSCD 北大核心 2006年第6期72-74,112,共4页 High Voltage Engineering
关键词 消融放电 等离子体发生器 等离子体射流 数值模拟 出口参数 ablative capillary discharge plasma generator plasma jet numerical calculation exit parameter
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参考文献17

  • 1夏胜国,刘克富,刘明海,潘垣.高能毛细管放电技术的应用综述[J].高电压技术,2001,27(5):32-33. 被引量:6
  • 2Liu Kefu, Xia Shengguo, Qin Shihong, et al. A novel capillary plasma switch (CPS) for electrothermal launchers[J]. IEEE Trans on Magnetics, 2003, 39(1): 398-401.
  • 3Katulka G L, Khong T N, Burden H, et al. Measurement techniques for electrothermal-chemical gun diagnostics:AD-A273952[R].USA:Army Research Laboratory ( ARL), 1993.
  • 4Powell J D, Zielinski A E. Capillary discharge in the electrothermal gun[J]. IEEE Trans on Magnetics, 1993, 29(1): 591-596.
  • 5Zoler D, Cuperman S. Quasi-one-dimensional model equations for plasma flows in high-pressure discharges in ablative capillaries[J]. J Plasma Phys, 1992, 48(3):215-231.
  • 6Ogurtsova N N, Podmoshenskii I V, Rogovtsev P N. Caleulation of the parameters of an optically dense plasma obtained by a discharge with an evaporating wall[J].High Temp, 1971, 9(2):430-438.
  • 7Kovitya P,Lowke J J. Theoretical prediction of ablation stabilized arcs confined in cylindrical tubes[J], J Phys D: Appl Phys, 1984, 17(4):1197-1209.
  • 8Loeb A. Kaplan Z. A theoretical model for the physical processes in the confined high pressure discharge of electrothermal launchers[J]. IEEE Trans on Magnetics, 1989, 25(1):342-354.
  • 9Gilligan J G, Mohanti R B. Time-dependent numerical simulation of ablation-controlled arcs[J]. IEEE Trans on Plasma Sci, 1990, 18(1):190-194.
  • 10Hurley J D, Bourham M A, Gilligan J G, Numerical simulation and experiment of plasma flow in the electrothermal launcher SIRENS[J].IEEE Trans on Magnetics, 1995, 31(1):616-621.

二级参考文献19

  • 1[1]Powell J D, Zielinski A E. Theory and experiment for an ablating capillary discharge and application to electrothermal-chemical guns. BRL-3355, 1992
  • 2[2]Zoler D, Cuperman S A. Time-dependent model for high-pressure discharges in narrow ablative capillaries. Plasma Physics, 1993, 50:51
  • 3[3]Melnek D et al. ETC technology development at soreq NRC, Israel. IEEE Trans Magnetics, 1999, 35(1):31
  • 4[4]Wald S et al. Hazardous waste treatment and recovery of valuable products with a thermal pulsed-plasma technology. IEEE Trans P S, 2000, 28(5):1576
  • 5[5]Wald S et al. Hard coatings of metals and ceramics with a new electrothermal-chemical gun technology. International Journal of Refractory metals & hard Materials, 1999, 171:7
  • 6[6]Rott M, Igenbergs E. New monopulse plasma generation and acceleration facility for surface treatment. IEEE Trans Magnetics, 2001, 37(1):232
  • 7[7]Peterson D R. Design and operation of the electrogun, an electrothermal gun for producing metal and carbon plasma jets. IEEE Trans Magnetics, 1997, 33(1):373
  • 8[8]Salge G H et al. Mass acceleration by plasma pulse. IEEE Trans Magnetics, 1989, 25(1):495
  • 9[9]Rott M. The LRT/TUM small caliber electrothermal accelerator. IEEE Trans Magnetics, 1993,29(1):597
  • 10[10]Shcolnikov E Y et al. Flow dynamics and microparticles acceleration in the electrothermal launcher. IEEE Trans magnetics, 1999, 35(1):240

共引文献6

同被引文献40

  • 1Wald S, Pokryvailo A, Appelbaum G, et al. Hazardous waste treatment and recovery of valuable products with a thermal pulsed-plasma technology[J]. IEEE Trans. Plasma Science, 2000, 28(5): 1576-1580.
  • 2Wald S, Appelbaum A G, Alimi R, et al. Hard coatings of metals and ceramics with a new electrothermal-chemical gun technology [J]. International Journal of Refractory Metals &Hard Materials, 1999, 17(1-3): 171-177.
  • 3Shcolnikov E Y, Guzeyev M Yu, Maslennikov S P, et al. Flow dynamics and microparticles acceleration in the Electrothermal Launcher[J]. IEEETrans. Magnetics, 1999, 35(1): 240-244.
  • 4Rott M, Igenbergs E. New monopulse plasma generation and acceleration facility for surface treatment[J]. IEEE Trans. Magnetics, 2001, 37(1): 232-237.
  • 5Peterson D R. Design and operation of the electrogun, an electrothermal gun for producing metal and carbon plasma jets [J]. IEEETrans. Magnetics, 1997, 33(1): 373-378.
  • 6Loeb A, Kaplan Z. A theoretical model for the physical processes in the confined high pressure discharge of electrothermal launchers [J]. IEEE Trans. Magnetics, 1989, 25(1): 342-346.
  • 7Liu Kefu, Xia Shengguo, Qin Shihong, et al. A novel capillary plasma switch (CPS) for electrothermal launchers[J]. IEEE Trans. Magnetics, 2003, 39(1): 398-401.
  • 8Spector N, Kaplan Z, Loeb A, et al. Confined high pressure discharge experiments[J]. IEEE Trans. Magnetics, 1989, 25(1): 538-540.
  • 9Powell J, and Zielinski A E. Theory and experiment for an ablating-capillary discharge and applications to electrothermalchemical guns[R]. Tech. Report BRL-TR-3355, U.S. Army Ballistic Research Laboratory, 1992.
  • 10Niemeyer L. Evaporation dominated high current arcs in narrow channels[J]. IEEE Trans. on Power Apparatus and Systems, 1978, PAS-97 (3): 950-958

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