FUEL STORAGE SYSTEM

摘要

A cryogenic fuel storage system 10 for an aircraft is disclosed including a cryogenic fuel tank 22 having a first wall 23 forming a storage volume 24 capable of storing a cryogenic liquid fuel 12; an inflow system 32 capable of flowing the cryogenic liquid fuel 12 into the storage volume 24; an outflow system 30 adapted to deliver the cryogenic liquid fuel 12 from the cryogenic fuel storage system 10; and a vent system 40 capable of removing at least a portion of a gaseous fuel 19 formed from the cryogenic liquid fuel 12 in the storage volume 24.