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NUMERICAL INVESTIGATION OF VELOCITY COEFFICIENT FOR ORGANIC TURBINE NOZZLES USING MM AS WORKING FLUID

机译:MM作为工作流体的有机涡轮喷嘴速度系数的数值研究

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Organic Rankine cycle (ORC) has gained an increasing worldwide attention due to its high efficiency in converting low-grade thermal energy into electricity. The expander is the most critical component in the ORC system. Among the influential factors that define the performance of the expander, the velocity coefficient of the nozzle is crucial. This work numerically investigates the effects of the nozzle height, length, surface roughness, outlet geometric angle, and expansion ratio, on the velocity coefficient of the nozzle in the ORC turbine with hexamethyldisiloxane (MM) as working fluid. In the 3-D viscous numerical analysis, the shear stress transports k-ω turbulence model is employed and the numerical method is verified by the experimental data of the nozzle with pressured air based on hotwire technology. The numerical results show that the velocity coefficient is almost independent of expansion ratio compared to other factors due to the relatively small flow boundary layer and high Reynolds number. Since the existing correlations for the gas nozzle cannot well predict the velocity coefficient of the organic nozzle, an empirical equation is proposed according to the numerical results with the maximum deviation of 3.0%.
机译:有机朗肯循环(ORC)已经获得了越来越多了全世界的关注,由于在低等级热能转换成电能的效率高。该扩展是在ORC系统中最重要的组成部分。间限定膨胀机的性能的影响因素,喷嘴的速度系数是至关重要的。这项工作数值研究了喷嘴的高度,长度,表面粗糙度,出口的几何角度,和膨胀比的影响,对在ORC涡轮喷嘴与六甲基二硅氧烷(MM)的速度系数作为工作流体。在3 d粘性数值分析,剪切应力传输K-ω湍流模型采用和数值方法是通过用基于热线技术加压空气喷嘴的实验数据证实。数值结果表明,该速度系数几乎是独立的相对于其他因素膨胀比由于相对小的流动边界层和高雷诺数。由于用于气体喷嘴不能很好地预测有机喷嘴的速度系数的现有的相关性,一个经验方程是根据与3.0%的最大偏差的数值结果提出。

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