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Organic Rankine Cycle Optimization With Explicit Designs of Evaporator and Radial Inflow Turbine

机译:蒸发器和径向流入汽轮机明确设计的有机朗肯循环优化

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Although there are studies on optimizing organic Rankine cycles (ORCs) through individual components, in this study, for the first time, both evaporator and turbine designs are included in a multiobjective optimization. Twenty-eight working fluids are used to find optimum cycle parameters for three source temperatures (90, 120, and 150 °C). A mean-line radial inflow turbine model is used. Nondominated Sorting Genetic Algorithm II is utilized to minimize total evaporator area per net power output and maximize performance factor simultaneously. The technique for Order Preference by Similarity to Ideal Situation (TOPSIS) procedure is followed to obtain ideal solutions. A group of working fluids with highest net power output is determined for each heat source temperature. Optimized geometric parameters of the evaporator vary in a narrow range independent of the working fluid and the source temperature, but evaporator PPTD and degree of superheating depend on the working fluid. The specific speed, the pressure ratio through the turbine, and the nozzle inlet-to-outlet radius ratio do not change significantly with cycle conditions.
机译:尽管有关于通过各个组件优化有机朗肯循环(ORCS)的研究,但在本研究中,首次包括在多目标优化中的蒸发器和涡轮机设计。二十八个工作流体用于找到三个源温度(90,120和150°C)的最佳循环参数。使用平均线径向流入涡轮机模型。 NondoMinated分类遗传算法II用于最小化每个净功率输出的总蒸发器面积,同时最大化性能因子。遵循相似性与理想情况(TOPSIS)程序的顺序偏好技术,以获得理想的解决方案。针对每个热源温度确定具有最高净功率输出的一组工作流体。优化的蒸发器几何参数在窄的范围内变化,与工作流体和源温度无关,但蒸发器PPTD和过热程度取决于工作流体。通过涡轮机的具体速度,压力比,并且喷嘴入口到出口半径比与循环条件没有显着变化。

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