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Experimental Study of the Flow Field in a Model Rotor-Stator Disk Cavity Using Particle Image Velocimetry.

机译:使用粒子图像测速技术的模型转子-定子盘腔内流场的实验研究。

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摘要

Modern day gas turbine designers face the problem of hot mainstream gas ingestion into rotor-stator disk cavities. To counter this ingestion, seals are installed on the rotor and stator disk rims and purge air, bled off from the compressor, is injected into the cavities. It is desirable to reduce the supply of purge air as this decreases the net power output as well as efficiency of the gas turbine. Since the purge air influences the disk cavity flow field and effectively the amount of ingestion, the aim of this work was to study the cavity velocity field experimentally using Particle Image Velocimetry (PIV).;Experiments were carried out in a model single-stage axial flow turbine set-up that featured blades as well as vanes, with purge air supplied at the hub of the rotor-stator disk cavity. Along with the rotor and stator rim seals, an inner labyrinth seal was provided which split the disk cavity into a rim cavity and an inner cavity. First, static gage pressure distribution was measured to ensure that nominally steady flow conditions had been achieved. The PIV experiments were then performed to map the velocity field on the radial-tangential plane within the rim cavity at four axial locations.;Instantaneous velocity maps obtained by PIV were analyzed sector-by-sector to understand the rim cavity flow field. It was observed that the tangential velocity dominated the cavity flow at low purge air flow rate, its dominance decreasing with increase in the purge air flow rate. Radially inboard of the rim cavity, negative radial velocity near the stator surface and positive radial velocity near the rotor surface indicated the presence of a recirculation region in the cavity whose radial extent increased with increase in the purge air flow rate. Qualitative flow streamline patterns are plotted within the rim cavity for different experimental conditions by combining the PIV map information with ingestion measurements within the cavity as reported in Thiagarajan (2013).
机译:当今的燃气轮机设计人员面临着将主流主流气体吸入转子-定子圆盘腔的问题。为了避免这种情况,在转子和定子盘的轮缘上安装了密封件,并将从压缩机排出的净化空气注入腔中。期望减少吹扫空气的供应,因为这会降低净功率输出以及燃气轮机的效率。由于吹扫空气会影响椎间盘腔的流场并有效地影响摄入量,因此本研究的目的是使用粒子图像测速技术(PIV)通过实验研究腔体的速度场。流量涡轮装置,具有叶片和叶片,在转子-定子盘腔的轮毂处提供吹扫空气。连同转子和定子轮缘密封件一起,提供了一个内部迷宫式密封件,它将盘形腔分成轮辋腔和一个内腔。首先,测量静压力计压力分布以确保达到名义上稳定的流量条件。然后进行PIV实验,将速度场映射到边缘腔内四个轴向位置的径向切线平面上;通过逐段分析PIV获得的瞬时速度图,以了解边缘腔流场。观察到,在低吹扫空气流量下,切向速度主导了腔体的流动,其优势随着吹扫空气流量的增加而减小。在轮辋腔的径向内侧,定子表面附近的负径向速度和转子表面附近的正径向速度表明腔中存在再循环区域,其径向范围随吹扫空气流速的增加而增加。根据Thiagarajan(2013)的报道,通过将PIV图信息与空腔内的摄入测量值相结合,可以在边缘空腔内针对不同的实验条件绘制定性流动流线型态。

著录项

  • 作者

    Pathak, Parag.;

  • 作者单位

    Arizona State University.;

  • 授予单位 Arizona State University.;
  • 学科 Engineering Mechanical.
  • 学位 M.S.
  • 年度 2013
  • 页码 94 p.
  • 总页数 94
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:41:59

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