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HEAT TRANSFER PERFORMANCE OF SUPERCRITICAL CARBON DIOXIDE IN MICROCHANNELS

机译:超临界二氧化碳在微通道中的传热性能

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摘要

This paper provides an experimental investigation of heat transfer performance and pressure drop of supercritical carbon dioxide cooling in microchannel heat exchanger. An extruded flat aluminum tube with 37 parallel channels and each channel of 0.5 mm × 0.5 mm cross section was used as the test section. Super critical carbon dioxide at pressure of 7.5 MPa and inlet temperature varied from 55 to 25 ℃ was tested. The temperature drops of CO_2 cooled inside the test section was controlled at 2, 4 and 8 ℃ separately for each test to investigate the effect of properties change on the friction and heat transfer performance at various temperature cooling ranges near the critical point. The test results showed that while the test conditions were away from (approximately 5 ℃ higher or lower) the critical point, both heat transfer and pressure drop performance agreed very well with those predicted by convention correlations. However, while the test conditions near the critical point, the difference between the present test results and the prediction values is very high. From the experiment results of various temperature change range inside the test section, we can find that both heat transfer and pressure drop were strongly affected by the temperature cooling ranges near the critical point. Since there is a drastic peak of the properties change near the critical point, neither fluid properties at the average temperature nor the average properties at the inlet and exit temperatures may appropriately present the actual properties change in the test process. If we use the properties integrated but not averaged from inlet to the exit temperatures, we may obtain the results that agree well with the values predicted by conventional correlations. The heat transfer and pressure drop performance of super critical carbon dioxide are indeed similar to these at normal conditions if its properties were appropriately evaluated.
机译:本文提供了微通道热交换器中超临界二氧化碳冷却的传热性能和压降的实验研究。将具有37个平行通道且每个通道横截面为0.5 mm×0.5 mm的挤压扁平铝管用作测试部分。测试了超临界二氧化碳,压力为7.5 MPa,入口温度为55至25℃。对于每个测试,分别将测试部分内部冷却的CO_2的温度降控制在2、4和8℃,以研究在临界点附近的各种温度冷却范围内,性能变化对摩擦和传热性能的影响。试验结果表明,在远离临界点(约5℃或更高)的条件下,传热和压降性能均与常规相关性非常吻合。但是,当测试条件接近临界点时,当前测试结果与预测值之间的差异非常大。从测试区域内各种温度变化范围的实验结果可以发现,传热和压降都受到临界点附近温度冷却范围的强烈影响。由于在临界点附近有一个急剧的特性变化峰值,因此在平均温度下的流体特性或在入口和出口温度下的平均特性都不会适当地显示测试过程中的实际特性变化。如果我们使用从入口温度到出口温度的积分但未求平均值的属性,则可以获得的结果与常规相关性预测的值非常吻合。如果适当评估其性能,超临界二氧化碳的传热和压降性能确实与正常条件下的相似。

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