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A comparison of three methodological approaches for meanline design of supercritical CO_2 radial inflow turbines

机译:超临界CO_2径向进汽涡轮平均线设计的三种方法比较。

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Supercritical CO2 (s-CO2) Brayton power cycles are proposed as the next generation of thermal energy conversion due to their high efficiency and compactness. They are also scalable allowing construction of power plants at different sizes without efficiency costs. The radial inflow turbine is the critical component of small scale s-CO2 cycles. This paper presents a comparative analysis of three design methodologies that are commonly used in preliminary design of air turbines and discusses their applicability to s-CO2 turbines while proposing a process in which the turbine design can be incorporated into the higher-level thermodynamic cycle design and optimization by using these methods. The codes developed based on the three different design approaches are validated against experimental data. The twelve radial turbine designs (3 models x 4 turbine outputs) are generated and compared to furnish significant observations on implications of selecting the relevant meanline design methodology in designing s-CO2 radial turbines. Results show that methodologies suggested by Aungier and Moustapha et al. (Moustapha) produce similar blade geometries and flow features while Whitfield and Baines (W&B)'s model results in larger rotor blade heights and different flow characteristics. The rotor inlet radius is determined primarily by the operating condition, while the blade heights are determined by the design parameters. Turbine losses and performance predictions of different meanline models are also examined.
机译:由于超临界CO2(s-CO2)的高效率和紧凑性,提出了布雷顿功率循环作为下一代热能转换的方法。它们还具有可扩展性,可在不提高效率的情况下以不同的规模建造电厂。径向流入涡轮机是小规模s-CO2循环的关键组成部分。本文对三种常用的空气涡轮机设计方法进行了比较分析,并讨论了它们在s-CO2涡轮机中的适用性,同时提出了将涡轮机设计纳入更高级别的热力循环设计的过程。通过使用这些方法进行优化。根据实验数据验证了基于三种不同设计方法开发的代码。生成并比较了十二种径向涡轮机设计(3个模型x 4个涡轮机输出),以提供关于在设计s-CO2径向涡轮机时选择相关平均线设计方法的含义的重要观察结果。结果表明,Aungier和Moustapha等人提出的方法论。 (Moustapha)产生相似的叶片几何形状和流动特征,而Whitfield和Baines(W&B)的模型导致更大的转子叶片高度和不同的流动特征。转子入口半径主要取决于运行条件,而叶片高度则取决于设计参数。还检查了涡轮损失和不同平均线模型的性能预测。

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