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A New Control Mechanism for Two-Phase Ejector in Vapor Compression Cycles Using Adjustable Motive Nozzle Inlet Vortex

机译:使用可调节动机喷嘴入口涡流的蒸汽压缩循环中两相喷射器的新控制机制

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Expansion work recovery by two-phase ejector is known to be beneficial to vapor compression cycle performance. However, one of the biggest challenges with ejector vapor compression cycle is that the ejector cycle performance is sensitive to working condition changes which are common in real world applications. Different working conditions require different ejector geometries to achieve maximum performance. Slightly different geometries may result in substantially different COPs under the same conditions. Ejector motive nozzle throat diameter (motive nozzle restrictiveness) is one of the key parameters that can significantly affect COP. This paper presents a new motive nozzle restrictiveness control mechanism for two-phase ejectors used in vapor compression cycles, which has the advantages of being simple, potentially less costly and less vulnerable to clogging. The new control mechanism can possibly avoid the additional frictional losses of previously proposed ejector control mechanisms using adjustable needle. The redesigned ejector utilizes an adjustable vortex at the motive inlet to control the nozzle restrictiveness on the flow expanded in the motive nozzle. An adjustable nozzle based on this new control mechanism was designed and manufactured for experiments with R134a. The experimental results showed that, without changing the nozzle geometry, the nozzle restrictiveness on the two-phase flow can be adjusted over a wide range. Under the same inlet and outlet conditions, the mass flow rate through the nozzle can be reduced by 36% of the full load. This feature could be very useful for the future application of ejector in mobile or stationary systems under changing working conditions.
机译:已知两相喷射器的扩展工作回收是有利于蒸汽压缩循环性能的。然而,喷射器蒸汽压缩周期的最大挑战之一是喷射器循环性能对现实世界应用中常见的工作条件变化敏感。不同的工作条件需要不同的喷射器几何形状以实现最大性能。略微不同的几何形状可能导致在相同条件下基本不同的警察。喷射器动力喷嘴喉部直径(动力喷嘴限制性)是可以显着影响警察的关键参数之一。本文提出了一种新的动力喷嘴限制性控制机构,用于蒸汽压缩循环中的两相喷射器,其具有简单,潜在的昂贵且易受堵塞的优点。新的控制机构可以避免使用可调节针的先前提出的喷射器控制机构的额外摩擦损失。重新设计的喷射器利用动力入口处的可调节涡流来控制动力喷嘴中膨胀的流动的喷嘴限制性。基于该新控制机构的可调节喷嘴设计和制造用于R134A的实验。实验结果表明,在不改变喷嘴几何形状的情况下,可以在宽范围内调节两相流上的喷嘴限制性。在相同的入口和出口条件下,通过喷嘴的质量流量可以减少36%的满载。此功能对于在更改工作条件下,在移动或静止系统中的未来应用时,这一功能非常有用。

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