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Preliminary Design of Small- Scale Supercritical CO_2 Radial Inflow Turbines

机译:小型超临界CO_2径流式涡轮机的初步设计

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In recent years, supercritical CO_2 (sCO_2) Brayton cycles have drawn the attention of researchers due to their high cycle efficiencies, compact turbomachinery, and environmental friendliness. For small-scale cycles, radial inflow turbines (RIT) are the prevailing choice and one of the key components. A mean line design procedure for sCO_2 RIT is developed and design space exploration conducted for a 100 kW-class turbine for a low-temperature waste-heat utilization sCO_2 Brayton cycle. By varying the two design parameters, specific speed and velocity ratio, different turbine configurations are setup and compared numerically by means of computational fluid dynamics (CFD) simulations. Results are analyzed to conclude on optimum design parameters with regard to turbine efficiency and expansion ratio. Specific speeds between 0.2 and 0.5 are recommended for sCO_2 RIT with small though flow (3 kg/s). The higher the velocity ratio, the bigger the turbine expansion ratio. Pairs of optimum design parameters that effectuate maximum efficiency are identified, with smaller velocity ratios prevailing for smaller specific speeds. The turbine simulation results for sCO_2 are compared to well-established recommendations for the design of RIT from literature, such as the Balje diagram. It is concluded that for the design of sCO_2 RITs, the same principles can be used as for those for air turbines. By achieving total-to-static stage and rotor efficiencies of 84% and 86%, respectively, the developed mean line design procedure has proven to be an effective and easily applicable tool for the preliminary design of small-scale sCO_2 RIT.
机译:近年来,超临界CO_2(sCO_2)布雷顿循环因其高循环效率,紧凑的涡轮机械和环境友好性而吸引了研究人员的注意。对于小规模循环,径向流入涡轮机(RIT)是主要选择,也是关键组件之一。针对sCO_2布雷顿循环的低温余热利用,针对100 kW级涡轮机开发了sCO_2 RIT的平均线设计程序,并进行了设计空间探索。通过改变两个设计参数,即特定的速度和速度比,可以设置不同的涡轮机配置,并通过计算流体动力学(CFD)仿真进行数值比较。分析结果以得出关于涡轮效率和膨胀比的最佳设计参数。对于流量较小(3 kg / s)的sCO_2 RIT,建议使用0.2至0.5的特定速度。速度比越高,涡轮膨胀率越大。确定了实现最大效率的最佳设计参数对,较小的速度比主要用于较小的特定速度。将sCO_2的涡轮机仿真结果与文献(例如Balje图)中针对RIT设计的公认建议进行比较。结论是,对于sCO_2 RIT的设计,可以使用与空气涡轮机相同的原理。通过分别达到84%和86%的静态总级和转子效率,已开发的平均线设计程序已被证明是用于小规模sCO_2 RIT初步设计的有效且易于应用的工具。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2020年第2期|021011.1-021011.10|共10页
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    Department of Power Mechanical Engineering National Tsing Hua University No. 101 Section 2 Kuang-Fu Road Hsinchu 30013 Taiwan;

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