Disclosed is a tank 1000, 1000' comprising one or several anti-sloshing wall arrangement/s 100, 100', with a frame portion 10 and a door portion 20, wherein the frame portion 10 is fixed to a tank wall 200 of the tank, and it edges an opening O, and wherein the door portion 20 is configured to selectively close or unclose the opening O.Further disclosed is an aircraft 1 comprising such tank and at least one engine 3000, the engine 3000 being configured to be fed with fuel, in particular with liquid hydrogen, contained in the tank.
TANK WITH AT LEAST ONE ANTI-SLOSHING WALL ARRANGEMENT, AND AIRCRAFT WITH SUCH TANK
TANK MIT MINDESTENS EINER SCHWALLSCHUTZWANDANORDNUNG UND FLUGZEUG MIT SOLCH EINEM TANK
RÉSERVOIR AVEC AU MOINS UN AGENCEMENT DE PAROI ANTI-BALLOTTEMENT, ET AÉRONEF AVEC UN TEL RÉSERVOIR
30.10.2024
Patent
Elektronische Ressource
Englisch
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