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The Characteristics of Gliding Arc Plasma and Its Activating Effect for Ramjet Combustion

Author

Listed:
  • Jiulun Sun

    (Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China)

  • Di Jin

    (Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China)

  • Shengfang Huang

    (China Aerodynamics Research and Development Center, Mianyang 621000, China)

  • Kai Zhang

    (Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China)

  • Weiqi Chen

    (Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China)

  • Xinyao Cheng

    (Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China)

Abstract

In order to improve the combustion performance of a ramjet under low temperature and pressure, a gliding arc plasma actuator was designed based on a typical evaporation flameholder. The discharge characteristics, as well as the activating effect of single-channel and three-channel gliding arc plasma under different carrier gas flow rates, were studied. Results show that with the increase in the carrier gas flow rate, the average duration of the gliding arc discharge becomes shorter, while the average power increases, and the specific input energy decreases. Compared with single-channel discharge, three-channel discharge has higher discharge power and energy injection rate, which makes a bigger actuated space. Through gliding arc plasma, the kerosene is cracked and H 2 , CH 4 , C 2 H 2 , C 2 H 4 , C 3 H 6 and other small molecule components are produced. For three-channel gliding arc discharge, the effective cracking rate and the production rate of each component are higher than those of the single-channel discharge; both of them gradually increase with the increase in the carrier gas flow rate. The experiment results indicate that three-channel gliding arc plasma can effectively widen the ignition boundary and improve the combustion efficiency of ramjet combustion. The ignition pressure boundary is expanded from 60 kPa to 50 kPa under 390 K; the combustion efficiency is increased from 76% to 82%.

Suggested Citation

  • Jiulun Sun & Di Jin & Shengfang Huang & Kai Zhang & Weiqi Chen & Xinyao Cheng, 2022. "The Characteristics of Gliding Arc Plasma and Its Activating Effect for Ramjet Combustion," Energies, MDPI, vol. 15(12), pages 1-16, June.
  • Handle: RePEc:gam:jeners:v:15:y:2022:i:12:p:4260-:d:835435
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