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Evaluation of a combined cycle based on an HCCI (Homogenous Charge Compression Ignition) engine heat recovery employing two organic Rankine cycles

机译:基于采用两个有机朗肯循环的HCCI(均质压缩压缩点火)发动机热回收的联合循环评估

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摘要

In this work, a combined power cycle which includes a HCCI (Homogenous Charge Compression Ignition) engine and two ORCs (Organic Rankine Cycles) is introduced. In the proposed cycle, the waste heats from the engine cooling water and exhaust gases are utilized to drive the ORCs. A parametric study is conducted to show the effects of decision parameters on the performance and on the total cost rate of cycle. Results of the parametric study reveal that increasing the pinch point temperature difference of evaporator and temperature of the condenser leads to reduction in both exergy efficiency and total cost rate of the bottoming cycle. There is a specific evaporator temperature where exergy efficiency is improved, but the total cost rate of the bottoming cycle is maximized. Also, a multi-objective optimization strategy is performed to achieve the best system design parameters from both thermodynamic and economic aspects. The exergy efficiency and the total cost rate of the system have been considered as objective functions. Optimization results indicate that the exergy efficiency of the cycle increases from 44.96% for the base case to 46.02%. Also, approximately1.3% reduction in the cost criteria is achieved. Results of the multi-objective optimization justify the results obtained through the parametric study and demonstrate that the design parameters of both ORCs have conflict effect on the objective functions. (C) 2016 Elsevier Ltd. All rights reserved.
机译:在这项工作中,引入了包括HCCI(均质压缩压缩点火)发动机和两个ORC(有机朗肯循环)的联合动力循环。在建议的循环中,发动机冷却水和废气产生的废热被用于驱动ORC。进行了参数研究,以显示决策参数对性能和周期总成本率的影响。参数研究的结果表明,蒸发器的收缩点温度差和冷凝器温度的升高会导致火用效率和底部循环总成本率的降低。在特定的蒸发器温度下,其能效效率得到改善,但底部循环的总成本率已达到最大化。此外,从热力学和经济方面考虑,执行多目标优化策略以实现最佳的系统设计参数。系统的火用效率和总成本率已被视为目标函数。优化结果表明,该循环的火用效率从基本情况的44.96%提高到46.02%。而且,成本标准可降低约1.3%。多目标优化的结果证明了通过参数研究获得的结果是合理的,并表明两个ORC的设计参数对目标函数都有冲突影响。 (C)2016 Elsevier Ltd.保留所有权利。

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