An assembly is provided for an aircraft. This aircraft assembly includes a hydrogen containment vessel, a hydrogen storage vessel, a hydrogen supply channel, a cavity purge channel and a plenum purge channel. The hydrogen containment vessel includes a containment vessel wall. The hydrogen storage vessel includes a storage vessel wall and a storage cavity. The hydrogen storage vessel is disposed within the hydrogen containment vessel. A containment plenum is disposed between the storage vessel wall and the containment vessel wall. The hydrogen supply channel is fluidly coupled with the storage cavity. The cavity purge channel is fluidly coupled with the storage cavity. The plenum purge channel is fluidly coupled with the containment plenum.
VENTED HYDROGEN FUEL RESERVOIR FOR AIRCRAFT ENGINE
2025-03-13
Patent
Electronic Resource
English
Vented dynamic pressure recovery module for aircraft ECS
European Patent Office | 2020
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