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Diagnostic study of low pressure supersonic DC plasma jets by emission spectroscopy and enthalpy probe techniques.

机译:发射光谱和焓探头技术对低压超声直流等离子体射流的诊断研究。

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In this work, the characteristics of plasma jets produced by a commercial DC plasma spray torch connected to a controlled pressure chamber are investigated. The plasma gas employed is a mixture of argon, nitrogen and hydrogen with the initial gas flow rates of 40, 10, and 1 SLPM respectively. The plasma torch is operated at chamber pressures of 6.5, 13, 26, 39, 53 and 101 kPa and a fixed input power of 17.5 kW.; Optical emission spectroscopy is used to measure the temperatures and electron density profiles. The measurements of temperature are carried out by means of a Boltzmann plot of several isolated argon atom spectral lines. The electron density is measured from the Stark broadening of the HR line 486.1 nm and the continuum emissivity. Partially resolved spectra of the N 2+ molecular band are used for the rotational temperature evaluation. The rotational emission from the (0,0) band of the first negative system is compared to synthetic spectra to evaluate the rotational temperature within the flow field. Finally, the measurements of the gas kinetic temperature and the plasma velocity are performed by the enthalpy probe technique.; The experimental results show the occurrence and the position of the different gas dynamics zones; i.e., supersonic expansion, stationary shock front and subsonic relaxation at low pressures (less than 40 kPa). The plasma flow is accelerated to its maximum velocity at the expansion where a minimum in the electron density and temperature is observed. At the end of the expansion a stationary shock front occurs at 4, 8, 12, and 15 mm downstream from the nozzle exit at pressures 39, 26, 13 and 6.5 kPa respectively. The electron density profiles show the variations along the plasma axis that coincide with the position of the shock waves. Good agreement between the electron density results obtained from the Stark broadening and from the continuum emissivity is observed.; Enthalpy probe measurements on gas kinetic temperature and plasma velocity reveal the general features of low pressure plasma jets, i.e., higher flow velocity and longer heating zone of expanded plasma with lower temperature. The measurements also coincide with the rotational temperature obtained from emission spectroscopy.; The temperature results confirm that the local thermodynamic equilibrium LTE exists at pressures of 100 and 53 kPa. However, at lower pressures where the supersonic shock waves are formed, the slow energy exchange between the heavy and light particles leads to significant deviations from the LTE especially in the shock region.
机译:在这项工作中,研究了由与受控压力室相连的商用DC等离子喷枪产生的等离子流的特性。使用的等离子气体是氩气,氮气和氢气的混合物,初始气体流速分别为40、10和1 SLPM。等离子炬的腔室压力为6.5、13、26、39、53和101 kPa,固定输入功率为17.5 kW。发射光谱用于测量温度和电子密度分布。温度的测量是通过几条孤立的氩原子光谱线的玻尔兹曼图进行的。电子密度是根据HR线486.1 nm的Stark展宽和连续发射率测得的。 N 2 + 分子带的部分分辨光谱用于旋转温度评估。将来自第一个负系统的(0,0)波段的旋转发射与合成光谱进行比较,以评估流场内的旋转温度。最后,通过焓探针技术进行气体动力学温度和等离子体速度的测量。实验结果表明了不同气体动力学区域的发生和位置。即在低压(小于40 kPa)下超音速膨胀,静止冲击波前和亚音速松弛。在观察到电子密度和温度最小的膨胀处,等离子体流被加速到其最大速度。在膨胀结束时,在压力分别为39、26、13和6.5 kPa的情况下,在喷嘴出口下游的4、8、12和15mm处出现静止的激波锋。电子密度分布显示出沿着等离子体轴的变化,该变化与冲击波的位置一致。观察到由斯塔克展宽获得的电子密度结果与连续谱发射率之间的良好一致性。焓探针对气体动力学温度和等离子体速度的测量揭示了低压等离子体射流的一般特征,即较高的流速和较低温度下膨胀的等离子体的较长加热区域。测量结果也与从发射光谱学获得的旋转温度一致。温度结果证实了局部热力学平衡LTE存在于100和53kPa的压力下。但是,在形成超声波冲击波的较低压力下,重粒子和轻粒子之间的缓慢能量交换会导致与LTE的明显偏离,尤其是在冲击区域。

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