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An experimental analysis of the impact of primary nozzle geometries on the ejector performance used in R141b ejector refrigerator

机译:R141b喷射制冷机中主要喷嘴几何形状对喷射器性能影响的实验分析

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This paper gives an experimental discussion of the geometrical impact of the primary nozzle on the ejector performance in an R141b ejector refrigerator. Primary nozzle area ratio is varied to observe its effect on the ejector performance. Six primary nozzles are investigated experimentally. Four of them (D2.4M2.5, D2.8M2.5, D3.2M2.5, and D3.6M2.5) are designed with different throat diameters, but they have an identical nozzle area ratio. Two of them, D2.4M2.0 and D2.4M3.0, have an identical throat diameter, but they have different nozzle area ratio, resulting in a different nozzle exit Mach number. All nozzles are tested with one fixed geometry ejector at various operating conditions. Variations of the primary momentum caused by the change in primary nozzle throat and nozzle exit Mach number on the ejector performance is observed and discussed. The purpose is to determine the optimal primary nozzle geometries at given operating conditions. It is found that using a bigger nozzle throat, operated with lower generator temperature, is preferable. The primary nozzle exit Mach number should be as high as possible. It should also be designed to be consistent with the heat source's temperature for implementing the nozzle at the designed conditions. The primary nozzle exit diameter must be consistent with the mixing chamber used. Therefore, the minimum required generator temperature (Tgen-min) at various nozzle exit Mach numbers and the largest possible nozzle exit diameter for one particular ejector are provided for this present work. (C) 2016 Elsevier Ltd. All rights reserved.
机译:本文对R141b喷射制冷机中主喷嘴的几何形状对喷射器性能的影响进行了实验性讨论。改变主喷嘴面积比以观察其对喷射器性能的影响。对六个主要喷嘴进行了实验研究。其中四个(D2.4M2.5,D2.8M2.5,D3.2M2.5和D3.6M2.5)设计为具有不同的喉管直径,但是它们具有相同的喷嘴面积比。其中两个D2.4M2.0和D2.4M3.0具有相同的喉管直径,但是它们具有不同的喷嘴面积比,从而导致不同的喷嘴出口马赫数。所有喷嘴均使用一个固定的几何形状喷射器在各种操作条件下进行测试。观察并讨论了由主喷嘴喉道和喷嘴出口马赫数的变化引起的主动量变化对喷射器性能的影响。目的是确定给定操作条件下的最佳主喷嘴几何形状。发现使用较大的喷嘴喉,在较低的发电机温度下操作是优选的。主喷嘴出口马赫数应尽可能高。还应将其设计为与热源温度保持一致,以便在设计条件下实施喷嘴。主喷嘴出口直径必须与使用的混合室一致。因此,为该当前工作提供了在各种喷嘴出口马赫数下的最低所需发生器温度(Tgen-min)和一个特定喷射器的最大可能喷嘴出口直径。 (C)2016 Elsevier Ltd.保留所有权利。

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