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Heat Transfer Enhancement by Using Fin for MH Hydrogen Storage Tank-Discuss on the Geometrical Optimization of Fin C

机译:用于MH储氢罐的鳍片探讨鳍片几何优化的热传递增强

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In this study, the heat transfer enhancement which effects of several fins on metal hydride particle layer are estimated by experiment and simulation. The unsteady state heat conduction calculation of MH particle layer with and without fins was researched by the Solidworks simulation software and the experimental method including calculation parameters, fins' charging volume ratio and the fin shape such as cross fin and circular cross fin. Besides, another estimation parameter is the diameter of storage tank. One storage tank has an outer diameter of 80 mm, an inner diameter of 78 mm, the other has an outer diameter of 25 mm and an inner diameter of 23.5 mm. The number of fins was increased until the charging volume ratio of the fin reaching to 25 volume %. We estimated the heat transfer enhancement influence of the fins on the MH ally layer. According to our calculation results, the effective thermal conductivity is increased with increasing of charging volume ratio of fin, but this heat transfer enhancing effect is saturated while it exceeded the 10 volume percentage. In our simulation model of a circle cross fin, the tank was set as an outer diameter of 52 mm and an inner diameter of 50 mm. In the simulation results of using circle cross fins cases, the highest heat transfer enhancement effect was obtained when circular diameter of circular cross fin was 24 mm. Compared with cross fins (which has a heat transfer enhancing effect of 4.68 times compared with no fins' case), the volume content of circle cross fin was 1.4% higher than that of cross fin. However, the heat transfer enhancement effect of circular cross fin was 2.46 times higher than that of cross fin. Besides, it is confirmed that circle cross fin whose charging volume ratio is under 10% can achieve a high heat transfer enhancing effect and is suitable to heat transfer enhancing of MH particle layer.
机译:在该研究中,通过实验和模拟估计了传热增强了几种翅片对金属氢化物颗粒层的影响的影响。通过SolidWorks仿真软件和实验方法研究了MH粒子层的不稳定状态热传导计算,包括计算参数,翅片充电体积比和翅片形状,如跨翅片和圆形交叉翅片等实验方法研究了MH颗粒层。此外,另一个估计参数是储罐的直径。一个储罐的外径为80mm,内径为78mm,另一个外径为25mm,内径为23.5mm。增加翅片的数量,直到翅片的充电体积比达到25体积%。我们估计了MH亚利层上翅片的热传递增强影响。根据我们的计算结果,随着翅片的充电量比增加,有效的导热率增加,但这种热传递增强效果在超过10体积百分比时饱和。在我们的圆形交叉翅片的仿真模型中,罐的外径为52毫米,内径为50mm。在使用圆圈交叉翅片壳体的仿真结果中,当圆形交叉翅片的圆形直径为24mm时获得最高的传热增强效果。与交叉翅片相比(与没有翅片的情况相比,传热增强效果为4.68倍),圆角翅片的体积含量比交叉翅片高1.4%。然而,圆形交叉翅片的热传递增强效果比跨鳍的高2.46倍。此外,确认其充电体积比率低于10%的圆形交叉翅片可以实现高传热增强效果,并且适合于MH颗粒的传热增强。

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