A tank comprising one or several anti-sloshing wall arrangements, with a frame portion and a door portion wherein the frame portion is fixed to a tank wall of the tank, and it edges an opening, and wherein the door portion is configured to selectively close or unclose the opening. Also an aircraft comprising such tank and at least one engine, the engine 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
2024-10-31
Patent
Electronic Resource
English
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