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ZHAO Bingbing(赵兵兵), HE Liming(何立明), DU Hongliang(杜宏亮), ZHANG Hualei(张华磊). Electrical Characteristics of an Alternating Current Plasma Igniter in Airflow[J]. Plasma Science and Technology, 2014, 16(4): 370-373. DOI: 10.1088/1009-0630/16/4/12
Citation: ZHAO Bingbing(赵兵兵), HE Liming(何立明), DU Hongliang(杜宏亮), ZHANG Hualei(张华磊). Electrical Characteristics of an Alternating Current Plasma Igniter in Airflow[J]. Plasma Science and Technology, 2014, 16(4): 370-373. DOI: 10.1088/1009-0630/16/4/12

Electrical Characteristics of an Alternating Current Plasma Igniter in Airflow

Funds: supported by National Natural Science Foundation of China (Nos. 50776100, 51106179)
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  • Received Date: January 03, 2013
  • The electrical characteristics of an alternating current (AC) plasma igniter were investigated for a working gas of air at atmospheric pressure. The discharge voltage and current were measured in air in both breakdown and stable combustion processes, respectively, and the current-zero phenomena, voltage-current (V -I) characteristics were studied for different working gas flow rates. The results indicated that the working gas between anode and cathode could be ionized to generate gas discharge when the voltage reached 8 kV, and the maximum current was 33.36 A. When the current came to zero, current-zero phenomena appeared with duration of 2 µs. At the current-zero moment, dynamic resistance between electrodes became extremely high, and the maximum value could reach 445 k?, which was the main factor to restrain the current. With increasing working gas flow rates, the gradient of V -I characteristic curves was increased, as was the dynamic resistance. At a constant driven power, the discharge voltage increased.
  • 1 Klimov A, Bityurin V, Moralev I, et al. 2005, Plasma Assisted Ignition and Combustion. AIAA, 2005-3428;
    2 Klimov A, Bityurin V, Kuznetsov A, et al. 2005, Non-Premixed Plasma-Assisted Combustion in High-Speed Airflow. AIAA, 2005-0599;
    3 Klimov A, Bitiurin V, Moralev I, et al. 2007, Non-Premixed Plasma-Assisted Combustion in High-Speed Vortex Airflow. AIAA, 2007-1388;
    4 Sy Stange, Yongho Kim, Vincent Ferreri, et al. 2005,IEEE Trans. Plasma Science, 33: 316;
    5 Pilla G, Galley D, and Lacosted D A. 2006, Influence of the Repetition Rate of a Nanosecond Pulsed Dis-charge on the Stabilization of a Turbulent Lean Pre-mixed Flame. AIAA, 2006-3243;
    6 Scott D Gallimore, Lance S Jacobsen. 2001, A Study of Plasma Ignition Enhancement for Aeroramp Injectors in Supersonic Combustion Applications [Ph.D]. Me-chanical Engineering of the Virginia Polytechnic Insti-tute and State University, Virginia, USA;
    7 Lance S Jacobsen, Campbell D Carter, Robert A Bau-rle. 2003, Toward Plasma-assisted Ignition in Scram-jets. AIAA, 2003-0871;
    8 Liu Jianbang, Paul Ronney, Wang Fei. 2003, Transient Plasma Ignition for Lean Burn Applications. AIAA,2003-0877;
    9 Igor Matveev, Svetlana Matveeva. 2005, Non-Equilibrium Plasma Igniters and Pilots for Aerospace Application. AIAA, 2005-0871 10 Pan Wenxia, Meng Xian, Wu Chengkang. 2005, Jour-nal of Engineering Thermophysics, 26: 677 (in Chi-nese) ;
    11 Wang Feng, He Liming, Cao Naochang. 2010, High Voltage Engineering, 36: 537 (in Chinese) ;
    12 Shao Xianjun, Zhang Guanjun, Zhan Jiangyang. 2011,High Voltage Engineering, 37: 1499 (in Chinese) ;
    13 Lan Yudan, He Liming, Du Hongliang. 2012, Atomic Energy Science and Technology, 45: 6 (in Chinese)
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