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Atomization and surface heat transfer characteristics of cryogen spray cooling with expansion-chambered nozzles

机译:膨胀腔喷嘴冷却剂喷雾冷却的雾化和表面传热特性

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Cryogen spray cooling (CSC) is commonly applied in laser dermatology to protect the epidermis from thermal damage. Many efforts have attempted to improve the cooling capacity of CSC, among which the use of expansion-chambered nozzles is an effectively simple method with considerable potential. This study examined the influences of the expansion-chambered nozzle structure, including the ratios of inlet nozzle diameter to discharge nozzle diameter and of chamber diameter to discharge nozzle diameter on R134a and R404A spray cooling. Fifteen transparent expansion-chambered nozzles with the expansion chamber aspect ratio of 1.0, chamber diameter to discharge nozzle diameter ratios of 5.0–10.0, and inlet nozzle diameter to discharge nozzle diameter ratios of 0.6–1.4 were tested. The internal flow pattern inside the expansion chamber, external spray pattern, and surface heat transfer characteristics of cryogen spray using different nozzles, including the straight-tube nozzle, were investigated. The structure of the expansion chamber was found to have an important effect on the spray patterns and cooling characteristics. The spray radius obviously decreased when the expansion-chambered nozzles were used, and the spray pattern became narrower as the ratio of chamber diameter to discharge nozzle diameter increased. By contrast, the increase in ratio of two nozzle diameters enlarged the spray radius. Surface temperature and heat flux with different nozzles and cryogens showed a similarity, and correlations of surface temperature and heat flux were proposed. The introduction of expansion-chambered nozzles could effectively improve the spray cooling capacity. The minimum average surface temperature during the fully developed spray period could be reached for both R134a spray and R404A spray by an expansion-chambered nozzle with a chamber diameter to discharge nozzle diameter ratio of roughly 5.0 and an inlet nozzle diameter to discharge nozzle diameter ratio of roughly 0.6.
机译:低温喷雾冷却(CSC)通常用于激光皮肤病学中,以保护表皮免受热损伤。已经进行了许多努力来提高CSC的冷却能力,其中使用膨胀腔喷嘴是一种有效的简单方法,具有很大的潜力。这项研究检查了膨胀腔喷嘴结构对R134a和R404A喷雾冷却的影响,包括入口喷嘴直径与排放喷嘴直径的比以及腔室直径与排放喷嘴直径的比。测试了十五个透明的膨胀室喷嘴,膨胀室的纵横比为1.0,室直径与排放喷嘴的直径之比为5.0–10.0,入口喷嘴直径与排放喷嘴的直径之比为0.6–1.4。使用不同的喷嘴(包括直管喷嘴)研究了膨胀室内部的内部流动模式,外部喷雾模式以及制冷剂喷雾的表面传热特性。发现膨胀室的结构对喷雾模式和冷却特性具有重要影响。当使用膨胀室喷嘴时,喷雾半径明显减小,并且随着腔室直径与排出喷嘴直径之比的增加,喷雾模式变窄。相反,两个喷嘴直径之比的增加扩大了喷射半径。不同喷嘴和冷却剂的表面温度和热通量具有相似性,并提出了表面温度和热通量的相关性。引入膨胀室喷嘴可以有效提高喷雾冷却能力。对于R134a喷雾和R404A喷雾,通过腔室直径与排放喷嘴直径之比约为5.0且入口喷嘴直径与排放喷嘴直径之比为1的膨胀型喷嘴,可以达到R134a喷雾和R404A喷雾在完全展开喷雾期间的最低平均表面温度。大约0.6。

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