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吸附式空调的性能研究 总被引:6,自引:0,他引:6
1引言近年来固体吸附式制冷或热泵得到了制冷工程研究领域的普遍关注,已有各种吸附式制冷机/热泵被开发研制的报导,其中大多数是活性炭一甲醇、分子筛一水、硅胶一水、氯化钙一氨以及金属氢化物一氢等。其中比较典型的有太阳能热利用的间隙式制冷机[‘]、回热型循环制冷机[‘]和复叠式制冷系统[’]。新的热力循环,如热波型制冷循环l‘]和对流热波型制冷循环问也在不断研究探索之中。对吸附式制冷的研究兴趣主要在于这种制冷方式没有CFCS方面的问题、其价格效用比高、结构简单、与吸收式制冷系统比不需溶液泵或分馏装置,另外它… 相似文献
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通过FLUENT软件对不同布置方式的蓄热器进行数值模拟,结果表明,采用间隔式蓄热器会使蓄热器的材料温度更高,前中期蓄放热速率更快;但存在很明显的区域不均匀的现象:具体表现为中心区域要较其他区域反应速率更快,温升明显更高.从模拟结果来看,此种布置方法虽然一定程度上节省了余热资源,但由于区域反应的不平衡,致使总反应时间滞后.将模拟所得到的数据整理结合云图分析出现"类死区现象的原因",并在此基础上进行优化.具体优化方法主要有两个方面:改变肋片的几何构型、改变肋片的布置方式;另一方面在蓄热器的边璧区域使用导热系数更高的蓄热材料.通过对优化后蓄热器的蓄放热速率与优化前相比,发现蓄热器中出现的"类死区"的区域在优化后蓄放热性能均得到了很大的增强,蓄放热总时间分别减少了19.4%. 相似文献
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单压过热蒸汽余热锅炉变工况解析解 总被引:9,自引:2,他引:7
主要符号说明符号:Cp比热DT温差F换热面积G工质流量H比焓值K换热系数L汽化潜热Q换热量Re余热回收率T温度Tg1烟气在蒸发器出口处的温度保热系数下标:a接近点e出口参数E省煤器g烟气d进口参数p节点B蒸汽V蒸发器B水0设计工况参数1序言余热锅炉是动力装置中余热回收的主要设备,由于余热锅炉的烟气侧热源变动大,因此在热力系统分析时,经常要对余热锅炉的各种工况的性能作出预报。余热锅炉变工况计算方法很多,但公开发表的文献较少。其中基于已知余热锅炉各部件详细尺寸,用类似于锅炉校核计算的方法进行变工况计算是比较精确的方法l… 相似文献
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TBM的安全设计是ITER设计的一部分,安全设计的目的是为了确保TBM对ITER的安全不会产生负面影响。因此,准确计算所有源项的放射性及其潜在的危害性,对装置的设计、包层和屏蔽材料的选择、环境安全分析、核废物的处置以及反应堆的运行都是十分重要的。 相似文献
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We propose a model for a three-terminal quantum well heat engine with heat leakage. According to the Landauer formula, the expressions for the charge current, the heat current, the power output and the efficiency are derived in the linear-response regime. The curves of the power output and the efficiency versus the positions of energy levels and the bias voltage are plotted by numerical calculation. Moreover, we obtain the maximum power output and the corresponding efficiency, and analyze the influence of the heat leakage factor, the positions of energy levels and the bias voltage on these performance parameters. 相似文献
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Cooling technology is facing new challenges with the increase of electronic equipment power onboard aircraft. The traditional heat sink based on high-altitude bleed air does not satisfy this increase of cooling demands. In this article, an air/air-type skin heat exchanger is studied for cooling aircraft electronic equipment. It uses outside high-altitude cold air rather than bleed air as a heat sink. This cooling technology can effectively remove the heat load of high-power electronic devices without greatly increasing aircraft performance penalty. To assess its high-altitude heat transfer performance, an experimental prototype was designed and made. Some experiments were conducted on a ground experimental test. The heat transfer criteria formulas were obtained for both the side air in the skin heat exchanger and its convective heat transfer coefficients. Based on these experimental analyses, the heat transfer performances of the skin heat exchanger in a high-altitude cruise condition are deduced when it is assumed to be installed at an unfavorable position and a favorable position, separately. This work tries to provide a technical support for its future onboard application. 相似文献
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Christian Maes Karel Netočný Michel Verschuere 《Journal of statistical physics》2003,111(5-6):1219-1244
We study networks of interacting oscillators, driven at the boundary by heat baths at possibly different temperatures. A set of first elementary questions are discussed concerning the uniqueness of a stationary possibly Gibbsian density and the nature of the entropy production and the local heat currents. We also derive a Carnot efficiency relation for the work that can be extracted from the heat engine. 相似文献
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Schrödinger operators on Sobolev spaces are considered as new solvable models with point interactions. A simple formula for the deficiency indices of a minimal Schrödinger operator with point interactions is given. Examples of point interactions on the space W21(
3) are constructed.Mathematical Subject Classification (2000). 37J10, 47A10 相似文献
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分离式热管换热器传热特性的实验研究 总被引:1,自引:0,他引:1
本文在自行设计分离式热管实验装置的基础上,对其传热特性进行了实验研究。其工作温度为170~250℃,热流密度为25~50 kW/m~2。蒸发段和冷凝段构成相同,均是由7根直径30 mm的无缝钢管短管束组成,管长为160 mm,带有紧套的钢帛环形肋片结构尺寸为:外径45 mm、厚1 mm、片间距4 mm。实验结果表明,在本实验条件下,分离式热管的最佳充液率按管束总容量计为18%~38%。根据实验结果拟合了最佳充液率(24%)下蒸发段内部平均沸腾换热系数和冷凝段内部凝结换热努塞尔数综合关系式。 相似文献
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