首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >DESIGN AND FLOW ANALYSIS OF A SUPERSONIC SMALL SCALE ORC TURBINE STATOR WITH HIGH MOLECULAR COMPLEXITY WORKING FLUID
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DESIGN AND FLOW ANALYSIS OF A SUPERSONIC SMALL SCALE ORC TURBINE STATOR WITH HIGH MOLECULAR COMPLEXITY WORKING FLUID

机译:高超复杂工作流体的超音速小型Orc涡轮定子的设计与流量分析

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In small scale and low temperature waste heat recovery systems, Organic Rankine Cycle (ORC) technology can be identified as a promising solution in converting low-grade heat into electricity. The principle of ORC is based on a conventional Rankine process but an organic working fluid is adopted instead of steam. The use of high molecular complexity working fluids enables the design of high efficiency ORCs and are characterized by dry expansion and high pressure ratios over the turbine, as well as low speed of sound, which typically leads to highly supersonic flows in the ORC turbine stator. In order to design supersonic ORC turbines, the geometry of the turbine stator has to be based on design methods that accurately take into account the real gas effects of the working fluid during the expansion. In this study, a highly supersonic small scale ORC turbine stator using siloxane MDM as working fluid, is studied. The accurate real gas model was implemented in a CFD-flow solver in order to predict the flow field in the stator in design and in off-design conditions. The results of this study gives valuable information on realising small capacity ORC tur-bomachinery, characterized by highly supersonic stators, and on the off-design performance of supersonic radial turbine stator that has not been documented or discussed in the previous studies.
机译:在小规模和低温废热回收系统中,可以将有机朗肯循环(ORC)技术鉴定为将低级热量转换为电力的有希望的解决方案。 ORC的原理基于传统的朗肯过程,而是采用有机工作流体而不是蒸汽。使用高分子复杂性工作流体使得能够设计高效兽人,其特征在于涡轮机的干膨胀和高压比,以及低的声音,这通常导致逆转带涡轮机定子中的高度超声波流动。为了设计超音速逆转录涡轮机,涡轮定子的几何形状必须基于精确考虑在膨胀期间工作流体的真实气体效果的设计方法。在该研究中,研究了使用硅氧烷MDM作为工作流体的高度超音速小刻度ORC涡轮定子。精确的真实气体模型在CFD流动求解器中实现,以预测设计和非设计条件中定子中的流场。该研究的结果提供了有关实现小型容量兽人Tur-Bomacherery的有价值的信息,其特征在于高度超声管,以及在先前的研究中未记录或讨论的超音速​​径向涡轮定子的偏移设计性能。

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