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

机译:跨临界二氧化碳小型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:第一个跨临界二氧化碳气密往复式压缩机原型已经过设计,数值优化,建造和实验测试。已经专门开发了不同的热交换器以在跨临界二氧化碳循环下使用。设计并建造了一个实验单元,以二氧化碳作为流体制冷剂工作,从而提出了实验研究并验证了从随附论文中获得的数值结果。在获得数值参数结果和实验比较数据之后,设计,测试和比较了一种半封闭式往复式压缩机,将吸入气室和气缸盖放置在与环境接触的位置。这项工作的首要目标是在跨临界循环中测试二氧化碳密闭和半密闭压缩机,其中要考虑到特殊的外壳,不同的消声器,压缩机腔室中的特定冲程与缸径比,以及增加和增强的气缸盖。在这两种情况下,阀板,吸气和排气阀,电动机和曲轴连杆机构也都需要进行修改。热交换器也已经适应了二氧化碳的特性和较高的气体冷却器压力。第二个目的是通过实验验证随附论文中获得的数值模拟结果,以确保在使用开发并适用于二氧化碳的数值模拟工具时确保真实的虚拟实验室原型。本文提出以下方面:ⅰ)在所需工作条件下的最佳气体冷却器压力; ⅱ)双管水逆流热交换器(气体冷却器和蒸发器)的实验验证; ⅲ)密闭压缩机在不同蒸发温度下的数值研究和实验数据之间的全球跨临界循环比较; ⅳ)封闭式CO_2和半封闭式CO_2往复式压缩机的实验比较。

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