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Thermal and fluid dynamic behaviour of a trans-critical carbon dioxide small cooling system: Experimental investigation

机译:跨关键二氧化碳小冷却系统的热和流体动力学行为:实验研究

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A first trans-critical carbon dioxide hermetic reciprocating compressor prototype has been designed, numerically optimised, built and experimentally tested. Different heat exchangers have been specially developed to be used under trans-critical carbon dioxide cycles. An experimental unit has been designed and constructed to work with carbon dioxide as fluid refrigerant allowing the experimental study proposed and the validation of the numerical results obtained from the companion paper. After the numerical parametric results and the experimental comparative data obtained, a semi-hermetic reciprocating compressor has been designed, tested and compared, locating the suction plenum and cylinder head in contact with ambient. The first objective of this work has been to test inside the trans-critical cycle, carbon dioxide hermetic and semi-hermetic compressors, taking into account a special shell, a different configuration muffler, an specific stroke to bore ratio in the compressor chamber, and an increased and reinforced cylinder head. In both cases, the valve plate, the suction and discharge valves, the motor and the crankshaft connecting rod mechanism has also been necessary modified. The heat exchangers have also been adapted to carbon dioxide properties and high gas cooler pressures. The second objective is to experimentally validate the numerical simulation results obtained in the companion paper, in order to assure a real virtual laboratory prototype when numerical simulation tool developed and adapted to carbon dioxide is used. The following aspects presented in this paper are: ⅰ) the optimal gas cooler pressure under the desired working conditions; ⅱ) the experimental validation of the double pipe water counter flow heat exchangers (gas cooler and evaporator); ⅲ) the global transcritical cycle comparison between the numerical study and the experimental data under different evaporation temperatures for the hermetic compressor; and ⅳ) the experimental comparison between both hermetic and semi-hermetic CO_2 reciprocating compressors.
机译:首款无临界二氧化碳密封往复式压缩压缩机原型已经设计,在数值优化,构建和实验测试。已经专门开发出不同的热交换器以在跨关键的二氧化碳循环下使用。设计和构造实验单元以与二氧化碳一起使用,作为流体制冷剂,允许实验研究提出并从伴随纸上获得的数值结果验证。在数值参数结果和所获得的实验比较数据之后,已经设计,测试和比较了半密封往复式压缩机,定位吸入增压室和气缸盖与环境接触。这项工作的第一个目的是在跨临界循环,二氧化碳密封和半密封压缩机内测试,考虑到特殊的壳体,不同的配置消声器,特定行程到压缩机室中的孔比,以及增加和加强汽缸盖。在这两种情况下,阀板,抽吸和排出阀,电动机和曲轴连接杆机构也得到了强化。热交换器也适用于二氧化碳性能和高气体冷却压力。第二个目的是通过在使用数值模拟工具使用和适应二氧化碳的数值模拟工具时,通过实验验证在伴随纸上获得的数值模拟结果,以确保真正的虚拟实验室原型。本文提出的以下方面是:Ⅰ)在所需的工作条件下最佳气体冷却压力; Ⅱ)双管水反流热交换器的实验验证(气体冷却器和蒸发器); Ⅲ)不同蒸发温度下数值研究与实验数据的全局跨临界循环比较。和ⅳ)密封和半密封CO_2往复式压缩机的实验比较。

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