A Thermodynamic Model for Cryogenic Liquid Hydrogen Fuel Tanks

被引:4
作者
Choi, Dongkuk [1 ]
Lee, Sooyong [2 ]
Kim, Sangwoo [2 ]
机构
[1] Korea Aerosp Univ, Res Inst Aerosp Engn & Technol, 76 Hanggongdaehak Ro, Goyang Si 10540, Gyeonggi Do, South Korea
[2] Korea Aerosp Univ, Sch Aerosp & Mech Engn, 76 Hanggongdaehang Ro, Goyang Si 10540, Gyeonggi Do, South Korea
来源
APPLIED SCIENCES-BASEL | 2024年 / 14卷 / 09期
基金
新加坡国家研究基金会;
关键词
hydrogen energy; liquid hydrogen; cryogenic tanks; thermodynamic model; STORAGE; AIRCRAFT; PRESSURE; PRESSURIZATION; AMMONIA; DESIGN; CELLS;
D O I
10.3390/app14093786
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
Hydrogen is used as a fuel in various fields, such as aviation, space, and automobiles, due to its high specific energy. Hydrogen can be stored as a compressed gas at high pressure and as a liquid at cryogenic temperatures. In order to keep liquid hydrogen at a cryogenic temperature, the tanks for storing liquid hydrogen are required to have insulation to prevent heat leakage. When liquid hydrogen is vaporized by heat inflow, a large pressure is generated inside the tank. Therefore, a technology capable of predicting the tank pressure is required for cryogenic liquid hydrogen tanks. In this study, a thermodynamic model was developed to predict the maximum internal pressure and pressure behavior of cryogenic liquid hydrogen fuel tanks. The developed model considers the heat inflow of the tank due to heat transfer, the phase change from liquid to gas hydrogen, and the fuel consumption rate. To verify the accuracy of the proposed model, it was compared with the analyses and experimental results in the referenced literature, and the model presented good results. A cryogenic liquid hydrogen fuel tank was simulated using the proposed model, and it was confirmed that the storage time, along with conditions such as the fuel filling ratio of liquid hydrogen and the fuel consumption rate, should be considered when designing the fuel tanks. Finally, it was confirmed that the proposed thermodynamic model can be used to sufficiently predict the internal pressure and the pressure behavior of cryogenic liquid hydrogen fuel tanks.
引用
收藏
页数:14
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