期刊
APPLIED THERMAL ENGINEERING
卷 193, 期 -, 页码 -出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.applthermaleng.2021.117007
关键词
Hydrogen tank; Geometric scale; Pressurization rate; Modified Rayleigh number; Mass transfer
资金
- National Natural Science Foundation of China [51936006]
- Joint Research Foundation of Shanghai Aerospace Advanced Technology [USCAST2019-4]
The study investigates the effects of scale on pressurization in cryogen storage tanks in space, finding that geometric scale only significantly influences pressurization rate in small-scale tanks. The causes of self-pressurization during the pressurization process are related to geometric scale, including direct sensible energy input of vapor, mass transfer on the liquid-vapor interface, and liquid thermal expansion. The findings can be utilized for pressurization prediction in various aerospace applications.
The primary challenge for the long-term storage of cryogens in space is evaporation and consequent pressurization due to heat leakage. This study innovatively presents the scale effects on pressurization covering a wide range of tank volume from 6.37 x 10(-3) to 208 m(3), under normal gravity and microgravity. A computational fluid dynamic model based on the volume-of-fluid method is constructed to predict the thermodynamic behaviors in partially filled hydrogen tanks. The geometric scale is found to play a significant role in influencing the pressurization rate only for tanks in the small-scale range, especially under normal gravity. The pressurization rate is lower under microgravity than under normal gravity for small tanks. However, the opposite is observed when the tank size exceeds a critical value. An empirical correlation is originally presented to relate the real pressurization rate to the tank diameter and the pressurization rate based on homogeneous model. According to a thermodynamic analysis, the direct sensible energy input of vapor, the mass transfer on the liquid-vapor interface, and the liquid thermal expansion are the three causes of self-pressurization, which are all related to the geometric scale. The conclusions can be used for the pressurization prediction of various emissions in the aerospace applications.
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