Abstract

A coaxial dielectric barrier discharge plasma-assisted combustion actuator (DBD-PACA) system was set up to study its discharge and optical emission spectrum (OES) characteristics in space in this paper. Results showed that each discharge cycle can be divided into four stages: a, b, c, and d. Discharge-on only occurred in stages b and d. Comparatively, the discharge intensity was larger in stage d due to the memory effect of excited electrons. Moreover, Lissajous figure and current-voltage methods were utilized to calculate the power of the coaxial DBD-PACA, and both methods produced roughly similar results. The power presented an upward trend with increasing input voltage and airflow rate. In addition, numerous second positive system (SPS) excited nitrogen molecules were detected from the OES signals. The intensity of the spectral lines (297.54 nm, 315.76 nm, 336.96 nm, and 357.56 nm) first increased, then maintained, and then increased rapidly with the increased radius; however, the intensity of the spectral lines (380.34 nm, 405.80 nm, and 434.30 nm) basically remained unchanged, then increased, and finally decreased with the increased radius. The vibrational temperature first decreased quickly and then increased and reached the minimum at r = 18 mm with the increased radius. The vibrational temperatures at all collection points decreased with the increased input voltage. However, within the range of 0–280 L/min, when r was lower than 15 mm, the vibrational temperatures first increased rapidly and then decreased slowly; when r was greater than 15 mm, the vibrational temperatures first increased and then basically remained stable.

Highlights

  • Plasma, which is an equal density of negative and positive particles ionized gas, belongs to the fourth state of matter and is composed of charged particles, atoms, radicals, molecules in ground and excited states, and photons [1, 2]

  • plasma-assisted combustion (PAC) is a remarkable solution to enlarging stable combustion boundary, improving combustion stability and combustion efficiency, and lowering nitric oxide emissions; it addresses these issues at a low energy cost, as put forward and studied by numerous relevant experts [8,9,10,11]. e superior performance of the PAC actuator (PACA) is the key of PAC technology, and numerous plasma discharge devices, such as dielectric barrier discharge (DBD) [12,13,14,15], pulsed corona [16], microwave discharges [17], and gliding arc [18], were investigated to improve combustion

  • The current contained a series of intermittent high-amplitude spikes. e coaxial DBD-PACA discharge contained numerous filament channels with continuous formation and extinguishment, which resulted in the appearance of spikes [30]. e phase difference between the applied voltage and charge was approximated 6 μs

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Summary

Introduction

Plasma, which is an equal density of negative and positive particles ionized gas, belongs to the fourth state of matter and is composed of charged particles (electrons and ions), atoms, radicals, molecules in ground and excited states, and photons [1, 2]. PAC is a remarkable solution to enlarging stable combustion boundary, improving combustion stability and combustion efficiency, and lowering nitric oxide emissions; it addresses these issues at a low energy cost, as put forward and studied by numerous relevant experts [8,9,10,11]. E superior performance of the PAC actuator (PACA) is the key of PAC technology, and numerous plasma discharge devices, such as dielectric barrier discharge (DBD) [12,13,14,15], pulsed corona [16], microwave discharges [17], and gliding arc [18], were investigated to improve combustion. Journal of Spectroscopy of absorbed energy by DBD actuator grew with temperature and the energy input determined the gap infill. Tang et al [21] studied the effects of airflows on a multicathode DBD and found that the discharge intensity increased along the direction of airflow

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