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Supercritical CO_2 Radial Turbine Design Performance as a Function of Turbine Size Parameters

机译:超临界CO_2径向涡轮设计性能与涡轮尺寸参数的关系

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Supercritical CO_2 (sCO_2) cycles are considered as a promising technology for next generation concentrated solar thermal, waste heat recovery, and nuclear applications. Particularly at small scale, where radial inflow turbines can be employed, using sCO_2 results in both system advantages and simplifications of the turbine design, leading to improved performance and cost reductions. This paper aims to provide new insight toward the design of radial turbines for operation with sCO_2 in the 100-200 kW range. The quasi-one-dimensional mean-line design code topgen is enhanced to explore and map the radial turbine design space. This mapping process over a state space defined by head and flow coefficients allows the selection of an optimum turbine design, while balancing performance and geometrical constraints. By considering three operating points with varying power levels and rotor speeds, the effect of these on feasible design space and performance is explored. This provides new insight toward the key geometric features and operational constraints that limit the design space as well as scaling effects. Finally, review of the loss break-down of the designs elucidates the importance of the respective loss mechanisms. Similarly, it allows the identification of design directions that lead to improved performance. Overall, this work has shown that turbine design with efficiencies in the range of 78-82% is possible in this power range and provides insight into the design space that allows the selection of optimum designs.
机译:超临界CO_2(sCO_2)循环被认为是下一代集中太阳能热,余热回收和核应用的有前途的技术。特别是在可以使用径向流入式涡轮机的小规模环境中,使用sCO_2既可以带来系统优势,也可以简化涡轮机设计,从而提高性能并降低成本。本文旨在为sCO_2在100-200 kW范围内运行的径向涡轮机设计提供新见解。准一维平均线设计代码topgen得到增强,以探索和绘制径向涡轮机设计空间。在由扬程和流量系数定义的状态空间上的这种映射过程允许选择最佳的涡轮机设计,同时平衡性能和几何约束。通过考虑具有不同功率水平和转子速度的三个工作点,探讨了它们对可行设计空间和性能的影响。这为限制设计空间和缩放效果的关键几何特征和操作约束提供了新的见解。最后,对设计的损耗分解的回顾阐明了各个损耗机制的重要性。同样,它可以识别导致性能提高的设计方向。总体而言,这项工作表明,在此功率范围内,涡轮机设计的效率在78-82%的范围内是可行的,并且可以深入了解允许选择最佳设计的设计空间。

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  • 来源
    《Journal of turbomachinery》 |2017年第8期|081008.1-081008.11|共11页
  • 作者单位

    Queensland Geothermal Energy Centre of Excellence, The University of Queensland, Brisbane 4072, Australia;

    Queensland Geothermal Energy Centre of Excellence, The University of Queensland, Brisbane 4072, Australia;

    Queensland Geothermal Energy Centre of Excellence, The University of Queensland, Brisbane 4072, Australia;

    Queensland Geothermal Energy Centre of Excellence, The University of Queensland, Brisbane 4072, Australia;

    Centre for Hypersonics, The University of Queensland, Brisbane 4072, Australia;

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