Disclosed is an aircraft fuel storage system comprising: a fuel tank comprising a chamber for storing fuel, the chamber comprising a first side, a second side, and a base connecting the first side to the second side; a collector; and a first conduit and a second conduit, each of the first and second conduits fluidically coupling the chamber to the collector so that fuel is freely passable from the chamber to the collector via the respective first and second conduits; wherein the first and second conduits open into the chamber at respective first and second conduit openings, wherein the first conduit opening is nearer to the first side than the second conduit opening is to the first side; and wherein the second conduit comprises a second conduit lock portion that is nearer to the first side than the second conduit opening is to the first side. Also disclosed is an aircraft comprising the aircraft fuel storage system.
AIRCRAFT FUEL STORAGE SYSTEM
KRAFTSTOFFSPEICHERSYSTEM FÜR FLUGZEUGE
SYSTÈME DE STOCKAGE DE CARBURANT D'AÉRONEF
2024-07-24
Patent
Electronic Resource
English