Design, Manufacture, and Cryogenic Testing of a Linerless Composite Tank for Liquid Hydrogen
Journal article, 2024

This paper describes design, manufacture, and testing of a linerless composite vessel for liquid hydrogen, having 0.3 m diameter and 0.9 m length. The vessel consists of a composite cylinder manufactured by wet filament winding of thin-ply composite bands, bonded to titanium end caps produced by additive manufacturing. The aim was to demonstrate the linerless design concept with a thin-ply composite for the cylinder. The investigation is limited to the internal pressure vessel, while real cryogenic tanks also involve an outer vessel containing vacuum for thermal insulation. Thermal stresses dominate during normal operation (4 bar) and the layup was selected for equal hoop strains in the composite cylinder and end caps during filling with liquid hydrogen. Two vessels were tested in 20 cycles, by filling and emptying with liquid nitrogen to 4 bar, without signs of damage or leakage. Subsequently, one vessel was tested until burst at almost 30 bar.

Burst test

Filament winding

Thin plies

Liquid hydrogen

Cryogenic

Composite tank

Author

Robin Olsson

Chalmers, Industrial and Materials Science, Material and Computational Mechanics

RISE Research Institutes of Sweden

Christopher Cameron

RISE Research Institutes of Sweden

Florence Moreau

Oxeon AB

Erik Marklund

RISE Research Institutes of Sweden

Matthias Merzkirch

RISE Research Institutes of Sweden

Jocke Pettersson

RISE Research Institutes of Sweden

Applied Composite Materials

0929-189X (ISSN) 1573-4897 (eISSN)

Vol. In Press

Subject Categories

Aerospace Engineering

DOI

10.1007/s10443-024-10219-y

More information

Latest update

3/27/2024