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Shroud leakage flow models and a multi-dimensional coupling CFD (computational fluid dynamics) method for shrouded turbines

机译:带罩涡轮的罩泄漏流模型和多维耦合CFD(计算流体动力学)方法

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摘要

Multi-dimensional coupling simulation is an effective approach for evaluating the flow and aero-thermal performance of shrouded turbines, which can balance the simulation accuracy and computing cost effectively. In this paper, 1D leakage models are proposed based on classical jet theories and dynamics equations, which can be used to evaluate most of the main features of shroud leakage flow, including the mass flow rate, radial and circumferential momentum, temperature and the jet width. Then, the 1D models are expanded to 2D distributions on the interface by using a multi-dimensional scaling method. Based on the models and multi-dimensional scaling, a multi-dimensional coupling simulation method for shrouded turbines is developed, in which, some boundary source and sink are set on the interface between the shroud and the main flow passage. To verify the precision, some simulations on the design point and off design points of a 1.5 stage turbine are conducted. It is indicated that the models and methods can give predictions with sufficient accuracy for most of the flow field features and will contribute to pursue deeper understanding and better design methods of shrouded axial turbines, which are the important devices in energy engineering. (C) 2016 Elsevier Ltd. All rights reserved.
机译:多维耦合仿真是评估带罩涡轮机流动和空气热力性能的有效方法,可以平衡仿真精度和有效计算成本。本文基于经典射流理论和动力学方程,提出了一维泄漏模型,可用于评估护罩泄漏流的大多数主要特征,包括质量流量,径向和周向动量,温度和射流宽度。然后,使用多维缩放方法将一维模型扩展到界面上的二维分布。基于模型和多维尺度,提出了带罩透平的多维耦合仿真方法,其中,在罩与主流道的界面处设置了一些边界源和汇。为了验证精度,对1.5级涡轮的设计点和非设计点进行了一些模拟。结果表明,该模型和方法可以对大多数流场特征进行足够准确的预测,并将有助于对作为能源工程重要设备的带罩轴流式涡轮机进行更深入的了解和更好的设计方法。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Energy》 |2016年第15期|410-429|共20页
  • 作者单位

    Beijing Univ Aero & Astro, Sch Energy & Power Engn, Na Key Lab Sci & Technol Aeroengine Aerothermodyn, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China;

    Beijing Univ Aero & Astro, Sch Energy & Power Engn, Na Key Lab Sci & Technol Aeroengine Aerothermodyn, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China;

    Beijing Univ Aero & Astro, Sch Energy & Power Engn, Na Key Lab Sci & Technol Aeroengine Aerothermodyn, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China;

    AVIC Shenyang Engine Design & Res Inst, Shenyang 110015, Peoples R China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Turbine; Shroud; Leakage flow; Modeling; Multi-dimensional scaling; Multi-dimensional coupling;

    机译:涡轮;护罩;泄漏流;建模;多维缩放;多维耦合;

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