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
2017-04-12
Patent
Electronic Resource
English
Aircraft cryogenic fuel system design issues
AIAA | 1993
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