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Experimental investigation on motive nozzle throat diameter for an ejector expansion refrigeration system

机译:喷射器膨胀制冷系统动力喷嘴喉径的实验研究

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In this study, ejector was used to reduce throttling losses in a vapour compression refrigeration system. Effects on system performance of throat diameter and position of motive nozzle of ejector were investigated experimentally. An ejector was designed based on the established mathematical model and manufactured. The experiments were carried out by using different primary nozzle throat diameters. The experiments were further conducted by changing condenser water inlet temperature, which is one of the external parameters. The experimental results of the ejector system and those of the classic system were compared under same external operating conditions and for the same cooling capacity. In order to obtain same external operating conditions in both systems, the inlet conditions of the brine supplied to the evaporator and inlet water conditions (flow rate and temperature) to the condenser were kept constant. Maximum performance was obtained when the primary nozzle throat diameter was 2.3 mm within the areas considered in this study. When compared, it was experimentally determined that the ejector system that uses the optimum motive nozzle throat diameter exhibits higher COP than the classic system by 5-13%. Furthermore, it was found that the variation of coefficient of performance based on position of motive nozzle in two-phase ejector expander refrigeration cycle is lower than 1%. (C) 2016 Elsevier Ltd. All rights reserved.
机译:在这项研究中,喷射器用于减少蒸汽压缩制冷系统中的节流损失。实验研究了对喉管直径和喷射器动力喷嘴位置系统性能的影响。根据已建立的数学模型设计并制造出一个喷射器。通过使用不同的主喷嘴喉直径进行实验。通过改变冷凝器水的入口温度进一步进行实验,冷凝器水的入口温度是外部参数之一。在相同的外部操作条件和相同的冷却能力下,比较了喷射器系统和经典系统的实验结果。为了在两个系统中获得相同的外部运行条件,供应给蒸发器的盐水的入口条件和冷凝器的入口水条件(流速和温度)应保持恒定。当本研究中考虑的主喷嘴喉部直径为2.3 mm时,可获得最佳性能。当进行比较时,通过实验确定使用最佳动力喷嘴喉部直径的喷射器系统比传统系统具有更高的COP 5-13%。此外,发现在两相喷射器膨胀机制冷循环中,基于动力喷嘴的位置的性能系数的变化小于1%。 (C)2016 Elsevier Ltd.保留所有权利。

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