An assembly is provided for an aircraft. This aircraft assembly includes a hydrogen containment vessel (70), a hydrogen storage vessel (68), a hydrogen supply channel, a cavity purge channel (106) and a plenum purge channel (86). The hydrogen containment vessel (70) includes a containment vessel wall (76). The hydrogen storage vessel (68) includes a storage vessel wall (72) and a storage cavity (74). The hydrogen storage vessel (68) is disposed within the hydrogen containment vessel (70). A containment plenum (82) is disposed between the storage vessel wall (72) and the containment vessel wall (76). The hydrogen supply channel is fluidly coupled with the storage cavity (74). The cavity purge channel (106) is fluidly coupled with the storage cavity (74). The plenum purge channel (86) is fluidly coupled with the containment plenum (82).
VENTED HYDROGEN FUEL RESERVOIR FOR AIRCRAFT ENGINE
BELÜFTETER WASSERSTOFFBRENNSTOFFBEHÄLTER FÜR FLUGZEUGTRIEBWERK
RÉSERVOIR VENTILÉ DE CARBURANT À HYDROGÈNE POUR MOTEUR D'AÉRONEF
2025-03-19
Patent
Electronic Resource
English
Vented dynamic pressure recovery module for aircraft ECS
European Patent Office | 2020
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