This study simulated the thermal characteristics of a liquefied hydrogen (LH) tank with varying multi-layer insulation (MLI) thickness and surrounding conditions. A transient heat conduction simulation was conducted using ANSYS Fluent software to predict the temperature distribution of the LH tank. The LH tank is composed of carbon fiber reinforced plastic (CFRP), MLI, and an Air layer for thermal insulation. A large MLI thickness delayed temperature changes inside the MLI due to its low thermal diffusivity. And then, the temperature rapidly increased near the outer wall, resulting in thermal non-uniformity. Therefore, when designing a LH tank with MLI materials, it would be necessary to optimize the design (i.e., MLI thickness) by considering structural stability issues caused by thermal non-uniformity. In addition, as the surrounding temperature increased and the convective heat transfer coefficient became higher, the enhanced heat transfer led to a higher temperature gradient within the LH tank, bringing the outer wall temperature of the LH tank closer to the environmental conditions. The results of this study will significantly contribute to establishing a comprehensive thermal database for predicting the thermal-structural behaviors, considering the thermal stress induced by the thermal distribution of LH tanks, which depends on the installation conditions and environment.

Demand for research on the use of hydrogen, an eco-friendly fuel, is rapidly increasing in accordance with global environmental problems and IMO environmental regulations in the shipbuilding and marine industry. In the case of hydrogen, similar to liquefied natural gas, it has a characteristic that its volume decreases hundreds of times during phase transformation from gas to liquid, so it must be stored in a tank in the form of liquefied hydrogen for transport efficiency. The material of the liquid hydrogen tank is selected in consideration of mechanical properties and hydrogen embrittlement at cryogenic temperatures. In this study, welding research was conducted on STS316L material, which was most commonly used in the space industry. In this study, flux cored arc welding was performed under 4 welding conditions to derive the optimal welding conditions for STS316L material, and then mechanical properties of the welded part were compared and analyzed.

본 논문은 슬로싱 상태에 놓인 포화 상태 액체수소탱크에서 열 유속 및 BOG(Boil-off gas)의 경향을 다루고 있다. 특히, 액체-기체 간의 침투 및 혼합에 의한 열 교환에 관심을 두었다. 먼저, VOF(Volume of fluid)와 Eulerian 기반의 다상 유동모델로 모형 슬로싱 실험 을 모사하여 압력을 예측하고 계측된 값과 비교하였다. 자유 수면 및 충격 압력 실험 결과와 해석 결과를 비교하였으며, 유체의 속도 예측에서 정확할 수 있음을 간접적으로 증명하였다. 그리고 2차원의 Type-C 원통형 수소탱크를 대상으로 다상열유동해석을 수행하 였다. 이때 포화상태에 놓인 액체 및 기체수소를 가정하고, 해석을 통해 각 상간의 혼합에 의한 열 교환의 수준을 확인하고자 하였다. 단, 상간의 열 교환만을 관심으로 두고 있었으므로 질량전달 및 기화모델은 해석에서 제외하였다. 최종적으로 상의 혼합으로 인해 액 체수소로 유입되는 열 유속의 기여도에 대하여 정리하였다. 또한 액체수소로 유입되는 열 유속과 집중 질량 기반의 간이식을 통해 BOG 발생량 및 경향을 예측하고 분석하였다.