TY - GEN
T1 - Advancing
Hydrogen Storage in Aviation: Stress State of Discretely Loaded
All-Composite Double-Walled Vacuum-Insulated Cryo-Compressed Vessels
AU - Poorte, V.K.
AU - Bergsma, O.K.
AU - van Campen, J.M.J.F.
AU - Alderliesten, R.C.
PY - 2025
Y1 - 2025
N2 - Hydrogen is a promising candidate for achieving aviation sustainability, but storage aboard aircraft presents significant challenges. All-composite, double-walled, vacuum-insulated cryo-compressed storage vessels offer a potential solution by achieving high volumetric and gravimetric efficiencies. Load transfer connections between the tank's shells and the surrounding structure introduce concentrated loads in the composite shells. This work develops analytical models to characterize the stress state in composite shells under discrete in-plane loading, showing how stress concentrations decay and how laminate selection influences the decay rate. Discrepancies between the analytical and numerical models are noted, with suggestions for improving both. Additionally, the current model’s limitations due to the number of roots obtained from the governing equations are addressed by proposing additional boundary conditions. This research supports the structural and thermal analysis of composite hydrogen storage vessels, aiding the adoption of hydrogen as a sustainable aviation fuel.
AB - Hydrogen is a promising candidate for achieving aviation sustainability, but storage aboard aircraft presents significant challenges. All-composite, double-walled, vacuum-insulated cryo-compressed storage vessels offer a potential solution by achieving high volumetric and gravimetric efficiencies. Load transfer connections between the tank's shells and the surrounding structure introduce concentrated loads in the composite shells. This work develops analytical models to characterize the stress state in composite shells under discrete in-plane loading, showing how stress concentrations decay and how laminate selection influences the decay rate. Discrepancies between the analytical and numerical models are noted, with suggestions for improving both. Additionally, the current model’s limitations due to the number of roots obtained from the governing equations are addressed by proposing additional boundary conditions. This research supports the structural and thermal analysis of composite hydrogen storage vessels, aiding the adoption of hydrogen as a sustainable aviation fuel.
UR - http://www.scopus.com/inward/record.url?scp=105001388068&partnerID=8YFLogxK
U2 - 10.2514/6.2025-0621
DO - 10.2514/6.2025-0621
M3 - Conference contribution
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - Proceedings of the AIAA SCITECH 2025 Forum
T2 - AIAA SCITECH 2025 Forum
Y2 - 6 January 2025 through 10 January 2025
ER -