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Controlled atomization using a twin-fluid swirl atomizer

机译:使用双流体旋流雾化器控制雾化

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This paper presents the results of an experimental study of a twin-fluid internally mixed swirl atomizer. In this type of injectors, atomization is attained by injecting a small amount of air (i.e. of the order of less than 16% of the mass flow rate of liquid) into a liquid stream within the injector and the two-phase air liquid mixture is passed through a swirling passage to impart a swirling motion to the flow. Since most of the energy for atomization is supplied to the liquid by the atomizing air, a significantly small pressure drop can produce very fine spray with a small amount of atomizing air. At low values of air–liquid mass ratio (ALR), the appreciable tangential component of velocity with respect to the axial velocity provides a hollow cone spray structure, which turns into a solid cone spray with the increase in axial momentum, through either an increase in ALR or the liquid supply pressure. The results presented in this paper suggest that the investigated injector could be used to control the flow rate and spray characteristics (e.g. spray cone angle, spray solidity, breaking distance, and the droplet diameter) independent of each other by simultaneously varying the supply pressure of the liquid and the atomizing air flow rate. The controlled atomization studied in this paper for a twin-fluid internally mixed swirl atomizer makes it attractive to be used for various commercial applications as the atomizer is capable of providing various spray characteristics depending upon the application requirement.
机译:本文介绍了双流体内部混合旋流雾化器的实验研究结果。在这种类型的喷射器中,通过向喷射器内的液流中注入少量空气(即小于液体质量流率的16%左右)来实现雾化。通过涡流通道使流体产生涡流运动。由于雾化的大部分能量是由雾化空气提供给液体的,因此,很小的压降可以用少量的雾化空气产生非常细的喷雾。在较低的气液质量比(ALR)值时,相对于轴向速度的明显切向速度分量提供了空心圆锥形喷雾结构,随着轴向动量的增加,空心圆锥形喷雾变为固体圆锥形喷雾,通过增加在ALR或液体供应压力中。本文介绍的结果表明,可以通过同时改变泵的供给压力来相互独立地控制所研究的喷射器来控制流量和喷射特性(例如喷射锥角,喷射固体,破裂距离和液滴直径)。液体和雾化空气的流速。本文针对双流体内部混合旋流雾化器研究的受控雾化使其具有诱人的吸引力,因为该雾化器能够根据应用需求提供各种喷雾特性,因此可用于各种商业应用。

著录项

  • 来源
    《Experiments in Fluids》 |2006年第4期|649-663|共15页
  • 作者

    J. Karnawat; A. Kushari;

  • 作者单位

    Department of Aerospace Engineering Indian Institute of Technology Kanpur India;

    Department of Aerospace Engineering Indian Institute of Technology Kanpur India;

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  • 正文语种 eng
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