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三维旋转滑动弧等离子体助燃激励器的光谱特性实验

何立明 张达 陈一 雷健平 张磊 张圣武 朱春昶 杨兴魁

空军工程大学学报(自然科学版)2017,Vol.18Issue(4):1-6,6.
空军工程大学学报(自然科学版)2017,Vol.18Issue(4):1-6,6.DOI:10.3969/j.issn.1009-3516.2017.04.001

三维旋转滑动弧等离子体助燃激励器的光谱特性实验

An Experiment of Spectral Characteristics on Plasma-assisted Combustion with 3D Rotating Gliding Arc Discharge

何立明 1张达 1陈一 1雷健平 1张磊 1张圣武 1朱春昶 1杨兴魁1

作者信息

  • 1. 空军工程大学航空航天工程学院,西安,710038
  • 折叠

摘要

Abstract

In view of studying the spectral characteristic laws of plasma-assisted combustion with 3D rotating gliding arc discharge under different jet flow and voltages, three kinds of electrodes (A, B, C) withdifferent geometrical structures are investigated upon its spectral signalsof gliding arc discharge plasma alternating current under atmosphericpressure.The results demonstrate that the vibrational temperaturesbecome higher with increase of jet flow and voltage, that is, vibrational excitation intensity becomes fiercer during discharging.Simultaneously, compared with the gliding arc discharge plasma spectral characteristics of another two electrodes, A with higher vibrational temperature of plasma during discharging is the best one to actuate the plasma.In consideration of factors mentioned above, the influence of flow rates onthe vibrational temperature is the most obvious.The larger the flow rate triggers, and the stronger the relative emission intensity of particles such as OH, O2 and O.For instance, the average emission intensity of O isabout 1 800 a.u.unit under 40 g/min (U0=120), and as the flow increasesto 100 g/min, the average emission intensity of O enlarges to 2 800 a.u.unit.

关键词

三维旋转滑动弧等离子体/助燃激励器/光谱特性/振动温度

Key words

3D rotating gliding arc discharge plasma/assisted combustionactuator/spectral characteristic/vibrational temperature

分类

航空航天

引用本文复制引用

何立明,张达,陈一,雷健平,张磊,张圣武,朱春昶,杨兴魁..三维旋转滑动弧等离子体助燃激励器的光谱特性实验[J].空军工程大学学报(自然科学版),2017,18(4):1-6,6.

基金项目

国家自然科学基金(51436008,51106179) (51436008,51106179)

空军工程大学学报(自然科学版)

OA北大核心CSCDCSTPCD

2097-1915

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