分析型电感耦合等离子体及其尾焰动态特性的实验研究

IF 3.1 2区 化学 Q2 CHEMISTRY, ANALYTICAL
Xin Han, Yongyang Su, Zhiming Li, Yuxuan Wang, Wei Wang, Ruiyang Xi, Shiyou Zhou, Guanyi Wei, Sui Fang, Yalong Wang, Jiang Xu and Xiaofei Lan
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引用次数: 0

摘要

已经为分析和工业ICP源开发了许多数值模拟模型;因此,实验验证是必不可少的。与等离子体温度相比,流速分布是一个直接、可靠的模型验证标准。本文利用高速彩色摄像机和高速光纤光谱仪对国产ICP分析源及其尾焰的动态特性进行了实验研究,得到了空间分辨的脉动频率和流动速度。实验确定了等离子体区域的脉动频率和发射强度。空间分辨的脉动频率表明,正常分析区(NAZ)的脉动非常稳定和同步,尾焰由于周围空气的夹带而波动。通过跟踪注入的氧化铝粉末颗粒的运动轨迹来表征冷却剂气体中的流动速度。在修正了具有高惯性的粉末颗粒与周围气流之间的速度差后,提出了冷却剂气体外缘轴向(Vz)和径向(Vr)速度的合理范围。通过跟踪和插值由单个铒悬浮粒子产生的离散铒离子云的速度,实验确定了NAZ下游轴上的流速。通过对模拟的轴向速度剖面与实验剖面的比较,估计现有ICP设备的功率耦合效率在80%左右。在0≤z≤50mm范围内,给出了Vz随轴向位置(z)变化的线性表达式。由于铒离子云与NAZ内非常明亮的发射背景难以区分,提出了一种结合等离子体脉动音频对流动速度曲线、模拟轴向速度曲线和脉动频率实验值的依赖关系来确定NAZ内流动速度的新方法。在1200w射频功率下,火炬出口轴向速度的测定值与拟合值吻合较好。这项工作提供了完整的实验数据,在一个单一的ICP设施流速和实验验证了以前开发的二维数值模型。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Experimental study on the dynamic characteristics of an analytical inductively coupled plasma and its tail flame†

Experimental study on the dynamic characteristics of an analytical inductively coupled plasma and its tail flame†

Many numerical simulation models for analytical and industrial ICP sources have been developed; hence, experimental verification is essential. Compared with plasma temperature, the flow velocity profile is a direct and reliable criterion for model verification. In this paper, an experimental study on the dynamic properties of a home-made analytical ICP source and its tail flame is conducted using a high-speed colour camera and a high-speed fibre-optic spectrometer, and the spatially resolved pulsation frequency and flow velocity are presented. The pulsation frequencies of the plasma area and emission intensity were experimentally determined, respectively. The spatially resolved pulsation frequency indicates that pulsation of the normal analytical zone (NAZ) is very stable and synchronous, and the tail flame fluctuates due to ambient air entrainment. The flow velocity in the coolant gas was characterised by tracking the trajectories of injected alumina powder particles. After correcting for the velocity difference between the powder particle with high inertia and the surrounding flow, a plausible range of axial (Vz) and radial (Vr) velocity at the outer edge of the coolant gas is proposed. The flow velocity on the axis downstream of the NAZ was experimentally determined by tracking and interpolating the velocity of discrete erbium ion clouds originating from individual erbia suspension particles. By comparing the simulated profile of axial velocity with the experimental profile, the power coupling efficiency of the present ICP facility is estimated to be around 80%. A linear expression is presented to describe the variation of Vz with the axial position (z) in the range of 0 ≤ z ≤ 50 mm. Because erbium ion clouds were not distinguishable from the very bright emission background within the NAZ, a novel method is proposed to determine the flow velocity in the NAZ by combining the dependence of the audio frequency of plasma pulsation on the flow velocity profile, the simulated profile of axial velocity, and the experimental value of pulsation frequency. The determined value of axial velocity at the torch outlet axis operating at an r.f. power of 1200 W is in good agreement with the fitted value. This work presents complete experimental data on flow velocity in a single ICP facility and experimentally verifies the previously developed 2D numerical model.

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来源期刊
CiteScore
6.20
自引率
26.50%
发文量
228
审稿时长
1.7 months
期刊介绍: Innovative research on the fundamental theory and application of spectrometric techniques.
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