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Flow and heat transfer characteristics in slip regime for an annulus of evacuated collector tube subjected to non-uniform solar flux boundary condition

机译:流动和传热特性在经过非均匀太阳能磁通边界条件的抽空集电管环形空间中的流动制度

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Due to the accumulation of residual gas, vacuum failure may occur in the annulus of evacuated collector tube in solar trough thermal power system, resulting in the changes of flow and heat transfer mechanism and characteristics. In this paper, based on the actual situation of solar radiation in summer of Chongqing, China, the flow and heat transfer characteristics of the annulus in slip regime were numerically studied. The effects of gas pressure, gas types (N-2, H-2 and He), heat transfer fluid temperature were analyzed and discussed. The results show that the temperature jump under lower gas pressure directly affects the heat loss and temperature distribution of the annulus. The temperature jump is most obvious for the residual gas of H-2 at gas pressure of 130Pa, while it basically disappears for N-2 and He (the corresponding Knudsen numbers Kn are 0.0019 and 0.0040; 0.0022 and 0.0046; 0.0026 and 0.0052 respectively under heat transfer fluid temperatures of 473.15 K, 573.15 K and 673.15 K). The heat loss and the outer wall temperature of glass envelope rise with the increasing of heat transfer fluid temperature and gas pressure, and are related to the thermo-physical properties and thermal adaptation coefficient of gas. For gas pressure being less than 70Pa (Kn > 0.0048) or greater than 20000Pa (continuous gas flow regime), the heat loss of N-2 keeps increasing with gas pressure, and the heat losses of H-2 and He are even more than 1200 W.m(-1) under heat transfer fluid temperature of 673.15 K. When the temperature of heat transfer fluid is 573.15 K and the pressure increases from 1.83Pa to 130Pa, the declining relative values of first law efficiency (thermal efficiency) and second law efficiency (exergic efficiency) for N-2, H-2 and He are 1.59%, 10.07% and 8.48% respectively.
机译:由于剩余气体的积累,在太阳能槽热电系统中的抽空集电管环形空间中可能发生真空衰竭,导致流动和传热机构的变化和特性。本文基于重庆夏季太阳辐射的实际情况,在数值上研究了防滑制度下环的流量和传热特性。分析并讨论了气体压力,气体类型(N-2,H-2和HE)的影响,并讨论了传热流体温度。结果表明,较低气体压力下的温度跳跃直接影响环空的热量损失和温度分布。温度跳跃对于130瓦的气体压力下的H-2残留气体最明显,而N-2基本上消失,并且他(相应的knudsen NumberNK为0.0019和0.0040; 0.0022和0.0046; 0.0026和0.0052传热液温度为473.15 k,573.15 k和673.15 k)。随着传热流体温度和气体压力的增加,玻璃包络的热量损失和外壁温度升高,与热物理性质和气体热适应系数有关。对于低于70Pa(KN> 0.0048)或大于20000PA(连续气体流动状态)的气体压力,N-2的热量损失与气体压力保持增加,H-2的热量损失甚至比1200 WM(-1)在传热流体温度下为673.15 K.当传热流体的温度为573.15 k时,压力从1.83Pa到130磅增加,第一法效率(热效率)和第二法的相对值下降N-2,H-2和他的效率(过敏效率)分别为1.59%,10.07%和8.48%。

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