A hydrogen supply device including at least one hydrogen tank, at least one hydrogen circuit and at least one upstream container joined to the hydrogen tank, as well as at least one removable downstream container. The upstream and downstream containers are configured to occupy an assembled state, in which the upstream and downstream containers are connected, and a detached state in which the upstream and downstream containers are not joined. The hydrogen circuit has an upstream segment positioned in the upstream container, a downstream segment positioned in the downstream container, as well as a first connection system which connects the upstream and downstream segments when the upstream and downstream containers are in the assembled state. Thus, each downstream container may be uninstalled and removed from the aircraft without it being necessary to uninstall the hydrogen tank.
AÉRONEF COMPRENANT AU MOINS UN DISPOSITIF D'ALIMENTATION EN HYDROGÈNE COMPRENANT UN RÉSERVOIR D'HYDROGÈNE AINSI QUE DES ÉQUIPEMENTS RÉPARTIS DANS AU MOINS UN CONTENANT RELIÉ AU RÉSERVOIR ET AU MOINS UN CONTENANT AMOVIBLE
AIRCRAFT COMPRISING AT LEAST ONE HYDROGEN SUPPLY DEVICE COMPRISING A HYDROGEN TANK AND DEVICES DISTRIBUTED IN AT LEAST ONE CONTAINER CONNECTED TO THE TANK AND AT LEAST ONE REMOVABLE CONTAINER
LUFTFAHRZEUG MIT MINDESTENS EINER WASSERSTOFFVERSORGUNGSVORRICHTUNG MIT EINEM WASSERSTOFFSPEICHER SOWIE IN MINDESTENS EINEM SPEICHERFESTEN BEHÄLTER UND MINDESTENS EINEM ABNEHMBAREN BEHÄLTER VERTEILT ANGEORDNETEN EINRICHTUNGEN
2025-06-18
Patent
Electronic Resource
French
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