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Experimental investigation of flow field characteristics in a mixed-flow trapped vortex combustor

机译:混合流动涡流燃烧器中流场特征的实验研究

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摘要

This paper describes an experimental investigation of flow field characteristics of a conceptual trapped vortex combustor (TVC). It is the first time that the novel TVC is evaluated for turboshaft engine that utilizes a single cavity to provide flame stabilization. A Particle Image Velocimetry (PIV) has been applied to observe the effect of inlet air velocity on the flow field patterns and velocity profiles in a three-dome sector test rig under atmospheric pressure and room temperature. Experiment results show that all average flow fields were stable and self-similar in the cavity in varying operating conditions. A counter-rotating vortex pair was created and safely locked in the cavity along the mainstream plane. As the inlet air velocity increased to 42 m/s, a third vortex was generated. A single dominant stream-wise vortex was spanned the entire cavity along the strut plane. There was a shift in the vortex center location of the strut plane and mainstream plane at the same inlet air velocity, which indicates the three dimensional nature of the flow field in the cavity. Further analysis of velocity profiles showed that flow fields remained stable. The velocity of the vortex downstream zone in the cavity was higher than that in the countercurrent zone. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:本文介绍了概念捕获涡流燃烧器(TVC)的流场特性的实验研究。这是第一次评估采用单腔的涡轮轴发动机提供火焰稳定的涡轮轴发动机。已经应用粒子图像速度(PIV)以观察在大气压和室温下三穹柄试验台中的流场图案和速度谱上的入口空气速度的影响。实验结果表明,在不同的操作条件下,所有平均流场在空腔中稳定和自相似。在主流平面上产生并安全地锁定在腔体中的反向旋转涡旋对。随着入口空气速度增加到42米/秒,产生第三涡流。沿着支柱平面跨越单个占优势流涡流。在支柱平面的涡旋中心位置和在相同的入口空气速度下存在换档,其表示腔中的流场的三维性质。进一步分析速度剖面显示流场保持稳定。腔内涡流下游区的速度高于逆流区中的速度。 (c)2019年Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2020年第1期|105533.1-105533.11|共11页
  • 作者

    Jiang Ping; He Xiaomin;

  • 作者单位

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Nanjing 210016 Peoples R China|Minist Ind & Informat Technol Aeroengine Thermal Environm & Struct Key Lab Nanjing Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Trapped vortex combustor; Flow field; Particle Image Velocimetry; Turboshaft engine;

    机译:被捕获的涡流燃烧器;流场;粒子图像速度;涡轮轴发动机;

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