Design, Manufacture, and Cryogenic Testing of a Linerless Composite Tank for Liquid Hydrogen
Artikel i vetenskaplig tidskrift, 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

Författare

Robin Olsson

Chalmers, Industri- och materialvetenskap, Material- och beräkningsmekanik

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

Ämneskategorier

Rymd- och flygteknik

DOI

10.1007/s10443-024-10219-y

Mer information

Senast uppdaterat

2024-03-27