A cryogenic fuel storage system for an aircraft is disclosed including a cryogenic fuel tank having a first wall forming a storage volume capable of storing a cryogenic liquid fuel; an inflow system capable of flowing the cryogenic liquid fuel into the storage volume; an outflow system adapted to deliver the cryogenic liquid fuel from the cryogenic fuel storage system; and a vent system capable of removing at least a portion of a gaseous fuel formed from the cryogenic liquid fuel in the storage volume.
CRYOGENIC FUEL STORAGE SYSTEM FOR AN AIRCRAFT
BRENNSTOFFSPEICHERSYSTEM
SYSTÈME DE STOCKAGE DE COMBUSTIBLE CRYOGÉNIQUE POUR UN AVION
12.04.2017
Patent
Elektronische Ressource
Englisch
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