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Investigation on the internal flow characteristics of pressure-swirl atomizers.

机译:压力旋流雾化器内部流动特性的研究。

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摘要

The performance of liquid fuel atomizer in gas turbine combustor has direct effects on flame stability, combustion efficiency, and pollutant emissions. Therefore, further understanding of the underlying physics of these atomizers is one of the primary requirements for advanced gas turbine combustor design. Simplex atomizers are commonly used in air-breathing gas turbine engines because they produce good atomization characteristics and are relatively simple and inexpensive to manufacture. Internal flow characteristics of simplex nozzles play a very important role on the atomizer performance. So it is of great practical interest to examine the relationships between internal flow characteristics, nozzle design variables, and important spray features.; Part I of this dissertation revealed the detailed flow structure inside simplex atomizers through the DPIV and LDV study. The internal flow field is generally symmetric except very near the inlet slot plane. The velocity profiles are very similar at different axial locations within the swirl chamber. The discharge parameters were measured and used to examine the correlations from previous researchers. Detailed flow field information was linked with the discharge parameters to obtain more insight into the nozzle performance. The relationship between the internal flow characteristics and discharge parameters confirmed that the internal flow structure plays a very important role on the atomizer performance.; Part II presents the internal flow structure of large-scale simplex nozzles at two different working-fluid/ambient-fluid density ratios. The effects of density ratio, Reynolds number and orifice geometry on the internal flow field were examined by using a 2-D LDV probe. At the higher density ratio, Reynolds number and orifice geometry has little impact on the internal flow field. At the lower density ratio, the orifice contraction angle has little effect on the internal flow field, whereas the expansion angle can significantly affect the internal flow structure. A dominant frequency was found from the velocity frequency analysis, which indicates that the internal flow is controlled by certain dominant frequency. A dimensionless vortex shedding frequency, similar to the Strouhal number in the flow past a cylinder, was defined using the orifice diameter and mean axial velocity in the orifice.; In the part III of this dissertation, the internal flow field of the simplex atomizer with macrolaminated geometry was measured using the refractive index matching fluid method and DPIV system. In the swirl chamber, the liquid flow shows unsteady three-dimensional features, which is more evident as the flow rate increases. In the orifice, the liquid flow is more uniform and axisymmetric. The discharge parameters were measured and compared with the correlations from previous researchers.
机译:燃气轮机燃烧室中液体燃料雾化器的性能直接影响火焰稳定性,燃烧效率和污染物排放。因此,进一步了解这些雾化器的基本物理原理是高级燃气轮机燃烧室设计的主要要求之一。单缸雾化器通常用于呼吸式燃气涡轮发动机,因为它们产生良好的雾化特性,并且制造起来相对简单且便宜。单纯形喷嘴的内部流动特性对雾化器的性能起着非常重要的作用。因此,研究内部流动特性,喷嘴设计变量和重要的喷雾特性之间的关系具有重大的实践意义。本文的第一部分通过DPIV和LDV研究揭示了单工雾化器内部的详细流动结构。除了非常靠近入口槽平面之外,内部流场通常是对称的。速度分布在涡流室内的不同轴向位置非常相似。测量了排放参数,并将其用于检查先前研究人员的相关性。详细的流场信息与排放参数相关联,以获得对喷嘴性能的更多了解。内部流动特性与排放参数之间的关系证实,内部流动结构对雾化器性能起着非常重要的作用。第二部分介绍了两种不同工作流体/环境流体密度比的大型单工喷嘴的内部流动结构。使用2-LDVDV探针检查密度比,雷诺数和孔口几何形状对内部流场的影响。在较高的密度比下,雷诺数和孔口几何形状对内部流场影响很小。在较低的密度比下,孔口收缩角对内部流场影响很小,而膨胀角会显着影响内部流场结构。从速度频率分析中发现了一个主导频率,这表明内部流动受某些主导频率控制。使用孔口直径和孔口中的平均轴向速度来定义无量纲的涡旋脱落频率,类似于通过圆柱体的流动中的斯特劳哈尔数。在本文的第三部分中,使用折射率匹配流体法和DPIV系统测量了具有大分层结构的单面雾化器的内部流场。在旋流室中,液体流显示出不稳定的三维特征,随着流速的增加,这一点更加明显。在孔口中,液体流动更均匀且轴对称。测量了排放参数,并将其与先前研究人员的相关性进行了比较。

著录项

  • 作者

    Ma, Zhanhua.;

  • 作者单位

    University of Cincinnati.;

  • 授予单位 University of Cincinnati.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 214 p.
  • 总页数 214
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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