In order to enlarge a tank volume of a hydrogen powered aircraft (12), the invention proposes an aircraft tank (18) for storing cryogenic H2 which is configured as a non-circular dorsal tank. Preferably, the aircraft tank (18) is configured as a conformal fuel tank fitted to an outer contour of an aircraft fuselage (10). Further, an aircraft 12 provided with such aircraft tank 18 has been described.
H2 CRYOGENIC NON CIRCULAR DORSAL TANK
KRYOGENER NICHTKREISFÖRMIGER WASSERSTOFFRÜCKENTANK
RÉSERVOIR DORSAL NON-CIRCULAIRE D'HYDROGÈNE CRYOGÉNIQUE
2025-03-12
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Cryogenic tank and aircraft comprising such cryogenic tank
European Patent Office | 2024
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