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Optimization of small-scale axial turbine for distributed compressed air energy storage system

机译:分布式压缩空气储能系统小型轴流式水轮机的优化

摘要

Small scale distributed compressed air energy storage (D-CAES) has been recognized as promising technology which can play major role in enhancing the use of renewable energy. Due to the transient behavior of the compressed air during the discharging phase, there are significant variations in air pressure, temperature and mass flow rate resulting in low turbine efficiency. This research aims to improve the expansion process of the small scale D-CAES system through optimization of a small scale axial turbine. A small scale axial air turbine has been developed using 1D Meanline approach and CFD simulation using ANSYS CFX 16.2. For improving the turbine efficiency, different optimization approaches like single and multi-operating point optimization have been performed. udThe turbine blade profiles for both stator and rotor have been optimized for minimum losses and maximum power output based on 3D CFD modelling and Multi Objective Genetic Algorithm (MOGA) optimization for single and multi-operating points. Using multi-operating point optimization, the maximum turbine efficiency of 82.767 % was achieved at the design point and this approach improved the overall efficiency of D-CAES system by 8.07% for a range of inlet mass flow rate indicating the potential of this optimization approach in turbine design development.
机译:小型分布式压缩空气储能(D-CAES)被认为是有前途的技术,可以在提高可再生能源的利用方面发挥主要作用。由于在排出阶段压缩空气的瞬态行为,空气压力,温度和质量流率存在显着变化,从而导致涡轮效率低下。本研究旨在通过优化小型轴流式涡轮机来改善小型D-CAES系统的扩展过程。使用一维均线方法和ANSYS CFX 16.2进行的CFD仿真已开发出小型轴流式空气涡轮机。为了提高涡轮效率,已经执行了诸如单工作点和多工作点优化之类的不同优化方法。 ud基于3D CFD建模和针对单点和多点操作的多目标遗传算法(MOGA)优化,针对定子和转子的涡轮叶片轮廓进行了优化,以实现最小损失和最大功率输出。使用多工作点优化,在设计点达到了82.767%的最大涡轮效率,该方法在一定范围的入口质量流量下将D-CAES系统的整体效率提高了8.07%,这表明该优化方法的潜力在涡轮设计开发中。

著录项

  • 作者

    Bahr Ennil Ali;

  • 作者单位
  • 年度 2017
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  • 原文格式 PDF
  • 正文语种 English
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