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首页> 外文期刊>Entropy >Similarity Theory Based Radial Turbine Performance and Loss Mechanism Comparison between R245fa and Air for Heavy-Duty Diesel Engine Organic Rankine Cycles
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Similarity Theory Based Radial Turbine Performance and Loss Mechanism Comparison between R245fa and Air for Heavy-Duty Diesel Engine Organic Rankine Cycles

机译:基于相似度理论的重型柴油机有机朗肯循环的径向涡轮性能和R245fa与空气之间的损失机理比较

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Organic Rankine Cycles using radial turbines as expanders are considered as one of the most efficient technologies to convert heavy-duty diesel engine waste heat into useful work. Turbine similarity design based on the existing air turbine profiles is time saving. Due to totally different thermodynamic properties between organic fluids and air, its influence on turbine performance and loss mechanisms need to be analyzed. This paper numerically simulated a radial turbine under similar conditions between R245fa and air, and compared the differences of the turbine performance and loss mechanisms. Larger specific heat ratio of air leads to air turbine operating at higher pressure ratios. As R245fa gas constant is only about one-fifth of air gas constant, reduced rotating speeds of R245fa turbine are only 0.4-fold of those of air turbine, and reduced mass flow rates are about twice of those of air turbine. When using R245fa as working fluid, the nozzle shock wave losses decrease but rotor suction surface separation vortex losses increase, and eventually leads that isentropic efficiencies of R245fa turbine in the commonly used velocity ratio range from 0.5 to 0.9 are 3%–4% lower than those of air turbine.
机译:使用径向涡轮作为膨胀机的有机朗肯循环被认为是将重型柴油机废热转化为有用功的最有效技术之一。基于现有空气涡轮轮廓的涡轮相似性设计可以节省时间。由于有机流体和空气之间的热力学性质完全不同,因此需要分析其对涡轮性能和损失机理的影响。本文对R245fa和空气在相似条件下的径向涡轮进行了数值模拟,并比较了涡轮性能和损失机理的差异。空气的比热率越大,空气涡轮机的压力比越高。由于R245fa气体常数仅为空气常数的五分之一,因此R245fa涡轮机降低的转速仅是空气涡轮机转速的0.4倍,而降低的质量流率大约是空气涡轮机转速的两倍。当使用R245fa作为工作流体时,喷嘴冲击波损失减少,但转子吸入表面分离涡流损失增加,最终导致R245fa涡轮在通常的速比范围从0.5到0.9时的等熵效率比3%–4%低。那些是涡轮机。

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