Print Email Facebook Twitter Structural integration of a full-composite, double-walled, vacuum-insulated, cryo-compressed hydrogen tank. Title Structural integration of a full-composite, double-walled, vacuum-insulated, cryo-compressed hydrogen tank. Author Poorte, V.K. (TU Delft Group van Campen) Bergsma, O.K. (TU Delft Group Bergsma) van Campen, J.M.J.F. (TU Delft Group van Campen) Alderliesten, R.C. (TU Delft Group Alderliesten) Date 2024 Abstract Hydrogen is being investigated as aviation fuel, with the objective to achieve an energy transition for the aviation sector. Effective storage solutions are crucial to mitigate the aerodynamic penalty caused by its low volumetric energy density. The focus of this study is the integration of a cryo-compressed vacuum-insulated storage vessel into the primary structure of aircraft, aiming to enhance structural efficiency. This is achieved by implementing analytical methods to analyse the thermo-mechanical loading of the inner and outer walls of the fuel tank. It is envisioned that the inner wall rather than the outer wall is more suitable to sustain additional loads. However, it is unclear how the cryogenic environment affects the stress state of the composite material. To reference this document use: http://resolver.tudelft.nl/uuid:2539af15-70fa-4876-9540-316a12771776 DOI https://doi.org/10.2514/6.2024-0834 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) ISBN 978-1-62410-711-5 Source Proceedings of the AIAA SCITECH 2024 Forum Event AIAA SCITECH 2024 Forum, 2024-01-08 → 2024-01-12, Orlando, United States Series AIAA SciTech Forum and Exposition, 2024 Part of collection Institutional Repository Document type conference paper Rights © 2024 V.K. Poorte, O.K. Bergsma, J.M.J.F. van Campen, R.C. Alderliesten Files PDF poorte_et_al_2024_structu ... nk_for.pdf 1.19 MB Close viewer /islandora/object/uuid:2539af15-70fa-4876-9540-316a12771776/datastream/OBJ/view