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High-power mode control for triaxial gas turbines with variable power turbine guide vanes

机译:具有可变功率涡轮导向叶片的三轴燃气涡轮机的高功率模式控制

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摘要

Factors such as the atmospheric environment or component performance influence various matching relationships as well as maximum output power in triaxial gas turbines with variable power turbine guide vanes. This paper proposes a control strategy called High Power Mode (HPM) which solves the matching problem, adjusts fuel flow, adjusts the guide vane to adapt the gas turbine to unpredictable factors automatically, and enhances its maximum output power without exceeding high- and low-pressure rotor rotational speeds or combustor outlet total temperature limits.We first built a component-level gas turbine simulation model to explore the control strategy and the influence of guide vane angle on gas turbine working for the variable geometry triaxial gas turbine. We conducted a series of gas turbine rig tests to validate the simulation model. We then determined the guide vane angle effect law on the gas turbine performance based on the simulations as well as experimental data. HPM, including guide vane angle and fuel flow rate control strategies, was established according to the acquired guide vane angle influence law. We wrote an HPM control program in MATIAB/SIMULINK to find that the program indeed optimizes components and parameters (high- and low-pressure rotor rotational speeds and combustor outlet total temperature) while matching them effectively within unpredictable environments. The maximum gas turbine output power can be increased with the program by more than 4% in certain atmospheric environments. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:诸如大气环境或部件性能之类的因素会影响具有可变功率涡轮导向叶片的三轴燃气涡轮机中的各种匹配关系以及最大输出功率。本文提出了一种称为高功率模式(HPM)的控制策略,该策略可解决匹配问题,调节燃料流量,调节导流叶片以使燃气轮机自动适应不可预测的因素,并在不超过高低功率的情况下提高其最大输出功率。我们首先建立了一个组件级燃气轮机仿真模型,以探讨控制策略以及导叶角度对可变几何三轴燃气轮机工作的影响。我们进行了一系列燃气轮机试验,以验证模拟模型。然后,基于仿真和实验数据,确定了导叶角度对燃气轮机性能的影响规律。根据所获得的导叶角度影响规律,建立了包括导叶角度和燃油流量控制策略在内的HPM。我们在MATIAB / SIMULINK中编写了一个HPM控制程序,发现该程序确实优化了组件和参数(高压和低压转子转速以及燃烧室出口总温度),同时在不可预测的环境中有效地匹配了它们。在某些大气环境下,通过该程序可以将燃气轮机的最大输出功率提高4%以上。 (C)2019 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2019年第3期|132-142|共11页
  • 作者单位

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China|Univ Chinese Acad Sci, Beijing, Peoples R China;

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China;

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China|Univ Chinese Acad Sci, Beijing, Peoples R China;

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China;

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China|Univ Chinese Acad Sci, Beijing, Peoples R China;

    Chinese Acad Sci, Inst Engn Thermophys, Beijing, Peoples R China|Univ Chinese Acad Sci, Beijing, 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

    Variable power turbine guide vanes; Triaxial gas turbine; High-power mode control; Simulation model; Effect law;

    机译:变功率涡轮导向叶片;三轴燃气轮机;大功率模式控制;仿真模型;影响规律;

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