Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank

As environmental pollution has become a global concern, regulations on carbon emissions from maritime activities are being implemented, and interest in using renewable energy as fuel for ships is growing. Hydrogen, which does not release carbon dioxide and has a high energy density, can potentially...

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Published in:Journal of Marine Science and Engineering
Main Authors: Seung-Joo Cha, Hyun-Jin Tak, Byeong-Kwan Hwang, Jong-Pil Lee, Jeong-Hyeon Kim, Jae-Myung Lee
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Subjects:
Online Access:https://www.mdpi.com/2077-1312/13/4/730
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author Seung-Joo Cha
Hyun-Jin Tak
Byeong-Kwan Hwang
Jong-Pil Lee
Jeong-Hyeon Kim
Jae-Myung Lee
author_facet Seung-Joo Cha
Hyun-Jin Tak
Byeong-Kwan Hwang
Jong-Pil Lee
Jeong-Hyeon Kim
Jae-Myung Lee
author_sort Seung-Joo Cha
collection DOAJ
container_title Journal of Marine Science and Engineering
description As environmental pollution has become a global concern, regulations on carbon emissions from maritime activities are being implemented, and interest in using renewable energy as fuel for ships is growing. Hydrogen, which does not release carbon dioxide and has a high energy density, can potentially replace fossil fuels as a renewable energy source. Notably, storage of hydrogen in a liquid state is considered the most efficient. In this study, a 0.7 m<sup>3</sup> liquid hydrogen fuel tank suitable for small vessels was designed, and a structural analysis was conducted to assess its structural integrity. The extremely low liquefaction temperature of hydrogen at −253 °C and the need for spatial efficiency in liquid hydrogen fuel tanks make vacuum insulation essential to minimize the heat transfer due to convection. A composite insulation system of sprayed-on foam insulation (SOFI) and multilayer insulation (MLI) was applied in the vacuum annular space between the inner and outer shells, and a tube-shaped supporter made of a G-11 cryogenic (CR) material with low thermal conductivity and high strength was employed. The material selected for the inner and outer layers of the tank was STS 316L, which exhibits sufficient ductility and strength at cryogenic temperatures and has low sensitivity to hydrogen embrittlement. The insulation performance was quantitatively assessed by calculating the boil-off rate (BOR) of the designed fuel tank. Structural integrity evaluations were conducted for nine load cases using heat transfer and structural analyses in accordance with the IGF code.
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spelling doaj-art-deee5b0a876f404ea4bca457a7bdcfc12025-08-20T01:21:01ZengMDPI AGJournal of Marine Science and Engineering2077-13122025-04-0113473010.3390/jmse13040730Structural Assessment of Independent Type-C Liquid Hydrogen Fuel TankSeung-Joo Cha0Hyun-Jin Tak1Byeong-Kwan Hwang2Jong-Pil Lee3Jeong-Hyeon Kim4Jae-Myung Lee5Department of Naval Architecture & Ocean Engineering, Pusan National University, Busan 46241, Republic of KoreaDepartment of Naval Architecture & Ocean Engineering, Pusan National University, Busan 46241, Republic of KoreaDepartment of Naval Architecture & Ocean Engineering, Pusan National University, Busan 46241, Republic of KoreaSamwoo MCP Co., Ltd., Busan 46730, Republic of KoreaHydrogen Ship Technology Center, Pusan National University, Busan 46241, Republic of KoreaDepartment of Naval Architecture & Ocean Engineering, Pusan National University, Busan 46241, Republic of KoreaAs environmental pollution has become a global concern, regulations on carbon emissions from maritime activities are being implemented, and interest in using renewable energy as fuel for ships is growing. Hydrogen, which does not release carbon dioxide and has a high energy density, can potentially replace fossil fuels as a renewable energy source. Notably, storage of hydrogen in a liquid state is considered the most efficient. In this study, a 0.7 m<sup>3</sup> liquid hydrogen fuel tank suitable for small vessels was designed, and a structural analysis was conducted to assess its structural integrity. The extremely low liquefaction temperature of hydrogen at −253 °C and the need for spatial efficiency in liquid hydrogen fuel tanks make vacuum insulation essential to minimize the heat transfer due to convection. A composite insulation system of sprayed-on foam insulation (SOFI) and multilayer insulation (MLI) was applied in the vacuum annular space between the inner and outer shells, and a tube-shaped supporter made of a G-11 cryogenic (CR) material with low thermal conductivity and high strength was employed. The material selected for the inner and outer layers of the tank was STS 316L, which exhibits sufficient ductility and strength at cryogenic temperatures and has low sensitivity to hydrogen embrittlement. The insulation performance was quantitatively assessed by calculating the boil-off rate (BOR) of the designed fuel tank. Structural integrity evaluations were conducted for nine load cases using heat transfer and structural analyses in accordance with the IGF code.https://www.mdpi.com/2077-1312/13/4/730liquid hydrogen fuel tankthermo-structural analysisboil-off rate
spellingShingle Seung-Joo Cha
Hyun-Jin Tak
Byeong-Kwan Hwang
Jong-Pil Lee
Jeong-Hyeon Kim
Jae-Myung Lee
Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
liquid hydrogen fuel tank
thermo-structural analysis
boil-off rate
title Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
title_full Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
title_fullStr Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
title_full_unstemmed Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
title_short Structural Assessment of Independent Type-C Liquid Hydrogen Fuel Tank
title_sort structural assessment of independent type c liquid hydrogen fuel tank
topic liquid hydrogen fuel tank
thermo-structural analysis
boil-off rate
url https://www.mdpi.com/2077-1312/13/4/730
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