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Aerodynamic design and computational fluid dynamic analysis of radial outflow turbines for steam Rankine cycle and supercritical carbon dioxide Brayton cycle

机译:蒸汽兰骏循环径向流出汽轮机的空气动力学设计与计算流体动力学分析及超临界二氧化碳布雷顿循环

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The first part of this paper presents the design of a radial outflow steam turbine for a micro steam power pump block of 200 kW capacity based on a unique Ljungstrom turbine design methodology. Computational fluid dynamic (CFD) simulations were carried out for the 18-stage radial outflow steam turbine at design and off-design points, and results proved the validity of the undertaken design methodology. The design point CFD simulation showed a total to total efficiency of 74.4% for the steam turbine. Specific speed and specific diameter values for the radial outflow steam turbine stages were calculated and superimposed on the Balje's specific speed-specific diameter chart, thus identifying a unique radial outflow turbine zone in the chart. The second part of this paper presents a new design methodology based on specific speed and specific diameter values for designing a supercritical carbon dioxide radial outflow turbine for a 1 MW supercritical carbon dioxide (SCO_2) Brayton cycle. CFD simulations were carried out at design and off-design points for the SCO_2 turbine. The total to total efficiency from the CFD simulation at the design point for the SCO_2 turbine is 84.6%.
机译:本文的第一部分介绍了基于独特的Ljungstrom汽轮机设计方法的200千瓦容量的微蒸汽动力泵块径向流出汽轮机的设计。在设计和非设计点的18级径向流出汽轮机进行计算流体动力学(CFD)模拟,结果证明了开展设计方法的有效性。设计点CFD仿真显示汽轮机总效率为74.4%。径向流出汽轮机级的比直径值被计算并叠加在Balje的特定速度直径图上,从而识别图表中的独特的径向流出涡轮区域。本文的第二部分是基于特定速度和特定直径值的新设计方法,用于设计用于1 MW超临界二氧化碳(SCO_2)Brayton循环的超临界二氧化碳径向流出涡轮机。 CFD仿真是在SCO_2涡轮机的设计和偏面设计点进行的。 SCO_2涡轮机设计点的CFD仿真总额总效率为84.6%。

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